发明名称 Thermally operated rotatable component restraint system
摘要 A turboalternator system includes a turboalternator having a rotatable member operatively engaged to a bearing set, a radial support element, and a contact structure engaged with the radial support element. The rotatable member defines a first end, a second end and an axis of rotation. The turboalternator system is configured to be thermally adjustable such that in a first thermal condition the contact structure is at a first radial position with respect to the axis of rotation and contacts the rotatable member to provide support, and in a second thermal condition the contact structure is at a second radial position with respect to the axis of rotation that is spaced further from the axis of rotation than the first radial position.
申请公布号 US2008197634(A1) 申请公布日期 2008.08.21
申请号 US20070708621 申请日期 2007.02.20
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 HIMMELMANN RICHARD A.
分类号 H02K7/18 主分类号 H02K7/18
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