Aircraft turbine engine comprising an air intake housing with a variable aerodynamic profile
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United States of America Patent
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app pub date -
Oct 30, 2015
filing date -
Nov 6, 2014
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Abstract
An aircraft turbine engine includes a fan duct having a wall; an air passage arranged in the wall and including an air inlet opening at the wall, the air passage being designed to receive part of the flow of air from the fan duct across the opening; an air intake housing located above the air inlet opening and fixed to the wall, the housing being arranged to intercept part of the air flow in the fan duct, and successively including, in the air flow direction, an upstream wall then a downstream wall, an upstream opening and a downstream opening arranged on the upstream wall and the downstream wall, respectively, the inside of the housing being in fluidic connection to the air inlet opening, and a movable sealing means between an “open” position; and a “closed” position relative to the downstream opening and the air inlet opening.
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