FIELD: aeronautical engineering. SUBSTANCE: motor glider 1 has fuselage 2 with wing 3, center-wing section, tail 5 and power plant 6 which consists of engine with reduction gear; motor glider is also provided with propeller 9. Engine 7 is connected to fuselage 2 in area of center-wing section; it is oriented upwards by axis of output shaft. Engine is provided with pylon with transmission inside it. Pusher propeller 9 is provided with automatic operating mechanism 14 for unfolding and folding the propeller in flight. Invention contains description of units for attachment of engine to its mount. EFFECT: enhanced reliability. 12 cl, 14 dwg
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Authors
Dates
1997-02-20—Published
1993-09-24—Filed