A turbofan engine nacelle has a downstream section which includes at least one front frame. The front frame is attached to a stationary portion of the nacelle, and the downstream section is provided with at least one rail or slide which extends in a longitudinal direction of the nacelle and is capable of engaging with at least one corresponding slide or rail of an attachment pylon of the turbofan engine. The front frame is connected to the rail or slide of the downstream section by means of at least one swiveled connecting rod.
Turbojet engine nacelle with downstream section
2016-05-17
Patent
Elektronische Ressource
Englisch
Turbojet engine nacelle with variable ventilation outlet cross section
Europäisches Patentamt | 2017
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