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
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