USB377172I5 - - Google Patents

Info

Publication number
USB377172I5
USB377172I5 US37717273A USB377172I5 US B377172 I5 USB377172 I5 US B377172I5 US 37717273 A US37717273 A US 37717273A US B377172 I5 USB377172 I5 US B377172I5
Authority
US
United States
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.)
Pending
Application number
Other languages
English (en)
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
Priority to US377172A priority Critical patent/US3918255A/en
Priority to CA201,013A priority patent/CA1004863A/en
Priority to JP49076534A priority patent/JPS5237126B2/ja
Publication of USB377172I5 publication Critical patent/USB377172I5/en
Application granted granted Critical
Publication of US3918255A publication Critical patent/US3918255A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/045Air inlet arrangements using pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
US377172A 1973-07-06 1973-07-06 Ceramic-lined combustion chamber and means for support of a liner with combustion air penetrations Expired - Lifetime US3918255A (en)

Priority Applications (3)

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
CA201,013A CA1004863A (en) 1973-07-06 1974-05-28 Ceramic-lined combustion chamber and means for support of a liner with combustion air penetrations
JP49076534A JPS5237126B2 (fr) 1973-07-06 1974-07-05

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
USB377172I5 true USB377172I5 (fr) 1975-01-28
US3918255A US3918255A (en) 1975-11-11

Family

ID=23488058

Family Applications (1)

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

Country Status (3)

Country Link
US (1) US3918255A (fr)
JP (1) JPS5237126B2 (fr)
CA (1) CA1004863A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439362A1 (fr) * 1978-10-19 1980-05-16 Mtu Muenchen Gmbh Chambre de combustion pour moteur a turbine a gaz
EP0149474A2 (fr) * 1984-01-13 1985-07-24 Hitachi, Ltd. Chambre de combustion pour turbine à gaz
DE19623300A1 (de) * 1996-06-11 1997-12-18 Siemens Ag Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau

Families Citing this family (44)

* 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
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
JPS57501537A (fr) * 1980-10-07 1982-08-26
US4459101A (en) * 1981-08-28 1984-07-10 Foster-Miller Associates, Inc. Burner systems
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
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
US5553455A (en) * 1987-12-21 1996-09-10 United Technologies Corporation Hybrid ceramic article
US5639531A (en) * 1987-12-21 1997-06-17 United Technologies Corporation Process for making a 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
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 (fr) * 2003-01-27 2004-07-28 Siemens Aktiengesellschaft Bouclier thermique, chambre de combustion et turbine à gaz
US6920836B2 (en) * 2003-10-02 2005-07-26 The Boeing Company Regeneratively cooled synthesis gas generator
EP1528343A1 (fr) * 2003-10-27 2005-05-04 Siemens Aktiengesellschaft Tuile réfractaire avec des éléments de renforcement noyés pour révêtement d'une chambre de combustion de turbines à gaz
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
US8673234B2 (en) * 2008-03-04 2014-03-18 Aerojet Rocketdyne Of De, Inc. Reactor vessel and liner
US7972572B2 (en) * 2008-03-04 2011-07-05 Pratt & Whitney Rocketdyne, 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 (fr) 2013-02-25 2018-10-17 Ansaldo Energia IP UK Limited Procédé de fabrication d'une structure composite métal-céramique et structure composite métal-céramique
US9423129B2 (en) 2013-03-15 2016-08-23 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

Citations (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
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2915877A (en) * 1954-03-03 1959-12-08 Parsons & Marine Eng Turbine Cylindrical furnaces
US3321922A (en) * 1964-10-29 1967-05-30 Jr William T Latto Small rocket engine
US3594109A (en) * 1968-07-27 1971-07-20 Leyland Gass Turbines Ltd Flame tube

Patent Citations (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
US2915877A (en) * 1954-03-03 1959-12-08 Parsons & Marine Eng Turbine Cylindrical furnaces
US3321922A (en) * 1964-10-29 1967-05-30 Jr William T Latto Small rocket engine
US3594109A (en) * 1968-07-27 1971-07-20 Leyland Gass Turbines Ltd Flame tube

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439362A1 (fr) * 1978-10-19 1980-05-16 Mtu Muenchen Gmbh Chambre de combustion pour moteur a turbine a gaz
EP0149474A2 (fr) * 1984-01-13 1985-07-24 Hitachi, Ltd. Chambre de combustion pour turbine à gaz
EP0149474A3 (en) * 1984-01-13 1985-08-07 Hitachi, Ltd. Combustion apparatus for gas turbine
DE19623300A1 (de) * 1996-06-11 1997-12-18 Siemens Ag Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau

Also Published As

Publication number Publication date
JPS5237126B2 (fr) 1977-09-20
US3918255A (en) 1975-11-11
JPS5036818A (fr) 1975-04-07
CA1004863A (en) 1977-02-08

Similar Documents

Publication Publication Date Title
AR201758A1 (fr)
AU465372B2 (fr)
AR201235Q (fr)
JPS5237126B2 (fr)
AU465453B2 (fr)
AU465434B2 (fr)
AU471343B2 (fr)
AU450229B2 (fr)
AU472848B2 (fr)
AU466283B2 (fr)
AR201432A1 (fr)
AU471461B2 (fr)
AR210729A1 (fr)
AU461342B2 (fr)
AU447540B2 (fr)
AR196212Q (fr)
AU1891376A (fr)
AR196123Q (fr)
CH566903A5 (fr)
AU479562A (fr)
CH559141A5 (fr)
CH1632773A4 (fr)
BG22070A3 (fr)
CH562717A5 (fr)
CH563627A5 (fr)