CA982829A - Combustor for a gas turbine engine - Google Patents

Combustor for a gas turbine engine

Info

Publication number
CA982829A
CA982829A CA171,134A CA171134A CA982829A CA 982829 A CA982829 A CA 982829A CA 171134 A CA171134 A CA 171134A CA 982829 A CA982829 A CA 982829A
Authority
CA
Canada
Prior art keywords
combustor
gas turbine
turbine engine
engine
gas
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
CA171,134A
Other versions
CA171134S (en
Inventor
Nicolas A. Azelborn
Joseph Errante
Antoni Paluszny
Original Assignee
Ford Motor Company of Canada 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 Ford Motor Company of Canada Ltd filed Critical Ford Motor Company of Canada Ltd
Application granted granted Critical
Publication of CA982829A publication Critical patent/CA982829A/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
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Air Supply (AREA)
  • Combustion Of Fluid Fuel (AREA)
CA171,134A 1972-05-25 1973-05-08 Combustor for a gas turbine engine Expired CA982829A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US256883A US3859786A (en) 1972-05-25 1972-05-25 Combustor

Publications (1)

Publication Number Publication Date
CA982829A true CA982829A (en) 1976-02-03

Family

ID=22973991

Family Applications (1)

Application Number Title Priority Date Filing Date
CA171,134A Expired CA982829A (en) 1972-05-25 1973-05-08 Combustor for a gas turbine engine

Country Status (5)

Country Link
US (1) US3859786A (en)
JP (1) JPS5319722B2 (en)
CA (1) CA982829A (en)
DE (1) DE2326302C2 (en)
GB (1) GB1414412A (en)

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US4586328A (en) * 1974-07-24 1986-05-06 Howald Werner E Combustion apparatus including an air-fuel premixing chamber
US4563875A (en) * 1974-07-24 1986-01-14 Howald Werner E Combustion apparatus including an air-fuel premixing chamber
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JPS5129726A (en) * 1974-09-06 1976-03-13 Mitsubishi Heavy Ind Ltd
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US4049021A (en) * 1975-04-14 1977-09-20 Phillips Petroleum Company Variable dome valves and combustors provided with said valves
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US4385490A (en) * 1978-08-14 1983-05-31 Phillips Petroleum Company Combustors and methods of operating same
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
US4498287A (en) * 1980-12-23 1985-02-12 Phillips Petroleum Company Combustors and methods of operating same
US4590769A (en) * 1981-01-12 1986-05-27 United Technologies Corporation High-performance burner construction
US4845940A (en) * 1981-02-27 1989-07-11 Westinghouse Electric Corp. Low NOx rich-lean combustor especially useful in gas turbines
DE3301355C2 (en) * 1983-01-18 1984-11-08 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Jump start device for a high pressure combustion chamber
US4702073A (en) * 1986-03-10 1987-10-27 Melconian Jerry O Variable residence time vortex combustor
DE3742891A1 (en) * 1987-12-17 1989-06-29 Bayerische Motoren Werke Ag GAS TURBINE SYSTEM
US5285628A (en) * 1990-01-18 1994-02-15 Donlee Technologies, Inc. Method of combustion and combustion apparatus to minimize Nox and CO emissions from a gas turbine
US5462430A (en) * 1991-05-23 1995-10-31 Institute Of Gas Technology Process and apparatus for cyclonic combustion
US5209187A (en) * 1991-08-01 1993-05-11 Institute Of Gas Technology Low pollutant - emission, high efficiency cyclonic burner for firetube boilers and heaters
US5220888A (en) * 1991-08-01 1993-06-22 Institute Of Gas Technology Cyclonic combustion
US5185541A (en) * 1991-12-02 1993-02-09 21St Century Power & Light Corporation Gas turbine for converting fuel to electrical and mechanical energy
DE4232383A1 (en) * 1992-09-26 1994-03-31 Asea Brown Boveri Gas turbine group
EP0895024B1 (en) * 1993-07-30 2003-01-02 United Technologies Corporation Swirl mixer for a combustor
DE69421896T2 (en) * 1993-12-22 2000-05-31 Siemens Westinghouse Power Corp., Orlando Bypass valve for the combustion chamber of a gas turbine
DE4435266A1 (en) * 1994-10-01 1996-04-04 Abb Management Ag burner
US5601789A (en) * 1994-12-15 1997-02-11 W. R. Grace & Co.-Conn. Raw gas burner and process for burning oxygenic constituents in process gas
DE19523094A1 (en) * 1995-06-26 1997-01-02 Abb Management Ag Combustion chamber
EP0918190A1 (en) * 1997-11-21 1999-05-26 Abb Research Ltd. Burner for the operation of a heat generator
US6240731B1 (en) * 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
US6983645B2 (en) * 2002-08-06 2006-01-10 Southwest Research Institute Method for accelerated aging of catalytic converters incorporating engine cold start simulation
US20040007056A1 (en) * 2001-08-06 2004-01-15 Webb Cynthia C. Method for testing catalytic converter durability
US6729141B2 (en) * 2002-07-03 2004-05-04 Elliot Energy Systems, Inc. Microturbine with auxiliary air tubes for NOx emission reduction
US7412335B2 (en) 2002-08-06 2008-08-12 Southwest Research Institute Component evaluations using non-engine based test system
US7617682B2 (en) * 2002-12-13 2009-11-17 Siemens Energy, Inc. Catalytic oxidation element for a gas turbine engine
US20050051155A1 (en) * 2003-08-12 2005-03-10 Tomlinson John L. Direct-fired, gas-fueled heater
US8425224B2 (en) 2005-03-17 2013-04-23 Southwest Research Institute Mass air flow compensation for burner-based exhaust gas generation system
US7748976B2 (en) * 2005-03-17 2010-07-06 Southwest Research Institute Use of recirculated exhaust gas in a burner-based exhaust generation system for reduced fuel consumption and for cooling
US20070039381A1 (en) * 2005-08-05 2007-02-22 Timmons Suzanne A Secondary Air Injector For Use With Exhaust Gas Simulation System
US8475124B2 (en) * 2007-11-13 2013-07-02 General Electric Company Exhaust hood for a turbine and methods of assembling the same
BRPI0821737A8 (en) * 2007-12-21 2018-12-18 Green Prtners Tech Holdings Gmbh open and closed and semi-closed gas turbine systems for power generation and expansion turbine and closed piston compressor, turbocharger, and operating gas compression open cycle gas turbine power production methods in turbocharger and engine system operation
EP2257736B1 (en) * 2008-03-07 2015-11-25 Alstom Technology Ltd Method for the production of hot gas
JP5453322B2 (en) * 2008-03-07 2014-03-26 アルストム テクノロジー リミテッド Burner device and use of burner device
US8622737B2 (en) 2008-07-16 2014-01-07 Robert S. Babington Perforated flame tube for a liquid fuel burner
US8745989B2 (en) * 2009-04-09 2014-06-10 Pratt & Whitney Canada Corp. Reverse flow ceramic matrix composite combustor
US9222674B2 (en) * 2011-07-21 2015-12-29 United Technologies Corporation Multi-stage amplification vortex mixture for gas turbine engine combustor
EP2700879B1 (en) * 2012-08-24 2019-03-27 Ansaldo Energia Switzerland AG Method for mixing a dilution air in a sequential combustion system of a gas turbine, and sequential combustion system for a gas turbine comprising dilution air injector
CN110107402B (en) * 2019-04-29 2021-06-08 中国航空工业集团公司金城南京机电液压工程研究中心 Ceramic turbine engine
CN111927625B (en) * 2020-07-13 2022-08-19 西安航天动力研究所 Two-phase rotary detonation combustion cavity structure capable of stably and controllably unidirectionally spreading rotary detonation wave
RU2757705C1 (en) * 2021-01-13 2021-10-20 Роман Лазирович Илиев Double-layer vortex countercurrent flow burner

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Publication number Priority date Publication date Assignee Title
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
US2635564A (en) * 1948-09-15 1953-04-21 Power Jets Res & Dev Ltd Combustion system for pulverulent fuel
US2837893A (en) * 1952-12-12 1958-06-10 Phillips Petroleum Co Automatic primary and secondary air flow regulation for gas turbine combustion chamber
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
FR1094871A (en) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Improvements to injected fuel combustion devices
US3293852A (en) * 1963-03-19 1966-12-27 Boeing Co Plasma propulsion method and means
GB1039133A (en) * 1963-05-15 1966-08-17 Lucas Industries Ltd Liquid fuel combustion apparatus for gas turbine engines
US3360929A (en) * 1966-03-10 1968-01-02 Montrose K. Drewry Gas turbine combustors
US3368604A (en) * 1966-06-14 1968-02-13 American Air Filter Co Combustion apparatus
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube
GB1278590A (en) * 1968-09-20 1972-06-21 Lucas Industries Ltd Combustion chambers for gas turbine engines
US3570242A (en) * 1970-04-20 1971-03-16 United Aircraft Corp Fuel premixing for smokeless jet engine main burner
US3691762A (en) * 1970-12-04 1972-09-19 Caterpillar Tractor Co Carbureted reactor combustion system for gas turbine engine

Also Published As

Publication number Publication date
DE2326302C2 (en) 1983-01-05
JPS4949011A (en) 1974-05-13
DE2326302A1 (en) 1974-01-17
GB1414412A (en) 1975-11-19
US3859786A (en) 1975-01-14
JPS5319722B2 (en) 1978-06-22

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