Air injection casing for a turbomachine
AssigneeSafran Aircraft Engines
InventorsJérôme Claude George Lemonnier, Franck Davy Boisnault, Fabrice Marcel Noël Garin, Damien Bonneau, Delphine Touchard
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AssigneeSafran Aircraft Engines
InventorsJérôme Claude George Lemonnier, Franck Davy Boisnault, Fabrice Marcel Noël Garin, Damien Bonneau, Delphine Touchard
Estimating the term…
The invention relates to a cooling-air injection casing comprising a casing upstream end, a casing downstream end, and a casing main wall and further including: an air mixing cavity; an air intake cavity; an air bleeding cavity; a first sealing gasket; a second sealing gasket; the injection casing having further an air passage cavity bounded by a substantially radial wall, the casing main wall and the substantially axial wall, the air passage cavity being in fluid communication with the air mixing cavity via apertures made in the substantially axial wall, and in that the air passage cavity is in fluid communication with the air bleeding cavity by means of apertures made in the substantially radial wall.
A cooling-air injection casing having an annular shape around a longitudinal axis defining an axial direction and comprising a casing upstream end, a casing downstream end and a casing main wall which connects the upstream casing end with the downstream casing end, the casing main wall having an annular shape with a diameter that increases from upstream to downstream, the casing further comprising:
Dependencies are inferred from the claim text.