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