AIR INTAKE SYSTEM FOR AN AIR VEHICLE
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United States of America Patent
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Issued Date -
Oct 31, 2013
app pub date -
Nov 23, 2011
filing date -
Dec 1, 2010
priority date (Note) -
Abandoned
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Abstract
A missile comprises a propulsion system, a passageway for delivering air to the propulsion system and a ducting element associated with the passageway. The ducting element has a ducting surface for ducting air into the passageway, and the ducting element is rotatable, about an axis that is aligned, or more preferably co-axial, with the axis of the passageway, from a stowed position in which the ducting surface is received in the passageway, to a deployed position in which the ducting surface protrudes from the passageway to duct air into the passageway.
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