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Mounting of integral platform turbine blades with skewed side entry roots 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/32
출원번호 US-0332187 (1989-04-03)
발명자 / 주소
  • Partington Albert J. (Winter Springs FL)
출원인 / 주소
  • Westinghouse Electric Corp. (Pittsburgh PA 02)
인용정보 피인용 횟수 : 43  인용 특허 : 3

초록

Method and apparatus for assembling integral platform blade groups to a rotor of a steam turbine in which the platform roots are skewed with respect to the axis of the turbine. The platform roots are formed to define a set of spaced grooves and steeples are formed on the rotor to mate with the platf

대표청구항

A system for attaching an integral platform blade group to a rotor of a steam turbine, the integral platform blade group comprising a plurality of blade foils connected into an integral group by a common platform, the system comprising: a plurality of spaced roots formed on the platform and oriented

이 특허에 인용된 특허 (3)

  1. Partington Albert J. (Media PA) Warner Ronald E. (Media PA), Method for assembling in a circular array turbine blades each with an integral shroud.
  2. Partington ; Albert J., Multiple side entry root for multiple blade group.
  3. Partington Albert J. (Media PA) Warner Ronald E. (Media PA), Turbine blade with integral shroud.

이 특허를 인용한 특허 (43)

  1. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  2. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  3. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Axial compressor for tip turbine engine.
  4. Caruso David Alan, Axial entry dovetail segment for securing a closure bucket to a turbine wheel and methods of installation.
  5. Nordeen, Craig A.; Suciu, Gabriel L., Balanced turbine rotor fan blade for a tip turbine engine.
  6. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Cantilevered tip turbine engine.
  7. Suciu, Gabriel L.; Nordeen, Craig A.; Kramer, Stephen, Combustor for turbine engine.
  8. Merry, Brian; Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Counter-rotating compressor case and assembly method for tip turbine engine.
  9. Suciu, Gabriel; Merry, Brian; McCune, Michael E., Counter-rotating gearbox for tip turbine engine.
  10. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Diffuser aspiration for a tip turbine engine.
  11. Suciu, Gabriel L.; Roberge, Gary D., Ejector cooling of outer case for tip turbine engine.
  12. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine.
  13. Nordeen, Craig A.; Norris, James W., Individual inlet guide vane control for tip turbine engine.
  14. Suciu, Gabriel L.; Portlock, Lawrence E.; Merry, Brian, Inflatable bleed valve for a turbine engine.
  15. Golinkin,Samuel; Lipski,Michael J.; Loudon,John S.; DiOrio,Gennaro J.; Ewer,Timothy, Locking arrangement for radial entry turbine blades.
  16. Wunderle, Helmar; Schlechtriem, Stefan; Graf, Peter; Glaser, Silvio; Von Arx, Beat, Method for improving the sealing on rotor arrangements.
  17. Suciu, Gabriel L.; Merry, Brian, Modular tip turbine engine.
  18. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Particle separator for tip turbine engine.
  19. Norris, James W.; Nordeen, Craig A., Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method.
  20. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Regenerative turbine blade and vane cooling for a tip turbine engine.
  21. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan rotor of a tip turbine engine.
  22. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan-turbine rotor of a tip turbine engine.
  23. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Stacked annular components for turbine engines.
  24. Merry, Brian; Webb, Scot Adams; McCune, Michael, Starter generator system for a tip turbine engine.
  25. Norris, James W.; Nordeen, Craig A., Tip turbine engine and operating method with reverse core airflow.
  26. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine composite tailcone.
  27. Suciu, Gabriel L.; Merry, Brian; Portlock, Lawrence, Tip turbine engine comprising a nonrotable compartment.
  28. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine blade clusters and method of assembly.
  29. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor.
  30. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine integral case, vane, mount and mixer.
  31. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Tip turbine engine integral fan, combustor, and turbine case.
  32. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine support structure.
  33. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine with a heat exchanger.
  34. Norris, James W.; Nordeen, Craig A.; Roberge, Gary, Tip turbine engine with multiple fan and turbine stages.
  35. Norris, James W.; Nordeen, Craig A., Tip turbine engine with reverse core airflow.
  36. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine single plane mount.
  37. Roberge, Gary D., Turbine blow down starter for turbine engine.
  38. Suciu, Gabriel L.; Pagluica, Gino J.; Duong, Loc Quang; Portlock, Lawrence E., Turbine engine with differential gear driven fan and compressor.
  39. Hogberg, Nicholas Alvin; Garcia-Crespo, Andres Jose, Turbine system and adapter.
  40. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly for gas turbine engine.
  41. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  42. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  43. Roberge, Gary D., Vectoring transition duct for turbine engine.
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