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Heat shield arrangement for a gas turbine combustion chamber 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02G-003/00
출원번호 US-0913122 (1997-09-08)
우선권정보 DE-0008111 (1995-03-08)
국제출원번호 PCT/EP96/00860 (1996-03-01)
§371/§102 date 19970908 (19970908)
국제공개번호 WO-9627765 (1996-09-12)
발명자 / 주소
  • Kwan William,DEX
출원인 / 주소
  • BMW Rolls-Royce GmbH, DEX
대리인 / 주소
    Evenson, McKeows Edwards & Lenahan, P.L.L.C.
인용정보 피인용 횟수 : 42  인용 특허 : 4

초록

In order to cool the hot surface of the heat shield that surrounds the burner of a gas turbine annular combustion chamber as efficiently as possible, especially in the vicinity of the burner throughflow opening, a cooling air stream that escapes through a ridge that runs around the edge of the throu

대표청구항

[ I claim:] [1.] A gas turbine combustion chamber having a heat shield with a central through-flow opening for a burner and a ridge running around an edge of the central through-flow opening, comprising:a plurality of air blow-by openings arranged in said ridge for cool air guided against a cold bac

이 특허에 인용된 특허 (4)

  1. Zeisser Melvin H. (Marlborough CT), Combustor bulkhead heat shield assembly.
  2. Peterson Steven C. (Vernon CT) Stevens Leonard W. (Vernon CT) Tanrikut Ibrahim S. (Manchester CT), Fuel nozzle guide heat shield for a gas turbine engine.
  3. Pearce Donald E. (Bristol GB2) Westlake Michael J. (Charfield GB2), Gas turbine engine combustor heatshield.
  4. Monty Joseph D. (Boxford MA), Regenerative cooled dome assembly for a gas turbine engine combustor.

이 특허를 인용한 특허 (42)

  1. Guezengar,Dominique; Hernandez,Didier Hippolyte; Noel,Thomas Olivier Marie; Zischek,Michel, Arrangement with a twist-lock coupling for a turbomachine combustion chamber.
  2. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  3. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  4. Clemen, Carsten; Ebel, Michael, Burner seal for gas-turbine combustion chamber head and heat shield.
  5. Gruschka, Uwe, Combustion chamber and gas turbine installation.
  6. Hernandez, Didier Hippolyte; Noel, Thomas Olivier Marie, Combustion chamber comprising chamber end wall heat shielding deflectors and gas turbine engine equipped therewith.
  7. Biebel, Romain; Gautier, Claude; Sandelis, Denis Jean Maurice, Combustion chamber end wall with ventilation.
  8. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.
  9. Smallwood, Michel S.; Wigal, Mindi D., Combustor assembly for a gas turbine engine.
  10. Papple, Michael, Combustor dome heat shield.
  11. Papple, Michael; Sze, Robert, Combustor dome heat shield.
  12. Hawie, Eduardo; Markarian, Lorin; Sampath, Parthasarathy, Combustor floating collar with louver.
  13. Stastny, Honza; Sampath, Parthasarathy; Desjardins, Carol; Parkman, Kenneth; Greer, John; Phillips, Stephen; Hawie, Eduardo; Schraenen, Yvan, Combustor heat shield.
  14. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor heat shield with variable cooling.
  15. Davis, Jr., Lewis Berkley; Chila, Ronald James, Combustor liner.
  16. Holcomb, Marcus Timothy; Taylor, Todd; Yount, Randall E., Combustor liner.
  17. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor liner and heat shield assembly.
  18. Patel, Bhawan B.; Markarian, Lorin; Sampath, Parthasarthy, Combustor liner and heat shield assembly.
  19. Webb, René´ James, Combustor liners.
  20. Commaret, Patrice Andre; Sandelis, Denis Jean Maurice; Trahot, Denis Gabriel, Device for injecting a mixture of air and fuel, and a combustion chamber and turbomachine provided with such a device.
  21. Matsuyama, Ryusuke; Kobayashi, Masayoshi; Horikawa, Atsushi; Fujiwara, Hitoshi, Fuel injection device.
  22. Horikawa, Atsushi; Ogata, Hideki; Yamaguchi, Kenta; Matsuyama, Ryusuke, Gas turbine combustor.
  23. Borns, Frederick G.; Riahi, Ardeshir, Gas turbine combustor heat shield impingement cooling baffle.
  24. Markarian, Lorin; Patel, Bhawan Bhai, Gas turbine floating collar.
  25. Markarian,Lorin; Patel,Bhawan Bhal, Gas turbine floating collar.
  26. Markarian,Lorin; Patel,Bhawan Bhai, Gas turbine floating collar arrangement.
  27. Gerendas, Miklos; Sadig, Sermed, Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall.
  28. Milburn, Richard G., Head part of an annular combustion chamber.
  29. Nicholls, Andrew; Carlisle, Michael L; Garry, Ian M; Wybrow, Michael N, Head part of an annular combustion chamber.
  30. Burd,Steven W., Heatshielded article.
  31. Jan Honza Stastny CA, Low cost combustor burner collar.
  32. DeVane, Shaun Michael; Show, Erika Suzanne; Wiehe, Glenn Edward; Umbaugh, Timothy Glen; Cooper, James Neil; Wenclik, Mateusz Pawel; Krol, Marek Krzysztof, Method and apparatus for heat shielding gas turbine engines.
  33. Barton, Jesse Ellis; Berry, Jonathan Dwight; Hadley, Mark Allan; Nelson, Glenn David; Rohrssen, Robert Joseph; Vanselow, John Drake, Method and apparatus for introducing diluent flow into a combustor.
  34. Barton, Jesse Ellis; Berry, Jonathan Dwight; Hadley, Mark Allan; Melton, Patrick Benedict, Method and apparatus of introducing diluent flow into a combustor.
  35. Bibler, John D.; Held, Timothy J.; Mueller, Mark A., Method and apparatus to decrease gas turbine engine combustor emissions.
  36. Stastny, Honza; Sampath, Parthasarathy; Desjardins, Carol; Parkman, Kenneth; Greer, John; Phillips, Stephen; Hawie, Eduardo; Schraenen, Yvan, Method for manufacturing a combustor heat shield.
  37. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.
  38. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.
  39. North, Gary Lee; Dodds, Willard James, Methods and systems for cooling gas turbine engine combustors.
  40. Emilianowicz, Edward John, Methods for replacing a portion of a combustor liner.
  41. Davis, Jr., Lewis Berkley; Chila, Ronald James, Thermally decoupled can-annular transition piece.
  42. Locatelli, David; Lunel, Romain Nicolas; Noel, Thomas Olivier Marie; Sandelis, Denis Jean Maurice, Turbomachine combustion chamber arrangement having a collar deflector.
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