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Combustion liner for a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
  • F02G-003/00
출원번호 US-0689253 (1985-01-07)
발명자 / 주소
  • Madden Thomas J. (Vernon CT)
출원인 / 주소
  • United Technologies Corporation (Hartford CT 02)
인용정보 피인용 횟수 : 50  인용 특허 : 4

초록

The liner of a combustor for a gas turbine engine is constructed to include a refilmer at the combustion/dilution air holes so as to form a film of cool air along the inner surface of the liner in the combustion, that would otherwise be destroyed by the combustion/dilution air.

대표청구항

For a gas turbine power plant, a combustor having a plurality of panels generally circular in shape and extending axially arranged end to end to define an annular combustion chamber, each of said panels having an inner surface subjected to combustion gases and an outer surface subjected to power pla

이 특허에 인용된 특허 (4)

  1. Dierberger, James A., Combustion liner cooling scheme.
  2. Saintsbury, John A.; Sampath, Parthasarathy; Weinberg, Maurice, Combustor for a gas turbine engine.
  3. Tanrikut Ibrahim S. (Manchester CT) Wagner Walter B. (Bolton CT) Segalman Irwin (Bloomfield CT) Goldberg Perry (West Hartford CT), Combustor liner construction.
  4. Austin ; Jr. George W. (Glastonbury CT) Breton Robert A. (Old Saybrook CT) Nolan James J. (Glastonbury CT) Striebel Edmund E. (South Windsor CT), Combustor liner for gas turbine engine.

이 특허를 인용한 특허 (50)

  1. Erbas-Sen, Nurhak; Hoke, James B.; Tu, John S.; Pacheco-Tougas, Monica, Active cooling of grommet bosses for a combustor panel of a gas turbine engine.
  2. Huth, Michael; Tiemann, Peter; Oltmanns, legal representative, Iris, Combustion chamber.
  3. Taylor, Robert A J; Foale, Marcus, Combustion chamber.
  4. Rasmussen Neil S. (Loveland OH) Szema Li-Chieh (West Chester OH) Abuaf Nesim (Schenectady NY), Combustion chamber liner insert.
  5. Clemen, Carsten, Combustion chamber tile of a gas turbine and method for its manufacture.
  6. Berry, Jonathan D.; DeForest, Russell P.; Som, Abhijit, Combustion liner thimble insert and related method.
  7. McKenzie, Crisen; Snyder, Timothy S., Combustor having a beveled grommet.
  8. Fadde, Elizabeth Angelyn; Stoia, Lucas John; Willis, Christopher Paul, Combustor leakage control system.
  9. Bangerter, James P.; Low, Kevin Joseph; Jause, Jonathan M.; Sonntag, Robert; Rezvani, Reza; Kwoka, David, Combustor with grommet having projecting lip.
  10. Rudrapatna, Nagaraja S.; Frye, Lowell; Landram, William, Combustors with quench inserts.
  11. H채ggander,Jan, Component for being subjected to high thermal load during operation and a method for manufacturing such a component.
  12. Sandoval, Jonathan P.; Smith, Randolph J., Conjoined grommet assembly for a combustor.
  13. Jause, Jonathan M.; Duhamel, Dennis John; Hoke, James B.; Tu, John S., Cooled combustor liner grommet.
  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. Lee, Ching-Pang; Morrison, Jay A., Ducting arrangement for cooling a gas turbine structure.
  22. 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.
  23. Howell Stephen J. ; Waslo Jennifer, Film cooled combustor liner and method of making the same.
  24. Dierberger, James A.; Schlichting, Kevin W.; Freling, Melvin, Floatwell panel assemblies and related systems.
  25. Mumford Stephen E. (Longwood FL) Smed Jan P. (Winter Springs FL), Gas turbine combustion chamber with air scoops.
  26. Yokota, Osami; Hidaka, Masataka; Numata, Shohei; Tatsumi, Tetsuma, Gas turbine combustion liner with triangular heat transfer element.
  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. Tu, John S.; Hoke, James B.; Pacheco-Tougas, Monica; Snyder, Timothy S.; Moura, Dennis M.; Van, Anthony, Hybrid through holes and angled holes for combustor grommet cooling.
  36. Kim, Young Bong; Choe, Jinhoon; Roh, Ujin, Liner, flow sleeve and gas turbine combustor each having cooling sleeve.
  37. Reed, Gordon Miller; Faughnan, Jr., Paul R.; Quitter, John, Manufacturing methods for multi-lobed cooling holes.
  38. Fortin, Thomas B.; Chetta, Gregory E.; Leung, David W.; Meyers, Duncan C.; Belson, Keith C.; Diaz, John V.; Holladay, Thomas E.; Ladd, Scott A.; McKinney, Randall G.; Rinella, Sergio; Sadil, Andreas;, Method and system for designing an impingement film floatwall panel system.
  39. Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole.
  40. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  41. Xu, JinQuan; Zelesky, Mark F.; Kohli, Atul; Gleiner, Matthew S., Multi-lobed cooling hole and method of manufacture.
  42. Xu, JinQuan, Multi-lobed cooling hole array.
  43. Xu, JinQuan, Multiple diffusing cooling hole.
  44. Kaleeswaran, Karthick; Pejawar, Rao Ganesh; Bhojani, Sonal, Ring cooling for a combustion liner and related method.
  45. Verdegan, Barry M.; Schwandt, Brian; Jeung, Soondeuk; Wieczorek, Mark T., Surface coalescers.
  46. Burd, Steven W., Thermal barrier coating of a combustor dilution hole.
  47. Grant ; Jr. James R. (Jupiter FL), Thrust augmentor flameholder.
  48. Zelesky, Mark F.; Kohli, Atul; Lewis, Scott D., Tri-lobed cooling hole and method of manufacture.
  49. Sandelis Denis,FRX, Turbojet engine combustion chamber with heat protecting lining.
  50. Anthony Pidcock GB; Desmond Close GB; Michael P. Spooner GB, Wall elements for gas turbine engine combustors.
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