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특허 상세정보

Mechanical control mixer and method therefor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/04    B64C-013/30    B64C-013/28   
미국특허분류(USC) 244/221; 244/223; 244/234; 074/471R
출원번호 US-0885630 (2011-11-15)
등록번호 US-9004411 (2015-04-14)
국제출원번호 PCT/US2011/060825 (2011-11-15)
§371/§102 date 20130716 (20130716)
국제공개번호 WO2012/068136 (2012-05-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Quarles & Brady LLP
인용정보 피인용 횟수 : 0  인용 특허 : 15
초록

A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one co...

대표
청구항

1. An aircraft, comprising: a mechanical control mixer coupled to the aircraft, the mechanical control mixer including: an axle mounted to a frame of the mechanical control mixer,a barrel configured to rotate about the axle, anda central rod disposed within the barrel, the central rod being configured to rotate with respect to the barrel;a roll control input connected to the central rod, the roll control input being configured to cause the central rod to rotate within the barrel;output control rods connected to the central rod, the output control rods be...

이 특허에 인용된 특허 (15)

  1. Lam Lawrence Y. ; Lam Michael. Aileron for fixed wing aircraft. USP2000066079672.
  2. Lam, Lawrence Y.; Lam, Michael. Aileron for fixed wing aircraft. USP2003046554229.
  3. Thomas Dieter (Buchenstrasse 15a D-8080 Fuerstenfeldbruck DEX). Aircraft control system. USP1992035100081.
  4. Nelson,Bruce A.; Klausmeyer,Patrick J.. Aircraft roll disconnect mechanism. USP2007067229047.
  5. Cazals, Olivier; Druot, Thierry. Aircraft with yaw control by differential drag. USP2014118876044.
  6. Pohling John G.. Bobweight assembly for establishing a force feedback on a manually movable control element. USP1999065911390.
  7. Pohling John G.. Cable control system having stored energy fail-safe mechanism. USP1999075924331.
  8. Kopp, John D.. Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein. USP2011128074940.
  9. Dorn Rupert I. (Seattle WA). Dual cam control mechanism for coordinated deployment and retraction of an air-craft\s leading and trailing edge wing fl. USP1981014244541.
  10. Dewey Daniel L.. Flight console for radio controlled aircraft. USP1999035878981.
  11. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  12. Baker ; Thomas M.. Mechanical mixer for controlling aircraft spoilers. USP1978014071208.
  13. Djuric, Mihailo P.. Non-jamming, fail safe flight control system with non-symmetric load alleviation capability. USP2005086929222.
  14. Rabouyt Denis (90ter ; rue Pierre Brossolette 92140 Clamart FRX). Steering aid for rotor aircraft. USP1991105058825.
  15. Moody, Larry A.. System, autopilot supplement assembly and method for increasing autopilot control authority. USP2004016675076.