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-072/68 |
미국특허분류(USC) | 60/039.091 ; 60/039.142 |
출원번호 | US-0771288 (1996-12-20) |
우선권정보 | FR-0015119 (1995-12-20) |
발명자 / 주소 | |
출원인 / 주소 | |
대리인 / 주소 |
|
인용정보 | 피인용 횟수 : 18 인용 특허 : 1 |
In an aircraft in which servocontrols are supplied with hydraulic fluid under pressure by a main pump driven by an engine of the aircraft and, in the event of loss of said engine power, by an emergency pump which is driven by a dynamic air pressure turbine deployed from the fuselage of the aircraft, a system is provided for assisting the restarting of said engine in the event of said aircraft suffering a total loss of engine power, wherein said main pump is of the reversible kind and means are provided for enabling surplus hydraulic power from the emerge...
[ I claim:] [1.] A system for assisting the restarting of at least one dead engine of an aircraft in flight using windmilling of said engine, especially in the event of said aircraft suffering a total loss of engine power, said aircraft including:servocontrols;a hydraulic circuit for supplying fluid under pressure to said servocontrols, said hydraulic circuit comprisinga main pump for pressurizing said fluid, said main pump being driven by said engine,an emergency pump for pressurizing said fluid in the event of loss of engine power,a fluid reservoir,fee...