Aircraft engine pylon

An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of r...

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Bibliographische Detailangaben
Hauptverfasser: Journade, Frederic, Terral, Romain, Bouchet, Eric, Coudouent, Gerard, Rogeron, Cyrielle, Cros, Sylvain, Sina, Bogdan, Puech, Jerome
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of reinforcements. The pylon also includes a reinforcement zone on each side panel and a front housing to receive a main front center reinforcement and a rear housing to receive a main rear center reinforcement.