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Active flexible wing aircraft control system

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/44
  • B64C-013/16
출원번호 US-0554094 (1990-07-16)
발명자 / 주소
  • Tulinius Jan (Huntington Beach CA)
출원인 / 주소
  • Rockwell International Corporation (El Segundo CA 02)
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,

대표청구항

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 s

이 특허를 인용한 특허 (66)

  1. Wainfan Barnaby S. ; Mrdeza Matthew N., Aerodynamic control effector.
  2. Chankaya, Kurt M.; Maines, Brant H., Aerodynamic force sensing apparatus.
  3. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
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  6. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
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  58. Reckzeh, Daniel, System for setting the span load distribution of a wing.
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