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특허 상세정보

Aerodynamic control surface system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/215; 244/213; 244/217; 244/0900R
출원번호 US-0996182 (2001-11-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perman & Green, LLP
인용정보 피인용 횟수 : 14  인용 특허 : 8
초록

A flight control system provides a maximized mechanical advantage when the load of the airstream on the airfoil is also at a maximum. A control surface is pivotally mounted for movement through a range of positions between a neutral position at which airstream load thereon is a minimum and upwardly and downwardly deflected positions, the airstream load being a maximum in either of the deflected positions. An operator mechanism for moving the control surface between the upwardly and downwardly deflected positions includes a rotor mounted on the airfoil fo...

대표
청구항

1. A flight control system for a generally planar airfoil subjected to an advancing airstream and extending in spanwise and chordwise directions comprising:a control surface mounted on the airfoil for pivotal movement about a spanwise extending axis through a range of positions between a neutral position at which airstream load thereon is a minimum and a upwardly deflected position, in one instance, and a downwardly deflected position in another instance, the airstream load on the control surface being a maximum in either the upwardly deflected position ...

이 특허를 인용한 특허 피인용횟수: 14

  1. Gomolko, Oleg; Merlet, Etienne. Actuator for flight control surface. USP20180610005543.
  2. Moser, Matthew A.; Finn, Michael R.. Adaptive trailing edge actuator system and method. USP20180710017243.
  3. Nelson, Paul E.. Aircraft control surface actuation system with helical actuation path. USP2013118590834.
  4. Clark, John McMurray. Compound motion structure. USP2015129205912.
  5. Geders, Paul F.. Continuous moldline technology (CMT) elastomeric control surface. USP2014088814100.
  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. Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A.. Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction. USP2014048695925.
  8. Arata, Allen A.. Elastomeric transition. USP2018059975623.
  9. Tao, Tony Shuo; Olson, Nathan; Miralles, Carlos Thomas; Plumb, Robert Nickerson. Elevon control system. USP2015089108713.
  10. Tao, Tony Shuo; Olson, Nathan; Miralles, Carlos Thomas; Plumb, Robert Nickerson. Elevon control system. USP2015038985504.
  11. Goettinger, Marco; Havar, Tamas; Hue, Xavier; Stadler, Franz. Method for producing a load introducing element. USP20180810046526.
  12. Morris, Ralph F.. Safety aileron system. USP2015059038943.
  13. Nagel, Alexander; Bauminger, Shlomo. Wing and devices therefor. USP2015069061752.
  14. Hue, Xavier; Schlipf, Bernhard. Wing of an aircraft. USP2015018925871.