$\require{mediawiki-texvc}$

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.

Angled multi-hole film cooled single wall combustor dome plate 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/04
출원번호 US-0910911 (1992-07-09)
발명자 / 주소
  • Stickles Richard W. (Loveland OH) Foltz Howard L. (West Chester OH) Taylor Keith K. (Cincinnati OH) Cook George E. (Cincinnati OH) MacLean Thomas (Loveland OH) Dodds Willard J. (West Chester OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 53  인용 특허 : 0

초록

A gas turbine engine combustor is provided with a combustor dome plate film cooling means having an annular slotted ring to provide a film starting means upstream of a multi-hole film cooled single wall metal dome plate which is annular in shape. One particular embodiment provides a starting slot in

대표청구항

An annular gas turbine combustor dome comprising: an annular combustor dome consisting of a single wall combustor dome plate disposed directly in a gas turbine engine flowpath and having a hot surface and a cold surface, a plurality of air/fuel nozzle inlet apertures disposed through said plate, and

이 특허를 인용한 특허 (53)

  1. McCaffrey, Michael G., Adjustable blade outer air seal apparatus.
  2. Schumacher,Jurgen C.; Zupanc,Frank J.; Dudebout,Rodolphe, Advanced effusion cooling schemes for combustor domes.
  3. Clum, Carey; Sandoval, Jonathan Perry, Angled rail holes.
  4. Sandelis,Denis; Salan,Yves, Annular combustion chamber for a turbomachine.
  5. Leen,Thomas Anthony; Al Roub,Marwan; Staker,John Robert, Combuster swirler assembly.
  6. Ansart Denis Roger Henri,FRX ; Ciccia Patrick Samuel Andre,FRX ; Desaulty Michel Andre Albert,FRX, Combustion chamber having a multi-hole cooling system with variably oriented holes.
  7. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.
  8. Condevaux, Jamey J.; Simpkins, Lisa M.; Sordyl, John, Combustion system.
  9. Morenko,Oleg; Patel,Bhawan Bhai, Combustor and method of improving manufacturing accuracy thereof.
  10. McMasters, Marie Ann; Cooper, James Neil; Vermeersch, Michael Louis; Thomsen, Duane Douglas; Danis, Allen Michael; Cimmarusti, Gregory Allen, Combustor dome assembly of a gas turbine engine having a contoured swirler.
  11. Howell, Stephen J.; Waslo, Jennifer; Carita, Robert G., Combustor dome plate and method of making the same.
  12. Hawie, Eduardo; Markarian, Lorin; Sampath, Parthasarathy, Combustor floating collar with louver.
  13. 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.
  14. Dodo, Satoshi; Koizumi, Hiromi; Miura, Keisuke; Takahashi, Hirokazu, Combustor having modified spacing of air blowholes in an air blowhole plate.
  15. Stastny, Honza; Sampath, Parthasarathy; Desjardins, Carol; Parkman, Kenneth; Greer, John; Phillips, Stephen; Hawie, Eduardo; Schraenen, Yvan, Combustor heat shield.
  16. Stastny,Honza, Combustor heat shield.
  17. Patel, Bhawan B.; Markarian, Lorin; Despres, Melissa, Combustor heat shield with integrated louver and method of manufacturing the same.
  18. Patel, Bhawan B.; Markarian, Lorin; Despres, Melissa, Combustor heat shield with integrated louver and method of manufacturing the same.
  19. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor heat shield with variable cooling.
  20. Patel, Bhawan B.; Markarian, Lorin; Phillips, Stephen; Hawie, Eduardo, Combustor liner and heat shield assembly.
  21. Patel, Bhawan B.; Markarian, Lorin; Sampath, Parthasarthy, Combustor liner and heat shield assembly.
  22. Hawie, Eduardo; Sze, Robert, Combustor with chamfered dome.
  23. Alkabie, Hisham, Combustor with improved cooling holes arrangement.
  24. Froemming Kenneth W. ; Vehr James W. ; Mamplata Caesar G. ; Cires Alfredo, Cooled liner apparatus.
  25. Sampath Parthasarathy,CAX ; Chevrefils Andre,CAX ; Leclair Denis,CAX ; Desroches Robert,CAX, Cooling louver for annular gas turbine engine combustion chamber.
  26. Harjit Singh Hura ; Paul Edward Sabla ; James Neil Cooper ; Beverly Stephenson Duncan ; Hukam Chand Mongia ; Steven Joseph Lohmueller, Fuel nozzle assembly for reduced exhaust emissions.
  27. DuBell Thomas L. ; Wisinski William T. ; Herrin John R., Gas turbine combustor.
  28. Patel,Bhawan; Parker,Russell, Gas turbine engine combustor with improved cooling.
  29. Patel,Bhawan; Sampath,Parthasarathy; Parker,Russell, Gas turbine engine combustor with improved cooling.
  30. Quach, San; King, Christopher; Slavens, Thomas N., Gas turbine engine component with increased cooling capacity.
  31. Craig Douglas Young ; Kenneth Edward Seitzer ; Paul James Ogden, Gas-turbine air-swirler attached to dome and combustor in single brazing operation.
  32. Kwan William,DEX, Heat shield for a gas turbine combustion chamber.
  33. Schmid Achim,DEX, Heat shield for a gas turbine combustion chamber.
  34. 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.
  35. Ackermann,John F.; Arszman,Paul V.; Nagaraj,Bangalore A.; Young,Craig D.; Justis,Nicole, High temperature splash plate for temperature reduction by optical reflection and process for manufacturing.
  36. Kutter, Ella Christine; Al-Roub, Marwan; Leen, Thomas Anthony; Brown, Daniel Dale; Young, Craig Douglas; Farmer, Gilbert; Ehteshami, Mohammad, Hybrid film cooled combustor liner.
  37. Vincent C. Martling ; Brian R. Mack ; Robert J. Kraft ; Mark A. Minnich, Low NOx combustion liner with cooling air plenum recesses.
  38. Patel, Bhawan B.; Markarian, Lorin; Despres, Melissa, Method for manufacturing of fuel nozzle floating collar.
  39. Currin,Aureen Cyr; Kaczorowski,Kamil Bazyli; Jacobson,John Carl; Monty,Joseph Douglas, Methods and apparatus for fabricating gas turbine engine combustors.
  40. Currin,Aureen Cyr; Kaczorowski,Kamil Bazyli; Jacobson,John Carl; Monty,Joseph Douglas, Methods and apparatus for fabricating gas turbine engine combustors.
  41. Reback,Scott Mitchell; Sebeika,Stephen Thomas, Methods and apparatus for injecting cleaning fluids into combustors.
  42. Ogden, Paul James; Young, Craig Douglas; Vise, Steven Clayton, Methods and apparatus for washing gas turbine engine combustors.
  43. Caldwell, James M.; Emilianowicz, Edward J.; Loveless, Gary Scott, Methods for replacing a portion of a combustor dome assembly.
  44. Emilianowicz, Edward John, Methods for replacing a portion of a combustor liner.
  45. Farmer, Gilbert; Patterson, David Bruce; Stiverson, Steven Allen; Caldwell, James Michael; Emilianowicz, Edward John; Martini, Jeffrey Michael, Methods for replacing combustor liner panels.
  46. Moertle,George E.; Emilianowicz,Edward John; Pelletier,Scott Howard, Methods for replacing combustor liners.
  47. Emilianowicz, Edward John, Methods for replacing nuggeted combustor liner panels.
  48. Prociw, Lev Alexander; Brand, Joseph Horace, Modular fuel nozzle and method of making.
  49. Prociw, Lev Alexander; Brand, Joseph Horace, Modular fuel nozzle and method of making.
  50. 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.
  51. Schumacher, Jurgen C.; Zupanc, Frank J.; Dudebout, Rodolphe, Segmented effusion cooled gas turbine engine combustor.
  52. Lewis, Scott D., Turbine airfoil film cooling holes.
  53. Cortes, Thierry, Turbomachine combustion chamber having a perforated chamber end wall and with no deflector.
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