| 摘要 |
A gas-turbine axial compressor has a casing 3 and a rotatable shaft 5, which form an annular duct, in which at least one stator 2 and one rotor 4 are arranged. A shroud 21 is arranged at a free end of the stator 2 vanes, which extends over part of the axial length of the stator 2. A further part of the axial length of the stator 2, at which no shroud 21 is arranged, radially adjoins a rotor platform 28 formed by a rotor hub 8.
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