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) | F42B-010/14 F42B-010/50 F42B-015/01 B64G-001/62 |
미국특허분류(USC) | 244/160 ; 244/138A ; 244/139 ; 244/063 ; 244/032.8 ; 102/384 ; 102/388 |
출원번호 | US-0719457 (1996-09-25) |
발명자 / 주소 | |
출원인 / 주소 | |
대리인 / 주소 |
|
인용정보 | 피인용 횟수 : 18 인용 특허 : 6 |
A nose assembly and method for controlling the rotation and stabilizing the orientation of a vehicle during landing maneuvers. The vehicle includes a nose assembly that is coupled to an airframe thereof and that has a frame and flap assembly. The flap assembly includes an actuating means and a flap coupled to the frame such that the actuating means moves the flap from and between a fully retracted position and a fully extended position in response to a guidance signal received from a flight control computer. In a preferred embodiment of the present inven...
[ What is claimed is:] [1.] A vehicle adapted to be launched into orbit about the earth and to return to the earth without jettisoning any portions of the vehicle, said vehicle comprising:an airframe; anda nose assembly coupled to said airframe, said nose assembly including a frame and a flap assembly having a plurality of independent flaps coupled to said frame for independent movement from and between fully retracted positions and fully extended positions, said flap assembly further including an actuating assembly for moving said flaps from and between...