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US 2016/0115902 A1Published application
Nacelle for a turbojet engine with a variable nozzle
AssigneeAircelle
InventorsOlivier KERBLER, Olivier GILO, Patrick GONIDEC
Life of this patent
Estimating the term…
Abstract
The present disclosure provides a turbojet engine nacelle having a downstream section including a cowl which is ended with a hinged flap constituting a nozzle. In particular, the hinged flap is hingedly and translatably hinged to the cowl.
Claims14
A nacelle for a turbojet engine having a downstream section comprising at least one cowling ended by at least one hinged flap forming a nozzle, wherein said at least one hinged flap is pivotally and translatably hinged relative to said at least one cowling.
Dependencies are inferred from the claim text.