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Centrifugal Compressors Chapter  3 33


             some machines employ variable guide vanes to induce swirl and alter the rel-
             ative flow angle seen by the compressor. After passing through the inlet, the
             flow is directed into the impeller. It is the impellers responsibility to increase
             the kinetic and potential energy of the gas by pushing it tangentially. This
             requires torque that is transferred to the impeller by the shaft, which is ulti-
             mately turned by a driver. After the flow leaves the impeller at high velocity,
             it slows down in the diffuser building pressure. Due to losses and the heat of
             compression, the gas builds up temperature as pressure increases. If there are
             more compression stages, the gas leaves the diffuser and enters a return channel,
             which directs the flow back to the inlet of the next stage. Once the gas leaves the
             final stage of compression in a given section, it passes from the diffuser into a
             collector or volute that directs the flow radially outward through the discharge
             flange.
                Other components consist of the casing that acts as an overall structure and
             pressure vessel. Seals and walls separate the stages and ensure that gas follows
             the primary path, minimizing leakage from the flow path. The shaft acts as the
             inner boundary of the flow and also supports and drives the impellers, which in
             turn performs the work and drives the gas. Bearings act as shaft support both
             radially and axially and as part of an overall rotor-bearing dynamic system that
             is tuned to allow robust operation of the machine.


             Types/Configuration
             Inline compressors typically have centrifugal stages located in between the
             bearings; however, the casing can be packaged in a few different configurations.
             They are typically a barrel style, horizontally split, or hermetically sealed.


             Barrel
             Fig. 3.2 shows a barrel-style compressor. In this photo, the rotor bundle, com-
             posed of rotor and stator blade passages that composes the compressor, is being
             removed axially from the casing. The casing has the responsibility of locating
             the centerline of the compressor relative to the ground and containing the pres-
             sure, while the bundle is responsible for directing the flow during the compres-
             sion process. Having no horizontal split, a barrel-style casing can operate at very
             high pressures.


             Horizontal Split
             Compressors with horizontal split casings as shown in Fig. 3.3 are used in rel-
             atively low-pressure applications having a pressure limitation of roughly 7MPa
             that is governed mostly by the ability to seal the split line against leakage. These
             horizontal split casing designs may also be described as “axially split.” The hor-
             izontal split of the casing is flat and bolted around the periphery with numerous
             split-line bolts to prevent leakage.
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