| 摘要 |
The invention relates to an axial compressor stator for a gas turbine, said stator comprising a rigid, external, annular frame (2), furthermore axially juxtaposed rings (4a, 4b, 4c) configured within the frame (2) and bearing annuli of stationary vanes (5), said rings being constituted by arcuate segments (7) affixed to the frame, the inside walls of said arcuate segments externally defining the aerodynamic conduit for the compressed gaseous fluid, and this invention is characterized in that the arcuate segments (2) are brazed segments consisting of a honeycomb component (8) sandwiched between an inner sheetmetal (10) bounding the aerodynamic conduit and an outer sheetmetal (9), and in that the connection to the frame (2) is solely implemented by the outer sheetmetal (9).
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