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Hollow airfoil for a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0217697 (1998-12-21)
발명자 / 주소
  • Tabbita Martin G.
  • Downs James P.
  • Soechting Friedrich O.
  • Auxier Thomas A.
  • Steinbauer
  • Jr. Frederick
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Getz
인용정보 피인용 횟수 : 46  인용 특허 : 9

초록

A hollow airfoil is provided which includes a body having an external wall and an internal cavity. The external wall includes a suction side portion and a pressure side portion. The portions extend chordwise between a leading edge and a trailing edge and spanwise between an inner radial surface and

대표청구항

[ We claim:] [1.] A hollow airfoil, comprising:an internal cavity;an external wall, which includes a suction side portion and a pressure side portion, wherein said portions extend chordwise between a leading edge and a trailing edge and spanwise between an inner radial surface and an outer radial su

이 특허에 인용된 특허 (9)

  1. Green Dennis J. (Amston CT), Airfoil having coolable leading edge region.
  2. Andress Dale E. (Palm Beach Gardens FL) Clevenger Douglas H. (Palm Beach Gardens FL), Cooled rotor blade.
  3. Clifford Rodney J. (Gloucestershire GB2) Charters Ian J. (Bristol GB2), Cooled turbine blade.
  4. Stahl ; William F., Cooled turbine vane.
  5. Coudray Xavier G. A. (Fontainebleau FRX) Derrien Mischal F. L. (Savigny Le Temple FRX) Pichon Philippe M. P. (Fontainebleau FRX), Cooled turbo-machine vane.
  6. Abdel-Messeh William,CAX ; Tibbott Ian,CAX ; Arora Subhash, Cooling passages for airfoil leading edge.
  7. Cunha Francisco J. (Schenectady NY), Integrated steam and air cooling for combined cycle gas turbines.
  8. Auxier Thomas A. (Palm Beach Gardens FL) Hall Kenneth B. (Jupiter FL), Leading edge cooling of turbine airfoils.
  9. Lee Ching-Pang (Cincinnati OH) Goebel Steven G. (Clifton Park NY) Abuaf Nesim (Schenectady NY), Micro-grooved heat transfer wall.

이 특허를 인용한 특허 (46)

  1. Lacy, Benjamin Paul, Airfoil.
  2. Lacy, Benjamin Paul, Airfoil.
  3. Spangler, Brandon W.; Bergman, Russell J., Airfoil cooling arrangement.
  4. Piggush, Justin D.; Kohli, Atul, Airfoil including trench with contoured surface.
  5. O'Hearn, Jason L.; Aggarwala, Andrew S., Airfoil leading edge shape tailoring to reduce heat load.
  6. Piggush, Justin D., Airfoil with cooling passage providing variable heat transfer rate.
  7. Piggush, Justin D., Airfoil with leading edge cooling passage.
  8. Piggush, Justin D.; Abdel-Messeh, William, Airfoil with tapered radial cooling passage.
  9. Abdel-Messeh, William; Piggush, Justin D., Airfoil with wrapped leading edge cooling passage.
  10. Abdel-Messeh, William; Piggush, Justin D., Airfoil with wrapped leading edge cooling passage.
  11. Groth, Pieter; Mårtensson, Hans, Blade for a flow machine.
  12. Albert, Jason Edward; Kohli, Atul; Couch, Eric L., Cast features for a turbine engine airfoil.
  13. Albert, Jason Edward; Kohli, Atul; Couch, Eric L., Cast features for a turbine engine airfoil.
  14. Albert, Jason Edward; Kohli, Atul; Couch, Eric L., Cast features for a turbine engine airfoil.
  15. Liang, George, Combustion turbine with airfoil having enhanced leading edge diffusion holes and related methods.
  16. Abdel-Messeh, William; Blair, Michael F.; Kohli, Atul; Piggush, Justin D., Cooled airfoils and gas turbine engine systems involving such airfoils.
  17. Janke, Erik; Taege, Jens; Schiessl, Thomas; Meier, Sebastian; Schiffer, Heinz-Peter; Winter, Nils; Lehmann, Knut, Cooled turbine blades for a gas-turbine engine.
  18. Liang,George, Cooling system for a showerhead of a turbine blade.
  19. Sugimoto, Takao; Tanaka, Ryozo; Tsuji, Koichiro; Bohn, Dieter; Kusterer, Karsten, Double jet film cooling structure.
  20. Kohli, Atul; Wagner, Joel H.; Aggarwala, Andrew S., Film cooled article with improved temperature tolerance.
  21. Kohli, Atul; Wagner, Joel H.; Aggarwala, Andrew S., Film cooled article with improved temperature tolerance.
  22. Slavens, Thomas N.; Snyder, Brooks E., Gas turbine engine airfoil with leading edge trench and impingement cooling.
  23. Cunha, Frank J.; Erbas-Sen, Nurhak, Gas turbine engine combustor with integrated combustor vane having swirler.
  24. Lewis, Scott D.; Rapp, Brandon M.; Beattie, Jeffrey S.; Hough, Matthew Andrew; Teller, Bret M.; Jacques, Jeffrey Michael; Asterlin, Max, Gas turbine engine component with combined mate face and platform cooling.
  25. Brittingham, Robert A.; Reed, Robert J.; Bruce, Kevin L.; Johns, David R., Metered cooling slots for turbine blades.
  26. Beeck, Alexander; Weigand, Bernhard, Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine component.
  27. Gannelli, Jesse; Gayman, Scott W.; Pietraszkiewicz, Edward F.; Jelks, Christopher B.; Pinero, Sandra S.; Rembish, Paul Thomas; Levy, Ryan Shepard, Method of creating an airfoil trench and a plurality of cooling holes within the trench.
  28. Paauwe,Corneil; Devore,Matthew, Method of producing cooling holes in highly contoured airfoils.
  29. Lewis, Scott D., Showerhead hole scheme apparatus and system.
  30. Kington, Harry Lester; Kanjiyani, Shezan; Wali, Natalie; Gintert, John; Tucker, Bradley R., Stationary airfoils configured to form improved slip joints in bi-cast turbine engine components and the turbine engine components including the same.
  31. Shelton, Monty Lee; Wallace, Thomas Tracy; Frederick, Robert Alan, System and method for airfoil film cooling.
  32. Bagnall, Adam MacGregor; Lockwood, Clive, Temperature controlling apparatus.
  33. Liang, George, Turbine airfoil cooling system with curved diffusion film cooling hole.
  34. Liang, George; Gu, Xubin, Turbine airfoil cooling system with spanwise equalizer rib.
  35. Liang,George, Turbine airfoil with endwall horseshoe cooling slot.
  36. Devore, Matthew A.; Paauwe, Corneil S., Turbine airfoil with improved cooling.
  37. Liang, George, Turbine airfoil with near-wall leading edge multi-holes cooling.
  38. Liang, George, Turbine airfoil with near-wall spiral flow cooling circuit.
  39. Liang, George, Turbine airfoil with showerhead cooling.
  40. Liang, George, Turbine airfoil with spiral trailing edge cooling passages.
  41. Dodd,Alec G, Turbine blade.
  42. Krumanaker, Matthew Lee; Brassfield, Steven Robert; Bergholz, Robert Frederick; Smith, Aaron Ezekiel; Dooley, Weston Nolan, Turbine blade.
  43. Krumanaker, Matthew Lee; Dooley, Weston Nolan; Brassfield, Steven Robert; Helmer, David Benjamin; Bailey, Jeremy Clyde; Briggs, Robert David, Turbine blade.
  44. Downs,James P.; Roeloffs,Norman F.; Pietraszkiewicz,Edward; Kontrovitz,David Michael; Fukuda,Takao, Turbine blade trailing edge construction.
  45. Liang, George, Turbine blade with a showerhead film cooling hole arrangement.
  46. Liang, George, Turbine blade with showerhead film cooling holes.
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