Page 431 - Compression Machinery for Oil and Gas
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410 SECTION    III Applications


            where.
               b 2 ¼impeller exit width
               μ 0 ¼viscosity at the inlet conditions
               U 2 ¼impeller tip speed
               ρ 00 ¼gas density at inlet conditions


            Impeller Work Coefficient

            The impeller imparts energy to the working fluid to raise the total enthalpy and
            the impeller work coefficient is defined as
                                      Δh  C p T 02  T 01 Þ
                                            ð
                                   τ ¼  2  ¼    2                      (10.4)
                                      u        u
                                       2
            where
               T 01 and T 02 ¼total inlet and outlet temperature
               C p ¼specific heat
               U 2 ¼impeller tip speed
               Polytropic efficiency. The polytropic efficiency is given by

                                                 p 2
                                             log
                                       k  1      p 1
                                   η ¼                                 (10.5)
                                    p
                                         k       T 2
                                             log
                                                  T 1
            where
               k¼C p /C v
               P 2 and P 1 ¼outlet and inlet pressure
               T 2 and T 1 ¼outlet and inlet temperature
               The head coefficient μ is defined as
                                         μ ¼ τη p                      (10.6)



            Two-dimensional (2D) and 3D Impellers

            Impeller flow coefficient and geometry are related. Lower flow coefficients
            correspond to shrouded, two-dimensional (2D) impeller geometry. Higher flow
            coefficients correspond to shrouded, 3D impeller geometry. For very high flow
            coefficients, an axial flow blade design is utilized. The LNG centrifugal com-
            pressors typically use a combination of 2D and 3D impellers.
               A 2D impeller basically has a constant blade angle from disk to shroud along
            the leading edge of the blade. It can therefore only match the incidence angle at
            one point on the leading edge, and has an increasingly mismatched leading edge
            flow field in moving toward the disk or shroud from that point. However, as 2D
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