发明名称 |
Multi-function heat shield for a gas turbine engine |
摘要 |
A rotor disk assembly for a gas turbine engine includes a rotor disk with a circumferentially intermittent slot structure that extends radially outward relative to an axis of rotation. A heat shield has a multiple of radial tabs engageable with the circumferentially intermittent slot structure to provide axial retention of the cover plate to the rotor disk. |
申请公布号 |
US8662845(B2) |
申请公布日期 |
2014.03.04 |
申请号 |
US201113004231 |
申请日期 |
2011.01.11 |
申请人 |
VIRKLER SCOTT D.;ARNOLD JASON;UNITED TECHNOLOGIES CORPORATION |
发明人 |
VIRKLER SCOTT D.;ARNOLD JASON |
分类号 |
F01D5/08;F01D5/18 |
主分类号 |
F01D5/08 |
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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