发明名称 |
COMPLIANT COUPLING FORCE CONTROL SYSTEM |
摘要 |
<p>A force compliant mechanism (750) for a force control system (600) includes a housing (752). A force compliant volute spring member (754) that has an input end (790) and an output end (792) is disposed within the housing (752). A force actuator input shaft (798) operates in response to a force induced thereon. An output shaft (800) is coupled to the output end (792) and to a test object (802). A force transducer (780) is in operative coupling with the force actuator input shaft (798) and generates a force signal in response to the induced force. A method of reducing force transients and increasing stability within a force control system (660) includes applying a force on a test object (666). A force actuator (669) is decoupled from the test object (666). The overall stiffness of the force control system is reduced and dynamic energy is absorbed via a force compliant member (662) coupled to the test object (666) and the force actuator (669).</p> |
申请公布号 |
EP1941332(B1) |
申请公布日期 |
2011.12.21 |
申请号 |
EP20060826522 |
申请日期 |
2006.10.24 |
申请人 |
THE BOEING COMPANY |
发明人 |
ENGLUND, NORMAN J.;FINIGAN, JOHN S. |
分类号 |
G05B19/19;F16F15/027 |
主分类号 |
G05B19/19 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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