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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Flap/slat actuation system for an aircraft

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/26   
미국특허분류(USC) 244/075R ; 244/213
출원번호 US-0602190 (1996-02-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Crowe
인용정보 피인용 횟수 : 73  인용 특허 : 10
초록
▼

The problem of providing a flight control panel actuation system, including asymmetry brakes, which will fit into aircraft wings having narrow supercritical air foil shapes, and yet provide a degree of safety with regard to preventing asymmetry which is as good or better than that provided by prior actuation systems is solved by an actuation system which positions an asymmetry brake inboard of an outermost flight control panel actuator within the aircraft wing. The asymmetry brake utilizes a jaw type clutch coupled to an electrical solenoid through a bal...

대표
청구항
▼

[ We claim:] [1.] In an aircraft having right and left wings extending in opposite directions from a centerline of said aircraft, each of said wings including a flight control panel thereof movable to its respective wing, an actuation system comprising:a) a right wing control panel actuator having a rotatable input for receiving a driving torque;said right control panel actuator being operably connected between said right wing and said flight control panel of said right wing for moving said right control panel relative to said right wing when said drivin...

이 특허에 인용된 특허 (10)

  1. Burandt Wesley A. (Rockford IL) Metcalf Jeffrey D. (Rockford IL) Wingate Duane (Rockford IL). Actuator system. USP1988104779822.
  2. Embree David G. (1916 Nebraska Rd. Rockford IL 61108). Actuator system for aircraft control surfaces. USP1981034256277.
  3. Hudson Philip (Wolverhampton GB2). Braking arrangement for a rotary drive system. USP1987014633984.
  4. Baston Trevor A. J. (Albrighton GB2) Wynne John R. (Finchfield GB2). Drive arrangement for lift control surfaces on all aircraft wings. USP1981044260121.
  5. Comollo Virgilio (Bellevue WA). Failure detector and indicator for aircraft flap actuation system. USP1976023935754.
  6. Boehringer Wilfred E. (Fullerton CA) Verhoeven Teunes (Long Beach CA). High lift surface actuation system. USP1984044441675.
  7. Caero Jose G. (Arlington VA). Jam resistant ball screw actuator. USP1992035092539.
  8. Jones Teddy L. (Rockford IL). Resettable force limiting device. USP1984074459867.
  9. Pohl Ulrich (Bremen DEX) Renken Juergen (Freyersen DEX). Segmentized flap system. USP1990014892274.
  10. Quick David C. (Rockford IL) Russ David E. (Rockford IL). Speed responsive brake device. USP1996015484043.

이 특허를 인용한 특허 피인용횟수: 73

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya. Actuation device positioning systems and associated methods, including aircraft spoiler droop systems. USP2007127309043.
  2. Recksiek,Martin; Rechter,Harald; Besing,Wolfgang. Adaptive flap and slat drive system for aircraft. USP2006057048234.
  3. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  4. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  5. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  6. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  8. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  9. Nelson, Paul E.. Aircraft control surface actuation system with helical actuation path. USP2013118590834.
  10. Jones, Kelly T.. Aircraft control surface drive system and associated methods. USP2004106799739.
  11. Pohl,Ulrich; Thomas,Carsten. Aircraft flap or slat drive system with redundant drives and shaft drive lines. USP2006057051975.
  12. McKay, Ted Alexander. Aircraft flight control actuation system with direct acting, force limiting, actuator. USP2012118312783.
  13. Benson, Dwayne M.. Aircraft flight control surface actuation system communication architecture. USP2010087770842.
  14. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  15. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  16. Mayer, Timothy Michael; Hastings, Paul F.; Massolle, Jr., Dale W.. Aircraft slat disconnect sensor. USP2013088516898.
  17. 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.
  18. 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.
  19. 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. USP2011108038103.
  20. 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.
  21. 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.
  22. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  23. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  24. Hirvonen, Jukka Matti. Apparatus and method for backup control in a distributed flight control system. USP2012088235328.
  25. Hirvonen, Jukka Matti. Apparatus and method for backup control in a distributed flight control system. USP2011077984878.
  26. Pohl,Ulrich; Thomas,Carsten; Lulla,Christian; Kloenne,Martin. Apparatus for driving and adjusting flaps hinged to an aircraft. USP2007067226020.
  27. Carl,Udo; V��tter,Axel. Apparatus for the adjustment of horizontal stabilizers for aircraft. USP2008127464896.
  28. Hill, David G.. Articulable rotational coupling for an aircraft. USP2014128910906.
  29. Jones, Kelly. Brake systems for aircraft wing flaps and other control surfaces. USP2004116824099.
  30. Rennhack, Joern. Device for determining the rotation angle of a shaft in an aircraft. USP2010017644634.
  31. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C.. Distributed flight control surface actuation system. USP2009077556224.
  32. Hauzenberger, Stefan; Hauber, Bernhard. Drive system and method for activating the same. USP2013028373376.
  33. Kracke, Jeremy Alan George. Dual actuator drive assembly with synchronization shaft. USP2012108276842.
  34. Hanlon, Casey; Wingett, Paul T.; Potter, Calvin C.. Electric flight control surface actuation system for aircraft flaps and slats. USP2009067549605.
  35. Maresko, William A.; Cavalier, Donald R.; Klap, Aaron M.. Enhanced lubrication skewed roller clutch assembly and actuator including same. USP2013038393568.
  36. Richter, Martin; Fleddermann, Andreas. Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system. USP2014088814085.
  37. Lang, David J.; Regan, James M.. Feedback torque limiter. USP2012038127912.
  38. Cavalier, Don R.; Klap, Aaron M.. Flap actuator. USP2010047690597.
  39. Cavalier, Don R.; Klap, Aaron M.. Flap actuator. USP2012028118254.
  40. Lang, David J.; Regan, James M.. High gain asymmetry brake. USP2013038393442.
  41. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  42. Winkelmann, Christoph. High-lift system for a wing of an aircraft. USP2016069376204.
  43. Santini, Gregory M.; Sakurai, Seiya. Horizontal folding wingtip. USP2018049950780.
  44. Finney, Adam M.. Integrated torque limiter/no-back device. USP2016029255632.
  45. Finney, Adam M.. Integrated torque limiter/no-back device. USP20190210215246.
  46. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  47. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  48. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  49. Huynh, Neal Van; Andersen, Peter James. Method and apparatus for optimizing a load in a flight control system while an aircraft is on the ground. USP2017079708054.
  50. Brueckner, Ina; Giebeler, Christoph; Heintjes, Mark; Recksiek, Martin; Rechter, Harald; Christmann, Markus. Method and device for fault detection in the load path of a spindle actuator. USP2012078224502.
  51. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  52. McGeer, Brian T.; von Flotow, Andreas H.; Roeseler, Cory. Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion. USP2010057712702.
  53. McGeer,Brian T.; von Flotow,Andreas H.; Roeseler,Cory. Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion. USP2008047360741.
  54. Jones, Tony; Bacon, Peter William. Monitoring component asymmetry. USP20180910081419.
  55. 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.
  56. Wallen, Gregory T.; Regan, James M.; Lang, David J.; Crandall-Seibert, Cory M.; Miller, Mark D.; Leden, William E.; Baines, Andrew N.; Jacobs, Jeffrey Paul. Resolver type skew sensor with gimbal attachment. USP2013058438743.
  57. Kordel, Jan A.; Sakurai, Seiya; Bowers, Bret A.; Glassmoyer, Christopher G.; Williams, Darren B.. Seal assemblies for use with drooped spoilers and other control surfaces on aircraft. USP2009117611099.
  58. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  59. Flatt, James E.; McKay, Ted Alexander. Shuttle stop force limiter. USP2013128616080.
  60. Geary, Robert; Stevenson, Jason Marc. System and method for aircraft cabin atmospheric composition control. USP2016019233756.
  61. Hirvonen, Jukka Matti; Palfreyman, Gary. System and method for an integrated backup control system. USP2012018104720.
  62. Hirvonen, Jukka Matti; Palfreyman, Gary. System and method for an integrated backup control system. USP2011027878461.
  63. 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.
  64. 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.
  65. 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.
  66. Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
  67. Christensen, Donald J.; Hanlon, Casey; Hopper, Douglas T.; Johnson, Andrew; Kortum, Robert D.. Thrust reverser system actuator having an integral torque limiter. USP2005126974107.
  68. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  69. Serven, Mark R.. Two-brake torque limiting device. USP2003126659398.
  70. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  71. Lassen, Matthew August; Good, Mark Steven. Wing fold controller. USP2016119499252.
  72. Fox, Stephen John; Sakurai, Seiya; Munsen, Victor A.; Noble, Jack S.; Skomorowski, John Tony. Wing fold system. USP2016089415857.
  73. Fox, Stephen John; Kordel, Jan A.; Townsend, Keith; Lassen, Matthew August; Gardner, Mark John; Good, Mark Steven. Wing fold system rotating latch. USP2016109469392.

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