CA993668A - Combustion apparatus air supply for gas turbine engine - Google Patents

Combustion apparatus air supply for gas turbine engine

Info

Publication number
CA993668A
CA993668A CA196,154A CA196154A CA993668A CA 993668 A CA993668 A CA 993668A CA 196154 A CA196154 A CA 196154A CA 993668 A CA993668 A CA 993668A
Authority
CA
Canada
Prior art keywords
air supply
gas turbine
turbine engine
combustion apparatus
apparatus air
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
CA196,154A
Other languages
English (en)
Other versions
CA196154S (en
Inventor
Samuel B. Reider
Harold L. Stocker
Jerry G. Tomlinson
Arthur H. Lefebvre
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
Application granted granted Critical
Publication of CA993668A publication Critical patent/CA993668A/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA196,154A 1973-08-27 1974-03-27 Combustion apparatus air supply for gas turbine engine Expired CA993668A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US391888A US3877221A (en) 1973-08-27 1973-08-27 Combustion apparatus air supply

Publications (1)

Publication Number Publication Date
CA993668A true CA993668A (en) 1976-07-27

Family

ID=23548373

Family Applications (1)

Application Number Title Priority Date Filing Date
CA196,154A Expired CA993668A (en) 1973-08-27 1974-03-27 Combustion apparatus air supply for gas turbine engine

Country Status (7)

Country Link
US (1) US3877221A (ja)
JP (2) JPS5045111A (ja)
CA (1) CA993668A (ja)
DE (1) DE2422362B2 (ja)
FR (1) FR2245855B1 (ja)
GB (1) GB1425438A (ja)
IT (1) IT1011411B (ja)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098074A (en) * 1976-06-01 1978-07-04 United Technologies Corporation Combustor diffuser for turbine type power plant and construction thereof
US4458479A (en) * 1981-10-13 1984-07-10 General Motors Corporation Diffuser for gas turbine engine
JPS5932863U (ja) * 1982-08-27 1984-02-29 三菱重工業株式会社 ガスタ−ビン燃焼器
FR2616889B1 (fr) * 1987-06-18 1992-07-31 Snecma Carter de chambre de combustion de turboreacteur comportant des orifices de prelevement d'air
GB8928378D0 (en) * 1989-12-15 1990-02-21 Rolls Royce Plc A diffuser
US5077967A (en) * 1990-11-09 1992-01-07 General Electric Company Profile matched diffuser
FR2694962B1 (fr) * 1992-08-19 1994-10-21 Snecma Turboréacteur dont la chambre de combustion est protégée contre les effets d'une ingestion massive d'eau.
US5279126A (en) * 1992-12-18 1994-01-18 United Technologies Corporation Diffuser-combustor
DE59504264D1 (de) * 1994-01-24 1998-12-24 Siemens Ag Brennkammer für eine gasturbine
US5737915A (en) * 1996-02-09 1998-04-14 General Electric Co. Tri-passage diffuser for a gas turbine
US6401447B1 (en) 2000-11-08 2002-06-11 Allison Advanced Development Company Combustor apparatus for a gas turbine engine
GB2390890B (en) * 2002-07-17 2005-07-06 Rolls Royce Plc Diffuser for gas turbine engine
US6843059B2 (en) * 2002-11-19 2005-01-18 General Electric Company Combustor inlet diffuser with boundary layer blowing
FR3064050B1 (fr) * 2017-03-14 2021-02-19 Safran Aircraft Engines Chambre de combustion d'une turbomachine
US11578869B2 (en) * 2021-05-20 2023-02-14 General Electric Company Active boundary layer control in diffuser

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB902511A (en) * 1960-04-19 1962-08-01 Bristol Siddeley Engines Ltd Improvements in or relating to combustion chambers
US3403510A (en) * 1966-11-23 1968-10-01 United Aircraft Corp Removable and replaceable fuel nozzle holder assembly for an annular combustion burner
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US3631675A (en) * 1969-09-11 1972-01-04 Gen Electric Combustor primary air control

Also Published As

Publication number Publication date
DE2422362A1 (de) 1975-03-27
DE2422362B2 (de) 1979-08-23
JPS5045111A (ja) 1975-04-23
IT1011411B (it) 1977-01-20
FR2245855B1 (ja) 1978-08-04
FR2245855A1 (ja) 1975-04-25
US3877221A (en) 1975-04-15
DE2422362C3 (ja) 1980-05-08
GB1425438A (en) 1976-02-18
JPS5395004U (ja) 1978-08-02

Similar Documents

Publication Publication Date Title
CA1013153A (en) Combustion apparatus for a gas turbine engine
CA982831A (en) Combustion apparatus for an engine with hot combustion air
CA985514A (en) Combustion apparatus for gas turbine
CA982829A (en) Combustor for a gas turbine engine
CA988309A (en) Impingement-convective cooling system for a gas turbine engine
CA1022350A (en) Combustion method and apparatus for gas turbine engine
GB1553847A (en) Fuel supply system for a gas turbine engine
JPS5236210A (en) Fuel system for gas turbine engine
CA993668A (en) Combustion apparatus air supply for gas turbine engine
CA1031170A (en) Start-up compressed air system for gas turbine engines
GB1539734A (en) Fuel supply system for a gas turbine engine
CA987918A (en) Gas turbine engine combustion equipment
GB1552132A (en) Combustion chambers for gas turbine engines
CA1031972A (en) Combustion control for a gas turbine engine
CA1007466A (en) Exhaust gas emission control device for multi-cylinder engines
CA993667A (en) Combustion apparatus for gas turbine engines
CA1023567A (en) Combustion chamber for a gas turbine engine
CA1031973A (en) Combustion chamber for a gas turbine engine
CA985918A (en) Gas turbine engine combustion equipment
CA1009854A (en) Regenerator for gas turbine engine
CA981920A (en) Compressor geometry control apparatus for gas turbine engine
CA1007331A (en) Device for controlling gas turbine engines
AU458794B2 (en) Device for controlling the recycle of exhaust gas in an internal combustion engine
CA948698A (en) Transistorized ignition system for gas turbine engines
CA970593A (en) Temperature measurement system for gas turbine engines