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Vortex generating flow passage design for increased film cooling effectiveness 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0580419 (1984-02-15)
발명자 / 주소
  • Papell S. Stephen (Berea OH)
출원인 / 주소
  • The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (Washington DC 06)
인용정보 피인용 횟수 : 51  인용 특허 : 1

초록

It is an object of the invention to provide a film cooling apparatus of increased effectiveness and efficiency. In accordance with the invention, a cooling fluid is injected into a hot flowing gas through a passageway in a wall which contains and is subject to the hot gas. The passageway is slanted

대표청구항

The apparatus of claim 9 wherein said pointed member extends at least half the height of said passageway.

이 특허에 인용된 특허 (1)

  1. Bratton Raymond J. (Delmont PA) Andersson Clarence A. (Pittsburgh PA), Method of manufacturing a transpiration cooled ceramic blade for a gas turbine.

이 특허를 인용한 특허 (51)

  1. Liang, George, Air seal unit adapted to be positioned adjacent blade structure in a gas turbine.
  2. Bunker, Ronald Scott; Lacy, Benjamin Paul, Articles which include chevron film cooling holes, and related processes.
  3. Sheaf, Christopher T. J.; Hussain, Zahid M., Boundary layer energiser.
  4. Sheaf, Christopher T. J.; Hussain, Zahid M., Boundary layer energiser.
  5. Vogt Robert L. (Marblehead MA), Breach-cooled structure.
  6. Sheaf, Christopher T J; Hussain, Zahid M, Breather duct shielding.
  7. Sheaf, Christopher T. J.; Hussain, Zahid M., Breather duct shielding.
  8. Lee,Ching Pang; Brassfield,Steven Robert; Bunker,Ronald Scott, Chevron film cooled wall.
  9. Auxier Thomas A. (Palm Beach Gardens FL) Stalker Kenneth W. (Fayetteville AR) Zimmerman Anthony M. (Palm Beach Gardens FL), Coolable thin metal sheet.
  10. Gleiner, Matthew S.; Kohli, Atul; Zelesky, Mark F., Cooling hole with asymmetric diffuser.
  11. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  12. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  13. Mongillo, Dominic; Gleiner, Matthew S, Cooling hole with curved metering section.
  14. Mongillo, Jr., Dominic J.; Gleiner, Matthew S., Cooling hole with curved metering section.
  15. Xu, JinQuan; Levasseur, Glenn, Cooling hole with enhanced flow attachment.
  16. Kohli, Atul; Gleiner, Matthew S.; Zelesky, Mark F.; Xu, JinQuan, Cooling hole with thermo-mechanical fatigue resistance.
  17. Kennedy Christopher A. (Palm Beach Gardens FL), Cooling means for augmentor liner.
  18. Ikeda Kazutaka,JPX ; Koga Akinori,JPX ; Ishii Junji,JPX, Cooling system for a main body used in a gas stream.
  19. Strock, Christopher W.; Lutjen, Paul M., Counter-vortex film cooling hole design.
  20. Tanaka, Ryozo; Kazari, Masahide; Sugimoto, Takao; Kusterer, Karsten; Bohn, Dieter; Elyas, Anas, Double-jet type film cooling structure.
  21. 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.
  22. Phillips James S. (Jupiter FL) Field Robert E. (Tequesta FL), Film coolant passage with swirl diffuser.
  23. Joshi, Narendra Digamber; Haynes, Joel Meier; Tangirala, Venkat Eswarlu; Vandervort, Christian Lee, Gas turbine engine and method of operating thereof.
  24. Dierberger, James A., Gas turbine engine component paired film cooling holes.
  25. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  26. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  27. Xu, JinQuan; Levasseur, Glenn, Gas turbine engine component with converging/diverging cooling passage.
  28. Xu, JinQuan, Gas turbine engine component with cusped cooling hole.
  29. Xu, JinQuan, Gas turbine engine component with diffusive cooling hole.
  30. Xu, JinQuan, Gas turbine engine component with impingement and diffusive cooling.
  31. Xu, JinQuan, Gas turbine engine component with impingement and lobed cooling hole.
  32. Gleiner, Matthew S.; Zelesky, Mark F.; Kohli, Atul, Gas turbine engine component with multi-lobed cooling hole.
  33. Ramachandran, Dhinagaran; Muthiah, Gopal Samy; Venkataramanan, Jyothishkumar; Srinivasan, Balamurugan; Liu, Jong; Tapia, Luis; Crites, Daniel Cregg; Malak, Malak Fouad, Gas turbine engine components with cooling hole trenches.
  34. Malak, Malak Fouad; Rana, Rajiv; Tapia, Luis; Chou, David; Liu, Jong, Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations.
  35. Venkataramanan, Jyothishkumar; Muthiah, Gopal Samy; Ramachandran, Dhinagaran; Srinivasan, Balamurugan; Malak, Malak Fouad; Liu, Jong; Tapia, Luis; Crites, Daniel, Gas turbine engine components with improved film cooling.
  36. Morris, Mark C.; Waldman, David; Malak, Malak Fouad; Tapia, Luis, Gas turbine engine components with lateral and forward sweep film cooling holes.
  37. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  38. Kvasnak, William S.; LaFleur, Ronald S.; Soechting, Friedrich O.; Joe, Christopher R.; Moroso, Joe; Hayes, Douglas A., Method and apparatus for cooling a wall within a gas turbine engine.
  39. LaFleur Ronald S., Method and apparatus for cooling a wall within a gas turbine engine.
  40. William S. Kvasnak ; Ronald S. LaFleur ; Friedrich O. Soechting ; Christopher R. Joe ; Joe Moroso ; Douglas A. Hayes, Method and apparatus for cooling a wall within a gas turbine engine.
  41. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  42. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  43. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  44. Xu, JinQuan, Multi-lobed cooling hole array.
  45. Xu, JinQuan, Multiple diffusing cooling hole.
  46. Kerrebrock Jack L., Radial flow turbine with internal evaporative blade cooling.
  47. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  48. Nita, Kozo; Okita, Yoji; Nakamata, Chiyuki; Yonekura, Kazuo; Kubo, Seiji; Watanabe, Osamu, Turbine blade.
  49. Ramachandran, Dhinagaran; Srinivasan, Balamurugan; Muthiah, Gopal; Venkataramanan, Jyothishkumar; Liu, Jong; Tapia, Luis; Malak, Malak Fouad, Turbine engine components.
  50. Jack L. Kerrebrock, Turbine or system with internal evaporative blade cooling.
  51. Ben-Amoz Meir (Lynn MA), Wall having cooling passage.
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