发明名称 |
Flow engine seal assembly |
摘要 |
The arrangement has shells (1-3) connected with one another in a circumferential direction (U) and arranged adjacent to each other in an axial direction (A). The shells comprise V or U-shaped cross sections opened opposite to a through flow direction and/or thread axis inclined opposite to the through flow direction. The cross sections are constant over the entire length of the shells, and the arrangement is arranged at a rotor and/or stator of a turbomachine. The thread axis is inclined at an angle to a radial direction (R), where the angle amounts to preferably 50 degrees. An independent claim is also included for a method for manufacturing a sealing arrangement. |
申请公布号 |
EP2617949(A2) |
申请公布日期 |
2013.07.24 |
申请号 |
EP20130151103 |
申请日期 |
2013.01.14 |
申请人 |
MTU AERO ENGINES GMBH |
发明人 |
WERNER, ANDRE;PRIESCHL, FRANZ;HES, THOMAS;SCHLOTHAUER, STEFFEN |
分类号 |
F01D11/08 |
主分类号 |
F01D11/08 |
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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