| 摘要 |
The present invention relates to a stator heat shield (6) for a gas turbi ne (1), comprising an outer side (11) which, in the installed state, faces a hot gas path (9) of the gas turbine (1), an inner side (12) facing away fro m the outer side (11), multiple ribs which are formed at the inner side (12) and which, in the installed state, extend axially with respect to an axis o f rotation (8) of a rotor (3) of the gas turbine (1) and which are at a dist ance from one another in the circumferential direction, at least one splash plate (14) which is disposed at the inner side (12) and which lies on the ri bs (13), at least one groove (16) which is formed in a front face (15) which forms the boundary of the stator heat shield (6) in the circumferential dir ection and into which at least one sealing element (18) can be inserted, and multiple boreholes (19) which terminate at a distance from one another in t he direction to the outer side (11), with one end at the inner side (12) and the other end at the front face (15) of the groove (16), and which are at a distance from one another in the axial direction.
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