$\require{mediawiki-texvc}$

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.

Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01B-005/18
  • F02C-007/16
출원번호 US-0047571 (1979-06-11)
발명자 / 주소
  • Rice Ivan G. (P.O. Box 233 Spring TX 77373)
인용정보 피인용 횟수 : 41  인용 특허 : 2

초록

Steam-cooling with a steam thermal barrier for reheat gas turbine vanes and blades offers advantages over cooling with air or water at the higher temperatures characteristic of existing high temperature gas tubines, in particular when coupled with a reheat steam cycle. Consequently, in such a combin

대표청구항

In the production of useful power wherein compressed heated gas is produced for contacting turbine blading for rotating a turbine shaft, and said turbine blading is cooled, the improvement comprising; introducing steam into the interior of said blading, directing steam from the interior of said blad

이 특허에 인용된 특허 (2)

  1. Leogrande John A. (West Hartford CT) Levine Richard (Bloomfield CT), Air cooled turbine vanes.
  2. Freeman ; Jr. William R. (North Muskegon MI), Cooled composite vanes for turbine nozzles.

이 특허를 인용한 특허 (41)

  1. Tabbita Martin G. ; Downs James P. ; Soechting Friedrich O. ; Auxier Thomas A., Apparatus and method for cooling an airfoil for a gas turbine engine.
  2. Groess Helmut (Esterhofen DEX) Graeml ; deceased Horst (late of Markt Indersdorf DEX by Edith Graeml ; administrator), Axial-flow turbine blade, especially axial-flow turbine rotor blade for gas turbine engines.
  3. Carreno Diether E. (Schenectady NY) Myers Albert (Amsterdam NY) Palmer Gene D. (Clifton Park NY) Caruso Philip M. (Selkirk NY) Wilson Ian D. (Clifton Park NY) Hemsworth Martin C. (Cincinnati OH), Closed or open circuit cooling of turbine rotor components.
  4. Mukherjee Dilip (Fislisbach CHX), Combined gas turbine and steam turbine power station.
  5. Rice Ivan G. (P.O. Box 233 Spring TX 77383), Compression intercooled gas turbine combined cycle.
  6. Sahm Michael K. (Ellington CT) Milano Robert (East Hartford CT), Convergent-divergent film coolant passage.
  7. LaFleur Ronald Samuel, Coolable airfoil for a gas turbine engine.
  8. Ahmad, Fathi, Coolant bridging line for a gas turbine, which coolant bridging line can be inserted into a hollow, cooled turbine blade.
  9. Lock Gary D,GBX ; Oldfield Martin L G,GBX, Coolant passages for gas turbine components.
  10. Auxier Thomas A. (Lake Park FL) Anderson Leon R. (Tequesta FL) Hill ; Jr. Edward C. (Tequesta FL), Coolant passages with full coverage film cooling slot.
  11. Ferber, J?rgen; Weigand, Bernhard, Cooled components with conical cooling passages.
  12. Hall Kenneth B. (Jupiter FL) Landis Kenneth K. (Tequesta FL), Cooled gas turbine blade.
  13. Frank J. Cunha ; Anthony L. Schiavo, Jr. ; Raymond Scott Nordlund ; Thomas Malow ; Barry L. McKinley, Cooled turbine vane with endcaps.
  14. Vehr James W. (Lake Park FL), Cross-flow film cooling passages.
  15. Graham, Robert W.; Papell, S. Stephen, Curved film cooling admission tube.
  16. Phillips James S. (Jupiter FL) Field Robert E. (Tequesta FL), Film coolant passage with swirl diffuser.
  17. Auxier Thomas A. (Lake Park FL) Field Robert E. (Tequesta FL), Film coolant passages for cast hollow airfoils.
  18. Field Robert E. (Tequesta FL), Film cooling passages with curved corners.
  19. Mukherjee,Dilip, Gas turbine and associated cooling method.
  20. Schott, Carl Gerard; Beadie, Douglas Frank; Black, Kenneth Damon; Cao, Khoa Dang, Gas turbine exhaust diffuser strut fairing having flow manifold and suction side openings.
  21. Cunha Frank J., Gas turbine row #1 steam cooled vane.
  22. Ackermann, John F.; Arszman, Paul V.; Nagaraj, Bangalore A., High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing.
  23. Ceric, Hajrudin; Gaio, Giuseppe; Günther, Frank; Hülfenhaus, Armin; Hülsemann, Gerhard; Jungnickel-Marques, Gabriel; Wanz, Stefan, Liquid injection in a gas turbine during a cooling down phase.
  24. Auxier Thomas A. ; Downs James P. ; Kvasnak William S. ; Soechting Friedrich O. ; Calhoun William H. ; Hayes Douglas A., Method and apparatus for cooling an airfoil.
  25. Soechting Friedrich O. ; Kvasnak William A. ; Auxier Thomas A. ; Downs James P. ; Calhoun William H. ; Hayes Douglas A., Method and apparatus for cooling an airfoil.
  26. Frutschi Hansulrich,CHX ; Hausermann Alfred,CHX, Method of operating a power station plant with steam cooling.
  27. McMahan, Kevin Weston; Chila, Ronald James; Johns, David Richard, Methods and systems for cooling a transition nozzle.
  28. Tonks Robert C. (Bridgwater GB2), Nozzle guide vane for a gas turbine engine.
  29. Cunha, Francisco J.; Chiu, R. Paul, Steam and air cooling for stator stage of a turbine.
  30. Palmer, Miles; Allam, Rodney John; Fetvedt, Jeremy Eron, System and method for high efficiency power generation using a nitrogen gas working fluid.
  31. Bunker Ronald Scott, Tandem airfoils.
  32. Wei George C. (Weston MA) Walsh John (Milford MA), Thermal shock test apparatus and the method of testing.
  33. Readnour Jack L. (Toledo OH), Turbine airfoil.
  34. Tung Stephen K. ; Weldon Donald C., Turbine airfoil breakout cooling.
  35. Liang, George, Turbine airfoil with showerhead cooling holes.
  36. Miranda, Carlos Miguel; Trimmer, Andrew Lee; Kottilingam, Srikanth Chandrudu; Lacy, Benjamin Paul, Turbine component having surface cooling channels and method of forming same.
  37. Hines William R. (Cincinnati OH), Turbine engine with air and steam cooling.
  38. Higashimori,Hirotaka; Osako,Katsuyuki; Shiraishi,Takashi; Mikogami,Takashi, Turbine rotor blade.
  39. Campbell, Christian X., Vane assembly with metal trailing edge segment.
  40. Campbell,Christian X., Vane assembly with metal trailing edge segment.
  41. Grieb Hubert (Germering DEX), Weapon system.
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