发明名称 Plastically deformable layer in the mounting area of a turbine blade and method of turbine blade attachment
摘要 <p>System for fixing a blade in the flow channel of a turbo machine comprises a rotor shaft (1) rotating in a housing. The blade is fixed in a connecting region on the rotor shaft or on the wall of the flow channel. The connecting region has a deformable layer (7). An independent claim is also included for a process for fixing a blade in the flow channel of a turbo machine. Preferred Features: A deformable layer is formed by a coating of a connecting contour (3) of the blade and/or a contour (5) of the rotor shaft or the wall of the flow channel.</p>
申请公布号 EP1561905(A1) 申请公布日期 2005.08.10
申请号 EP20040002822 申请日期 2004.02.09
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 DAVID, WALTER;RICHTER, CHRISTOPH, DR.
分类号 F01D5/30;(IPC1-7):F01D5/30 主分类号 F01D5/30
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