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) | B64C-013/16 |
미국특허분류(USC) | 244/203 ; 244/91 ; 244/76R ; 244/78 |
출원번호 | US-0380473 (1982-05-20) |
우선권정보 | FR-0002548 (1982-02-15) |
발명자 / 주소 | |
인용정보 | 피인용 횟수 : 52 인용 특허 : 3 |
A wing assembly in an aircraft includes a pair of wings and a winglet situated at each of the wing tips, the winglets or portions thereof being movably mounted. In order to avoid the need for providing structural reinforcement for the wings to accommodate the additional bending moments acting on the wings due to the presence of the winglets, a system is provided for automatically moving the winglets between a first position wherein each winglet has a first aerodynamically optimal angle of attack and a second position wherein each winglet has a second min...
In an aircraft including a pair of structurally conventional elongate wings, each having a leading edge, a trailing edge and a wing tip, the improvement comprising a retrofit assembly for said structurally conventional wings, said retrofit assembly including a winglet situated at each of said wing tips so as to extend substantially upwardly therefrom, at least a portion of the winglets being movably mounted; and means for automatically moving said winglets or said portions thereof symmetrically with respect to the aircraft plane of symmetry between a fir...