A helicopter engine air intake including an anti-icing grid that provides a large bypass flow in event of icing. The air intake includes air intake lips and an anti-icing grid mounted on outer ends of the air intake lips, being interposed in the air flow penetrating into the air intake, at least one air intake lip being formed by a thin metal sheet.
ENTREE D'AIR POUR MOTEUR D'HELICOPTERE A CIRCULATION DE CONTOURNEMENT AUGMENTEE
AIR INLET FOR HELICOPTER ENGINE WITH INCREASED CIRCUMFERENTIAL INTAKE LIPS
LUFTEINLASS FÜR HUBSCHRAUBERMOTOR MIT VERGRÖSSERTEN UMFANGSEINLASSLIPPEN
26.02.2020
Patent
Elektronische Ressource
Französisch
ENTREE D'AIR POUR MOTEUR D'HELICOPTERE A CIRCULATION DE CONTOURNEMENT AUGMENTEE
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