发明名称 |
ACTUATOR WITH LIMITED TRAVEL AND EMERGENCY UNCOUPLING |
摘要 |
<p>The present 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. 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 within a recess ( 19 ).</p> |
申请公布号 |
EP1360433(B1) |
申请公布日期 |
2005.09.14 |
申请号 |
EP20010984710 |
申请日期 |
2001.12.14 |
申请人 |
ROBERT BOSCH GMBH |
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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|