发明名称 AIRCRAFT OF THE PARAWING TYPE
摘要 1. An engine of the type comprising in combination : a tubular frame (2) on wheels (14, 15, 16) ; a motor (6) equipped with a propeller (7) ; an aerofoil of the parawing type (1) provided in order to make the engine into a flying one, under the driving action of the motor (6) and the concomitant effect of the wind, this aerofoil (1) being fixed to the said frame (2) by left and right lifting suspending ropes (3a), and being stored in a pack (19), under no-use condition of the engine as a flying engine ; a pilot seat (8) mounted on the said frame (2) ; a rudder bar (4) for the steering control of the engine on the ground or in flight, actuated by the pilot's feet, which further actuates the right and left steering suspending ropes (3b), linked laterally to the parawing (1), the said propeller (7) and the said pilot seat (8), and thus the pilot, being protected by tubular ring bows (9a, 9b, 9c, 9d) being integrated part of the said tubular frame (2), the said engine being characterized in that the pack (19) containing the parawing (1) is equipped with ejection means, of a well known type of the parawing enabling the automatic opening of this latter, under the driving action of the motor and the concomitant effect of the wind, to take place during the normal rolling on the ground, without having to shut down previously the motor (6), the said ejection means being either mechanical or pyrotechnical or of any other known type.
申请公布号 DE3660954(D1) 申请公布日期 1988.11.24
申请号 DE19863660954 申请日期 1986.07.29
申请人 AERONAUTIQUE SERVICE 发明人 RANJON, MARC
分类号 B64C31/024;B64C31/036;(IPC1-7):B64C31/02;B64D17/72 主分类号 B64C31/024
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