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Morane-Borel monoplane
The Morane-Borel monoplane (sometimes referred to with the retronym Morane-Saulnier Type A or simply the Morane monoplane) was an early French single-engine, single-seat aircraft. It was flown in several European air races.
==Design==
The Monoplane was a mid-wing tractor configuration monoplane powered by a 50 hp Gnome Omega 7 cylinder rotary engine driving a two-bladed Chauvière ''Intégrale'' propeller. The fuselage was a rectangular section wire-braced box girder, with the forward part covered in plywood and the rear part fabric covered: the rear section was left uncovered in some examples. The two-spar wings had elliptical ends and were braced by a pyramidal cabane in front of the pilot and an inverted V strut underneath the fuselage behind the undercarriage. Lateral control was effected by wing warping and the empennage consisted of a fixed horizontal stabiliser with tip-mounted full-chord elevators at either end and an aerodynamically balanced rudder, with no fixed vertical surface. In later examples the horizontal surfaces were modified, and consisted of a fixed surfacee with balanced elevators hinged to the trailing edge.〔(The Borel Monoplane )''Flight 20 July 1912 p. 651〕 The undercarriage consisted of a pair of short skids each carried on a pair of struts and a pair of wheels on a cross axle bound to the skids by bungee cords and a tailskid.
A two-seat version was later produced, with the fuselage lengthened to and wingspan increased to .〔
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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