$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Hinge fairings for control surfaces

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/215 ; 244/213 ; 244/212 ; 244/87
출원번호 US-0168456 (1993-12-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 45  인용 특허 : 0
초록

A new hinge fairing design for control surfaces such as ailerons, elevators, and rudders. By staggering the two curved hinge fairings, one mounted to the fixed airfoil and the other to the leading edge of the control surface, a curving load path is opened up that allows installation of hinge fittings and actuators without having to make cut-outs in the curved fairings. This principle makes it possible to keep the control surface faired and sealed over its entire span and during its entire motion range. This improves the effectiveness of the control surfa...

대표
청구항

A system for providing a smooth transition between a fixed airfoil of an aircraft and a movable control surface mounted on the fixed airfoil, said control surface having a neutral position and being movable in a first direction to a first deployed position and in a second opposite direction to a second deployed position, said system comprising: first and second fairings carried by the airfoil and the control surface, respectively; and first and second edge portions carried by, and fixed in position relative to, the airfoil and the control surface, respec...

이 특허를 인용한 특허 피인용횟수: 45

  1. Brewer, Paul R.; Shorcoll, Steven; Raval, Reg R.. Active gurney flap. USP2013128616504.
  2. Brewer, Paul R.; Shorcott, Steven; Raval, Reg R.. Active gurney flap. USP2014068757557.
  3. Brewer, Paul R.; Shorcott, Steven; Raval, Reg R.. Active gurney flap. USP2014048695926.
  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. Ogawa, Toshiaki; Itoh, Koji; Nagashima, Makoto. Actuator-link assembly for aircraft control surface. USP2015089097327.
  6. Wainfan Barnaby S. ; Mrdeza Matthew N.. Aerodynamic control effector. USP1999105961068.
  7. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  8. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  9. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  10. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  11. McDonald, Lynn. Aileron actuator bracket. USP2012128328142.
  12. Ito, Koji. Aircraft control surface drive mechanism. USP2014068757544.
  13. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  14. Casse, Christophe. Aircraft hinge arranged between a movable panel and a load-bearing structure. USP2017039604716.
  15. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  16. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  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. USP2013108567726.
  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. USP2011108038103.
  19. 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.
  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. USP2009017475854.
  21. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  22. Huynh,Neal V.. Control surface controller force measurement system. USP2006016981409.
  23. Huber Thomas,DEX. Conversion device for installation in an aircraft deck. USP1999075927650.
  24. Balayn Frederic,FRX ; Magre Eric,FRX. Convertible aircraft with tilting rotors. USP2001076260793.
  25. McAlinden, Jon; Wildman, Eric. Cross-bleed dam. USP2013108556214.
  26. McDermott, Brian K.; Greenwood, Kevin R.; Streeter, James D.. Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell. USP2012118312813.
  27. Milliere, Jérôme. Device for articulating a flap to an aircraft aerodynamic surface. USP2004056729583.
  28. Kim Sharp GB. Fairing arrangement for an aircraft. USP2002096450457.
  29. Johnson,Brian D. Fairing arrangements for aircraft. USP2006057051982.
  30. Zeon, Young L.; Achtner, Gerfried R.; Lee, Robert M.. Flight control surface seal. USP2016099452819.
  31. Parker, Simon John. Hinge sealing element and an assembly including said element. USP2014128919703.
  32. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  33. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  34. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  35. Mason, Garth L.; Taylor, Lane G.; Cooney, Daniel E.. Live trim tabs. USP2012098256710.
  36. 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.
  37. 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.
  38. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  39. Koppelman H. John. Spherical mating fairings for hingeline applications. USP1999065915653.
  40. 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.
  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. USP2008037338018.
  42. 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.
  43. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  44. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  45. Dorsett, Kenneth M.. Vortex generation. USP2016119505485.