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Bristol Type 138 : ウィキペディア英語版
Bristol Type 138

The Bristol Type 138 High Altitude Monoplane was a British high-altitude research aircraft of the 1930s. It was a single-engine, low-wing monoplane with a fixed, tailwheel undercarriage.
==Design and development==
The Type 138 was born of a period of intense competition between aviation manufacturers in the 1920s and 1930s. There was a great deal of prestige, as well as technological progress, to be gained from breaking any of the major aviation records: airspeed, distance and altitude. By the 1930s absolute speed and distance records were beyond the resources of individual companies, and required the involvement of national governments.
Bristol were well placed to compete in this field but in the event they found themselves lagging. Between 1929 and 1934, there were a number of altitude records established by rival machines including a Junkers W.34, a Vickers Vespa and a Caproni Ca.113 biplane, as well as the first flight over Everest by a pair of Westland Wallaces in 1933; all these aircraft used Bristol or Bristol-designed engines.〔Barnes 1964, p. 254.〕
Sensing Air Ministry interest resulting from the success of the Everest flight, Barnwell proposed a purpose-built high-altitude research aircraft in November 1933. This, the Type 138, was a large single-engine, single-seat monoplane with retractable undercarriage and a supercharged Pegasus engine.〔Winchester 2005, pp. 26–27.〕 Nothing came of this until Renato Donati set a new record in April 1934; public opinion demanded a new, government-sponsored record attempt.〔 In June, the Air Ministry issued Specification 2/34 for two prototypes capable of reaching 50,000 ft (15,030 m).〔Thetford 1957, pp. 102–103.〕 Barnwell revised the Type 138 to produce the Type 138A. This was of the original size and configuration but had a special, two-stage supercharged, Pegasus and, although remaining basically a single-seater, had provision for an observer's cockpit to be fitted if required. Weight-saving was a priority; the airframe other than the steel tube engine mount was a wooden monocoque and the undercarriage was replaced with a lightweight, fixed assembly.〔Winchester 2005, p. 26.〕
The supercharger installation, with detail work by Clifford Tinson, was a two-stage system; the first-stage compressor was permanently engaged but the second-stage was engaged by the pilot at the correct height. The system employed an intercooler between first and second stages.〔
Considerable research was carried out by the Royal Aircraft Establishment and National Physical Laboratory both to establish the most efficient design for the aircraft and to develop a reliable pressure suit for the pilot. Sir Robert Davis of Siebe Gorman and Professor J.S. Haldane were instrumental in developing the helmet.〔("Bristol Type 138." ) ''Flight,'' 1 October 1936.〕
The airframe was complete in early 1936 and the Type 138A was flown for the first time on 11 May with a standard Pegasus IV driving a three-bladed propeller, piloted by Cyril Uwins, who had flown the Vickers Vespa on its world record flight. Two more flights were made at Filton before the aircraft was delivered to Farnborough, where tests of the pressure helmet were made before the aircraft was returned to Filton for the special Pegasus and four-blade airscrew to be fitted, being returned to Farnborough on 5 September.〔("Height record home again." ) ''Flight,'' 8 July 1937.〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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