发明名称 Shape memory alloy actuator
摘要 An aircraft system may include an airfoil and a deployable device coupled to the airfoil. The system may further include a shape memory alloy actuator coupled between the airfoil and the deployable device. The actuator may be movable between a first position with the deployable device deployed relative to the airfoil, and a second position with the deployable device stowed relative to the airfoil. The system may additionally include an activatable link positioned between the actuator and the deployable device. The link may have an engaged configuration in which motion of the actuator is transmitted to the deployable device, and a disengaged configuration in which motion of the actuator is not transmitted to the deployable device.
申请公布号 US8118264(B2) 申请公布日期 2012.02.21
申请号 US20100960271 申请日期 2010.12.03
申请人 MABE JAMES H.;CALKINS FREDERICK T.;BUSHNELL GLENN S.;BIENIAWSKI STEFAN R.;THE BOEING COMPANY 发明人 MABE JAMES H.;CALKINS FREDERICK T.;BUSHNELL GLENN S.;BIENIAWSKI STEFAN R.
分类号 B64C9/00 主分类号 B64C9/00
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