AIRCRAFT TURBOMACHINE HAVING A VARIABLE SECTION AIR INTAKE

摘要

A turbomachine for an aircraft comprising a fan duct delimited by a wall and through which an air stream flows from upstream to downstream, and an air passage arranged in the wall comprising an air inlet opening flush with the wall, the air passage being designed to draw part of the air flow of the fan duct through the air inlet opening. To control the amount of air entering the air passage, a flap is rotatably mounted on the wall of the fan duct, about an axis of rotation disposed downstream of the air inlet opening, between an open position, in which the flap partially closes the air inlet opening and leaves free the fan duct downstream of the air inlet opening, and a closed position, in which the flap leaves open the air inlet opening and partially closes the fan duct downstream of the air inlet opening.