FR997672A - Système d'échappement en dépression applicable aux turbines à gaz - Google Patents

Système d'échappement en dépression applicable aux turbines à gaz

Info

Publication number
FR997672A
FR997672A FR997672DA FR997672A FR 997672 A FR997672 A FR 997672A FR 997672D A FR997672D A FR 997672DA FR 997672 A FR997672 A FR 997672A
Authority
FR
France
Prior art keywords
exhaust system
gas turbines
vacuum exhaust
system applicable
applicable
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
Other languages
English (en)
Inventor
Joseph Bayon
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 FR997672A publication Critical patent/FR997672A/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
    • F02K3/062—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 with aft fan
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • 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
    • F02K3/06—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 with front fan
FR997672D 1949-09-29 1949-09-29 Système d'échappement en dépression applicable aux turbines à gaz Expired FR997672A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR997672T 1949-09-29

Publications (1)

Publication Number Publication Date
FR997672A true FR997672A (fr) 1952-01-09

Family

ID=9558830

Family Applications (1)

Application Number Title Priority Date Filing Date
FR997672D Expired FR997672A (fr) 1949-09-29 1949-09-29 Système d'échappement en dépression applicable aux turbines à gaz

Country Status (1)

Country Link
FR (1) FR997672A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2422105A1 (de) * 1973-05-08 1974-11-28 Snecma Zwei- oder mehrstromgasturbinentriebwerk
FR2364336A1 (fr) * 1976-09-09 1978-04-07 Benson William Appareil de propulsion
FR2378182A1 (fr) * 1977-01-19 1978-08-18 Rolls Royce Perfectionnements aux propulseurs a turbine a gaz
FR3050485A1 (fr) * 2016-04-26 2017-10-27 Snecma Turbomachine a double flux

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2422105A1 (de) * 1973-05-08 1974-11-28 Snecma Zwei- oder mehrstromgasturbinentriebwerk
FR2228949A1 (fr) * 1973-05-08 1974-12-06 Snecma
FR2364336A1 (fr) * 1976-09-09 1978-04-07 Benson William Appareil de propulsion
FR2378182A1 (fr) * 1977-01-19 1978-08-18 Rolls Royce Perfectionnements aux propulseurs a turbine a gaz
FR3050485A1 (fr) * 2016-04-26 2017-10-27 Snecma Turbomachine a double flux

Similar Documents

Publication Publication Date Title
FR1021359A (fr) Perfectionnements à l'ensemble d'échappement des moteurs à turbine à gaz
FR1033849A (fr) Perfectionnements aux turbines à gaz
FR1020989A (fr) Perfectionnements aux moteurs à turbines à gaz
FR1062311A (fr) Perfectionnements aux turbines à gaz
FR997672A (fr) Système d'échappement en dépression applicable aux turbines à gaz
FR1006338A (fr) Perfectionnements aux turbines à gaz
FR1013999A (fr) Dépoussiérreur perfectionné d'air ou autres gaz
FR1007743A (fr) Turbine à gaz
FR1059635A (fr) Perfectionnements aux turbines à gaz
FR1114538A (fr) Perfectionnements aux turbines à gaz
FR980416A (fr) Turbine à gaz compound
FR1017477A (fr) Perfectionnements relatifs aux installations de turbines à gaz
FR995175A (fr) Perfectionnements aux turbines à gaz
FR1035814A (fr) Perfectionnements apportés aux turbines à gaz
FR1006585A (fr) Perfectionnements aux turbines à gaz
FR1066103A (fr) Perfectionnements apportés aux turbines à gaz
FR917976A (fr) Turbo-compresseur à gaz d'échappement
FR966308A (fr) Perfectionnements aux moteurs à turbine à gaz
FR979897A (fr) Turbine à gaz
FR1110874A (fr) Perfectionnements aux turbines à gaz
FR1038625A (fr) Moteur à turbine à gaz
FR1046175A (fr) Perfectionnements aux turbines à gaz
FR1062654A (fr) Perfectionnements aux turbines à gaz
FR975686A (fr) Perfectionnements aux locomotives entraînées par turbines à gaz
FR933048A (fr) Perfectionnements aux compresseurs d'air ou de gaz