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Arrangement of heat resistant tiles for a gas turbine engine combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/60
출원번호 US-0898278 (1997-07-22)
우선권정보 GB-0003581 (1995-02-23)
발명자 / 주소
  • Bell Lance P.,GB3
  • Gater Neil,GB3
  • Pidcock Anthony,GB3
  • Close Desmond,GB3
  • Cross Simon,GB3
출원인 / 주소
  • Rolls-Royce PLC, GB3
대리인 / 주소
    Oliff & Berridge, PLC
인용정보 피인용 횟수 : 40  인용 특허 : 4

초록

A plurality of heat resistant tiles are provided which combine to form an internal liner around the walls of an annular combustor. In a first embodiment a plurality of tiles are arranged in an overlapping relationship to form a fully annular shield around an upstream bulkhead wall. In a second embod

대표청구항

[ We claim:] [1.] An arrangement of heat resistant tiles forming an internal liner of a gas turbine combustor, comprising a plurality of tiles mounted in a contiguous manner on an inner surface of the combustor, each of the plurality of tiles being mounted on a wall of the combustor by attachment me

이 특허에 인용된 특허 (4)

  1. Sterman Albert P. (Cincinnati OH) Wakeman Thomas G. (Cincinnati OH) Williams Jesse J. (Cincinnati OH), Combustion chamber construction.
  2. Able Edward C. (Tolland CT) Gibler Martin J. (Manchester CT), Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles.
  3. Veau Albert L. P. (Combs la Ville FRX), Heat protective lining for a passage in a turbojet engine.
  4. Able Edward C. (Tolland CT) Gibler Martin J. (Manchester CT), High temperature combustor liner.

이 특허를 인용한 특허 (40)

  1. Holt, Alistaire S; MacQuisten, Michael A; Whiteman, Michael; Moran, Anthony J, Acoustic damper.
  2. Eastwood, Jonathan Jeffery; Wong, Joey; Sonntag, Robert M., Annular combustor.
  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. Davenport, Nigel Caldwell; Hawie, Eduardo David, Asymmetric combustor heat shield panels.
  5. Ruberte Sanchez, Jose E.; McAlice, Timothy J.; Rugg, Kevin L., Attachment assembly for protective panel.
  6. Dierberger, James A.; Schlichting, Kevin W.; Freling, Melvin, Ceramic combustor liner panel for a gas turbine engine.
  7. Commaret, Patrice Andre; Hernandez, Didier Hippolyte; Lunel, Romain Nicolas, Chamber-bottom baffle, combustion chamber comprising same and gas turbine engine fitted therewith.
  8. Anthony Pidcock GB; Desmond Close GB; Michael P Spooner GB, Combustion apparatus.
  9. Garry, Ian Murray; Carlisle, Michael Lawrence; Clark, Daniel; Barcock, Carl Lee, Combustion apparatus.
  10. Pidcock, Anthony; Close, Desmond; Spooner, Michael P, Combustion apparatus.
  11. Pidcock, Anthony; Close, Desmond; Spooner, Michael P., Combustion apparatus.
  12. Tentorio, Luca, Combustion apparatus having a fuel controlled valve that temporarily flows purging air.
  13. Davis, Jr., Lewis Berkley; Chila, Ronald James, Combustor liner.
  14. Patel, Bhawan Bhai; Sampath, Parthasarathy; Fish, Jason Araan, Combustor liner V-band design.
  15. Patel,Bhawan Bhal; Sampath,Parthasarathy; Fish,Jason Araan, Combustor liner v-band design.
  16. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with decreased liner cooling.
  17. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with reduced cooling dilution openings.
  18. Garry, Ian Murray; Carlisle, Michael Lawrence, Combustor wall apparatus with parts joined by mechanical fasteners.
  19. Cunha, Frank J.; Kostka, Stanislav; Snyder, Timothy S., Combustor wall assembly for a turbine engine.
  20. H채ggander,Jan, Component for being subjected to high thermal load during operation and a method for manufacturing such a component.
  21. Chandler, Paul I.; Pidcock, Anthony, Cooled double walled article.
  22. Bellucci,Valter; Hurter,Jonas; Pross,Joerg, Device for efficient usage of cooling air for acoustic damping of combustion chamber pulsations.
  23. Mitchell, Ian Edward; Clark, Daniel; Tuppen, Stephen John, Gas heater.
  24. Bagnall, Adam MacGregor, Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction.
  25. Kostka, Stanislav; Cunha, Frank J., Heat shield panels with overlap joints for a turbine engine combustor.
  26. Hawie, Eduardo; Ozem, Hayley, Heat shield sealing for gas turbine engine combustor.
  27. Hofmann, Daniel; Jeppel, Paul-Heinz; Maghon, Hans; Rettig, Uwe; Schmahl, Milan; Taut, Christine, Heat-shield brick, combustion chamber comprising an internal, combustion chamber lining and a gas turbine.
  28. Gross Heinz-Jurgen,DEX ; Schulten Wilhelm,DEX, Heat-shield component with cooling-fluid return and heat-shield configuration for a component directing hot gas.
  29. Dierberger, James A.; Hongoh, Masamichi; Sullivan, Dennis J., Insert adjacent to a heat shield element for a gas turbine engine combustor.
  30. Hayton Paul R,GBX ; Bacon Richard A E,GBX, Jet pipe liner.
  31. Stastny, Honza; Sampath, Parthasarathy, Method for a fabricated heat shield with rails and studs mounted on the cold side of a combustor heat shield.
  32. 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.
  33. Graves, Charles B.; Cummings, III, William G.; Bennett, Russell N.; Shi, Jun, Shell and tiled liner arrangement for a combustor.
  34. Graves, Charles B; Cummings, III, William G; Bennett, Russell N; Shi, Jun, Shell and tiled liner arrangement for a combustor.
  35. O'Leary, Mark, Shielding for a gas turbine engine component.
  36. Tiemann, Peter, Thermal shield for a component carrying hot gases, especially for structural components of gas turbines.
  37. Hadder,James L., Tube cooled combustor.
  38. Eastwood, Jonathan J.; Moura, Dennis M., Turbine engine combustor heat shield with multi-height rails.
  39. Carlisle, Michael Lawrence; Garry, Ian Murray, Wall element for use in combustion apparatus.
  40. Anthony Pidcock GB; Desmond Close GB; Michael P. Spooner GB, Wall elements for gas turbine engine combustors.
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