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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Method and apparatus for optimizing the aerodynamic effect of an airfoil

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/16   
미국특허분류(USC) 244/203 ; 244/209 ; 244/214 ; 244/215 ; 244/219
출원번호 US-0596653 (1996-02-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fasse
인용정보 피인용 횟수 : 41  인용 특허 : 0
초록

The optimum wing flow is thereby maintained more exactly. For transonic wings, the position and strength of compression shocks is also effectively controlled, which leads to a reduction of the direct shock induced separation.

대표
청구항

[ We claim:] [1.] In an aircraft having at least one airfoil including a leading edge flap arranged at a leading edge of said airfoil, a high lift flap arranged at a trailing edge of said airfoil, a spoiler, an aileron, and driveable actuators respectively connected to said leading edge flap and said high lift flap, an apparatus for automatically optimizing the aerodynamic effect of said airfoil comprising a process computer with at least one memory area for storing actual flight data and parametric wing data, a plurality of pressure sensors arranged dis...

이 특허를 인용한 특허 피인용횟수: 41

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