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Transitional multihole combustion liner 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
출원번호 US-0116509 (1998-07-16)
발명자 / 주소
  • Burns Craig P.
  • Duncan Beverly S.
  • Thompson James E.
  • Wiehe Glenn E.
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 26  인용 특허 : 8

초록

A combustor liner includes a wall having an outboard surface and an opposite inboard surface. A plurality of first holes are inclined through the wall in a multihole pattern to channel cooling fluid therethrough to form a cooling film layer along the inboard surface. A second hole extends perpendicu

대표청구항

[ What is claimed is:] [1.] A combustor liner comprising:a wall having an outboard surface over which is flowable a cooling fluid, and a opposite inboard surface for facing combustion gases;a plurality of first holes inclined through said wall at an acute inclination angle from said surfaces thereof

이 특허에 인용된 특허 (8)

  1. Ansart Denis Roger Henri,FRX ; Ciccia Patrick Samuel Andre,FRX ; Desaulty Michel Andre Albert,FRX, Combustion chamber having a multi-hole cooling system with variably oriented holes.
  2. Napoli Phillip D. (West Chester OH), Combustor liner with circumferentially angled film cooling holes.
  3. Joshi Narendra D. ; Angel Paul R. ; Caldwell James M. ; Heberling Paul V. ; Dean Anthony J., Dual fuel mixer for gas turbine combustor.
  4. Wakeman Thomas G. (Lawrenceburg OH IN) Walker Alan (Wyoming OH) Maclin Harvey M. (Cincinnati OH), Gas turbine engine multi-hole film cooled combustor liner and method of manufacture.
  5. Lampes Elias H. (Lynn MA), Multi-hole film cooled combuster linear with differential cooling.
  6. Foltz Howard L. (West Chester OH), Multi-hole film cooled combustor liner with rectangular film restarting holes.
  7. Napoli Phillip D. (West Chester OH), Multi-hole film cooled combustor liner with slotted film starter.
  8. Sandelis Denis,FRX, Turbojet engine combustion chamber with heat protecting lining.

이 특허를 인용한 특허 (26)

  1. Caldwell,James Michael; Tomlinson,Thomas John; Zimmerman, Jr.,Robert George; Heidorn,Raymond William; Farmer,Gilbert, Adjusting airflow in turbine component by depositing overlay metallic coating.
  2. Kwon, Okey, Augmented cooling system.
  3. Bronson, Thomas J.; Zupanc, Frank J., Circumferentially varied quench jet arrangement for gas turbine combustors.
  4. Clemen, Carsten, Combustion chamber of a gas turbine.
  5. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.
  6. Burd, Steven W.; Cheung, Albert K., Combustor cooling hole pattern.
  7. Suleiman, Baha; Vise, Steven Clayton; Brown, Daniel Dale, Combustor liner and method of fabricating same.
  8. Tariq Kay Harris ; Michael Burke Briski, Combustor liner having preferentially angled cooling holes.
  9. Anderson,Morris G.; Kawamura,Hiroshi; Flamand,Luis M., Effusion momentum control.
  10. Yokota, Osami; Hidaka, Masataka; Numata, Shohei; Tatsumi, Tetsuma, Gas turbine combustion liner with triangular heat transfer element.
  11. Cheung,Albert K.; Napoli,Nikolaos; Segalman,Irving, Gas turbine combustor heat shield panel or exhaust panel including a cooling device.
  12. Dudebout, Rodolphe; Brandt, Dustin; Waldman, David; Neumann, James; Payne, Art, Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques.
  13. Pinnick, Donald E.; Froemming, Kenneth W.; Varney, Bruce E., Gas turbine engine variable porosity combustor liner.
  14. Pinnick, Donald E.; Froemming, Kenneth W.; Varney, Bruce E., Gas turbine engine variable porosity combustor liner.
  15. Pinnick, Donald E.; Froemming, Kenneth W.; Varney, Bruce E.; Loebig, James C.; Taylor, Todd, Gas turbine engine with improved combustion liner.
  16. Gerendas, Miklos, Gas-turbine combustion chamber with a cooling-air supply device.
  17. Slabaugh, Carson D.; Kapat, Jayanta S., Heat transfer augmented fluid flow surfaces.
  18. Burd, Steven W.; Cheung, Albert K., Local cooling hole pattern.
  19. Farmer, Gilbert; Tomlinson, Thomas John; Heidorn, Raymond William; Fehrenbach, Jeffrey Arnold; Imhoff, William Lee; Rutherford, Myron Edward, Method for thermal barrier coating and a liner made using said method.
  20. Bernier, Daniel Francis Paul; Campion, Jean-Michel Jacques; Touchaud, Stéphane Henri Guy, Performance of a combustion chamber by multiple wall perforations.
  21. Brown, Daniel Dale; Farmer, Gilbert; Rutherford, Myron Edward, Preferential multihole combustor liner.
  22. Farmer, Gilbert; Brown, Daniel Dale; Rutherford, Myron Edward, Preferential multihole combustor liner.
  23. Schumacher, Jurgen C.; Zupanc, Frank J.; Dudebout, Rodolphe, Segmented effusion cooled gas turbine engine combustor.
  24. Moura, Dennis M.; Pacheco-Tougas, Monica; Eastwood, Jonathan J.; Bouldin, Lee E., Turbine engine combustor heat shield with multi-angled cooling apertures.
  25. Leglaye, Francois; Oblaza, Sylvain; Lutz, Patrick, Turbine engine wall having at least some cooling orifices that are plugged.
  26. Beule,Frederic; Desaulty,Michel, Turbomachine annular combustion chamber.
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