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FR2018565A1 - - Google Patents

Info

Publication number
FR2018565A1
FR2018565A1 FR6932136A FR6932136A FR2018565A1 FR 2018565 A1 FR2018565 A1 FR 2018565A1 FR 6932136 A FR6932136 A FR 6932136A FR 6932136 A FR6932136 A FR 6932136A FR 2018565 A1 FR2018565 A1 FR 2018565A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6932136A
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of FR2018565A1 publication Critical patent/FR2018565A1/fr
Withdrawn legal-status Critical Current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
    • F23R3/06Arrangement of apertures along the flame tube
    • 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
    • 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
    • F23R3/26Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR6932136A 1968-09-20 1969-09-22 Withdrawn FR2018565A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB44805/68A GB1278590A (en) 1968-09-20 1968-09-20 Combustion chambers for gas turbine engines

Publications (1)

Publication Number Publication Date
FR2018565A1 true FR2018565A1 (en) 1970-05-29

Family

ID=10434833

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6932136A Withdrawn FR2018565A1 (en) 1968-09-20 1969-09-22

Country Status (4)

Country Link
US (1) US3593518A (en)
FR (1) FR2018565A1 (en)
GB (1) GB1278590A (en)
SE (1) SE357028B (en)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859786A (en) * 1972-05-25 1975-01-14 Ford Motor Co Combustor
US3814575A (en) * 1973-04-25 1974-06-04 Us Air Force Combustion device
US4021186A (en) * 1974-06-19 1977-05-03 Exxon Research And Engineering Company Method and apparatus for reducing NOx from furnaces
GB1481617A (en) * 1974-10-07 1977-08-03 Rolls Royce Gas turbine fuel burners
DE2452178C3 (en) * 1974-11-02 1981-05-07 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Combustion chamber for gas turbine engines
DE2545234C2 (en) * 1975-10-09 1983-09-15 Fa. J. Eberspächer, 7300 Esslingen Mixing device for burners
US4052144A (en) * 1976-03-31 1977-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Fuel combustor
DE2839627C2 (en) * 1977-09-13 1983-11-03 Hitachi, Ltd., Tokyo Gas burner
US4276018A (en) * 1979-05-30 1981-06-30 Davey Compressor Co. Mobile heater
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
FR2674317B1 (en) * 1991-03-20 1993-05-28 Snecma COMBUSTION CHAMBER OF A TURBOMACHINE COMPRISING AN ADJUSTMENT OF THE FUEL FLOW.
US5289686A (en) * 1992-11-12 1994-03-01 General Motors Corporation Low nox gas turbine combustor liner with elliptical apertures for air swirling
US5322026A (en) * 1992-12-21 1994-06-21 Bay Il H Waste combustion chamber with tertiary burning zone
GB9726697D0 (en) 1997-12-18 1998-02-18 Secr Defence Fuel injector
US20060130486A1 (en) * 2004-12-17 2006-06-22 Danis Allen M Method and apparatus for assembling gas turbine engine combustors
DE102006041955A1 (en) * 2006-08-30 2008-03-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for controlling combustion in a combustion chamber and combustion chamber device
US8171740B2 (en) * 2009-02-27 2012-05-08 Honeywell International Inc. Annular rich-quench-lean gas turbine combustors with plunged holes
US8141365B2 (en) * 2009-02-27 2012-03-27 Honeywell International Inc. Plunged hole arrangement for annular rich-quench-lean gas turbine combustors
US20100242483A1 (en) * 2009-03-30 2010-09-30 United Technologies Corporation Combustor for gas turbine engine
US9222674B2 (en) * 2011-07-21 2015-12-29 United Technologies Corporation Multi-stage amplification vortex mixture for gas turbine engine combustor
CN103032891B (en) * 2013-01-04 2015-07-29 中国科学院工程热物理研究所 A kind of many eddy combustion methods
US20140190171A1 (en) * 2013-01-10 2014-07-10 Honeywell International Inc. Combustors with hybrid walled liners
CA2820365C (en) * 2013-06-25 2021-03-23 Unique Gas Products Ltd. Direct venting system for free-standing propane powered absorption refrigerator
EP3039340B1 (en) * 2013-08-30 2018-11-28 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
US11112115B2 (en) * 2013-08-30 2021-09-07 Raytheon Technologies Corporation Contoured dilution passages for gas turbine engine combustor
US10451281B2 (en) * 2014-11-04 2019-10-22 United Technologies Corporation Low lump mass combustor wall with quench aperture(s)
DE102016201452A1 (en) * 2016-02-01 2017-08-03 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor with wall contouring
US20180283695A1 (en) * 2017-04-03 2018-10-04 United Technologies Corporation Combustion panel grommet
US11959643B2 (en) * 2021-06-07 2024-04-16 General Electric Company Combustor for a gas turbine engine
US12222104B2 (en) * 2022-03-21 2025-02-11 General Electric Company Turbine engine combustor and combustor liner

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB738006A (en) * 1952-07-12 1955-10-05 Rolls Royce Improvements in or relating to gas turbine engines
US2807933A (en) * 1954-04-01 1957-10-01 Martin Peter Combustion chambers
US2841182A (en) * 1955-12-29 1958-07-01 Westinghouse Electric Corp Boundary layer fluid control apparatus
GB1075958A (en) * 1966-04-29 1967-07-19 Rolls Royce Gas turbine engine

Also Published As

Publication number Publication date
DE1947762A1 (en) 1970-04-02
GB1278590A (en) 1972-06-21
SE357028B (en) 1973-06-12
US3593518A (en) 1971-07-20
DE1947762B2 (en) 1975-07-24

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Legal Events

Date Code Title Description
ST Notification of lapse