$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Gas turbine engine combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-003/06
출원번호 US-0729167 (1991-07-12)
우선권정보 GB-0018013 (1990-08-16)
발명자 / 주소
  • Richardson John S. (Alvaston GB2)
출원인 / 주소
  • Rolls-Royce plc (London GB2 03)
인용정보 피인용 횟수 : 59  인용 특허 : 0

초록

A gas turbine engine annular combustor having a bulkhead at its upstream which is thermally protected by an annular array of heat shields. Each heat shield is provided with integral flanges which space apart the heat shields and bulkhead to define chambers therebetween. Apertures in the bulkhead dir

대표청구항

A gas turbine engine annular combustor including a bulkhead at its upstream end, said bulkhead having a plurality of apertures therein, each aperture being adapted to receive a fuel burner, the longitudinal axes of said apertures all lying on a virtual surface if rotation, the axis of which is coaxi

이 특허를 인용한 특허 (59)

  1. McCaffrey, Michael G., Adjustable blade outer air seal apparatus.
  2. Eastwood, Jonathan Jeffery; Wong, Joey; Sonntag, Robert M., Annular combustor.
  3. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  4. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  5. Clemen, Carsten; Ebel, Michael, Burner seal for gas-turbine combustion chamber head and heat shield.
  6. Hernandez, Didier Hippolyte; Noel, Thomas Olivier Marie, Combustion chamber comprising chamber end wall heat shielding deflectors and gas turbine engine equipped therewith.
  7. Sadig, Sermed; Gerendas, Miklos, Combustion chamber head of a gas turbine.
  8. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.
  9. Morenko,Oleg; Patel,Bhawan Bhai, Combustor and method of improving manufacturing accuracy thereof.
  10. Lockyer, John F.; Greenwood, Stuart A.; Dutta, Partha X.; Groocock, Ted E.; Fox, Michael D., Combustor assembly for gas turbine engine.
  11. Green, Andrew; Stuttaford, Peter; Chen, Yan; Rizkalla, Hany, Combustor end cap assembly.
  12. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor heat shield with variable cooling.
  13. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor liner and heat shield assembly.
  14. Patel, Bhawan B.; Markarian, Lorin; Sampath, Parthasarthy, Combustor liner and heat shield assembly.
  15. Stastny, Honza; Verhiel, Jeffrey Richard, Combustor with enhanced cooling access.
  16. Shafique, Harris; Prociw, Lev Alexander, Dual conduit fuel manifold for gas turbine engine.
  17. Morenko, Oleg, Fuel conveying member for a gas turbine engine.
  18. Prociw, Lev Alexander; Shafique, Harris, Fuel conveying member with heat pipe.
  19. Patel, Bhawan B.; Morenko, Oleg; Rudrapatna, Nagaraja, Fuel injection system for a gas turbine engine.
  20. Olver, Bryan William, Fuel manifold with reduced losses.
  21. Shum, Frank; Verhiel, Jeffrey, Fuel nozzle providing shaped fuel spray.
  22. Morenko, Oleg, Gas turbine combustor and fuel manifold mounting arrangement.
  23. Borns, Frederick G.; Riahi, Ardeshir, Gas turbine combustor heat shield impingement cooling baffle.
  24. Patel, Bhawan; Sampath, Parthasarathy; Parker, Russell, Gas turbine engine combustor with improved cooling.
  25. Prociw, Lev Alexander; Shafique, Harris; Fish, Jason; Patel, Bhawan B., Gas turbine engine fuel conveying member.
  26. Markarian, Lorin; Patel, Bhawan Bhai, Gas turbine floating collar.
  27. Markarian,Lorin; Patel,Bhawan Bhal, Gas turbine floating collar.
  28. Markarian, Lorin; Patel, Bhawan B., Gas turbine floating collar arrangement.
  29. Markarian,Lorin; Patel,Bhawan Bhai, Gas turbine floating collar arrangement.
  30. Ebel Michael,DEX, Head part of an annular combustion chamber of a gas turbine having a holding part to secure a burner collar in a bayonet-catch type manner.
  31. Eastwood, Jonathan Jeffery; Wong, Joey; Sonntag, Robert M.; Cheung, Albert K.; Snyder, Timothy S., Heat shield for a combustor.
  32. Prociw, Lev Alexander; Morenko, Oleg; Shafique, Harris, Heat shield for a fuel manifold and method.
  33. Schmid Achim,DEX, Heat shield for a gas turbine combustion chamber.
  34. Davenport, Nigel; Wang, Yen-Wen, Heat shield labyrinth seal.
  35. Fish, Jason; Patel, Bhawan B., Heat shield with stress relieving feature.
  36. Burd,Steven W., Heatshielded article.
  37. Sullivan, Dennis J., Interface heat shield for a combustor of a gas turbine engine.
  38. Rudrapatna, Nagaraja; Morenko, Oleg; Patel, Bhawan B., Internal fuel manifold having temperature reduction feature.
  39. Prociw, Lev Alexander; Kojovic, Aleksandar; Shafique, Harris, Internal fuel manifold with airblast nozzles.
  40. Patel, Bhawan B.; Fish, Jason; Gaudet, Dany; Gagnon, Lafleche, Internal fuel manifold with turned channel having a variable cross-sectional area.
  41. Fish, Jason Araan, Internally mounted fuel manifold with support pins.
  42. Fish, Jason Araan, Internally mounted fuel manifold with support pins.
  43. Jan Honza Stastny CA, Low cost combustor burner collar.
  44. Mueller, Mark Anthony; Dai, Zhongtao; Vermeersch, Michael Louis; Ananthakrishnanlyer, Venkatraman; Held, Timothy James; Xu, Jun; McManus, Keith Robert, Method and apparatus for assembling a gas turbine engine.
  45. Deuker, Eberhard; Pernau, Stefan; Bode, Siegfried; Diebels, Andreas; Hahner, Thomas; Hesse, Thomas; Krebs, Werner; Prade, Bernd; Schneider, Peter-Andreas; Simon, Dieter; Sturm, Berthold; Thölking, Heinrich; Warnack, Dieter; Bauer, Andreas; Lepers, Joachim; Müller, Martin, Method and device for regulating the operating line of a gas turbine combustion chamber.
  46. Dansereau, Michael Thomas; Snow, Kyle Robert, Method and system for rotating air seal with integral flexible heat shield.
  47. Patel, Bhawan B.; Morenko, Oleg; Rudrapatna, Nagaraja, Method of manufacturing a heat shield for a fuel manifold.
  48. North, Gary Lee; Dodds, Willard James, Methods and systems for cooling gas turbine engine combustors.
  49. Prociw, Lev Alexander; Kojovic, Aleksander; Shafique, Harris, Multi-channel fuel manifold.
  50. Lebel, Larry; Papple, Michael, Multiple ventilated rails for sealing of combustor heat shields.
  51. Prociw, Lev Alexander; Shafique, Harris; Sokalski, John; Pelletier, Claude Raymond, Nested channel ducts for nozzle construction and the like.
  52. Prociw,Lev Alexander; Shafique,Harris; Sokalski,John; Pelletier,Claude Raymond, Nested channel ducts for nozzle construction and the like.
  53. Fish, Jason; Patel, Bhawan B., Optimized internal manifold heat shield attachment.
  54. Fish, Jason; Patel, Bhawan B.; Oskooei, Saeid, Reduced stress internal manifold heat shield attachment.
  55. Prociw, Lev Alexander; Shafique, Harris, Redundant fuel manifold sealing arrangement.
  56. Fish, Jason; Urac, Tibor, Redundant mounting system for an internal fuel manifold.
  57. Monty Joseph D. (Boxford MA), Regenerative cooled dome assembly for a gas turbine engine combustor.
  58. Faulder, Les; Abreu, Mario E.; Srinivasan, Ram; Lane, Michael A., Splash plate dome assembly for a turbine engine.
  59. Berry, Jonathan Dwight; Dinu, Constantin; Barker, Carl Robert; Venkataraman, Krishna Kumar, Systems and methods of providing high pressure air to a head end of a combustor.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로