Hydraulic actuation system for aircraft control surfaces

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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Details

244225, 244 75R, 244 78, 244 90R, B64C 1336

Patent

active

055382029

ABSTRACT:
A hydraulic actuation system for an aircraft control surface such as an elevon. A pair of spaced pivot points are provided to alternately rotate the control surface either clockwise or counterclockwise.

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