$\require{mediawiki-texvc}$

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.

Resilient pivot type aircraft mounting 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-027/00
출원번호 US-0770058 (1991-09-30)
발명자 / 주소
  • Schmidt Warren E. (Erie PA)
출원인 / 주소
  • Lord Corporation (Erie PA 02)
인용정보 피인용 횟수 : 41  인용 특허 : 0

초록

A pivot type aircraft mounting for resiliently connecting a structure to an aircraft engine which uses a pivoting and siding joint on a beam at the engine attachment point, a vertically stiff and laterally soft intermediate pivot joint on the beam, and a resilient compression section near the end of

대표청구항

A resilient engine mounting for flexibly attaching an aircraft engine to a structure, comprising: (a) a first pivot means slidably receiving a first portion of a beam for connecting said beam to said engine about said first portion of said beam and accommodating pivoting motion and sliding motion of

이 특허를 인용한 특허 (41)

  1. Jones Peter J. ; Ivers Douglas E. ; Cooney Kevin C. ; Whiteford Gerald P., Active fluid mounting.
  2. Cousin, Antoine; Cassagne, Jerome, Aircraft engine mounting device attachment arrangement.
  3. Whiteford, Gerald P.; Zameroski, Daniel, Aircraft engine mounting system and method of mounting aircraft engines.
  4. Gallant, Guillaume; Delahaye, Romain, Aircraft including floor support cross-members with bearings including a flexible material connecting the cross-member to the support.
  5. Cassagne, Jerome; Deforet, Thomas, Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system.
  6. Cassagne, Jerome; Deforet, Thomas, Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system.
  7. Binks, Alan J.; Penda, Allan R., Assembly for mounting a turbine engine to a pylon.
  8. Parrish, Russell P.; Barry, Thomas M., Blind retention mount.
  9. Kunz, Peter; Jackson, Clifford; Thomasian, Craig Aram, Capture devices for unmanned aerial vehicles, including track-borne capture lines, and associated systems and methods.
  10. George,William J., Cartridge heater with a release coating.
  11. Knapp, Jeffrey H.; Tasker, David; Viviani, Gary Lee, Controlled range and payload for unmanned vehicles, and associated systems and methods.
  12. Knapp, Jeffrey H.; Tasker, David; Viviani, Gary Lee, Controlled range and payload for unmanned vehicles, and associated systems and methods.
  13. Parks, Robert, Ducted spinner for engine cooling.
  14. McGuire Dennis P. ; Whiteford Gerald P. ; Herbst Paul T. ; Wu Henry T., Dynamically optimized engine suspension system.
  15. Dennis, Brian D., Frangible fasteners for aircraft components and associated systems and methods.
  16. Cottrell, Brian; Zalewski, George Jerzy; Kroeger, James, Gas turbine engine rotor tip clearance and shaft dynamics system and method.
  17. Terpay, Gregory Weston; Ernst, Ronald G., Hydraulic actuator.
  18. Thomas, Justin; Nussenblatt, Eric L.; Casey, Ryan T.; Parsons, Eric S.; Hunter, David H., In-wing device retention.
  19. Parks,Robert, Inbound transition control for a tail-sitting vertical take off and landing aircraft.
  20. Dickson, Matthew Robert; Thomasian, Craig Aram, Line capture devices for unmanned aircraft, and associated systems and methods.
  21. Dickson, Matthew Robert; Thomasian, Craig Aram, Line capture devices for unmanned aircraft, and associated systems and methods.
  22. Dickson, Matthew Robert; Thomasian, Craig Aram, Line capture devices for unmanned aircraft, and associated systems and methods.
  23. Badescu, Ovidiu; Pizzi, Antonio, Mounting system for mounting engine nacelle components and associated method.
  24. Whiteford Gerald P., Multi-directional tuned vibration absorber.
  25. Olsen Kirk W., Multi-linkage suspension system including outboard isolators.
  26. Pasquer,F챕lix; Loewenstein,Philippe; Tesniere,Marc, Rear fastening device for aircraft engine.
  27. Roberts, Ana-Maria; Friedrich, Andreas, Rear handle.
  28. Roberts, Ana-Maria; Friedrich, Andreas, Rear handle.
  29. Roberts, Ana-Maria; Friedrich, Andreas, Rear handle.
  30. Roberts, Ana-Maria; Friedrich, Andreas, Rear handle.
  31. Dron, Sebastien; Fontenoy, Gilles Lucien; Tesniere, Marc Patrick, Suspension for suspending a turbine engine from the structure of an aircraft.
  32. Parks,Robert, System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft.
  33. Parks,Robert; Led��,Jean Charles; Drela,Mark, System and method for controlling engine RPM of a ducted fan aircraft.
  34. Gilchrist, III, Robert; Stafford, John; Dennis, Brian D.; Smith, Allen; Mack, Jaime; Sliwa, Steven M.; Schrick, Bradley; Hughes, Robert, Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft.
  35. Watson, Bill Russell; Warden, Max, Turbomachine core coupling assembly.
  36. Van Duyn Keven G., Variable stiffness positioning link for a gearbox.
  37. Parks, Robert; Ledé, Jean-Charles, Vibration isolation engine mount system and method for ducted fans.
  38. Cottrell, Brian, Vibration isolation mounting assembly.
  39. Cottrell, Brian; Davis, Porter, Vibration isolation mounting assembly.
  40. Whiteford Gerald P. (Waterford PA) Herbst Paul T. (Erie PA), Vibration isolation system including a passive tuned vibration absorber.
  41. Dyckrup, Werner, Wing for an aircraft.
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

맨위로