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Film cooled slotted wall 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0354194 (1994-12-12)
발명자 / 주소
  • Lee Ching-Pang (Cincinnati OH) Prakash Chander (West Chester OH) Starkweather John H. (Cincinnati OH) Zerkle Ronald D. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 39  인용 특허 : 0

초록

A wall adapted for use in a gas turbine engine between a first fluid and a second hotter fluid includes a first side over which is flowable the first fluid, and an opposite second side over which is flowable the second fluid. An elongate slot extends partly inwardly and perpendicularly from the seco

대표청구항

A wall adaptable for use in a gas turbine engine between a first fluid and a hotter second fluid comprising: a first side over which is flowable said first fluid; an opposite second side spaced from said first side along a transverse axis and over which is flowable said second fluid in a downstream

이 특허를 인용한 특허 (39)

  1. Brainch Gulcharan S. ; Danowski Michael J. ; Clarke Jonathan P., Aerodynamic article with partial outer portion and method for making.
  2. McCarty,Michael W., Aerodynamic noise abatement device and method for air-cooled condensing systems.
  3. Lacy, Benjamin Paul, Airfoil.
  4. Lacy, Benjamin Paul, Airfoil.
  5. Simpson, Stanley Frank; Lacy, Benjamin Paul, Airfoil.
  6. Piggush, Justin D.; Kohli, Atul, Airfoil including trench with contoured surface.
  7. Spangler, Brandon W.; Draper, Sam, Airfoil with hybrid drilled and cutback trailing edge.
  8. Tabbita Martin G. ; Downs James P. ; Soechting Friedrich O. ; Auxier Thomas A., Apparatus and method for cooling an airfoil for a gas turbine engine.
  9. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with convergent cooling channel.
  10. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with decreased liner cooling.
  11. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with improved film cooling.
  12. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with reduced cooling dilution openings.
  13. Budmir, Rosic; Sakamoto, Yasuro; Uchida, Sumiu; Ito, Eisaku; Kitamura, Tsuyoshi; Hada, Satoshi; Nakamura, Sosuke, Communicating structure between adjacent combustors and turbine portion and gas turbine.
  14. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Component wall having diffusion sections for cooling in a turbine engine.
  15. Bunker, Ronald Scott, Components with conformal curved film holes and methods of manufacture.
  16. LaFleur Ronald Samuel, Coolable airfoil for a gas turbine engine.
  17. Zelesky Mark F., Coolable vane or blade for a turbomachine.
  18. Rhodes Jeffrey F., Cooled airfoil.
  19. Abdel-Messeh, William; Blair, Michael F.; Kohli, Atul; Piggush, Justin D., Cooled airfoils and gas turbine engine systems involving such airfoils.
  20. Zuniga, Humberto A.; Lee, Ching-Pang; Crawford, Michael E., Cooled component wall in a turbine engine.
  21. Vandervaart, Peter C.; Rhodes, Jeffrey F.; Kwon, Okey; Heffernan, Tab M., Cooled gas turbine engine component.
  22. Lacy, Benjamin Paul; Good, Randall Richard; Brzek, Brian Gene, Cooling structures for turbine rotor blade tips.
  23. Spangler, Brandon W.; Pietraszkiewicz, Edward F., Dual cut-back trailing edge for airfoils.
  24. Maltson, John David, Eccentric chamfer at inlet of branches in a flow channel.
  25. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Film cooled component wall in a turbine engine.
  26. Vandervaart, Peter C.; Rhodes, Jeffrey F.; Kwon, Okey; Heffernan, Tab M.; Barker, Brett J., Gas turbine engine component arrangement.
  27. Boeke, Mark A.; Otero, Edwin; DeGray, Jeffrey J.; Propheter-Hinckley, Tracy A.; Fernandez, Guillermo J.; Riley, Sarah, Gas turbine engine component with discharge slot having oval geometry.
  28. 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.
  29. 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.
  30. 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.
  31. Rockstroh Todd J. ; Crow John M. ; Lee Ching-Pang ; Risbeck James D., Method of laser forming a slot.
  32. Amann, Christian; Beck, Thomas; Beckmann, Björn; Böttcher, Andreas; Esser, Winfried; Gaio, Giuseppe; Küperkoch, Rudolf; Schumann, Eckart; Teteruk, Rostislav, Modified interface around a hole.
  33. Sakamoto, Yasuro; Ito, Eisaku, One-stage stator vane cooling structure and gas turbine.
  34. Messelling William G., Repair of a recess in an article surface.
  35. Shelton, Monty Lee; Wallace, Thomas Tracy; Frederick, Robert Alan, System and method for airfoil film cooling.
  36. Kercher David M., Triple tip-rib airfoil.
  37. Marini, Remo; Girgis, Sami, Turbine blade for a gas turbine engine.
  38. Cherry, David Glenn; Lee, Ching-Pang; Prakash, Chander; Wadia, Aspi Rustom; Keith, Brian David; Brassfield, Steven Robert, Turbine blade having angled squealer tip.
  39. Laurello, Vincent P.; Lee, Ching-Pang, Turbine rotor disk inlet orifice for a turbine engine.
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