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특허 상세정보

Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38   
미국특허분류(USC) 244/099.4; 244/220; 244/225; 244/087; 244/099.9; 244/211
출원번호 US-0991174 (2009-05-05)
등록번호 US-8814085 (2014-08-26)
우선권정보 DE-10 2008 022 092 (2008-05-05)
국제출원번호 PCT/EP2009/003219 (2009-05-05)
§371/§102 date 20101123 (20101123)
국제공개번호 WO2009/135653 (2009-11-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz P.C.
인용정보 피인용 횟수 : 6  인용 특허 : 33
초록

A fault-tolerant actuating system with at least one flap, adjustable on a respective wing of an aircraft, and with a control and monitoring device, includes: drive devices that are functionally connected to the control and monitoring device, with one of these drive devices in each case being associated with a flap, where each flap in each case is associated with a drive device, in each case including: two drive motors, two brake mechanisms, where each drive motor is associated with a brake mechanism for stopping rotation of the output of the respective d...

대표
청구항

1. A fault-tolerant actuating system, comprising: at least one flap, adjustable on a respective wing of an aircraft;a control and monitoring device;drive devices that are functionally connected to the control and monitoring device, each drive device being associated with a respective flap, each drive device comprising: (i) two drive motors, and two brake mechanisms, wherein each drive motor is associated with a respective brake mechanism for stopping rotation of an output of the respective drive motor, (ii) a differential that couples the outputs of the ...

이 특허에 인용된 특허 (33)

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