$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색도움말
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"

통합검색

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

특허 상세정보

Folding truss mechanism for trailing edge flaps

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/16   
미국특허분류(USC) 244/216 ; 244/215
출원번호 US-0463455 (1982-09-29)
국제출원번호 PCT/US82/01356 (1982-09-29)
§371/§102 date 19820929 (19820929)
국제공개번호 WO-8401343 (1984-03-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 34  인용 특허 : 4
초록

A swinging drive link (10) is pivotally connected at its lower end (18) to a forward support (16) for a flap (20). The flap rear support is provided by a pivotal connection (24) between a rear support point and the lower end of a swing link (22). The upper end of the swing link (22) is pivotally connected (31) to the upper end of a support link (26) and the rear end of a slave link (30). The lower end of the support link (26) is attached (27) to a beam structure (28) projecting rearwardly from the main wing section (13, 29). The forward end of the slave ...

대표
청구항

A folding truss mechanism interconnected between a wing section, and a flap, for supporting and driving the flap from the wing section, comprising: an upper frame portion carried by said wing section; a lower frame portion carried by said wing section and positioned both below and aft of said upper frame portion; a drive link having an upper end and a lower end; first pivot means pivotally connecting the upper end of the drive link to the upper frame portion of said wing section for pivotal movement about a first pivot axis; a support link having an uppe...

이 특허를 인용한 특허 피인용횟수: 34

  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. Ferreira, Clóvis Augusto Eça; Da Silva, Israel. Aerodynamic surface drive mechanism. USP2017019540095.
  3. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  4. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  5. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  6. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  7. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  8. Peirce, Robert James. Aircraft slat assembly. USP2013078474762.
  9. 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.
  10. 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.
  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. USP2011108038103.
  12. 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.
  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. USP2009017475854.
  14. Osborn, Matthew James; Sakurai, Seiya; Clark, Benjamin A.; Penn, Steven C.. Aircraft wing fairing drive assembly, system, and method. USP2018019856014.
  15. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  16. Colaciti, Alysson Kennerly; Crenite Simões, Leandro Guilherme; Ferreira, Alexandre Viana; Valle do Carmo, Micael Gianini; Triches, Jr., Mário; Gouveia, Vinicius Losada. Airfoil flap assembly with split flap track fairing system. USP2017029567063.
  17. Pohl, Ulrich. Airfoil for an aircraft and aircraft. USP2012018104721.
  18. Holert, Ben. Drive and guide arrangement for a flap which is arranged on an aircraft mainplane. USP2011017861978.
  19. Soenarjo, Mochamad-Agoes. Flap support. USP2016019227722.
  20. Soenarjo, Mochamad-Agoes. Flap support. USP2018029889922.
  21. 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.
  22. Schroeder, Karsten; Friedel, Hendrik. Formvariable aerodynamic fairing body for a flap actuator mechanism of an aircraft. USP20180710035580.
  23. Voss, Timo; Loerke, Joachim. High lift system for an aircraft. USP2014098844878.
  24. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  25. Perez Sanchez,Juan; Bechheim,Claudia; Voglsinger,Martin. Lift-flap mechanism. USP2007117293744.
  26. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  27. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  28. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  29. Siers Geoffrey L.. Slotted cruise trailing edge flap. USP1998085788190.
  30. Tsai, Kevin R.. System and method for operating a droop panel using a pin joint linkage assembly. USP2018019878774.
  31. 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.
  32. 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.
  33. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  34. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.