A secondary flight control system is provided. The secondary flight control system comprising: a first flight control surface system; a second flight control surface system; and a power distribution unit operably connected to the first flight control surface system and the second flight control surface system, wherein the power distribution unit is configured to generate torque to actuate the first flight control surface system and the second flight control surface system.
CONTROL OF MULTIPLE FLIGHT CONTROL SURFACE SYSTEMS USING SINGLE POWER DRIVE UNIT
CONTROLE DE PLUSIEURS SYSTEMES DE SURFACE DE CONTROLE DE VOL AU MOYEN D'UN SEUL MODULE D'ENTRAINEMENT
2019-05-22
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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