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특허 상세정보

Active flexible wing aircraft control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44    B64C-013/16   
미국특허분류(USC) 244/76R ; 244/203 ; 244/219 ; 244/195
출원번호 US-0554094 (1990-07-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 66  인용 특허 : 0
초록

A system for controlling an aircraft by aeroelastic deflections of the wings which is effective beyond control surface reversal is disclosed. The system includes flexible wings, leading and trailing edge control surfaces attached to the wings, sensors to measure selected aircraft flight parameters, an information processing system to receive and process pilot command signals and signals from the sensors, and control mechanisms in the wing that respond to processed signals from the information processing system. The control mechanisms selectively position...

대표
청구항

A system for control of an aircraft in one or more of its axes comprising: flexible wings; flight control surfaces mounted on said flexible wings; aircraft sensors for providing signals indicative of the overall motion of the aircraft; processing means responsive to said signals from said aircraft sensors for determining control surface movements which will aeroelastically induce desired deflections in said wings to effect the desired control of the aircraft and selectively generating control signals to bring about said control surface movements; and con...

이 특허를 인용한 특허 피인용횟수: 66

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