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특허 상세정보

Methods and apparatus for integrating rotary actuators in flight control systems

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/30    B64C-009/02    B64C-013/28    B64C-009/00   
출원번호 US-0529694 (2014-10-31)
등록번호 US-9950782 (2018-04-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ostrager Chong Flaherty & Broitman P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 18

Methods and apparatus for reacting rotary actuator and control surface loads into a wing structure using reaction links. The apparatus incorporates a structural interface feature that can facilitate a change of the component(s) in the load loop, such as the path connecting a control surface to a fixed aircraft structure via a rotary actuator. In particular, the structural interface between the rotary actuator and the rear spar of a wing can be tuned for stiffness to achieve an optimized load path that reacts actuator and control surface loads back into t...


1. An apparatus comprising: an aircraft structure;first and second hinges coupled to said aircraft structure;a control surface coupled to said first and second hinges;a rotary actuator comprising a housing and an output shaft rotatable relative to said housing, the output shaft being coupled to said control surface for causing pivoting of said control surface about a hinge line;a first reaction link having a first end rotatably coupled to said housing of said rotary actuator for transmitting reaction forces to said aircraft structure during pivoting of s...

이 특허에 인용된 특허 (18)

  1. Sakurai, Seiya; Wheaton, James M.; Fox, Stephen J.; Che, Sharon Xiangdong. Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions. USP2014048684316.
  2. Mabe, James H.; Calkins, Frederick T.; Bushnell, Glenn S.; Bieniawski, Stefan R.. Aircraft systems with shape memory alloy (SMA) actuators, and associated methods. USP2011027878459.
  3. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2010057708231.
  4. Cole James B. (Mercer Island WA). Airplane wing trailing-edge flap-mounting mechanism. USP1981024248395.
  5. Durand Yves,FRX. Conical rotary actuator and its application to the control of a rudder. USP1998035722616.
  6. Tieys, Pierre; Sagansan, Alain; Andrieu, Laurent. Device for mechanical connection of a control surface to a fixed structural element of an aircraft and aircraft wing element equipped with said device. USP2016069376203.
  7. Robinson, Curtiss W.. Drive mechanism for combined flap-aileron surface. USP1985104544118.
  8. Rudolph, Peter K. C.. Flap assembly for aircraft wing. USP1983044381093.
  9. Arena Aldo (Smithtown NY). Integrated power hinge actuator. USP1992035098043.
  10. Aldrich Allyn M. (Rockford IL). Jam tolerant rotary actuation system. USP1987084688744.
  11. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  12. Scobie William B. (Houston TX) Frenzel Robert A. (Waller TX). Rotary actuator. USP1991105054374.
  13. Kraft Kurt R.. Self centering hinge. USP1999025864922.
  14. Patzelt, Aicke; Reiprich, Michael; Stegmaier, Gunther; Wiglema, Wietse. Support structure for a retractable and extendable flap, and use of said structure. USP2010097798450.
  15. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  16. Schwartz, Douglas John; Meyer, Mark Robert. Torque tube assemblies for use with aircraft high lift devices. USP2017089739316.
  17. Ambrose,David R.. Unitized rotary actuator hinge fitting. USP2007067229049.
  18. Stephenson Martin F. (Issaquah WA). Wing flap mechanism. USP1986084605187.