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AssigneeSafran Aircraft Engines
InventorsPaco MAURER, Julien Fabien Patrick BECOULET, Serge Rene MORREALE, Nicolas STOLIAROFF-PEPIN
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A scoop for an aircraft turbine engine, this scoop including a body which is movable between at least two positions, including a first position in which it is configured to capture part of a first air stream flowing in a first direction, wherein the body is movable into a second position in which it is configured to capture part of a second air stream flowing in a second direction which is opposite to the first direction, and wherein the body is mounted to move freely between the at least two positions so as to automatically adopt the first position when the first air stream flows, and to automatically adopt the second position when the second air stream flows.
A scoop for an aircraft turbine engine, this scoop comprising a body which is movable between at least two positions, including a first position in which it is configured to capture a part of a first air stream flowing in a first direction, wherein said body is movable into a second position in which it is configured to capture a part of a second air stream flowing in a second direction which is opposite to the first direction and in that said body is mounted to move freely between said at least two positions so as to automatically adopt the first position when the first air stream flows, and to automatically adopt the second position when the second air stream flows.
Dependencies are inferred from the claim text.