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Fabricated liner article and method 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/00
출원번호 US-0562959 (1983-12-19)
발명자 / 주소
  • Kelm James S. (Milford OH) Ludwig Arthur L. (Cincinnati OH) Maclin Harvey M. (Cincinnati OH) Roggenkamp Steven K. (West Chester OH) Wakeman Thomas G. (West Chester OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 30  인용 특허 : 7

초록

A method of fabricating sheet metal panels and the article produced thereby. According to one form, the method of fabrication includes the steps of providing a panel of sheet metal, perforating the panel to provide a plurality of holes, forming the panel into a preselected curve about a longitudinal

대표청구항

A fabricated sheet metal panel comprising: a plate member having first and second oppositely facing surfaces bounded by a leading edge, a trailing edge and first and second opposing side edges; said plate member further comprising an integral shoulder spaced from and extending substantially parallel

이 특허에 인용된 특허 (7)

  1. Snell Leonard Stanley (Bristol EN), Combustion equipment for gas turbine engines.
  2. Caruel ; Jacques E. J. ; Stora ; Guy D., Double-walled combustion chamber shell having combined convective wall cooling and film cooling.
  3. Vogt Robert L. (Schenectady NY), Fuel injection staged sectoral combustor for burning low-BTU fuel gas.
  4. Pane ; Francis C. ; Sepulveda ; Domingo, Louver construction for liner of gas turbine engine combustor.
  5. Vogt Robert L. (Schenectady NY), Sectoral combustor for burning low-BTU fuel gas.
  6. DuBell Thomas L. (Maineville OH), Stabilizing dimple for combustion liner cooling slot.
  7. Ludowici Michael C. (5-7 Josef-Wiesberger Str. D-8013 Haar DEX), Wall facing assembly.

이 특허를 인용한 특허 (30)

  1. Tiemann, Peter, Annular combustion chambers for a gas turbine and gas turbine.
  2. Timothy P. McCaffrey ; Frank A. Lastrina ; Joseph D. Monty ; David E. Hrencecin, Apparatus for reducing heat load in combustor panels.
  3. Chang, Hoyt Y., Ceramic and metal engine components with gradient transition from metal to ceramic.
  4. Pidcock,Anthony; Close,Desmond; Spooner,Michael P, Combustion apparatus.
  5. Tentorio, Luca, Combustion apparatus having a fuel controlled valve that temporarily flows purging air.
  6. Berdou, Caroline Jacqueline Denise; Cameriano, Laurent Bernard, Combustion chamber for a turbine engine.
  7. Bagchi, Imon Kalyan, Combustion chamber of a gas turbine.
  8. Clemen, Carsten, Combustion chamber of a gas turbine.
  9. Gerendás, Miklós; Clemen, Carsten; Doerr, Thomas, Combustion chamber of a gas turbine.
  10. Woerz, Ulrich, Combustor assembly including a transition inlet cone in a gas turbine engine.
  11. Garry, Ian Murray; Carlisle, Michael Lawrence, Combustor wall apparatus with parts joined by mechanical fasteners.
  12. Erbas-Sen, Nurhak; Cunha, Frank J., Combustor wall with tapered cooling cavity.
  13. Bangerter, James P.; Low, Kevin Joseph; Jause, Jonathan M.; Sonntag, Robert; Rezvani, Reza; Kwoka, David, Combustor with grommet having projecting lip.
  14. Vetters, Daniel K., Combustor with tiled liner.
  15. Yankowich, Paul; Xu, Fang, Combustors with inserts between dual wall liners.
  16. Rudrapatna, Nagaraja S.; Frye, Lowell; Landram, William, Combustors with quench inserts.
  17. Rudrapatna, Nagaraja S.; Smalley, Philip; Frye, Lowell; Landram, William, Combustors with quench inserts.
  18. McCaldon Kian,CAX ; Aze Robert Ming Lap,CAX ; Sampath Parthasarathy,CAX, Double pass air impingement and air film cooling for gas turbine combustor walls.
  19. Sze, Robert; Verhiel, Jeffrey Richard, Floatwall dilution hole cooling.
  20. Mitchell, Ian Edward; Clark, Daniel; Tuppen, Stephen John, Gas heater.
  21. Zborovsky, James M.; Heilos, Andreas, Gas turbine: seal between adjacent can annular combustors.
  22. Hessler, William K.; Popovic, Predrag; Nyberg, Charles, Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface.
  23. Farmer, Gilbert; Kutter, Ella Christine; Vise, Steven Clayton; Staker, John Robert; Al-Roub, Marwan; Harris, Tariq Kay, Method and apparatus for cooling gas turbine engine igniter tubes.
  24. Hawtin, Philip Robert; Smith, Michael, Methods and apparatus for manufacturing turbine engine components.
  25. Mc Caffrey, Timothy P.; Lastrina, Frank A.; Monty, Joseph D.; Hrencecin, David E., Methods for reducing heat load in combustor panels.
  26. Malot, Hélène; Guegou, Jean-Pierre; Bienvenu, Philippe; Prunin, Philippe, Nozzle for an aircraft turboprop engine with an unducted fan.
  27. Hughes, Michael John; Berry, Jonathan Dwight, Staged fuel and air injection in combustion systems of gas turbines.
  28. Commaret Patrice (Le Mee s/Seine FRX) Desaulty Michel A. A. (Vert St Denis FRX) Hernandez Didier H. (Ormoy FRX) Laugeois Jean-Claude (Palaiseau FRX) Mandet Grard M. F. (Fericy FRX) Martinez Rodolphe , Turbojet engine combustion chamber with a double wall converging zone.
  29. Hadder,James L., Waffled impingement effusion method.
  30. Anthony Pidcock GB; Desmond Close GB; Michael P. Spooner GB, Wall elements for gas turbine engine combustors.
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