发明名称 Electromechanical aircraft brake with tiltable actuators
摘要 The invention relates to an electromechanical brake, in particular for aircraft, the brake comprising a support carrying at least one electromechanical actuator comprising a pusher that is axially displaceable towards friction elements in order to apply a braking force to the friction elements, selectively, wherein the actuator is mounted on the support via a connection member allowing at least a portion of the actuator carrying the pusher to tilt angularly.
申请公布号 US8844682(B2) 申请公布日期 2014.09.30
申请号 US200611429258 申请日期 2006.05.08
申请人 Messier-Bugatti-Dowty 发明人 Perrault Maurice;Chico Philippe
分类号 F16D55/36;F16D65/18;F16D121/24 主分类号 F16D55/36
代理机构 Sughrue Mion, PLLC 代理人 Sughrue Mion, PLLC
主权项 1. An electromechanical brake, the brake comprising: friction elements, at least one electromechanical actuator, said at least one electromechanical actuator comprising : a housing, a pusher that is moveable within said housing, a driving member comprising an electric motor that actuates said pusher, and, a transmission unit comprising a screw-and-nut system that is driven in rotation by said driving member and that drives in translation said pusher so as to move axially the pusher towards said friction elements in order to apply a braking force to the friction elements, selectively, and, a support carrying said at least one elecromechanical actuator, wherein both said driving member and said transmission unit extend inside said housing, wherein said at least one actuator is mounted on said support via a connection member that couples said housing to said support, allowing at least a portion of the actuator carrying the pusher to tilt angularly, whereby the pusher as a whole can entirely tilt angularly with respect to the support.
地址 Velizy, Villacoublay FR