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Method and apparatus for cooling a wall within a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0412950 (1999-10-05)
발명자 / 주소
  • William S. Kvasnak
  • Ronald S. LaFleur
  • Friedrich O. Soechting
  • Christopher R. Joe
  • Joe Moroso
  • Douglas A. Hayes
출원인 / 주소
  • United Technologies Corporation
인용정보 피인용 횟수 : 91  인용 특허 : 35

초록

A cooling circuit is provided disposed between a first wall portion and a second wall portion of a wall for use in a gas turbine engine, one or more inlet apertures, and one or more exit apertures. The inlet aperture(s) provides a cooling airflow path into the cooling circuit and the exit aperture(s

대표청구항

1. A cooling circuit disposed between a first wall portion and a second wall portion of a wall for use in a gas turbine engine, comprising:a plurality of first pedestals extending between said first wall portion and said second wall portion, and arranged in rows, and wherein adjacent said first pede

이 특허에 인용된 특허 (35)

  1. Meginnis George B. (Indianapolis IN) Sodeberg Earl W. (Indianapolis IN), Airfoil fabrication.
  2. Liang George P. (Jupiter FL), Airfoil pedestaled trailing edge region cooling configuration.
  3. Hill Edward C. (Tequesta FL) Liang George P. (Palm City FL) Auxier Thomas (Lake Park FL), Airfoil trailing edge cooling arrangement.
  4. Green Dennis J. (Amston CT) Yamarik George J. (Vernon CT), Coolable airfoil structure.
  5. Clifford Rodney J. (Gloucestershire GB2) Charters Ian J. (Bristol GB2), Cooled turbine blade.
  6. Horvath Richard L. (Hamilton OH) Harris Robert W. (Fairfield OH), Cooled turbine blade tip closure.
  7. Stahl ; William F., Cooled turbine vane.
  8. Auxier Thomas A. (Palm Beach Gardens FL) Przirembel Hans R. (Jupiter FL) Soechting Friedrich O. (Tequesta FL), Cooled vane.
  9. Przirembel Hans R. (Jupiter FL) Meyer Robert C. (Palm Beach Gardens FL), Cooled vane.
  10. North William E. (Concord Township ; Delaware County PA) Holden Paul C. (Newtown PA) Hultgren Kent G. (Swarthmore PA), Cooling arrangement for airfoil stator vane trailing edge.
  11. Chen Yu-Lin (Indianapolis IN), Diffusion bonding method.
  12. Jackson Melvin Robert ; Skelly David William ; Rowe Raymond Grant ; LaChapelle Donald George ; Wilson Paul Stuart, Double wall turbine parts.
  13. Phillips James S. (Jupiter FL) Field Robert E. (Tequesta FL), Film coolant passage with swirl diffuser.
  14. Lee Ching-Pang (Cincinnati OH), Film cooling of turbine airfoil wall using mesh cooling hole arrangement.
  15. Hauser Ambrose A. (Wyoming OH), Fluid-cooled element.
  16. Franklin Clifford John (Winterthur CH), Gas turbine guide vane.
  17. Corsmeier Robert J. (Cincinnati OH) Koff Bernard L. (Cincinnati OH), Impingement baffle collars.
  18. Cunha Francisco J. (Schenectady NY), Integrated steam/air cooling system for gas turbines.
  19. Okpara Nnawuihe A. (Peoria AZ) Henry Chester L. (Tempe AZ) Bischoff Michael K. (Mesa AZ), Internally cooled gas turbine vane.
  20. Memmen, Robert L., Internally cooled hollow airfoil.
  21. Linask Indrik (Tolland CT), Internally cooled turbine airfoil.
  22. Corrigan Charles E. (Tempe AZ), Laminated airfoil and method for turbomachinery.
  23. Gupta Bhupendra K. ; Ziegler Robert P. ; Scheidt Wilbur D., Method for making a fluid cooled article with protective coating.
  24. Ritter Ann Melinda ; Hughes John Raymond ; Jackson Melvin Robert ; Kirkpatrick Francis Lawrence ; Cunha Francisco Jose Tenreiro ; Abuaf Nesim ; Bunker Ronald Scott, Method for making cylindrical structures with cooling channels.
  25. Darrow Kenneth A. (Sprakers NY) Pagnotta Gasper (Rexford NY), Method of manufacture of cooled turbine or compressor buckets.
  26. Havercroft Peter (Derby GB2), Porous sheet structure for a combustion chamber.
  27. Hess W. Graig (Lake Park FL), Radial wafer airfoil construction.
  28. Sylvestro Joseph A. (New Britain CT) Linask Indrik (Tolland CT) Beabout Brian K. (Coventry CT), Turbine airfoil including diffusing trailing edge pedestals.
  29. Isburgh Anne M. (Loveland OH) Lee Ching-Pang (Cincinnati OH), Turbine airfoil with convectively cooled double shell outer wall.
  30. Starkweather John H., Turbine blade.
  31. Kercher David Max (Ipswich MA), Turbine blade having auxiliary turbulators.
  32. Bailly Yves Maurice,FRX ; Coudray Xavier Gerard Andre,FRX ; Derrien Mischael Francois Louis,FRX ; Fougeres jean-Michel Roger,FRX ; Pellier Philippe Christian,FRX ; Taillant Jean-Claude Christian,FRX , Turbine vane cooling system.
  33. Magowan John W. (Longmeadow MA) Pawlaczyk Richard J. (Newington CT) Pighetti Annette M. (Andover CT) Schwarz ; Jr. Richard A. (Somers CT), Turbine vane having dedicated inner platform cooling.
  34. Calderbank John C. (Glastonbury CT), Turbine vane with a platform cavity having a double feed for cooling fluid.
  35. Papell S. Stephen (Berea OH), Vortex generating flow passage design for increased film cooling effectiveness.

이 특허를 인용한 특허 (91)

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  2. Lee, Ching-Pang; Marra, John J., Airfoil incorporating tapered cooling structures defining cooling passageways.
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  5. Liang, George, Blade for a gas turbine.
  6. Mongillo, Jr., Dominic J.; Levine, Jeffrey R.; Lana, Kyle C.; Moore, Sasha M., Blade tip cooling arrangement.
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  8. Lee, Ching-Pang; Heneveld, Benjamin E., Casting core for a cooling arrangement for a gas turbine component.
  9. Cherolis, Anthony P.; Letizia, Eric P.; Devore, Matthew A., Castings, casting cores, and methods.
  10. Lofy, John, Climate controlled seating assembly with sensors.
  11. Widrig, Scott M.; Rudolph, Ronald J.; Wagner, Gregg P., Closed loop steam cooled airfoil.
  12. Lofy, John, Condensation and humidity sensors for thermoelectric devices.
  13. Lofy, John D., Condensation and humidity sensors for thermoelectric devices.
  14. Lee,Ching Pang; Bunker,Ronald Scott; Prakash,Chander, Converging pin cooled airfoil.
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  19. Gregg, Shawn J.; Mongillo, Jr., Dominic J., Cooled rotor blade with vibration damping device.
  20. Gregg,Shawn J., Cooled rotor blade with vibration damping device.
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  22. Lee, Ching-Pang; Heneveld, Benjamin, Cooling configuration for a gas turbine engine airfoil.
  23. Xu, Jinquan, Cooling having tailored flow resistance.
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  26. Morgan, Victor John; Gergely, George Andrew; Roberts, Jr., Frederic Woodrow; Smith, Aaron Ezekiel, Cooling structure for hot-gas path components with methods of fabrication.
  27. Spangler, Brandon W.; Abdel-Messeh, William, Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals.
  28. Lee, Ching-Pang, Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways.
  29. Liang,George, Cooling system including mini channels within a turbine blade of a turbine engine.
  30. Lee, Ching-Pang; Matthews, Ralph W.; Azad, Gm Salam; Shivanand, Manjit, Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly.
  31. Cunha, Frank J., Distributed cooling for gas turbine engine combustor.
  32. Brykalski, Michael J.; Terech, John; Petrovski, Dusko, Environmentally-conditioned bed.
  33. Brykalski, Michael J.; Terech, John; Petrovski, Dusko, Environmentally-conditioned bed.
  34. Draper,Samuel David; Blair,Michael; Alahyari,Abbas, Film cooling for microcircuits.
  35. Lutjen, Paul M., Gas turbine engine airfoil cooling passage turbulator pedestal.
  36. Vandervaart, Peter C.; Rhodes, Jeffrey F.; Kwon, Okey; Heffernan, Tab M.; Barker, Brett J., Gas turbine engine component arrangement.
  37. Morris, Mark C.; Kettinger, Jon; Yang, Yong-Qing; Crites, Daniel Cregg, Gas turbine engines with improved trailing edge cooling arrangements.
  38. Liang,George, Gas turbine vane with integral cooling system.
  39. Joe, Christopher R.; Lutjen, Paul M., Heat transfer augmentation in a compact heat exchanger pedestal array.
  40. Joe, Christopher R.; Lutjen, Paul M., Heat transfer augmentation in a compact heat exchanger pedestal array.
  41. Petrovski, Dusko, Heating and cooling systems for seating assemblies.
  42. Snyder, James G., High performance fire-retardant kraft facing for fiberglass insulation.
  43. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and dimpled cooling.
  44. Bunker,Ronald Scott; Lee,Ching Pang, Hot gas path component with mesh and impingement cooling.
  45. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and turbulated cooling.
  46. Spangler, Brandon W.; Mongillo, Jr., Dominic J.; Blair, Michael F., Impingement skin core cooling for gas turbine engine blade.
  47. Lee, Ching-Pang; Haubert, Richard Clay; Maclin, Harvey Michael, Integrated bridge turbine blade.
  48. Weaver, Adam M., Interwoven channels for internal cooling of airfoil.
  49. Lofy, John; Walsh, Ryan, Low-profile blowers and methods.
  50. Lee, Ching-Pang; Zuniga, Humberto A.; Morrison, Jay A., Mesh cooled conduit for conveying combustion gases.
  51. Cunha, Frank J.; Palumbo, Michael A., Method and apparatus for cooling an airfoil.
  52. Petrovski, Dusko; Zheng, Sihai; Maass, Michael, Method and system for controlling an operation of a thermoelectric device.
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  57. Cunha, Frank; Dube, Bryan, Microcircuit cooling for a turbine blade tip.
  58. Brykalski, Michael; Marquette, David, Moisture abatement in heating operation of climate controlled systems.
  59. Arthurs,Trevor; Lee,Joel, Multi-layered flame retardant wrap.
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  79. Liang,George, Turbine airfoil with integral cooling system.
  80. Liang, George, Turbine airfoil with near-wall spiral flow cooling circuit.
  81. Smith, Aaron Ezekiel; Foster, Gregory Thomas; Iduate, Michelle Jessica; Leary, Brendon James; Weber, David Wayne, Turbine airfoil with trailing edge cooling circuit.
  82. Weber, David Wayne; Foster, Gregory Thomas; Iduate, Michelle Jessica; Leary, Brendon James; Smith, Aaron Ezekiel, Turbine airfoil with trailing edge cooling circuit.
  83. Krumanaker, Matthew Lee; Dooley, Weston Nolan; Brassfield, Steven Robert; Helmer, David Benjamin; Bailey, Jeremy Clyde; Briggs, Robert David, Turbine blade.
  84. Liang, George, Turbine blade having a vortex forming cooling system for a trailing edge.
  85. Devore, Matthew A.; Luczak, Blake J., Turbine component with axially spaced radially flowing microcircuit cooling channels.
  86. Cunha,Frank J.; Dahmer,Matthew T., Turbine element.
  87. Lee, Ching-Pang, Turbine engine component wall having branched cooling passages.
  88. Schilp, Reinhard, Turbine vane for a gas turbine engine.
  89. Moore, Robert P.; Seleski, Richard; Cox, Dale Lee, Vane enhanced trailing edge cooling design.
  90. Chon, Young H., Vane with enhanced heat transfer.
  91. Steinman, Adam Joseph; Bunyak, Kenneth James; Orlando, Bruno Antonio, Vehicle headliner assembly for zonal comfort.
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