发明名称 |
Method for mounting an integral inner ring of a turbocompressor stator |
摘要 |
A method for mounting an integral inner ring (10) of a turbocompressor stator to a guide vane ring (12) comprises the following steps: -Providing the guide vane ring (12) with an inner radius S; -Providing inner ring (10) with an outer radius R, which corresponds to the inner radius S; -Pre-tensioning inner ring (10) to an outer radius r that is smaller than the outer radius R of the untensioned inner ring (10); and -Relaxing inner ring (10) to the outer radius R. |
申请公布号 |
US8943689(B2) |
申请公布日期 |
2015.02.03 |
申请号 |
US201013143358 |
申请日期 |
2010.01.14 |
申请人 |
MTU Aero Engines GmbH |
发明人 |
Stiehler Frank |
分类号 |
B21K25/00;F01D9/04;F01D17/16;F01D25/24 |
主分类号 |
B21K25/00 |
代理机构 |
Barlow, Josephs & Holmes, Ltd. |
代理人 |
Barlow, Josephs & Holmes, Ltd. |
主权项 |
1. A method for mounting an integral inner ring of a turbocompressor stator to a guide vane ring having the following steps:
providing the guide vane ring with an inner radius S; providing the inner ring with an outer radius R, which corresponds to the inner radius S; pre-tensioning the inner ring to an outer radius r, which is constant over the periphery of the inner ring and which is smaller than the outer radius R of the untensioned inner ring; and unwinding the inner ring in the guide vane ring by relaxing the inner ring to the outer radius R; wherein for pre-tensioning the inner ring, a die plate having a radius whose outer radius is smaller than the outer radius R of the untensioned inner ring minus its radial thickness is used. |
地址 |
Munich DE |