검색연산자 | 기능 | 검색시 예 |
---|---|---|
() | 우선순위가 가장 높은 연산자 | 예1) (나노 (기계 | machine)) |
공백 | 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 | 예1) (나노 기계) 예2) 나노 장영실 |
| | 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 | 예1) (줄기세포 | 면역) 예2) 줄기세포 | 장영실 |
! | NOT 이후에 있는 검색어가 포함된 문서는 제외 | 예1) (황금 !백금) 예2) !image |
* | 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 | 예) semi* |
"" | 따옴표 내의 구문과 완전히 일치하는 문서만 검색 | 예) "Transform and Quantization" |
국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) | B64D-027/02 B64D-041/00 B64D-029/00 |
미국특허분류(USC) | 244/058; |
출원번호 | US-0393625 (2009-02-26) |
등록번호 | US-8220739 (2012-07-17) |
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...