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특허 상세정보

Flexible/fixed support for engine cowl

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/14    B64C-001/16   
미국특허분류(USC) 244/129.4; 244/054; 244/127; 244/131
출원번호 US-0006588 (2001-12-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renault, Ogilvy
인용정보 피인용 횟수 : 30  인용 특허 : 17
초록

A support assembly is provided for selectively supporting an aircraft engine cowling on an aircraft, the latch assembly including a cowling support mounted to the cowling, an aircraft support mounted to the aircraft frame; and a latching member. The latching member is moveable between a first position, in which it substantially fixes the cowling support to the aircraft support, and a second position, in which it permits the cowling support to move relative to the aircraft support. The support assembly also variably mounts the engine cowling to the aircra...

대표
청구항

A support assembly is provided for selectively supporting an aircraft engine cowling on an aircraft, the latch assembly including a cowling support mounted to the cowling, an aircraft support mounted to the aircraft frame; and a latching member. The latching member is moveable between a first position, in which it substantially fixes the cowling support to the aircraft support, and a second position, in which it permits the cowling support to move relative to the aircraft support. The support assembly also variably mounts the engine cowling to the aircra...

이 특허에 인용된 특허 (17)

  1. Grognard, Leon L.. Apparatus for the suspension of an aircraft engine cowling. USP1985114555078.
  2. Arnold Michael J. (Bangor GB5) Johnson Kenneth H. (Belfast GB5) Hall Brian J. (Comber GB5). Closure default indicator. USP1996055518206.
  3. Glancy Jerry L. (Wichita KS). Cowl structure alignment and shear device. USP1982124365775.
  4. Shine Paul R. (Bellevue WA). Cowling interlock system. USP1991095046689.
  5. Porte Alain,FRX ; Lasserre Jean-Louis,FRX. Device for fixing an air intake to a jet engine and jet engine incorporating such a device. USP1998045737914.
  6. Hey Kenneth E. (Seattle WA). Fail-safe engine mount system. USP1997075649417.
  7. Vermilye Michael L. (Redmond WA). Hinge system for thrust reverser cowl. USP1987104697763.
  8. Smith Keith O. (Wichita KS) Glancy Jerry L. (Wichita KS). Latch signal and cowling structure. USP1986094613099.
  9. Carimali Felix,FRX ; Hogie Jean-Paul Rene Andre,FRX ; Lore Xavier Raymond Yves,FRX ; Rouyer Pascal Gerard,FRX. Linkage system for an aircraft turbojet engine. USP2000036032901.
  10. Bower Charles R. (Middletown CT) Fowler Frank L. (Guilford CT). Load sharing for engine nacelle. USP1987044658579.
  11. Legrand Paul J. (Vaux le Penil FRX) Naud Henry (Verrieres le Buisson FRX). Locking system for sliding cowlings of turbojet engine nacelles. USP1979114174609.
  12. Hersen, Rene M. J.; Soulter, Pascal-Marie P. M.. Movable aircraft engine cowling. USP1991075035379.
  13. Brodell Robert F. (Marlborough CT) Hovan Edward J. (Manchester CT) Selfors Steven T. (Somerville MA) Loffredo Constantino V. (Newington CT) Duesler Paul W. (Manchester CT). Nacelle and mounting arrangement for an aircraft engine. USP1996065524847.
  14. Bart Jacques R. (Evry FRX). Pod for a turbofan aero engine of the forward contrafan type having a very high bypass ratio. USP1992105157915.
  15. Naud Henry (Verrieres Le Buisson FRX). Structural cowlings of twin flow turbo jet engines. USP1987084683717.
  16. Dunstan Kent W. ; Hey Kenneth E.. Three link failsafe engine mount. USP1999015860623.
  17. Hey Kenneth E. (Seattle WA). Three link failsafe engine mount. USP1997045620154.

이 특허를 인용한 특허 피인용횟수: 30

  1. Cloft, Thomas G.; Gukeisen, Robert L.. Access door for gas turbine engine components. USP2015099126691.
  2. Thornock, Russel L.; Sangwin, Michael L.; Hsiao, Entsung. Aircraft systems including cascade thrust reversers. USP2010047690190.
  3. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Engine mount system for a turbofan gas turbine engine. USP2012038128021.
  4. Suciu, Gabriel L.; Marx, Jon A.; Merry, Brian D.; Nordeen, Craig A.; Dye, Christopher M.. Engine mounting configuration for a turbofan gas turbine engine. USP2012098256707.
  5. Stierle, Holger. Fastening system for hanging mountable overhead containers. USP2015109150309.
  6. Isebrand, Scott Darrell; Powell, James Russell. Force sensing clevis insert. USP2010027661321.
  7. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2014088807477.
  8. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2013058448895.
  9. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine with low stage count low pressure turbine. USP2014048695920.
  10. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine with low stage count low pressure turbine. USP2014088800914.
  11. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine with low stage count low pressure turbine. USP2013088511604.
  12. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine with low stage count low pressure turbine. USP2013088511605.
  13. Soulier, Pascal-Marie Paul Marcel; De Sorbay, Aurélie. Locking device designed to be arranged in a junction region of a nacelle. USP2013118573934.
  14. Burnett, John L.; Hackler, David W.; Wilson, Timothy C.; Welch, John M.; Popp, Thomas D.; Sawyer, Christopher S.; Hoadley, Leo B.; Fulbright, Leroy J.; Granger, Mitchel B.; Craig, Barry B.; Kenney, Phillip E.. Mandrel for fabrication of a monolithic composite nacelle panel. USP2009087571527.
  15. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012058167237.
  16. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012128328133.
  17. Suciu, Gabriel L.; Merry, Brian D.; Marx, Jon A.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012028118251.
  18. Badescu, Ovidiu; Pizzi, Antonio. Mounting system for mounting engine nacelle components and associated method. USP2015038979020.
  19. Penda, Allan R.; Merry, Brian D.; Suciu, Gabriel L.; Dye, Christopher M.. Single plane mount system for gas turbine engine. USP2014038672260.
  20. Suciu, Gabriel L.; Alvanos, Ioannis. TEC mount redundant fastening. USP2015079091210.
  21. Leedy, Glenn J. Three dimensional structure memory. USP2014128907499.
  22. Leedy, Glenn J.. Three dimensional structure memory. USP2014098824159.
  23. Strunk,John T.; Gabel,Bruce. Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers. USP2007107275362.
  24. Harrison, Geoffrey E.; Sternberger, Joe E.; Lallement, Michael K.; Strunk, John T.; Byrd, William S.; Jundt, Darrell C.. Thrust reversers including locking assemblies for inhibiting deflection. USP2009077559507.
  25. Sternberger, Joe E.. Thrust reversers including support members for inhibiting deflection. USP2009107600371.
  26. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.. Turbine section of high bypass turbofan. USP2014108850793.
  27. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L.. Turbine section of high bypass turbofan. USP2014098844265.
  28. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L.. Turbine section of high bypass turbofan. USP2015049010085.
  29. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph Brent; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L.. Turbine section of high bypass turbofan. USP20180810060357.
  30. Joret, Jean-Philippe; Segat, Peter; Vauchel, Guy Bernard; Bouret, Georges Alain. Turbojet engine nacelle including a device for absorbing circumferential stresses. USP2014108869506.