Bristol Type 95
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The Bristol Bagshot, also known as the Type 95, was a prototype heavily armed British fighter built by the
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 ...
and first flown in 1927. Flight testing revealed serious problems, and the project was abandoned.


Development

The Bagshot was built to Air Ministry Specification F.4/24 in December 1924. This called for a large twin-engined fighter aircraft with a crew of three (pilot and two gunners), a maximum speed of , and a landing speed of .Mason 1992, p. 191. Initially, the details of the required armament were not specified.
Frank Barnwell Captain Frank Sowter Barnwell OBE AFC FRAeS BSc (23 November 1880 – 2 August 1938) was a Scottish aeronautical engineer. With his elder brother Harold, he built the first successful powered aircraft made in Scotland and later went on to a ...
's design to meet this requirement, the Bagshot, was a high-wing all-metal monoplane with an unusual triangular-section fabric-covered steel-tube
fuselage The fuselage (; from the French language, French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds Aircrew, crew, passengers, or cargo. In single-engine aircraft, it will usually contain an Aircraft engine, engine as wel ...
with two upper
longerons In engineering, a longeron or stringer is a load-bearing component of a framework. The term is commonly used in connection with aircraft fuselages and automobile chassis. Longerons are used in conjunction with stringers to form structural frame ...
and a single lower member. The pilot sat in line with the wing's leading edge, with one gun positioned in the nose and another just behind the wing. The two-spar wing had a steel primary structure and
duralumin Duralumin (also called duraluminum, duraluminium, duralum, dural(l)ium, or dural) is a trade name for one of the earliest types of age hardening, age-hardenable aluminium–copper alloys. The term is a combination of ''Düren'' and ''aluminium'' ...
nose ribs and end-members, and was a semi-
cantilever A cantilever is a rigid structural element that extends horizontally and is unsupported at one end. Typically it extends from a flat vertical surface such as a wall, to which it must be firmly attached. Like other structural elements, a cantilev ...
, braced by a pair of diagonal struts on each side. The legs of the fixed undercarriage met the wing at the same place as the struts and had an axle fairing of airfoil section, contributing some lift. Power was provided by two wing-mounted
Bristol Jupiter The Bristol Jupiter is a British nine-cylinder single-row piston radial engine that was 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 developme ...
VI engines. In September 1925 the Air Ministry amended the specification, calling for
supercharger In an internal combustion engine, a supercharger compresses the intake gas, forcing more air into the engine in order to produce more power for a given displacement (engine), displacement. It is a form of forced induction that is mechanically ...
s on the engines, increased fuel load and a higher top speed at altitude. Barnwell attended a design conference to discuss these new demands and was told that the purpose of the aircraft was to carry a pair of
Coventry Ordnance Works Coventry Ordnance Works was a British manufacturer of heavy guns particularly naval artillery jointly owned by Cammell Laird & Co of Sheffield and Birkenhead, Fairfield Shipbuilding and Engineering Company of Govan, Glasgow and John Brown & Comp ...
/a>guns, generally called COW guns. When Barnwell received the full details of the required equipment, which included two Lewis guns in addition to the main armament, he realised that the aircraft would be overweight and have a landing speed of . He suggested making an alternative fuselage of rolled steel strip to save weight, and abandoning the project as a waste of time if load testing of this proved unsatisfactory. The Air Ministry declined to cancel the contract and the Bagshot was completed, being provisionally accepted by the Air Ministry on 12 May 1927 and assigned serial number J7767.


Operational history

The Bagshot was first flown without any armament at Filton on 15 July 1927 by
Cyril Uwins Cyril Frank Uwins OBE, AFC, FRAeS (1896–1972) was a British test pilot who worked for Bristol Aeroplane Company, where he made the first flight of 58 types of aircraft. On 16 September 1932 he broke the world aeroplane height record by climbin ...
, Bristol's chief test pilot.Russell, p. 20. This first flight was short: 'Always a bad sign' remarked
Archibald Russell Sir Archibald Russell, CBE, FRS (30 May 1904 – 29 May 1995) was a British aerospace engineer who worked most of his career at the Bristol Aeroplane Company, before becoming managing director of the Filton Division when Bristol merged into Bri ...
(later Sir Archibald), who, at that time, was working in the stress calculations office at Filton. Uwins reported that control in the roll axis was poor. A second flight, during which Uwins increased the speed to , revealed that the problem became worse as the speed increased. Uwins was unable to observe the wing's behaviour (He had a damaged neck thanks to an aircraft accident). It was decided that the aircraft was safe enough to carry an observer if the speed was kept down and Russell, who had recently been working on measuring the deflection of the aircraft's wing spars under load, was given the job. The rear gun position gave an excellent view of the wing. Uwins and Russell agreed on a simple system of hand signals to communicate. By the time the aircraft reached the agreed speed and height for the trials Russell was already very concerned. Although the "writhing movements" of the wing were "large and alarming" he had no signal to tell Uwins that enough was enough and so the whole planned flight program was flown.Russell, p. 21. It was concluded that
control reversal Control reversal is an adverse effect on the controllability of aircraft. The flight controls reverse themselves in a way that is not intuitive, so pilots may not be aware of the situation; to roll to the left, they have to push the control stick ...
resulting from twisting of the wing when the
aileron An aileron (French for "little wing" or "fin") is a hinged flight control surface usually forming part of the trailing edge of each wing of a fixed-wing aircraft. Ailerons are used in pairs to control the aircraft in roll (or movement aroun ...
s were applied was the cause of the problems. The aircraft was grounded for a structural test to be made. It was transferred to the Air Ministry's experimental unit and briefly flown during 1931 but shortly afterwards broken up for scrap.


Specifications


References


Notes


Bibliography

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