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Combustor liner 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02G-003/00
  • F02G-001/00
출원번호 US-0447836 (1982-12-08)
발명자 / 주소
  • Kenworthy Milton J. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 35  인용 특허 : 7

초록

A combustor liner for use between a cooling fluid and hot combustion gases is disclosed. The combustor liner includes portions having different thermal coefficients of expansion so that portions subject to relatively high temperatures have relatively low coefficients of expansion and portions subjec

대표청구항

A combustor liner for use between a cooling fluid and hot combustion gases comprising adjacent portions having different thermal coefficients of expansion effective for reducing stress due to differential thermal expansion tendency of said adjacent portions.

이 특허에 인용된 특허 (7)

  1. Koshoffer John M. (Cincinnati OH) Ekstedt Edward E. (Montgomery OH) Stamm Edward I. (Cincinnati OH), Combustor liner slot with cooled props.
  2. Stamm Edward I. (Cincinnati OH), Combustor liner structure.
  3. Caruel Jacques E. J. (Maincy FRX) Gastebois Philippe M. D. (Melun FRX) Coutor Simone (Melun FRX), Cooling of combustion chamber walls using a film of air.
  4. Holland Brian C. (Darley Abbey GB2) Hirst Roy T. (Ticknall GB2) Sills Roger J. M. (Littleover GB2) Moore Cyril G. (Littleover GB2), Gas turbine engines.
  5. Needham Peter Richard (Bristol EN) Langley Kenneth Richard (Wotton-under-Edge EN), Gas turbine engines.
  6. Jenkinson John (Bristol EN), Matching differential thermal expansions of components in heat engines.
  7. DuBell Thomas L. (Maineville OH), Stabilizing dimple for combustion liner cooling slot.

이 특허를 인용한 특허 (35)

  1. Gely Jean-Marie L. (Le Havre FRX), Air take-off for a turbojet engine cold flow duct.
  2. Bulman, David Edward; Darkins, Jr., Toby George; Schroder, Mark Stewart; Lipinski, John Joseph, Bolting configuration for joining ceramic combustor liner to metal mounting attachments.
  3. Vogt Robert L. (Marblehead MA), Breach-cooled structure.
  4. Dierberger James A. (Hebron CT) Tumicki Thomas F. (Yantic CT), Coated high temperature combustor liner.
  5. Jopp, Lisa Jane; Willis, Nathan Thomas, Combustion chamber arrangement.
  6. Berdou, Caroline Jacqueline Denise; Cameriano, Laurent Bernard, Combustion chamber for a turbine engine.
  7. Farmer,Gilbert; Groeschen,James A.; Redden,Ronald D.; DeVane,Shaun M., Combustor linear and method for making thereof.
  8. Farmer, Gilbert; Groeschen, James A.; Redden, Ronald D.; DeVane, Shaun M., Combustor liner and method for making thereof.
  9. Foltz Howard L. (Westchester OH), Combustor liner cooling arrangement.
  10. Sahm Michael K. (Ellington CT) Milano Robert (East Hartford CT), Convergent-divergent film coolant passage.
  11. Lee, Ching-Pang; Prakash, Chander; Schilp, Reinhard; Little, David A., Cooled conduit for conveying combustion gases.
  12. Lee Ching-Pang, Dimpled impingement baffle.
  13. Barry, Vincent Anthony; Demarche, Thomas Edward, Failsafe film cooled wall.
  14. Field Robert E. (Tequesta FL), Film cooling passages with curved corners.
  15. Nagai, Tomoto; Katou, Eigo; Konishi, Tetsu, Gas turbine combustor.
  16. Farmer, Gilbert; Brown, Daniel D.; Rutherford, Myron E.; Vise, Steven C.; Martini, Jeffrey M., Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form.
  17. Tschuor, Remigi; Schneider, Lothar; Markovic, Alen; Hähnle, Harmut, Gas turbine with welded combustor liners.
  18. Grote, Holger; Heilos, Andreas; Tertilt, Marc, Heat shield element, method and mold for the production thereof, hot-gas lining and combustion chamber.
  19. Grote, Holger; Heilos, Andreas; Tertilt, Marc, Heat shield element, method and mold for the production thereof, hot-gas lining and combustion chamber.
  20. Ramier, Stephen A.; Ryan, William R., Integral flow sleeve and fuel injector assembly.
  21. Caldwell, James M.; Emilianowicz, Edward John; Loveless, Gary, Method for repair and replacement of combustor liner panel.
  22. Wunderlich, Thomas; Roth-Fagaraseanu, Dan; Schruefer, Susanne, Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component.
  23. Christopher K. Nelson ; David B. Patterson ; Eugene F. Pridgett, Method of making a combustion chamber liner.
  24. Bouillot Pierre A. P. (Yerres FRX) Genet Claude A. L. (Vigneux FRX), Method of manufacturing cooling film devices for combustion chambers of turbomachines.
  25. Manteiga, John Alan; Thomsen, Duane Douglas; Brown, Daniel Dale; Brauer, John Christopher, Methods and apparatus for assembling gas turbine engines.
  26. Howell,Stephen John; Jacobson,John Carl; McCaffrey,Timothy P.; Barnes,Barry Francis, Methods and apparatus for film cooling gas turbine engine combustors.
  27. Reback,Scott Mitchell; Sebeika,Stephen Thomas, Methods and apparatus for injecting cleaning fluids into combustors.
  28. Caldwell, James M.; Emilianowicz, Edward J.; Loveless, Gary Scott, Methods for replacing a portion of a combustor dome assembly.
  29. Farmer, Gilbert; Patterson, David Bruce; Stiverson, Steven Allen; Caldwell, James Michael; Emilianowicz, Edward John; Martini, Jeffrey Michael, Methods for replacing combustor liner panels.
  30. Moertle,George E.; Emilianowicz,Edward John; Pelletier,Scott Howard, Methods for replacing combustor liners.
  31. Emilianowicz, Edward John, Methods for replacing nuggeted combustor liner panels.
  32. Monty, Joseph Douglas; Jacobson, John C., Slot cooled combustor line.
  33. Abuaf Nesim ; Goebel Steven George, Thermal spreading combustion liner.
  34. McMasters,Marie Ann, Thick coated combustor liner.
  35. Slavens, Thomas N.; Snyder, Brooks E., Variable vane segment.
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