DE2209727C3 - Umkehr-Ringbrennkammer für Gasturbinentriebwerke - Google Patents

Umkehr-Ringbrennkammer für Gasturbinentriebwerke

Info

Publication number
DE2209727C3
DE2209727C3 DE2209727A DE2209727A DE2209727C3 DE 2209727 C3 DE2209727 C3 DE 2209727C3 DE 2209727 A DE2209727 A DE 2209727A DE 2209727 A DE2209727 A DE 2209727A DE 2209727 C3 DE2209727 C3 DE 2209727C3
Authority
DE
Germany
Prior art keywords
combustion chamber
air
flame tube
rear wall
tube body
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
DE2209727A
Other languages
German (de)
English (en)
Other versions
DE2209727B2 (de
DE2209727A1 (de
Inventor
Heinrich 8031 Puchheim Leibach
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 AG
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
Priority to DE2209727A priority Critical patent/DE2209727C3/de
Priority to GB1009873A priority patent/GB1379368A/en
Priority to FR7307386A priority patent/FR2174260B1/fr
Publication of DE2209727A1 publication Critical patent/DE2209727A1/de
Publication of DE2209727B2 publication Critical patent/DE2209727B2/de
Application granted granted Critical
Publication of DE2209727C3 publication Critical patent/DE2209727C3/de
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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
    • F23R3/52—Toroidal combustion chambers
    • 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Processes For Solid Components From Exhaust (AREA)
DE2209727A 1972-03-01 1972-03-01 Umkehr-Ringbrennkammer für Gasturbinentriebwerke Expired DE2209727C3 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE2209727A DE2209727C3 (de) 1972-03-01 1972-03-01 Umkehr-Ringbrennkammer für Gasturbinentriebwerke
GB1009873A GB1379368A (en) 1972-03-01 1973-03-01 Gas turbine engine having apparatus for the admission and condi tioning of fuel/air constituents
FR7307386A FR2174260B1 (OSRAM) 1972-03-01 1973-03-01

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2209727A DE2209727C3 (de) 1972-03-01 1972-03-01 Umkehr-Ringbrennkammer für Gasturbinentriebwerke

Publications (3)

Publication Number Publication Date
DE2209727A1 DE2209727A1 (de) 1973-09-13
DE2209727B2 DE2209727B2 (de) 1974-11-07
DE2209727C3 true DE2209727C3 (de) 1975-06-12

Family

ID=5837532

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2209727A Expired DE2209727C3 (de) 1972-03-01 1972-03-01 Umkehr-Ringbrennkammer für Gasturbinentriebwerke

Country Status (3)

Country Link
DE (1) DE2209727C3 (OSRAM)
FR (1) FR2174260B1 (OSRAM)
GB (1) GB1379368A (OSRAM)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636093B1 (fr) * 1988-09-02 1993-10-29 Serrier Michel Reacteur de petites dimensions fonctionnant au gaz propane
US10976052B2 (en) * 2017-10-25 2021-04-13 General Electric Company Volute trapped vortex combustor assembly

Also Published As

Publication number Publication date
DE2209727B2 (de) 1974-11-07
GB1379368A (en) 1975-01-02
FR2174260B1 (OSRAM) 1977-12-30
FR2174260A1 (OSRAM) 1973-10-12
DE2209727A1 (de) 1973-09-13

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
EHJ Ceased/non-payment of the annual fee