Aircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle

A nacelle for an aircraft turbofan includes a rear section including a thrust reversal device having an upper door and a lower door, the upper and lower doors being mobile in rotation between a stowed position in which they are aerodynamically continuous with the rest of the nacelle and a deployed p...

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Bibliographische Detailangaben
1. Verfasser: Guillois, Denis
Format: Patent
Sprache:eng
Schlagworte:
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