Differential linkage apparatus for an aircraft series servoactuator apparatus
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Jan 17, 1984
Grant Date -
N/A
app pub date -
Mar 12, 1982
filing date -
Mar 12, 1982
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
In a servoactuator system for an aircraft, a strapdown series servoactuator having an external linkage assembly is coupled between the pilot's control stick and a control surface member. The external linkage assembly includes a differential link and servo link having specially tapered stop surfaces adapted to be varied in dimensions to accommodate a wide variety of installations, which stop surfaces cooperate with fixed stops on the servoactuator housing whereby to provide a variety of pilot authority limits and series servo authority limits depending upon particular installation requirements.
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