Rotary-shaft brake system, in particular for an aircraft rotor or propeller, including a linear actuator
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United States of America Patent
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Oct 13, 2015
Grant Date -
Aug 21, 2014
app pub date -
Nov 20, 2012
filing date -
Nov 21, 2011
priority date (Note) -
In Force
status (Latency Note)
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Abstract
Rotary-shaft brake system includes a rotary braking member attached to a rotary shaft, first and second friction members arranged on either side of the rotary braking member, each friction member being moveable between a first braking position when the friction members are in contact with the rotary braking member and a second idle position away from the rotary braking member, a bracket holding the friction members and guiding device and control device controlling movement of the friction members on the bracket. The control device comprises a linear actuator acting on at least a first lever and a solid elastically deformable element.
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