JPS5237126B2 - - Google Patents

Info

Publication number
JPS5237126B2
JPS5237126B2 JP49076534A JP7653474A JPS5237126B2 JP S5237126 B2 JPS5237126 B2 JP S5237126B2 JP 49076534 A JP49076534 A JP 49076534A JP 7653474 A JP7653474 A JP 7653474A JP S5237126 B2 JPS5237126 B2 JP S5237126B2
Authority
JP
Japan
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP49076534A
Other languages
Japanese (ja)
Other versions
JPS5036818A (en:Method
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of JPS5036818A publication Critical patent/JPS5036818A/ja
Publication of JPS5237126B2 publication Critical patent/JPS5237126B2/ja
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
JP49076534A 1973-07-06 1974-07-05 Expired JPS5237126B2 (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US377172A US3918255A (en) 1973-07-06 1973-07-06 Ceramic-lined combustion chamber and means for support of a liner with combustion air penetrations

Publications (2)

Publication Number Publication Date
JPS5036818A JPS5036818A (en:Method) 1975-04-07
JPS5237126B2 true JPS5237126B2 (en:Method) 1977-09-20

Family

ID=23488058

Family Applications (1)

Application Number Title Priority Date Filing Date
JP49076534A Expired JPS5237126B2 (en:Method) 1973-07-06 1974-07-05

Country Status (3)

Country Link
US (1) US3918255A (en:Method)
JP (1) JPS5237126B2 (en:Method)
CA (1) CA1004863A (en:Method)

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4174608A (en) * 1972-08-15 1979-11-20 Stal-Laval Turbin Ab Combustion chamber for a gas turbine
US3981142A (en) * 1974-04-01 1976-09-21 General Motors Corporation Ceramic combustion liner
US4073137A (en) * 1976-06-02 1978-02-14 United Technologies Corporation Convectively cooled flameholder for premixed burner
US4118925A (en) * 1977-02-24 1978-10-10 Carmel Energy, Inc. Combustion chamber and thermal vapor stream producing apparatus and method
DE2845588A1 (de) * 1978-10-19 1980-04-24 Motoren Turbinen Union Brennkammer fuer gasturbinentriebwerke
US4380896A (en) * 1980-09-22 1983-04-26 The United States Of America As Represented By The Secretary Of The Army Annular combustor having ceramic liner
US4459101A (en) * 1981-08-28 1984-07-10 Foster-Miller Associates, Inc. Burner systems
EP0061494B1 (en) * 1980-10-07 1988-01-20 Foster-Miller Associates, Inc. Thermal enhancement
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine
US4787208A (en) * 1982-03-08 1988-11-29 Westinghouse Electric Corp. Low-nox, rich-lean combustor
US4485630A (en) * 1982-12-08 1984-12-04 General Electric Company Combustor liner
DE3328485A1 (de) * 1983-08-06 1985-02-14 Motan Gmbh, 7972 Isny Schwingbrenner
US4655044A (en) * 1983-12-21 1987-04-07 United Technologies Corporation Coated high temperature combustor liner
JPS60149828A (ja) * 1984-01-13 1985-08-07 Hitachi Ltd 燃焼器
USH140H (en) 1985-04-18 1986-10-07 The United States Of America As Represented By The Secretary Of The Air Force Carbon/carbon combustor external insulation
JPS63243630A (ja) * 1987-03-30 1988-10-11 Tokyo Electric Power Co Inc:The ガスタ−ビン燃焼器
US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
US4838030A (en) * 1987-08-06 1989-06-13 Avco Corporation Combustion chamber liner having failure activated cooling and dectection system
US5639531A (en) * 1987-12-21 1997-06-17 United Technologies Corporation Process for making a hybrid ceramic article
US5553455A (en) * 1987-12-21 1996-09-10 United Technologies Corporation Hybrid ceramic article
AT394768B (de) * 1990-11-02 1992-06-25 Chamottewaren U Thonoefenfabri Brennerflammenfuehrungsteil
US5184455A (en) * 1991-07-09 1993-02-09 The United States Of America As Represented By The Secretary Of The Air Force Ceramic blanket augmentor liner
US5687572A (en) * 1992-11-02 1997-11-18 Alliedsignal Inc. Thin wall combustor with backside impingement cooling
US5291733A (en) * 1993-02-08 1994-03-08 General Electric Company Liner mounting assembly
DE4343319A1 (de) * 1993-12-18 1995-06-22 Abb Patent Gmbh Brennkammer mit keramischer Auskleidung
US5636508A (en) * 1994-10-07 1997-06-10 Solar Turbines Incorporated Wedge edge ceramic combustor tile
GB2298267B (en) * 1995-02-23 1999-01-13 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor
US5749229A (en) * 1995-10-13 1998-05-12 General Electric Company Thermal spreading combustor liner
DE19623300A1 (de) * 1996-06-11 1997-12-18 Siemens Ag Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau
US6014855A (en) * 1997-04-30 2000-01-18 Stewart & Stevenson Services, Inc. Light hydrocarbon fuel cooling system for gas turbine
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine
US6495207B1 (en) 2001-12-21 2002-12-17 Pratt & Whitney Canada Corp. Method of manufacturing a composite wall
EP1441180A1 (de) * 2003-01-27 2004-07-28 Siemens Aktiengesellschaft Hitzeschildelement, Brennkammer sowie Gasturbine
US6920836B2 (en) * 2003-10-02 2005-07-26 The Boeing Company Regeneratively cooled synthesis gas generator
EP1528343A1 (de) * 2003-10-27 2005-05-04 Siemens Aktiengesellschaft Keramischer Hitzeschildstein mit eingebetteten Verstärkungselementen zur Auskleidung einer Gasturbinenbrennkammerwand
CZ15297U1 (cs) * 2005-02-24 2005-04-04 Dis-R S. R. O. Ústí spalovacího hořáku
US7740671B2 (en) * 2006-12-18 2010-06-22 Pratt & Whitney Rocketdyne, Inc. Dump cooled gasifier
US7731783B2 (en) * 2007-01-24 2010-06-08 Pratt & Whitney Rocketdyne, Inc. Continuous pressure letdown system
US8771604B2 (en) * 2007-02-06 2014-07-08 Aerojet Rocketdyne Of De, Inc. Gasifier liner
US7972572B2 (en) * 2008-03-04 2011-07-05 Pratt & Whitney Rocketdyne, Inc. Reactor vessel and liner
US8673234B2 (en) * 2008-03-04 2014-03-18 Aerojet Rocketdyne Of De, Inc. Reactor vessel and liner
GB0913580D0 (en) * 2009-08-05 2009-09-16 Rolls Royce Plc Combustor tile
US9341118B2 (en) * 2009-12-29 2016-05-17 Rolls-Royce Corporation Various layered gas turbine engine component constructions
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
EP2769969B1 (en) 2013-02-25 2018-10-17 Ansaldo Energia IP UK Limited Method for manufacturing a metal-ceramic composite structure and metal-ceramic composite structure
US9651258B2 (en) 2013-03-15 2017-05-16 Rolls-Royce Corporation Shell and tiled liner arrangement for a combustor
GB2540769A (en) * 2015-07-27 2017-02-01 Rolls Royce Plc Combustor for a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544538A (en) * 1948-12-01 1951-03-06 Wright Aeronautical Corp Liner for hot gas chambers
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
GB758213A (en) * 1954-03-03 1956-10-03 Parsons & Marine Eng Turbine Improvements in and relating to cylindrical combustion chambers or furnaces
US3321922A (en) * 1964-10-29 1967-05-30 Jr William T Latto Small rocket engine
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube

Also Published As

Publication number Publication date
US3918255A (en) 1975-11-11
JPS5036818A (en:Method) 1975-04-07
USB377172I5 (en:Method) 1975-01-28
CA1004863A (en) 1977-02-08

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