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Film coolant passage with swirl diffuser 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0812102 (1985-12-23)
발명자 / 주소
  • Phillips James S. (Jupiter FL) Field Robert E. (Tequesta FL)
출원인 / 주소
  • United Technologies Corporation (Hartford CT 02)
인용정보 피인용 횟수 : 36  인용 특허 : 17

초록

The wall of a hollow turbine airfoil has a longitudinally extending coolant outlet slot in its external surface which intersects, along its length, a longitudinally extending cylindrical channel within the wall. Metering passages extend from the inside surface of the airfoil wall to the cylindrical

대표청구항

A hollow, longitudinally extending airfoil including a cooled wall having an outer surface defining a pressure and suction surface of said airfoil, said pressure and suction surfaces adapted to have a hot gas stream flowing thereover in a downstream direction substantially perpendicular to said long

이 특허에 인용된 특허 (17)

  1. Groess Helmut (Esterhofen DEX) Graeml ; deceased Horst (late of Markt Indersdorf DEX by Edith Graeml ; administrator), Axial-flow turbine blade, especially axial-flow turbine rotor blade for gas turbine engines.
  2. Dodd Alec G. (Belper GB2), Blade or vane for a gas turbine engine.
  3. Dierberger, James A., Combustion liner cooling scheme.
  4. Koshoffer John M. (Cincinnati OH) Ekstedt Edward E. (Montgomery OH) Stamm Edward I. (Cincinnati OH), Combustor liner slot with cooled props.
  5. Stamm Edward I. (Cincinnati OH), Combustor liner structure.
  6. Parkes Roger J. (Stanton-by-Bridge GB2), Cooled blade for a gas turbine engine.
  7. DuBell Thomas L. (Maineville OH) Campbell Thomas C. (Cincinnati OH) Thompson James L. (Cincinnati OH), Cooling ring construction for combustion chambers.
  8. Hartmann Max (Baden CHX) Thuringer Ferdinand (Wettingen CHX), Cooling-air nozzle for use in a heated chamber.
  9. Graham, Robert W.; Papell, S. Stephen, Curved film cooling admission tube.
  10. Braddy Bruce T. (Boxford MA), Film cooled airfoil body.
  11. Rice Ivan G. (P.O. Box 233 Spring TX 77373), Integrated gas/steam nozzle.
  12. Corrigan Charles E. (Tempe AZ), Laminated airfoil and method for turbomachinery.
  13. Sidenstick James E. (Cincinnati OH), Method and apparatus for forming diffused cooling holes in an airfoil.
  14. Tamura Raymond M. (218 Lagoon Dr. Honolulu HI 96819), Pollution reducing aircraft propulsion.
  15. 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.
  16. Andersen Richard H. (Cincinnati OH), Tip cooling for turbine blades.
  17. Papell S. Stephen (Berea OH), Vortex generating flow passage design for increased film cooling effectiveness.

이 특허를 인용한 특허 (36)

  1. Lang ; III William F. ; Auxier Thomas Alvin, Airfoils with leading edge pockets for reduced heat transfer.
  2. Tabbita Martin G. ; Downs James P. ; Soechting Friedrich O. ; Auxier Thomas A., Apparatus and method for cooling an airfoil for a gas turbine engine.
  3. Bunker, Ronald Scott, Components with conformal curved film holes and methods of manufacture.
  4. LaFleur Ronald Samuel, Coolable airfoil for a gas turbine engine.
  5. Ewald Lutum CH; Klaus Semmler DE; Jens Wolfersdorf CH, Cooled blade for a gas turbine.
  6. Liang, George, Cooling system for a tip of a turbine blade.
  7. Rawlinson, Anthony J.; Ireland, Peter; Turner, Lynne H.; Tibbott, Ian, Endwall component for a turbine stage of a gas turbine engine.
  8. Bunker, Ronald Scott, Engine component for a gas turbine engine.
  9. 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.
  10. 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.
  11. Hatman, Anca, Heat exchanging hollow passages with helicoidal grooves.
  12. Brittingham, Robert A.; Reed, Robert J.; Bruce, Kevin L.; Johns, David R., Metered cooling slots for turbine blades.
  13. 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.
  14. LaFleur Ronald S., Method and apparatus for cooling a wall within a gas turbine engine.
  15. 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.
  16. 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.
  17. 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.
  18. 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.
  19. Palmer,Nicholas Charles; Kirkeng,Kevin Lee; Lee,Ching Pang, Pattern cooled turbine airfoil.
  20. Liang, George, Process for cooling a turbine blade trailing edge.
  21. Shaw James S. ; Fleck James N., Striated cooling hole.
  22. Liang, George, Turbine airfoil cooling system with near wall vortex cooling chambers.
  23. Liang, George, Turbine airfoil with leading edge cooling.
  24. Liang, George, Turbine airfoil with near-wall impingement and vortex cooling.
  25. Krumanaker, Matthew Lee; Brassfield, Steven Robert; Bergholz, Robert Frederick; Smith, Aaron Ezekiel; Dooley, Weston Nolan, Turbine blade.
  26. Krumanaker, Matthew Lee; Dooley, Weston Nolan; Brassfield, Steven Robert; Helmer, David Benjamin; Bailey, Jeremy Clyde; Briggs, Robert David, Turbine blade.
  27. Liang, George, Turbine blade with trailing edge cooling.
  28. Harvey,Neil W; Ireland,Peter T; Ling,John P C W, Turbine component.
  29. Kitamura,Tsuyoshi; Takeishi,Kenichiro; Matsuura,Masaaki; Nogami,Ryoma, Turbine cooling vane of gas turbine engine.
  30. Lee, Ching-Pang, Turbine engine component wall having branched cooling passages.
  31. Kennepohl, Fritz; Korte, Detlef, Turbine of a gas turbine.
  32. Maldonado, Jaime Javier, Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components.
  33. Liang, George, Vortex cooled turbine blade outer air seal for a turbine engine.
  34. Liang,George, Vortex cooling for turbine blades.
  35. Liang,George, Vortex cooling of turbine blades.
  36. Ben-Amoz Meir (Lynn MA), Wall having cooling passage.
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