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Walter M601
The Walter M601 is a turboprop aircraft engine produced by Walter Aircraft Engines of the Czech Republic. The company's first turboprop, the M601 is used in business, agricultural and military training aircraft. Development The turboprop was designed for use on the Let L-410 Turbolet, Let L-410 and the M601 first ran in 1967. It was not suitable for the prototype L-410 and the company developed an upgraded version, the M601A, with a slightly wider diameter. Variants ;M601A: :Initial production variant for early version of the Let L410. ;M601B: :Production variant for the Let L410UVP. ;M601D :Developed for the Let L410UVP. ;M601D-1: :Agricultural variant for high-cycle operation, used on the PZL Kruk and Ayres Thrush. ;M601D-2: :Special variant for paradrop aircraft, used on the Do 28 and some Finist conversions. ;M601D-11: :Agricultural and paradrop variant with a higher Time Between Overhaul of up to 1800 hours. ;M601D-11NZ: :Downrated variant for use in the FU-24 Fletcher. ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
WikiProject Aircraft
A WikiProject, or Wikiproject, is an affinity group for contributors with shared goals within the Wikimedia movement. WikiProjects are prevalent within the largest wiki, Wikipedia, and exist to varying degrees within Wikimedia project, sibling projects such as Wiktionary, Wikiquote, Wikidata, and Wikisource. They also exist in different languages, and translation of articles is a form of their collaboration. During the COVID-19 pandemic, CBS News noted the role of Wikipedia's WikiProject Medicine in maintaining the accuracy of articles related to the disease. Another WikiProject that has drawn attention is WikiProject Women Scientists, which was profiled by ''Smithsonian Magazine, Smithsonian'' for its efforts to improve coverage of women scientists which the profile noted had "helped increase the number of female scientists on Wikipedia from around 1,600 to over 5,000". On Wikipedia Some Wikipedia WikiProjects are substantial enough to engage in cooperative activities with outsi ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Zlín Z 37
Zlín (in 1949–1989 Gottwaldov; ; ) is a city in the Czech Republic. It has about 75,000 inhabitants. It is the seat of the Zlín Region and it lies on the Dřevnice River. It is known as an industrial centre. The development of the modern city is closely connected to the Bata Shoes company and its social scheme, developed after World War I. A large part of Zlín is urbanistically and architecturally valuable and is protected as an urban monument zone. Administrative division Zlín consists of 16 municipal parts (in brackets population according to the 2021 census): *Zlín (48,317) *Prštné (3,345) *Louky (1,027) *Mladcová (2,525) *Příluky (2,931) *Jaroslavice (822) *Kudlov (2,195) *Malenovice (7,156) *Chlum (144) *Klečůvka (332) *Kostelec (1,909) *Lhotka (235) *Lužkovice (634) *Salaš (195) *Štípa (1,798) *Velíková (613) Prštné, Louky, Mladcová, Příluky, Jaroslavice, Kudlov and Malenovice are urbanistically fused with Zlín. They are sometimes called Zlín I ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
List Of Aircraft Engines
This is an alphabetical list of aircraft engines by manufacturer. 0–9 2si *2si 215 *2si 230 *Cuyuna 430, 2si 430 *2si 460 *2si 500 *2si 540 *2si 690 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 * ABC 30 hp V-4 * ABC 45 hp V-6 * ABC 60 hp V-8 * ABC 85 hp V-6 * ABC 100 hp V-8 * ABC 115 hp * ABC 170 hp V-12 * ABC 225 hp V-16 *ABC Dragonfly *ABC Gadfly *ABC Gnat *ABC Hornet *ABC Mosquito *ABC Scorpion *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 Amer ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Pratt & Whitney Canada PT6
The Pratt & Whitney Canada PT6 is a turboprop aircraft engine produced by Pratt & Whitney Canada. Its design was started in 1958, it first ran in February 1960, first flew on 30 May 1961, entered service in 1964, and has been continuously updated since. The PT6 consists of two basic sections: a gas generator with accessory gearbox, and a free-power turbine with reduction gearbox. In aircraft, the engine is often mounted "backwards," with the intake at the rear and the exhaust at the front, so that the turbine is directly connected to the propeller. Many variants of the PT6 have been produced, not only as turboprops but also as turboshaft engines for helicopters, land vehicles, hovercraft, and boats; as auxiliary power units; and for industrial uses. By November 2015, 51,000 had been produced, which had logged 400 million flight hours from 1963 to 2016. It is known for its reliability, with an in-flight shutdown rate of 1 per 651,126 hours in 2016. The PT6A turboprop engine c ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Klimov VK-800
The Klimov VK-800 is a turboshaft engine of the fifth generation. It is designed to equip the Mi-54, Ansat and Ka-226 "Sergei" type helicopters. The VK-800V derivative was developed for the power units of helicopters of small and large load-carrying capacity, both in twin- and single-engine configuration. The engine parameters meet the requirements of the tested model of a centrifugal compressor and the single-stage un-cooled turbines. All this simplifies the engine design and reduces expenses for its manufacture and operation. Moreover, the enhanced characteristics of the main units of the engine provide its high efficiency. History This multipurpose engine core was disclosed at the Moscow 'Engines 98' exhibition. At that time test-bed running was said to be about to begin, but by 2004 development had been suspended, for lack of funds. Some literature gave the designation as VKS-800, the S highlighting participation by Motor Sich, which in 2000 described this engine as a joi ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Garrett TPE331
The Honeywell TPE331 (military designation: T76) is a turboprop engine. It was designed in the 1950s by Garrett AiResearch, and produced since 1999 by successor Honeywell Aerospace. The engine's power output ranges from . Design and development Garrett AiResearch designed the TPE331 from scratch in 1959 for the military. “Designed as a 575-horsepower engine it was not a scaled-down version of a larger engine, as competitors were offering.” The TPE331 originated in 1961 as a gas turbine (the "331") to power helicopters. It first went into production in 1963. More than 700 had been shipped by the end of 1973. It was designed to be both a turboshaft A turboshaft engine is a form of gas turbine that is optimized to produce shaft horsepower rather than jet thrust. In concept, turboshaft engines are very similar to turbojets, with additional turbine expansion to extract heat energy from the ex ... (TSE331) and a turboprop (TPE331), but the turboshaft version never went into ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Centrifugal Compressor
Centrifugal compressors, sometimes called impeller compressors or radial compressors, are a sub-class of dynamic axisymmetric work-absorbing turbomachinery. They achieve pressure rise by adding energy to the continuous flow of fluid through the rotor/impeller. The equation in the next section shows this specific energy input. A substantial portion of this energy is kinetic which is converted to increased potential energy/static pressure by slowing the flow through a diffuser. The static pressure rise in the impeller may roughly equal the rise in the diffuser. Components of a simple centrifugal compressor A simple centrifugal compressor stage has four components (listed in order of throughflow): inlet, impeller/rotor, diffuser, and collector. Figure 1.1 shows each of the components of the flow path, with the flow (working gas) entering the centrifugal impeller axially from left to right. This turboshaft (or turboprop) impeller is rotating counter-clockwise when looking downs ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Axial Compressor
An axial compressor is a gas compressor that can continuously pressurize gases. It is a rotating, airfoil-based compressor in which the gas or working fluid principally flows parallel to the axis of rotation, or axially. This differs from other rotating compressors such as centrifugal compressor, axi-centrifugal compressors and mixed-flow compressors where the fluid flow will include a "radial component" through the compressor. The energy level of the fluid increases as it flows through the compressor due to the action of the rotor blades which exert a torque on the fluid. The stationary blades slow the fluid, converting the circumferential component of flow into pressure. Compressors are typically driven by an electric motor or a steam or a gas turbine. Axial flow compressors produce a continuous flow of compressed gas, and have the benefits of high efficiency and large mass flow rate, particularly in relation to their size and cross-section. They do, however, require several ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Turbine Legend
The Performance Turbine Legend is an American sports monoplane designed by Performance Aircraft for sale as a kit for Homebuilt aircraft, amateur construction.Vandermeullen, Richard: ''2012 Kit Aircraft Buyer's Guide'', Kitplanes, Volume 28, Number 12, December 2011, page 59. Belvoir Publications. ISSN 0891-1851 Design and development The Legend is a streamlined low-wing monoplane mainly constructed of carbon-fiber-reinforced polymer. It has swept-back tail surfaces with a mid-mounted tailplane and tapered wings, with optional winglets. The prototype was powered by a Chevrolet V-8 engine with a three-bladed tractor propeller and a ventral air-scoop, the Turbine Legend has a Walter M601 turboprop with a three-bladed tractor propeller. The Legend has a retractable tricycle landing gear; the mainwheels retract inwards and the nosewheel rearwards. The enclosed cockpit has room for two persons in tandem seats with dual controls and has a rear-hinged, upward-opening, canopy with a f ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Technoavia Rysachok
The Technoavia Rysachok (Ru:Рысачок, ) is a general purpose, twin turboprop-powered engined light utility aircraft, designed and built in Russia by Technoavia. Certification was expected by 2012 and by autumn 2011 three flight pre-production examples had been completed and flown. As of 2015 the certification process is stalled and Technoavia has declared that it is no longer involved in the project. Design and development The Rysachok programme development began in 2006. It was designed as a twin engine conversion trainer but is now seen more generally as an Antonov An-2 replacement in medical, survey, parachuting, navigator and air engineer training and other light transport roles. The Rysachok is a conventionally laid out low wing, twin engine monoplane. Outboard of the engines the wings have constant chord (aircraft), chord and blunt wing tips; inboard, the chord increases toward the fuselage via sweep on the trailing edge. The starboard aileron carries a trim tab and ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Technoavia SM92 Finist
The Technoavia SM92 Finist is STOL utility aircraft, designed by the Russian company Technoavia which first flew on the 28 December 1993. It is built at the Smolensk Aviation Plant. Variants ; SM92 Finist :Basic version, powered by 270 kW (360 hp) Vedeneyev M14P radial engine.Taylor 1999, p.482. ; SM92P Finist :Armed version for Border guard duties. Two fixed forward firing PK machine guns and one inside cabin firing through open cabin doors and two rocket launchers. ; SM-92T Turbo Finist :Version powered by Walter M601 turboprop engine. One prototype converted.Simpson, Longley & Swan 2022, p. 90 ; SMG-92 Turbine Finist :Walter M601 powered version built in Slovakia by Aerotech Slovakia for use in skydiving.Technoavia SP-91 . ''Yak UK''. Retrieved 29 November 2009. At least six converted. ; Zlin Z400 :Ve ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
PZL-106 Kruk
The PZL-106 Kruk () is a Polish agricultural aircraft designed and built by Państwowe Zakłady Lotnicze, WSK PZL Warszawa-Okęcie (later PZL "Warszawa-Okęcie" and now EADS-PZL). Design and development The PZL-106 was developed as a modern agricultural aircraft for Poland and Comecon countries to replace the less-capable PZL-101 Gawron and aging PZL Antonov An-2. (According to Comecon decisions, Polish industry was responsible for developing agricultural aircraft). There were several agricultural plane designs proposed in the early 1960s by a group of young designers from WSK PZL Warszawa-Okęcie, led by Andrzej Frydrychewicz. These proposals were made on their own initiative, but they were never realized because the USSR was content with the An-2 and was planning to replace it with a jet aircraft (later PZL M-15 Belphegor). The first was the PZL-101M Kruk 63 of 1963. That remained a paper airplane, but it did give its name to later designs. Next were the PZL-106 Kruk 65 (1965) ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
