FR2065688A1 - - Google Patents

Info

Publication number
FR2065688A1
FR2065688A1 FR6944968A FR6944968A FR2065688A1 FR 2065688 A1 FR2065688 A1 FR 2065688A1 FR 6944968 A FR6944968 A FR 6944968A FR 6944968 A FR6944968 A FR 6944968A FR 2065688 A1 FR2065688 A1 FR 2065688A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6944968A
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2065688A1 publication Critical patent/FR2065688A1/fr
Withdrawn legal-status Critical Current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
    • 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
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/41—Movement of component with one degree of freedom
    • F05B2250/411—Movement of component with one degree of freedom in rotation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
FR6944968A 1969-09-11 1969-12-24 Withdrawn FR2065688A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691945921 DE1945921A1 (en) 1969-09-11 1969-09-11 Combustion chamber

Publications (1)

Publication Number Publication Date
FR2065688A1 true FR2065688A1 (en) 1971-08-06

Family

ID=5745136

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6944968A Withdrawn FR2065688A1 (en) 1969-09-11 1969-12-24

Country Status (2)

Country Link
DE (1) DE1945921A1 (en)
FR (1) FR2065688A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5211675A (en) * 1991-01-23 1993-05-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Variable volume combustion chamber for a gas turbine engine

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2133832B1 (en) * 1971-04-15 1975-10-24 United Aircraft Canada
DE2620424C2 (en) * 1976-05-08 1983-07-21 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Combustion chamber with variable geometry of the air supply for gas turbine engines
JPS61195214A (en) * 1985-02-22 1986-08-29 Hitachi Ltd Air flow part adjusting device for gas turbine combustor
FR2676529B1 (en) * 1991-05-16 1994-11-25 Snecma COMBUSTION SUPPLY DEVICE FOR A GAS TURBINE COMPRISING FLOW ADJUSTMENT DIAPHRAGMS.
DE4120831A1 (en) * 1991-06-24 1993-01-07 Asea Brown Boveri Gas turbine combustion chamber operating method - involves by=passing part of air into pre-mixing zone at part-load operation
FR2690977B1 (en) * 1992-05-06 1995-09-01 Snecma COMBUSTION CHAMBER COMPRISING ADJUSTABLE PASSAGES FOR THE ADMISSION OF PRIMARY FUEL.
US7540152B2 (en) * 2006-02-27 2009-06-02 Mitsubishi Heavy Industries, Ltd. Combustor
DE102020132494A1 (en) 2020-12-07 2022-06-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gas turbine combustor system and method of operating a gas turbine combustor system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5211675A (en) * 1991-01-23 1993-05-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Variable volume combustion chamber for a gas turbine engine

Also Published As

Publication number Publication date
DE1945921A1 (en) 1971-03-25

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Legal Events

Date Code Title Description
ST Notification of lapse