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.
Nacelle for a turbojet engine with a variable nozzle
2018-11-13
Patent
Electronic Resource
English
Turbojet engine nacelle with variable ventilation outlet cross section
European Patent Office | 2017
|