$\require{mediawiki-texvc}$
  • 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

High lift system control assembly

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/32    B64C-013/38   
미국특허분류(USC) 244/75R ; 244/213 ; 244/221 ; 244/233
출원번호 US-0454559 (1982-12-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 51  인용 특허 : 2
초록
▼

A control assembly (50) for deployment of aircraft wing flaps is comprised of an input cam mechanism (54), a feedback cam mechanism (56) and a summing lever member (58) operatively interconnecting the cam mechanisms for mechanically summing independent inputs therefrom to yield a mechanical output signal for actuating flap deployment drives, wherein the input cam mechanism is comprised of a cam (64) rotationally operable in response to a command input signal and a cam follower (68) in mating engagement therewith for cammed movement with rotation thereof ...

대표
청구항
▼

A control assembly for deployment of aircraft wing flaps, comprising an input cam mechanism, a feedback cam mechanism and a summing lever means operatively interconnecting said cam mechanisms for mechanically summing independent inputs therefrom to yield a mechanical output signal for actuating flap deployment means, wherein said input cam mechanism is comprised of a cam rotationally operable in response to a command input signal and a cam follower in mating engagement therewith for deflecting movement with rotation thereof to provide a first input signa...

이 특허에 인용된 특허 (2)

  1. Dorn Rupert I. (Seattle WA). Dual cam control mechanism for coordinated deployment and retraction of an air-craft\s leading and trailing edge wing fl. USP1981014244541.
  2. Baker ; Thomas M.. Mechanical mixer for controlling aircraft spoilers. USP1978014071208.

이 특허를 인용한 특허 피인용횟수: 51

  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. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  3. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  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. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  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. USP2010057708231.
  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. USP2013108567726.
  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. 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. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  17. Pohl,Ulrich; Thomas,Carsten; Lulla,Christian; Kloenne,Martin. Apparatus for driving and adjusting flaps hinged to an aircraft. USP2007067226020.
  18. Ergun, Mustafa A.; Fluhrer, Robert W.; Wong, Thiem; Asamarai, Saeb; Cain, John. Cam balance mechanism systems and methods. USP2015038967560.
  19. Ergun, Mustafa A.; Fluhrer, Robert W.; Wong, Thiem; Asamarai, Saeb; Cain, John. Cam balance mechanism systems and methods. USP2017029581285.
  20. Schievelbusch, Bernd. Device for monitoring the synchronism of flaps of an aircraft wing. USP2015028950705.
  21. Ergun, Mustafa A.; Cain, John; Segar, Peter; Lindblad, Shaun C.. Display and keyboard positioning apparatus, system, and method. USP20181010104957.
  22. Hazzard, Joel; Fluhrer, Robert W.; Segar, Peter; Theis, John W.; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2014098826831.
  23. Hazzard, Joel; Fluhrer, Robert W.; Segar, Peter; Theis, John W.; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2015079080721.
  24. Hazzard, Joel; Fluhrer, Robert W.; Segar, Peter; Theis, John W.; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP20190110172450.
  25. Hazzard, Joel; Fluhrer, Robert W.; Segar, Peter; Theis, John; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2014098839723.
  26. Hazzard, Joel; Fluhrer, Robert William; Segar, Peter; Theis, John William; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2017089717329.
  27. Hazzard, Joel; Fluhrer, Robert William; Segar, Peter; Theis, John William; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2017119820566.
  28. Hazzard, Joel; Fluhrer, Robert William; Segar, Peter; Theis, John William; Ergun, Mustafa A.; Trish, Scott. Display positioning apparatus and method. USP2016109470357.
  29. Ergun, Mustafa A.; Cain, John; Segar, Peter; Lindblad, Shaun C.. Edge mount positioning apparatus, system, and method. USP2015119188275.
  30. Ergun, Mustafa A.; Cain, John; Segar, Peter; Lindblad, Shaun C.. Edge mount positioning apparatus, system, and method. USP2017089743757.
  31. Davies, Jonathan Paul; Farley, Brian. Flight surface actuator. USP2004106802475.
  32. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  33. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  34. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  35. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  36. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  37. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  38. 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.
  39. Djuric, Mihailo P.. Non-jamming, fail safe flight control system with non-symmetric load alleviation capability. USP2005086929222.
  40. 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.
  41. Nieman, Ronald J.. Self-centering aircraft flap position command apparatus. USP2016059327826.
  42. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  43. McLean,James D.; Witkowski,David P.; Campbell,Richard L.. Slotted aircraft wing. USP2006057048235.
  44. Vassberg,John C.; Gea,Lie Mine; McLean,James D.; Witkowski,David P.; Krist,Steven E.; Campbell,Richard L.. Slotted aircraft wing. USP2006057048228.
  45. 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.
  46. 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.
  47. 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.
  48. Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
  49. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  50. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  51. Stache Ernst (Weyhe DEX). Wing flap operation. USP1989054834326.

IPC 상위 출원인