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Film cooled wall 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
  • F02G-003/00
출원번호 US-0012493 (1993-01-25)
발명자 / 주소
  • Lee Ching-Pang (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 66  인용 특허 : 0

초록

A wall adapted for use in a gas turbine engine between a first and a hotter second fluid includes a first side over which is flowable the first fluid, and an opposite second side over which is flowable the second fluid. An elongate notch includes a forward surface extending inwardly from the second

대표청구항

A wall adaptable for use in a gas turbine engine between a first fluid and a second fluid being hotter than said first fluid, comprising: a first side over which is flowable said first fluid: an opposite second side spaced from said first side along a transverse axis and over which is flowable said

이 특허를 인용한 특허 (66)

  1. Roy, Subrata, Active film cooling for turbine blades.
  2. Spangler, Brandon W.; Bergman, Russell J., Airfoil cooling arrangement.
  3. Piggush, Justin D.; Kohli, Atul, Airfoil including trench with contoured surface.
  4. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Airfoil leading edge end wall vortex reducing plasma.
  5. Tabbita Martin G. ; Downs James P. ; Soechting Friedrich O. ; Auxier Thomas A., Apparatus and method for cooling an airfoil for a gas turbine engine.
  6. Guemmer, Volker, Blade with tangential jet generation on the profile.
  7. Jopp, Lisa Jane; Willis, Nathan Thomas, Combustion chamber arrangement.
  8. Kopmels,Michiel, Component having a film cooling arrangement.
  9. Bunker, Ronald Scott, Components with conformal curved film holes and methods of manufacture.
  10. Lee,Ching Pang; Bunker,Ronald Scott; Prakash,Chander, Converging pin cooled airfoil.
  11. LaFleur Ronald Samuel, Coolable airfoil for a gas turbine engine.
  12. Lock Gary D,GBX ; Oldfield Martin L G,GBX, Coolant passages for gas turbine components.
  13. Rhodes Jeffrey F., Cooled airfoil.
  14. Abdel-Messeh, William; Blair, Michael F.; Kohli, Atul; Piggush, Justin D., Cooled airfoils and gas turbine engine systems involving such airfoils.
  15. Ewald Lutum CH; Klaus Semmler DE; Jens Wolfersdorf CH, Cooled blade for a gas turbine.
  16. Vandervaart, Peter C.; Rhodes, Jeffrey F.; Kwon, Okey; Heffernan, Tab M., Cooled gas turbine engine component.
  17. Ohtomo Fumio (Zama JPX) Fukuyama Yoshitaka (Yokohama JPX) Nakata Yuji (Yokohama JPX) Inomata Asako (Yokohama JPX) Matsuda Hisashi (Yokohama JPX) Ito Shoko (Yokohama JPX), Cooled turbine blade for a gas turbine.
  18. Gleiner, Matthew S.; Kohli, Atul; Zelesky, Mark F., Cooling hole with asymmetric diffuser.
  19. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  20. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  21. Mongillo, Dominic; Gleiner, Matthew S, Cooling hole with curved metering section.
  22. Mongillo, Jr., Dominic J.; Gleiner, Matthew S., Cooling hole with curved metering section.
  23. Xu, JinQuan; Levasseur, Glenn, Cooling hole with enhanced flow attachment.
  24. Kohli, Atul; Gleiner, Matthew S.; Zelesky, Mark F.; Xu, JinQuan, Cooling hole with thermo-mechanical fatigue resistance.
  25. Ikeda Kazutaka,JPX ; Koga Akinori,JPX ; Ishii Junji,JPX, Cooling system for a main body used in a gas stream.
  26. Pfitzner, Michael; Kroess, Bernhard; Schreivogel, Peter, Device for cooling a wall of a component.
  27. Tanaka, Ryozo; Kazari, Masahide; Sugimoto, Takao; Kusterer, Karsten; Bohn, Dieter; Elyas, Anas, Double-jet type film cooling structure.
  28. Lee, Ching-Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je-Chin, Downstream plasma shielded film cooling.
  29. Levasseur, Glenn; Pietraszkiewicz, Edward F.; Zelesky, Mark F.; Mongillo, Jr., Dominic J.; Klinefelter, Kevin J.; Doll, Stephen D.; Fritch, Markus W., EDM method for multi-lobed cooling hole.
  30. Barry, Vincent Anthony; Demarche, Thomas Edward, Failsafe film cooled wall.
  31. Kohli, Atul; Wagner, Joel H.; Aggarwala, Andrew S., Film cooled article with improved temperature tolerance.
  32. Yufeng Phillip Yu ; Gary Michael Itzel ; Sarah Jane Osgood ; Radhakrishna Bagepalli ; Waylon Willard Webbon ; Steven Sebastian Burdgick, Film cooling air pocket in a closed loop cooled airfoil.
  33. Xu, JinQuan, Film cooling channel array having anti-vortex properties.
  34. Xu, JinQuan; Levasseur, Glenn, Film cooling channel array with multiple metering portions.
  35. Johnson, Jamie Jay, Film cooling holes for gas turbine airfoils.
  36. Guemmer, Volker, Fluid flow machine with peripheral energization near the suction side.
  37. Cheung,Albert K.; Napoli,Nikolaos; Segalman,Irving, Gas turbine combustor heat shield panel or exhaust panel including a cooling device.
  38. Vandervaart, Peter C.; Rhodes, Jeffrey F.; Kwon, Okey; Heffernan, Tab M.; Barker, Brett J., Gas turbine engine component arrangement.
  39. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  40. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  41. Xu, JinQuan; Levasseur, Glenn, Gas turbine engine component with converging/diverging cooling passage.
  42. Xu, JinQuan, Gas turbine engine component with cusped cooling hole.
  43. Xu, JinQuan, Gas turbine engine component with diffusive cooling hole.
  44. Xu, JinQuan, Gas turbine engine component with impingement and diffusive cooling.
  45. Xu, JinQuan, Gas turbine engine component with impingement and lobed cooling hole.
  46. Gleiner, Matthew S.; Zelesky, Mark F.; Kohli, Atul, Gas turbine engine component with multi-lobed cooling hole.
  47. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  48. Auxier Thomas A. ; Downs James P. ; Kvasnak William S. ; Soechting Friedrich O. ; Calhoun William H. ; Hayes Douglas A., Method and apparatus for cooling an airfoil.
  49. Soechting Friedrich O. ; Kvasnak William A. ; Auxier Thomas A. ; Downs James P. ; Calhoun William H. ; Hayes Douglas A., Method and apparatus for cooling an airfoil.
  50. Shih, Tom I-P; Na, Sangkwon, Momentum preserving film-cooling shaped holes.
  51. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  52. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  53. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  54. Xu, JinQuan, Multi-lobed cooling hole array.
  55. Xu, JinQuan, Multiple diffusing cooling hole.
  56. Arness,Brian Peter; Sherlock,Graham David; Moroso,Joseph Leonard; Beitz,Stewart William; Peters,Graydon Wayne, Repaired turbine nozzle.
  57. Chan, George Joe-Kueng; Bunker, Ronald Scott; Correia, Victor Hugo Silva; Hoffman, Christopher Kanoa, Trench cooling of airfoil structures.
  58. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  59. Fujimoto, Shu, Turbine blade and engine component.
  60. Bradshaw, Sean D., Turbine blade having film cooling hole arrangement.
  61. Spangler, Brandon W., Turbine blade with reverse cooling air film hole direction.
  62. Miranda, Carlos Miguel; Trimmer, Andrew Lee; Kottilingam, Srikanth Chandrudu; Lacy, Benjamin Paul, Turbine component having surface cooling channels and method of forming same.
  63. Laurello, Vincent P.; Lee, Ching-Pang, Turbine rotor disk inlet orifice for a turbine engine.
  64. Liang, George, Turbine vane endwall with cascading film cooling diffusion slots.
  65. Liang, George, Turbine vane with endwall film cooling.
  66. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Upstream plasma shielded film cooling.
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