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    • 2. 发明授权
    • Device for radially centering turbine housings
    • 用于放射性中心涡轮外壳的装置
    • US3754833A
    • 1973-08-28
    • US3754833D
    • 1972-04-17
    • KRAFTWERK UNION AG
    • REMBERG A
    • F01D25/26
    • F01D25/265F05D2230/642
    • In order to attain an axially fixed mounting of the inner shell of a turbomachine housing in the vicinity of the bearing and centering locations of a respective, axially-normal plane, a pocket space of a groove widening provided in an axial groove formed in the outer shell of the housing is located, as viewed from the outside, axially behind a respective retaining claw received in the axial groove and is formed by a reduction of the narrower axial groove with respect to the groove widening. Another fitting member in form of a cross bar is insertable into the pocket space, rearwardly engages the retaining claw and abuts axially against housing shoulders located in vicinity of a bottom surface of the pocket space, thereby fixing the inner shell against displacement in one axial direction. The inner shell is formed with annular surfaces abuttable against corresponding annular shoulder-countersurfaces formed on the outer shell, thereby fixing the inner shell against displacement in the other axial direction.