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184                              TRƯỜNG ĐẠI HỌC SƯ PHẠM KỸ THUẬT - ĐẠI HỌC ĐÀ NẴNG

                  In  there:  W ' :a  function  in  the  coil  and  its   3. DESIGNING, SIMULATING THE NOZZLE
                             m
               inductance.                                       Based on the calculated parameters, the design in
                                                              Table 2, and the design software, the team concluded
                  The  inductance  L(x)  of  coil  is  calculated  as   and produced a detailed drawing and 3D model of the
               follows:
                                                              nozzle.  All  the  component  details  of  the  nozzle  are
                             N 2                              shown in Figure 1.
                     L ( ) x =                             (13)   Choosing  the  material  for  the  nozzle  directly  in
                             n 1 Ri
                                                              the  engine  combustion  chamber  greatly  affects  the
                  In there:   1 Ri                           performance  and  life  of  the  nozzle.  The  materials
                           n
                                                              used  must  meet  many  requirements,  such  as  being
                  is the total magnetoresistance of the system.   able to withstand high temperatures in the combustion
                  The relationship between the number of wire rings   chamber  without  deformation  or  loss  of  mechanical
               and the intensity of the current, is expressed through   properties.  Corrosion  resistance  is  also  an  important
               the Ampe law:                                  factor,  high  corrosion  resistance  is  necessary  to
                       Hdl=N i                            (14)   maintain  accuracy  and  long  life,  as  the  nozzle  is
                                                              subjected  to  the  influence  of  the  fuel  flow  injected
                  2.2. Technical specifications               with high pressure. High mechanical strength enables
                        Table 1. Specifications required      the  nozzle  to  withstand  high  pressure  without
                         for the Honda GX160 engine           cracking  or  breaking.  Good  thermal  conductivity
                No         Symbols       Parameter   Dimensions   helps  to  distribute  heat  evenly,  reducing  the  risk  of
                 1   Cylinder Capacity (D)   163     cm   3   local overheating. Good machinability is an essential
                                                              element in the manufacture of the complex details of
                 2   Number of crankshaft   3000     Rpm      the  nozzle  with  high  precision.  Finally,  the  material
                    revolutions (n)
                                                              needs to maintain its mechanical properties (such as
                 3   Charging performance(  )   0,8          hardness and durability) at high temperatures without
                                     v
                 4   End of charge temperature   330   K      much  reduction.  In  this  study,  the  material  is  C45
                    (T)                                       alloy steel. The mechanical and logistical conditions
                 5   Initial loading temperature   700   K    correspond  to  the  working  conditions  of  the  engine,
                    (T 0)                                     and  the  simulation  results  also  show  that  the  nozzle
                  Table 1 has given the specific parameters for the   meets the requirements for nozzles used on the Honda
               operating conditions of the Honda GX160 engine, and   GX160 engine.
               this  is  an  important  basis  for  calculating  and   To  lower processing  costs  as  well  as  the  cost  of
               designing  the  nozzle  in  the  most  optimal  way.  The   direct  injection  products  into  the  combustion
               characteristic parameters of the engine for the nozzle   chamber,  the  team  took  advantage  of  the  details
               include:  Cylinder  capacity  (D);  the  number  of   already available on the market. The precision CNC
               crankshaft rotations (n); filling performance ( η ), end   machining method is chosen to produce the remaining
                                                     v
               of filling temperature (T), beginning of filling temperature   details. With this method, the particles in the nozzle
               (T0).  After  applying  the  calculation  equations  in   will  be  handled  with  the  smallest  assembly  error
               section 2.1, we get the following parameter table:   tolerance.
                 Table 2. Specifications of the injector are designed   3.1. Design
                    based on syngas components 15-20% H2,        The  design  also  shows  that  when  the  door  is
                      15-20% CO, 1-5% CH4, 10-15% CO2         opened,  the  syngas  will  be  injected  into  the
                No        Symbols       Parameter   Dimensions   combustion  chamber  under high  pressure.  When  the
                 1   Air Flow (R m)     3,2636.10    kg/s     compression process is completed, the high pressure
                                              -5
                 2   Amount of fuel injected   2,72.10    kg   in  the  combustion  chamber  will  push  the  nozzle
                                              -5
                     into the cylinder (m syngas)             pushbar  to  the  closed  position  while  closing  the
                 3                                            nozzle as the xupap loads and discharges. Thanks to
                     ρ                   487,01     kg/m   3
                      syngas                                  this,  the  syngas  is  completely  retained  in  the
                 4
                     γ                   4777,6     N/m       combustion  chamber,  preventing  leakage  and
                                                       3
                      syngas
                 5                                     2      optimizing  fuel  efficiency.  The  reverse  nozzle  is  a
                                        24,502     N/m       unique  invention  applied  to  internal  combustion
                      p
                 6   T m                  0,01       s        engines,  using  poor  syngas  gas  as  fuel.  The  special
                 7   Injection hole diameter (d)   0,006   m   feature of this nozzle lies in its intelligent operation
               ISBN: 978-604-80-9779-0
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