Page 86 - Theory and Design of Air Cushion Craft
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70  Air  cushion theory

              The  air cushion  characteristic  curves for both  ACV/SES  are shown  by Fig.  2.21 (the
              calculation  in detail can  be found  in Chapter  11, Lift  system design), where

              •  Hj-Q  represents the characteristic curve of  lift  fans, p t-Q  represents the  character-
                istic of  the air ducting, i.e. the characteristic curve of  a fan  at any given revolution
                minus the  pressure loss of flow in air  duct, p v  represents  the  bag  pressure  of  skirts
                a.ndp t~Q  also represents the characteristic of  the  bag.
             •  P~Q  represents  the  characteristic  for  static  air  cushion  performance,  namely  the
                relation  between flow and  bag  pressure  at various hovering heights,  which can  be
                obtained  by the foregoing formula. For  this reason,  the curve p-Q  represents  the
                relation between the bag pressure and flow rate andp t-Q  denotes the total pressure
                of  air duct  (or bag) at various hovering heights and  fan revolutions.
             The intersection point  of  both  curves represents the hovering height of  the craft at a
             given craft  weight (a given cushion pressure) and  any  given fan  speed.  Hence,  the  air
             cushion characteristic curve for  an  ACV can  be described  as follows  (also similar for
             an  SES):
              1.  The minimum fan  speed  for inflating  the  skirt of  an  ACV (similar to  the hovering
                attitude 4 in Fig.  2.20), will be that at which the total pressure of the lift fan  equals
                the  cushion  pressure  at  the  zero  flow  rate.  At  this  point  the  craft  weight  is sup-
                ported  by cushion lift  perfectly,  but without having risen from  the static condition.
                In the case of  zero flow rate the total  pressure of  the fan is equal to  the total pres-
                sure of  the duct  bag and  thus to the cushion pressure.
             2.  The  factors  necessary for  hovering the  craft,  i.e. from  attitude  1 transient  to  atti-
                tude  3, is that  the  bottom  of  the  buoyancy tank  has  to  leave the  water  surface in
                order  to  exert  the  cushion  pressure  to  the  bottom  and  lift  the  craft.  At  MARIC

                            p,


                                               H-Q























              Fig. 2.21  Air  duct and  air cushion characteristics  curves of ACV/SES.
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