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Vickers Viastra : ウィキペディア英語版
Vickers Viastra

The Vickers Viastra was an all-metal 12-seat passenger high-wing monoplane, with variants powered by one, two and three engines. Two twin-engined Viastras operated commercially in Australia from 1931-6; another served as a Royal transport.
==Development==
The Vickers-Wibault construction method was based on the patents of Michel Wibault, who began working with Vickers in 1922. It was a way of producing an all-metal aircraft with an airframe built up from simple, non-machined metal shapes, covered with very thin e.g. 0.016 in (0.4 mm) corrugated light alloy sheets. Skin panels were riveted to each other and to the underlying structure; the skin on the wings was not stressed. Vickers' first experience of the method was with the licence built Wibault Scout. The first Vickers design using this construction was the Vireo and the third, the Viastra, used a blend of Wibault and Vickers construction techniques.〔
The Viastra was envisaged as a one or three-engined commercial aircraft capable of carrying ten passengers and designed with an eye to operations in countries with poor surface transport facilities. Vickers built several variants, largely similar apart from the engines: ultimately, there were Viastras with one, two and three engines. They were high-wing monoplanes, the wings having constant chord, square tips and a thick Raf 24 section. The wings, like the rest of the aircraft were covered with the corrugated skin and carried balanced ailerons and outboard slots. There was a biplane tail unit with a pair of narrow chord planes, the lower attached to the fuselage underside and the upper mounted clear above. The outboard vertical tail surfaces were again very narrow and served as the main rudders; the single-engined and tri-motor variants also had a small triangular central fin, carrying an auxiliary rudder and supporting the upper horizontal plane. With one exception, the twin-engined Viastras had the central fin and rudder replaced by tubular bracing.
The fuselage had a square cross-section, parallel in the passenger cabin area and narrowing towards the tail. The passenger compartment had six rectangular windows on each side and the crew had an enclosed cabin forward of the wings. Each wing was braced to the lower fuselage with a parallel pair of struts; the forward of these was used to carry a main undercarriage leg with the help of further robust strutting. The two and three-engined Viastras had their outer engines mounted just below the wings. The outer engines were enclosed by a narrow chord Townend ring, but the central engines of the tri-motored and single-engined Viastras were uncowled.〔

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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