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-013/06 |
미국특허분류(USC) | 244/1185 ; 244/58 ; 60/3933 ; 62/134 |
출원번호 | US-0164491 (1993-12-09) |
발명자 / 주소 | |
출원인 / 주소 | |
인용정보 | 피인용 횟수 : 38 인용 특허 : 0 |
An aircraft subsystem provides the aircraft with all its electrical and conditioned air requirements without requiring the extraction of either shaft power and/or pressurized air from the aircraft\s main engines. At the core of this subsystem are two rotating assemblies journaled on non-oil lubricated bearings to a housing. One assembly includes a cooling turbine, a starter/generator, a core compressor, and a high pressure stage of a two stage axial turbine, all mounted on a single shaft. A combustor is disposed between the core compressor and the turbin...
An aircraft subsystem comprising: a first and second shaft journalled for rotation to a housing; a first compressor mounted to said first shaft; a first turbine mounted to said first shaft; a combustor disposed between said first compressor and said first turbine and in fluid communication therewith; a starter/generator mounted to said first shaft for providing electricity to said aircraft; a second compressor mounted to said second shaft and providing a flow of pressurized air; a second turbine mounted to said second shaft and in fluid communication wit...