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WO1996008679B1 - Dispositif combustor hybride - Google Patents

Dispositif combustor hybride

Info

Publication number
WO1996008679B1
WO1996008679B1 PCT/US1995/011583 US9511583W WO9608679B1 WO 1996008679 B1 WO1996008679 B1 WO 1996008679B1 US 9511583 W US9511583 W US 9511583W WO 9608679 B1 WO9608679 B1 WO 9608679B1
Authority
WO
WIPO (PCT)
Prior art keywords
combustor
combustors
annular
set forth
fuel
Prior art date
Application number
PCT/US1995/011583
Other languages
English (en)
Other versions
WO1996008679A1 (fr
Filing date
Publication date
Priority claimed from US08/306,090 external-priority patent/US6182451B1/en
Application filed filed Critical
Priority to EP95933085A priority Critical patent/EP0781392A1/fr
Publication of WO1996008679A1 publication Critical patent/WO1996008679A1/fr
Publication of WO1996008679B1 publication Critical patent/WO1996008679B1/fr

Links

Abstract

Un dispositif combustor hybride (10) de moteur à turbine à gaz comporte plusieurs chambres de combustion tubulaire (12) en céramique disposées en cercle dont les sorties communiquent avec l'entrée d'une chambre de combustion métallique annulaire (16). Le processus de combustion se déroule en continu au travers des chambres de combustion tubulaire (12) et de la chambre de combustion annulaire unique (16). Cette combustion est de préférence exclusivement à mélange riche dans chacune des chambres de combustion tubulaires (12), et se poursuit en mélange pauvre dans la chambre de combustion annulaire unique (16).
PCT/US1995/011583 1994-09-14 1995-09-13 Dispositif combustor hybride WO1996008679A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP95933085A EP0781392A1 (fr) 1994-09-14 1995-09-13 Dispositif combustor hybride

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/306,090 1994-09-14
US08/306,090 US6182451B1 (en) 1994-09-14 1994-09-14 Gas turbine combustor waving ceramic combustor cans and an annular metallic combustor

Publications (2)

Publication Number Publication Date
WO1996008679A1 WO1996008679A1 (fr) 1996-03-21
WO1996008679B1 true WO1996008679B1 (fr) 1996-05-09

Family

ID=23183759

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1995/011583 WO1996008679A1 (fr) 1994-09-14 1995-09-13 Dispositif combustor hybride

Country Status (3)

Country Link
US (1) US6182451B1 (fr)
EP (1) EP0781392A1 (fr)
WO (1) WO1996008679A1 (fr)

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US20020157400A1 (en) * 2001-04-27 2002-10-31 Siemens Aktiengesellschaft Gas turbine with combined can-type and annular combustor and method of operating a gas turbine
FR2825787B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Montage de chambre de combustion cmc de turbomachine par viroles de liaison souples
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
EP1288574A1 (fr) * 2001-09-03 2003-03-05 Siemens Aktiengesellschaft Agencement de chambre de combustion
US6495207B1 (en) 2001-12-21 2002-12-17 Pratt & Whitney Canada Corp. Method of manufacturing a composite wall
EP1508761A1 (fr) * 2003-08-22 2005-02-23 Siemens Aktiengesellschaft Pierre servant de bouclier thermique pour garnir une paroi de chambre de combustion, chambre de combustion et turbine a gaz correspondantes
US7043921B2 (en) * 2003-08-26 2006-05-16 Honeywell International, Inc. Tube cooled combustor
US7093441B2 (en) * 2003-10-09 2006-08-22 United Technologies Corporation Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
US20050210862A1 (en) * 2004-03-25 2005-09-29 Paterro Von Friedrich C Quantum jet turbine propulsion system
US7954325B2 (en) * 2005-12-06 2011-06-07 United Technologies Corporation Gas turbine combustor
US7665307B2 (en) * 2005-12-22 2010-02-23 United Technologies Corporation Dual wall combustor liner
US8863528B2 (en) * 2006-07-27 2014-10-21 United Technologies Corporation Ceramic combustor can for a gas turbine engine
US9127565B2 (en) * 2008-04-16 2015-09-08 Siemens Energy, Inc. Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell
EP2233835A1 (fr) * 2009-03-23 2010-09-29 Siemens Aktiengesellschaft Chambre de combustion brasée avec des inserts en céramique
US8745989B2 (en) 2009-04-09 2014-06-10 Pratt & Whitney Canada Corp. Reverse flow ceramic matrix composite combustor
US8739546B2 (en) * 2009-08-31 2014-06-03 United Technologies Corporation Gas turbine combustor with quench wake control
US8443610B2 (en) 2009-11-25 2013-05-21 United Technologies Corporation Low emission gas turbine combustor
US9068751B2 (en) * 2010-01-29 2015-06-30 United Technologies Corporation Gas turbine combustor with staged combustion
US8966877B2 (en) 2010-01-29 2015-03-03 United Technologies Corporation Gas turbine combustor with variable airflow
US8479521B2 (en) 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US9068748B2 (en) 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US9010120B2 (en) 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US8919137B2 (en) 2011-08-05 2014-12-30 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
US9134028B2 (en) * 2012-01-18 2015-09-15 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
EP3015770B1 (fr) * 2014-11-03 2020-07-01 Ansaldo Energia Switzerland AG Chambre de combustion de caisson
US9810434B2 (en) * 2016-01-21 2017-11-07 Siemens Energy, Inc. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine

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GB588572A (en) * 1944-11-28 1947-05-28 William Henry Darlington Improvements in combustion chambers for internal combustion turbines
US2447482A (en) 1945-04-25 1948-08-24 Westinghouse Electric Corp Turbine apparatus
US2446013A (en) 1945-05-31 1948-07-27 Gen Electric Combustion chamber drain arrangement
US2885858A (en) * 1947-12-02 1959-05-12 Power Jets Res & Dev Ltd Combustion system with mixing chamber
US2676460A (en) * 1950-03-23 1954-04-27 United Aircraft Corp Burner construction of the can-an-nular type having means for distributing airflow to each can
SU151158A1 (ru) * 1961-04-21 1961-11-30 тский З.М. Св Камера сгорани
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube
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US3990231A (en) 1974-10-24 1976-11-09 General Motors Corporation Interconnections between ceramic rings permitting relative radial movement
EP0193029B1 (fr) * 1985-02-26 1988-11-17 BBC Brown Boveri AG Chambre de combustion pour turbines à gaz
DE3519938A1 (de) * 1985-06-04 1986-12-04 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Brennkammereinrichtung
DE3615226A1 (de) * 1986-05-06 1987-11-12 Mtu Muenchen Gmbh Heissgasueberhitzungsschutzeinrichtung fuer gasturbinentriebwerke
US5285632A (en) * 1993-02-08 1994-02-15 General Electric Company Low NOx combustor

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