Page 46 - Theory and Design of Air Cushion Craft
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30  Introduction  to  hovercraft

              and  it was re-named  as  SES-200.  As a result of  the  modifications, the  craft  drag was
              reduced  at cruising speed, and  the economy and  seakeeping quality of  such SES with
                      and  thickened sidewalls was improved  significantly. The craft speed on calm
              high LJB C
              water  was about  30 knots  but  the  speed  loss less than  20% in a sea state  of  Beaufort
              4. In these conditions the craft  captain  would have to throttle back  the governor so as
              to  reduce  the engine revolutions,  or change  the course,  in order  to  avoid the  extreme
              slamming  motions  and  shipping  of  water.  The  BH-110  has  good  seakeeping:  it  can
              maintain  a  speed  of  28 knots  in calm  seas,  16 knots in head  seas of  8 ft and  25 knots
              in following seas  of  12 to  14 ft,  respectively.
                Three production  BH-110 craft  in service with the US Coastguard  during the  1980s
              have been  operated  for up  to  181 consecutive days and  nights. The  Coastguard  con-
              cluded  that  maintenance  labour  was equal  or  less than  that  on  conventional  coastal
              patrol  vessels,  and  also  realised  that  the  crews  had  a  good  rest  during  a  three  day
              patrol  operation.
                Features  of  third generation  SES craft  are as  follows:
              1.  A  fair  performance  at  low/medium  speed,  and  low peak  drag  as  well as  increased
                range;
              2.  Good  seakeeping  capability  in  cushion  borne  operation  due  to  its  raised  wetted
                deck, which was similar to  a  catamaran;
              3.  Thanks  to  the craft  ride control  system (RCS),  the cushion pressure could  be kept
                almost constant, arising from  regulating both the air inlet and outlet control valves,
                so as to  reduce  the vertical motion  of  craft  in waves. The  RCS had  been  mounted
                on the XR-1D, SES  100A and  SES-200, and  a large number  of  tests had  been  car-
                ried  out  which validated  the  excellent  effect  of  these  systems. Vertical  acceleration
                could  be reduced by 50%, 30% and  25% at sea states of  1 to 2, 3 and  4, respectively;
             4.  The pitch angle of  SES-100 at full  speed in head seas was decreased,  as shown in Table
                1.6.  It was found that the pitch motion  of  the craft  was less than the required  pitch
                motion  for  landing helicopters  (less than  3°). It  is probably  safe  to  assume  that  the
                helicopters could be landed  safely  on  SES-200 weighing 200t at less than  sea-state 4;
              5.  Thanks  to  the  medium  speed  of  the  craft,  the  wear  rate  of  skirt  bow  segments  tip
                improved to  between  1500 and  3000 hours, whereas the  life  of  the bow skirt might be
                reduced to 300-700 hours at operational  speeds of 40-60 knots. In addition, the main-
                tenance  cost  was  reduced  further  due  to  adopting  a  skirt  design  which  could  be
                replaced  while the  craft  was moored  on  water, and  was found  to  be  lower than  the
                main engine maintenance cost which was relatively low due to the use of diesel engines.
              The  US  Navy  were  encouraged  by  the  success  of  tests  carried  out  on  the  SES-200
              craft,  and  later  worked  on  the  development  of  two  applications  of  such  craft,  the
              Mine Countermeasures  SES and  the medium  sized Patrol  SES.

                            Table  1.6  The  pitch  motion  of  SES-200 at  full  speed  and
                            in head sea
                            Sea State          Pitch  angle (single amplitude)
                            1                  < 0.2 degrees
                            2                  <0.9
                            3                  <2.2
                            3.5                2.5
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