Page 19 - Theory and Design of Air Cushion Craft
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4  Introduction  to hovercraft

              immersed  in  salt  water  an  important  design  parameter  for  marine  vehicles.
              Additionally, it suggested a number of alternatives to the basic principle of pumping air
              into a cavity under a hull, using a modified wing form instead, to achieve vehicles with
              speeds closer to that of aircraft. Several vehicle concepts have developed from this work.

              Amphibious    hovercraft  (or ACV)

              The  amphibious  hovercraft  (Fig.  1.3) is supported  totally by its air  cushion, with an
              air curtain  (high pressure jet) or a flexible skirt system around  its periphery to seal the
              cushion  air. These  craft  possess  a shallow draft  (or a negative draft  of  the hull  struc-
              ture  itself)  and  amphibious  characteristics.  They  are  either  passive  (being  towed  by
              other equipment) or active, i.e. propelled  by air propellers  or fans.  Some 'hybrid' craft
              have used surface stroking, balloon wheels, outboard  motors  and water jets to achieve
              different  utility requirements.


























              Fig.  1.3  First  Chinese  medium-size amphibious hovercraft  model 722-1.



              Sidewall  hovercraft  (or SES)

              This concept  (Figs  1.4 and  1.5) reduces the flexible skirt to a seal at the bow and  stern
              of  a marine (non-amphibious) craft, using walls or hulls like a catamaran at the  sides.
              The  walls or  hulls at both  sides of  the  craft,  and  the  bow/stern  seal  installation,  are
              designed  to minimize  the  lift  power.
                Due to the lack of air leakage at the craft  sides, lift power can be reduced significantly
              compared with an  ACV. Also, it is possible to install conventional water propellers  or
              waterjet propulsion, with rather smaller machinery space requirements compared to that
              for  air propellers or fans  used on ACVs. This more compact machinery  arrangement,
              combined with the possibility for higher cushion pressure supporting higher specific pay-
              load, has made a transition to larger size much easier for this concept than for the ACV.
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