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Circumferentially grooved shroud liner 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-011/08
  • F01D-005/20
출원번호 US-0228889 (1981-01-27)
우선권정보 GB-0029653 (1977-07-14); GB-0040287 (1978-10-12)
발명자 / 주소
  • Okapuu lo (309 Place Valencay St. Lambert
  • Quebec CAX J4S 1S3) Patel Kiritkumar V. (4176 Trellis Crescent Mississauga
  • Ontari CAX L5L 2M2)
인용정보 피인용 횟수 : 59  인용 특허 : 2

초록

A turbine is provided with a stationary shroud surrounding a rotor provided with a plurality of radially extending blades. The stationary shroud includes a plurality of spaced-apart lands defining therebetween openings to deflect the flow leakage from the high pressure side of each blade to the low

대표청구항

A gas turbine engine having a rotor provided with a plurality of radially extending blades and a stationary shroud surrounding the rotor, each blade having a high pressure side and a low pressure side relative to the fluid flow and a substantially smooth tip end surface, the stationary shroud compri

이 특허에 인용된 특허 (2)

  1. Roberts ; Jr. Frank (Manchester CT), Blade tip shroud for a compression stage of a gas turbine engine.
  2. Adamson Arthur P. (Cincinnati OH) Sargisson Donald F. (Cincinnati OH) Stotler ; Jr. Charles L. (Fairfield OH), Integrated gas turbine engine-nacelle.

이 특허를 인용한 특허 (59)

  1. Le Biez, Philippe; Vigneau, Joël, Abradable coating for gas turbine walls.
  2. Childs, Dara W., Annular seals for non-contact sealing of fluids in turbomachinery.
  3. Gelmedov Fagim S.,RUX ; Lokshtanov Evgenij A.,RUX ; Olstain Lev Echielevich-Meerovich,RUX ; Sidorkin Michail A.,RUX, Anti-stall tip treatment means.
  4. Tudor, David J., Blade and rotor arrangement.
  5. Lutjen, Paul M.; Joe, Christopher R., Blade outer air seal formed of stacked panels.
  6. Liang, George, Blade tip shroud with circular grooves.
  7. Brunet, Antoine Robert Alain; Domercq, Olivier Stephane; Jablonski, Laurent; Perrot, Vincent Paul Gabriel, Casing for a moving-blade wheel of turbomachine.
  8. Barnett Mark ; Graf Martin ; Raw John A.,CAX ; Sharma Om ; Sprout William D., Casing treatment for a fluid compressor.
  9. Johann, Erik, Casing treatment for axial compressors in a hub area.
  10. Jactat, Paul-Etienne; Lebrusq, Pascal; Sarramea, Jerome; Scuiller, Lionel, Centrifugal compressor provided with a marker for measuring wear and a method of monitoring wear using said marker.
  11. Paul R. Adams, Compressor casing for a gas turbine engine.
  12. Schmuecker, Juergen, Compressor casing structure.
  13. Lauterbach Jerre F. (Columbus IN) Kahlenbeck James D. (Columbus IN) Turner Bruce W. (Columbus IN), Compressor range improvement means.
  14. McMillan, Alison J., Containment casing.
  15. Guemmer, Volker, Fluid flow machine.
  16. Guemmer, Volker, Fluid flow machine featuring a groove on a running gap of a blade end.
  17. Guemmer, Volker; Swoboda, Marius, Fluid flow machine featuring an annulus duct wall recess.
  18. Tholen, Susan; Luljen, Paul M., Gas turbine engine component having dual flow passage cooling chamber formed by single core.
  19. Lutjen, Paul M.; Tholen, Susan M, Gas turbine engines and related systems involving blade outer air seals.
  20. Lutjen, Paul M.; Tholen, Susan M., Gas turbine engines and related systems involving blade outer air seals.
  21. Maar, Karl; Hess, Thomas; Kufner, Petra, Housing section of a turbine engine compressor stage or turbine engine turbine stage.
  22. LeBlanc Andre Denis,CAX ; Ouellet Gilbert,CAX, Low aspect ratio compressor casing treatment.
  23. Bennington, Matthew A.; Connors, Kerrin E., Optimized circumferential groove casing treatment for axial compressors.
  24. Lee Ching-Pang, Ribbed turbine blade tip.
  25. Marini, Bonnie D.; Keller, Douglas A., Ring seal for a turbine engine.
  26. Yu, Hong, Rotor casing treatment with recessed baffles.
  27. Feulner, Matthew R., Rotor tip bleed in gas turbine engines.
  28. Allen, Jeffrey; Wright, Adrian; Grassby, Anthony; Lowe, Barry; O'Sullivan, Kevin; Carroll, Philip; Minion, Philip Gordon, Sealing element.
  29. Alvanos, Ioannis, Serrated outer surface for vortex initiation within the compressor stage of a gas turbine.
  30. Jeremy Clyde Bailey ; Ronald Scott Bunker, Shroud leakage flow discouragers.
  31. Duong, Hien; Kandasamy, Vijay, Shroud treatment for a centrifugal compressor.
  32. Tholen, Susan M.; Strock, Christopher W., Systems and methods involving abradable air seals.
  33. Kevin J. Farrell ; Walter S. Gearhart, Technique for reducing acoustic radiation in turbomachinery.
  34. Lee, Ching-Pang; Azad, Gm Salam; Gao, Zhihong; Hitchman, Neil; Martin, Jr., Nicholas F.; Sansom, David G.; Subramanian, Ramesh, Turbine abradable layer with asymmetric ridges or grooves.
  35. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam; Gao, Zhihong; Johnson, Erik; Schroeder, Eric; Martin, Jr., Nicholas F., Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern.
  36. Tham, Kok-Mun; Lee, Ching-Pang, Turbine abradable layer with inclined angle surface ridge or groove pattern.
  37. Lee, Ching-Pang; Tham, Kok-Mun; Laurello, Vincent P.; Azad, Gm Salam; Martin, Jr., Nicholas F., Turbine abradable layer with nested loop groove pattern.
  38. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam; Gao, Zhihong; Hitchman, Neil; Sansom, David G.; Allmon, Barrry L.; Shipper, Jr., Jonathan E.; Schillig, Cora; Merrill, Gary B.; Zois, Dimitrios; Subramanian, Ramesh, Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface.
  39. Lee, Ching-Pang; Tham, Kok-Mun, Turbine abradable layer with progressive wear zone multi depth grooves.
  40. Tham, Kok-Mun; Laurello, Vincent P.; Lee, Ching-Pang; Azad, Gm Salam; Martin, Jr., Nicholas F.; Sansom, David G.; Hitchman, Neil, Turbine abradable layer with progressive wear zone multi level ridge arrays.
  41. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam; Gao, Zhihong; Hitchman, Neil; Sansom, David G.; Allmon, Barrry L., Turbine abradable layer with progressive wear zone terraced ridges.
  42. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam, Turbine abradable layer with zig zag groove pattern.
  43. Subramanian, Ramesh; Hitchman, Neil; Zois, Dimitrios; Shipper, Jr., Jonathan E.; Schillig, Cora, Turbine component thermal barrier coating with crack isolating engineered groove features.
  44. Sech John R. ; Ellis Patrick H., Turbine engine rotor assembly blade outer air seal.
  45. Dextraze, Stephanie, Turbine hub with surface discontinuity and turbocharger incorporating the same.
  46. Lutjen, Paul M.; Wiedemer, John D.; Knapp, James N.; Mongillo, Jr., Dominic J.; Joe, Christopher R.; Luczak, Blake J.; Grogg, Gary L.; Benamati, Michael F., Turbine outer air seal.
  47. Tham, Kok-Mun; Lee, Ching-Pang, Turbine shroud with abradable layer having dimpled forward zone.
  48. Lee, Ching-Pang; Subramanian, Ramesh; Tham, Kok-Mun, Turbine shroud with abradable layer having ridges with holes.
  49. Bell Ralf,DEX, Turbine, in particular steam turbine, and turbine blade.
  50. Hough Geoffrey S. (Littleover GB2), Turbines.
  51. Irie Kouichi,JPX ; Okamura Tomoyoshi,JPX ; Manabe Akira,JPX ; Kurokawa Junichi,JPX, Turbo machines.
  52. Irie, Kouichi; Okamura, Tomoyoshi; Manabe, Akira; Kurokawa, Junichi, Turbo machines.
  53. Kouichi Irie JP; Tomoyoshi Okamura JP; Akira Manabe JP; Junichi Kurokawa JP, Turbo machines.
  54. Kurokawa, Junichi; Kimura, Hitoharu; Okamura, Tomoyshi; Nagahara, Takahide; Sudo, Sumio; Manabe, Akira; Kuwabara, Norimitsu, Turbo machines.
  55. Irie, Kouichi; Okamura, Tomoyoshi; Sudo, Sumio; Kurokawa, Junichi, Turbo-type machines.
  56. Dextraze, Stephanie; Grabowska, David G., Turbocharger shroud with cross-wise grooves and turbocharger incorporating the same.
  57. Guemmer, Volker, Turbomachine exerting dynamic influence on the flow.
  58. Streit, Josef Anton, Venturi effect endwall treatment.
  59. John, Joshy; Jain, Sanjeev Kumar; Rai, Sachin Kumar, Vortex chambers for clearance flow control.
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