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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0467534 (1990-01-19) |
발명자 / 주소 |
|
인용정보 | 피인용 횟수 : 12 인용 특허 : 0 |
An assembly for controlling the lateral stability of a swept-wing aircraft by varying the geometric dihedral of the wing as a function of the wing\s lift coefficient, such assembly including a mechanism for producing a signal or other type response representative of the lift coefficient of the wing
In a swept-wing aircraft having wing sections extending in opposite directions from a particular location on said aircraft, each of said wing sections having fist and second wing portions, each of said second wing portions being angularly movable relative to said first wing portions, actuating means
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