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특허 상세정보

Combustion chamber construction

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/20   
미국특허분류(USC) 60/3932 ; 60/752
출원번호 US-0316530 (1972-12-19)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 33  인용 특허 : 1

A combustion chamber for use in gas turbine engines is provided with a liner formed of a high temperature material. The liner includes a plurality of panels of the material mounted by means of a slideable friction mounting arrangement upon a high strength structural frame. As a result of this mounting arrangement, the liner is substantially isolated from structural forces associated with the combustion chamber, while the frame is substantially isolated from thermal stresses associated with the liner. Means are provided for positioning and securing indivi...


A combustion chamber for use in gas turbine engines, the chamber comprising: an inlet for receiving air and fuel to be burned; an outlet for expelling products of combustion; high strength structural frame means disposed between the inlet and the outlet for supporting mechanical forces associated with the chamber; liner means cooperating with the frame and defining a combustion zone, said liner means including a plurality of panels of high temperature materials; circumferential mounting means for positioning said panels laterally with respect to one anot...

이 특허를 인용한 특허 피인용횟수: 33

  1. Tiemann, Peter. Annular combustion chambers for a gas turbine and gas turbine. USP2005096938424.
  2. Bell Lance P.,GB3 ; Gater Neil,GB3 ; Pidcock Anthony,GB3 ; Close Desmond,GB3 ; Cross Simon,GB3. Arrangement of heat resistant tiles for a gas turbine engine combustor. USP1998095799491.
  3. Davenport, Nigel Caldwell; Hawie, Eduardo David. Asymmetric combustor heat shield panels. USP2017019534784.
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  7. Barbier Grard Y. G. (Morangis FRX) Laboure Grard J. P. B. (Avon FRX) Desaulty Michel A. A. (Vert-Saint-Denis FRX) Duchene Francois (Melun FRX) Truvillot Pascal M. (Courbevoie FRX). Combustion chamber structure for a turbojet engine. USP1989024805397.
  8. Harding, Stephen Charles. Combustion chamber wall and a method of manufacturing a combustion chamber wall. USP20190410260749.
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  11. Stastny, Honza; Sze, Robert. Combustor skin assembly for gas turbine engine. USP2017059657949.
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  14. Nguyen, Ly D.; Woodcock, Gregory O.; Kujala, Stony. Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engine. USP2005076912782.
  15. Coutandin, Daniele. Gas turbine combustor, particularly for an aircraft engine. USP2004116810672.
  16. Rice, Edward Claude; Rau, Naveen; Koth, Robert C. Gas turbine engine flange assembly including flow circuit. USP2014128899051.
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  21. Davenport, Nigel Caldwell; Hawie, Eduardo David. Interlocking combustor heat shield panels. USP2015038984896.
  22. Kuhn,Terrel E.; Freeman,William G.; Maszk,Francis S.; Freiberg,Douglas P.; Struzek,Kenneth A.; Kobold,Lawrence A.. Method for controlling carbon formation on repaired combustor liners. USP2006107124487.
  23. Czachor, Robert P.. Methods and apparatus for assembling gas turbine engines. USP2005106951112.
  24. Czachor, Robert P.; Groeschen, James Anthony; Hoppa, Jason Paul. Methods and apparatuses for assembling a gas turbine engine. USP2009127637110.
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  26. Moertle,George E.; Emilianowicz,Edward John; Pelletier,Scott Howard. Methods for replacing combustor liners. USP2006016986201.
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  29. Murphy, Michael Joseph; Lavin, Jeffrey R.. Recoatable exhaust liner cooling arrangement. USP2012038127526.
  30. Rubio, Mark B.; Ritland, David M.. Segmented annular combustor. USP2011017874138.
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  33. Bird, Connie E.; Prill, Lisa A.. Simple CMC fastening system. USP2013108556531.