Door-closing system for a thrust reverser of an aircraft nacelle
AssigneeSafran Nacelles
InventorsPierre Caruel, Alexandre Descamps
Life of this patent
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AssigneeSafran Nacelles
InventorsPierre Caruel, Alexandre Descamps
Estimating the term…
A closing system that includes a closing actuator for doors of a thrust reverser, two sliding members, and a detection device. The closing actuator includes two first connecting rods. Each first connecting rod is configured to be connected to a first lateral edge of each door. The closing actuator is arranged to move each door at least towards the direct jet position. Each sliding member carries a second connecting rod configured to be connected to a second lateral edge of each door. The second connecting rods are arranged to be driven by the doors when the closing actuator moves the doors towards the direct jet position so as to displace the two sliding members. The detection device detects a defect of one of the first and second connecting rods. The detection device is configured to detect the relative position of the two sliding members in the direct jet position.
A closing system for a pair of doors for a thrust reverser of an aircraft nacelle, the doors being diametrically opposed and pivotally mounted between a direct jet position in which the doors provide aerodynamic continuity of the aircraft nacelle, and a reverse jet position in which the doors open at least one passage in the aircraft nacelle, the closing system comprising:
A method for using a closing system for a pair of doors for a thrust reverser of an aircraft nacelle, the doors being diametrically opposed and pivotally mounted such that the doors are pivotable between a direct jet position in which the doors provide aerodynamic continuity of the aircraft nacelle, and a reverse jet position in which the doors open at least one passage in the aircraft nacelle, the closing system comprising:
A method for using a closing system for a pair of doors for a thrust reverser of an aircraft nacelle, the doors being diametrically opposed and pivotally mounted such that the doors are pivotable between a direct jet position in which the doors provide aerodynamic continuity of the aircraft nacelle, and a reverse jet position in which the doors open at least one passage in the aircraft nacelle, the closing system comprising:
Dependencies are inferred from the claim text.