| 摘要 |
Turbo compressor in an axial type of construction, having a bladed stator and a bladed rotor, and having a longitudinally split compressor casing and a guide blade ring with adjustable guide blades, wherein the guide blades are pivotably mounted about radial axes radially within their aerofoil on an inner ring belonging to the stator. The inner ring is split, i.e. segmented, at at least two points of its circumference; furthermore, the inner ring has for each guide blade at least one bearing bush which can be inserted radially into an opening from inside. |
