A landing gear (0) for an aircraft comprising a wheel (R), a system (1) for rotationally driving the wheel that is mobile between a clutched position and a safety position by passing through a declutched position, and a manoeuvring system (3) to displace the driving system (1) between its declutched and clutched positions. The gear comprises an elastic return (4) for returning the driving system (1) to its safety position and first and second abutments (51a, 52a) that are separated as long as the driving system (1) is away from its safety position and in contact with one another when the driving system (1) is in safety position. The first and second abutments (51a, 52a) oppose the passing of the driving system (1) from its safety position to its declutched position when the abutments are in contact with one another.
SYSTEME DE DESENGAGEMENT VERROUILLABLE D'ACTIONNEUR DE ROUE SUR UN ATTERISSEUR D AERONEF
LOCKABLE WHEEL ACTUATOR DISENGAGEMENT SYSTEM ON AN AIRCRAFT LANDING GEAR
VERRIEGELBARES DEBLOCKIERSYSTEM EINES STELLGLIEDS AM RAD DES FAHRWERKS EINES LUFTFAHRZEUGS
03.07.2019
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
SYSTEME DE DESENGAGEMENT VERROUILLABLE D’ACTIONNEUR DE ROUE SUR UN ATTERISSEUR D’AERONEF.
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