发明名称 Convertible fixed wing aircraft
摘要 A fixed wing aircraft that can be converted to an automotive vehicle, comprising a generally rectangular planform fuselage having four wheels as in conventional automobile practice, and a telescopic wing which retracts into a housing in the roof of the fuselage. Telescopic horizontal and vertical stabilizers are provided at the rear end of the fuselage, as well as a retractable pusher propeller that is driven by an engine mounted on the front end of the fuselage. Both the propeller and the rear wheels are connected by a transmission box to the engine, so that either can be driven to operate the vehicle as an aircraft or as an automobile. On take-off, the rear wheels are partially retracted so as to place the aircraft at a proper angle of attack at the same time that the elevators are raised by pulling back on the control wheel. The control wheel is also connected to both the front wheels and the ailerons, and when turned 90 DEG to the left or right while in the flight configuration, causes the ailerons to move to their extreme angular positions while the front wheels are turned only a minimal amount. Further turning of the control wheel causes the front wheels to turn to their full angular position, without causing further movement of the ailerons. The wing is also movable longitudinally with respect to the fuselage so as to trim the aircraft for shifts in the center of gravity with varying load conditions.
申请公布号 US4986493(A) 申请公布日期 1991.01.22
申请号 US19880279778 申请日期 1988.12.05
申请人 SARH, BRANKO 发明人 SARH, BRANKO
分类号 B60F5/02;B64C37/00 主分类号 B60F5/02
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