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Internally grooved turbine wall 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0286802 (1999-04-06)
발명자 / 주소
  • Lee Ching-Pang
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 48  인용 특허 : 5

초록

A turbine wall includes an outer surface for facing combustion gases, and an opposite inner surface for being impingement air cooled. A plurality of adjoining ridges and grooves are disposed in the inner surface for enhancing heat transfer by the impingement cooling air.

대표청구항

[ Accordingly, what is desired to be secured by Letters Patent of the United States is the invention as defined and differentiated in the following claims in which I claim:] [1.] A turbine wall comprising an outer surface for facing combustion gases; an opposite inner surface for being air cooled; a

이 특허에 인용된 특허 (5)

  1. Wettstein Hans (Fislisbach CHX), Baffle-cooled wall part.
  2. Lee Ching-Pang (Cincinnati OH) Goebel Steven G. (Clifton Park NY) Abuaf Nesim (Schenectady NY), Micro-grooved heat transfer wall.
  3. Whidden Graydon L. (Orlando FL), Shroud design.
  4. Okpara Nnawuihe (Peoria AZ) Henry Chester L. (Tempe AZ), Turbine blade with improved heat transfer surface.
  5. Lee Ching-Pang ; Knable David B., Turbulator configuration for cooling passages of an airfoil in a gas turbine engine.

이 특허를 인용한 특허 (48)

  1. Gregg, Shawn J.; Propheter-Hinckley, Tracy A.; Learned, Amanda Jean, Airflow influencing airfoil feature array.
  2. Xu, JinQuan, Airfoil cooling enhancement and method of making the same.
  3. Benson, Adebukola; Itzel, Gary Michael, Airfoil cooling hole flag region.
  4. Hasz, Wayne Charles; Johnson, Robert Alan; Lee, Ching-Pang; Rettig, Mark Gerard; Abuaf, Nesim; Starkweather, John Howard, Article having turbulation and method of providing turbulation on an article.
  5. Hasz, Wayne Charles; Johnson, Robert Alan; Lee, Ching-Pang; Rettig, Mark Gerard; Abuaf, Nesim; Starkweather, John Howard, Article having turbulation and method of providing turbulation on an article.
  6. Wayne Charles Hasz ; Robert Alan Johnson ; Ching-Pang Lee ; Mark Gerard Rettig ; Nesim Abuaf ; John Howard Starkweather, Article having turbulation and method of providing turbulation on an article.
  7. Ching-Pang Lee ; Wayne C. Hasz ; Nesim Abuaf ; Robert A. Johnson, Article surface with metal wires and method for making.
  8. Lee, Ching-Pang; Nichols, Glenn Herbert, Article wall with interrupted ribbed heat transfer surface.
  9. Lee Ching Pang ; Hasz Wayne Charles ; Abuaf Nesim ; Johnson Robert Alan, Casting having an enhanced heat transfer surface, and mold and pattern for forming same.
  10. Ching Pang Lee ; Wayne Charles Hasz ; Nesim Abuaf ; Robert Alan Johnson, Casting having an enhanced heat transfer, surface, and mold and pattern for forming same.
  11. Lee, Ching Pang; Hasz, Wayne Charles; Abuaf, Nesim; Johnson, Robert Alan, Casting having an enhanced heat transfer, surface, and mold and pattern for forming same.
  12. Lee, Ching Pang; Hasz, Wayne Charles; Abuaf, Nesim; Johnson, Robert Alan, Casting having an enhanced heat transfer, surface, and mold and pattern for forming same.
  13. Chon, Young H.; Propheter-Hinckley, Tracy A.; Couch, Eric L., Chambered airfoil cooling.
  14. Froehlich, Anton, Combustion chamber comprising a cooling unit and method for producing said combustion chamber.
  15. Froehlich, Anton, Combustion chamber comprising a cooling unit and method for producing said combustion chamber.
  16. Zelesky Mark F., Coolable vane or blade for a turbomachine.
  17. Shchukin, Sergey; Marmilic, Robert, Cooled wall.
  18. Bunker, Ronald Scott; Wei, Bin, Cooling passages and methods of fabrication.
  19. Nakamata, Chiyuki; Yamane, Takashi; Fukuyama, Yoshitaka; Bamba, Takahiro, Cooling structure of turbine airfoil.
  20. Lee, Ching Pang; Wang, Hsin Pang; Upadhyay, Ram Kumar; Myers, Paul Richard; Edgar, Marc Thomas, Disposable insert, and use thereof in a method for manufacturing an airfoil.
  21. Lee, Ching-Pang; Jackson, Melvin Robert; Ferrigno, Stephen Joseph; Zhao, Ji-Cheng, Foil formed cooling area enhancement.
  22. Horiuchi, Yasuhiro; Tagawa, Hisato; Morisaki, Tetsuro, Gas turbine blade.
  23. Daux, Stéphan; Giot, Chantal; Joubert, Hugues; Sauthier, Benjamin, Gas turbine blade cooling circuit having a cavity with a high aspect ratio.
  24. Propheter-Hinckley, Tracy A.; Zelesky, Mark F.; Mongillo, Jr., Dominic J.; Devore, Matthew A.; Gautschi, Steven Bruce; Fisk, Benjamin T., Gas turbine engine airfoil impingement cooling.
  25. Powis, Andrew Charles; McRae, Jr., Ronald Eugene; Clarke, Jonathan Philip; Peterman, Jonathan Jordan; Frederick, Robert Alan; Gibler, Edward Eugene; Keith, Brian David, Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity.
  26. Srinivasan, Balamurugan; Narayanan, Sridharan Reghupathy; Paramanandam, Karthikeyan; Jayamurugan, Chandiran; Malak, Malak Fouad, Gas turbine engines with improved leading edge airfoil cooling.
  27. Eifel, Marcel; Gloss, Daniel; Heselhaus, Andreas; Klumpp, Stephan; Link, Marco; Sieber, Uwe; Volker, Stefan; Wagner, Michael, Internally coolable component for a gas turbine with at least one cooling duct.
  28. Lee, Ching-Pang; Hillier, Gerald L.; Um, Jae Y.; Azad, Gm Salam, Investment casting method for gas turbine engine vane segment.
  29. Kizuka, Nobuaki; Horiuchi, Yasuhiro; Marushima, Shinya; Kuroki, Hidetoshi, Member having internal cooling passage.
  30. Kizuka, Nobuaki; Horiuchi, Yasuhiro; Marushima, Shinya; Kuroki, Hidetoshi, Member having internal cooling passage.
  31. Chan,Sze Bun Brian; Greene,John Ellington; Farral,Linda Jean, Method and apparatus for convective cooling of side-walls of turbine nozzle segments.
  32. Vedhagiri, Sivaraman; Moran, Brian David; Kelley, Shawn, Method for diverting flow around an obstruction in an internal cooling circuit.
  33. Lee, Ching-Pang; Chiu, Rong-Shi Paul, Method for enhancing heat transfer inside a turbulated cooling passage.
  34. Hasz, Wayne Charles; Abuaf, Nesim; Johnson, Robert Alan; Lee, Ching-Pang, Method for providing turbulation on the inner surface of holes in an article, and related articles.
  35. Malecki, Stacy T.; Propheter-Hinckley, Tracy A.; Learned, Amanda Jean; Gregg, Shawn J., Recessed metering standoffs for airfoil baffle.
  36. Malecki, Stacy T.; Propheter-Hinckley, Tracy A.; Learned, Amanda Jean; Gregg, Shawn J., Recessed metering standoffs for airfoil baffle.
  37. Darkins, Jr., Toby George; Alford, Mary Ellen; Noe, Mark Eugene, Shroud segment and assembly with circumferential seal at a planar segment surface.
  38. Alford, Mary Ellen; Darkins, Toby George; Noe, Mark Eugene, Shroud segment and assembly with surface recessed seal bridging adjacent members.
  39. Liang, George, Turbine airfoil cooling system with near wall vortex cooling chambers.
  40. Liang, George, Turbine airfoil cooling system with perimeter cooling and rim cavity purge channels.
  41. Cunha, Frank J.; Chon, Young H.; Dube, Bryan P., Turbine airfoil with enhanced heat transfer.
  42. Lee, Ching-Pang; Brown, Glenn E.; Heneveld, Benjamin E., Turbine blade incorporating trailing edge cooling design.
  43. Darkins, Jr., Toby George; Alford, Mary Ellen; Noe, Mark Eugene, Turbine engine axially sealing assembly including an axially floating shroud, and assembly method.
  44. Hasz, Wayne Charles; Abuaf, Nesim; Johnson, Robert Alan; Lee, Ching-Pang, Turbine engine component having enhanced heat transfer characteristics and method for forming same.
  45. Glynn, Christopher Charles; Alford, Mary Ellen; Noe, Mark Eugene; Darkins, Jr., Toby George, Turbine engine shroud assembly including axially floating shroud segment.
  46. Klasing,Kevin Samuel; Carson,Scott Michael, Turbine nozzle with purge cavity blend.
  47. Cooper,Brian G, Vane apparatus for a gas turbine engine.
  48. Moore, Robert P.; Seleski, Richard; Cox, Dale Lee, Vane enhanced trailing edge cooling design.
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