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Film cooled slotted wall 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0094998 (1993-07-23)
발명자 / 주소
  • Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY) Brzozowski Steven Joseph (Scotia NY)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 58  인용 특허 : 0

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 특허를 인용한 특허 (58)

  1. Spangler, Brandon W.; Bergman, Russell J., Airfoil cooling arrangement.
  2. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Airfoil leading edge end wall vortex reducing plasma.
  3. Slavens, Thomas N.; Devore, Matthew A., Airfoil leading edge film array.
  4. Guemmer, Volker, Blade with tangential jet generation on the profile.
  5. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with convergent cooling channel.
  6. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with decreased liner cooling.
  7. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with improved film cooling.
  8. Bunker,Ronald Scott, Combustor liner with inverted turbulators.
  9. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with reduced cooling dilution openings.
  10. Bunker, Ronald Scott, Combustor liner with ring turbulators and related method.
  11. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Component wall having diffusion sections for cooling in a turbine engine.
  12. Zuniga, Humberto A.; Lee, Ching-Pang; Crawford, Michael E., Cooled component wall in a turbine engine.
  13. Nakamata, Chiyuki; Okita, Yoji, Cooled turbine component and cooled turbine blade.
  14. Gleiner, Matthew S.; Kohli, Atul; Zelesky, Mark F., Cooling hole with asymmetric diffuser.
  15. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  16. Levasseur, Glenn; Pietraszkiewicz, Edward F., Cooling hole with crenellation features.
  17. Mongillo, Dominic; Gleiner, Matthew S, Cooling hole with curved metering section.
  18. Mongillo, Jr., Dominic J.; Gleiner, Matthew S., Cooling hole with curved metering section.
  19. Xu, JinQuan; Levasseur, Glenn, Cooling hole with enhanced flow attachment.
  20. Kohli, Atul; Gleiner, Matthew S.; Zelesky, Mark F.; Xu, JinQuan, Cooling hole with thermo-mechanical fatigue resistance.
  21. Bunker, Ronald Scott, Double wall combustor liner segment with enhanced cooling.
  22. Lee, Ching-Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je-Chin, Downstream plasma shielded film cooling.
  23. 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.
  24. Lee, Ching-Pang; Um, Jae Y.; Munshi, Mrinal; Zuniga, Humberto A., Film cooled component wall in a turbine engine.
  25. Bunker, Ronald Scott, Film cooled slotted wall and method of making the same.
  26. Bunker,Ronald Scott, Fluid passages for power generation equipment.
  27. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  28. Xu, JinQuan, Gas turbine engine component with compound cusp cooling configuration.
  29. Xu, JinQuan; Levasseur, Glenn, Gas turbine engine component with converging/diverging cooling passage.
  30. Xu, JinQuan, Gas turbine engine component with cusped cooling hole.
  31. Xu, JinQuan, Gas turbine engine component with diffusive cooling hole.
  32. Xu, JinQuan, Gas turbine engine component with impingement and diffusive cooling.
  33. Xu, JinQuan, Gas turbine engine component with impingement and lobed cooling hole.
  34. Gleiner, Matthew S.; Zelesky, Mark F.; Kohli, Atul, Gas turbine engine component with multi-lobed cooling hole.
  35. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and dimpled cooling.
  36. Bunker,Ronald Scott; Lee,Ching Pang, Hot gas path component with mesh and impingement cooling.
  37. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and turbulated cooling.
  38. Vehr, James William, Interior cooling channels.
  39. Bunker, Ronald Scott, Linear surface concavity enhancement.
  40. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  41. 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.
  42. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  43. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  44. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  45. Xu, JinQuan, Multi-lobed cooling hole array.
  46. Lee,Ching Pang, Multiform film cooling holes.
  47. Xu, JinQuan, Multiple diffusing cooling hole.
  48. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  49. Bunker, Ronald Scott; Itzel, Gary Michael, Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method.
  50. Krumanaker, Matthew Lee; Brassfield, Steven Robert; Bergholz, Robert Frederick; Smith, Aaron Ezekiel; Dooley, Weston Nolan, Turbine blade.
  51. Krumanaker, Matthew Lee; Dooley, Weston Nolan; Brassfield, Steven Robert; Helmer, David Benjamin; Bailey, Jeremy Clyde; Briggs, Robert David, Turbine blade.
  52. Bunker, Ronald Scott; Klug, Frederic Joseph; Huang, Shyh-Chin; Hyde, Susan Marie; Nirmalan, Nirm Velumylum, Turbine blade core cooling apparatus and method of fabrication.
  53. Bunker, Ronald Scott; Klug, Frederic Joseph; Huang, Shyh-Chin, Turbine blade cover cooling apparatus and method of fabrication.
  54. Bunker, Ronald Scott; Klug, Frederic Joseph; Huang, Shyh-Chin, Turbine blade wall cooling apparatus and method of fabrication.
  55. Miranda, Carlos Miguel; Trimmer, Andrew Lee; Kottilingam, Srikanth Chandrudu; Lacy, Benjamin Paul, Turbine component having surface cooling channels and method of forming same.
  56. Lee, Ching-Pang, Turbine engine component wall having branched cooling passages.
  57. Laurello, Vincent P.; Lee, Ching-Pang, Turbine rotor disk inlet orifice for a turbine engine.
  58. Lee, Ching Pang; Wadia, Aspi Rustom; Cherry, David Glenn; Han, Je Chin, Upstream plasma shielded film cooling.
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