Device with remote motor for controlling an aerodynamic control surface of a missile
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United States of America Patent
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N/A
Issued Date -
Dec 28, 2006
app pub date -
Jul 8, 2005
filing date -
Jul 9, 2004
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
An aircraft comprising at least one aerodynamic control surface (26) controlled using a remote motor (4), through a transmission comprising a linear device (7) rigid in torsion but flexible in bending and in tension and compression, to absorb thermomechanical deformations. This transmission comprises small clearances, good flexibility, does not require any additional support and makes favourable use of a reduction gear (9) located near the control surface (26) rather than near the motor (4).
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