FR1435410A - Combustion chamber, in particular for gas turbines, and turbines provided with the combustion chamber - Google Patents

Combustion chamber, in particular for gas turbines, and turbines provided with the combustion chamber

Info

Publication number
FR1435410A
FR1435410A FR17972A FR17972A FR1435410A FR 1435410 A FR1435410 A FR 1435410A FR 17972 A FR17972 A FR 17972A FR 17972 A FR17972 A FR 17972A FR 1435410 A FR1435410 A FR 1435410A
Authority
FR
France
Prior art keywords
combustion chamber
turbines
gas turbines
gas
turbines provided
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
FR17972A
Other languages
French (fr)
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.)
Prvni Brnenska Strojirna Zavody Klementa Gottwalda Narodni Podnik
Original Assignee
Prvni Brnenska Strojirna Zavody Klementa Gottwalda Narodni Podnik
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 Prvni Brnenska Strojirna Zavody Klementa Gottwalda Narodni Podnik filed Critical Prvni Brnenska Strojirna Zavody Klementa Gottwalda Narodni Podnik
Application granted granted Critical
Publication of FR1435410A publication Critical patent/FR1435410A/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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/202—Heat transfer, e.g. cooling by film cooling

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)
FR17972A 1964-05-21 1965-05-21 Combustion chamber, in particular for gas turbines, and turbines provided with the combustion chamber Expired FR1435410A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CS291664 1964-05-21

Publications (1)

Publication Number Publication Date
FR1435410A true FR1435410A (en) 1966-04-15

Family

ID=5367680

Family Applications (1)

Application Number Title Priority Date Filing Date
FR17972A Expired FR1435410A (en) 1964-05-21 1965-05-21 Combustion chamber, in particular for gas turbines, and turbines provided with the combustion chamber

Country Status (5)

Country Link
AT (1) AT257279B (en)
CH (1) CH428324A (en)
DE (1) DE1291554B (en)
FR (1) FR1435410A (en)
GB (1) GB1089467A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2493920A1 (en) * 1980-11-08 1982-05-14 Rolls Royce AIR CIRCULATION COOLING WALL FOR A GAS TURBINE ENGINE COMBUSTION CHAMBER
FR2567250A1 (en) * 1984-07-06 1986-01-10 Gen Electric Combustion chamber for a gas turbine engine
EP0219723A1 (en) * 1985-10-04 1987-04-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Annular combustion chamber for gas turbines
EP0344877A1 (en) * 1988-05-31 1989-12-06 General Electric Company Heat shield for gas turbine engine frame
EP0348500A1 (en) * 1987-12-28 1990-01-03 Sundstrand Corp Annular combustor with tangential cooling air injection.
EP0397566A1 (en) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat insulation structure for an afterburner liner or turbine transition piece

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4414816A (en) * 1980-04-02 1983-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustor liner construction
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
GB2160964B (en) * 1984-06-25 1988-04-07 Gen Electric Combustion chamber construction
US5259182A (en) * 1989-12-22 1993-11-09 Hitachi, Ltd. Combustion apparatus and combustion method therein
DE10233805B4 (en) * 2002-07-25 2013-08-22 Alstom Technology Ltd. Annular combustion chamber for a gas turbine
DE102014204481A1 (en) * 2014-03-11 2015-09-17 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
DE102014204476A1 (en) 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH255541A (en) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Cooled metal combustion chamber for generating heating and propellant gases.
BE490776A (en) * 1948-10-26
FR1034669A (en) * 1949-12-12 1953-07-29 Babcock & Wilcox France Improvements to combustion devices

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2493920A1 (en) * 1980-11-08 1982-05-14 Rolls Royce AIR CIRCULATION COOLING WALL FOR A GAS TURBINE ENGINE COMBUSTION CHAMBER
FR2567250A1 (en) * 1984-07-06 1986-01-10 Gen Electric Combustion chamber for a gas turbine engine
EP0219723A1 (en) * 1985-10-04 1987-04-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Annular combustion chamber for gas turbines
EP0348500A1 (en) * 1987-12-28 1990-01-03 Sundstrand Corp Annular combustor with tangential cooling air injection.
EP0348500A4 (en) * 1987-12-28 1990-04-10 Sundstrand Corp Annular combustor with tangential cooling air injection.
EP0344877A1 (en) * 1988-05-31 1989-12-06 General Electric Company Heat shield for gas turbine engine frame
EP0397566A1 (en) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat insulation structure for an afterburner liner or turbine transition piece
FR2646880A1 (en) * 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
US5069034A (en) * 1989-05-11 1991-12-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat protective lining for an afterburner or transition duct of a turbojet engine

Also Published As

Publication number Publication date
DE1291554B (en) 1969-03-27
AT257279B (en) 1967-09-25
CH428324A (en) 1967-01-15
GB1089467A (en) 1967-11-01

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