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Impingement/effusion cooled combustor liner 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02G-003/00
출원번호 US-0692142 (1996-08-05)
발명자 / 주소
  • Abreu Mario E.
  • Sood Virenda M.
출원인 / 주소
  • Solar Turbines Incorporated
대리인 / 주소
    Cain
인용정보 피인용 횟수 : 43  인용 특허 : 3

초록

Existing combustors have the tendency to emit emissions and require a large quantity of cooling air to retain or extend the life of the components to a reasonable life expectancy. The present combustor reduces the emissions emitted therefrom, requires a reduced quantity of cooling air while resultin

대표청구항

[ We claim:] [1.] A combustor comprising:an interior liner defining an inlet end portion and an outlet end portion being spaced apart by an axial portion, said interior liner defining a combustion side and a cooling side having a plurality of effusion holes defined therein extending between the comb

이 특허에 인용된 특허 (3)

  1. North Richard P. (Derby GB2) Madden Christopher P. (West Yorkshire GB2) Parkin Christopher S. (Derby GB2), Gas turbine engine combustor.
  2. Havercroft Peter (Derby GB2), Porous sheet structure for a combustion chamber.
  3. Pidcock Anthony (Derby GB2) Cooper Stephen M. (Derby GB2) Fry Peter (Derby GB2), Removable combustor liner for gas turbine engine combustor.

이 특허를 인용한 특허 (43)

  1. Robert James Bland, Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method.
  2. Bes,Martine; Hernandez,Didier; Lepretre,Gilles; Trahot,Denis, Annular combustion chamber for a turbomachine with an improved inner fastening flange.
  3. Kuhn, Terrel E.; Freeman, William G.; Maszk, Francis S.; Freiberg, Douglas P.; Struzek, Kenneth A.; Kobold, Lawrence A., Apparatus and method for controlling combustor liner carbon formation.
  4. Stuttaford, Peter John; Kojovic, Aleksandar, Apparatus for adjusting combustor cycle.
  5. Gates Roger Jonathan,CAX, Apparatus for reducing combustor exit duct cooling.
  6. Huth, Michael; Tiemann, Peter; Oltmanns, legal representative, Iris, Combustion chamber.
  7. Alkabie, Hisham Salman; McMillan, Robin Thomas David, Combustion chamber for a gas turbine engine.
  8. Koenig, Michael H.; Ryan, William R., Combustor assembly comprising a combustor device, a transition duct and a flow conditioner.
  9. Davis, Jr., Lewis Berkley; Chila, Ronald James, Combustor assembly for a turbine engine with enhanced cooling.
  10. Glezer Boris ; Greenwood Stuart A. ; Dutta Partha ; Moon Hee-Koo, Combustor for a low-emissions gas turbine engine.
  11. Hu, Tin Cheung John; Sze, Robert; Stastny, Honza, Combustor heat shield with carbon avoidance feature.
  12. Davis, Jr., Lewis Berkley; Chila, Ronald James, Combustor liner.
  13. Stastny, Honza; Sze, Robert, Combustor skin assembly for gas turbine engine.
  14. Stuttaford, Peter; Fischer, Bernhard; Cowburn, David Edwin; Oskooei, Saeid; Fryer, Michael Andrew; Kojovic, Aleksandar; Acton, Jeffrey Scott, Combustor turbine successive dual cooling.
  15. Alkabie, Hisham, Combustor with improved cooling holes arrangement.
  16. Alkabie, Hisham; Morenko, Oleg; McCaldon, Kian, Combustor with improved swirl.
  17. Ansart Denis Roger Henri,FRX ; Sandelis Denis Jean Maurice,FRX, Control of cooling flows for high-temperature combustion chambers having increased permeability in the downstream direction.
  18. Chandler, Paul I.; Pidcock, Anthony, Cooling arrangement for a combustion chamber.
  19. Benz,Urs; Hellat,Jaan; Joos,Franz, Damping arrangement for reducing combustion-chamber pulsation in a gas turbine system.
  20. McCaldon Kian,CAX ; Aze Robert Ming Lap,CAX ; Sampath Parthasarathy,CAX, Double pass air impingement and air film cooling for gas turbine combustor walls.
  21. Rudrapatna, Nagaraja S.; Yankowich, Paul; Hanson, Amy, Dual walled combustors with improved liner seals.
  22. Chila, Ronald James; McMahan, Kevin Weston, Effusion cooled one-piece can combustor.
  23. Jorgensen, Stephen W.; Leahy, Jr., James H., Effusion cooled transition duct.
  24. Leahy, Jr., James H., Effusion cooled transition duct with shaped cooling holes.
  25. Woodcock, Gregory O.; Ertz, Timothy; Koch, Brian, Effusion cooling techniques for combustors in engine assemblies.
  26. Ikeda,Kazufumi; Ishiguro,Tatsuo; Tanaka,Katsunori; Tanimura,Satoshi, Gas turbine combustor.
  27. Ohnishi, Keizo; Ikeda, Kazufumi; Ono, Masaki; Nishimura, Masaharu; Tanaka, Katsunori, Gas turbine combustor having an acoustic energy absorbing wall.
  28. Dudebout, Rodolphe; Brandt, Dustin; Waldman, David; Neumann, James; Payne, Art, Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques.
  29. Patel, Bhawan B.; Markarian, Lorin, Gas turbine engine reverse-flow combustor.
  30. Inoue, Tsutomu; Yamazaki, Atsushi, Gas-turbine engine combustor.
  31. Justis, Nicole; Ackermann, John F.; Arszman, Paul V.; Nagaraj, Bangalore A.; Young, Craig D., High temperature combustor wall for temperature reduction by optical reflection and process for manufacturing.
  32. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Widener,Stanley Kevin; Johnson,Thomas Edward; Intile,John C, Method and apparatus for cooling combustor liner and transition piece of a gas turbine.
  33. Intile,John Charles; West,James A.; Byrne,William, Method and apparatus for cooling combustor liner and transition piece of a gas turbine.
  34. Huffman, Marcus B., Method and apparatus to enhance transition duct cooling in a gas turbine engine.
  35. Kuhn,Terrel E.; Freeman,William G.; Maszk,Francis S.; Freiberg,Douglas P.; Struzek,Kenneth A.; Kobold,Lawrence A., Method for controlling carbon formation on repaired combustor liners.
  36. Stuttaford, Peter John; Kojovic, Aleksandar, Method of combustor cycle airflow adjustment.
  37. Starkweather, John Howard; Bennett, William; Gibbons, John; Urbanski, Anthony, Method of forming a cooling hole by laser drilling.
  38. Patel, Bhawan B.; Markarian, Lorin, Method of repairing a gas turbine engine combustor.
  39. Alkabie, Hisham, Noise reducing combustor.
  40. Alkabie, Hisham, Noise reducing combustor.
  41. Davis, Jr., Lewis Berkley; Chila, Ronald James, Thermally decoupled can-annular transition piece.
  42. Hadder,James L., Tube cooled combustor.
  43. Erbas-Sen, Nurhak; Hoke, James B.; Cheung, Albert K.; Sonntag, Robert M.; Snyder, Timothy S., Turbine engine combustor wall with non-uniform distribution of effusion apertures.
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