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특허 상세정보

Elastomeric transition for aircraft control surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/52   
미국특허분류(USC) 246/213 ; 244/215 ; 244/219 ; 244/130
출원번호 US-4879538 (1995-06-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 45  인용 특허 : 12
초록

Elastomeric transition sections (118, 124) are mounted between the upper and lower portions of a wing (100) and a control surface (102) hinged thereto. The elastomeric transition sections include elastomeric material (126) having a plurality of holes (128) formed therethrough. Flexible rods (134, 136) are secured to either the wing or the control surface and extend through the holes (128) in the elastomeric material (126). The elastomeric transition sections provide a smooth aerodynamic transition between the wing and the control surface while permitting...

대표
청구항

[ We claim:] [1.] An aircraft wing assembly, comprising:

이 특허를 인용한 특허 피인용횟수: 45

  1. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard. Active reinforced elastomer system. USP1999085931422.
  2. Kota,Sridhar; Hetrick,Joel A.. Adaptive compliant wing and rotor system. USP2008067384016.
  3. Frederick E. To CH; Res Kammer CH. Adaptive pneumatic wings for flying devices with fixed wings. USP2002026347769.
  4. Kendall G. Young ; Steven L. Pauletti. Aerodynamic control surface system. USP2002106467733.
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  8. Birkenstock, David. Apparatus, system and method for drag reduction. USP2017099764823.
  9. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry. Blade seal for an aircraft. USP1999065913494.
  10. Wille Robert Henry. Conformable weapons platform. USP1999115988567.
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  13. 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.
  14. Arata, Allen A.. Elastomeric transition. USP2018059975623.
  15. Gruensfelder Cynthia Ann ; Wille Robert Henry. Expandable aircraft bay and method. USP1999115975463.
  16. Munoz Saiz Manuel,ESXITX 28017. Flight controls with automatic balance. USP2000086109567.
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  21. Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
  22. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
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  24. Young Kendall Gardner ; Pauletti Steven Louis. Low density flexible edge transition. USP2001016173924.
  25. Luippold David Arthur ; Brown Mark David ; Tully John Wilbur. Method for reducing reflected radio frequency electromagnetic radiation. USP2001096284175.
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  29. Loyet, Jessica; Pitt, Dale M.. Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft. USP20180610000274.
  30. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  31. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael. Passive adaptive structures. USP2015059033283.
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  34. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul. Seal. USP2016069365283.
  35. Martin Hernandez, Agustin Mariano. Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabilizer. USP2010047699266.
  36. Jasklowski, Christopher T.. Shape memory alloy actuation system for variable area fan nozzle. USP2017029581145.
  37. Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
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  45. Canal Vila, Marc; Miguel Alfaro, Daniel. Wind turbine blade and methods of operating it. USP2017109790917.