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특허 상세정보

Systems and methods for alleviating aircraft loads with plasma actuators

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-017/00    B64C-021/00    B64C-023/00    H05H-001/24   
출원번호 US-0166199 (2008-07-01)
등록번호 US-9446840 (2016-09-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 1  인용 특허 : 46
초록

Systems and methods for alleviating aircraft loads with plasma actuators are disclosed. A method for operating an aircraft in accordance with a particular embodiment includes receiving an input corresponding to an aircraft component structural response to an aerodynamic load. The method can further include, based at least in part on the input corresponding to the aircraft component's structural response, reducing the structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or m...

대표
청구항

1. A method for establishing operational parameters for an aircraft, comprising: receiving a baseline structural response profile corresponding to expected total flight time of the aircraft as a function of flight condition, the profile including an expected structural response level at a first corresponding total flight time value;selecting activation parameters for one or more plasma actuators carried by the aircraft based on an effect of the parameters to shift the total flight time value at which the expected structural response level occurs from the...

이 특허에 인용된 특허 (46)

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