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Gas turbine stator vane assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-009/04
출원번호 US-0855082 (1997-05-13)
발명자 / 주소
  • Heumann David E.
  • Maier M. Stefan
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Getz
인용정보 피인용 횟수 : 34  인용 특허 : 8

초록

A stator vane assembly for a gas turbine engine includes a plurality of stator vane segments and fasteners. Each stator vane segment includes an inner radial platform, an outer radial platform, at least one airfoil extending between said platforms, and a first mounting flange extending radially outw

대표청구항

[ We claim:] [1.] A stator vane assembly for a gas turbine engine, comprising:a plurality of stator vane segments, each segment having an inner radial platform, an outer radial platform, at least one airfoil extending between said platforms, and a first mounting flange extending radially outward fro

이 특허에 인용된 특허 (8)

  1. Donlan John P. (Ovideo FL), Apparatus and method for supporting a vane segment in a gas turbine.
  2. Kunz Cleon V. (West Hartford CT), Axial flow compressor case.
  3. Wentzell Timothy H. (South Windsor CT), Compression sleeve tube repair.
  4. Donlan John P. (Aston PA) Krauss Alfred R. (Oak Valley NJ), Locking structure for an alignment bushing of a combustion turbine engine.
  5. McLaurin Leroy D. (Winter Springs FL) Williams Roland E. (Altamonte Springs FL) Donlan John P. (Oviedo FL) Hultgren Kent G. (Swarthmore PA), Method and apparatus for vane segment support and alignment in combustion turbines.
  6. Duran John A. (Glendora CA), Non-removable structural fastener assembly.
  7. Harris Harold S. (Glastonbury CT), One piece band seal.
  8. Brown Henry B. (Manchester CT) Cantor Eugene (Glastonbury CT) DeTolla Francis L. (Vernon CT) Vollinger Gary J. (Simsbury CT), Turbine cooling.

이 특허를 인용한 특허 (34)

  1. Grant, Carl; Douglas, David Curr; Payling, Stephen Rex; Vota, James, Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine.
  2. Jason Francis Pepi ; Brian Edward Dix ; Tyler Frederick Hooper, Bolted joint for rotor disks and method of reducing thermal gradients therein.
  3. Jason Francis Pepi ; Todd Alan Ebert, Bolted joint for rotor disks and method of reducing thermal gradients therein.
  4. Boeke, Mark A.; Rajchel, Kevin; Blake, Mosheshe Camara-khary; Simms, Vincent E., Chordal seal.
  5. Michel Shawn Smallwood ; Jack D. Petty, Sr. ; Edward Claude Rice, Combustor liner support and seal assembly.
  6. Samuelsson, Rickard; Jansson, Niklas, Component and a gas turbine engine comprising the component.
  7. Drelon, Godefroy Francis Frederic; Prestel, Sebastien Jean Laurent; Soupizon, Jean-Luc, Connection of radial arms to a circular sleeve via axes and spacers.
  8. Belmonte, Olivier; Le Goff, Stevan; Rodrigues, Paul, Cooling device for cooling the slots of a turbomachine rotor disk downstream from the drive cone.
  9. Rice, Edward Claude; Molnar, Jr., Daniel E., Fan case assembly and method.
  10. Bash,Gary; Strohl,J. Page, Fastened vane assembly.
  11. Ivakitch, Richard; Eleftheriou, Andreas; Carrieres, Alain, Fastening system for fan and shaft interconnection.
  12. Damgaard, Jocelyn C.; Roberts, Steven D.; Dale, Timothy, Flexible seal system for a gas turbine engine.
  13. Eastwood, Jonathan Jeffery; Low, Kevin Joseph, Gas turbine engine combustor surge retention.
  14. Samuelsson, Rickard; Reimers, Robert, Gas turbine engine component.
  15. Czachor,Robert Paul, Gas turbine engine frame having struts connected to rings with morse pins.
  16. Edward C. Rice ; Jack D. Petty, High temperature capable flange.
  17. Rainous Edward A. ; Barber Daniel J. ; Vickers Edward C. ; Maue Gregory P. ; Cody William E. ; Yee Sharon L. ; McMahan Kevin W., Inter-stage seal retainer and assembly.
  18. Drelon, Godefroy Francis Frederic; Pabion, Philippe Jean-Pierre; Prestel, Sebastien Jean Laurent; Soupizon, Jean-Luc, Joining device for joining two assemblies, for example for a stator of a turbomachine.
  19. Bertino, Gianluigi, Maintenance method of a gas turbine unit and gas turbine unit.
  20. Stilin, Nicholas D., Mechanical joint with a flanged retainer.
  21. Cant, Andrew; Twell, Philip, Mounting apparatus.
  22. North,David D., Multidirectionally compliant fastening system.
  23. Bergman, Russell J.; Yea, Stephen J.; Bach, Leonard A.; Bridges, Jr., Joseph W.; Willey, Lawrence J.; Spangler, Brandon W., Nozzle segment with reduced weight flange.
  24. Lepretre,Gilles; Monville,Bertrand, Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions.
  25. Illedits,Thomas; Holzl,Hubert, Self-locking bolted fastener.
  26. Bacon, Bruce Bennett; Rinehart, Michael Edwin; Boudreau, Thomas, Sleeved bolt assemblies for aircraft engine mount assemblies.
  27. Mohammed-Fakir, Abdul-Azeez; Aksit, Mahmut Faruk; Safi, Ahmad; Vedantam, Srikanth; Fang, Ning, Supplemental seal for the chordal hinge seals in a gas turbine.
  28. Mohammed-Fakir, Abdul-Azeez; Aksit, Mahmut Faruk; Safi, Ahmad; Vedantam, Srikanth; Fang, Ning, Supplemental seal for the chordal hinge seals in a gas turbine.
  29. Heyerman, Jeffrey Bernard; Olver, Bryan W., Support links with lockable adjustment feature.
  30. Milligan, Peter, System and method for limiting movement of a retainer ring of a gas turbine engine.
  31. Durocher, Eric; Lefebvre, Guy, Thermal expansion joint connection for sheet metal assembly.
  32. Tiemann,Peter, Turbine, fixing device for blades and working method for dismantling the blades of a turbine.
  33. Kouris Konstantino ; Leogrande John A, Turbomachinery module with improved maintainability.
  34. Stanka Rudolf,DEX, Vane elements adapted for assembly to form a vane ring of a gas turbine.
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