Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct
AssigneeAirbus Operations GmbH
InventorsPascal Gardes, José Goncalves, Bastian Sabathier
Life of this patent
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AssigneeAirbus Operations GmbH
InventorsPascal Gardes, José Goncalves, Bastian Sabathier
Estimating the term…
A turbofan having a nacelle comprising a slider mobile in translation between an advanced and a retracted position to open a window between a duct and the exterior, a plurality of blades, each one mobile in rotation on the slider between a stowed and a deployed position, where the blades are split into groups, where each group comprises a first blade, and a maneuvering system moving each blade and comprising a cam integral with the first blade of one of the groups and having a tooth, a groove receiving the tooth, a first transmission system transmitting the movement of the first blade bearing the cam to a first blade of each other group, and, for each group, a second transmission system transmitting the movement of the blade that bears the cam or is moved by the first transmission system to each of the other blades of the group.
A turbofan having a longitudinal axis and comprising a motor and a nacelle, surrounding the motor, which comprises a fan casing, in which a duct for a bypass flow is delimited between the nacelle and the motor and in which a flow of air flows in a flow direction, said nacelle comprising:
Dependencies are inferred from the claim text.