PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A THRUST REVERSER WITH MOVABLE CASCADES AND WITH AN ACTUATOR MOUNTED IN AN OPTIMIZED MANNER

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A THRUST REVERSER WITH MOVABLE CASCADES AND WITH AN ACTUATOR MOUNTED IN AN OPTIMIZED MANNER

The invention relates to a propulsion assembly for an aircraft equipped with a thrust reverser comprising an actuator (52) for moving a movable structure (29) between an advanced direct thrust position and a retracted thrust reversal position, the propulsion assembly further comprising an actuator s...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BOILEAU, Patrick André, FERRIER, Gina
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 propulsion assembly for an aircraft equipped with a thrust reverser comprising an actuator (52) for moving a movable structure (29) between an advanced direct thrust position and a retracted thrust reversal position, the propulsion assembly further comprising an actuator support device (58) equipped with a first connecting part (60a) for connecting it to the deflection edge (46') and/or to the outer shell (40') of the intermediate casing, with a second connecting part (60b) for connecting it to a body (52a) of the actuator, and with a central part (60c) running axially between the shell (40') and the actuator. Moreover, the actuator support device (58) forms a guide means (66) for a set of cascades (32') of the movable structure.