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Duct support assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0501994 (1990-03-30)
발명자 / 주소
  • MacGee Andrew (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 38  인용 특허 : 0

초록

A duct support assembly includes first and second spaced rings joined by a plurality of circumferentially spaced links. First and second means pivotally join the links to the first and second rings, and the links may be assembled through an outer surface of the first ring and are adjustable from the

대표청구항

A duct support assembly comprising: a) a first ring having an outer surface; b) a second ring spaced radially inwardly from said first ring to define an annual duct there between; c) a plurality of circumferentially spaced links joining said first and second rings, each of said links comprising a bo

이 특허를 인용한 특허 (38)

  1. Roth, Douglas R.; Munshi, Mrinal, Adjustable bracing apparatus and assembly method for gas turbine exhaust diffuser.
  2. Peters, Donald W., Adjustable cable for exhaust duct liner hanger.
  3. Peters, Donald W., Adjustable cable for exhaust duct liner hanger.
  4. Preston, III, Lon H., Adjustable hanger and method for gas turbine engine exhaust liner.
  5. Farah, Jorge I.; Hickman, Jason; Cintron, Jose, Bushing for torque load transfer attachment hardware.
  6. Morenko,Oleg, Combustor attachment with rotational joint.
  7. Preston, Lon H., Compliant heat shield liner hanger assembly for gas turbine engines.
  8. Commaret, Patrice Andre; Duval, Sylvain; Hernandez, Didier Hippolyte; Vuillemenot, Yann Francois Jean-Claude, Device for attaching a combustion chamber.
  9. Porte, Alain; Fargues, Matthieu; Lalane, Jacques, Device for connecting an air inlet with an aircraft nacelle actuator assembly.
  10. Combes, Stephane; Lafont, Laurent, Engine mounting structure interposed between an aircraft wing system and said engine.
  11. Conete, Eric; Baroumes, Laurent; Habarou, Georges, Exhaust system for gas turbine.
  12. Roberge, Gary D, Exhaust system having a flow path liner supported by structural duct segments.
  13. Eleftheriou, Andreas; Menheere, David; Liu, Quantai, Fabricated intermediate case with engine mounts.
  14. Salamon, Keith T.; Turner, Matthew A.; Tirone, John P., Flexible connection between a wall and a case of a turbine engine.
  15. Dhaliwal, Kamaljit Kaur, Gas turbine engine comprising a casing surrounding a rotary assembly and a manifold secured to the casing via a securing arrangement.
  16. Major, Daniel W.; Torres, Edward, Inlet guide vane inner air seal surge retaining mechanism.
  17. Vrljes, Ljubisa; Caulfeild, Stephen, Inner bypass duct wall attachment.
  18. Todorovic, Predrag, Joint between components.
  19. Peters, Donald W., Liner hanger cable.
  20. Bellabal, Francois Robert; Florent, Nicolas, Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements.
  21. Casavant, Matthew Stephen; Wilson, Bradley Edwin, Methods and apparatus to facilitate turbine casing assembly.
  22. Scheper, Frank; Eismann, Jens; Langhorst, Friedhelm; Knopp, Soren, Motor vehicle with a vehicle frame.
  23. Thompson, Ewan F, Mounting arrangement.
  24. McAlice, Timothy J.; Figueroa, Carlos G., Panel support hanger for a turbine engine.
  25. Petty, Dale William; Martinez, Gonzalo F., Pivoting liner hanger.
  26. Prociw, Lev Alexander; Kojovic, Aleksandar, Positioning arrangement for components of a pressure vessel and method.
  27. Prociw, Lev Alexander; Kojovic, Alexsandar, Positioning arrangement for components of a pressure vessel and method.
  28. Spitzer, Robert Watson; Light, Kevin; Terpos, Brian Harry; Guinan, Dan, Radially expanding turbine engine exhaust cylinder interface.
  29. Eleftheriou, Andreas; Olver, Bryan; Alecu, Carmen, Rear mount assembly for gas turbine engine.
  30. Martinez, Gonzalo F., Slideable liner link assembly.
  31. Kramer, George J., Spherical collet for mounting a gas turbine engine liner.
  32. Cameriano, Laurent Bernard; Girard, Nicolas Pierre-Marie, Structural turbine engine casing.
  33. Heyerman, Jeffrey Bernard; Olver, Bryan W., Support links with lockable adjustment feature.
  34. Heyerman, Jeffrey Bernard; Olver, Bryan W., Support links with lockable adjustment feature.
  35. Gekht,Eugene; Fontaine,Mike; Jutras,Martin, Turbine exhaust case and method of making.
  36. Heyerman, Jeffrey Bernard; Olver, Bryan; Caulfeild, Stephen, Turbofan mounting arrangement.
  37. Heyerman, Jeffrey Bernard; Olver, Bryan W.; Fielding, Bruce; Smythe, Carl, Turbofan mounting system.
  38. Watson, Bill Russell; Warden, Max, Turbomachine core coupling assembly.
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