发明名称 Actuator with limited travel and emergency upcoupling
摘要 The invention relates to an actuator drive mechanism with a control motor (1), which on the power takeoff side drives a control gear that includes a final control element (3) on the drive side and a final control element (5) on the power takeoff side, and the final control element (5) on the power takeoff side cooperates with an adjusting element (11), by way of which engines or machines can be varied in their operating behavior. Associated with the final control element (3, 5) on the drive side or the power takeoff side is a power takeoff component (8), which includes a force-transmission-free region (25), and on which a spring element (21) is received movably in a recess (19).
申请公布号 US2004012281(A1) 申请公布日期 2004.01.22
申请号 US20030343364 申请日期 2003.01.30
申请人 NEUBAUER ACHIM;ASCHOFF JOERG;DILGER WERNER;PIERENKEMPER ROLF;BOLZ MARTIN-PETER 发明人 NEUBAUER ACHIM;ASCHOFF JOERG;DILGER WERNER;PIERENKEMPER ROLF;BOLZ MARTIN-PETER
分类号 F16H1/16;F16H19/00;(IPC1-7):F16H19/00 主分类号 F16H1/16
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