AU445514B2 - Combustion apparatus - Google Patents

Combustion apparatus

Info

Publication number
AU445514B2
AU445514B2 AU35980/71A AU3598071A AU445514B2 AU 445514 B2 AU445514 B2 AU 445514B2 AU 35980/71 A AU35980/71 A AU 35980/71A AU 3598071 A AU3598071 A AU 3598071A AU 445514 B2 AU445514 B2 AU 445514B2
Authority
AU
Australia
Prior art keywords
combustion apparatus
combustion
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
AU35980/71A
Other versions
AU3598071A (en
Inventor
Robert Wade Wallace
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 AU3598071A publication Critical patent/AU3598071A/en
Application granted granted Critical
Publication of AU445514B2 publication Critical patent/AU445514B2/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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F23R3/045—Air inlet arrangements using pipes
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03342—Arrangement of silo-type combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Gas Burners (AREA)
  • Combustion Of Fluid Fuel (AREA)
AU35980/71A 1970-11-27 1971-11-22 Combustion apparatus Expired AU445514B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US9301970A 1970-11-27 1970-11-27
USUS93019 1970-11-27

Publications (2)

Publication Number Publication Date
AU3598071A AU3598071A (en) 1973-05-31
AU445514B2 true AU445514B2 (en) 1974-02-21

Family

ID=22236381

Family Applications (1)

Application Number Title Priority Date Filing Date
AU35980/71A Expired AU445514B2 (en) 1970-11-27 1971-11-22 Combustion apparatus

Country Status (4)

Country Link
US (1) US3656298A (en)
AU (1) AU445514B2 (en)
DE (1) DE2158215C3 (en)
GB (1) GB1301968A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1335134A (en) * 1970-12-05 1973-10-24 Nissan Motor Combustion apparatus of a gas turbine engine
JPS4724483Y1 (en) * 1970-12-22 1972-08-02
US3854503A (en) * 1971-08-05 1974-12-17 Lucas Industries Ltd Flame tubes
US3969892A (en) * 1971-11-26 1976-07-20 General Motors Corporation Combustion system
US3744242A (en) * 1972-01-25 1973-07-10 Gen Motors Corp Recirculating combustor
FR2312654A1 (en) * 1975-05-28 1976-12-24 Snecma COMBUSTION CHAMBERS IMPROVEMENTS FOR GAS TURBINE ENGINES
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US3990232A (en) * 1975-12-11 1976-11-09 General Electric Company Combustor dome assembly having improved cooling means
US4008568A (en) * 1976-03-01 1977-02-22 General Motors Corporation Combustor support
US4195476A (en) * 1978-04-27 1980-04-01 General Motors Corporation Combustor construction
US4222230A (en) * 1978-08-14 1980-09-16 General Electric Company Combustor dome assembly
US4345426A (en) * 1980-03-27 1982-08-24 Egnell Rolf A Device for burning fuel with air
JP3951909B2 (en) * 2002-12-12 2007-08-01 株式会社日立製作所 Gas turbine combustor
US7260936B2 (en) * 2004-08-27 2007-08-28 Pratt & Whitney Canada Corp. Combustor having means for directing air into the combustion chamber in a spiral pattern
EP2767696A1 (en) * 2013-02-15 2014-08-20 Siemens Aktiengesellschaft Assembly comprising a gas turbine
US10539073B2 (en) 2017-03-20 2020-01-21 Chester L Richards, Jr. Centrifugal gas compressor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE550737A (en) *
DE1130958B (en) * 1956-08-25 1962-06-07 Schmidt Sche Heissdampf Large capacity burner for burning liquid fuels, especially heavy oils, for heating steam boilers
US3024608A (en) * 1958-09-24 1962-03-13 Snecma Combustion device
US3498055A (en) * 1968-10-16 1970-03-03 United Aircraft Corp Smoke reduction combustion chamber

Also Published As

Publication number Publication date
GB1301968A (en) 1973-01-04
DE2158215C3 (en) 1975-12-11
AU3598071A (en) 1973-05-31
DE2158215A1 (en) 1972-06-08
US3656298A (en) 1972-04-18
DE2158215B2 (en) 1975-04-24

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