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Film cooled wall 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0968544 (1992-10-29)
발명자 / 주소
  • Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 48  인용 특허 : 11

초록

A wall adapted for use in a gas turbine engine between a first and a hotter second 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 inwardly from the second side and is disposed in flow c

대표청구항

A wall adaptable for use in a gas turbine engine between a first fluid and a second fluid being hotter than said first 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

이 특허에 인용된 특허 (11)

  1. Auxier Thomas A. (Lake Park FL) Anderson Leon R. (Tequesta FL) Hill ; Jr. Edward C. (Tequesta FL), Coolant passages with full coverage film cooling slot.
  2. Hall Kenneth B. (Jupiter FL) Landis Kenneth K. (Tequesta FL), Cooled gas turbine blade.
  3. Marriage Peter V. (Derby GB2), Cooled turbomachinery components.
  4. Cunha Francisco J. (Schenectady NY) De Angelis David A. (Voorheesville NY), Cooling circuit for turbine stator vane trailing edge.
  5. Lee Ching-Pang (Cincinnati OH) Thomas ; Jr. Theodore T. (Loveland OH) Isburgh Anne M. (Loveland OH), Cooling hole arrangements in jet engine components exposed to hot gas flow.
  6. Vehr James W. (Lake Park FL), Cross-flow film cooling passages.
  7. Anderson Leon R. (Tequesta FL) Auxier Thomas A. (Lake Park FL), Film cooled vanes and turbines.
  8. Field Robert E. (208-16 Airport Rd. West Lafayette IN 47906), Film cooling passages with step diffuser.
  9. Hall Kenneth B. (Jupiter FL) Landis Kenneth K. (Tequesta FL), Method of fabricating an air cooled turbine blade.
  10. Richardson John S. (Derby GB2), Perforated two layered sheet for use in film cooling.
  11. Pidcock Anthony (Derby GB2) Cooper Stephen M. (Derby GB2) Fry Peter (Derby GB2), Removable combustor liner for gas turbine engine combustor.

이 특허를 인용한 특허 (48)

  1. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Airfoil leading edge end wall vortex reducing plasma.
  2. Guemmer, Volker, Blade with tangential jet generation on the profile.
  3. Bunker,Ronald Scott, Combustor liner with inverted turbulators.
  4. Bunker, Ronald Scott, Combustor liner with ring turbulators and related method.
  5. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Component wall having diffusion sections for cooling in a turbine engine.
  6. Bunker, Ronald Scott, Components with conformal curved film holes and methods of manufacture.
  7. Ewald Lutum CH; Klaus Semmler DE; Jens Wolfersdorf CH, Cooled blade for a gas turbine.
  8. Zuniga, Humberto A.; Lee, Ching-Pang; Crawford, Michael E., Cooled component wall in a turbine engine.
  9. Gleiner, Matthew S.; Kohli, Atul; Zelesky, Mark F., Cooling hole with asymmetric diffuser.
  10. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  11. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  12. Mongillo, Dominic; Gleiner, Matthew S, Cooling hole with curved metering section.
  13. Mongillo, Jr., Dominic J.; Gleiner, Matthew S., Cooling hole with curved metering section.
  14. Xu, JinQuan; Levasseur, Glenn, Cooling hole with enhanced flow attachment.
  15. Kohli, Atul; Gleiner, Matthew S.; Zelesky, Mark F.; Xu, JinQuan, Cooling hole with thermo-mechanical fatigue resistance.
  16. Bunker, Ronald Scott, Double wall combustor liner segment with enhanced cooling.
  17. Lee, Ching-Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je-Chin, Downstream plasma shielded film cooling.
  18. Levasseur, Glenn; Pietraszkiewicz, Edward F.; Zelesky, Mark F.; Mongillo, Jr., Dominic J.; Klinefelter, Kevin J.; Doll, Stephen D.; Fritch, Markus W., EDM method for multi-lobed cooling hole.
  19. Bunker, Ronald Scott, Engine component.
  20. Bunker, Ronald Scott; Briggs, Robert David, Engine component.
  21. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Film cooled component wall in a turbine engine.
  22. Bunker, Ronald Scott, Film cooled slotted wall and method of making the same.
  23. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  24. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  25. Xu, JinQuan; Levasseur, Glenn, Gas turbine engine component with converging/diverging cooling passage.
  26. Xu, JinQuan, Gas turbine engine component with cusped cooling hole.
  27. Xu, JinQuan, Gas turbine engine component with diffusive cooling hole.
  28. Xu, JinQuan, Gas turbine engine component with impingement and diffusive cooling.
  29. Xu, JinQuan, Gas turbine engine component with impingement and lobed cooling hole.
  30. Gleiner, Matthew S.; Zelesky, Mark F.; Kohli, Atul, Gas turbine engine component with multi-lobed cooling hole.
  31. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and dimpled cooling.
  32. Bunker,Ronald Scott; Lee,Ching Pang, Hot gas path component with mesh and impingement cooling.
  33. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and turbulated cooling.
  34. Bunker, Ronald Scott, Linear surface concavity enhancement.
  35. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  36. 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.
  37. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  38. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  39. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  40. Xu, JinQuan, Multi-lobed cooling hole array.
  41. Liang,George, Multi-metered film cooled blade tip.
  42. Xu, JinQuan, Multiple diffusing cooling hole.
  43. Hu, Zhaoli; Darling, Abe Denis; McDowell, Shamgar Elijah; Serieno, Douglas Anthony, System and method for forming a cooling hole in an airfoil.
  44. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  45. Miranda, Carlos Miguel; Trimmer, Andrew Lee; Kottilingam, Srikanth Chandrudu; Lacy, Benjamin Paul, Turbine component having surface cooling channels and method of forming same.
  46. Lee, Ching-Pang, Turbine engine component wall having branched cooling passages.
  47. Laurello, Vincent P.; Lee, Ching-Pang, Turbine rotor disk inlet orifice for a turbine engine.
  48. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Upstream plasma shielded film cooling.
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