Hydraulic actuation system for aircraft control surfaces
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United States of America Patent
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Jul 23, 1996
Grant Date -
N/A
app pub date -
Nov 2, 1993
filing date -
Nov 2, 1993
priority date (Note) -
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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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