DE2320594C3 - Zweikreis-Strahltriebwerk - Google Patents

Zweikreis-Strahltriebwerk

Info

Publication number
DE2320594C3
DE2320594C3 DE2320594A DE2320594A DE2320594C3 DE 2320594 C3 DE2320594 C3 DE 2320594C3 DE 2320594 A DE2320594 A DE 2320594A DE 2320594 A DE2320594 A DE 2320594A DE 2320594 C3 DE2320594 C3 DE 2320594C3
Authority
DE
Germany
Prior art keywords
flow
core engine
obstacles
channel
turbine
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
DE2320594A
Other languages
German (de)
English (en)
Other versions
DE2320594B2 (de
DE2320594A1 (de
Inventor
Marc Francois Bernard Buisson
Herve Alain Quillevere
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE2320594A1 publication Critical patent/DE2320594A1/de
Publication of DE2320594B2 publication Critical patent/DE2320594B2/de
Application granted granted Critical
Publication of DE2320594C3 publication Critical patent/DE2320594C3/de
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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

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)
  • Exhaust Gas After Treatment (AREA)
  • Testing Of Engines (AREA)
DE2320594A 1972-04-25 1973-04-24 Zweikreis-Strahltriebwerk Expired DE2320594C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7214684A FR2181472B1 (https=) 1972-04-25 1972-04-25

Publications (3)

Publication Number Publication Date
DE2320594A1 DE2320594A1 (de) 1973-11-08
DE2320594B2 DE2320594B2 (de) 1978-03-16
DE2320594C3 true DE2320594C3 (de) 1978-11-09

Family

ID=9097496

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2320594A Expired DE2320594C3 (de) 1972-04-25 1973-04-24 Zweikreis-Strahltriebwerk

Country Status (4)

Country Link
US (1) US3871174A (https=)
DE (1) DE2320594C3 (https=)
FR (1) FR2181472B1 (https=)
GB (1) GB1386938A (https=)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7334409B2 (en) * 2004-05-19 2008-02-26 Alltech, Inc. Retractable afterburner for jet engine
US7506501B2 (en) * 2004-12-01 2009-03-24 Honeywell International Inc. Compact mixer with trimmable open centerbody
US9097136B2 (en) * 2012-01-03 2015-08-04 General Electric Company Contoured honeycomb seal for turbine shroud
RU2682220C1 (ru) * 2018-03-01 2019-03-15 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Форсажная камера сгорания турбореактивного двухконтурного двигателя

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
US2883828A (en) * 1954-11-10 1959-04-28 Alun R Howell Power plant incorporating a dynamic compressor
US2978865A (en) * 1956-02-06 1961-04-11 Curtiss Wright Corp Turbo fan exhaust mixing device
GB838602A (en) * 1957-03-06 1960-06-22 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine plant
US3048376A (en) * 1958-04-09 1962-08-07 Curtiss Wright Corp Fluid mixing apparatus

Also Published As

Publication number Publication date
DE2320594B2 (de) 1978-03-16
GB1386938A (en) 1975-03-12
FR2181472A1 (https=) 1973-12-07
DE2320594A1 (de) 1973-11-08
US3871174A (en) 1975-03-18
FR2181472B1 (https=) 1975-08-29

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8328 Change in the person/name/address of the agent

Free format text: GERNHARDT, C., DIPL.-ING., PAT.-ANW., 8000 MUENCHEN

8339 Ceased/non-payment of the annual fee