|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-027/02 B64D-041/00 B64D-029/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 13 인용 특허 : 6|
A propulsive system for an aircraft including an auxiliary jet engine is integrated into a tail cone of a fuselage. A carrying structure of the jet engine is primarily formed with beams and frames or half-frames to which the auxiliary jet engine is fixed by lateral beams. The beams are interdependent of the frames and half-frames, and the beams are overhanging behind a frame behind which is fixed the engine. Each beam includes a lower half-beam and a higher half-beam, separated on at least a part of its length ahead from attachments of the jet engine to ...
1. An auxiliary propulsive system for an aircraft, integrated within a tail cone of a fuselage, said propulsive system comprising an auxiliary jet engine, having at least one operating mode in which said auxiliary jet engine is a propulsive engine, a carrying structure to which said engine is fixed, a device for supplying external air to said jet engine, wherein: the carrying structure comprises beams assembled to the aircraft, overhanging rearward of a rear load carrying frame of the fuselage in a substantially longitudinal direction of the fuselage and...