FR920635A - Perfectionnements apportés aux installations motrices avec turbines à combustion interne et utilisées pour la propulsion d'aéronefs
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Perfectionnements apportés aux installations motrices avec turbines à combustion interne et utilisées pour la propulsion d'aéronefs
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Power Jets Research and Development Ltd
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Power Jets Research and Development Ltd
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Publication of FR920635ApublicationCriticalpatent/FR920635A/fr
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
F02C3/073—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 the compressor and turbine stages being concentric
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Engineering & Computer Science
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Chemical & Material Sciences
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Combustion & Propulsion
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Mechanical Engineering
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General Engineering & Computer Science
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FR920635D1944-01-311946-01-23Perfectionnements apportés aux installations motrices avec turbines à combustion interne et utilisées pour la propulsion d'aéronefs
ExpiredFR920635A
(fr)
Perfectionnements apportés aux installations motrices avec turbines à combustion interne et utilisées comme moyens propulseurs principaux pour des aéronefs