Control linkage for T-tail aircraft elevator surfaces
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United States of America Patent
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Feb 19, 2008
Grant Date -
N/A
app pub date -
Dec 2, 2004
filing date -
Dec 2, 2004
priority date (Note) -
Expired
status (Latency Note)
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Abstract
Systems and methods for implementing control linkages that may be employed to produce synchronous motion in two adjacent controlled devices controlled by a common input. In one example implementation, a semi-rigid modified constant velocity (CV) joint control linkage may be provided that is laterally self-stabilizing. The modified constant velocity CV joint control linkage may include an input push rod assembly that is self-aligning, deflectable and of an adjustable length. The CV joint may be configured with a central cage that is allowed to skew to allow for alignment of the controlled devices.
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