Page 62 - Compression Machinery for Oil and Gas
P. 62

Centrifugal Compressors Chapter  3 53


                If these flow channels are in a rotating system (e.g., in an impeller), mechan-
             ical energy is added to or removed from the system. Nevertheless, if the veloc-
             ities are considered in a rotating system of coordinates, above principles are
             applicable as well.
                Another important concept is the conservation of momentum. The change in
             momentum M of gas flowing from a point 1 to a point 2 is its mass times its
             velocity (mc), and is also the sum of all forces F acting. The change in momen-
             tum is thus:

                                     !
                                   dM       !  !     !
                                       ¼ _ mc 2   c 1 ¼F
                                    dt
                To change the momentum of this gas, either by changing the velocity or the
             direction of the gas (or both), a force is necessary. Fig. 3.24 outlines this concept
             for the case of a bent, conical pipe. The gas flows in through the area A 1 with w 1 ,
             p 1 , and out through the flow area A 2 with w 2 , p 2 . The differences in the force is
             due to the pressure (p 1 A 1 and p 2 A 2 , respectively), and the fact that a certain mass
             flow of gas is forced to change its direction generates a reaction force F R . Split
             into x and y coordinates, and considering that

                                    _ m ¼ ρ A 1 w 1 ¼ ρ A 2 w 2
                                                2
                                        1
             we get (due to the choice of coordinates, w 1y ¼0)
                                   ð
                                                   ð
                           x : ρA 1 w 1 w 2x  w 1 Þ ¼ p 1 A 1   p 2 A 2 Þ + F Rx
                                                         x

                                          ð
                           y : ρA 1 w 1 w 2y ¼  p 2 A 2 Þ + F Ry
                                                y
                                                               W
                                                                 2
                                                                    p 2
                             y                      2
                                  x
                                                       A 2
                           1

                     U
                W    p  1
                 1
                         A
                      1
                                                                        2
                          1
                                                                (p + QW  )
                                                                 1      1
                                                            F x     A
                                                        F y           1
                                                            F
                                           (p + QW  )A
                                                   2
                                             2     2  2
             FIG. 3.24 Conservation of momentum [3].
   57   58   59   60   61   62   63   64   65   66   67