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Interstage seal cooling 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F03B-011/00
출원번호 US-0660572 (2000-09-13)
발명자 / 주소
  • Robert Barry Solda
  • Robert Francis Manning
  • David Gellman
출원인 / 주소
  • General Electric Company
대리인 / 주소
    William S. Andes
인용정보 피인용 횟수 : 34  인용 특허 : 7

초록

A turbine nozzle includes a seal pad mounted to a seal support from an inner band thereof. The seal pad is provided for cooperating with seal teeth in an interstage seal. A bypass aperture extends through the seal support to bypass cooling air around the seal pad for providing relatively cool air af

대표청구항

1. A turbine nozzle comprising:a plurality of hollow stator vanes extending between outer and inner bands, and including a flow passage having an inlet in said outer band and an outlet in said inner band for channeling cooling air therethrough; a seal support extending from said inner band laterally

이 특허에 인용된 특허 (7)

  1. Webb Alan L. (Cincinnati OH) Eckert Terry T. (Fairfield OH), Angled cooling air bypass slots in honeycomb seals.
  2. Lee Richard M. (Media PA), Cooling system for a gas turbine.
  3. North William E. (Winter Springs FL) Kennedy Mark T. (Oviedo FL), Gas turbine vane with a cooled inner shroud.
  4. Davis Paul H. (Orlando FL) Kennedy Mark T. (Oviedo FL) North William E. (Winter Springs FL), Gas turbine vane with enhanced cooling.
  5. Clarke Jonathon P. ; Steckle Charles E. ; McMahan Kevin W. ; Durgin George A. ; Bauer Randall C., Interstage seal assembly for a turbine.
  6. Correia Victor H. S. (Scotia NY) Albrecht Richard W. (Fairfield OH) Frederick Robert A. (West Chester OH), Turbine nozzle backflow inhibitor.
  7. Rieck ; Jr. Harold P. ; Kress Jeffrey A., Turbine nozzle having purge air circuit.

이 특허를 인용한 특허 (34)

  1. McCaffrey, Michael G.; Caprario, Joseph T.; Allen, George E.; Moore, Christopher; Gagnon, Ronald R., Angled on-board injector.
  2. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  3. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  4. Lee,Ching Pang; Shi,Baolan; Lu,Wenfeng; Guentert,Joseph Michael; Brassfield,Steven Robert, Corner cooled turbine nozzle.
  5. Flodman,David Allen; Shapiro,Jason David; Kulyk,Michael Peter, Countercooled turbine nozzle.
  6. Aschenbruck, Emil; Ebbing, Hildegard; Kleinefeldt, Andreas; Mohr, Klaus Dieter, Device for sealing turbomachines.
  7. Broomer, Mark; Manning, Robert Francis; Liu, Haidong, Flange cooled turbine nozzle.
  8. Rued, Peter Klaus; Koch, David; Humhauser, Werner, Flow device comprising a cavity cooling system.
  9. Johnson, Richard William; Miller, Bradley James; Johnson, David Martin, Flow inducer for a gas turbine system.
  10. Alvanos, Ioannis; Wagner, Joel H., Fluid injection system.
  11. Veith, Bjoern; Simon-Delgado, Carlos; Seng, Daniel; Haubitz, Andreas, Gas turbine.
  12. Oyarbide, Asier; Hecken, Reinhold, Gas turbine with high-pressure turbine cooling system.
  13. Bowes, Christopher Sean; Wilson, Ian David, Method and apparatus for turbine interstage seal ring.
  14. Lee, Ching-Pang; Estill, Eric Alan; Laflen, James Harvey; Vitt, Paul Hadley; Wymore, Michael Elliot, Method and system to facilitate cooling turbine engines.
  15. Lee, Ching Pang; Estill, Eric Alan; Laflen, James Harvey; Vitt, Paul Hadley; Wymore, Michael Elliot, Method and system to facilitate enhanced local cooling of turbine engines.
  16. Lee, Ching-Pang; Estill, Eric Alan; Laflen, James Harvey; Vitt, Paul Hadley; Wymore, Michael Elliot, Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly.
  17. Lee,Ching Pang; Lu,Wenfeng; Fortuna,Douglas Marti; Roniewicz,Jakub; Gniazdowski,Robert Andrzej, Methods and apparatus for assembling turbine engines.
  18. Habedank, Mark Steven; Wines, Daniel Edward; League, Christopher James; Dziech, Aaron Michael; Whitaker, George Edwin, Methods and apparatus to reduce seal rubbing within gas turbine engines.
  19. Lee, Ching-Pang; Estill, Eric Alan; Laflen, James Harvey; Jones, Daniel Verner, Methods and system for cooling integral turbine nozzle and shroud assemblies.
  20. Lee, Ching-Pang; Laflen, James Harvey; Placke, Dustin Alfred; Moore, George Elliott; Andersen, Katherine Jaynetorrence; Jones, Daniel Verner, Methods and system for cooling integral turbine shround assemblies.
  21. Lee, Ching Pang; Estill, Eric Alan; Laflen, James Harvey; Andersen, Katherine Jaynetorrence, Methods and system for recuperated circumferential cooling of integral turbine nozzle and shroud assemblies.
  22. Lee, Ching-Pang; Estill, Eric Alan; Laflen, James Harvey; Andersen, Katherine Jaynetorrence, Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies.
  23. Lee, Ching-Pang; Estill, Eric Alan; Laflen, James Harvey; Jones, Daniel Vern, Methods and system for shielding cooling air to facilitate cooling integral turbine nozzle and shroud assemblies.
  24. Walker, David E.; Toth, Barry P., Milling bleed holes into honeycomb process.
  25. Orlando,Robert Joseph; Moniz,Thomas Ory; Brauer,John Christopher; Prentice,Ian Francis; Krammer,Erich Alois; Dolan,James Patrick; Frederick,Robert Alan, Modulated flow turbine nozzle.
  26. Klasing, Kevin Samuel; Lee, Ching Pang; Hunter, Scott David, Ovate band turbine stage.
  27. Eng, Darryl; Rawlings, Christopher; Pechette, Thomas; Rogers, Friedrich T.; Um, Jae Y.; Lee, Ching-Pang, Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines.
  28. Iacopetti, Piero, Simplified support device for nozzles of a gas turbine stage.
  29. Hafner, Matthew Troy, Systems, methods, and apparatus for a turbine interstage rim seal.
  30. Liang, George, Turbine rim cavity sealing.
  31. Hafner, Matthew Troy, Turbine seal system and method.
  32. Hafner, Matthew Troy, Turbine seal system and method.
  33. Liang, George, Turbine stator vane.
  34. Schilling, John Creighton; Briggs, Robert David; McRae, Jr., Ronald Eugene, Windward cooled turbine nozzle.
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