| 发明名称 |
Gas turbine engine bearing support |
| 摘要 |
To further isolate imbalances in a rotating structure such as a gas turbine engine, an effective length (L 1 ) between two bearings (60, 70) may exceed an actual length (L). This may be achieved via one or more tapering bearing supports (72) associated with at least one of the bearings (70). |
| 申请公布号 |
EP1596038(A2) |
申请公布日期 |
2005.11.16 |
| 申请号 |
EP20050252863 |
申请日期 |
2005.05.10 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
VAN DUYN, KEVEN G. |
| 分类号 |
F01D21/04;F01D25/16;F02C7/00;F02C7/06;F02K3/06;F16C27/04;F16C35/07 |
主分类号 |
F01D21/04 |
| 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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