发明名称 Guide blade assembly and fluid flow engine
摘要 The vane ring has a static inner ring that is provided for radial inner stabilization of the guide vanes. The sealing elements are provided to seal a radial gap between the inner ring and opposed rotor portion. A connecting device (8) arranged in region of separating joints (52) is provided to connect the adjacent carrier segments (48,50). The connecting device is provided with cooperating connecting elements (70,72) which are respectively formed on the end of carrier segments.
申请公布号 EP2725200(A1) 申请公布日期 2014.04.30
申请号 EP20120189935 申请日期 2012.10.25
申请人 MTU AERO ENGINES AG 发明人 ZOTZ, GEORG;BECKER, HERMANN;MAIRHANSER, VITALIS
分类号 F01D9/04;F01D17/14;F01D17/16 主分类号 F01D9/04
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