FR1552119A - - Google Patents

Info

Publication number
FR1552119A
FR1552119A FR1552119DA FR1552119A FR 1552119 A FR1552119 A FR 1552119A FR 1552119D A FR1552119D A FR 1552119DA FR 1552119 A FR1552119 A FR 1552119A
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.)
Expired
Application number
Other languages
French (fr)
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
Application granted granted Critical
Publication of FR1552119A publication Critical patent/FR1552119A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
FR1552119D 1967-11-17 1967-11-17 Expired FR1552119A (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR128761 1967-11-17

Publications (1)

Publication Number Publication Date
FR1552119A true FR1552119A (zh) 1969-01-03

Family

ID=8641906

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1552119D Expired FR1552119A (zh) 1967-11-17 1967-11-17

Country Status (3)

Country Link
DE (1) DE1809228A1 (zh)
FR (1) FR1552119A (zh)
GB (1) GB1238897A (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3109408A1 (fr) * 2020-04-21 2021-10-22 Safran Aircraft Engines Turbomachine à taux de dilution modulable pneumatiquement
FR3126733A1 (fr) * 2021-09-06 2023-03-10 Safran Aircraft Engines Turbomachine a double flux a bec variable en position

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2740904A1 (de) * 1977-09-10 1979-03-22 Motoren Turbinen Union Vorrichtung zur betaetigung von absperrorganen in gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken
US10794281B2 (en) 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components
US11073090B2 (en) 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3109408A1 (fr) * 2020-04-21 2021-10-22 Safran Aircraft Engines Turbomachine à taux de dilution modulable pneumatiquement
FR3126733A1 (fr) * 2021-09-06 2023-03-10 Safran Aircraft Engines Turbomachine a double flux a bec variable en position

Also Published As

Publication number Publication date
DE1809228A1 (de) 1969-06-19
GB1238897A (zh) 1971-07-14

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Legal Events

Date Code Title Description
ST Notification of lapse