Cowl of an aircraft turbine engine comprising a central gripping interface
AssigneeSafran Nacelles
InventorsVivien Lucienne, Tony Dehais, Francois Bellet, Pierre Charles Caruel
Life of this patent
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Abstract
The invention relates to a cowl of an aircraft turbine engine extending about an axis, comprising a conical reinforcement centred about the axis, an external skin fixed around the reinforcement, and a revolution member fixed to the conical reinforcement along the axis and against the external skin, the external skin and the revolution member each comprising a hole coaxial with the axis, the revolution member being configured to allow the cowl to be gripped by inserting a bar into the hole.
Claims11
A cowl for an aircraft turbine engine, extending about an axis, and comprising a conical reinforcement centred about the axis, an external skin fixed around the conical reinforcement, and a revolution member fixed to the conical reinforcement along the axis and against the external skin, the external skin and the revolution member each comprising a hole coaxial with the axis, the revolution member being configured to allow the cowl to be gripped by inserting a bar into the holes.
Dependencies are inferred from the claim text.