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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Aircraft engine mount

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00    F02C-007/20   
미국특허분류(USC) 244/54 ; 60/39031 ; 248/555 ; 248/554
출원번호 US-0821376 (1992-01-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 67  인용 특허 : 0
초록
▼

An aircraft engine mount includes a frame fixedly joined in a gas turbine engine and a platform fixedly joined to an aircraft wing or tail pylon. A first beam is pivotally joined to the frame and the platform at first and second joints, respectively. The first beam is additionally joined to the platform at a third joint which allows longitudinal movement between the first beam and the platform at the third joint while preventing rotation of the first beam. A second beam is spaced from the first beam and is pivotally joined to the frame and platform at fo...

대표
청구항
▼

A mount for supporting a gas turbine engine to an aircraft pylon comprising: a frame fixedly joined in said gas turbine engine; a platform fixedly joined to said pylon; a first beam pivotally joined to said frame at a first joint and pivotally joined to said platform at a second joint, and joined additionally to said platform at a third joint including a third-joint pin extending between said platform and said first beam and through a third-joint aperture in one of said first beam and said platform sized for allowing longitudinal displacement of said thi...

이 특허를 인용한 특허 피인용횟수: 67

  1. Butcher, Michael R.; Stanescu, Adrian. AFT engine mounting link rotational stop collar. USP20180710029801.
  2. Sandy, David F; Zheng, Zhijun. Adjustable engine mount. USP2015129217337.
  3. Dron, Sebastien. Aircraft engine mount. USP2009057527220.
  4. Mangeiga John A. ; Wilusz Christopher J. ; Dykhuizen Cornelius H.. Aircraft engine mount. USP2001126330995.
  5. Stretton, Richard Geoffrey; Udall, Kenneth Franklin. Aircraft engine mount. USP2017079701412.
  6. Dunstan Kent W.. Aircraft engine thrust mount. USP1999025873547.
  7. Hey Kenneth E.. Aircraft engine thrust mount. USP1998035725181.
  8. Gaillot, Mathieu; Bertucchi, Jean; Leyko, Matthieu. Assembly formed by a turbine engine and a system for attaching it to an aircraft structure. USP2016119488106.
  9. Foster, Lawrence D.. Catcher pin assembly. USP2014058714033.
  10. McCormick, Kelly Jon; Smallwood, Michel Shawn. Combustor liner support and seal assembly. USP2014068752395.
  11. Balk, Wouter. Connecting a propulsion system to a structural element of an aircraft. USP2014098827203.
  12. Schilling, Jan Christopher. Connector assembly for gas turbine engines. USP2003126669393.
  13. Mauran, Guy; Blades, Paul; Burness, Richard John Henry. Control surface failsafe drop link. USP2012058181908.
  14. Marche, Herve; Weyland, Gilles. Damage-tolerant attachment system for an aircraft engine. USP2012128328132.
  15. Pascal Jule FR; Stephane Levert FR. Device for aircraft thrust recovery capable of linking a turboshaft engine and an engine strut. USP2002126494403.
  16. Jule Pascal FR; Alain Porte FR; Stephane Levert FR. Device for attaching an aircraft engine. USP2002016341746.
  17. Pascal Jule FR; Alain Porte FR; Stephane Levert FR. Device for attaching an aircraft engine to a strut. USP2002026347765.
  18. Le Blaye Sebastien,FRX ; Canadas Marc,FRX. Device for attaching an engine to an aircraft. USP2000056059227.
  19. Roszak, Sebastien. Device for attachment of an engine onto an aircraft nacelle stub. USP2003086601796.
  20. Levert, Stephane; Roszak, Sebastien. Device for recovery of forces generated by an aircraft engine. USP2003116648271.
  21. Faure, Benjamin; Bertrand, Jérôme; Coraboeuf, Yohann; Chevrollier, Samuel; Abadie-La-Haille, Robert; Mezieres, Pascal; Santerre, Angélique. Device for retaining a tank in an aircraft. USP2018049938025.
  22. Levert, Stephane; Roszak, Sebastien. Device for the attachment of an engine to an aircraft. USP2004016682015.
  23. Ellis Joe E. ; Stuart Alan R.. Double failsafe engine mount. USP1999075927644.
  24. El Hamel,Karim; Newton,Arnold C. Engine arrangement. USP2006097107755.
  25. Diochon, Lionel; Petrissans, Isabelle; Seguin, Guillaume. Engine assembly for aircraft. USP2010087770840.
  26. Diochon, Lionel; El Hammami, Samir; Le Louvetel-Poilly, Julie; Dumas, Jean-Baptiste; Koenig, Nicolas. Engine assembly for aircraft comprising an engine and a mounting device for such an engine. USP2010037677493.
  27. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Engine mount system for a turbofan gas turbine engine. USP2012038128021.
  28. Zheng, Zhijun; Foster, Joseph P.; Dailey, Stephen P.; Sandy, David F.. Engine mount waiting fail safe lug joint with reduced dynamic amplification factor. USP20190310220950.
  29. Foster, Lawrence David. Engine mounting apparatus. USP2011128074923.
  30. Foster, Lawrence David. Engine mounting apparatus. USP2012048152094.
  31. Foster, Lawrence David. Engine mounting arrangement. USP2013058443612.
  32. 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.
  33. Machado,St��phane; Cassagne,J��r��me; Del Blanco,Anthony; Martin,Yvon; Chambreuil,Arnaud. Engine mounting structure under an aircraft wing. USP2008047350747.
  34. Proctor Robert ; Epstein Michael J. ; Fraser Gordon G. ; Farley Scott E. ; Koch Richard F. ; Siebert Robert W.. External cooling system for turbine frame. USP2001026185925.
  35. Hartshorn, Scott; Parham, Dean Leon; Powell, Donald T.. Fail safe extended torque box strut-to-wing mount. USP2013018342444.
  36. Hey Kenneth E. (Seattle WA). Fail-safe engine mount system. USP1997075649417.
  37. Pasquer,Felix; Loewenstein,Philippe; Tesniere,Marc. Front fastening device for aircraft engine. USP2007017165743.
  38. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2014088807477.
  39. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2013058448895.
  40. Zheng, Zhijun; Sandy, David F.. Gas turbine engine mounting structure with secondary load paths. USP2013108561942.
  41. 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.
  42. 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.
  43. 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.
  44. 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.
  45. Scarr, Antony Brett; Weir, Thomas Joseph; Woolley, Allen Madsen; Janzon, Carol Marie. Inner cowl structure for aircraft turbine engine. USP2016089404507.
  46. Ellis Joe E. ; Stuart Alan R.. Integrated failsafe engine mount. USP1999075921500.
  47. Schilling,Jan Christopher; Mollmann,Daniel Edward; Allmon,Barry Lynn; Durchholz,Anthony. Methods for optimizing turbine engine shell radial clearances. USP2007087260892.
  48. Piezunka, Volker. Mounting device for mounting an energy supply device on a structural component of an aircraft and aircraft with a mounting device. USP2016039290275.
  49. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012058167237.
  50. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012128328133.
  51. Suciu, Gabriel L.; Merry, Brian D.; Marx, Jon A.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012028118251.
  52. Leonard, Nicholas; Ahmed, Sohail; Waitkus, Christopher. Oil tank mount with stiffeners. USP2018019863324.
  53. Pasquer,F챕lix; Loewenstein,Philippe; Tesniere,Marc. Rear fastening device for aircraft engine. USP2006016988692.
  54. Zheng, Zhijun; Sandy, David F.. Secondary load path for gas turbine engine. USP2016019227734.
  55. Ersoy Metin,DEX ; Siemer Hubert,DEX. Springrate controlled motor bearing. USP2001106299149.
  56. Bonnet, Mathieu; Journade, Frederic; Lafont, Laurent; Valery, Benoit. Structural rod incorporating a vibration filtration mode. USP2015038973885.
  57. Antoine Emmanuel Cousin FR; Georges Mazeaud FR; Jean-Louis Picard FR. Suspension system with intrinsic safety features for aircraft powerplants. USP2002116474596.
  58. Dunstan Kent W. ; Hey Kenneth E.. Three link failsafe engine mount. USP1999015860623.
  59. Hey Kenneth E. (Seattle WA). Three link failsafe engine mount. USP1997045620154.
  60. Somanath, Nagendra; Dye, Christopher M.; Kumar, Keshava B.. Turbine engine frame having an actuated equilibrating case. USP2011088001791.
  61. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.. Turbine section of high bypass turbofan. USP2014108850793.
  62. 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.
  63. 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.
  64. 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.
  65. Beutin,Bruno; Dos Santos,Nelson; Fert,Jeremy; Lacorre,Fabienne; Picard,Jean Louis. Turbojet having a large bypass ratio. USP2008107430852.
  66. Van Duyn Keven G.. Variable stiffness positioning link for a gearbox. USP2001046212974.
  67. Bachmeyer, Paul J.; Blewett, Michael R.; Ohme, Marvin D.. Vibration isolation device with load dependent stiffness. USP2004046715746.

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