Page 80 - Compression Machinery for Oil and Gas
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70  SECTION   II Types of Equipment


            converging taper, a converging taper is recommended as the conservative
            approach. While the direct damping increases as seal clearance divergence
            increases (more diverging, more damping), a cliff is reached where the damping
            suddenly becomes negative and the seal becomes destabilizing. In addition, the
            seal clearance taper can be largely influenced by the seal carrier structure.
            Deflection of the seal carrier or support structure can impact the taper, thus
            influencing the available damping and resulting stability. Overall, seal taper
            and carrier deflection should be considered in a rotordynamic analysis for all
            honeycomb or hole-pattern seals.
               Centrifugal impellers generate destabilizing aerodynamic forces. A widely
            applied approach for predicting the bulk impeller aerodynamic cross-coupling
            coefficients including eye and shaft seal effects is the Wachel method [11]. This
            method was derived when the phenomenon of instability in high-pressure cen-
            trifugal compressors first started to cause problems for oil and gas applications.
            The original Wachel equation for cross-coupling is shown in Fig. 3.35. For com-
            pressors with a single suction and no side streams, this formula may be
            collapsed to a single stream.
               API 617 provides a slightly different formulation of the Wachel number
            known as a modified Wachel’s equation. It differs from the original Wachel for-
            mulation in two ways. First, the mole weight variable is replaced with a constant
            value of 30. Second, the density ratio is based on a particular impeller stage, not
            the density ratio across a section. This density ratio difference can make a large
            difference in beam-style compressors as opposed to an overhung design. In
            addition, the CFD-based methods have been shown in literature for the calcu-
            lation of impeller cross-coupling, including Moore et al. [12a]. While not as
            widely used as the Wachel-based equations, CFD methods offer a more


























            FIG. 3.35 Wachel equation and input parameters [12].
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