$\require{mediawiki-texvc}$
  • 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

도움말도움말
상세검색 다국어 입력

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

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Mechanism for supporting and extending a high lift device for aircraft wings

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214 ; 244/213
출원번호 US-0193786 (1988-05-13)
우선권정보 GB-0011252 (1987-05-13)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 46  인용 특허 : 1
초록
▼

A mechanism for supporting and extending a high lift device relative to an aerofoil, comprises one or more support beams (10) connected to the aerofoil, a pair of spaced apart chordwise extending wing ribs (20) bounding the support beam, a set of cylindrical rollers (23) mounted between the wing ribs for supporting the support beam (10) with their rotational axes aligned transversely with respect to the support beam (10), the support beam (10) including a gear rack (12) with gear teeth facing downwardly and a pinion gear (13) lying in meshing engagement ...

대표
청구항
▼

A mechanism for supporting and extending a high lift device relative to an aerofoil, comprising one or more carrier beams adapted to be connected to said aerofoil, a pair of spaced apart chordwise extending wing ribs bounding said carrier beam(s), supporting means mounted between said wing ribs for supporting said carrier beam(s), said carrier beam(s) carrying a gear rack with gear teeth facing downwardly and a pinion gear in meshing engagement with said gear rack, and an actuator in driving engagement with said pinion gear to extend and retract the high...

이 특허에 인용된 특허 (1)

  1. Cole James B. (Mercer Island WA). Extendible airfoil track assembly. USP1984094471928.

이 특허를 인용한 특허 피인용횟수: 46

  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. Gyuricsko, Frederick S.; Phoenix, Jay; Fredericksen, Arnold E.; Cowles, Jr., John H.. Actuation system for a lift assisting device and lined track rollers used therein. USP20180710023302.
  3. Gyuricsko, Frederick S.; Phoenix, Jay; Gay, Arthur; Patel, Nirad; Fredericksen, Arnold. Actuation system for a lift assisting device and roller bearings used therein. USP2013038387924.
  4. Gyuricsko, Frederick S.; Phoenix, Jay; Gay, Arthur; Patel, Nirad; Fredericksen, Arnold E.. Actuation system for a lift assisting device and roller bearings used therein. USP2011098025257.
  5. Moser, Matthew A.; Finn, Michael R.. Adaptive trailing edge actuator system and method. USP20180710017243.
  6. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  7. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  8. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  9. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  10. Eden, James. Aircraft assembly and spar. USP2016029248903.
  11. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  12. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  13. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  14. Peirce, Robert James. Aircraft slat assembly. USP2013078474762.
  15. Mayer, Timothy Michael; Hastings, Paul F.; Massolle, Jr., Dale W.. Aircraft slat disconnect sensor. USP2013088516898.
  16. 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.
  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.; 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.
  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. USP2009017475854.
  20. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  21. Pachikara, Abraham J.; Moser, Matthew A.; Carpenter, Paul H.; Finn, Michael R.; Koch, Thomas S.; Bieniawski, Stefan R.; Whitehead, Brian T.. Closed loop control of aircraft control surfaces. USP2017119821903.
  22. Moser, Matthew A.; Finn, Michael R.; Thoreen, Adam. Control interface for leading and trailing edge devices. USP2017059656741.
  23. Grieco, James R.; Pakhlevanyan, Gary. Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting. USP2014118876065.
  24. Moser, Matthew A.; Liu, Benjamin M.; Finn, Michael R.. Leading and trailing edge device deflections during descent of an aircraft. USP2016059327827.
  25. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  26. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  27. Moser, Matthew A.; Finn, Michael R.; Park, Duk; Konings, Christopher A.. Leading edge system and method for approach noise reduction. USP2017099771141.
  28. Moser, Matthew A.; Gardner, Mark J.; Finn, Michael R.; Good, Mark S.; Malachowski, Adam P.; Thommen, Monica E.; Amorosi, Stephen R.; Onu, Dan. Leading edge variable camber system and method. USP2015119180962.
  29. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  30. McNeil, Scott. Low friction bearing assembly and link apparatus. USP2016029261132.
  31. 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.
  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. Moser, Matthew A.; Finn, Michael R.; Liu, Benjamin M.. Optimized flap positioning for go-around operations. USP2016029254909.
  34. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  35. Parker, Simon John. Slat monitoring system. USP2015038967551.
  36. Parker, Simon John. Slat support assembly. USP2016039296473.
  37. Jaggard, Philip R.; West, Robert H.. Slat support funk plate. USP2012058181913.
  38. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Murphy, Robert M.; Thoreen, Adam. System and method for optimizing performance of an aircraft. USP2016069359065.
  39. Moser, Matthew A.; Leopold, David D.; Finn, Michael R.. System and method for reducing the stopping distance of an aircraft. USP2016039296475.
  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. Brakes, David. Track container. USP20190110179641.
  44. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  45. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Good, Mark S.; Jones, Sarah A.. Variable camber flap system and method. USP2015119193440.
  46. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.

IPC 상위 출원인