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Page Title: LOCATION AND DESCRIPTION OF MAJOR COMPONENTS - continued
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TM 10-4320-342-24 1-11.  LOCATION AND DESCRIPTION OF MAJOR COMPONENTS - continued. j. (11) Engine.    The  engine  is  mounted  to  the  engine  mounts  on  the  frame.    Its  purpose  is  to  drive  the  200/600 GPM  fuel  pump.    It  consists  of  a  compressor,  gearbox,  turbine  wheel,  enclosure,  combustion  assembly  and electronic sequencing unit. k. (12) Boost Pumps.  Three boost pumps are provided on each  unit.    The  first  supplies  a  positive  pressure  of  fuel to the fuel control module on the turbine.  The second supplies a positive pressure of oil to the inlet of the speed reducer.  The third removes oil from the speed reducer and returns it to the reservoir. l. (13) Fuel/Oil  Filters.    Provides  clean/oil  by  separating  the  dirt  and  water  from  the  contaminated  fuel/oil  before entering into the gas turbine.  Filter assembly is an aluminum construction with operating pressure of 3000 psi at 6  gpm.    Also,  filter  assembly  includes  an  40  micron  element,  visual  differential  pressure  indicator  and  bypass relief valve.  When fuel/oil is flowing through the filter assembly a drop in pressure occurs between the inlet side and outlet side.  This is due mainly to the flow resistance of the 40 micron element.  As contaminates (dirt, water, etc) are collected by the 40 micron element, the drop in pressure increases.  Eventually, when the pressure drop reaches  15  psi,  the  visual  differential  pressure  indicator  turns  from  gold  to  red.    This  enables  the  operator  to detect  contaminant  build  up  before  the  40  micron  element  is  completely  plugged  and  provides  ample  time  to change  the  40  micron  element.    If,  the  40  micron  element  is  not  changed,  the  bypass  relief  valve  will  activate when   the   differential   pressure   reaches   17   psi   and   start   bypassing   the   40   micron   element   within   the   filter assembly.  The bypass relief valve will continue bypassing until the 40 micron element is changed. m. (14) Speed Reducer.  A reduction gear system is  used  to  reduce  the  speed  of  the  turbine  (12,000  rpm)  to  the operating speed of the pump (8,000 rpm). n. (15) Clutch.    An  electromagnetic  clutch  is  incorporated  int  he  centrifugal  type  pump  adapter  assembly.    The clutch permits decoupling of the centrifugal type pump from the turbine during starting and priming. o. (16) Air Filters.  Provides clean air for the turbine inlet by separating the dirt particles and water droplets from the contaminated  air.    The  contaminated  air  entering  the  filter  is  given  a  swirling  motion  induced  by  the  vortex generator.    This  swirling  motion  separates  the  dirt  particles  and  water  droplets  leaving  on  the  clean  air  to  pass through the filter.  The dirt particles and water droplets are scavenged out the exhaust. 1-6

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