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.
Helicopter engine air intake with increased bypass flow
11.09.2018
Patent
Elektronische Ressource
Englisch
HELICOPTER ENGINE AIR INTAKE WITH INCREASED BYPASS FLOW
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