| 发明名称 |
SUPPORT ASSEMBLY FOR A GAS TURBINE ENGINE |
| 摘要 |
A support assembly (100) for a gas turbine engine (20) includes a control ring (106) that extends about a circumferential axis. A plurality of first supports (104) has a cavity (126) that receives the control ring (106). A plurality of cover plates (108) are attached to the first plurality of supports (104) and enclose the cavity (126). |
| 申请公布号 |
EP3095966(A1) |
申请公布日期 |
2016.11.23 |
| 申请号 |
EP20160170475 |
申请日期 |
2016.05.19 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MILLER, ANDREW S.;BALAWAJDER, PETER |
| 分类号 |
F01D11/18 |
主分类号 |
F01D11/18 |
| 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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