GB1467499A - Combustion apparatus - Google Patents

Combustion apparatus

Info

Publication number
GB1467499A
GB1467499A GB5374074A GB5374074A GB1467499A GB 1467499 A GB1467499 A GB 1467499A GB 5374074 A GB5374074 A GB 5374074A GB 5374074 A GB5374074 A GB 5374074A GB 1467499 A GB1467499 A GB 1467499A
Authority
GB
United Kingdom
Prior art keywords
air
chamber
slots
fuel
fed
Prior art date
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
GB5374074A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB1467499A publication Critical patent/GB1467499A/en
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
    • F23R3/26—Controlling the air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • F05D2250/411—Movement of components with one degree of freedom in rotation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1467499 Gas turbine combustion chamber GENERAL MOTORS CORP 12 Dec 1974 [4 Feb 1974] 53740/74 Heading F1L A combustion chamber for a gas turbine engine includes a liner 11 defining in sequence an upstream pre-chamber 27 in which liquid fuel is vaporized and mixed with air, a combustion zone 23, and a dilution zone 24, fuel being fed to the pre-chamber 27 through tangential slots 54 around its periphery from a manifold 46 encircling the pre-chamber and enclosed by a cooling air jacket 48, the liquid fuel forming a layer on the inner surface of the liner wall which is formed with intersecting helical grooves to facilitate vaporization. A heat shield 39 surrounds the cooling jacket. Air is fed to the prechamber via swirl blades 30 to vaporize and mix with the layer of liquid fuel. Further primary air is admitted to the pre-chamber via slots 60, and dilution air is fed to zone 24 via slots 70, both sets of slots being progressively covered or uncovered by valve sleeves 66, 71 respectively, to vary the ratio of primary air to secondary air. The sleeves may move together, as shown, or, Fig. 12, (not shown), slots 60 may be replaced by holes (122) not provided with adjustment means. The engine may be started with gaseous fuel or, as shown, by fuel sprayed through a nozzle 110 at the centre of the swirl vanes.
GB5374074A 1974-02-04 1974-12-12 Combustion apparatus Expired GB1467499A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US439648A US3859787A (en) 1974-02-04 1974-02-04 Combustion apparatus

Publications (1)

Publication Number Publication Date
GB1467499A true GB1467499A (en) 1977-03-16

Family

ID=23745561

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5374074A Expired GB1467499A (en) 1974-02-04 1974-12-12 Combustion apparatus

Country Status (8)

Country Link
US (1) US3859787A (en)
JP (1) JPS5825931B2 (en)
CA (1) CA1013153A (en)
DE (1) DE2460709C2 (en)
FR (1) FR2259989B1 (en)
GB (1) GB1467499A (en)
IT (1) IT1026493B (en)
SE (1) SE393839B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0035869A1 (en) * 1980-03-05 1981-09-16 Hitachi, Ltd. A gas turbine combustor

Families Citing this family (64)

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FR2253389A5 (en) * 1973-12-04 1975-06-27 France Etat
US3925002A (en) * 1974-11-11 1975-12-09 Gen Motors Corp Air preheating combustion apparatus
US3930368A (en) * 1974-12-12 1976-01-06 General Motors Corporation Combustion liner air valve
US3938324A (en) * 1974-12-12 1976-02-17 General Motors Corporation Premix combustor with flow constricting baffle between combustion and dilution zones
US3958416A (en) * 1974-12-12 1976-05-25 General Motors Corporation Combustion apparatus
US4045956A (en) * 1974-12-18 1977-09-06 United Technologies Corporation Low emission combustion chamber
US3973395A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Low emission combustion chamber
US4058977A (en) * 1974-12-18 1977-11-22 United Technologies Corporation Low emission combustion chamber
DE2629761A1 (en) * 1976-07-02 1978-01-05 Volkswagenwerk Ag COMBUSTION CHAMBER FOR GAS TURBINES
GB1592858A (en) * 1977-01-21 1981-07-08 Rolls Royce Combustion equipment for gas turbine engines
US4246757A (en) * 1979-03-27 1981-01-27 General Electric Company Combustor including a cyclone prechamber and combustion process for gas turbines fired with liquid fuel
US4269466A (en) * 1979-11-23 1981-05-26 Amp Incorporated Connector and strain relief for flat transmission cable
US4263780A (en) * 1979-09-28 1981-04-28 General Motors Corporation Lean prechamber outflow combustor with sets of primary air entrances
DE2949388A1 (en) * 1979-12-07 1981-06-11 Kraftwerk Union AG, 4330 Mülheim COMBUSTION CHAMBER FOR GAS TURBINES AND METHOD FOR OPERATING THE COMBUSTION CHAMBER
FR2471480A1 (en) * 1979-12-13 1981-06-19 Snecma INJECTION DEVICE FOR A COMBUSTION CHAMBER FOR A TURBINE ENGINE
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
US4467610A (en) * 1981-04-17 1984-08-28 General Electric Company Gas turbine fuel system
US4404806A (en) * 1981-09-04 1983-09-20 General Motors Corporation Gas turbine prechamber and fuel manifold structure
DE3209135A1 (en) * 1982-03-12 1983-09-15 Kraftwerk Union AG, 4330 Mülheim GAS TURBINE COMBUSTION CHAMBER
JP2644745B2 (en) * 1987-03-06 1997-08-25 株式会社日立製作所 Gas turbine combustor
JPH0816531B2 (en) * 1987-04-03 1996-02-21 株式会社日立製作所 Gas turbine combustor
JP2516822Y2 (en) * 1988-08-04 1996-11-13 川崎重工業株式会社 Gas turbine combustor
DE4435266A1 (en) * 1994-10-01 1996-04-04 Abb Management Ag burner
US5669218A (en) * 1995-05-31 1997-09-23 Dresser-Rand Company Premix fuel nozzle
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
GB2351343A (en) 1999-06-22 2000-12-27 Alstom Gas Turbines Ltd Telescopically-moveable combustion chamber
US6539721B2 (en) * 2001-07-10 2003-04-01 Pratt & Whitney Canada Corp. Gas-liquid premixer
SE523082C2 (en) * 2001-11-20 2004-03-23 Volvo Aero Corp Device at a combustion chamber of a gas turbine for controlling gas inflow to the combustion zone of the combustion chamber
US7028484B2 (en) 2002-08-30 2006-04-18 Pratt & Whitney Canada Corp. Nested channel ducts for nozzle construction and the like
US7654088B2 (en) 2004-02-27 2010-02-02 Pratt & Whitney Canada Corp. Dual conduit fuel manifold for gas turbine engine
US20060156733A1 (en) 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US7565807B2 (en) 2005-01-18 2009-07-28 Pratt & Whitney Canada Corp. Heat shield for a fuel manifold and method
US7533531B2 (en) 2005-04-01 2009-05-19 Pratt & Whitney Canada Corp. Internal fuel manifold with airblast nozzles
US7540157B2 (en) 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US7559201B2 (en) 2005-09-08 2009-07-14 Pratt & Whitney Canada Corp. Redundant fuel manifold sealing arrangement
DE102005062079A1 (en) * 2005-12-22 2007-07-12 Rolls-Royce Deutschland Ltd & Co Kg Magervormic burner with a nebulizer lip
US7607226B2 (en) 2006-03-03 2009-10-27 Pratt & Whitney Canada Corp. Internal fuel manifold with turned channel having a variable cross-sectional area
US7854120B2 (en) 2006-03-03 2010-12-21 Pratt & Whitney Canada Corp. Fuel manifold with reduced losses
US7942002B2 (en) 2006-03-03 2011-05-17 Pratt & Whitney Canada Corp. Fuel conveying member with side-brazed sealing members
US7624577B2 (en) 2006-03-31 2009-12-01 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
US8096130B2 (en) 2006-07-20 2012-01-17 Pratt & Whitney Canada Corp. Fuel conveying member for a gas turbine engine
US8353166B2 (en) 2006-08-18 2013-01-15 Pratt & Whitney Canada Corp. Gas turbine combustor and fuel manifold mounting arrangement
US7765808B2 (en) 2006-08-22 2010-08-03 Pratt & Whitney Canada Corp. Optimized internal manifold heat shield attachment
US8033113B2 (en) 2006-08-31 2011-10-11 Pratt & Whitney Canada Corp. Fuel injection system for a gas turbine engine
US7703289B2 (en) 2006-09-18 2010-04-27 Pratt & Whitney Canada Corp. Internal fuel manifold having temperature reduction feature
US7775047B2 (en) 2006-09-22 2010-08-17 Pratt & Whitney Canada Corp. Heat shield with stress relieving feature
US7926286B2 (en) 2006-09-26 2011-04-19 Pratt & Whitney Canada Corp. Heat shield for a fuel manifold
US7716933B2 (en) * 2006-10-04 2010-05-18 Pratt & Whitney Canada Corp. Multi-channel fuel manifold
US8572976B2 (en) 2006-10-04 2013-11-05 Pratt & Whitney Canada Corp. Reduced stress internal manifold heat shield attachment
US20080104961A1 (en) * 2006-11-08 2008-05-08 Ronald Scott Bunker Method and apparatus for enhanced mixing in premixing devices
US7856825B2 (en) 2007-05-16 2010-12-28 Pratt & Whitney Canada Corp. Redundant mounting system for an internal fuel manifold
US8096104B2 (en) * 2007-05-31 2012-01-17 United Technologies Corporation Fluidic vectoring for exhaust nozzle
US8146365B2 (en) 2007-06-14 2012-04-03 Pratt & Whitney Canada Corp. Fuel nozzle providing shaped fuel spray
US8096132B2 (en) * 2008-02-20 2012-01-17 Flexenergy Energy Systems, Inc. Air-cooled swirlerhead
US8887390B2 (en) 2008-08-15 2014-11-18 Dresser-Rand Company Method for correcting downstream deflection in gas turbine nozzles
US9181813B2 (en) 2012-07-05 2015-11-10 Siemens Aktiengesellschaft Air regulation for film cooling and emission control of combustion gas structure
EP3015772B1 (en) * 2014-10-31 2020-01-08 Ansaldo Energia Switzerland AG Combustor arrangement for a gas turbine
AU2016295720B2 (en) * 2015-07-21 2021-09-02 Fluidsens International Inc. System and method for detection of particles in liquid or in air
US10995699B2 (en) * 2018-02-19 2021-05-04 Mra Systems, Llc. Thrust reverser cascade
ES2975239T3 (en) * 2018-05-15 2024-07-04 Air Prod & Chem Combustion system and operating procedure of a combustion system
US10989413B2 (en) * 2019-07-17 2021-04-27 General Electric Company Axial retention assembly for combustor components of a gas turbine engine
CN112483260A (en) * 2020-12-15 2021-03-12 通化师范学院 Starting equipment of gas turbine
US11428411B1 (en) 2021-05-18 2022-08-30 General Electric Company Swirler with rifled venturi for dynamics mitigation
US20240263786A1 (en) * 2023-02-02 2024-08-08 Pratt & Whitney Canada Corp. Central air passage with radial fuel distributor

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US3075352A (en) * 1958-11-28 1963-01-29 Gen Motors Corp Combustion chamber fluid inlet construction
DE1131947B (en) * 1959-03-28 1962-06-20 Maschf Augsburg Nuernberg Ag Combustion process for gas turbine combustion chambers and equipment for carrying out the process
US3780530A (en) * 1969-10-23 1973-12-25 United Aircraft Corp Combustion chamber
US3691762A (en) * 1970-12-04 1972-09-19 Caterpillar Tractor Co Carbureted reactor combustion system for gas turbine engine
JPS5134524B2 (en) * 1971-12-09 1976-09-27

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0035869A1 (en) * 1980-03-05 1981-09-16 Hitachi, Ltd. A gas turbine combustor

Also Published As

Publication number Publication date
FR2259989B1 (en) 1980-01-11
SE393839B (en) 1977-05-23
DE2460709A1 (en) 1975-08-07
SE7500960L (en) 1975-08-05
JPS50140716A (en) 1975-11-12
CA1013153A (en) 1977-07-05
IT1026493B (en) 1978-09-20
JPS5825931B2 (en) 1983-05-31
DE2460709C2 (en) 1982-12-16
FR2259989A1 (en) 1975-08-29
US3859787A (en) 1975-01-14

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee