FR905229A - Improvements to thermal reaction machines such as thermo-propellants - Google Patents

Improvements to thermal reaction machines such as thermo-propellants

Info

Publication number
FR905229A
FR905229A FR905229DA FR905229A FR 905229 A FR905229 A FR 905229A FR 905229D A FR905229D A FR 905229DA FR 905229 A FR905229 A FR 905229A
Authority
FR
France
Prior art keywords
propellants
thermo
thermal reaction
reaction machines
machines
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
French (fr)
Inventor
Dimitri Sensaud De Lavaud
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 FR905229A publication Critical patent/FR905229A/en
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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • 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
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR905229D 1944-01-17 1944-01-17 Improvements to thermal reaction machines such as thermo-propellants Expired FR905229A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR905229T 1944-01-17

Publications (1)

Publication Number Publication Date
FR905229A true FR905229A (en) 1945-11-28

Family

ID=9405291

Family Applications (1)

Application Number Title Priority Date Filing Date
FR905229D Expired FR905229A (en) 1944-01-17 1944-01-17 Improvements to thermal reaction machines such as thermo-propellants

Country Status (1)

Country Link
FR (1) FR905229A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3390527A (en) * 1967-07-19 1968-07-02 Avco Corp High bypass ratio turbofan
US3396905A (en) * 1966-09-28 1968-08-13 Gen Motors Corp Ducted fan
US3467198A (en) * 1966-12-05 1969-09-16 Rolls Royce Gear transmission
FR2588612A1 (en) * 1985-10-16 1987-04-17 Onera (Off Nat Aerospatiale) Improvements applied to turbocompressors
ES2069486A2 (en) * 1993-07-06 1995-05-01 Pardo Carlos Moreno Improved ejector for converting calorific energy into kinetic energy
WO2013012316A1 (en) * 2011-07-15 2013-01-24 Leep Cor Turbofan engine with convergent - divergent exhaust nozzle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3396905A (en) * 1966-09-28 1968-08-13 Gen Motors Corp Ducted fan
US3467198A (en) * 1966-12-05 1969-09-16 Rolls Royce Gear transmission
US3390527A (en) * 1967-07-19 1968-07-02 Avco Corp High bypass ratio turbofan
FR2588612A1 (en) * 1985-10-16 1987-04-17 Onera (Off Nat Aerospatiale) Improvements applied to turbocompressors
ES2069486A2 (en) * 1993-07-06 1995-05-01 Pardo Carlos Moreno Improved ejector for converting calorific energy into kinetic energy
WO2013012316A1 (en) * 2011-07-15 2013-01-24 Leep Cor Turbofan engine with convergent - divergent exhaust nozzle

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