Rotor assembly for an aircraft capable of hovering and equipped with an improved constraint assembly
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United States of America Patent
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Feb 16, 2016
Grant Date -
Apr 3, 2014
app pub date -
Jun 24, 2013
filing date -
Jun 27, 2012
priority date (Note) -
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status (Latency Note)
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Abstract
A constraint assembly for an aircraft, having a first member; a second member mounted to translate along and rotate about its own axis; and connecting means for connecting the first and second member, to prevent rotation of the second member about the axis with respect to the first member; the connecting means having a retaining arm, which projects outwards from one of the first and second member, and extends at a distance of other than zero from the axis; and an antirotation bracket, which projects from the other of the first and second member, extends at a distance of other than zero from the axis, and defines a through opening engaged in sliding manner by the retaining arm.
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