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Westland Wallace : ウィキペディア英語版
Westland Wallace

The Westland Wallace was a British two-seat, general-purpose biplane of the Royal Air Force, developed by Westland as a follow-on to their successful Wapiti. As the last of the inter-war general purpose biplanes, it was used by a number of front line and Auxiliary Air Force Squadrons. Although the pace of aeronautical development caused its rapid replacement in front line service, its useful life was extended into the Second World War with many being converted into target tugs and wireless trainers. In 1933 a Westland Wallace became the first aircraft to fly over Mount Everest, as part of the Houston Mount Everest Expedition.〔''The Times'', 15 February 1933.〕
==Design and development==
In 1931, Westland produced the PV-6, a private-venture development of its successful Wapiti. This updated aircraft embodied a number of improvements including a lengthened fuselage, brakes and wheel spats on the undercarriage and a new engine. By this time both the appearance and performance differed considerably from the standard Wapiti, so the company designated it the "PV6 Wallace." Compared with the earlier Wapiti, the Wallace was 20 inches (0.5 m) longer, incorporated an improved undercarriage and was powered by a 655 hp (488 kW) Bristol Pegasus IV engine. The first batches of MK I Wallaces were conversions of Wapitis, a total of 68 powered by 570 bhp (425 kW) Pegasus IIM3 engines.
Westland designed an improved version, the Mk II which fitted with a more powerful engine and the then-novel idea of an enclosed canopy over both crew positions. This offered greater comfort for the crew and improved the rear gunner's aim by protecting him from the slipstream. Three Wallace Is (''K4346''-''K4348'') were later converted to Mk II standards, including fitting the closed canopy.

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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