Device for de-icing a turbomachine nozzle
AssigneeSafran Aircraft Engines
InventorsRémi Roland Robert Mercier, Fabrice Michel François René Aubert, Arnaud Langlois
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AssigneeSafran Aircraft Engines
InventorsRémi Roland Robert Mercier, Fabrice Michel François René Aubert, Arnaud Langlois
Estimating the term…
A de-icing device to supply de-icing air to a turbomachine separation nozzle extending along a longitudinal axis, the turbomachine comprising: a separation nozzle positioned downstream from a turbomachine fan and comprises an internal casing and an external casing which form a separation between a primary flow vein for a primary stream and a secondary flow vein for a secondary stream, the internal casing and the external casing defining an inter-vein space; turbomachine guide vanes secured by screws to the internal casing, the screws extend into the inter-vein space, the de-icing device positioned in the inter-vein space and comprising an air inlet; an air outlet; a plurality of channels extending from the air inlet toward the air outlet; the channels arranged in relation to one another such that they extend from the air inlet toward the air outlets, passing between the screws for securing the guide vanes.
A turbomachine comprising:
Dependencies are inferred from the claim text.