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특허 상세정보

Flight controls with automatic balance

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 24/4215
출원번호 US-0110744 (1998-07-02)
우선권정보 ES-0000050 (1998-01-14)
발명자 / 주소
대리인 / 주소
    Schwartz
인용정보 피인용 횟수 : 37  인용 특허 : 5
초록

Flight controls with automatic balance for use in control of the movement of an aircraft through a fluid system, the control system consists of ailerons divided into two parts, which at low speed adopt the shape of a conventional aileron and rotate in their entirety with the same degree and at high speeds, a part of it rotates or extends to a determinated angle by means of the actuator and the other part of the aileron, that is hinged or articulated to the main part of the aileron, rotates with reference to the main part as a function of the air speed pr...

대표
청구항

[ I claim:] [1.] Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and at high speed flex backward comprising:a wing,an aileron comprising:a front part, wherein said front part is rigid,a rear part, wherein said rear part is flexible and is connected to said front part,a hinge that connects said wing to the front section of said aileron,an actuator that rotates said aileron on said hinge, and,springs that tend to keep said rear part in line with said front part.

이 특허를 인용한 특허 피인용횟수: 37

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  15. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
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