Example high-fowler flap actuation apparatus and related methods are disclosed. An example apparatus includes a control surface operatively coupled to a wing of an aircraft via a first support arm and a drive arm, the drive arm linearly extendible from a retracted position to a deployed position, the deployed position including the control surface extended away from the wing at a first angle with respect to the wing.
HIGH-FOWLER FLAP ACTUATION APPARATUS AND RELATED METHODS
2019-03-28
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
High-fowler flap actuation apparatus and related methods
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|Engineering Index Backfile | 1941
|Emerald Group Publishing | 1936
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