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특허 상세정보

Torsional twist airfoil control means

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44    B64C-003/52    B64D-015/10   
미국특허분류(USC) 244/219 ; 244/48 ; 244/134 ; A ; 244/206
출원번호 US-0323779 (1994-10-17)
발명자 / 주소
인용정보 피인용 횟수 : 48  인용 특허 : 0
초록

A control system for aircraft airfoils, which is an improvement over existing aileron, flap, spoiler and deicing technologies, in providing increased roll control and aerodynamic lifting and braking functions; with greatly reduced drag increased airspeed and precise control performance at all airspeeds, due to clean uninterrupted airfoil surfaces and directional conformance of wing to the intended flight path. This is accomplished by use of a torque tube mounted internally in the aeroelastic airfoil structure, and firmly attached to the airfoil tip struc...

대표
청구항

An aeroelastic airfoil control means, said aeroelastic airfoil control means providing for aircraft maneuverability control and/or automatic deicing means for a wing of an airplane, said airfoil control means including roll control means; wherein said wing provides for slow flight, high lift and maneuverability functions at both low and high airspeeds, said wing means comprising: an aircraft aeroelastic wing structure, wherein said aeroelastic wing structure extends outwardly from a fuselage of said airplane, to a wing tip structure of said airplane, sai...

이 특허를 인용한 특허 피인용횟수: 48

  1. Thomas, James P.; O'Brien, Michael J.; Pogue, III, William R.. Active twist hollow beam system. USP2014058721282.
  2. Thomas, James P; O'Brien, Michael J; Pogue, III, William R. Active twist hollow beam system. USP2012088246303.
  3. Pitt, Dale M.; Eckstein, Nicholas Stephen. Active twisting of an aircraft lifting surface via modulated clamping of substructure. USP2012038128020.
  4. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya. Actuation device positioning systems and associated methods, including aircraft spoiler droop systems. USP2007127309043.
  5. Kota,Sridhar; Hetrick,Joel A.. Adaptive compliant wing and rotor system. USP2008067384016.
  6. Zamponi, Laurent; Fontaine, Nicolas; Durand, Valerian; Hirsch, Jean-Francois; Grohmann, Boris. Adaptively-twistable blade, and an aircraft including such a blade. USP2017109802699.
  7. Weaver, Thomas L.; Sheahan, Jr., James J.. Aerodynamically-assisted landing gear. USP2012048162255.
  8. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  9. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  10. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  11. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  12. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  13. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  14. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  15. 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. USP2013108567726.
  16. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
  17. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2009017475854.
  18. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  19. Pitt, Dale M. Apparatus and method for controlling twist of a wing of an airborne mobile platform. USP2009127637454.
  20. Phillips, Warren F.. Apparatus and method for reducing induced drag on aircraft and other vehicles. USP2005116970773.
  21. Phillips, Warren F.. Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles. USP2011027883060.
  22. Ferman,Marty Allen. Device and method of control of fixed and variable geometry rhomboid wings. USP2006117131611.
  23. Schweiger, Johannes. Fluid dynamically effective surface for minimizing induced resistance. USP2009107597285.
  24. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2013018342445.
  25. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2014068752789.
  26. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  27. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  28. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  29. Kelm Roland,DEX ; Grabietz Michael,DEX. Method of reducing wind gust loads acting on an aircraft. USP2000126161801.
  30. Costantino, Stephan; Roellinger, Marcel. Method to produce a composite material. USP2015059034776.
  31. Hinnant, Harris O.; Black, David J.; Brekke, Darin W.; Castelluccio, Mark A.; Dickerson, Matt R.. Methods and systems for active wing and lift surface control using integrated aeroelasticity measurements. USP2014098838298.
  32. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick. Multi-function trailing edge devices and associated methods. USP2007077243881.
  33. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael. Passive adaptive structures. USP2015059033283.
  34. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael. Passive adaptive structures. USP2013048418967.
  35. Hemmelgarn, Christopher Douglas; Pelley, Bryan Michael; Cable, Kristin Marie; Kirby, Brandon Charles. Passive adaptive structures. USP2014038678324.
  36. Volk John Alan. Selectively rotatable and torsionally flexible aerodynamic control apparatus. USP2000076089503.
  37. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  38. Mueller Dietmar,DEX ; Schuermann Helmut,DEX. Skin-rib structure. USP2001016173925.
  39. Clark, Walter D.. System and method for controlling an aircraft. USP2003116641086.
  40. From, Dave. System, apparatus and method to improve the aerodynamics of a floatplane. USP2009067552895.
  41. 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.
  42. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2008037338018.
  43. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
  44. Rinn Aaron ; Khamly Somphone ; Hornick David ; Obrigkeit Matthew ; Kota Sridhar. Variable camber airfoil. USP2000046045096.
  45. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  46. Canal Vila, Marc; Miguel Alfaro, Daniel. Wind turbine blade and methods of operating it. USP2017109790917.
  47. Matte, Francois. Wing flapping mechanism and method. USP2015129216823.
  48. Najmabadi, Kioumars; Shivitz, William F.; Coleman, Edward Ernest; Ho, John Koon-hung; Johnson, Richard D.; Carver, William F.; Grubb, David W.; McIntosh, Robert James. Wing-body load alleviation for aircraft. USP2011098024079.