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Deflecting feeder bowl assembly for a turbojet engine combustion chamber 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/10
출원번호 US-0898403 (1997-07-22)
우선권정보 FR-0009363 (1996-07-25)
발명자 / 주소
  • Sandelis Denis,FRX
출원인 / 주소
  • Snecma-Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, FRX
대리인 / 주소
    Bacon & Thomas, PLLC
인용정보 피인용 횟수 : 32  인용 특허 : 9

초록

A combustion chamber is disclosed for a gas turbine engine having a feeder owl interposed between the forward end wall of the combustion chamber and an associated air and fuel injection device, the feeder bowl having a generally annular configuration with spaced apart outer and inner walls forming a

대표청구항

[ I claim:] [1.] A combustion chamber for a gas turbine engine wherein the combustion chamber has a forward end wall with at least one opening, and an air and fuel injection device having an outer wall located so as to inject air and fuel into the combustion chamber through the at least one opening,

이 특허에 인용된 특허 (9)

  1. Barbier Gerard Y. G. (Morangis FRX) Bayle-Labour Gerard J. P. (Avon FRX) Desaulty Michel A. A. (Vert Saint Denis FRX) Martinez Rodolphe (Perigny s/Yerres FRX) Perigne Jerme (Vaux le Penil FRX), Axial-centripetal swirler injection apparatus.
  2. Bayle-Laboure Gerard J. P. (Avon FRX) Desaulty Michel A. A. (Vert Saint Denis FRX) Perigne Jrome (Vaux le Peinl FRX) Sandelis Denis J. M. (Nangis FRX), Enlarged bowl member for a turbojet engine combustion chamber.
  3. Suliga William G. (Rocky Hill CT), Fuel nozzle guide structure and retainer for a gas turbine engine.
  4. Johnson Thomas G. (Palm Beach Gardens FL) Ling Cheng-Chang (Tainan TWX), Fuel nozzle swirler for combustors.
  5. Zarzalis Nikolaos,DEX ; Meikis Gunter,DEX, Gas turbine engine flame tube cooling system and integral swirler arrangement.
  6. Nagaraj Bangalore A. (West Chester OH) Weil Antoinette E. (Cincinnati OH) Devitt John W. (Loveland OH), Non-degrading reflective coating system for high temperature heat shields and a method therefor.
  7. Monty Joseph D. (Boxford MA), Regenerative cooled dome assembly for a gas turbine engine combustor.
  8. Campbell Thomas C. (Glendale OH), Thermally protected venturi for combustor dome.
  9. Barbier Gerard Y. G. (Morangis FRX) Bayle-Laboure Gerard J. P. (Avon FRX) Bouillot Pierre A. P. (Yerres FRX) Desaulty Michel A. A. (Vert-Saint-Denis FRX) Martinez Rodolphe (Perigny S/Yerre FRX), Variable flow air-fuel mixing device for a turbojet engine.

이 특허를 인용한 특허 (32)

  1. Sandelis,Denis; Salan,Yves, Annular combustion chamber for a turbomachine.
  2. Zuo, Baifang; Washam, Roy Marshall; Wu, Chunyang, Apparatus and method for cooling a combustor cap.
  3. Schreiber,Karl, Arrangement for the cooling of thermally highly loaded components.
  4. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  5. Pacheco-Tougas, Monica; Costigan, Francis K.; Stoner, Matthew D., Bulkhead panel for use in a combustion chamber of a gas turbine engine.
  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. Jakob Keller CH; Georg Keller CH; Vera Keller CH, Combustion chamber for a gas turbine.
  9. Bunel, Jacques Marcel Arthur; Ulryck, Gilles, Combustion chamber for a turbine engine.
  10. Commaret, Patrice Andre; Sandelis, Denis Jean Maurice, Combustion chamber of a turbomachine.
  11. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.
  12. Green, Andrew; Stuttaford, Peter; Chen, Yan; Rizkalla, Hany, Combustor end cap assembly.
  13. Rathmann, Ulrich; Aluri, Naresh; Loeffel, Kaspar; Huber, Michael, Combustor front panel.
  14. Patel,Bhawan Bhai; Morenko,Oleg; Sampath,Parthasarathy; Stastny,Honza; Zhou,Jian Ming, Combustor having means for directing air into the combustion chamber in a spiral pattern.
  15. Reiss, Frank; El Masalme, Jaman, Combustor head plate assembly with impingement.
  16. Xie Ping ; Huang Yonglin, Compact polarization insensitive circulators with simplified structure and low polarization mode dispersion.
  17. Xie Ping ; Huang Yonglin, Compact polarization insensitive circulators with simplified structure and low polarization mode dispersion.
  18. Xie, Ping; Huang, Yonglin, Compact polarization insensitive circulators with simplified structure and low polarization mode dispersion.
  19. Cayre, Alain; Desaulty, Michel Andre Albert; Pommier, Nicolas, Device for injecting a mixture of air and fuel, combustion chamber and turbomachine both equipped with such a device.
  20. Shum, Frank; Verhiel, Jeffrey, Fuel nozzle providing shaped fuel spray.
  21. Cheung,Albert K.; Napoli,Nikolaos; Segalman,Irving, Gas turbine combustor heat shield panel or exhaust panel including a cooling device.
  22. Pacheco Tougas,Monica; Coughlan, III,Joseph D.; Hoke,James B.; Goetschius,Alan J., Heat shield panels for use in a combustor for a gas turbine engine.
  23. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.
  24. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.
  25. North, Gary Lee; Dodds, Willard James, Methods and systems for cooling gas turbine engine combustors.
  26. Emilianowicz, Edward John, Methods for replacing a portion of a combustor liner.
  27. Francisco, Jay M.; Napier, James C.; Sapiro, Dan G.; Hagshenas, Behzad, Mixed-flow exhaust silencer assembly.
  28. Cunha, Frank J.; Kostka, Stanislav, Nozzle guide for a combustor of a gas turbine engine.
  29. Xie, Ping; Huang, Yonglin, Optical circulators using beam angle turners.
  30. Bellucci,Valter; Flohr,Peter; Paschereit,Christian Oliver; Schuermans,Bruno; Tabacco,Daniele, Reheat combustion system for a gas turbine.
  31. Patel, Nayan Vinodbhai; Kim, Kwanwoo; Sutton, Chad Holden; Thomsen, Duane Douglas; Gonyou, Craig Alan; Abramson, Harris Daniel; Russo, James A.; Stowers, Robert Andrew; Wang, Shanwu; Wang, Anquan, Sealed conical-flat dome for flight engine combustors.
  32. Cayre, Alain; Sandelis, Denis Jean Maurice, Turbomachine combustion chamber.
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