发明名称 Blade segment of a flow engine with radial support surfaces
摘要 <p>The blade segment (1) has a blade (3) having a tip that is connected to a shroud (7) having a contact surface (11). A tip of another blade (3') is connected to another shroud (7') having an opposite bearing surface (12'). The contact surface of the shroud (7) is arranged in radial direction (R) such that the frictional engagement is provided between the contact surface and the bearing surface. The blades are made of creeping material stronger than nickel material.</p>
申请公布号 EP2460979(A1) 申请公布日期 2012.06.06
申请号 EP20100193687 申请日期 2010.12.03
申请人 MTU AERO ENGINES GMBH 发明人 BOECK, ALEXANDER
分类号 F01D5/22 主分类号 F01D5/22
代理机构 代理人
主权项
地址