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) | F02C-007/268 F02C-007/32 |
미국특허분류(USC) | 60/3907 ; 60/39142 |
출원번호 | US-0502902 (1983-06-10) |
발명자 / 주소 | |
출원인 / 주소 | |
인용정보 | 피인용 횟수 : 50 인용 특허 : 1 |
The invention is a multi role primary/auxiliary power system with engine start capability for aircraft that provides electric, mechanical and air conditioning power as well as engine starting functions. The compressor (20), turbine (26) and motor/generator (24) are coupled to a drive shaft (14) of the aircraft\s engine (12) with the motor/generator (24) mounted between the compressor (20) and turbine (26). A first clutch (28) is mounted on the drive shaft (14) between the motor/generator (24) and the turbine (26). Coupled to the outlet (29) of the compre...
A multi role primary/auxiliary power system for an aircraft having at least one engine, said engine having a drive shaft, said power system comprising: a turbine coupled to said drive shaft; a compressor coupled to said drive shaft; a motor/generator coupled to said drive shaft, said motor/generator mounted between said compressor and said turbine; first passage means coupling the outlet of said compressor to said inlet of said turbine; a combustor mounted in said first passage means; first clutch means mounted on said drive shaft adapted to disengage sa...