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검색연산자 기능 검색시 예
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공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
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| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
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! 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"

특허 상세정보

Systems and methods for controlling aircraft flaps and spoilers

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/215; 244/217; 244/213
출원번호 US-0966361 (2007-12-28)
등록번호 US7891611 (2011-02-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 15  인용 특허 : 237

Systems and methods for controlling aircraft flaps and spoilers are disclosed. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned at least partially aft of the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally c...


I/We claim: 1. A system for controlling an aircraft wing, comprising:a flapa flap actuator operatively coupled to the flap;a spoiler;a spoiler actuator operatively coupled to the spoiler;a controller operatively coupled to the flap actuator and the spoiler actuator, the controller being programmed with instructions to:place the wing in a high lift configuration during a first operation mode by directing the flap actuator to deflect the flap downwardly to form a gap with a trailing edge of the wing, and directing the spoiler actuator to deflect the spoile...

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