Page 558 - Handbook of Biomechatronics
P. 558

Artificial Hearts                                            551


                                 →
                                V 2                              V
                                                       V rb2  V n2  t2  →
                  V rb2                 U = r w           b     a 2   V 2
                                         2
                                            2
                      b 2                                  2
                                                                           U 2
                                                         Velocity components
                                  V rb1                  at the outlet
                               b
                            r 2  1
                                         →
                                        V 1
                                                              V t1
                                                    V       V    →
                                r 1                  rb1     n1  V 1
                                             = r w               a
                                          U 1   1         b 1     1
                                                                        U
                  Absolute velocity as the sum                           1
                  of the velocity relative to the       Velocity components
                  blade and rotor velocity              at the inlet
              Fig. 25 Geometry used to develop the velocity diagram for a centrifugal pump where r 1
              and r 2 are the inlet and outlet radii of the pump, and the various velocity vectors are as
              defined in the text. (Based on Fox, R., McDonald, A., 1998. Introduction to Fluid Mechanics.
              John Wiley & Sons, Inc., New York.)



              and simplifying.

                                            ηρQU V t2
                                                 2
                                      ΔP ¼
                                                Q                           (6)
                                            ¼ ηρU 2 V t2
              This means that the differential pressure, ΔP is proportional to the fluid tan-
              gential velocity V t2 at a constant rotational speed U 2 .
                 The relationship between V t2 and U 2 is a function of the normal fluid
              velocity V n2 and the outflow angle β 2 relative to the blade.

                                                 V n2
                                      V t2 ¼ U 2
                                                tanβ 2
              The normal velocity V n2 is equal to.

                                                Q
                                          V n2 ¼
                                               A 2
                         2
              where A 2 (m ) is pump cross section over which outflow takes place and is
              proportional to r 2 .
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