Page 625 - Mechanical Engineers' Handbook (Volume 2)
P. 625

616   Servoactuators for Closed-Loop Control






































                          Figure 57 Spectrum of aerospace applications of electrohydraulic servomechanisms. (Courtesy of
                          Moog, Inc., East Aurora, NY.)



                          required to produce stability results in significantly poorer dynamic performance. But only
                          case (d), with a dynamic pressure feedback servovalve, combines good dynamic performance
                          with a significant improvement in static stiffness to external load disturbances.


           10.6  Range of Control for Electrohydraulic and Electromechanical Servosystems
                          Two principal parameters characterize the range of control for most electrohydraulic servo-
                                   36
                          mechanisms : power level and dynamic response. Figure 55 is a graph of control power
                          versus control dynamics showing three dominant ranges of control for electrohydraulic ser-
                          vomechanisms. The middle region of the graph represents the range where electrohydraulic
                          servomechanisms traditionally have dominated applications. Yet developments of high-
                          effeciency and high-speed-of-response rare earth servomotors have led to increased numbers
                          of electromechanical servomechanism applications in parts of this region. For applications
                          requiring low power levels and low dynamic response, electromechanical solutions are gen-
                          erally preferred. There remains a region involving high power level and high dynamic re-
                          sponse where neither electrohydraulic nor electromechanical solutions are available.
                             Areas of typical applications of electrohydraulic servosystems are plotted on the control
                          power versus control dynamics graphs of Figs. 56 and 57. Future needs for both electro-
   620   621   622   623   624   625   626   627   628   629   630