发明名称 Buckling resistant piezoelectric actuator
摘要 A piezoelectric actuator assembly allows maximization of the cross-sectional area of a piezoelectric driver assembly such that axial stiffness of the actuator assembly is substantially increased. The actuator assembly is coupled to an application structure and includes the piezoelectric driver assembly having a stack inboard end longitudinally extending in an inboard direction with respect to the application structure. The driver assembly also has a stack outboard end longitudinally extending in an outboard direction with respect to the application structure. The driver assembly further provides a longitudinal displacement in response to an applied voltage. The actuator assembly also includes an amplification arm having an arm outboard end coupled to a load. An outboard hinge mechanism rotatably couples an arm inboard end of the amplification arm to the stack outboard end such that the arm outboard end extends in the outboard direction. Voltage signals selectively applied to the driver assembly cause rotational displacement of the amplification arm.
申请公布号 US6307301(B1) 申请公布日期 2001.10.23
申请号 US20000497048 申请日期 2000.02.02
申请人 THE BOEING COMPANY 发明人 NGO HIEU THIEN;BIRCHETTE TERRENCE SELWYN;WEISENBURGER RICHARD KARL;STEMPLE ALAN DOUGLAS
分类号 H01L41/09;H02N2/00;(IPC1-7):H01L41/08 主分类号 H01L41/09
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