Deployment system for adjusting a leading edge high lift device, in particular a slat, between a retracted position, in which, in use, the high lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the high lift device is deployed with respect to the airfoil, comprising at least one actuation unit that is configured to actuate the high lift device between the retracted position and the at least one deployed position, at least one guidance unit that is configured to guide the high lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path, wherein the guidance unit is independent from the actuation unit.
Deployment System for an Airfoil High Lift Leading Edge Device
2020-01-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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