TURBOFAN ENGINE COMPRISING A THRUST REVERSER UNIT WITH TILTING BEAMS

The invention relates to a turbofan engine (100) comprising a motor (252) and a nacelle (102) defining a bypass channel (250). The turbofan engine (100) comprises a thrust reverser unit (204) comprising a fixed structure (206), an external door (208) and an internal door (210) mobile in rotation on...

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Bibliographische Detailangaben
Hauptverfasser:	ANDREANI, Luc, GARDES, Pascal, RIDRAY, Frédéric
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to a turbofan engine (100) comprising a motor (252) and a nacelle (102) defining a bypass channel (250). The turbofan engine (100) comprises a thrust reverser unit (204) comprising a fixed structure (206), an external door (208) and an internal door (210) mobile in rotation on the fixed structure (206). The turbofan engine (100) comprises a mechanism (270) moving the doors (208, 210) from a stocked position to a deployed position and comprising at least one beam (272) articulated on the fixed structure (206) around a main axis (274), for each beam (272), an external rod (276) articulated by one end to the beam (272) and by the other end to the external door (208), for each beam (272), an internal rod (278) articulated by one end to the beam (272) and by the other end to the internal door (210), and an actuator (280) moving the beam (272) around the main axis (274).Such a thrust reverser unit comprises a simple mechanism to move the doors.