发明名称 |
Bladed disk fixing undercut |
摘要 |
An undercut is provided in a gas turbine engine disk to smooth out an uneven axial distribution of radial stress in the disk. The undercut is defined radially inwardly of the blade attachment slots provided at the periphery of the disk.
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申请公布号 |
US2005254952(A1) |
申请公布日期 |
2005.11.17 |
申请号 |
US20040845189 |
申请日期 |
2004.05.14 |
申请人 |
STONE PAUL |
发明人 |
STONE PAUL |
分类号 |
B63H1/20;F01D5/02;(IPC1-7):B63H1/20 |
主分类号 |
B63H1/20 |
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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