发明名称 Frangible bearing support for a turbomachine rotor
摘要 <p>The break point (14) is formed by dividing the non-rotating bearing support (26) into sections (26a, 26b) and providing two partition surfaces (28a, 28b) extending at right angles to the bearing rotation axis. Guide surfaces evenly distributed around the bearing support periphery are provided in between the support sections and arranged in pairs in opposing partition surfaces. These partition surfaces and the guide bodies housed in between the guide surfaces are held in contact with each other without play using axially oriented clamping screws (32) evenly distributed around the bearing support periphery and applying a pre-determined tensile force. Bearing forces (44) acting upon the bearing support are converted into axial tensile forces acting upon the screws and upon exceeding a pre-determined threshold value, the bearing forces will cause the screws to break.</p>
申请公布号 EP1314858(B1) 申请公布日期 2009.01.28
申请号 EP20020024038 申请日期 2002.10.28
申请人 MTU AERO ENGINES GMBH 发明人 DIEPOLDER, WOLFGANG, DR.;WOEHRL, BERNHARD, DR.
分类号 F01D21/04;F01D25/16;F16C19/52;F16C35/04;F16D9/04 主分类号 F01D21/04
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