Variable stator blade supporting structure
A technology of stator blades and supporting structures, applied in the field of turbines
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[0024] Referring now to the drawings, and in particular to figure 1 , shows a part of the axial flow compressor 10 in enlarged detail. Two series-connected compressor stages are shown, each of which includes a number of circumferentially spaced, generally radially extending stator blades 12, 14, only one of which is shown. Also forming part of each compressor stage are a plurality of circumferentially spaced, generally radially extending rotor blades 16, 18 carried by respective rotor disks 20, 22, only one of which is shown. An annular casing 24 surrounds and encloses each compressor stage to define the outer circumference of the annular flow path through the compressor. The rotor disks 20, 22 are each drivably connected to a frustoconical drive shaft which is operatively connected to a high pressure turbine (not shown) which supplies torque to the rotary compressor shaft.
[0025] The stator vanes 12 are identical to 14 and are also described below, having a longitudinal a...
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