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Film cooling passages with curved corners 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0812104 (1985-12-23)
발명자 / 주소
  • Field Robert E. (Tequesta FL)
출원인 / 주소
  • United Technologies Corporation (Hartford CT 02)
인용정보 피인용 횟수 : 72  인용 특허 : 12

초록

A film cooling passage through the external wall of a hollow airfoil for a gas turbine engine has a metering section in series flow relation with a diffusing section leading to the passage outlet at the external surface of the airfoil over which a hot gas flows during operation. The diffusing sectio

대표청구항

A cooled wall having an outer surface adapted to be exposed to a hot gas stream flowing in a downstream direction over said outer surface, and an inner surface adapted to define a portion of a coolant compartment for receiving coolant therein under pressure, a coolant passage within said wall, said

이 특허에 인용된 특허 (12)

  1. Dodd Alec G. (Belper GB2), Blade or vane for a gas turbine engine.
  2. Kenworthy Milton J. (Cincinnati OH), Combustor liner.
  3. Stamm Edward I. (Cincinnati OH), Combustor liner structure.
  4. Parkes Roger J. (Stanton-by-Bridge GB2), Cooled blade for a gas turbine engine.
  5. Hartmann Max (Baden CHX) Thuringer Ferdinand (Wettingen CHX), Cooling-air nozzle for use in a heated chamber.
  6. Graham, Robert W.; Papell, S. Stephen, Curved film cooling admission tube.
  7. Braddy Bruce T. (Boxford MA), Film cooled airfoil body.
  8. Rice Ivan G. (P.O. Box 233 Spring TX 77373), Integrated gas/steam nozzle.
  9. Sidenstick James E. (Cincinnati OH), Method and apparatus for forming diffused cooling holes in an airfoil.
  10. Tamura Raymond M. (218 Lagoon Dr. Honolulu HI 96819), Pollution reducing aircraft propulsion.
  11. Rice Ivan G. (P.O. Box 233 Spring TX 77373), Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine.
  12. Andersen Richard H. (Cincinnati OH), Tip cooling for turbine blades.

이 특허를 인용한 특허 (72)

  1. Beabout Brian K. (Coventry CT), Airfoil having expanded wall portions to accommodate film cooling holes.
  2. Liang, George, Airfoil tip squealer cooling construction.
  3. Lang ; III William F. ; Auxier Thomas Alvin, Airfoils with leading edge pockets for reduced heat transfer.
  4. Pietraszkiewicz, Edward F.; Klinefelter, Kevin J.; Kohli, Atul; Coons, Todd R., Article having diffuser holes and method of making same.
  5. Lee,Ching Pang, Bell-shaped fan cooling holes for turbine airfoil.
  6. Lee,Ching Pang; Wadia,Aspi Rustom; Brauer,John Christopher, Blunt tip turbine blade.
  7. Liang, George, Combustion turbine with airfoil having multi-section diffusion cooling holes and methods of making same.
  8. Forrester,Ronald E.; Kimberlin,Dwight Evans; Lang,Gregory J., Complex hole shaping.
  9. Bunker, Ronald Scott, Components with conformal curved film holes and methods of manufacture.
  10. Pope, J. Edward; Rhodes, Jeffery Forest; Snyder, Douglas J., Cooled gas turbine engine component.
  11. Nakamata, Chiyuki; Okita, Yoji, Cooled turbine component and cooled turbine blade.
  12. Moore, Sasha M.; Jennings, Timothy J.; Slavens, Thomas N.; Musto, Clifford J.; LoRicco, Nicholas M.; Clum, Carey; McBrien, John; Whitfield, Christopher; Quach, San, Cooling for gas turbine engine components.
  13. Xu, JinQuan, Cooling hole for a gas turbine engine component.
  14. Gleiner, Matthew S.; Kohli, Atul; Zelesky, Mark F., Cooling hole with asymmetric diffuser.
  15. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  16. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  17. Mongillo, Dominic; Gleiner, Matthew S, Cooling hole with curved metering section.
  18. Mongillo, Jr., Dominic J.; Gleiner, Matthew S., Cooling hole with curved metering section.
  19. Xu, JinQuan; Levasseur, Glenn, Cooling hole with enhanced flow attachment.
  20. Kohli, Atul; Gleiner, Matthew S.; Zelesky, Mark F.; Xu, JinQuan, Cooling hole with thermo-mechanical fatigue resistance.
  21. Lu, Wenfeng; Castle, Russel Michael, Counterbalanced flow turbine nozzle.
  22. 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.
  23. Johnson, Thomas Edward; Keener, Christopher Paul; Ostebee, Heath Michael; Wegerif, Daniel Gerritt, Effusion plate using additive manufacturing methods.
  24. Cross Jack A. (Cincinnati OH) Jackson Cletis M. (West Chester OH), Electro-discharge machining electrode.
  25. Liang, George, Electrode for shaped film cooling hole.
  26. Stroud David (Bristol GB2) Corfe Arthur G. (Bristol GB2) Towill Jonathan P. W. (Cardiff GB2) Cooper Brian G. (Derby GB2), Film cooled components.
  27. Liang, George, Film cooling hole for a turbine airfoil.
  28. Liang, George, Film cooling hole for turbine airfoil.
  29. Liang, George, Film cooling hole for turbine airfoil.
  30. Musto, Clifford J.; LoRicco, Nicholas M.; Slavens, Thomas N.; Jennings, Timothy J.; Clum, Carey; Moore, Sasha M.; McBrien, John; Quach, San; Whitfield, Christopher, Film hole with protruding flow accumulator.
  31. Liang,George, Gas turbine airfoil leading edge cooling construction.
  32. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  33. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  34. Xu, JinQuan; Levasseur, Glenn, Gas turbine engine component with converging/diverging cooling passage.
  35. Xu, JinQuan, Gas turbine engine component with cusped cooling hole.
  36. Xu, JinQuan, Gas turbine engine component with diffusive cooling hole.
  37. Musto, Clifford J.; Moore, Sasha M.; Slavens, Thomas N.; Quach, San; LoRicco, Nicholas M.; Jennings, Timothy J.; McBrien, John, Gas turbine engine component with film cooling hole with accumulator.
  38. Xu, JinQuan, Gas turbine engine component with impingement and diffusive cooling.
  39. Xu, JinQuan, Gas turbine engine component with impingement and lobed cooling hole.
  40. Gleiner, Matthew S.; Zelesky, Mark F.; Kohli, Atul, Gas turbine engine component with multi-lobed cooling hole.
  41. 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.
  42. Morris, Mark C.; Waldman, David; Malak, Malak Fouad; Tapia, Luis, Gas turbine engine components with lateral and forward sweep film cooling holes.
  43. Thompson Robert Alan, High aspect ratio EDM electrode assembly.
  44. Killion Douglas P. ; Lodin David W., Intravascular dilation catheter.
  45. Liang, George, Laser shaped film cooling hole.
  46. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  47. Bunker Ronald Scott ; Bailey Jeremy Clyde ; Lee Ching-Pang ; Abuaf Nesim, Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture.
  48. Gannelli, Jesse; Gayman, Scott W.; Pietraszkiewicz, Edward F.; Jelks, Christopher B.; Pinero, Sandra S.; Rembish, Paul Thomas; Levy, Ryan Shepard, Method of creating an airfoil trench and a plurality of cooling holes within the trench.
  49. Shih, Tom I-P; Na, Sangkwon, Momentum preserving film-cooling shaped holes.
  50. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  51. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  52. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  53. Xu, JinQuan, Multi-lobed cooling hole array.
  54. Lee,Ching Pang, Multiform film cooling holes.
  55. Xu, JinQuan, Multiple diffusing cooling hole.
  56. Liang, George, Multiple expansion film cooling hole for turbine airfoil.
  57. Fahndrich, Marc, Percussion drilled shaped through hole and method of forming.
  58. Liang, George, Shaped film cooling hole for turbine airfoil.
  59. Lee,Ching Pang; Palmer,Nicholas Charles; Kirkeng,Kevin Lee, Skewed tip hole turbine blade.
  60. Kercher David M., Spanwise fan diffusion hole airfoil.
  61. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  62. Liang, George, Turbine airfoil cooling system with curved diffusion film cooling hole.
  63. Liang, George, Turbine airfoil cooling system with diffusion film cooling hole.
  64. Liang, George, Turbine airfoil cooling system with diffusion film cooling hole having flow restriction rib.
  65. Liang,George, Turbine airfoil cooling system with elbowed, diffusion film cooling hole.
  66. Bergholz, Jr., Robert Frederick; Durstock, Daniel Lee, Turbine airfoil trailing edge cooling slots.
  67. Liang, George, Turbine airfoil with continuous curved diffusion film holes.
  68. Liang, George, Turbine airfoil with enhanced cooling.
  69. Liang, George, Turbine airfoil with film cooling hole.
  70. Kercher David Max (Ipswich MA), Turbine blade having transpiration strip cooling and method of manufacture.
  71. Liang, George, Turbine blade with film cooling slot.
  72. Ben-Amoz Meir (Lynn MA), Wall having cooling passage.
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