Described are deployment apparatuses that include a deployment object, a deployment arm with a first end coupled to the deployment object and a second end having a pivot, and a hinge assembly rotatably attached to the pivot of the deployment arm. The hinge assembly includes an enclosure and a friction stop device disposed within the enclosure such that the friction stop device includes a friction portion configured to be pressed against a lateral surface of the pivot of the deployment arm such that the friction portion provides a predetermined torque. The predetermined torque may be calculated based on maintaining a deployed angle of the deployment arm such that the deployment object is held in a raised deployed position.
申请公布号
WO2015006388(A2)
申请公布日期
2015.01.15
申请号
WO2014US45846
申请日期
2014.07.09
申请人
ZODIAC SEATS US LLC
发明人
PARKER, TY, W.;JOHNSTON, JEFFREY;ZEMLER, MATTHEW, K.;DELGADILLO, SEBASTIAN, S.;JONES, MATT