TURBOMACHINE A TURBINE DE PUISSANCE EQUIPEE D'UN GENERATEUR ELECTRONIQUE DE PUISSANCE CENTRE SUR L'AXE DE LA TURBOMACHINE

A turbine engine for an aircraft is disclosed. The engine includes a gas generator and a receiver driven by a power turbine. The receiver includes a propeller driven by a free power turbine provided with an outer case. The propeller includes a propeller case located radially outwards relatively to t...

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Bibliographic Details
Main Authors BEUTIN BRUNO ALBERT, YVON DIDIER JEAN LOUIS, COLIN ANTOINE OLIVIER FRANCOIS, REAUX CLARISSE SAVINE MATHILDE
Format Patent
LanguageFrench
Published 09.09.2011
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A turbine engine for an aircraft is disclosed. The engine includes a gas generator and a receiver driven by a power turbine. The receiver includes a propeller driven by a free power turbine provided with an outer case. The propeller includes a propeller case located radially outwards relatively to the outer case, and from which blades protrude radially outwards. The engine also includes an electric power generator. The rotor of the generator is centered on the longitudinal axis of the turbine engine, and is driven into rotation by the power turbine while being attached on the propeller case.
Bibliography:Application Number: FR20090050409