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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Aircraft gas turbine engine sideways mount

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00    F02C-007/20   
미국특허분류(USC) 244/54 ; 248/555 ; 60/3931
출원번호 US-0165627 (1993-12-13)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 66  인용 특허 : 0
초록
▼

An aircraft engine sideways mount assembly includes a thrust mount and an engine suspension for suspending the engine structure sideways from the aircraft such that the thrust mount is operable to react substantially all the thrust load forces from the engine to the aircraft. The thrust mount has a thrust bar extending between the engine structure and a structure fixed to the aircraft such that the thrust bar has a line of action which intersects the engine centerline in a support mount plane through which the engine suspension suspends the engine and wh...

대표
청구항
▼

A mount assembly for mounting an aircraft gas turbine engine sideways to an aircraft by the engine\s structure which rotatably supports the engine rotor assembly about an engine centerline, said mount assembly comprising; a pivotable engine suspension including a pivotable support mount for mounting the engine structure sideways from the aircraft and which is operably constructed to permit at least limited axial movement of the engine, a thrust mount having a thrust bar means for reacting out substantially all thrust load forces from the engine to the ai...

이 특허를 인용한 특허 피인용횟수: 66

  1. Udall, Kenneth F; Beardsley, Peter K. Aeroengine mounting. USP2013058444084.
  2. Mangeiga John A. ; Wilusz Christopher J. ; Dykhuizen Cornelius H.. Aircraft engine mount. USP2001126330995.
  3. Seda, Jorge F.. Aircraft engine with inter-turbine engine frame. USP2005046883303.
  4. Seda, Jorge F.. Aircraft engine with inter-turbine engine frame. USP2004036708482.
  5. Andre,Joan; Andrieu,Laurent. Aircraft provided with thrust reversers. USP2006097107757.
  6. Kismarton, Max U.. Aircraft window. USP201310D691548.
  7. Cazals, Olivier; Manneville, Alexis. Airplane with rear engines. USP2013118573531.
  8. Harrison, Kenneth M.; Powell, Donald T.; Schnelz, James R.; Whitmer, Brett D.. Apparatuses and methods for attaching engine nacelles to aircraft. USP2004076758439.
  9. Llamas Sandín, Raúl Carlos. Arrangement for mounting an engine on the airframe of an aircraft. USP2010067726602.
  10. Lisiewicz, Stephan; Todorovic, Predrag. Arrangement for the suspension of a jet engine to a supporting structure. USP2013108561940.
  11. Ewens, David; Blanc, Jonathan. Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon. USP2018029889943.
  12. Ewens, David; Blanc, Jonathan. Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section. USP2018019862497.
  13. Durocher, Eric; Sleiman, Mohamad; Tsifourdaris, Panagiota. Deflector for a gas turbine strut and vane assembly. USP2012058182204.
  14. Journade, Frédéric; Quiroz-Hernandez, Esteban; Saucray, Jean-Michel. Device for locking an engine on an aircraft pylon. USP2013088517304.
  15. Levert, Stephane; Roszak, Sebastien. Device for recovery of forces generated by an aircraft engine. USP2003116648271.
  16. Stretton, Richard Geoffrey. Engine installation. USP2016059346551.
  17. Stretton, Richard Geoffrey; Udall, Kenneth Franklin. Engine mount. USP2017119809317.
  18. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Engine mount system for a turbofan gas turbine engine. USP2012038128021.
  19. Udall, Kenneth F; Stretton, Richard G. Engine mounting assembly. USP2010107806363.
  20. 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.
  21. Eleftheriou, Andreas; Menheere, David; Liu, Quantai. Fabricated intermediate case with engine mounts. USP2014088801376.
  22. Guillemaut, Julien; Gallant, Guillaume. Fish joint device having an improved mechanical hold. USP2017089738373.
  23. Suciu, Gabriel L.; Chandler, Jesse M.. Gas generator with mount having air passages. USP2017109790811.
  24. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2014088807477.
  25. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M.. Gas turbine engine compressor arrangement. USP2013058448895.
  26. 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.
  27. 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.
  28. 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.
  29. 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.
  30. Glynn, Christopher Charles; Zatorski, Darek Tomasz; Yeager, Donald Scott; Dinsmore, Nicholas Rowe; Menard, Jeffrey Raymond; Miller, Brandon Wayne. Hydraulic system for fan pitch change actuation of counter-rotating propellers. USP2013028371105.
  31. Williams,Nicholas A.. Integrated mount duct for use with airborne auxiliary power units and other turbomachines. USP2008097419121.
  32. Thies, Robert. Intermediate casing for a gas-turbine engine. USP2014108857193.
  33. West, Randall Ray. Intermediate structure for independently de-mountable propulsion components. USP2016119481470.
  34. Brochard, Wolfgang; Terral, Romain. Lateral propulsion unit for aircraft comprising a turbine engine support arch. USP2016059328630.
  35. Glover, Anthony R.. Lightweight engine mounting. USP2015099145047.
  36. Durocher, Eric; Pietrobon, John. Locking apparatus for a radial locator for gas turbine engine mid turbine frame. USP2013018347635.
  37. Czachor, Robert Paul; Barron, Michael Leon. Method and apparatus for stiffening and apparatus. USP2004066755005.
  38. Durocher, Eric; Pietrobon, John. Method of assembly and disassembly of a gas turbine mid turbine frame. USP2013018347500.
  39. Wallace,Thomas Tracy; Gibbens,Nelson Dirk; Pierce,Martin Joseph; Dykhuizen,Cornelius H.. Methods and apparatus for mounting a gas turbine engine. USP2006087093996.
  40. Durocher, Eric; Pietrobon, John. Mid turbine frame for gas turbine engine. USP2012018091371.
  41. Durocher, Eric; Pietrobon, John; Nguyen, Lam. Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine. USP2012018099962.
  42. Durocher, Eric; Pietrobon, John; Nguyen, Lam. Mid turbine frame system for gas turbine engine. USP2012088245518.
  43. Durocher, Eric; Pietrobon, John; Nguyen, Lam. Mid turbine frame system for gas turbine engine. USP2011118061969.
  44. Udall, Kenneth F. Mounting arrangement for a gas turbine engine. USP2004036708925.
  45. Udall, Kenneth F. Mounting arrangement for a gas turbine engine. USP2005086935591.
  46. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012058167237.
  47. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012128328133.
  48. Suciu, Gabriel L.; Merry, Brian D.; Marx, Jon A.; Dye, Christopher M.. Mounting system for a gas turbine engine. USP2012028118251.
  49. Beardsley, Peter K. Mounting system for use in mounting a gas turbine engine. USP2010107815145.
  50. Glynn, Christopher Charles; Zatorski, Darek Tomasz; Yeager, Donald Scott; Dinsmore, Nicholas Rowe; Menard, Jeffrey Raymond; Miller, Brandon Wayne. Pitch change apparatus for counter-rotating propellers. USP2012128336290.
  51. Brochard, Wolfgang; Alby, Sébastien; Ewens, David. Primary structure for an attachment pylon with firewall and thermal layers. USP2018019868545.
  52. Marche, Jacques Hervé. Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment. USP2013098540186.
  53. Heyerman, Jeffrey Bernard; Olver, Bryan W.. Support links with lockable adjustment feature. USP2016029267435.
  54. Heyerman, Jeffrey Bernard; Olver, Bryan W.. Support links with lockable adjustment feature. USP2013108567202.
  55. Vignali, Mark; Merritt, Brent J.. Three-way mount bracket for aircraft cabin air supply system. USP2015028955809.
  56. Petty, Dale William. Tie rod for a gas turbine engine. USP2018029896966.
  57. Lord, Wesley K.. Transverse mounted gas turbine engine. USP2014048708274.
  58. Gallet, Francois; Grede, Audrey. Turbine engine comprising a contrarotating propeller receiver supported by a structural casing attached to the intermediate housing. USP2015129217391.
  59. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.. Turbine section of high bypass turbofan. USP2014108850793.
  60. 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.
  61. 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.
  62. 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.
  63. Heyerman, Jeffrey Bernard; Olver, Bryan; Caulfeild, Stephen. Turbofan mounting arrangement. USP2015038979491.
  64. Heyerman, Jeffrey Bernard; Olver, Bryan W.; Fielding, Bruce; Smythe, Carl. Turbofan mounting system. USP2012118313293.
  65. Beutin,Bruno; Yvon,Didier; Mazeaud,Georges; Burdin,Fabien. Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position. USP2006037007890.
  66. Chouard, Pierre-Alain Jean-Marie Philippe Hugues; Vincent, Thomas Alain Christian. Unducted propeller gas turbine engine attachment structure. USP2016129522739.

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