Method of controlling an electromechanical aircraft brake
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United States of America Patent
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N/A
Issued Date -
Dec 9, 2004
app pub date -
May 26, 2004
filing date -
Jun 6, 2003
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
The invention provides a method of controlling an electromechanical aircraft brake comprising a stack of disks and a ring carrying a plurality of electromechanical actuators each fitted with a pusher that is movable in register with the stack of disks under drive from an associated electric motor so that rotation of the motor in a first direction causes the pusher to be pressed against the stack of disks. According to the invention, the method comprises the step of causing at least one motor to rotate in a second direction opposite to the first direction so as to cause the corresponding pusher to reverse beyond a distance corresponding to normal operating clearance between the pusher and the stack of disks.
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