$\require{mediawiki-texvc}$
  • 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"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Aileron for fixed wing aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/00   
미국특허분류(USC) 24/4217 ; 24/409.0R
출원번호 US-0993241 (1997-12-18)
발명자 / 주소
대리인 / 주소
    Burns, Doane, Swecker & Mathis, LLP
인용정보 피인용 횟수 : 44  인용 특허 : 6
초록
▼

An aircraft aileron system unique in its construction, method of deployment and the functional results obtained, is comprised of two panels located at the rear portion of the wing, in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel is capa...

대표
청구항
▼

[ What is claimed is:] [1.] An aerodynamic control system for control of an aircraft around a longitudinal axis of the aircraft, comprising an aileron assembly disposed on each wing of the aircraft, each aileron assembly having an upper panel and a lower panel each pivotally attached adjacent to the trailing edge of the wing, with the upper surface of the upper panel forming a continuation of the wing's upper surface when the upper panel is in a neutral position and the lower surface of the lower panel forming a continuation of the wing's lower surface w...

이 특허에 인용된 특허 (6)

  1. Warrink Berned J. J. (Rijsenhout NLX) Obert Ed (Nieuw-Vennep NLX). Aileron for an airplane wing. USP1988014720062.
  2. Thornburg Francis L. (Canoga Park CA). Aileron segment control for a flaperon system. USP1979124180222.
  3. Sepstrup James L. (King County WA). Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps. USP1988014717097.
  4. Carter Glenn T. (Fort Worth TX) Paniszczyn Thomas F. (Fort Worth TX). Combination airbrake and pitch control device. USP1977014003533.
  5. Williams Edgar P. (Huntington Beach CA) Wasson Norman F. (Hacienda Heights CA) Sears William B. (Grand Prairie TX). Split rudder control system aerodynamically configured to facilitate closure. USP1997085655737.
  6. Dean Roy Delmar (BOTH OFSeattle WA) Weiland Richard Herschel (BOTH OFSeattle WA). Variable pivot trailing edge flap. USP1977094049219.

이 특허를 인용한 특허 피인용횟수: 44

  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. Gruenewald Michael,DEX ; Moeser Clemens,DEX ; Steigenberger Josef,DEX ; Mueller Guenther,DEX. Adaptive flow body. USP2001086276641.
  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. Lam, Lawrence Y.; Lam, Michael. Aileron for fixed wing aircraft. USP2003046554229.
  8. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  9. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  10. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  11. 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.
  12. 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.
  13. 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.
  14. 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.
  15. Lam, Michael; Cole, Greg. Aircraft wing structure and control system. USP2017129846432.
  16. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  17. Cazals, Olivier; Druot, Thierry. Aircraft with yaw control by differential drag. USP2014118876044.
  18. Sonneborn, Walter Gerd Oskar. Anemometer drive apparatus and method. USP2015018939394.
  19. Phillips, Warren F.. Apparatus and method for reducing induced drag on aircraft and other vehicles. USP2005116970773.
  20. Phillips, Warren F.. Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles. USP2011027883060.
  21. Wildman, Eric. Control surface assembly. USP2015059038964.
  22. Volk, John A.. Control system for alleviating a gust load on an aircraft wing. USP2004076766981.
  23. Bushnell, Glenn S.. Deployable aerodynamic devices with reduced actuator loads. USP2014028646729.
  24. Lam, Lawrence. Flap panel shuttle system and method therefor. USP2015089108723.
  25. Saliveros, Efstratios; Friedel, Hendrik. Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system. USP2017119815547.
  26. Bauer Karl,DEX. Helicopter rotor blade with a movable flap. USP2001016168379.
  27. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  28. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  29. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  30. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  31. Lam, Lawrence. Mechanical control mixer and method therefor. USP2015049004411.
  32. Beyer,Kevin W.; Fox,Stephen J.; Lacy,Douglas S.; Meredith,Paul T.; Prow,Clayton A.; Sakurai,Seiya; Wells,Stephen L.. Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. USP2007087258308.
  33. 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.
  34. Bonnaud, Cyril; Laporte, Florent; Bedoin, Stéve. Pylon for suspending a turboengine. USP2012048146868.
  35. Easter, William Craig. Rapidly convertible hybrid aircraft and manufacturing method. USP2013028371520.
  36. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  37. Clark, Walter D.. System and method for controlling an aircraft. USP2003116641086.
  38. 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.
  39. 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.
  40. 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.
  41. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  42. Morris, Stuart. Trailing edge flap. USP2014058714493.
  43. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  44. Kimura, Yukihide; Morimoto, Tomoaki. Wing structure and fairing device. USP2015079090346.

IPC 상위 출원인