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-015/033 |
미국특허분류(USC) | 244/322 |
출원번호 | US-0796750 (1985-11-08) |
우선권정보 | DE-3442974 (1984-11-24) |
발명자 / 주소 | |
출원인 / 주소 | |
인용정보 | 피인용 횟수 : 3 인용 특허 : 2 |
The flight path of a flying body, such as an artillery shell, is stabilized against disturbing forces and against pendulum type motions by fluid steering jets ejected from said flying body for causing forces countering the disturbing forces. The steering jets pass through a fluid jet distributing member which has inlet openings communicating with fluid ducts leading to a fluid supply chamber. The distributing member is mounted in the flying body by a spring which permits a deflection or shifting of the distributing member in a direction across a central ...
An apparatus for stabilizing a flying body, especially a flying body travelling at supersonic speeds, said flying body having a longitudinal central axis and fluid flow passages including outlet ports leading from inside said flying body to the outside of said flying body for blowing stabilizing fluid jets into an air flow through which said flying body is passing, said fluid jets extending approximately radially relative to said longitudinal central axis, said apparatus further comprising an internal fluid jet distributing member having a rotational axi...