FR1388005A - Gas turbine combustion chamber - Google Patents

Gas turbine combustion chamber

Info

Publication number
FR1388005A
FR1388005A FR4934A FR31004934A FR1388005A FR 1388005 A FR1388005 A FR 1388005A FR 4934 A FR4934 A FR 4934A FR 31004934 A FR31004934 A FR 31004934A FR 1388005 A FR1388005 A FR 1388005A
Authority
FR
France
Prior art keywords
combustion chamber
gas turbine
turbine combustion
gas
chamber
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
FR4934A
Other languages
French (fr)
Inventor
Gaston Bayard
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 filed Critical
Priority to FR4934A priority Critical patent/FR1388005A/en
Priority to US367011A priority patent/US3287905A/en
Priority to GB23689/64A priority patent/GB1037923A/en
Application granted granted Critical
Publication of FR1388005A publication Critical patent/FR1388005A/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
    • F23R3/42—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

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)
FR4934A 1963-12-09 1963-12-09 Gas turbine combustion chamber Expired FR1388005A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR4934A FR1388005A (en) 1963-12-09 1963-12-09 Gas turbine combustion chamber
US367011A US3287905A (en) 1963-12-09 1964-05-13 Combustion chamber for a gas turbine
GB23689/64A GB1037923A (en) 1963-12-09 1964-06-08 Combustion chamber for a gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR4934A FR1388005A (en) 1963-12-09 1963-12-09 Gas turbine combustion chamber

Publications (1)

Publication Number Publication Date
FR1388005A true FR1388005A (en) 1965-02-05

Family

ID=8570510

Family Applications (1)

Application Number Title Priority Date Filing Date
FR4934A Expired FR1388005A (en) 1963-12-09 1963-12-09 Gas turbine combustion chamber

Country Status (3)

Country Link
US (1) US3287905A (en)
FR (1) FR1388005A (en)
GB (1) GB1037923A (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3902314A (en) * 1973-11-29 1975-09-02 Avco Corp Gas turbine engine frame structure
US4018043A (en) * 1975-09-19 1977-04-19 Avco Corporation Gas turbine engines with toroidal combustors
GB1600130A (en) * 1977-05-21 1981-10-14 Rolls Royce Combustion systems
US4845941A (en) * 1986-11-07 1989-07-11 Paul Marius A Gas turbine engine operating process
US5058375A (en) * 1988-12-28 1991-10-22 Sundstrand Corporation Gas turbine annular combustor with radial dilution air injection
US5033263A (en) * 1989-03-17 1991-07-23 Sundstrand Corporation Compact gas turbine engine
US5140808A (en) * 1989-03-17 1992-08-25 Sundstrand Corporation Gas turbine engine with fuel mainfold system
US5048298A (en) * 1989-07-10 1991-09-17 Sundstrand Corporation Low cost fuel system for a gas turbine engine
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5363644A (en) * 1989-12-21 1994-11-15 Sundstrand Corporation Annular combustor
US20070245710A1 (en) * 2006-04-21 2007-10-25 Honeywell International, Inc. Optimized configuration of a reverse flow combustion system for a gas turbine engine
US20120023964A1 (en) * 2010-07-27 2012-02-02 Carsten Ralf Mehring Liquid-fueled premixed reverse-flow annular combustor for a gas turbine engine
DE102013222863A1 (en) 2013-11-11 2015-05-13 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor and method for its production
WO2024019723A1 (en) * 2022-07-21 2024-01-25 Raytheon Technologies Corporation Electrolysis energy recovery

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2296023A (en) * 1941-03-03 1942-09-15 Northrop Aircraft Inc Burner
US2633705A (en) * 1946-03-30 1953-04-07 John Hawkins And Associates Re Segmentally separable gas turbine power plant
GB721899A (en) * 1952-03-06 1955-01-12 Lucas Industries Ltd Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines
BE535905A (en) * 1954-02-23
US3088278A (en) * 1957-05-01 1963-05-07 Avco Mfg Corp Gas turbine engine
GB863011A (en) * 1957-12-20 1961-03-15 Constuction De Moteurs D Aviat Burner device for continuous-flow internal combustion engine

Also Published As

Publication number Publication date
US3287905A (en) 1966-11-29
GB1037923A (en) 1966-08-03

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