A latching device for a wing including a support structure (29), a latching bolt (35) having a longitudinal axis (36) and being slidably supported by the support structure (29) such that the latching bolt (35) is movable between a retracted position and an extended position. The latching device (27) includes a first hydraulic actuator (47a) and a first connector assembly (38a) adapted to be connected to a first hydraulic system of an aircraft (1), and at least one second hydraulic actuator (47b) and a second connector assembly (38b) connected to a second hydraulic system. The first hydraulic actuator (47a) and the second hydraulic actuator (47b) are adapted to effect movement of the latching bolt (35) from the extended position into the retracted position independent of the other one of the at least one first hydraulic actuator (47a) and the at least one second hydraulic actuator (47b).
Latching device for a foldable wing arrangement
2020-03-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LATCHING AND LOCKING MECHANISM FOR A FOLDABLE WING ARRANGEMENT
Europäisches Patentamt | 2018
|Latching and locking mechanism for a foldable wing arrangement
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|LATCHING AND LOCKING MECHANISM FOR A FOLDABLE WING ARRANGEMENT
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