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Turbine blade with trailing edge root section cooling 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0993023 (1997-12-17)
발명자 / 주소
  • Liang George P.
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Hayes
인용정보 피인용 횟수 : 44  인용 특허 : 12

초록

A convectively cooled turbine blade has two distinct cooling air passage systems. The first system cools the blade leading edge and emits cooling air through outlet passageways in the leading edge arranged in showerhead array. The second system includes a five-pass series flow passage comprising fiv

대표청구항

[ I claim:] [1.] A turbine blade having a hollow elongated body including a root portion at one end and a blade portion extending from said root portion and terminating at a tip at the other end of said body, said body having opposing side walls and longitudinally extending leading and trailing edge

이 특허에 인용된 특허 (12)

  1. Zelesky Mark F. ; Mongillo Dominic J. ; Candelori David J. ; Steuber Gary D., Coolable air foil for a gas turbine engine.
  2. Green Dennis J. (Amston CT) Yamarik George J. (Vernon CT), Coolable airfoil structure.
  3. Hoff Richard W. (Glastonbury CT) Martin David R. (East Hartford CT), Coolable airfoil structure.
  4. Hall Kenneth B. (Jupiter FL) McClelland Robert J. (Palm Beach Gardens FL) Auxier Thomas A. (Palm Beach Gardens FL), Cooled blades for a gas turbine engine.
  5. Deptowicz Donald L. (Hamden CT) Soechting Friedrich O. (Tequesta FL), Core for fabrication of gas turbine engine airfoils.
  6. Hall Kenneth B. (Jupiter FL) Auxier Thomas A. (Palm Beach Gardens FL) Brown Wesley D. (Jupiter FL), Dirt removal means for air cooled blades.
  7. Moss Roger W. (Derby GB2) Coney Michael H. (Derby GB2) Richardson David A. (Derby GB2), Hollow fluid cooled turbine blades.
  8. Clevenger Douglas H. ; Matyas Mary Curley, Method for cooling a gas turbine stator vane.
  9. Lee Ching-Pang (Cincinnati OH) Subramanian Sundaresa V. (Cincinnati OH) Durgin George A. (West Chester OH), Multi-tier turbine airfoil.
  10. Auxier Thomas A. (Lake Park FL) Hall Kenneth B. (Jupiter FL) Landis Kenneth K. (Tequesta FL), Triple pass cooled airfoil.
  11. Thomas ; Jr ; Theodore T. (Maineville OH) Lee Ching-Pang (Cincinnati OH), Turbine blade composite cooling circuit.
  12. Corsmeier Robert J. (Cincinnati) MacLin Harvey M. (Cincinnati OH), Turbine blade impingement baffle.

이 특허를 인용한 특허 (44)

  1. Blaskovich,Timothy; Lebel,Larry; Trindade,Ricardo, Airfoil cooling passage trailing edge flow restriction.
  2. Lee, Ching-Pang; Munshi, Mrinal; Azad, Gm S.; Um, Jae Y., Airfoil having built-up surface with embedded cooling passage.
  3. Cunha,Frank J.; Albert,Jason E., Airfoil with large fillet and micro-circuit cooling.
  4. Robert J. Kildea, Attachment air inlet configuration for highly loaded single crystal turbine blades.
  5. Townes, Roderick M.; Tibbott, Ian; Dane, Edwin, Blade.
  6. Alexander Beeck DE; Jorgen Ferber DE; Christoph Nagler CH; Lothar Schneider DE; Klaus Semmler DE, Blade for gas turbines with choke cross section at the trailing edge.
  7. Palumbo Michael A. ; Mongillo ; Jr. Dominic J. ; Zelesky Mark F., Coolable airfoil structure.
  8. Bariaud Christian Bernard,FRX ; Bil Eric Stephan,FRX, Cooled turbine blade.
  9. Semmler Klaus,DEX ; Weigand Bernhard,DEX, Cooled vane for gas turbine.
  10. Scott, Robert Kenmer; Tapley, Joseph Theodore, Cooling of combustion turbine airfoil fillets.
  11. Liang,George, Cooling system for a turbine vane.
  12. Jacala,Ariel Caesar Prepena; Itzel,Gary M.; Kornau,Joshua R.; Ladhani,Azadali A., Cooling system for the trailing edges of turbine bucket airfoils.
  13. Lee, Ching-Pang, Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways.
  14. 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.
  15. Mongillo, Jr.,Dominic J.; Chon,Young H.; Kulak, legal representative,Eugene; Kulak, deceased,Raymond, Fanned trailing edge teardrop array.
  16. Mongillo, Jr.,Dominic J.; Chon,Young H.; Kulak, legal representative,Eugene; Kulak,Raymond, Fanned trailing edge teardrop array.
  17. Liang,George, Gas turbine airfoil leading edge cooling.
  18. Ishiguro Tatsuo,JPX ; Watanabe Koji,JPX ; Matsuura Masaaki,JPX ; Takeishi Kenichiro,JPX ; Masada Junichiro,JPX ; Tomita Yasuoki,JPX ; Suenaga Kiyoshi,JPX, Gas turbine cooled blade.
  19. Yasuoki Tomita JP; Yukihiro Hashimoto JP; Kiyoshi Suenaga JP; Hisato Arimura JP; Shunsuke Torii JP; Jun Kubota JP; Akihiko Shirota JP; Sunao Aoki JP; Tatsuo Ishiguro JP, Gas turbine moving blade.
  20. Morris, Mark C.; Wolfmeyer, George W.; Tapia, Luis A.; Agarwal, Vivek; Poon, Kin; Smoke, Jason C.; Baker, William C.; Armstrong, Henry M., High effectiveness cooled turbine blade.
  21. Liang,George, Impingement cooling system for a turbine blade.
  22. Papple,Michael Leslie Clyde, Internally cooled gas turbine airfoil and method.
  23. Papple,Michael Leslie Clyde, Internally cooled gas turbine airfoil and method.
  24. Papple,Michael Leslie Clyde, Internally cooled gas turbine airfoil and method.
  25. Papple,Michael Leslie Clyde, Internally cooled turbine blade.
  26. Corcoran, Christopher; Ghigliotty, Jamie G.; Perez, Rafael A.; Pietraszkiewicz, Edward F., Low pressure loss cooled blade.
  27. Danowski, Michael Joseph; Brainch, Gulcharan Singh, Method for reducing cooled turbine element stress and element made thereby.
  28. Rinck, Gerard Anthony; Clarke, Jonathan Philip; Norton, Brian Alan, Methods and systems for cooling gas turbine engine airfoils.
  29. Tung Stephen K. ; Solda Robert B. ; Manning Robert F., Pressure compensated turbine nozzle.
  30. Lee, Ching-Pang, Trailing edge cooling system in a turbine airfoil assembly.
  31. Liang,George, Turbine airfoil trailing edge cooling system with segmented impingement ribs.
  32. Liang, George, Turbine airfoil with leading edge cooling.
  33. Liang, George, Turbine airfoil with near wall inflow chambers.
  34. Liang, George, Turbine airfoil with serpentine trailing edge cooling circuit.
  35. Downs,James P.; Roeloffs,Norman F.; Pietraszkiewicz,Edward F., Turbine blade cooling system.
  36. Liang, George, Turbine blade with multiple metering trailing edge cooling holes.
  37. Liang, George, Turbine blade with showerhead film cooling holes.
  38. Cherolis, Anthony P.; Page, Richard H., Turbine blade with split impingement rib.
  39. Liang, George, Turbine blade with trailing edge bleed slot arrangement.
  40. Cherolis, Anthony P.; Christophel, Jesse R.; Abdel Messeh, William, Turbine component with tip flagged pedestal cooling.
  41. Cunha, Frank J.; Dahmer, Matthew T., Turbine element.
  42. Liang, George; Gao, Zhihong; Wessell, Brian J.; Gilliam, Joseph B., Turbine endwall with grooved recess cavity.
  43. Soechting,Friedrich; Ellis,Charles; Tomita,Yasuoki; Torii,Shunsuke, Turbine moving blade and gas turbine.
  44. Liang, George, Turbine rotor blade with serpentine cooling.
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