COMBUSTION CHAMBER OF A TURBINE ENGINE COMPRISING A THROUGH-PART WITH AN OPENING

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United States of America Patent

SERIAL NO

15552056

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Abstract

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A combustion chamber of a turbine engine, including at least one wall defining the combustion chamber and including an aperture for enabling a through-part to pass therethrough. The through-part includes, in the portion thereof located within the combustion chamber, at least one opening able to create an air film to cool the area downstream of the through-part.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN HELICOPTER ENGINESBORDEAUX BORDEAUX GIRONDE

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
LAMAISON, Olivier Montardon, FR 5 6
SAVARY, Nicolas Jurancon, FR 7 15

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