发明名称 |
Gas turbine engine bearing support |
摘要 |
A bearing support for a rotor (12) of an aircraft turbine engine (10) includes a front bearing and a front bearing support (118) and bearing strut (120) for securely attaching the front bearing to the aircraft turbine engine support structure (122). The front bearing support (118) and bearing strut (120) are integral with the aircraft turbine engine support structure (122). |
申请公布号 |
EP1447543(A3) |
申请公布日期 |
2007.01.17 |
申请号 |
EP20040250779 |
申请日期 |
2004.02.13 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DITOMASSO, JOHN C. |
分类号 |
F02C7/06;F01D25/00;F01D25/16;F01D25/28;F02C7/20;F16C3/02;F16C27/04 |
主分类号 |
F02C7/06 |
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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