$\require{mediawiki-texvc}$

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.

Combustor-turbine nozzle interconnection 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/20
  • F02C-007/12
  • F02C-007/18
출원번호 US-0451512 (1974-03-15)
발명자 / 주소
  • Sterman Albert P. (Cincinnati OH) Brands Henry J. (Cincinnati OH) Weissborn
  • Jr. Frederick W. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 56  인용 특허 : 0

초록

A seal for use between an annular combustor and a turbine nozzle, disposed downstream of the combustor, is provided with means for effectively innerconnecting the combustor with a sidewall surrounding the nozzle. The sidewall includes an upstream extending radially projecting flange and the combusto

대표청구항

A seal for use between an annular combustor and a turbine nozzle disposed downstream of the combustor, the nozzle including a circumscribing sidewall, wherein the seal comprises: an upstream-extending first flange associated with the nozzle; a downstream-extending second flange associated with the c

이 특허를 인용한 특허 (56)

  1. Clum, Carey; Sandoval, Jonathan Perry, Angled rail holes.
  2. Conete, Eric; Forestier, Alexandre; Hernandez, Didier, Architecture for a combustion chamber made of ceramic matrix material.
  3. Sonokawa, Masayoshi; Witlicki, Russell B.; Larson, Christopher J.; Stutz, Robert C.; Mundell, Eric Charles; Muldoon, Marc J., Buffer airflow to bearing compartment.
  4. Alvanos,Ioannis; Agrawal,Rajendra; Pinero,Hector M.; Hu,Jin, Cavity on-board injection for leakage flows.
  5. Poyyapakkam, Madhavan Narasimhan; Magni, Fulvio; Ince, Nadir, Combustion chamber arrangement for operating a gas turbine.
  6. Böttcher, Andreas; Kleinfeld, Jens; Krusch, Claus, Combustion chamber wall, gas turbine installation and process for starting or shutting down a gas turbine installation.
  7. Bancalari, Eduardo; Wilson, Jody; Little, David A.; Fadok, Joseph, Combustion transition duct providing stage 1 tangential turning for turbine engines.
  8. Michel Shawn Smallwood ; Jack D. Petty, Sr. ; Edward Claude Rice, Combustor liner support and seal assembly.
  9. Weinstein, Barry, Cool tip combustor.
  10. Weidner Robert H. (Glastonbury CT), Coolable seal assembly for a gas turbine engine.
  11. Weidner Robert H. (Glastonbury CT), Coolable seal segment for a rotary machine.
  12. Neal William F. (South Windsor CT) Stevens Leonard W. (East Hampton CT), Coolable stator assembly for a gas turbine engine.
  13. Weidner Robert H. (Glastonbury CT), Coolable stator assembly for a rotary machine.
  14. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu, Cooling air recycling for gas turbine transition duct end frame and related method.
  15. Mezzedimi, Vasco; Frosini, Franco, Device for keeping the annular outlet mouth of the gas volute always centered about the nozzle assembly in a gas turbine.
  16. McCaldon Kian,CAX ; Aze Robert Ming Lap,CAX ; Sampath Parthasarathy,CAX, Double pass air impingement and air film cooling for gas turbine combustor walls.
  17. Lewis Eric A. (Chestnut Hill MA) Slater Robert H. (Beverly MA), Double rabbet combustor mount.
  18. Rudrapatna, Nagaraja S.; Yankowich, Paul; Hanson, Amy, Dual walled combustors with improved liner seals.
  19. Patel,Bhawan Bhal; Markarian,Lorin, Exit duct of annular reverse flow combustor and method of making the same.
  20. Comeau Roger J. (Ware MA) Baran ; Jr. Walter J. (So. Glastonbury CT), First stage turbine vane support structure.
  21. Sze, Robert; Verhiel, Jeffrey Richard, Floatwall dilution hole cooling.
  22. Alvanos, Ioannis; Wagner, Joel H., Fluid injection system.
  23. Tschuor, Remigi; Jones, Russell Bond; Rodriguez, Luis J.; Haehnle, Hartmut; Duggan (-Oneil), Marion, Gas turbine.
  24. Grivas, Nicolas; Patel, Bhawan B.; Morenko, Oleg; Durocher, Eric, Gas turbine combustor exit duct and HP vane interface.
  25. Grivas, Nicolas; Patel, Bhawan B.; Morenko, Oleg; Durocher, Eric, Gas turbine combustor exit duct and hp vane interface.
  26. John Charles Aicholtz, Gas turbine combustor having dome-to-liner joint.
  27. Grosjean William C. (Poway CA) Hensley John J. (Delmar CA), Gas turbine cooling systems.
  28. Nanda, Sujit; Taylor, Todd S.; Farris, Brad, Gas turbine engine flow path member.
  29. Batt, Stephen, Gas turbine nozzle arrangement and gas turbine.
  30. Nash Dudley O. (Cincinnati OH) Quinn Ronald E. (Hamilton OH), Heat shield for gas turbine engine frame.
  31. Chila, Ronald James; McMahan, Kevin Weston; Repikov, Timur, High temperature seal for a turbine engine.
  32. Carlson, Andrew, Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine.
  33. Lee,Ching Pang; Lu,Wenfeng; Fortuna,Douglas Marti; Roniewicz,Jakub; Gniazdowski,Robert Andrzej, Methods and apparatus for assembling turbine engines.
  34. Drerup, Vincent M.; Galley, Ronald; Budinger, David E.; Staszak, Mariusz P.; Lee, Ching-Pang; Albrecht, Richard W., Methods and apparatus to reduce seal rubbing within gas turbine engines.
  35. Sweeney Ralph B. (Indianapolis IN) Verdouw Albert J. (Indianapolis IN), Mount assembly for porous transition panel at annular combustor outlet.
  36. Wilkinson Wilfred H. (Turnditch GB2) Henshaw Harry (Duffield GB2), Nozzle guide vane assembly for a gas turbine engine.
  37. Davis, Anthony, Platform cooling of turbine vane.
  38. Davi, Michael Alan; Chillar, Rahul Jaikaran; Black, Stephen Hugh; Herbold, John William, Quick disconnect combustion endcover.
  39. Thompson James L. (Union Township ; Cincinnati County OH) Hauser Ambrose A. (Wyoming OH) Zlatic Mark S. (West Chester OH) Lake John C. (Hamilton OH), Seal vibration-reducing apparatus.
  40. Matthews John A. (Melrose CT) Zeisser Melvin H. (Marlborough CT) Coburn Robert E. (Mansfield Center CT), Sealing and cooling arrangement for combustor vane interface.
  41. Matsuda, Yoshihiro; Kobayashi, Masayoshi; Yoshimura, Takanobu; Miyamoto, Hiroaki, Sealing structure for combustor liner.
  42. Venkataraman, Krishna Kumar; McMahan, Kevin Weston; Repikov, Timur R.; Edwards, Kara, Seals for a turbine engine, and methods of assembling a turbine engine.
  43. Coburn Robert E. (Mansfield Center CT) Matthews John A. (Melrose CT), Sliding joint for an annular combustor.
  44. Weaver, Adam; Wilson, Jody, Support system for transition ducts.
  45. Hain, Klemens, Suspension.
  46. Crothers, Sarah Lori; Stoia, Lucas John; Carnell, Jr., William Francis, System and method for control of combustion dynamics in combustion system.
  47. Belsom, Keith Cletus, System for sealing between combustors and turbine of gas turbine engine.
  48. Kuwabara, Masamitsu; Tomita, Yasuoki; Suenaga, Kiyoshi; Kataoka, Masahito; Sato, Yoshichika; Watanabe, Koji, Tail tube seal structure of combustor and a gas turbine using the same structure.
  49. Zborovsky, James M.; Hsu, Johan; McQuiggan, Andrew G., Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine.
  50. Heinz-Schwarzmaier, Thomas; Widmer, Marc; Zahirovic, Selma; Marlow, Paul, Transitional region for a secondary combustion chamber of a gas turbine.
  51. Hines William R. (Cincinnati OH), Turbine engine with air and steam cooling.
  52. Steiger, Ulrich; Hurter, Jonas, Turbine stator nozzle cooling structure.
  53. Sandelis Denis,FRX, Turbojet engine combustion chamber with heat protecting lining.
  54. Pruthi, Rohit; Jadhav, Sanjay Shankar, Turbomachine seal assembly.
  55. Benz, Urs; Hurter, Jonas; Motzkus, Thorsten, Turbomachine, especially gas turbine.
  56. Kelm James S. (Milford OH) Maclin Harvey M. (Cincinnati OH) Vickers Edward C. (Cincinnati OH) Wakeman Thomas G. (West Chester OH), Variable turbine vane support.
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