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Fluted compressor flowpath 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01B-009/00
출원번호 US-0507408 (2000-02-18)
발명자 / 주소
  • Decker, John J.
  • Breeze-Stringfellow, Andrew
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Herkamp, Nathan D.Conte, Francis L.
인용정보 피인용 횟수 : 66  인용 특허 : 7

초록

A compressor flowpath includes circumferentially spaced apart airfoils having axially spaced apart leading and trailing edges and radially spaced apart outer and inner ends. An outer wall bridges the airfoil outer ends, and an inner wall bridges the inner ends. One of the walls includes a flute adja

대표청구항

A compressor flowpath includes circumferentially spaced apart airfoils having axially spaced apart leading and trailing edges and radially spaced apart outer and inner ends. An outer wall bridges the airfoil outer ends, and an inner wall bridges the inner ends. One of the walls includes a flute adja

이 특허에 인용된 특허 (7)

  1. Spear David A. (Manchester CT) Biederman Bruce P. (Meriden CT), Flow directing assembly for the compression section of a rotary machine.
  2. Wadia Aspi R. (Loveland OH) Szucs Peter N. (West Chester OH) Niskode Padmakar M. (Cincinnati OH) Battle Pamela A. (Forest Park OH), Forward swept rotor blade.
  3. Hoeger Martin,DEX ; Schmidt-Eisenlohr Uwe,DEX, Rotary turbomachine having a transonic compressor stage.
  4. Corcokios Nicholas (Palm Beach Gardens FL), Stator vane cluster.
  5. Spear David A. (Manchester CT) Biederman Bruce P. (Meriden CT) Orosa John A. (Palm Beach Gardens FL), Swept turbomachinery blade.
  6. Anderson Neal P. (Broad Brook CT) Giamei Anthony F. (Middletown CT) Salkeld Richard W. (South Windsor CT), Transverse directional solidification of metal single crystal articles.
  7. Matheny Alfred Paul ; Chou Chen Yu J., Turbine engine rotor blade pair.

이 특허를 인용한 특허 (66)

  1. Harvey, Neil William; Stokes, Mark Richard; Bagshaw, David Andrew, Aerofoil members for a turbomachine.
  2. Allen-Bradley, Eunice; Grover, Eric A.; Praisner, Thomas J.; Wagner, Joel H., Airfoil array with an endwall depression and components of the array.
  3. Allen-Bradley, Eunice; Grover, Eric A.; Praisner, Thomas J.; Wagner, Joel H., Airfoil array with an endwall protrusion and components of the array.
  4. Xu, JinQuan, Airfoil member and composite platform having contoured endwall.
  5. Lee, Ching-Pang; Tham, Kok-Mun; Schroeder, Eric; Meeroff, Jamie; Miller, Jr., Samuel R.; Marra, John J., Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling.
  6. Harvey,Neil W., Axial compressor blading.
  7. Pandey, Vidhu Shekhar; Clements, Jeffrey Donald; Lee, Ching-Pang, Banked platform turbine blade.
  8. Kuhne, Craig Miller; Bubnick, Joseph Steven; Kalb, Alisha Vachhani, Biformal platform turbine blade.
  9. Gier, Jochen; Guendogdu, Yavuz; Engel, Karl, Blade cascade and turbomachine.
  10. Allen-Bradley, Eunice; Grover, Eric A.; Praisner, Thomas J., Blade or vane with a laterally enlarged base.
  11. Pernleitner, Martin; Bichlmaier, Christian; Zscherp, Carsten, Blade ring segment having an annular space delimiting surface having a wavy height profile.
  12. Solomon, William J.; Wilkin, II, Daniel A.; Breeze-Stringfellow, Andrew; Hansell, Kevin S., Blade row for a rotary machine and method of fabricating same.
  13. Guimbard, Jean-Michel; Kueny, Olivier; Pintat, Ludovic, Blade with non-axisymmetric platform.
  14. Lee, Ching-Pang; Wang, Hsin-Pang; Upadhyay, Ram Kumar; Myers, Paul Richard; Edgar, Marc Thomas; Martyn, Thomas Donald; Estill, Eric Alan, Composite core die, methods of manufacture thereof and articles manufactured therefrom.
  15. Lee, Ching-Pang; Wang, Hsin-Pang; Upadhyay, Ram Kumar; Myers, Paul Richard; Edgar, Marc Thomas; Martyn, Thomas Donald; Estill, Eric Alan, Composite core die, methods of manufacture thereof and articles manufactured therefrom.
  16. Li, Yau-Wai; Anand, Karan; Townsend, Peter, Compressor stator with contoured endwall.
  17. Lee,Ching Pang; Tam,Anna; Kirtley,Kevin Richard; Lamson,Scott Henry, Crescentic ramp turbine stage.
  18. Pandey, Vidhu Shekhar; Lee, Ching-Pang; Schilling, Jan Christopher; Wadia, Aspi Rustom; Keith, Brian David; Clements, Jeffrey Donald, Curved platform turbine blade.
  19. Lee, Ching Pang; Wang, Hsin Pang; Upadhyay, Ram Kumar; Myers, Paul Richard; Edgar, Marc Thomas, Disposable insert, and use thereof in a method for manufacturing an airfoil.
  20. Wang,Hsin Pang; Edgar,Marc Thomas; Leman,John Thomas; Lee,Ching Pang; Estill,Eric Alan, Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom.
  21. Venugopal, Prem; Stein, Alexander; Otta, Shourya Prakash; Suresh, Ambady, End wall contour for an axial flow turbine stage.
  22. Praisner, Thomas J.; Aggarwala, Andrew S.; Grover, Eric A.; Jurek, Renee J., Endwall contouring.
  23. Grover, Eric A.; Praisner, Thomas J.; Modesto-Madera, Noel; Jurek, Renee J., Endwall with leading-edge hump.
  24. Turner, Matthew A.; Brown, Charles W.; Bugaj, Shari L.; Quinn, Christopher M.; Hyland, David J.; Alarcon, Andrew G., Fairing assembly.
  25. Thomas, Flavien L., Fan exit guide vane platform contouring.
  26. Lee,Ching Pang, Fillet energized turbine stage.
  27. Sakamoto, Yasuro; Ito, Eisaku; Wakazono, Susumu, Flow path structure and gas turbine exhaust diffuser.
  28. Guemmer, Volker, Fluid flow machine with sidewall boundary layer barrier.
  29. Johann, Erik, Fluid-flow machine.
  30. Lee,Ching Pang; Schilling,Jan Christopher; Wadia,Aspi Rustom, Funnel fillet turbine stage.
  31. Kawarada, Satoshi; Sonoda, Toyotaka, Gas turbine engine.
  32. Power, Bronwyn; Fulayter, Roy D.; Rivers, Jonathan M., Gas turbine engine flow path geometry.
  33. Salunkhe, Anil L.; Orosa, John A.; Shteyman, Yevgeniy; Han, Lijuan; Delisa, III, Matthew J.; Riveros, Daniel F., Industrial gas turbine exhaust system diffuser inlet lip.
  34. Orosa, John A.; Hinklein, Angelina, Industrial gas turbine exhaust system with area ruled exhaust path.
  35. Salunkhe, Anil L.; Orosa, John A.; Shteyman, Yevgeniy; Porter, Matthew R.; Han, Lijuan; Delisa, III, Matthew J.; Riveros, Daniel F., Industrial gas turbine exhaust system with modular struts and collars.
  36. Salunkhe, Anil L.; Orosa, John A.; Shteyman, Yevgeniy; Porter, Matthew R.; Han, Lijuan; Delisa, III, Matthew J., Industrial gas turbine exhaust system with splined profile tail cone.
  37. Decker,John Jared; Szucs,Peter Nicholas; Solomon,William Joseph; Wilson,Virginia Louise, Low solidity turbofan.
  38. Fulayter, Roy; Wellborn, Steve, Method and apparatus for enhancing compressor performance.
  39. Lee, Ching-Pang; Wang, Hsin-Pang; Bunker, Ronald Scott; Tewari, Sudhir Kumar; Azer, Magdi Naim, Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom.
  40. Siden, Gunnar L.; Bielek, Craig A.; Barr, Brian C.; Boyer, Bradley T.; Vandeputte, Thomas W.; Galie, Peter A., Methods and apparatus relating to improved turbine blade platform contours.
  41. Nguyen,Bao Q., Non-axisymmetric end wall contouring for a turbomachine blade row.
  42. Gillant, Gregory Nicolas Gerald; Dousseaud, Sylvain; Clemot, Stephane, Part to modify the profile of an aerodynamic jet.
  43. Xu, JinQuan, Platform with curved edges.
  44. Xu, JinQuan, Platform with curved edges adjacent suction side of airfoil.
  45. Johann, Erik; Heinichen, Frank, Rotor of an axial compressor stage of a turbomachine.
  46. Tam,Anna; Lee,Ching Pang; Kirtley,Kevin Richard; Bunker,Ronald Scott; Lamson,Scott Henry; Carson,Scott Michael, Scalloped surface turbine stage.
  47. Sonoda, Toyotaka; Hasenjaeger, Martina, Shape of gas passage in axial-flow gas turbine engine.
  48. Kray, Nicholas Joseph; Lamboy, Jorge Orlando, Spinner assembly with removable fan blade leading edge fairings.
  49. Johann, Erik; Heinichen, Frank, Stator of an axial compressor stage of a turbomachine.
  50. Wadia,Aspi Rustom; Szucs,Peter Nicholas; Farson,Max Robert; Wilson,Virginia Louise; Solomon,William Joseph, Tip cambered swept blade.
  51. Ceglio, Christopher Michael; Bauer, Randall Charles; Molter, Stephen Mark; Stegemiller, Mark Edward, Turbine airfoil with local wall thickness control.
  52. Iida, Koichiro, Turbine blade cascade end wall.
  53. Mariotti, Massimiliano; Bielek, Craig Allen; D'Ercole, Michele; Mei, Luciano, Turbine inlet guide vane with scalloped platform and related method.
  54. Clements, Jeffrey Donald; Pandey, Vidhu Skekhar; Lee, Ching-Pang, Turbine nozzle with contoured band.
  55. Smith, Paul Kendall; Siden, Gunnar Leif; Bielek, Craig Allen; Vandeputte, Thomas William, Turbine of a turbomachine.
  56. Stein, Alexander; Boyer, Bradley Taylor, Turbine of a turbomachine.
  57. Stein, Alexander; Brunt, Thomas James, Turbine of a turbomachine.
  58. Heitland,Gregory B.; Vogiatzis,Costas, Turbine rotor hub contour.
  59. Gallagher, Edward J.; Chuang, Sue-Li, Turbofan arrangement with blade channel variations.
  60. Barnes, Roland R.; Yilmaz, Cagdas, Turbofan flow path trenches.
  61. Aubin, Stephan; Belmonte, Olivier, Turbojet compressor.
  62. Stein, Alexander; Boyer, Bradley Taylor; Pierre, Sylvain, Turbomachine blade including a squeeler pocket.
  63. Hergt, Alexander; Meyer, Robert; Baier, Ralf-Dietmar, Turbomachine with axial compression or expansion.
  64. Lohaus, Andrew S.; Campbell, Christian Xavier; Miller, Jr., Samuel R.; Marra, John J., Vane array with one or more non-integral platforms.
  65. Aotsuka, Mizuho; Hamazaki, Hiroshi; Takahashi, Akira; Tanimitsu, Haruyuki, Wall configuration of axial-flow machine, and gas turbine engine.
  66. Mitsuhashi, Katsunori; Takahashi, Akira; Hamazaki, Hiroshi; Yamawaki, Ruriko, Wall of turbo machine and turbo machine.
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