
This is an alphabetical list of
aircraft engine
An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Most aircraft engines are either piston engines or gas turbines, although a few have been rocket powered and in recent years ma ...
s by manufacturer.
0–9
2si
*
2si 215
The 2si 215 is a family of single-cylinder, fan-cooled, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft.Cuyuna Development Company: ''Cuyuna Engines'', Cuyuna Development Company, undated
The basic engin ...
*
2si 230
The 2si 230 is a family of single-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-2 Cybair Limited Publishing, 2001.
T ...
*
2si 430
The Cuyuna 430 and Cuyuna 340 are a family of two-stroke, twin-cylinder piston snowmobile engines that were redesigned to serve as ultralight aircraft powerplants.Cuyuna Development Company: ''Cuyuna Engines'', Cuyuna Development Company, undat ...
*
2si 460
The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-2 Cybair Limited Publishing, 200 ...
*
2si 500
The 2si 540 and 2si 500 are a family of in-line twin-cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-2 Cyba ...
*
2si 540
The 2si 540 and 2si 500 are a family of in-line twin-cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-2 Cyba ...
*
2si 690
The 2si 690 is a family of in-line three cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-3 Cybair Limited P ...
3W
''Source: RMV''
*3W 106iB2
*3W-110
*3W-112
*3W-170
*3W-210
*3W-220
A
Abadal (Francisco Serramalera Abadal)
*Abadal Y-12 350/400 hp
[
]
ABC
''Source: Lumsden.''
* ABC 8 hp
The ABC 8 hp is an 8 hp (6 kW) two-cylinder aero engine designed by the noted British engineer Granville Bradshaw for use in ultralight aircraft. The engine was derived from a specially tuned motorcycle unit and was built by ABC ...
* ABC 30hp V-4
* ABC 45hp V-6 [
* ABC 60hp V-8 ][
* ABC 85hp V-6 ][
* ABC 100hp V-8 ][
* ABC 115 hp][
* ABC 170hp V-12 ][
* ABC 225hp V-16 ][
*]ABC Dragonfly
The ABC Dragonfly was a British radial engine developed towards the end of the First World War. It was expected to deliver excellent performance for the time and was ordered in very large numbers. It proved, however, to be extremely unreliable ...
*ABC Gadfly
*ABC Gnat
The ABC Gnat was a 45 hp (34 kW) two-cylinder aero engine designed by British engineer Granville Bradshaw for use in light aircraft. The Gnat was built by ABC Motors, first running in 1916, production ceased in December 1918. 17 eng ...
*ABC Hornet
The ABC Hornet was an 80 hp (90 kW) four-cylinder aero engine designed in the late 1920s by the noted British engineer Granville Bradshaw for use in light aircraft. The Hornet was effectively a double Scorpion and was built by ABC ...
*ABC Mosquito
The ABC Mosquito was a 120 hp (90 kW) six-cylinder radial aero engine designed by the noted British engineer Granville Bradshaw for use in light aircraft. The single Mosquito engine was built by ABC Motors, first running in 1916. It i ...
*ABC Scorpion
The ABC Scorpion is a 30 hp (22 kW) two-cylinder Aircraft engine, aero engine designed by British engineer Granville Bradshaw for use in light aircraft. The engine was built by ABC Motors, ABC Motors Limited and first ran in 1921.Gun ...
*ABC Wasp
The ABC Wasp was an experimental 170 hp (127 kW) seven-cylinder radial engine designed by the noted British engineer Granville Bradshaw, and primarily built by ABC Motors, ABC Motors Limited. An order for twelve experimental ABC Wasp ...
*ABC type 10 APU
*ABC type 11 APU[
]
ABECO
''Source: RMV''
*ABECO GEM
Aberg
''Source: RMV''
*Type Sklenar
ABLE
''Source: RMV'', Able Experimental Aircraft Engine Co. (Able Experimental Aircraft Engine Co., Altimizer, Hoverhawk (US))
*ABLE 2275
*ABLE 2500
*ABLE VW x 2 Geared Drive
Accurate Automation Corp
*Accurate Automation AT-1500
*Accurate Automation AT-1700
Ace
(Ace American Engr Corp, Horace Keane Aeroplane Co, North Beach, Long Island NY.)
* Ace 1919 40hp
ACE
(American Cirrus Engine Inc)
''Source: RMV''[
*]ACE Cirrus
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and ...
*ACE LA-1 19?? (ATC 31) = 140 hp 7RA. Evolved into Jacobs LA-1.
*ACE Mk III
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
1929 (ATC 30, 44) = 90 hp 310ci 4LAI; (44) for 110 hp supercharged model.
*ACE Mk III Hi-Drive
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
*ACE Ensign
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
ACT
(Aircraft Cylinder and Turbine Co)
''Source: RMV''
* ACT Super 600
Adams
''Source: RMV''
*Adams (UK) 4 Cylinder in-line of 140 HP
*Adams (UK) 8 V
Adams-Dorman
''Source: RMV''
*Adams-Dorman 60/80 HP
Adams-Farwell
The Adams Company, Dubuque, Iowa / F.O. Farwell, engines for gyrocopters
*Adams-Farwell 36 hp 5-cyl rotary engine [
*Adams-Farwell 50 HP][
*Adams-Farwell 55hp 5-cyl rotary ][
*Adams-Farwell 63hp 5-cyl rotary ][
*Adams-Farwell 72hp 5-cyl rotary ][
*Adams-Farwell 280hp 6cyl double rotary ][
*Adams-Farwell 6-cyl double rotary ]
*Adams-Farwell 10-cyl double rotary
*Adams-Farwell 14-cyl double rotary
*Adams-Farwell 18-cyl double rotary
*Adams-Farwell KM 11[
]
ADC
ADC
ADC may refer to:
Science and medicine
* ADC (gene), a human gene
* AIDS dementia complex, neurological disorder associated with HIV and AIDS
* Allyl diglycol carbonate or CR-39, a polymer
* Antibody-drug conjugate, a type of anticancer treatment ...
(from "Aircraft Disposal Company") bought 35,000 war-surplus engines in 1920. Initially produced engines from Renault 70 hp
The Renault 70 hp or Type WB was a French V-8 aero engine that first ran circa 1907. It was also manufactured under license by Renault Limited of West Brompton, London between August 1914 and December 1918, three other companies, including ...
spares.
*ADC Airdisco
The ADC Airdisco is a British V-8 aero engine that first ran in 1925.
Design and development
The 'Airdisco' was developed from the French Renault 70 hp aero engine by Frank Halford of the Aircraft Disposal Company, the main difference being ...
*ADC Cirrus
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
*ADC Nimbus
The ADC Nimbus was a British Inline engine (aviation), inline Aircraft engine, aero engine that first ran in 1926. The Nimbus was developed from the Siddeley Puma aero engine by Frank Halford of the ADC Aircraft, Aircraft Disposal Company, the ...
, development of Siddeley Puma
The Siddeley Puma was a British aero engine developed towards the end of World War I and produced by Siddeley-Deasy. The first engines left the production lines of Siddeley-Deasy in Coventry in August 1917, production continued until December ...
*ADC Airsix, air-cooled version of Nimbus. Not put into use
*ADC BR2
*ADC Viper
*ADC Airdisco-Renault
Adept-Airmotive
''Source: RMV''
*Adept 280 N
*Adept 300 R
*Adept 320 T
The Adept Airmotive 320T is a liquid-cooled V-6 engine for aviation use.
Specifications (320T)
See also
References
{{Reflist
External links
Adept Airmotive Corporate Video
2010s aircraft piston engines ...
Ader
''Source: RMV''
*Ader Eole engine (Vapour)
*Ader Avion engine (Vapour)
*Ader 2V
*Ader 4V
Adler
''Source: RMV''
*Adler 50hp 4-cyl in-line
*Adler 100hp 6-cyl in-line
*Adler 222hp V-8
Adorjan & Dedics
''Source: RMV''
*Adorjan & Dedics 2V
Advance Engines
''Source: RMV''
*Advance 4V, 20/25 HP
Advanced Engine Design
''Source: RMV''
*Advanced Engine Design Spitfire 1 Cylinder
*Advanced Engine Design Spitfire 2 Cylinder
*Advanced Engine Design Spitfire 3 Cylinder
*Advanced Engine Design Spitfire 4 Cylinder
*Advanced Engine Design K2-1000
*Advanced Engine Design 110 HP (BMW Conversion)
*Advanced Engine Design 220 LC
*Advanced Engine Design 440 LC
*Advanced Engine Design 660 LC
*Advanced Engine Design 880 LC
*Advanced Engine Design 530 (Kawasaki Conversion)
AEADC
(Aircraft Engine & Accessory Development Corporation)
''Source: RMV''
*AEADC Gryphon M[
*AEADC Gryphon N][
*AEADC O-510 (Gryphon M)][
*AEADC O-810 (Gryphon N)][
]
AEC
''Source: RMV''
*AEC Keane
Aeolus Flugmotor
''Source: RMV''
Aerien CC
''Source: RMV''
*Aerien 20/25 HP
*Aerien 30 HP
Aermacchi
''Source: RMV''
*Aermacchi MB-2
Aero & Marine
*Aero & Marine 50 HP
Aero Adventure
''Source: RMV''
*Aero Adventure GFL-2000
AeroConversions
* AeroConversions AeroVee 2180
Aero Development
''Source: RMV''
(See SPEER)
Aero Engines Ltd.
(formerly William Douglas (Bristol) Ltd.)
*Aero Engines Dryad
*Aero Engines Pixie
*Aero Engines Sprite
*Aero Engines inverted V-4
*Aero Engines inverted V-6
* Douglas 750cc
Aero Motion
''Source: RMV''
*Aero Motion 0-100
*Aero Motion 0-101
Aero Motors
''Source: RMV''
*Aero Motors Aerobat 150 HP
Aero Pixie
''Source: RMV''
*Aero Pixie 153 cc, 2T
Aero Prag
''Source: RMV''
*Aeroprag KT-422
*Aeroprag AP-45
*Aeroprag TP-422
Aero Products
(Aero Products Aeronautical Products Corp, Naugatuck CT.)
''Source: RMV''
*Aero Products Scorpion 100 HP
Aero Sled
''Source: RMV''
*Aero Sled Twin Flat, 20 HP
Aero Sport International
''Source: RMV''
*Aero Sport International Wade Aero (WANKEL) 2 Types
AeroTwin Motors Corporation
*AeroTwin AT972T
The AeroTwin AT972T is an American aircraft engine, designed and produced by the AeroTwin Motors Corporation, a subsidiary of the AirScooter Corporation of Henderson, Nevada for use in ultralight aircraft, in particular their AirScooter helic ...
Aerojet
Aerojet
Aerojet was an American rocket and missile propulsion manufacturer based primarily in Rancho Cordova, California, with divisions in Redmond, Washington, Orange and Gainesville in Virginia, and Camden, Arkansas. Aerojet was owned by GenCorp ...
produced rocket engines for missiles. It merged with Pratt & Whitney Rocketdyne
Pratt & Whitney Rocketdyne (PWR) was an American company that designed and produced rocket engines that use liquid propellants. It was a division of Pratt & Whitney, a fully owned subsidiary of United Technologies Corporation. It was headquarter ...
.
*Aerojet LR1 (Aerojet 25AL-1000)
*Aerojet LR3 (Aerojet 25ALD-1000)
*Aerojet LR5 (Aerojet X40ALD-3000)
*Aerojet LR7 (Aerojet ZCALT-6000)
*Aerojet LR9 (Aerojet X4AL-1000)
*Aerojet LR13 (Aerojet X60ALD-4000 / Aerojet 4.104a / Aerojet 4.103a)
*Aerojet LR15 (Aerojet XCNLT-1500)
*Aerojet LR45 (Aerojet AJ24-1)
*Aerojet LR49
*Aerojet LR51
*Aerojet LR53
*Aerojet LR59 (CIM-99 Bomarc booster engine)
*Aerojet LR87
The LR87 was an American liquid-propellant rocket engine used on the first stages of Titan intercontinental ballistic missiles and launch vehicles. Composed of twin motors with separate combustion chambers and turbopump machinery, it is cons ...
*Aerojet LR91
The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles. While the original version - the LR91-3 - ran on RP-1/LOX (as did the companion LR ...
*Aerojet-General SR19 (Aerojet Minuteman 2nd stage motor)
*Aerojet 1KS-2800A
*Aerojet 2KS-11000 (X102C1)
*Aerojet 2KS-33000A
*Aerojet 2.2KS-33000[
*Aerojet 2.5KS-18000 (X103C1)]
*Aerojet 5KS-4500[
*Aerojet 12AS-250 Junior][
*Aerojet 14AS-1000 (D-5) – RATO unit]
*Aerojet 15KS-1000 RATO unit
*Aerojet 15NS-250
*Aerojet 30AS-1000C – RATO unit
*Aerojet 2.2KS-11000
*Aerojet AJ10
The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III. Variants were and are used as the ser ...
*Aerojet AJ-260
The Aerojet 260 was an experimental solid rocket motor constructed and tested in the mid-1960s by Aerojet for NASA.
History
In the 1960s the 260 was initially designed to test the feasibility of solid rocket motors for space exploration, includ ...
– largest solid-rocket motor ever built
*Aerojet M-1
The Aerojet M-1 was the largest and most powerful liquid-hydrogen-fueled liquid-fuel rocket engine to be designed and component-tested. It was originally developed during the 1950s by the US Air Force. The M-1 offered a baseline thrust of 6.67 ...
*Aerojet Hawk motor (for Hawk SAM)
*Aerojet Polaris motor
*Aerojet Senior
Aeromarine Company
''Source: RMV''
*Aeromarine Company D5-1 (Pulse-Jet)
Aeromarine
*Aeromarine AL
*Aeromarine NAL
*Aeromarine S
*Aeromarine S-12
*Aeromarine AR-3[
**Aeromarine AR-3-40][
*Aeromarine AR-5][
*Aeromarine AR-7]
*Aeromarine AL-24
*Aeromarine B-9
*Aeromarine B-45
The Aeromarine B-45 is an aircraft engine built by the Aeromarine Plane and Motor Company
The Aeromarine Plane and Motor Company was an early American aircraft manufacturer founded by Inglis M. Upperçu which operated from 1914 to 1930. From 192 ...
*Aeromarine B-90
The Aeromarine B-90 is an aircraft engine built by the Aeromarine Plane and Motor Company
The Aeromarine Plane and Motor Company was an early American aircraft manufacturer founded by Inglis M. Upperçu which operated from 1914 to 1930. From 19 ...
*Aeromarine D-12 150 hp [
*]Aeromarine K-6
The Aeromarine K-6 is an aircraft engine built by the Aeromarine Plane and Motor Company in 1915. It is an Aeromarine 90hp
The Aeromarine 90 hp was the first aircraft motor built by the Aeromarine Plane and Motor Company in 1914. In tha ...
*Aeromarine L-6 130 hp
**Aeromarine L-6-D (direct drive)
**Aeromarine L-6-G (geared)[
*Aeromarine L-8 192 hp ][
*Aeromarine RAD][
*Aeromarine T-6][
*Aeromarine U-6][
**Aeromarine U-6-D]
*Aeromarine U-8
**Aeromarine U-8-873
**Aeromarine U-8D[
*Aeromarine 85hp 1914][
*]Aeromarine 90hp
The Aeromarine 90 hp was the first aircraft motor built by the Aeromarine Plane and Motor Company in 1914. In that year, Aeromarine had acquired the patents and manufacturing rights to the aircraft and engines of the Boland brothers. Alth ...
*Aeromarine 100hp V-8 [
]
Aeromax
''Source: RMV''
*Aeromax 100 I-F-B
*Aeromax 100 L-D
Aeromotion
''See: AMI''
Aeromotor
(Detroit Aeromotor. Const. Co)
''Source: RMV''
*Aeromotor 30hp 4-cyl in-line
*Aeromotor 75hp 6-cyl in-line
Aeronamic
''Source: RMV''
*Aeronamic ATS
Aeronautical Engineering Co.
''Source: RMV''
*Aeronautical Engineering 9-cyl radial 200 HP
Aeronca
*Aeronca E-107
The Aeronca E-107 was one of the first low-cost reliable engines of the post-World War I era.
Design and development
The E-107A was a production aviation flathead engine designed to replace a Morehouse engine on the first prototype of the Aero ...
(O-107)
*Aeronca E-113
The E-113 was a small flat-twin piston engine developed by Aeronca for use in some of their light aircraft. It was an overhead valve development of the flathead configuration E-107.
Design and development
Originally fitted with a single igniti ...
(O-113)
Aeroplane Motors Company
(Aeroplane Motors)
''Source: RMV''
*Aeroplane 59hp V-8
Aeroprotech
''Source: RMV''
*Aeroprotech VW 2.3
Aerosila
''Source: RMV''
*Aerosila TA-4 FE
*Aerosila 6 A/U
*Aerosila 8 N/K
*Aerosila 12
*Aerosila 12-60
*Aerosila 14 (-032,-130,-35)
*Aerosila 18-100 (-200)
*GTTP-300
Aerosport
*Aerosport-Rockwell LB600 __NOTOC__
The Aerosport-Rockwell LB600 was a two-cylinder, two-stroke, air-cooled, horizontally opposed engine intended to power ultralights. It was developed in partnership by Aerosport and Rockwell International, based on a Rockwell-designed JLO ...
Aerostar
''Source: RMV''
* Aerostar M14P
* Aerostar M14V-26
Aerotech engines
''Source: RMV''
*Aerotech 2 Cylinder 2T
Aerotech-PL
''Source: RMV''
*Aerotech-PL EA81, Subaru conversion
*Aerotech-PL VW conversion
*Aerotech-PL BMW conversion
*Aerotech-PL Suzuki conversion
*Aerotech-PL Guzzi conversion
Aerotechnik
''Source: RMV''
*Aerotechnik Tatra-100
*Aerotechnik Tatra-102
*Aerotechnik Hirth (Lic)
*Aerotechnik Mikron
The Walter Mikron is a four-cylinder, air-cooled, inverted straight engine for aircraft.
Development
Developed in Czechoslovakia in the early 1930s, the engine saw limited use in late 1930s and early 1950s. In the 1980s an initial batch of engi ...
(Lic)
*Aerotechnik Tatra-714 (VW)
Aerotek
''Source: RMV''
*Aerotek Mazda RX-7 (conversion)
AES
(See Rev-Air)
Affordable Turbine Power
''Source: RMV''
*Affordable Turbine Power Model 6.5
AFR
''Source: RMV''
*AFR BMW Conversion
*AFR R 100 70/80 hp
*AFR R 1100D 90/100 hp
*AFR R 1100S 98 hp
*AFR R 1150RT 95 hp
*AFR R 1200GS 100 hp
Agilis
(Agilis Engines)
''Sources: RMV''
*Agilis TF-800
*Agilis TF-1000
*Agilis TF-1200
*Agilis TF-1400
*Agilis TF-1500
*Agilis TJ-60 (MT-60)
*Agilis TJ-75
*Agilis TJ-80
*Agilis TJ-400
Agusta
*Agusta GA.40
The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.
Specifications
Applications
...
*Agusta GA.70
The Agusta GA.70 was a four-cylinder, air-cooled, horizontally opposed engine developed in Italy for light aircraft and helicopter use. The GA.70/V featured a bottom sump for vertical applications and was rated at . It was produced in the 1950s an ...
*Agusta GA.140 __NOTOC__
The Agusta GA.140/V is a 4-cylinder, air-cooled, horizontally opposed engine mounted vertically, developed in Italy for helicopter use and produced from 1962 to 1969.
Specifications (G.A.140/V)
Applications
* Agusta A.104
The Agust ...
*Agusta A.270
*Turbomeca-Agusta TA.230
The Turbomeca Astazou is a highly successful series of turboprop and turboshaft engines, first run in 1957. The original version weighed and developed at 40,000 rpm. It was admitted for aviation service on May 29, 1961, after a 150-hour test ru ...
Ahrbecker Son and Hankers
''Source: RMV''
*Ahrbecker Son and Hankers 10 HP
*Ahrbecker Son and Hankers 20 HP
*Ahrbecker Son and Hankers 1 Cylinder – vapor
AIC
(Aviation Ind. China. See Catic and Carec)
Aichi
''Source:''Gunston 1989 except where noted.
*Aichi AC-1
__NOTOC__
The Aichi AC-1 was an experimental nine-cylinder air-cooled radial engine. In 1929, it was used to power the newly designed Aichi AB-2, a catapult-launched reconnaissance seaplane.
The AB-2 with its AC-1 engine is noted for being the ...
*Aichi Atsuta
The Aichi AE1A Atsuta (Japanese: or ) was a Japanese licensed version of the German Daimler-Benz DB 601A 12-cylinder liquid-cooled inverted-vee aircraft engine. The Atsuta powered only two models of Imperial Japanese Navy Air Service (IJNAS) air ...
(Atsuta 31) – Licence-builtDaimler-Benz DB 601
The Daimler-Benz DB 601 was a German aircraft engine built during World War II. It was a liquid-cooled inverted V12, and powered the Messerschmitt Bf 109, Messerschmitt Bf 110, and many others. Approximately 19,000 601's were produced befo ...
A for IJN
**Aichi AE1A (Atsuta 21)
**Aichi AE1P (Atsuta 32)
*Aichi Ha-70
The Aichi Ha-70 was a compound engine composed of two 1,700 hp 12-cylinder liquid-cooled inverted V-12 Aichi Atsuta aircraft engines mounted to a common gearbox. The only aircraft powered by the Ha-70 was the Yokosuka R2Y, an Imperial Japane ...
(Coupled Atsuta 30s)
AICTA
(AICTA Design Work, Prague, Czech Republic)
*AICTA LMD 416-00R
The AICTA LMD 416-00R is a Czech aircraft engine, that was designed and produced by AICTA Design Work of Prague for use in light aircraft.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 256-257. Flying P ...
Aile Volante
*Aile Volante C.C.2[
*Aile Volante C.C.4][
]
Air Repair Incorporated
''Source: RMV''
(Jacobs Licence)
*Air Repair Incorporated L-4
The Jacobs R-755 (company designation L-4) is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States by the Jacobs Aircraft Engine Company.
Design and development
The R-755 was first run in 1933 and was stil ...
*Air Repair Incorporated L-5
The Jacobs R-830 or L-5 is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States, production started in 1935.Gunston 1989, p.85.
Design and development
The R-830 was effectively an enlargement of the R-755 ...
*Air Repair Incorporated L-6
The Jacobs R-915 or Jacobs L-6 is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States, production started in 1936.
Design and development
The R-915 was effectively an enlargement of the R-755 with strengt ...
(Jacobs-Page Licence)
*Air Repair Incorporated R755
The Jacobs R-755 (company designation L-4) is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States by the Jacobs Aircraft Engine Company.
Design and development
The R-755 was first run in 1933 and was stil ...
Air Ryder
''Source: RMV''
*Air Ryder Subaru EA-81 (Conversion)
Air Technical Arsenal
''Source: RMV''
*Air Technical Arsenal TSU-11
*Air Technical Arsenal TR-30
Air-Craft Engine Corp
''Source: RMV''
*Air-Craft Engine Corp LA-1
Aircat
(Detroit Aircraft Eng. Corp.)
''Source: RMV''
*Aircat Radial 5 cylinders
Aircooled Motors
''See: Franklin
Franklin may refer to:
People
* Franklin (given name)
* Franklin (surname)
* Franklin (class), a member of a historical English social class
Places Australia
* Franklin, Tasmania, a township
* Division of Franklin, federal electoral di ...
''
Aircraft Engine Co
(Aircraft Engine Co Inc, Oakland, CA)
* Aircraft 1911 80hp
Aircraft & Ind. Motor Corp
(See Schubert)
AiResearch
''See: Garrett Garrett may refer to:
Places
;United States
* Garrett, Illinois
* Garrett, Indiana
* Garrett, Kentucky (multiple places)
** Garrett, Floyd County, Kentucky, an unincorporated community
** Garrett, Meade County, Kentucky, an unincorporated communi ...
, Allied Signal
AlliedSignal was an American aerospace, automotive and engineering company created through the 1985 merger of Allied Corp. and Signal Companies. It subsequently purchased Honeywell for $14.8 billion in 1999, and thereafter adopted the Honeywell ...
and Honeywell
Honeywell International Inc. is an American publicly traded, multinational conglomerate corporation headquartered in Charlotte, North Carolina. It primarily operates in four areas of business: aerospace, building technologies, performance ma ...
''
Airex
*Airex Rx2
*Airex Rx10
Airmotive-Perito
:''See: Adept-Airmotive''
Airship Aircraft Engine Company
*Airship A-Tech 100 Diesel
Airtrike
(AirTrike GmbH i.L., Berlin, Germany)
*Airtrike 850ti
The Airtrike 850ti is a German aircraft engine, that was designed and produced by Airtrike of Berlin for use in ultralight aircraft and in particular their Airtrike Eagle 5 design.Tacke, Willi; Marino Boric; et al: ''World Directory of Light A ...
AISA
''Source: RMV''
*Ramjet
A ramjet, or athodyd (aero thermodynamic duct), is a form of airbreathing jet engine that uses the forward motion of the engine to produce thrust. Since it produces no thrust when stationary (no ram air) ramjet-powered vehicles require an a ...
on rotor
Aixro
''Source: RMV''
*Aixro XF-40
The Aixro XF-40 (or XF40) is a German aircraft engine, designed and produced by Aixro of Aachen for use in ultralight aircraft.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 256-257. Flying Pages Europ ...
*Aixro XH-40
*Aixro XP-40
*Aixro XR-30
*Aixro XR-40
*Aixro XR-50
Ajax
''Source: RMV''
*Ajax 7-cyl rotary
*Ajax 6-cyl radial (2 rows of 3 cyls.), 80 HP
Akkerman
*Akkerman Model 235 30 HP, special fuel
Akron
*Funk E200
*Funk E4L
Albatross
(Albatross Co Detroit)
*Albatross 50hp 6-cyl radial
*Albatross 100hp 6-cyl radial
Aldasoro
*Aldasoro aero engine
Alexander
*Alexander 4-cyl
*Alexanderradial 5-cyl
Alfa Romeo
''Societa per Azioni Alfa Romeo''
*Romeo 600hp V-12[
*Alfa Romeo V-6 diesel]
*Alfa Romeo V-12 diesel
*Alfa Romeo D2
The Alfa Romeo D2 was a nine-cylinder radial engine for aircraft use produced in Italy. It was typically rated between 240 and 270 hp.
The engine was designed by Vittorio Jano, 600 units were produced between 1931 and 1934. This engine was al ...
*Alfa Romeo 100 or RA.1100
*Alfa Romeo 101 or RA.1101
* Alfa Romeo 110/111
* Alfa Romeo 115/116
*Alfa Romeo 121
The Alfa Romeo 121 was an eight-cylinder, air-cooled, inverted V engine for aircraft use produced in Italy. It was typically rated at .
Variants
;121 R.C.14:
;121 R.C.20:
;121 R.C.22:
Applications
* Ambrosini S.7
Specifications
See also
R ...
*Alfa Romeo 122
The Alfa Romeo 122 was a 12-cylinder inverted-V aircraft engine produced in 1941 by Alfa Romeo Milano as a licence-built Czechoslovakian Walter Sagitta, featuring a single-speed supercharger. The 122 R.C.38 major production variant had a reduction ...
* Alfa Romeo 125/126/127/128/129/131
* Alfa Romeo 135/136
*Alfa Romeo 138 R.C.23/65
*RA.1000 ''Monsone'' – licensed Daimler-Benz DB 601
The Daimler-Benz DB 601 was a German aircraft engine built during World War II. It was a liquid-cooled inverted V12, and powered the Messerschmitt Bf 109, Messerschmitt Bf 110, and many others. Approximately 19,000 601's were produced befo ...
*Alfa Romeo RA.1050
*Alfa Romeo RA.1100 or AR.100
*Alfa Romeo RA.1101 or AR.101
*Alfa Romeo AR.318
*Alfa Romeo Dux
*Alfa Romeo Jupiter – licensed Bristol Jupiter
The Bristol Jupiter was a British nine-cylinder single-row piston radial engine built by the Bristol Aeroplane Company. Originally designed late in World War I and known as the Cosmos Jupiter, a lengthy series of upgrades and developments tur ...
*Alfa Romeo Lynx/Lince – licensed Armstrong Siddeley Lynx
The Armstrong Siddeley Lynx is a British seven-cylinder aero engine developed by Armstrong Siddeley. Testing began in 1920 and 6,000 had been produced by 1939. In Italy Alfa Romeo built a licensed version of this engine named the Alfa Romeo ...
*Alfa Romeo Mercury
Alfa Romeo built/designed a range of aircraft engines based on the Bristol Jupiter and Bristol Pegasus designs, designated Alfa 125, Alfa 126, Alfa 127, Alfa 128, Alfa 129 and Alfa 131. All these essentially similar engines were mainly fitted ...
*Alfa Romeo Pegasus
Alfa Romeo built/designed a range of aircraft engines based on the Bristol Jupiter and Bristol Pegasus designs, designated Alfa 125, Alfa 126, Alfa 127, Alfa 128, Alfa 129 and Alfa 131. All these essentially similar engines were mainly fitted ...
Alfaro
*Alfaro baby engine
* Alfaro 155 hp 4-cyl barrel engine
Allen
* Allen O-675
Alliance
(Aubrey W. Hess/Alliance Aircraft Corporation)
* Hess Warrior
Allied
*Allied Monsoon Licensed manufacturer of French Règnier 4L
AlliedSignal
*AlliedSignal TPE-331
The Honeywell TPE331 (military designation: T76) is a turboprop engine. It was originally designed in the 1950s by Garrett AiResearch, and produced since 1999 by Honeywell Aerospace. The engine's power output ranges from .
Design and develo ...
*Garrett TPF351
The Garrett TPF351 is a turboprop engine designed by Garrett Engine Division of AlliedSignal Aerospace Company. Initiated by Garrett in October 1987, the TPF351-20 engine was selected by Embraer to power the Embraer/FMA CBA 123 Vector, a high-s ...
* AlliedSignal LTS101
* AlliedSignal ALF502/LF507
Allis-Chalmers
''Source:'' Gunston
*Allis-Chalmers J36
The de Havilland Goblin, originally designated as the Halford H-1, is an early turbojet engine designed by Frank Halford and built by de Havilland. The Goblin was the second British jet engine to fly, after Whittle's Power Jets W.1, and the ...
Allison
*Allison V-1410 – Liberty L-12
The Liberty L-12 is an American water-cooled 45° V-12 aircraft engine displacing and making designed for a high power-to-weight ratio and ease of mass production. It saw wide use in aero applications, and, once marinized, in marine use both ...
*Allison V-1650 – Liberty L-12
*Allison V-1710
The Allison V-1710 aircraft engine designed and produced by the Allison Engine Company was the only US-developed V-12 liquid-cooled engine to see service during World War II. Versions with a turbocharger gave excellent performance at hig ...
*Allison V-3420
The Allison V-3420 was a large experimental piston aircraft engine, designed in 1937 by the American Allison Engine Company.
Design and development
In 1937, at the behest of the United States Army Air Corps, the Allison Engine Company agreed t ...
*Allison X-4520
*Allison 250
The Allison Model 250, now known as the Rolls-Royce M250, (US military designations T63 and T703) is a highly successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s. The Model 250 has been p ...
(T63)(T703)
*Allison 252[
*Allison 504
*Allison 545]
*Allison 550[
* Pratt & Whitney/Allison 578-DX
*]Allison J33
The General Electric/Allison J33 is a development of the General Electric J31, enlarged to produce significantly greater thrust, starting at and ending at with an additional low-altitude boost to with water-alcohol injection.
Development
Th ...
(Allison 400)
*Allison J35
The General Electric/Allison J35 was the United States Air Force's first axial-flow (straight-through airflow) compressor jet engine. Originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based ce ...
(Allison 450)
*Allison J56
*Allison J71
The Allison J71 was a single spool turbojet engine, designed and built in the United States. It began development in 1948 as a much modified J35, originally designated J35-A-23.
Operational history
The Allison J71 turbojet powered the Douglas ...
*Allison J89
*Allison J102
The Allison J102 was a turbojet engine developed as a supersonic missile engine by the Allison Engine Company.
Operational history
The J102-100 is an axial flow turbojet that was first run in March 1991. In 1997 it was being considered for use i ...
*Allison T38
The Allison T38 (company Model 501) was an early turboprop engine developed by Allison Engine Company during the late 1940s. The T38 became the basis for the very successful family of Allison T56 turboprop engine.
Design and development
Develope ...
*Allison T39
Allison may refer to:
People
* Allison (given name)
* Allison (surname) (includes a list of people with this name)
* Eugene Allison Smith (1922-1980), American politician and farmer
Companies
* Allison Engine Company, American aircraft engine m ...
*Allison T40
Allison may refer to:
People
* Allison (given name)
* Allison (surname) (includes a list of people with this name)
* Eugene Allison Smith (1922-1980), American politician and farmer
Companies
* Allison Engine Company, American aircraft engin ...
(Allison 500, 503)
* Allison T44
*Allison T54
Allison may refer to:
People
* Allison (given name)
* Allison (surname) (includes a list of people with this name)
* Eugene Allison Smith (1922-1980), American politician and farmer
Companies
* Allison Engine Company, American aircraft engine ...
*Allison T56
The Allison T56 is an American single-shaft, modular design military turboprop with a 14-stage axial flow compressor driven by a four-stage turbine. It was originally developed by the Allison Engine Company for the Lockheed C-130 Hercules tran ...
(501-D)
*Allison T61
The Allison T61 (known internally as the Allison 550-B1) was a turboprop engine that was to power the 1959 version of the proposed Lockheed Super Hercules military and civil freight aircraft. The U.S. Air Force (USAF) had helped Allison fund the ...
*Allison T63
The Allison Model 250, now known as the Rolls-Royce M250, (US military designations T63 and T703) is a highly successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s. The Model 250 has been pro ...
*Allison T71
*Allison T78
*Allison T80
*Allison T406
The Rolls-Royce T406 (company designation AE 1107) is a turboshaft engine that powers the Bell Boeing V-22 Osprey tiltrotor. The engine delivers 6,000 shp (4,470 kW).
Development
In 1982, Detroit Diesel Allison (DDA) prepared a new ...
(AE1107)
*Allison T701
The Allison T56 turboprop engine has been developed extensively throughout its production run, the many variants are described by the manufacturer as belonging to four main series groups.
Initial civil variants (Series I) were designed and pr ...
(Allison 501-M62)
*Allison T703
The Allison Model 250, now known as the Rolls-Royce M250, (US military designations T63 and T703) is a highly successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s. The Model 250 has been pro ...
(Allison 250)
*Allison TF32
*Allison TF41
The Allison TF41 (Company designations RB.168-62 and Model 912) is a low-bypass turbofan engine.
Design and development
The TF41 was jointly developed by Allison Engine Company and Rolls-Royce from the latter's RB.168-25R Spey. Allison manufac ...
(development of Rolls-Royce Spey
The Rolls-Royce Spey (company designations RB.163 and RB.168 and RB.183) is a low-bypass turbofan engine originally designed and manufactured by Rolls-Royce that has been in widespread service for over 40 years. A co-development version of the ...
)
*Allison GMA 200
*Allison GMA 500
*Allison AE3010
*Allison AE3012
*Allison PD-37 Pyrodyne
Almen
*Almen A-4
Axial engines (sometimes known as barrel or Z-crank engines) are a type of reciprocating engine with pistons arranged around an output shaft with their axes parallel to the shaft. Barrel refers to the cylindrical shape of the cylinder group (result ...
Alvaston
* Alvaston 20hp 2-cyl opposed
* Alvaston 30hp 2-cyl opposed
* Alvaston 50hp 4-cyl opposed
Alvis
*Alvis Alcides
The Alvis Pelides was an unflown British air-cooled radial aero engine first developed in 1936. The Pelides Major was a projected but unbuilt development as were the Alcides, Alcides Major and the Maeonides Major, the Alvis aircraft engine ra ...
*Alvis Alcides Major
The Alvis Pelides was an unflown United Kingdom, British air-cooled radial engine, radial aircraft engine, aero engine first developed in 1936. The Pelides Major was a projected but unbuilt development as were the Alcides, Alcides Major and th ...
*Alvis Leonides
The Alvis Leonides was a British air-cooled nine-cylinder radial aero engine first developed by Alvis Car and Engineering Company in 1936.
Design and development
Development of the nine-cylinder engine was led by Capt. George Thomas Smith-Cl ...
*Alvis Leonides Major
The Alvis Leonides Major was a British air-cooled 14-cylinder radial aero engine developed by Alvis from the earlier nine-cylinder Leonides.
Design and development
In 1951 Alvis started development of a 14-cylinder, two row radial of 1,118 ...
*Alvis Maeonides Major
The Alvis Pelides was an unflown British air-cooled radial aero engine first developed in 1936. The Pelides Major was a projected but unbuilt development as were the Alcides, Alcides Major and the Maeonides Major, the Alvis aircraft engine ra ...
* Alvis Pelides
*Alvis Pelides Major
The Alvis Pelides was an unflown British air-cooled radial aero engine first developed in 1936. The Pelides Major was a projected but unbuilt development as were the Alcides, Alcides Major and the Maeonides Major, the Alvis aircraft engine r ...
American Cirrus Engine
''See: ACE
An ace is a playing card, die or domino with a single pip. In the standard French deck, an ace has a single suit symbol (a heart, diamond, spade, or club) located in the middle of the card, sometimes large and decorated, especially in the ca ...
''
American Engineering Corporation
''Source: RMV''
*ACE Keane
American Helicopter
*American Helicopter PJ49 Pulsejet
300px, Diagram of a pulsejet
A pulsejet engine (or pulse jet) is a type of jet engine in which combustion occurs in pulses. A pulsejet engine can be made with few or no moving parts, and is capable of running statically (i.e. it does not need ...
*American Helicopter XPJ49-AH-3
American Motor & Aviation Co
*American 1911 rotary
*American S-5 radial
AMCEL
(AMCEL Propulsion Company)
* AMCEL controllable solid fuel rocket
AMI
(AeroMotion Inc.)
* AeroMotion Twin
*AeroMotion O-100 Twin
*AeroMotion O-101 Twin
AMT Netherlands
(Aviation Microjet Technology)
* AMT Olympus
* AMT Titan
* AMT Lynx
AMT USA
(AMT USA, LLC, Cincinnati)
* AMT-450
A.M.U.A.L
(Établissement A.M.U.A.L)
* A.M.U.A.L M.J.5 65° V-8 350 hp [
* A.M.U.A.L M.J.6 90° V-8 400 hp ][
* A.M.U.A.L M.J.7 90° V-8 600 hp ][
]
Angle
*Angle 100hp Radial
Ansaldo
* Ansaldo San Giorgio 4E-145 6I 300 hp[
* Ansaldo San Giorgio 4E-150 6I 300 hp]
* Ansaldo San Giorgio 4E-284 V-12 450 hp[
* Ansaldo San Giorgio 4E-290 V-12 550 hp][
]
Antoinette
''Source:''Gunston
*Antoinette 32hp V-8 [
*Antoinette 46hp?
*Antoinette 64hp V-16 ][
*]Antoinette 67hp V-8
The Antoinette 8V was an early French eight-cylinder, liquid-cooled, V engine, the first series production gasoline-fueled, spark plug ignition engine of any kind produced with manifold injection. It was typically rated at . First produced in 1 ...
*Antoinette 165hp V-16
*Antoinette 134hp V-8 [
*Antoinette 55hp V-8][
*Antoinette V-32][
]
Anzani
''For British Anzani products see: British Anzani''
''Source:''
Air-cooled Anzani engines
*Anzani V-2
*Anzani 3-cylinder fan engines
From 1905 to 1915, Alessandro Anzani built a number of three-cylinder fan engines and radial engines, one of which powered Louis Blériot's 1909 cross-channel flight. An Anzani three-cylinder engine that powers a Blériot XI based in England is ...
**Anzani 14hp [
**Anzani 15hp ][
**Anzani 24.5hp ][
**Anzani 31.6hp ][
**Anzani 42.3hp ][
**Anzani 10-12hp
**Anzani 12-15hp
**Anzani 25-30hp
**Anzani 30-35hp
**Anzani 40-45hp
**Anzani 45-50hp][
*]Anzani 30hp 3-cyl radial
From 1905 to 1915, Alessandro Anzani built a number of three-cylinder fan engines and radial engines, one of which powered Louis Blériot's 1909 cross-channel flight. An Anzani three-cylinder engine that powers a Blériot XI based in England i ...
[
*Anzani 45hp 5-cyl radial][
*Anzani 60hp 5-cyl radial
*]Anzani 6-cylinder
Alessandro Anzani developed the first two-row radial from his earlier 3- cylinder Y engine by merging two onto the same crankshaft with a common crankweb.
Development
By December 1909 Anzani had a 3-cylinder air-cooled true radial engine run ...
**Anzani 40-45hp radial [
**Anzani 50-60hp radial ][
**Anzani 70hp radial
**Anzani 80hp radial ]
*Anzani 95hp 7-cyl radial
*Anzani 10-cylinder
The Anzani 10 was a 1913 10-cylinder air-cooled radial aircraft engine. It powered several experimental aircraft and also the later production versions of the Caudron G.3 reconnaissance aircraft, the Caudron G.4 bomber/trainer and the first pro ...
**Anzani 60-70hp radial [
**Anzani 100-110hp radial ][
**Anzani 95-100hp radial ][
**Anzani 125hp radial ][
**Anzani 125hp radial ][
**Anzani 200hp radial][
*Anzani 100hp 14-cyl radial ][
*Anzani 150-160hp 14-cyl radial ]
* Anzani 20 200hp 20-cyl radial
Water-cooled Anzani engines
*Anzani 30-32hp V-4 [
*Anzani 56-70hp V-4 ][
*Anzani 600-700hp 20-cyl radial ][ In-line radial 10 banks of 2 cylinders][
*Anzani W-6][
*Anzani 6A3 (6-cyl radial 60 hp)
]
ARDEM
(Avions Roger Druine Engines M)
*Ardem 4 CO2
Ares
(Ares ltd., Finland)
* Ares diesel Cirrus[
]
Argus Motoren
''Source:Gunston except where noted''
* Argus Type I ("50hp") – 4-cyl. 50-70 hp )
* Argus Type II (4-cyl. 100 hp )[
* ]Argus Type III
The Argus 110 hp aircraft engine, aka Argus Type III (not As.III), from 1912 was a six-cylinder, water cooled inline engine built by the German Argus Motoren company.
Design and development
The first known six-cylinder aircraft engine pr ...
(aka Argus 110 hp) – 6-cyl )
* Argus Type IV (aka 140/150hp) – 4-cyl. 140 hp )[
* Argus Type V (6-cyl. 140 hp )][
* Argus Type VI (6-cyl. 140 hp )][
* Argus Type VII (6-cyl. 115-130 hp )][
* Argus Type VIII (6-cyl. 190 hp )][
*]Argus As I
The Argus As I was a four-cylinder, water-cooled, aircraft engine produced in Germany by Argus Motoren from 1911 until about 1913.
The engine saw widespread use in aircraft in pre-war Germany and initially was also sold under the brand name 'Avi ...
4-cylinder, 100-hp, year 1913
*Argus As II
The Argus As II was a six-cylinder, in-line, water-cooled, aircraft engine produced in Germany by Argus Motoren in 1914.
The Argus As II produced at 1,350 rpm.Der Argus Flugmotor, 1916
Design and development
The Argus As II was a major re ...
, 6-cylinder, 120-hp, year 1914
*Argus As III
The Argus As III was a six-cylinder, in-line, water-cooled, aircraft engine produced in Germany by Argus Motoren during World War I. The Argus As III produced at 1,400 rpm.Huth, 1920, pp. 232-233
Design and development
Argus Motoren a ...
6-cylinder upright inline
*Argus As 5
The Argus As 5 was a large 24-cylinder 6 blocks' star aircraft engine, designed and built in Germany in the early 1920s by Argus Motoren.
Design and development
Following the Armistice of 1918, Germany continued to build aircraft and engines ...
24-cylinder in-line radial
Radial is a geometric term of location which may refer to:
Mathematics and Direction
* Vector (geometric), a line
* Radius, adjective form of
* Radial distance, a directional coordinate in a polar coordinate system
* Radial set
* A bearing from ...
(6 banks of four cylinders)
*Argus As VI 700 hp V-12[
*Argus As VIA][
*Argus As 7 9R 700 hp]
*Argus As 8
The Argus As 8 was a four-cylinder, air-cooled, inverted inline aircraft engine produced in Germany by Argus Motoren in the 1930s.
Variants
;As 8A:Initial production version maximum for 5 minutes, continuous.
;As 8B:A more powerful variant d ...
4-cylinder inverted inline
*Argus As 10
The Argus As 10 was a German-designed and built, air-cooled 90° cylinder bank-angle inverted V8 "low power" aircraft engine, used mainly in training aircraft such as the Arado Ar 66 and Focke-Wulf Fw 56 Stösser and other small short-range re ...
8-cylinder inverted V
*Argus As 12 16H 550 hp
*Argus As 16 4-cylinder horizontally-opposed 35 hp
*Argus As 17
The Argus As 17 was an air cooled six-cylinder in-line aircraft engine designed by the German engineering company Argus Motoren in the 1930s. Developed from the same company's smaller As 8, the engine was produced in ratings between . First d ...
*Argus As 014
The Argus As 014 (designated 109-014 by the RLM) was a pulsejet engine used on the German V-1 flying bomb of World War II, and the first model of pulsejet engine placed in mass production. License manufacture of the As 014 was carried out in J ...
(aka "Argus 109-014") – pulse jet engine
300px, Diagram of a pulsejet
A pulsejet engine (or pulse jet) is a type of jet engine in which combustion occurs in pulses. A pulsejet engine can be made with few or no moving parts, and is capable of running statically (i.e. it does not need ...
for V-1 flying bomb
The V-1 flying bomb (german: Vergeltungswaffe 1 "Vengeance Weapon 1") was an early cruise missile. Its official Reich Aviation Ministry () designation was Fi 103. It was also known to the Allies as the buzz bomb or doodlebug and in Germany ...
and Tornado boat
*Argus As 044
*Argus As 16 4-cylinder inverted inline 40 hp
*Argus As 17
The Argus As 17 was an air cooled six-cylinder in-line aircraft engine designed by the German engineering company Argus Motoren in the 1930s. Developed from the same company's smaller As 8, the engine was produced in ratings between . First d ...
6-cylinder inverted inline 225 hp / 285 hp
* Argus As 401 development and renumbering of the As 10
*Argus As 402
*Argus As 410
The Argus As 410 was a German air-cooled inverted V-12 light aircraft engine that was first produced by Argus Motoren in 1938.
Design and development
The engine marked a departure from earlier Argus engines in that it had new construction tech ...
12-cylinder inverted V
*Argus As 411
The Argus 411 was a twelve-cylinder, air-cooled, inverted-V12 aircraft engine developed by Argus Motoren in Germany during World War II.
Design and development
The As 411 was a refined and more powerful version of the Argus As 410. Most 411 prod ...
12-cylinder inverted V
*Argus As 412 24-cylinder H-block, prototyped
*Argus As 413 – similar to 412, never built
*Argus 109-044
''Argus Motoren'' was a German manufacturing firm known for their series of small inverted-V engines and the Argus As 014 pulsejet for the V-1 flying bomb.
History
Started in Berlin in 1906 as a subsidiary of Henri Jeannin's automobile business, ...
*Argus 115 hp
The Argus 115 hp aircraft engine from 1913 was a six-cylinder, water cooled inline engine built by the German Argus Motoren company.
Design and development
The Argus 115 hp engine was a development from the earlier Argus 110 hp engine of ...
6-cylinder upright inline [
*]Argus 130 hp
The Argus 140/150 hp 6-cylinder aircraft engine from 1913 was a six-cylinder, water cooled inline engine built by the German Argus Motoren company from 1913 to 1914.
The engine design evolved from earlier four- and six-cylinder Argus engin ...
6-cylinder upright inline [
*]Argus 145 hp
The Argus 140/150 hp 6-cylinder aircraft engine from 1913 was a six-cylinder, water cooled inline engine built by the German Argus Motoren company from 1913 to 1914.
The engine design evolved from earlier four- and six-cylinder Argus engi ...
6-cylinder upright inline [
*Argus 190 hp 6-cylinder upright inline ][
]
Argylls
*a 120-130hp sleeve valve
The sleeve valve is a type of valve mechanism for piston engines, distinct from the usual poppet valve. Sleeve valve engines saw use in a number of pre-World War II luxury cars and in the United States in the Willys-Knight car and light truck. T ...
6-cylinder exhibited at Olympia 1914
Armstrong Siddeley
Armstrong Siddeley
Armstrong Siddeley was a British engineering group that operated during the first half of the 20th century. It was formed in 1919 and is best known for the production of luxury vehicles and aircraft engines.
The company was created following ...
was formed by purchase of Siddeley-Deasy
The Siddeley-Deasy Motor Car Company Limited was a British automobile, aero engine and aircraft company based in Coventry in the early 20th century. It was central to the formation, by merger and buy-out, of the later Armstrong Siddeley Motor ...
in 1919.
Piston Engines
*Armstrong Siddeley Terrier
The Armstrong Siddeley Deerhound was a large aero engine developed by Armstrong Siddeley between 1935 and 1941. An increased capacity variant known as the Boarhound was never flown,Gunston 1989, p.18. and a related, much larger, design known ...
*Armstrong Siddeley Mastiff
The Armstrong Siddeley Deerhound was a large aero engine developed by Armstrong Siddeley between 1935 and 1941. An increased capacity variant known as the Boarhound was never flown,Gunston 1989, p.18. and a related, much larger, design known a ...
*Armstrong Siddeley Boarhound
The Armstrong Siddeley Deerhound was a large aero engine developed by Armstrong Siddeley between 1935 and 1941. An increased capacity variant known as the Boarhound was never flown,Gunston 1989, p.18. and a related, much larger, design known ...
*Armstrong Siddeley Cheetah
The Armstrong Siddeley Cheetah is a seven-cylinder British air-cooled aircraft radial engine of 834 cu in (13.65 L) capacity introduced in 1935 and produced until 1948. Early variants of the Cheetah were initially known as the Lynx Major.Lums ...
*Armstrong Siddeley Civet
The Armstrong Siddeley Genet Major is a British five-cylinder (later seven-cylinder), air-cooled, radial engine for aircraft, designed and built by Armstrong Siddeley and first run in 1928. It developed 140 horsepower (104 kW). In Royal A ...
*Armstrong Siddeley Cougar
The Armstrong Siddeley Cougar was an aero engine developed by Armstrong Siddeley in 1945. The design was a departure from earlier Armstrong Siddeley engines in many ways, it was the company's only nine-cylinder radial design. Although the engi ...
*Armstrong Siddeley Deerhound
The Armstrong Siddeley Deerhound was a large aero engine developed by Armstrong Siddeley between 1935 and 1941. An increased capacity variant known as the Boarhound was never flown,Gunston 1989, p.18. and a related, much larger, design known a ...
*Armstrong Siddeley Genet
The Armstrong Siddeley Genet was a five-cylinder, air-cooled, radial engine for aircraft use built in the UK, first run in 1926. It developed 80 hp at 2,200 rpm in its final form and was a popular light aircraft powerplant. Followin ...
*Armstrong Siddeley Genet Major
The Armstrong Siddeley Genet Major is a British five-cylinder (later seven-cylinder), air-cooled, radial engine for aircraft, designed and built by Armstrong Siddeley and first run in 1928. It developed 140 horsepower (104 kW). In Royal ...
*Armstrong Siddeley Hyena
The Armstrong Siddeley Hyena was a British aero engine developed by Armstrong Siddeley. Designed in the 1930s, it was an unusual experimental radial engine with inline cylinder banks. It was flown using an Armstrong Whitworth A.W.16 fighter ...
*Armstrong Siddeley Jaguar
The Armstrong Siddeley Jaguar was an aircraft engine developed by Armstrong Siddeley. The Jaguar was a petrol-fuelled air-cooled 14-cylinder two-row radial engine design. The Jaguar III was first used in 1923, followed in 1925 by the Jagua ...
*Armstrong Siddeley Leopard
The Armstrong Siddeley Leopard was a British 14-cylinder twin-row air-cooled radial aero engine developed in 1927 by Armstrong Siddeley. It was the most powerful radial engine in the world when introduced.
Variants
;Leopard I
:700 hp, medium ...
*Armstrong Siddeley Lynx
The Armstrong Siddeley Lynx is a British seven-cylinder aero engine developed by Armstrong Siddeley. Testing began in 1920 and 6,000 had been produced by 1939. In Italy Alfa Romeo built a licensed version of this engine named the Alfa Romeo ...
*Armstrong Siddeley Mongoose
The Armstrong Siddeley Mongoose is a British five-cylinder radial aero engine produced by Armstrong Siddeley. Developed in the mid-1920s it was used in the Hawker Tomtit trainer and Parnall Peto seaplane amongst others. With a displacement ...
*Armstrong Siddeley Ounce
The Armstrong Siddeley Ounce was a small two-cylinder aero engine developed by Armstrong Siddeley in 1920.Gunston 1989, p.18. The engine was originally conceived as a test piece but ran very well and was put into production for early ultralig ...
*Armstrong Siddeley Panther
The Armstrong Siddeley Panther was a 27-litre 14-cylinder twin-row air-cooled radial aero engine developed by Armstrong Siddeley. It was originally named the Jaguar Major.Lumsden 2003, p.72.
Applications
* Armstrong Whitworth Atlas Mk II
* ...
*Armstrong Siddeley Puma
The Siddeley Puma was a British aero engine developed towards the end of World War I and produced by Siddeley-Deasy. The first engines left the production lines of Siddeley-Deasy in Coventry in August 1917, production continued until December 1 ...
– originally the Siddeley Puma
*Armstrong Siddeley Serval
The Armstrong Siddeley Serval was a British ten-cylinder aero engine developed by Armstrong Siddeley in the late 1920s. Following company tradition, the engine was named for the serval.
Design and development
The Serval was a ten-cylinder, do ...
*Armstrong Siddeley Tiger
The Armstrong Siddeley Tiger was a British 14-cylinder air-cooled aircraft radial engine developed by Armstrong Siddeley in the 1930s from their Jaguar engine. The engine was built in a number of different versions but performance and dimensi ...
*Armstrong Siddeley Wolfhound – paper project of developed Deerhound
Gas turbines
*Armstrong Siddeley Adder
The Armstrong Siddeley ASA.1 Adder was an early British turbojet engine developed by the Armstrong Siddeley company and first run in November 1948.
Design and development
The Adder, a turbojet derivative of the Armstrong Siddeley Mamba, was or ...
*Armstrong Siddeley ASX
The Armstrong Siddeley ASX was an early axial flow jet engine built by Armstrong Siddeley that first ran in April 1943.Gunston 1989, p.18. Only a single prototype was constructed, and it was never put into production. A turboprop version as ...
*Armstrong Siddeley Double Mamba
The Armstrong Siddeley Double Mamba is a turboprop engine design developed in the late 1940s of around . It was used mostly on the Fairey Gannet anti-submarine aircraft developed for the Fleet Air Arm of the Royal Navy.
Design and development ...
*Armstrong Siddeley Mamba
The Armstrong Siddeley Mamba was a British turboprop engine produced by Armstrong Siddeley in the late 1940s and 1950s, producing around 1,500 effective horsepower (1,100 kW).
Armstrong Siddeley gas turbine engines were named after sna ...
*Armstrong Siddeley Python
The Armstrong Siddeley Python was an early British turboprop engine designed and built by the Armstrong Siddeley company in the mid-1940s. Its main use was in the Westland Wyvern, a carrier-based heavy fighter. The prototypes had used the Roll ...
*Armstrong Siddeley Sapphire
The Armstrong Siddeley Sapphire is a British turbojet engine that was produced by Armstrong Siddeley in the 1950s. It was the ultimate development of work that had started as the Metrovick F.2 in 1940, evolving into an advanced axial flow ...
*Armstrong Siddeley Viper
The Armstrong Siddeley Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol Siddeley and Rolls-Royce Limited. It entered service in 1953 and remained in use with the Roy ...
Rocket engines
* Armstrong Siddeley Alpha
* Armstrong Siddeley Beta
Armstrong Siddeley Beta was an early rocket engine, intended for use in supersonic aircraft.
The Miles M.52, the intended British contender for supersonic flight, had been cancelled in 1946 due to uncertainty concerning its turbojet engine's th ...
* Armstrong Siddeley Delta
* Armstrong Siddeley Gamma
The Armstrong Siddeley, later Bristol Siddeley Gamma was a family of rocket engines used in British rocketry, including the Black Knight and Black Arrow launch vehicles. They burned kerosene fuel and hydrogen peroxide. Their construction wa ...
* Armstrong Siddeley Screamer
The Armstrong Siddeley Screamer was a British rocket engine intended to power the Avro 720 manned interceptor aircraft ( Avro's competitor to the Saunders-Roe SR.53 for a rocket-powered interceptor). Thrust was variable, up to a maximum of . ...
* Armstrong Siddeley Snarler
The Armstrong Siddeley Snarler was a small rocket engine used for mixed-power experiments with an early turbojet engine. and was the first British liquid-fuelled rocket engine to fly.
Design and development
Unlike other British rocket engin ...
* Armstrong Siddeley Spartan
* Armstrong Siddeley Stentor
The Armstrong Siddeley Stentor, latterly Bristol Siddeley BSSt.1 Stentor, was a two-chamber HTP rocket engine used to power the Blue Steel stand-off missile carried by Britain's V bomber force. The high thrust chamber was used for the first ...
Armstrong Whitworth
* Armstrong Whitworth 1918 30° V-12[
]
Arrow SNC
*Arrow 250
The Arrow 250 is a family of single-cylinder, two-stroke, single- or dual-ignition aircraft engines that were designed for ultralight aircraft by Arrow SNC of Italy.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-1 Cyb ...
*Arrow 270 AC
The Arrow 250 is a family of single-cylinder, two-stroke, single- or dual-ignition aircraft engines that were designed for ultralight aircraft by Arrow SNC of Italy.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-1 Cyb ...
*Arrow 500
The Arrow 500 is a twin-cylinder, horizontally opposed, two-stroke, single or dual ignition, aircraft engine that was designed for ultralight aircraft by Arrow SNC of Italy.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page ...
*Arrow 1000
The Arrow 1000 is a four-cylinder, horizontally opposed, two-stroke, single- or dual-ignition, aircraft engine that was designed for float-equipped ultralight aircraft by Arrow SNC of Italy.Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' ...
Arsenal
''Source:''Gunston
*Arsenal 213
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling ...
* Arsenal 12H
* Arsenal 12H-Tandem
*Arsenal 12K
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling ...
*Arsenal 24H
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling ...
* Arsenal 24H-Tandem
Asahina
* Asahina 9-cyl 100hp rotary[
]
Ashmusen
(Ashmusen Manufacturing Company)
*Ashmusen 1908 60hp 8HOA[
*Ashmusen 1908 105hp 12HOA][
]
Aspin
(F.M. Aspin & Company)
*Aspin Flat-Four[
]
Aster
*Aster 51hp 4-cylinder-line[
]
Astrodyne
(Astrodyne Inc.)
* Astrodyne 16NS-1000[
* Astrodyne XM-34 (]ZELL Zell may refer to:
Places Austria
* Zell am See, in Salzburg state
* Zell am Ziller, in Tyrol
* Zell, Carinthia, in Carinthia
* in Upper Austria:
** Bad Zell
** Zell am Moos
** Zell an der Pram
** Zell am Pettenfirst
Germany
* Zell im Fichtelge ...
booster)[
]
ATAR
(Atelier Technique Aéronautique de Rickenbach – pre SNECMA take-over)
* ATAR 101
The SNECMA ATAR 101 is a French axial-flow turbojet engine built by SNECMA. It was derived from engines and design work carried out at BMW in Germany during World War II, and extensively developed though a progression of more powerful models. T ...
* ATAR 103
* ATAR 104 (Vulcain)
* ATAR 201
* ATAR 202
* ATAR 203
Atwood
(Atwood Aeronautic Company, Williamsport, PA / Harry N. Atwood)
*Atwood 120-180hp V-12 ( bore x stroke
*Atwood M-1 (1916)
*Atwood M-2 (1916)
*Atwood Twin Six
Aubier & Dunne
''Data from:''Italian Civil & Military Aircraft 1930–1945
*Aubier & Dunne 2-cyl 17hp[
*Aubier & Dunne 3-cyl][
*Aubier-Dunne V.2D
]
Austin
* Austin V-12[
* Austin rotary engine][
]
Austro-Daimler
''Source:''Gunston
*Austro-Daimler 35-40hp 4-cyl. (35-40 hp )[
*Austro-Daimler 65-70hp 4-cyl. (65-70 hp )][
* Austro-Daimler 90hp 6-cyl. (90 hp )][
*]Austro-Daimler 120hp 6-cyl.
The Austro-Daimler 6 was a series of Austrian six-cylinder water-cooled inline SOHC aero engines first produced in 1910 by the Austro-Daimler company.
Design and development
The first Austro-Daimler six-cylinder engine was designed by Dr-Ing Fe ...
(120 hp )[
*]Austro-Daimler 160hp 6-cyl.
The Austro-Daimler 6 was a series of Austrian six-cylinder water-cooled inline SOHC aero engines first produced in 1910 by the Austro-Daimler company.
Design and development
The first Austro-Daimler six-cylinder engine was designed by Dr-Ing F ...
* Austro-Daimler 185hp 6-cyl.
* Austro-Daimler 200hp 6-cyl. (200 hp )[
* Austro-Daimler 210hp 6-cyl.
*]Austro-Daimler 225hp 6-cyl.
The Austro-Daimler 6 was a series of Austrian six-cylinder water-cooled inline SOHC aero engines first produced in 1910 by the Austro-Daimler company.
Design and development
The first Austro-Daimler six-cylinder engine was designed by Dr-Ing F ...
*Austro-Daimler 300hp V-12
*Austro-Daimler 360hp 6-cyl (360 hp )[
*Austro-Daimler 400hp V-12 (400 hp )][
*Austro-Daimler D-35 (400 hp )][
]
Austro Engine
* Austro Engine E4 (AE 300)
*Austro Engine AE50R
The Austro Engine EA50R is an Austrian aircraft engine, produced by Austro Engine of Wiener Neustadt for use in motorgliders and UAVs.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 238-239. WDLA UK, ...
*Austro Engine AE75R
The Austro Engine AE75R is an Austrian aircraft engine, that was designed and produced by Austro Engine of Wiener Neustadt for use in ultralight aircraft.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 256- ...
*Austro Engine AE80R
The Austro Engine AE80R is an aircraft Wankel engine that was first run on 8 January 2013 and is under development by Austro Engine of Wiener Neustadt.
Design and development
Development of the AE80R started in 2010 based on the Austro Engine AE ...
*Austro Engine AE500
Austro may refer to:
* Austro-, a prefix denoting Austria
* Austro (automobile), an Austrian cyclecar manufactured 1913–1914
* Austro Engine, an aircraft engine manufacturer
* Ēostre or *Austrō, a Proto-Germanic goddess widely associated with ...
*Austro Engine GIAE110R
The Austro Engine GIAE110R is an Austrian aircraft engine, designed and produced by Austro Engine of Wiener Neustadt for use in light aircraft.Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 238-2 ...
Auto Diesels
* Auto Diesels STAD A250
* Auto Diesels STAD A260[
* Auto Diesels LPI Mk.12A/L][
* Auto Diesels LPI Mk.12A/T][
* Auto Diesels LPI Mk.12A/D][
* Auto Diesels GT15][
* Auto Diesels 7660.001.020][
]
Ava
(L'Agence General des Moteurs Ava)
* Ava 4A
The Ava 4A was a low power flat-four ( boxer engine) developed for very light aircraft in France in the 1930s. It was used by several prototypes and at least one production series.
Design and development
Marcel Violet was a French racing drive ...
Avco Lycoming
''See: Lycoming''
Avia
Aviadvigatel
*Aviadvigatel PD-14
The Aviadvigatel PD-14 (previously known as PS-12) is a high-bypass turbofan being developed by Aviadvigatel to power the Irkut MC-21 twin-jet airliner. It is a 14 tf (30,865 lbf) thrust powerplant.
Development
In December 2009, the PD-14 ...
*Aviadvigatel PS-90
The Aviadvigatel PS-90 is a Russian high-bypass commercial turbofan rated at 16000 kgf (157 kN, 35,300 lbf) thrust. It powers Russian airliners such as the Ilyushin Il-96 and the Tupolev Tu-204/Tu-214 series and transport aircraft such as ...
Aviatik
Argus engines sold in France under the brand name 'Aviatik' by Automobil und Aviatik AG
Automobil und Aviatik AG was a German aircraft manufacturer during World War I. The company was established at Mülhausen (today in France) in 1909 and soon became one of the country's leading producers of aircraft. It relocated to Freiburg in ...
* Aviatik 70hp 4-cyl in-line
* Aviatik 100hp 4-cyl in-line
* Aviatik 150hp 4-cyl in-line
A.V. Roe
*A.V. Roe 20hp 2-cyl.
Avro
*Avro Alpha
Avro Canada
* Avro Chinook
*Avro Iroquois
The Orenda PS.13 Iroquois was an advanced turbojet engine designed for military use. It was developed by the Canadian aircraft engine manufacturer Orenda Engines, a part of the Avro Canada group. Intended for the CF-105 Arrow interceptor, deve ...
*Avro Orenda
The Avro Canada TR5 Orenda was the first production jet engine from Avro Canada's Gas Turbine Division. Similar to other early jet engines in design, like the Rolls-Royce Avon or General Electric J47, the Orenda nevertheless outperformed its r ...
*Avro P.35 Waconda
Axelson
*Axelson A-7-R 115hp
*Axelson-Floco B 150hp
Axial Vector Engine Corporation
*Dyna-Cam
Axial engines (sometimes known as barrel or Z-crank engines) are a type of reciprocating engine with pistons arranged around an output shaft with their axes parallel to the shaft. Barrel refers to the cylindrical shape of the cylinder group (result ...
Aztatl
* Aztatl 3-cyl radial[
* Aztatl 6-cyl 80hp radial]
* Aztatl 10-cyl radial[
]
B
Bailey
*Bailey C-7-R "Bull's Eye" 1927 = 140hp 7RA.
Bailey Aviation
*Bailey B200
The Bailey B200 is a British single cylinder, four valve, four stroke aircraft engine, designed and produced by Bailey Aviation of Bassingbourn, Royston, specifically for paramotors, powered hang gliders, microlights and ultralight aircraft.Ba ...
*Bailey Hornet
The Bailey Hornet is a British aircraft engine, under development by Bailey Aviation of Royston, Hertfordshire for use in powered paragliders.Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', pages 256-257. Fly ...
*Bailey V5 engine
The Bailey V5 is a British aircraft engine, designed and produced by Bailey Aviation of Royston, Hertfordshire for use in powered paragliders, in particular the Bailey V5 paramotor.Tacke, Willi; Marino Boric; et al: ''World Directory of Light A ...
Baradat–Esteve
(Claudio Baradat Guillé & Carlos Esteve)
* Baradat toroidal engine
Basse und Selve
*Basse und Selve BuS. 120hp ( 120-130 hp)[
*Basse und Selve BuS.III 150 hp
*Basse und Selve BuS.IV ( / 260 hp / 270 hp)][
* Basse und Selve BuS.IVa 300 hp][
]
Bates
''Data from:''
*Bates 29hp V-4
Bayerische
(Bayerische Motoren Gesellschaft)
* Bayerische 7-cyl 50hp rotary[
]
Beardmore
''Source: Lumsden''
*Beardmore 90 hp ()[
*]Beardmore 120 hp
The Beardmore 120 hp was a British six-cylinder, water-cooled aero engine that first ran in 1914, it was built by William Beardmore and Company as a licensed-built version of the Austro-Daimler 6. The engine featured cast iron cylinders ...
*Beardmore 160 hp
The Beardmore 160 hp is a British six-cylinder, water-cooled aero engine that first ran in 1916, it was built by Arrol-Johnston and Crossley Motors for William Beardmore and Company as a development of the Beardmore 120 hp, itself a lic ...
*Beardmore Pacific
*Beardmore Simoon
*Beardmore Cyclone
The Beardmore Cyclone was an aero engine produced by William Beardmore & Co with the aim of producing an engine generating a high power output at low revolutions by designing an engine of large displacement. The design did not enter volume prod ...
*Beardmore Tornado
The Beardmore Tornado was an eight-cylinder inline diesel aircraft engine
Diesel may refer to:
* Diesel engine, an internal combustion engine where ignition is caused by compression
* Diesel fuel, a liquid fuel used in diesel engines
* Di ...
*Beardmore 12-cyl opposed diesel
* Beardmore Typhoon
*Galloway Adriatic
*Galloway Atlantic[
]
Béarn
''Construction Mécanique du Béarn/Société de Construction et d'Exploitation de Matériels et de Moteurs''
* Béarn 6
* Béarn 12A
* Béarn 12B
Beatty
*Beatty 40hp 4-cyl.()[
*Beatty 50hp 4-cyl.()]
*Beatty 60hp 4-cyl. (geared 0.66:1 )[
*Beatty 80hp 8-cyl. V-8 ()]
Beck
* Beck 1910 toroidal engine[
* Beck 35hp 4cyl toroidal engine ]
* Beck 50hp 4cyl toroidal engine
* Beck 75hp 4cyl toroidal engine
Beecher
(B.L. Beecher Company, New Haven, Connecticut)
* Beecher 8HOA[
]
Bell Aerosystems Company
*Bell Model 117
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a sing ...
* Bell Model 8001
*Bell Model 8048
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a sing ...
* Bell Model 8081
* Bell Model 8096
* Bell Model 8096-39
* Bell Model 8096A
* Bell Model 8096B
*Bell Model 8096L
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single ...
* Bell Model 8247
*Bell Model 8533
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a si ...
*Bell LR67
* Bell XLR-81
* Bell XLR-81-BA-3
* Bell XLR-81-BA-5
* Bell XLR-81-BA-7
*Bell XLR-81-BA-11
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single ...
*Bell XLR-81-BA-13
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single ...
*Bell Hustler[
*Bell Nike-Ajax engine][
]
Bentley
W. O. Bentley
Walter Owen Bentley, MBE (16 September 1888 – 13 August 1971) was an English engineer who founded Bentley Motors Limited in London. He was a motorcycle and car racer as a young man. After making a name for himself as a designer of aircraft an ...
*Bentley BR1
The Bentley BR.1 was a British rotary aircraft engine of the First World War. Designed by the motor car engine designer W. O. Bentley, the BR.1 was built in large numbers, being one of the main powerplants of the Sopwith Camel.
Design and develo ...
*Bentley BR2
The Bentley B.R.2 was a nine-cylinder British rotary aircraft engine developed during the First World War by the motor car engine designer W. O. Bentley from his earlier Bentley BR.1. Coming as it did near the end of the war, the BR.2 was built ...
Benz
''Source:''Gunston
*Benz 195hp [
*Benz FX ][
*Benz Bz.I (Type FB) ][
* Benz Bz.II (Type FD)
* Benz Bz.III (Type FF)
*Benz Bz.IIIa
*]Benz Bz.IIIav
Benz, an old Germanic clan name dating to the fifth century (related to "bear", "war banner", "gau", or a "land by a waterway") also used in German () as an alternative for names such as Berthold, Bernhard, or Benedict, may refer to:
People Su ...
[
* Benz Bz.IIIb
*]Benz Bz.IV
The Benz Bz.IV was a German six-cylinder, water-cooled, inline engine developed for aircraft use. Deliveries began in 1916, and some 6,400 were produced.
Design and development
The Bz.IV was a dual-camshaft design, with two intake and two exhau ...
* Benz Bz.IVa
*Benz Bz.V [
*Benz Bz.Vb ][
*Benz Bz.VI ][
*Benz Bz.VIv ][
]
Berliner
*Berliner 6hp rotary helicopter engine
Bertin
* Bertin 50hp X-4[
* Bertin 100hp X-8][
]
Besler
''See: Doble-Besler''
Beaussier
(''Moteurs Beaussier'')
* Beaussier 4-cyl
Bessonov
(A. A. Bessonov)
* Bessonov MM-1
Better Half
*Better Half VW
The Better Half VW is an American aircraft engine, designed by Leonard Milholland of Brookshire, Texas, in 1993 for use in ultralight aircraft. The engine is supplied in the form of plans for amateur construction.Bayerl, Robby; Martin Berkemei ...
Beardmore Halford Pullinger (B.H.P.)
*Atlantic
*230 hp – built by Galloway and Siddeley-Deasy developed into Siddeley Puma
The Siddeley Puma was a British aero engine developed towards the end of World War I and produced by Siddeley-Deasy. The first engines left the production lines of Siddeley-Deasy in Coventry in August 1917, production continued until December ...
Binetti
* Binetti B-300[
]
Blackburn
Includes engines of Cirrus Engine Division of Blackburn
''Source: Lumsden''
*Blackburn Cirrus – originally ADC Cirrus
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
,
*Blackburn Cirrus Midget
The Blackburn Cirrus Midget was a British four-cylinder, inverted, inline air-cooled aero engine designed and built in 1937 by the Cirrus Engine Section of Blackburn Aircraft Limited. Little is known of its development and use, its sole aircraf ...
*Blackburn Cirrus Minor
The Blackburn Cirrus Minor is a British four-cylinder, inverted, in-line air-cooled aero-engine that was designed and built by the Cirrus Engine Section of Blackburn Aircraft Limited in the late 1930s.
Design and development
The Cirrus Minor st ...
*Blackburn Cirrus Major
The Blackburn Cirrus Major is a British, inline-four aircraft engine that was developed in the late 1930s.
Design and development
The Blackburn Cirrus Major started life as a continued evolution of the original Cirrus and Hermes series of ai ...
*Blackburn Cirrus Bombardier
The Blackburn Cirrus Bombardier was a British four-cylinder inline aircraft engine, developed and built by the Blackburn Aircraft company in the mid-1950s. The engine featured fuel injection.
Variants
;Cirrus Bombardier 203
:Military version, ...
*Blackburn Cirrus Grenadier[
*Blackburn Cirrus Musketeer][
* Blackburn Nimbus
*Blackburn Artouste – licence built ]Turbomeca Artouste
The Turbomeca Artouste is an early French turboshaft engine, first run in 1947. Originally conceived as an auxiliary power unit (APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopter ...
*Blackburn Turbomeca Palouste – Turbomeca Palouste
The Turbomeca Palouste is a French gas turbine engine, first run in 1952. Designed purely as a compressed air generator, the Palouste was mainly used as a ground-based aircraft engine starter unit. Other uses included rotor tip propulsion for h ...
*Blackburn Turbomeca Palas – Turbomeca Palas
The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca,Gunston 1989, p. 169. ...
*Blackburn Turbomeca Turmo – Turbomeca Turmo
The Turbomeca Turmo is a family of French turboshaft engines manufacturered for helicopter use. Developed from the earlier Turbomeca Artouste, later versions delivered up to . A turboprop version was developed for use with the Bréguet 941 tran ...
* Blackburn A.129
Blackburne
*Blackburne Tomtit
The Blackburne Tomtit was a 670 cc V-twin aero engine for light aircraft that was designed and produced by Burney and Blackburne Limited. Burney and Blackburne was based at Bookham, Surrey, England and was a former motorcycle manufacture ...
*Blackburne Thrush
The Blackburne Thrush was a 1,500 cc three-cylinder radial aero-engine for light aircraft produced by Burney and Blackburne Limited. Burney and Blackburne were based at Bookham, Surrey, England and was a former motorcycle manufacturer.
F ...
Bliss
(E.W. Bliss Company)
* Bliss Jupiter[
* Bliss Neptune][
* Bliss Titan][
]
Bloch
* Bloch 4B-1[
* Bloch 6B-1]
BMW
''Source: Gunston except where noted''
*BMW Sytlphe 5-cyl rotary [
*]BMW III
BMW IIIa was an inline six-cylinder SOHC valvetrain, water-cooled aircraft engine, the first-ever engine produced by Bayerische Flugzeugwerke AG, who, at the time, were exclusively an aircraft engine manufacturer. Its success laid the foundatio ...
*BMW IIIa
BMW IIIa was an inline six-cylinder SOHC valvetrain, water-cooled aircraft engine, the first-ever engine produced by Bayerische Flugzeugwerke AG, who, at the time, were exclusively an aircraft engine manufacturer. Its success laid the foundati ...
*BMW IV
The BMW IV was a six-cylinder, water-cooled inline aircraft engine built in Germany in the 1920s. Power was in the 180 kW (250 hp) range.
World record
On 17 June 1919 Franz Zeno Diemer flew a DFW F37, powered by a BMW IV engine t ...
* BMW V
*BMW Va
__NOTOC__
The BMW V was a six-cylinder, water-cooled inline aircraft engine built in Germany
Germany, officially the Federal Republic of Germany (FRG),, is a country in Central Europe. It is the most populous member state of the Eur ...
*BMW VI
The BMW VI was a water-cooled V-12 aircraft engine built in Germany in the 1920s. It was one of the most important German aero engines in the years leading up to World War II, with thousands built. It was further developed as the BMW VII and ...
* BMW VIIa
*BMW VIII
*BMW IX
*BMW X
BMW X may refer to the following BMW crossovers, SAVs, and SACs:
*BMW X1 (SUV based on 1 Series platform)
*BMW X2 (SUV with coupé roofline, based on X1 platform)
*BMW X3 (SUV based on 3 Series platform)
*BMW X4 (SUV with coupé roofline, based ...
*BMW XI
*BMW 003
The BMW 003 (full RLM designation 109-003) is an early axial turbojet engine produced by BMW AG in Germany during World War II. The 003 and the Junkers Jumo 004 were the only German turbojet engines to reach production during World War II.
...
axial-flow turbojet
*BMW 112 12-cylinder, (prototype)
*BMW 114
The BMW 114 was a nine-cylinder air-cooled radial engine intended for military aircraft use. Developed in 1935 from the BMW 132, with which it could be interchanged, work did not progress beyond experimental prototype engines.
Gunston 1989, p.2 ...
*BMW 116
The BMW 116 was a piston aircraft engine
An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Most aircraft engines are either piston engines or gas turbines, although a few have ...
*BMW 117
The BMW 117 was a piston aircraft engine
An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Most aircraft engines are either piston engines or gas turbines, although a few have be ...
*BMW 132
The BMW 132 was a nine-cylinder radial aircraft engine produced by BMW starting in 1933.
Design and development
BMW took over a license for manufacturing air-cooled radial engines from Pratt & Whitney on 3 January 1928. The nine-cylinder mod ...
*BMW 139
*BMW 801
The BMW 801 was a powerful German air-cooled 14-cylinder-radial aircraft engine built by BMW and used in a number of German Luftwaffe aircraft of World War II. Production versions of the twin-row engine generated between 1,560 and 2,000 PS ( ...
*BMW 802
The BMW 802 was a large air-cooled radial aircraft engine, built using two rows of nine cylinders to produce what was essentially an 18-cylinder version of the 14-cylinder BMW 801. Although promising at first, development dragged on and the pr ...
* BMW 803
*BMW 804
*BMW 805
*BMW 109-002 (Bramo 109-002)
* BMW 109-003
*BMW 109-018
The BMW 018 ( ''RLM'' designation 109-018) was an early axial-flow turbojet engine project by BMW AG in Germany.
Design
The 018 design was begun in 1940. It was generally similar to the BMW 003, but had a twelve-stage axial compressor and th ...
*BMW 109-028
*BMW 109-510
*BMW 109-511
*BMW 109-528
*BMW 109-548
*BMW 109-558
The BMW 109-558 is a liquid fuelled sustainer rocket motor developed by BMW at their Bruckmühl facility, in Germany during the Second World War.
The 109-558 (with the "109-" prefix being the ''Reichsluftfahrtministerium'', or ''RLM'', d ...
*BMW 109-708
*BMW 109-718
The BMW 109-718 was a liquid-fuelled rocket engine developed by BMW at their Bruckmühl facility, in Germany during the Second World War.
Development
The 109-718 (109 prefix number for the ''Reichsluftfahrtministerium'', or ''RLM'', designa ...
*BMW P-3306
*BMW P-3307
*BMW MTU 6011
*BMW 6002
*BMW 6011
*BMW 6012
The BMW 6012 (later MTU 6012) was a German turboshaft and gas generator engine. Designed in the late-1950s by BMW the engine powered the Dornier Do 32 helicopter and was also used as an auxiliary power unit (APU).
Applications
* Dornier D ...
(MTU 6012)
*BMW 8025
*BMW 8026
* BMW GO-480-B1A6
* BMW-Lanova 114 V-4 9-cyl. radial diesel engine
*BMW M2 B15 – 2 cyl. air-cooled boxer
Boeing
''Source:Pelletier except where noted''
*Boeing T50
The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s. An up-rated versio ...
* Boeing T60
*Boeing 500
*Boeing 502
The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s. An up-rated versio ...
*Boeing 514[
* Boeing 520
*Boeing 540 gas turbine engine (turboprop)
* Boeing 550
*Boeing 551 gas turbine engine (turboprop)
*Boeing 553 gas turbine engine (turboprop)
]
Boitel
* Boitel soleil[
]
Boland
*Boland V-8
The Boland V-8 was an aircraft engine that was developed by the Boland Brothers
Frank Edward Boland (July 31, 1873 – January 3, 1913), James Paul Boland (August 20, 1882 – December 19, 1967) and Joseph John Boland (May 27, 1879 – Se ...
Bonner
(Aero Bonner Ltd.)
*Bonner Super Sapphire
Borzecki
(Jozef Borzecki)
*Borzecki 2RB
The Borzecki 2RB is a Polish air-cooled, four-cylinder, horizontally opposed, two-stroke
A two-stroke (or two-stroke cycle) engine is a type of internal combustion engine that completes a Thermodynamic power cycle, power cycle with two strokes ...
*Borzecki JB 2X250
Botali
*Botali Diesel – eight-cylinder air-cooled 118 hp
Bramo
''Source:''Gunston except where noted
* Bramo Sh.14A[
*Bramo 301]
* Bramo 314
*Bramo 322
The Siemens-Halske Sh 22 (also known as SAM 22) was a nine-cylinder aircraft radial engine manufactured by Siemens & Halske in Germany in the 1930s. Following the reorganization of its manufacturer and change in military nomenclature, the engin ...
*Bramo 323 Fafnir
The Bramo 323 ''Fafnir'' is a nine-cylinder radial aircraft engine of the World War II era. Based heavily on Siemens/Bramo's earlier experience producing the Bristol Jupiter under licence, the Bramo 323 saw limited use.
Design and development
D ...
*Bramo 325
*Bramo 328
*Bramo 329 Twin Fafnir
*Bramo 109-002
* Bramo 109-003
Brandner
*Brandner E-300
The Brandner E-300 was an Egyptian turbojet engine, developed for the Helwan HA-300 light jet fighter.
Development
Austrian engineer Ferdinand Brandner, who had worked in the Soviet Union, leading the development of the Kuznetsov NK-12 turbopro ...
Breda
* Breda 320hp V-8[
]
Breguet-Bugatti
*Breguet-Bugatti U.16
The Bugatti U-16 was a 16-cylinder water-cooled double-8 vertical in-line "U engine", designed by Ettore Bugatti in 1915-1916 and built in France in small numbers. The US Bolling Commission bought a license to build the engine in the US, and sm ...
*Breguet-Bugatti U.24
*Breguet-Bugatti U.24bis
*Breguet-Bugatti Quadrimotor Type A
*Breguet-Bugatti Quadrimotor Type B
*Breguet-Bugatti H-32B
Breitfeld & Danek
*Breitfeld & Danek Perun I 6-cylinder 170 hp
*Breitfeld & Danek Perun II 6-cylinder 276 hp
*Breitfeld & Danek BD-500 500 hp
*Breitfeld & Daněk Hiero IV
*Breitfeld & Daněk Hiero L
*Breitfeld & Daněk Hiero N
Breese
* Breese 40hp 3-cyl radial[
]
Breuer
(''Breuer Werke G.m.b.H.'')
*Breuer 9-091
*Breuer 9-094
Brewer
(Captain R.W.A. Brewer)
* Brewer Type M Gryphon O-8[
* Brewer 250hp O-12][
* Brewer 500hp X-16][
]
Briggs & Stratton
*Briggs & Stratton Vanguard Big Block V-Twin
The Briggs & Stratton Vanguard Big Block V-Twin is a series of American piston engines, designed and produced by Briggs & Stratton of Wauwatosa, Wisconsin for use in commercial applications. They have also been adapted for use as ultralight air ...
Bristol Engine Company (Bristol)
Division of Bristol Aeroplane Company
The Bristol Aeroplane Company, originally the British and Colonial Aeroplane Company, was both one of the first and one of the most important British aviation companies, designing and manufacturing both airframes and aircraft engines. Notable a ...
formed when Cosmos Engineering
Cosmos Engineering was a company that manufactured aero-engines in a factory in Fishponds, Bristol during World War I. Sir Roy Fedden, the company's principal designer, developed the 14-cylinder radial Mercury engine during this period. The com ...
was taken over in 1920. Became Bristol Aero Engines in 1956. Merged with Armstrong Siddeley in 1958 to form Bristol Siddeley.
''Sources:'' Piston engines, Lumsden, gas turbine and rocket engines, Gunston.
*Bristol Aquila
The Aquila was a nine-cylinder single-row radial aircraft engine designed by the Bristol Engine Company starting in 1934. A sleeve valve engine, its basic design was developed from the Bristol Perseus. The Aquila was never used in production, ...
*Bristol Centaurus
The Centaurus was the final development of the Bristol Engine Company's series of sleeve valve radial aircraft engines. The Centaurus is an 18-cylinder, two-row design that eventually delivered over . The engine was introduced into service l ...
*Bristol Coupled Centaurus[
*]Bristol Cherub
The Bristol Cherub is a British two-cylinder, air-cooled, aircraft engine designed and built by the Bristol Aeroplane Company. Introduced in 1923 it was a popular engine for ultralight and small aircraft in the 1930s.
Variants
;Cherub I
:Initi ...
* Bristol Draco – fuel injected Pegasus radial
*Bristol Hercules
The Bristol Hercules is a 14-cylinder two-row radial aircraft engine designed by Sir Roy Fedden and produced by the Bristol Engine Company starting in 1939. It was the most numerous of their single sleeve valve ( Burt-McCollum, or Argyll, ...
*Bristol Hydra
The Bristol Hydra (also known as the Double Octagon) was an experimental 16-cylinder, twin-row radial engine, radial aircraft engine built by the Bristol Engine Company. It is a relatively rare example of a radial with an even number of cylind ...
*Bristol Jupiter
The Bristol Jupiter was a British nine-cylinder single-row piston radial engine built by the Bristol Aeroplane Company. Originally designed late in World War I and known as the Cosmos Jupiter, a lengthy series of upgrades and developments tur ...
– originally Cosmos Jupiter
*Bristol Lucifer
The Bristol Lucifer was a British three-cylinder, air-cooled, radial engine for aircraft. Built in the UK in the 1920s by the Bristol Aeroplane Company, it produced 100 horsepower (75 kW).
The Lucifer was originally a Cosmos Engineering e ...
*Bristol Mercury
The Bristol Mercury is a British nine-cylinder, air-cooled, single-row, piston radial engine
The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central c ...
*Bristol Neptune
The Bristol Neptune was a seven-cylinder air-cooled radial engine developed in 1930. It had the same size cylinders as the earlier Mercury and Titan engines, 5.75 in (146 mm) x 6.5 in (165 mm) which gave a displacement of 1,182 cu ...
*Bristol Olympus
The Rolls-Royce Olympus (originally the Bristol B.E.10 Olympus) was the world's second two- spool axial-flow turbojet aircraft engine design, first run in May 1950 and preceded only by the Pratt & Whitney J57, first-run in January 1950. It is ...
*Bristol Orion
The Bristol Orion aero engine was a two-shaft turboprop intended for use in later marks of the Bristol Britannia and the Canadair CL-44. Although the engine was built and underwent a development program, the BE.25 Orion project was cancelled i ...
– Jupiter variant
*Bristol Orion
The Bristol Orion aero engine was a two-shaft turboprop intended for use in later marks of the Bristol Britannia and the Canadair CL-44. Although the engine was built and underwent a development program, the BE.25 Orion project was cancelled i ...
sleeve-valve
*Bristol Orion
The Bristol Orion aero engine was a two-shaft turboprop intended for use in later marks of the Bristol Britannia and the Canadair CL-44. Although the engine was built and underwent a development program, the BE.25 Orion project was cancelled i ...
(BE.25) turbo-prop/shaft
*Bristol Orpheus
The Bristol Siddeley Orpheus was a single-spool turbojet developed by Bristol Siddeley for various light fighter/trainer applications such as the Folland Gnat and the Fiat G.91. Later, the Orpheus formed the core of the first Bristol Pegasus ve ...
*Bristol Pegasus
The Bristol Pegasus is a British nine-cylinder, single-row, air-cooled radial aero engine. Designed by Roy Fedden of the Bristol Aeroplane Company, it was used to power both civil and military aircraft of the 1930s and 1940s. Developed from t ...
(radial engine)
* Bristol BE53 Pegasus (later, BS53 the Harrier engine)
*Bristol Perseus
The Bristol Perseus was a British nine-cylinder, single-row, air-cooled radial aircraft engine produced by the Bristol Engine Company starting in 1932. It was the first production sleeve valve aero engine.
Design and development
In late 1925 ...
*Bristol Phoebus
The Bristol Phoebus was an early turbojet engine developed by Bristol Engines. It was based on the gas generator core of the Bristol Proteus. The Phoebus was used for development but only a handful were made. As with other Bristol engines, it too ...
*Bristol Phoenix
The Phoenix was an experimental version of the Bristol Aeroplane Company's Pegasus engine, adapted to run on the Diesel cycle. Only a few were built between 1928 and 1932, although samples fitted to a Westland Wapiti held the altitude record f ...
diesel radial
*Bristol Proteus
The Bristol Proteus was the Bristol Engine Company's first mass-produced gas turbine engine design, a turboprop that delivered just over 4,000 hp (3,000 kW). The Proteus was a reverse-flow gas turbine. Because the second turbine dro ...
– turboprop
*Bristol Taurus
The Taurus is a British 14-cylinder two-row radial aircraft engine, produced by the Bristol Engine Company starting in 1936. The Taurus was developed by adding cylinders to the existing single-row Aquila design and transforming it into a twi ...
*Bristol Theseus
The Theseus was the Bristol Aeroplane Company's first attempt at a gas-turbine engine design. A turboprop delivering just over 2,000 hp (1,500 kW) was chosen rather than compete with companies that were already developing turbojets. ...
– turboprop
*Bristol Thor
The Bristol Thor, latterly Bristol Siddeley BS.1009 Thor, was a diameter ramjet engine developed by Bristol Aero Engines (later Bristol Siddeley Engines) for the Bristol Bloodhound anti-aircraft missile.
Although Bristol Aero Engines acquire ...
– ramjet
*Bristol Titan
The Bristol Titan was a British five-cylinder air-cooled radial engine, designed and built by the Bristol Aeroplane Company in the late 1920s. It had the same size cylinders as the earlier Bristol Mercury engine, (displacing ), and produced ...
– 5-cylinder radial
Ramjets
*Bristol BE.25
*Bristol BRJ.1 6in ramjet, Initial development model using Boeing combustor.
*Bristol BRJ.2 16in ramjet. Scaled up BRJ1 with Boeing combustor.
*Bristol BRJ.2/5 16in M2 ramjet. Used on early Red Duster. Known to the MoS as BT.1 Thor
*Bristol BRJ.3 16in M2 ramjet. Fitted with NGTE combustor and used on XRD. Rated at at M3, Ø =
*Bristol BRJ.4/1 16in M2 ramjet. Used on early Red Duster and Bloodhound I. Known to the MoS as BT.2 Thor
*Bristol BRJ.5/1 16in M2 ramjet. Used on Bloodhound II. Became BT.3 Thor
*Bristol BRJ.601 16in M3 ramjet. Tested on Bobbin.
*Bristol BRJ.701 23in M3 ramjet project study.
*Bristol BRJ.801[
*Bristol BRJ.801 18in M3 ramjet. Initial M3 ramjet developed for Stage 1 ]Blue Envoy
Blue Envoy (a Rainbow Code name) was a British project to develop a ramjet-powered surface-to-air missile. It was tasked with countering supersonic bomber aircraft launching stand-off missiles, and thus had to have very long range and high-speed ...
.
*Bristol BRJ.811 18in M3 ramjet. M3 ramjet developed for Stage 1 Blue Envoy.
*Bristol BRJ.824 18in M3 ramjet. Cancelled with Blue Steel Mk2.
Bristol Siddeley
Bristol Siddeley
Bristol Siddeley Engines Ltd (BSEL) was a British aero engine manufacturer. The company was formed in 1959 by a merger of Bristol Aero-Engines Limited and Armstrong Siddeley Motors Limited. In 1961 the company was expanded by the purchase of t ...
was formed by Bristol taking over Armstrong Siddeley
Armstrong Siddeley was a British engineering group that operated during the first half of the 20th century. It was formed in 1919 and is best known for the production of luxury vehicles and aircraft engines.
The company was created following ...
, rebranding several of the engines. It took over de Havilland engines and, in turn, became a division of Rolls-Royce Limited.
*Bristol Siddeley BE.58[
*]Bristol Siddeley Pegasus
The Rolls-Royce Pegasus, formerly the Bristol Siddeley Pegasus, is a British turbofan engine originally designed by Bristol Siddeley. It was manufactured by Rolls-Royce plc. The engine is not only able to power a jet aircraft forward, but also ...
(BE.53
*Bristol Siddeley BS.59
* Bristol Siddeley BS.100
*Bristol Siddeley BS.143
*Bristol Siddeley BS.347
*Bristol Siddeley BS.358
*Bristol Siddeley BS.360 -ex de Havilland, finalised as Rolls-Royce Gem
The Rolls-Royce Gem is a turboshaft engine developed specifically for the Westland Lynx helicopter in the 1970s. The design started off at de Havilland (hence the name starting with "G") and was passed to Bristol Siddeley as the BS.360. When ...
* Bristol Siddeley BS.605
*Bristol Siddeley BS.1001 Bristol Siddeley M2.4 – 4.2 ramjet.
*Bristol Siddeley BS.1002 Bristol Siddeley M4.5 ramjet.
*Bristol Siddeley BS.1003 Odin
The Bristol Odin is a ramjet engine originally developed by Bristol Siddeley Engines, later taken over by Rolls-Royce plc, Rolls-Royce.
Odin was specifically designed to power the Sea Dart missile. Unlike the earlier Bristol Thor, Thor ramjet ...
Bristol Siddeley M3.5 ramjet, Odin.
*Bristol Siddeley BS.1004 Bristol Siddeley M2.3 ramjet.
*Bristol Siddeley BS.1005
*Bristol Siddeley BS.1006 Bristol Siddeley M4 research ramjet. Became R.2 research engine.
*Bristol Siddeley BS.1007
*Bristol Siddeley BS.1008 Bristol Siddeley M1.2 ramjet.
*Bristol Siddeley BS.1009 Bristol Siddeley M3 ramjet. Modified BT.3 Thor intended for proposed Bloodhound III. Modified nozzle, intake and diffuser.
*Bristol Siddeley BS.1010
*Bristol Siddeley BS.1011 Rated at 40000 lb (177.9KN).
*Bristol Siddeley BS.1012 Bristol Siddeley combination powerplant for APD 1019 and P.42. Used Olympus or BS.100 turbomachinery, bypass duct burning and ramjets.
*Bristol Siddeley BS.1013 Bristol Siddeley ramjet study for stand-off missile. Possibly for Pandora.
*Bristol Siddeley/SNECMA M45G
* Bristol Siddeley/SNECMA M45H
*Bristol Siddeley Gamma
The Armstrong Siddeley, later Bristol Siddeley Gamma was a family of rocket engines used in British rocketry, including the Black Knight and Black Arrow launch vehicles. They burned kerosene fuel and hydrogen peroxide. Their construction was b ...
(for Black Knight
The black knight is a literary stock character who masks his identity and that of his liege by not displaying heraldry. Black knights are usually portrayed as villainous figures who use this anonymity for misdeeds. They are often contrasted wit ...
)
* Bristol Siddeley Gnome – ex de Havilland
* Bristol Siddeley Gyron Junior ex de Havilland
* Bristol Siddeley Stentor – Ex Armstrong-Siddeley
* Bristol Siddeley Double Spectretwo stacked de Havilland Spectre
The de Havilland Spectre is a rocket engine that was built by the de Havilland Engine Company in the 1950s. It was one element of the intended mixed power-plant for combination rocket-jet interceptor aircraft of the Royal Air Force, such as ...
s
*Bristol Siddeley PR.23[
*Bristol Siddeley PR.37]
*Bristol Siddeley Artouste – licence-built Turbomeca Artouste
The Turbomeca Artouste is an early French turboshaft engine, first run in 1947. Originally conceived as an auxiliary power unit (APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopter ...
*Bristol Siddeley Cumulus
*Bristol Siddeley Nimbus
The Bristol Siddeley Nimbus, later known as the Rolls-Royce Nimbus, was a British turboshaft engine developed under license by Blackburn Aircraft Ltd. from the Turbomeca Turmo in the late 1950s. It was used on the Westland Scout and Westland ...
*Bristol Siddeley Orpheus
The Bristol Siddeley Orpheus was a single-spool turbojet developed by Bristol Siddeley for various light fighter/trainer applications such as the Folland Gnat and the Fiat G.91. Later, the Orpheus formed the core of the first Bristol Pegasus ve ...
*Bristol Siddeley Palouste – licence-built Turbomeca Palouste
The Turbomeca Palouste is a French gas turbine engine, first run in 1952. Designed purely as a compressed air generator, the Palouste was mainly used as a ground-based aircraft engine starter unit. Other uses included rotor tip propulsion for h ...
* Bristol Siddeley Sapphire – ex Armstrong Siddeley
*Bristol Siddeley Spartan I
* Bristol Siddeley T64 (T64-BS-6)
*Bristol Siddeley Viper
The Armstrong Siddeley Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol Siddeley and Rolls-Royce Limited. It entered service in 1953 and remained in use with the Royal ...
*Bristol Siddeley BSRJ.801
*Bristol Siddeley BSRJ.824
*Bristol Siddeley NRJ.1
*Bristol Siddeley R.1 Bristol Siddeley research ramjet.
*Bristol Siddeley R.2 Bristol Siddeley research ramjet.
British Anzani
''For French Anzani engines see: Anzani
Anzani was an engine manufacturer founded by the Italian Alessandro Anzani (1877–1956), which produced proprietary engines for aircraft, cars, boats, and motorcycles in factories in Britain, France and Italy.
Overview
From his native I ...
''
*British Anzani 35hp 2-cyl.
*British Anzani 45hp 6-cyl.
*British Anzani 60hp 6-cyl.
*British Anzani 100hp
The Anzani 10 was a 1913 10-cylinder air-cooled radial aircraft engine. It powered several experimental aircraft and also the later production versions of the Caudron G.3 reconnaissance aircraft, the Caudron G.4 bomber/trainer and the first pro ...
10-cyl.
British Salmson
*British Salmson AD.3
*British Salmson AC.7
*British Salmson AC.9
* British Salmson AD.9
*British Salmson AD.9R srs III
*British Salmson AD.9NG
British Rotary
*British Rotary 100hp 10-cyl. rotary[
]
Brooke
(Brooke, Chicago)
* Brooke 85hp 10-cyl. rotary[
* Brooke 24hp 6-cyl. rotary][
* Brooke Multi-X][
]
Brott
(A. Brott, Denver, Colorado)
* Brott 35hp V-4 air-cooled[
* Brott 45hp V-4 water-cooled][
* Brott 60hp V-8 air-cooled][
]
Brouhot
*Brouhot 60hp V-8[
]
Brownback
(Brownback Motor Laboratories Inc.)
*Brownback C-400 (Tiger 100)[
]
Bucherer
*Bucherer 2-cyl rotary[
]
Buchet
*Buchet 6 in-line[
*Buchet 8-12hp 3-cyl inline
*Buchet 24hp 6-cyl radial ][
]
Bücker
*Bücker M 700
Budworth
(David Budworth Limited)
* Budworth Puffin
* Budworth Brill
* Budworth Buzzard
Bugatti
*Bugatti 8
Automobiles Ettore Bugatti was a German then French manufacturer of high-performance automobiles. The company was founded in 1909 in the then-German city of Molsheim, Alsace, by the Italian-born industrial designer Ettore Bugatti. The cars ...
*Bugatti U-16
The Bugatti U-16 was a 16-cylinder water-cooled double-8 vertical in-line " U engine", designed by Ettore Bugatti in 1915-1916 and built in France in small numbers. The US Bolling Commission bought a license to build the engine in the US, and ...
*Bugatti Type 14
* Bugatti Type 34 U-16
*Bugatti Type 50B
*Bugatti Type 60
Burgess-White
(W. Starling Burgess, Rollin H. White / Burgess Company of Marblehead, MA and White Company of Cleveland, OH)
* Burgess-White X-16[
]
Burlat
(''Société des Moteurs Rotatifs Burlat'')
* Burlat 8cyl. 35hp rotary – at 1800 rpm, . . 6 500F
*Burlat 8cyl. 60hp rotary – at 1800 rpm, , , 11000F
*Burla 8cyl. 75hp rotary – at 1800 rpm, , , 11000F[
*Burlat 16cyl. 120hp rotary – p at 1750 rpm, , , 22000 F]
Burnelli
* Burnelli AR-3
Burt
(Peter Burt)
* Burt 180hp V-12[
]
C
CAC
*CAC R-975 Cicada
* CAC R-1340
*CAC R-1830
The Pratt & Whitney R-1830 Twin Wasp is an American air-cooled radial aircraft engine. It displaces and its bore and stroke are both . The design traces its history to 1929 experiments at Pratt & Whitney on twin-row designs. Production began ...
* CAC Merlin
CAE
''See:Teledyne CAE
Teledyne Turbine Engines (TTE) is a turbine engine manufacturer located in Toledo, Ohio. A division of Teledyne Technologies Inc., TTE is the successor to the former Teledyne CAE.
History
In 1940, Continental Motors Corporation formed Continent ...
''
Caffort
(''Anciens Etablissements Caffort Frères'')
* Caffort 12Aa[
]
Cal-Aero
(Cal-aero Institute, California)
* Cal-Aero Project
Call
(Henry L. Call)
* Call E-1 2OW[
* Call E-2 4OW][
]
CAM
(Canadian Airmotive Inc.)
* CAM TURBO 90[
]
Canton-Unné
* Canton-Unné X-9
Cameron
(Cameron Aero Engine Division / Everett S. Cameron)
* Cameron C4-I-E1[
* Cameron C6][
* Cameron C12][
]
Campini
''Source:Gunston''
* Secondo Campini thermojet
CANSA
(''Fabbrica Italiana Automobili Torino'' – ''Costruzioni Aeronautiche Novaresi S.A.'')
*CANSA C.80
Carden Aero Engines
''Source:Ord-Hume''.
* Carden-Ford 31hp 4-cyl.
* Carden-Ford S.P.1
CAREC
(China National Aero-Engine Corporation)
* CAREC WP-11
Casanova
(Ramon Casanova)
* Casanova pulse-jet
Cato
* Cato 35hp 2-cyl 2OA[
* Cato 60hp 4-cyl 4IL][
* Cato C-2 75 hp 2OA][
]
Caunter
*Caunter B[
*Caunter C]
*Caunter D
Centrum
* Centrum 150hp 6-cyl radial[
]
Ceskoslovenska Zbrojovka
''Data from:''
*Ceskoslovenska Zbrojovka ZOD 260-B 2-stroke radial diesel engine – 260 hp
CFM International
*CFM International CFM56
The CFM International CFM56 (U.S. military designation F108) series is a Franco-American family of high-bypass turbofan aircraft engines made by CFM International (CFMI), with a thrust range of . CFMI is a 50–50 joint-owned company of Saf ...
*CFM International LEAP
The CFM International LEAP ("Leading Edge Aviation Propulsion") is a high-bypass turbofan engine produced by CFM International, a 50–50 joint venture between American GE Aviation and French Safran Aircraft Engines (formerly Snecma). It is the ...
Chaise
(''Societe Anonyme Omnium Metallurgique et Industriel / Etablissements Chaise et Cie'')
* Chaise 12hp V-2
* Chaise 30hp V-4[
* Chaise 4A 101 hp
* Chaise 4B 120 hp (14° inverted V-4)]
* Chaise 4Ba
* Chaise AV.2[
]
Chamoy
(M. Fernand Chamoy)
* Chamoy 5-cyl radial
Chamberlin
*Chamberlin L-236
*Chamberlin L-267
Changzhou
(Changzhou Lan Xiang Machinery Works)
*Changzhou WZ-6
The Turbomeca Turmo is a family of French turboshaft engines manufacturered for helicopter use. Developed from the earlier Turbomeca Artouste, later versions delivered up to . A turboprop version was developed for use with the Bréguet 941 tran ...
Charomskiy
''Source:Gunston''
*Charomskiy AN.1
* Charomskiy ACh-30
*Charomskiy ACh-31
*Charomskiy ACh-32
*Charomskiy ACh-39
*Charomskiy M-40
The Charomskiy M-40 was a Soviet turbocharged aircraft diesel engine developed during World War II. It was used in a few Petlyakov Pe-8 heavy bombers until August 1941 when it was removed, because it was unreliable at high altitudes. The engines w ...
Chelomey
* Chelomey D-3 Pulse-jet
*Chelomey D-5 Pulse-jet
*Chelomey D-6 Pulse-jet
*Chelomey D-7 Pulse-jet
Chenu
* Chenu 50-65hp 4-cyl DD [
* Chenu 75hp 6-cyl in-line ]
* Chenu 90hp 4-cyl GD [
* Chenu 80-90hp 6-cyl DD][
* Chenu 80-90hp 6-cyl GD][
* Chenu 200-250hp 6-cyl DD ] (for dirigibles)[
]
Chengdu
* Chengdu WS-18
Chevrolair
(The Arthur Chevrolet Aviation Motors Corporation)
* Chevrolair 1923 Water-cooled in-line 4 upright[
* Chevrolair D-4][
* Chevrolair D-6]
* Chevrolair 1923 Air-cooled in-line 4 upright and inverted
Chevrolet
* Chevrolet Turbo-Air 6 engine
The Chevrolet Turbo-Air 6 is a flat-six air-cooled automobile engine developed by General Motors (GM) in the late 1950s for use in the rear-engined Chevrolet Corvair of the 1960s. It was used in the entire Corvair line, as well as a wide varie ...
Chinese aero-engines
Chotia
*Chotia 460
Christoffersen
(Christoffersen Aircraft Company)
* Christoffersen 120hp 6-cyl in-line[
* Christoffersen 120hp V-12][
]
Chrysler
*Chrysler IV-2220
The Chrysler XIV-2220 (XI-2220 from 1944) was an experimental 2,500 hp, 2,220 cubic inch (36.4 liter) liquid-cooled inverted- V-16 aircraft engine designed by Chrysler starting in 1940. Although several aircraft designs had considered using ...
* Chrysler T36D
Church
(Jim Church)
* Church J-3 Marathon
* Church V-248 V-8
Cicaré
*Cicaré 4C2T
The Cicaré 4CT2 is an Argentine air-cooled, four-cylinder, horizontally opposed, two-stroke
A two-stroke (or two-stroke cycle) engine is a type of internal combustion engine that completes a power cycle with two strokes (up and down movement ...
Cirrus
* Cirrus I
* Cirrus II
*Cirrus III
The ADC Cirrus is a series of British aero engines manufactured using
surplus Renault parts by the Aircraft Disposal Company (ADC) in the 1920s.
The engines were air-cooled, four-cylinder inline types. They were widely used for private and l ...
*Cirrus Hermes
The Cirrus and Hermes or Cirrus-Hermes are a series of British aero engines manufactured, under various changes of ownership, from the 1920s until the 1950s. The engines were all air-cooled, four-cylinder inline types, with earlier ones upright an ...
*Cirrus Major
The Blackburn Cirrus Major is a British, inline-four aircraft engine that was developed in the late 1930s.
Design and development
The Blackburn Cirrus Major started life as a continued evolution of the original Cirrus and Hermes series of ai ...
* Cirrus Minor
Cisco Motors
* Cisco Snap 100
Citroën
* Citroen 2cyl Citroën 2CV – 18 hp
* Citroen 4cyl Citroën GS 1.2 – 65 hp at 5,700 rpm
Clapp's Cars
* Clapp's Cars Spyder Standard
The Standard is a 4 stroke aircraft engine for Homebuilt aircraft
Design and development
The engine is based on the Corvair engine. It is extensively modified for aircraft use. This modification consists of an IFB Internal front bearing modifi ...
Clément-Bayard
''Data from:''
*Clément-Bayard 30hp 2-cyl HOW[
*Clément-Bayard 29hp 4-cyl in-line][
*Clément-Bayard 40hp 4-cyl in-line][
*Clément-Bayard 100hp 4-cyl in-line ]
*Clément-Bayard 118.5hp 4-cyl in-line[
*Clément-Bayard 117.5hp 6-cyl in-line][
*Clément-Bayard 250hp 6-cyl in-line][ (for dirigibles)
*Clément-Bayard 50hp 7-cyl Radial][
*Clément-Bayard 300hp 8-cyl in-line][ (for airships)
*Clément-Bayard V-16][ (for airships)
]
Cleone
* Cleone 1930 25hp 2-cyl hor opp 2 stroke
Clerget
('' Société Clerget-Blin et Cie'' / Pierre Clerget)
Source:Lumsden except where noted
*Clerget 50hp 7-cyl water-cooled radial (1907)
*Clerget 50hp 4-cyl[
*Clerget 100hp 4-cyl][
*Clerget 200hp V-8][ ]
*Clerget 2K 16 hp[ ]
*Clerget 4V 40 hp 4-cyl in-line water-cooled (1908)
*Clerget 4W 40 hp 4-cyl in-line water-cooled (1910)
*Clerget 7Y 60 hp[
*]Clerget 7Z
The Clerget 7Z was a seven-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. First appearing in 1911 it was nominally rated at 80 horsepower (60 kW). 347 examples were jointly built in Britain by Gordon Watne ...
*Clerget 9A
Clerget was the name given to a series of early rotary aircraft engine types of the World War I era that were designed by Pierre Clerget. Manufactured in France by Clerget-Blin and in Great Britain by Gwynnes Limited they were used on such airc ...
(Diesel radial engine)
*Clerget 9B
The Clerget 9B was a nine-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. Manufactured in both France and Great Britain ( Gwynnes Limited), it was used on such aircraft as the Sopwith Camel. The Clerget 9Bf wa ...
*Clerget 9B
The Clerget 9B was a nine-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. Manufactured in both France and Great Britain ( Gwynnes Limited), it was used on such aircraft as the Sopwith Camel. The Clerget 9Bf wa ...
f British version of 9B 140 hp[
*]Clerget 9C
Clerget was the name given to a series of early rotary aircraft engine types of the World War I era that were designed by Pierre Clerget. Manufactured in France by Clerget-Blin and in Great Britain by Gwynnes Limited they were used on such air ...
*Clerget 9F[
*Clerget 9J 100 hp][
*]Clerget 9Z
Clerget-Blin (full name being ''Société Clerget-Blin et Cie'') was a French precision engineering company formed in 1913 by the engineer and inventor Pierre Clerget and industrialist Eugène Blin. In 1939, the company was absorbed into the ''Gr ...
110 hp
*Clerget 11A 200 hp variable compression[
* Clerget 11Eb
*Clerget 11G 250 hp][ 5.7:1 compression
*Clerget 14D]
*Clerget 14E
*Clerget 14F (Diesel radial engine)
**Clerget 14Fcs
**Clerget 14F1
**Clerget 14F2
*Clerget 14U
*Clerget 16H diesel V-16 (180x200=81.43L
*Clerget 16SS diesel
*Clerget 16X
The Clerget 16X was an experimental French 16-cylinder X engine built in about 1918.
Design
Clerget are best known for their well engineered rotary engines produced from 1911 to the end of World War I in 1918, the first of their type to deliver ...
*Clerget 18 rotary 300 hp[
*Clerget 32 diesel]
*Clerget Type Transatlantique (H type)
*Clerget monocylinder powder powdered coal test engine
*Clerget monocylinder 2x variable compression
*Clerget monocylinder 4x variable compression
*Clerget 180-2T V-8 2x variable compression
*Clerget 180-4T V-8 4x variable compression
*Clerget 100hp diesel 1928 9-cyl. radial[
*Clerget 200hp diesel 1929 9-cyl. radial][
*Clerget 250hp diesel 9-cyl. radial]