$\require{mediawiki-texvc}$

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.

Aileron segment control for a flaperon system

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-009/06
  • B64C-009/12
출원번호 US-0754823 (1976-12-27)
발명자 / 주소
  • Thornburg Francis L. (Canoga Park CA)
출원인 / 주소
  • Lockheed Aircraft Corporation (Burbank CA 02)
인용정보 피인용 횟수 : 47  인용 특허 : 0

초록

An improved control system for the aileron segment of a combined flap and aileron (flaperon) wherein the flaperon, supported, extended and retracted by conventional means, is described. It consists of a splined shaft rotatably mounted on an aircraft wing, its longitudinal axis being substantially al

대표청구항

In an aircraft wing flaperon system comprising a flap, flap power means and means driven thereby to extend and retract the flap, flap guide means mounted in the wing to support and guide the flap, and an aileron segment contained within, defining a portion of and attached to the flap for rotation re

이 특허를 인용한 특허 (47)

  1. Ritter, Andreas; Mintgen, Rolf, Actuating system.
  2. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  3. Burandt Wesley A. (Rockford IL) Metcalf Jeffrey D. (Rockford IL) Wingate Duane (Rockford IL), Actuator system.
  4. Hauber, Bernhard; Kohloeffel, Christian, Aeronautical high-lift system with an overload safety device.
  5. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  6. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  7. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  8. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  9. Lam Lawrence Y. ; Lam Michael, Aileron for fixed wing aircraft.
  10. Lam, Lawrence Y.; Lam, Michael, Aileron for fixed wing aircraft.
  11. Rudolph Peter K. C. (Seattle WA), Aileron system for aircraft and method of operating the same.
  12. Nelson, Paul E., Aircraft control surface actuation system with helical actuation path.
  13. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  14. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  15. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  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.
  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.
  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.
  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.
  20. Mourani George D. (Huntington Beach CA), Aircraft wing section movement apparatus.
  21. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  22. Carl,Udo; V��tter,Axel, Apparatus for the adjustment of horizontal stabilizers for aircraft.
  23. Clark, John McMurray, Compound motion structure.
  24. Fairbairn Terence W. F. (Welwyn Garden City GB2) Capewell Terence J. (Stafford GB2), Device for limiting output force applied by a rotary transmission.
  25. Rudolph, Peter K. C., Flap assembly for aircraft wing.
  26. Lam, Lawrence, Flap panel shuttle system and method therefor.
  27. Grieco, James R.; Pakhlevanyan, Gary, Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting.
  28. 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.
  29. Heidlage, John K.; Hornbach, David W.; Hutchison, Stephen, Height adjustable bed framework with a lift chain and a planetary gear train.
  30. Aldrich Allyn M. (Rockford IL), Jam tolerant rotary actuation system.
  31. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  32. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  33. Arena Aldo (Smithtown NY), Linear flap drive system.
  34. 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.
  35. 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.
  36. Robinson Curtiss W. (Seattle WA) Raymond Eugene T. (Seattle WA), Rotary digital electrohydraulic actuator.
  37. Wataru Yada JP; Hiroshi Yamanouchi JP; Minoru Uchida JP; Katsutoshi Tada JP, Rotor blade operating device in airplane and flaperon operating device in airplane.
  38. Pohl Ulrich (Bremen DEX) Renken Juergen (Freyersen DEX), Segmentized flap system.
  39. DuRant,Cecil John, Servo mounting system for direct drive of an aircraft control surface.
  40. Oswald Peter (Bernhaupten DEX) Nagler Josef (Rothenbach DEX), Setting device for a control surface.
  41. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  42. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  43. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  44. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  45. Schwartz, Douglas John; Meyer, Mark Robert, Torque tube assemblies for use with aircraft high lift devices.
  46. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  47. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트