Dual control mechanism for aircraft
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United States of America Patent
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-
Jun 27, 1995
Grant Date -
N/A
app pub date -
Feb 24, 1993
filing date -
Feb 24, 1993
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A control mechanism for aircraft having a vertically extending, short stub with a cross bar attached to its upper end and a pair of arcuate lower members extending from the cross bar toward the forward end of the aircraft with an adjustable positioning arm on each lower member extending rearwardly and which mounts a hand grip for controlling the aircraft. In a single control mechanism, one arcuate lower member is attached directly to the stub.
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