发明名称 Electric brake actuator module for aircraft
摘要 An electro-mechanical brake assembly comprising a brake disk stack having a center axis; and a plurality electro-mechanical actuators for applying braking pressure to the brake disk stack. The actuators are circumferentially arranged around the center axis, and each actuator includes a housing, a linearly movable ram, a screw for linearly moving the ram, a nut mounted for rotation in the housing and operatively engaged with the screw such that rotation of the nut effects linear movement of the screw for urging the ram into forceful engagement with the brake disk stack, an electric motor for rotating the nut, and an anti-rotation device for preventing rotation of the screw relative to the housing when the nut is rotated to effect linear movement of the screw. The foregoing arrangement provides for greater stroke than prior art actuators without sacrificing durability and performance.
申请公布号 AU1365301(A) 申请公布日期 2001.04.17
申请号 AU20010013653 申请日期 2000.09.12
申请人 THE B.F. GOODRICH COMPANY 发明人 THOMAS H. HAYDON;MICHAEL J. ORTMAN;STEVEN ANDERSON;ERIC SCHWAIGERT
分类号 F16D55/00;F16D55/36;F16D65/14;F16D65/18;F16D66/00 主分类号 F16D55/00
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