SE8102132L - Brennarinsatskonstruktion for gasturbiner - Google Patents

Brennarinsatskonstruktion for gasturbiner

Info

Publication number
SE8102132L
SE8102132L SE8102132A SE8102132A SE8102132L SE 8102132 L SE8102132 L SE 8102132L SE 8102132 A SE8102132 A SE 8102132A SE 8102132 A SE8102132 A SE 8102132A SE 8102132 L SE8102132 L SE 8102132L
Authority
SE
Sweden
Prior art keywords
construction
flow
turbiner
counter
gas
Prior art date
Application number
SE8102132A
Other languages
English (en)
Other versions
SE453221B (sv
Inventor
T L Dubell
Original Assignee
United Technologies Corp
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 by United Technologies Corp filed Critical United Technologies Corp
Publication of SE8102132L publication Critical patent/SE8102132L/sv
Publication of SE453221B publication Critical patent/SE453221B/sv

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
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/221—Improvement of heat transfer
    • F05B2260/224—Improvement of heat transfer by increasing the heat transfer surface
    • F05B2260/2241—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
SE8102132A 1980-04-02 1981-04-02 Brennkammarfoder for gasturbinmotor SE453221B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/136,631 US4302941A (en) 1980-04-02 1980-04-02 Combuster liner construction for gas turbine engine

Publications (2)

Publication Number Publication Date
SE8102132L true SE8102132L (sv) 1981-10-03
SE453221B SE453221B (sv) 1988-01-18

Family

ID=22473671

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8102132A SE453221B (sv) 1980-04-02 1981-04-02 Brennkammarfoder for gasturbinmotor

Country Status (9)

Country Link
US (1) US4302941A (sv)
JP (1) JPS56168038A (sv)
BE (1) BE888246A (sv)
DE (1) DE3113379A1 (sv)
FR (1) FR2479901B1 (sv)
GB (1) GB2074307B (sv)
IL (1) IL62556A (sv)
NO (1) NO151434C (sv)
SE (1) SE453221B (sv)

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US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
US4653279A (en) * 1985-01-07 1987-03-31 United Technologies Corporation Integral refilmer lip for floatwall panels
US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means
DE3535442A1 (de) * 1985-10-04 1987-04-09 Mtu Muenchen Gmbh Ringbrennkammer fuer gasturbinentriebwerke
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US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
US4916906A (en) * 1988-03-25 1990-04-17 General Electric Company Breach-cooled structure
US4887663A (en) * 1988-05-31 1989-12-19 United Technologies Corporation Hot gas duct liner
US4921401A (en) * 1989-02-23 1990-05-01 United Technologies Corporation Casting for a rotary machine
US4955202A (en) * 1989-03-12 1990-09-11 Sundstrand Corporation Hot gas generator
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
FR2668246B1 (fr) * 1990-10-17 1994-12-09 Snecma Chambre de combustion munie d'un dispositif de refroidissement de sa paroi.
US5144793A (en) * 1990-12-24 1992-09-08 United Technologies Corporation Integrated connector/airtube for a turbomachine's combustion chamber walls
US5129447A (en) * 1991-05-20 1992-07-14 United Technologies Corporation Cooled bolting arrangement
US5201799A (en) * 1991-05-20 1993-04-13 United Technologies Corporation Clip attachment for combustor panel
US5216886A (en) * 1991-08-14 1993-06-08 The United States Of America As Represented By The Secretary Of The Air Force Segmented cell wall liner for a combustion chamber
DE4223733C2 (de) * 1992-07-18 1995-05-18 Gutehoffnungshuette Man Verbindung von Mischrohr und Flammrohr einer Gasturbine
US5323601A (en) * 1992-12-21 1994-06-28 United Technologies Corporation Individually removable combustor liner panel for a gas turbine engine
DE4335413A1 (de) * 1993-10-18 1995-04-20 Abb Management Ag Verfahren und Vorrichtung zur Kühlung einer Gasturbinenbrennkammer
FR2714152B1 (fr) * 1993-12-22 1996-01-19 Snecma Dispositif de fixation d'une tuile de protection thermique dans une chambre de combustion.
US5533330A (en) * 1993-12-27 1996-07-09 United Technologies Corporation Ignitor plug guide for a gas turbine engine combustor
US5542246A (en) * 1994-12-15 1996-08-06 United Technologies Corporation Bulkhead cooling fairing
US5461866A (en) * 1994-12-15 1995-10-31 United Technologies Corporation Gas turbine engine combustion liner float wall cooling arrangement
US5758503A (en) * 1995-05-03 1998-06-02 United Technologies Corporation Gas turbine combustor
DE19547703C2 (de) 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Brennkammer, insbesondere Ringbrennkammer, für Gasturbinentriebwerke
DE19631616A1 (de) * 1996-08-05 1998-02-12 Asea Brown Boveri Brennkammer
GB9919981D0 (en) * 1999-08-24 1999-10-27 Rolls Royce Plc Combustion apparatus
DE10114619B4 (de) * 2000-03-27 2006-07-27 Cummins Inc., Columbus Belüftendes Befestigungselement
IT1317538B1 (it) * 2000-05-15 2003-07-09 Nuovo Pignone Spa Dispositivo per il controllo dei flussi di refrigerazione delleturbine a gas
US6701714B2 (en) 2001-12-05 2004-03-09 United Technologies Corporation Gas turbine combustor
US6910853B2 (en) * 2002-11-27 2005-06-28 General Electric Company Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
CA2476803C (en) 2003-08-14 2010-10-26 Mitsubishi Heavy Industries, Ltd. Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine
US7578134B2 (en) * 2006-01-11 2009-08-25 General Electric Company Methods and apparatus for assembling gas turbine engines
EP1813869A3 (en) * 2006-01-25 2013-08-14 Rolls-Royce plc Wall elements for gas turbine engine combustors
US7726131B2 (en) * 2006-12-19 2010-06-01 Pratt & Whitney Canada Corp. Floatwall dilution hole cooling
JP4823186B2 (ja) * 2007-09-25 2011-11-24 三菱重工業株式会社 ガスタービン燃焼器
US8056342B2 (en) * 2008-06-12 2011-11-15 United Technologies Corporation Hole pattern for gas turbine combustor
US8161752B2 (en) * 2008-11-20 2012-04-24 Honeywell International Inc. Combustors with inserts between dual wall liners
US20100263386A1 (en) * 2009-04-16 2010-10-21 General Electric Company Turbine engine having a liner
US8359866B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US8359865B2 (en) 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US9010123B2 (en) 2010-07-26 2015-04-21 Honeywell International Inc. Combustors with quench inserts
JPWO2012161142A1 (ja) * 2011-05-24 2014-07-31 三菱重工業株式会社 中空湾曲板及びその製造方法ならびにガスタービンの燃焼器
US9062884B2 (en) 2011-05-26 2015-06-23 Honeywell International Inc. Combustors with quench inserts
GB201116608D0 (en) * 2011-09-27 2011-11-09 Rolls Royce Plc A method of operating a combustion chamber
US9038395B2 (en) 2012-03-29 2015-05-26 Honeywell International Inc. Combustors with quench inserts
US8910378B2 (en) * 2012-05-01 2014-12-16 United Technologies Corporation Method for working of combustor float wall panels
DE102012022259A1 (de) * 2012-11-13 2014-05-28 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung
US10415477B2 (en) * 2013-07-31 2019-09-17 General Electric Company Turbine casing false flange flow diverter
WO2015030927A1 (en) * 2013-08-30 2015-03-05 United Technologies Corporation Contoured dilution passages for a gas turbine engine combustor
WO2015038232A1 (en) * 2013-09-13 2015-03-19 United Technologies Corporation Sealed combustor liner panel for a gas turbine engine
EP3066387B1 (en) * 2013-11-04 2019-10-02 United Technologies Corporation Assembly for a turbine engine with acombustor comprising a quench air aperture
US10197285B2 (en) * 2013-12-06 2019-02-05 United Technologies Corporation Gas turbine engine wall assembly interface
WO2015085069A1 (en) 2013-12-06 2015-06-11 United Technologies Corporation Combustor quench aperture cooling
EP3084307B1 (en) * 2013-12-19 2018-10-24 United Technologies Corporation Dilution passage arrangement for gas turbine engine combustor
EP3102883B1 (en) * 2014-02-03 2020-04-01 United Technologies Corporation Film cooling a combustor wall of a turbine engine
WO2015117139A1 (en) * 2014-02-03 2015-08-06 United Technologies Corporation Stepped heat shield for a turbine engine combustor
FR3017928B1 (fr) * 2014-02-27 2019-07-26 Safran Aircraft Engines Turbomachine a bride externe de chambre de combustion de type "sandwich"
US10012385B2 (en) * 2014-08-08 2018-07-03 Pratt & Whitney Canada Corp. Combustor heat shield sealing
JP6521283B2 (ja) * 2014-09-25 2019-05-29 三菱日立パワーシステムズ株式会社 燃焼器、ガスタービン
US10018064B2 (en) 2015-03-02 2018-07-10 United Technologies Corporation Floating panel for a gas powered turbine
US20160258623A1 (en) * 2015-03-05 2016-09-08 United Technologies Corporation Combustor and heat shield configurations for a gas turbine engine
US10094564B2 (en) * 2015-04-17 2018-10-09 Pratt & Whitney Canada Corp. Combustor dilution hole cooling system
GB201518345D0 (en) * 2015-10-16 2015-12-02 Rolls Royce Combustor for a gas turbine engine
GB2545459B (en) * 2015-12-17 2020-05-06 Rolls Royce Plc A combustion chamber
US10344978B2 (en) * 2016-03-15 2019-07-09 General Electric Company Combustion liner cooling
US10443846B2 (en) * 2016-04-21 2019-10-15 United Technologies Corporation Combustor thermal shield fabrication method
GB201613110D0 (en) 2016-07-29 2016-09-14 Rolls Royce Plc A combustion chamber
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10655853B2 (en) 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10830433B2 (en) 2016-11-10 2020-11-10 Raytheon Technologies Corporation Axial non-linear interface for combustor liner panels in a gas turbine combustor
US20180283689A1 (en) * 2017-04-03 2018-10-04 General Electric Company Film starters in combustors of gas turbine engines
US11022308B2 (en) 2018-05-31 2021-06-01 Honeywell International Inc. Double wall combustors with strain isolated inserts
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine
US11560843B2 (en) 2020-02-25 2023-01-24 General Electric Company Frame for a heat engine
US11255264B2 (en) 2020-02-25 2022-02-22 General Electric Company Frame for a heat engine
US11566787B2 (en) 2020-04-06 2023-01-31 Rolls-Royce Corporation Tile attachment scheme for counter swirl doublet
US11867402B2 (en) * 2021-03-19 2024-01-09 Rtx Corporation CMC stepped combustor liner

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Also Published As

Publication number Publication date
NO151434C (no) 1985-04-10
DE3113379A1 (de) 1982-05-06
IL62556A (en) 1984-10-31
IL62556A0 (en) 1981-06-29
JPH0229936B2 (sv) 1990-07-03
GB2074307B (en) 1983-10-12
BE888246A (fr) 1981-07-31
DE3113379C2 (sv) 1990-05-17
FR2479901B1 (fr) 1986-12-05
GB2074307A (en) 1981-10-28
NO811129L (no) 1981-10-05
FR2479901A1 (fr) 1981-10-09
US4302941A (en) 1981-12-01
SE453221B (sv) 1988-01-18
NO151434B (no) 1984-12-27
JPS56168038A (en) 1981-12-24

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