Turbine engine equipped with a means to heat the air...

Details Turbine engine equipped with a means to heat the air... Turbine engine equipped with a means to heat the air...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/08 (2006.01) F02C 6/20 (2006.01)

Patent

CA 2643618

L'invention concerne un turbomoteur (10), notamment pour un hélicoptère, comportant un générateur de gaz (12) et une turbine libre (14) entraînée en rotation par un flux de gaz (F) généré par le générateur de gaz. L'invention se caractérise par le fait que le turbomoteur comporte en outre des moyens de chauffage (26) disposés entre le générateur de gaz et la turbine libre (14), lesdits moyens de chauffage (26) étant aptes à augmenter la température du flux de gaz (f) généré par le générateur de gaz- (12) et entraînant la turbine libre.

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