发明名称 Securing module for axial securing of a root of a turbo engine blade
摘要 The securing unit (20) i.e. securing plate, has a partially curved outer contour (24) facing toward a groove wall that is designed as a groove base (33). The outer contour includes different radii (R1-R3), where the first radius is arranged between the second and third radii, and the second radius is larger than the first and third radii. A section of the outer contour forms a securing unit-contact region (21) that is arranged in contact with a groove contact region (31) of the groove wall, where the securing unit includes an elastic material.
申请公布号 EP2455588(B1) 申请公布日期 2017.03.01
申请号 EP20100191240 申请日期 2010.11.15
申请人 MTU Aero Engines AG 发明人 Stanka, Rudolf;Dopfer, Manfred;Pernleitner, Martin;Schütte, Wilfried
分类号 F01D5/26;F01D5/30 主分类号 F01D5/26
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