| Starion
      turbochargers | 
  
    |  |  | 
  
    |  Starions used 6 different turbochargers
      depending on engine and market 1) TC06-11A (8 cm2 turbine housing) non intercooled
      4G63 2.0 litre SOHC (Australia, JDM, Europe) 2) TC06-11A (8 cm2 turbine housing) intercooled
      4G63 2.0 litre SOHC (Australia, JDM, Europe) 3) TC05-12A (6cm2 turbine housing) non intercooled
      JDM 4G63 2.0 litre SOHC (JDM) 4) TC05-12A (6cm2 turbine housing) intercooled
      JDM 4G63 2.0 litre SOHC (Australia, JDM) 5) TD05-12A (8cm2 turbine housing) non intercooled
      4G54 2.6 litre (USA, JDM, Europe) 6) TD05-12A (8cm2 turbine housing) intercooled
      4G54 2.6 litre (USA, JDM, Europe) The intercooled and non-intercooled turbos
      had the same wheels but the compressor housing was different.
      The compressor outlet was different to enable connection of the
      intercooler hose. Because of this the wastegate actuator was
      also different. Also there were watercooled and non-watercooled
      versions for some models.
     |  | 
  
    |   | TD05-12A turbo (with intercooled
      type compressor housing) | 
  
    | 
 | 
  
    | Turbo
      comparison and identification | 
  
    |  | Turbo compressor housings.
      Australian JA,JB Starion uses 4G63
      SOHC engine with a TC06-11A (left hand pic)
      Various Japanese domestic market (JDM)
      4G63 SOHC used TC05-12A. | 
  
    |  | TC06-11A compressor wheel on the left
      TC05-12A compressor wheel on the right. | 
  
    |  | JDM TC05 housing compared to
      TCO6. Dimension shown only to highlight obvious external size
      difference of the housing and hence internal size/area. | 
  
    |  | Identification number are on
      the housings | 
  
    |  |  | 
  
    | Australian
      spec 4G63 SOHC 2.0 Starion used TC06-11A turbo with 8cm2 (080)
      exhaust. The US market G54B 2.6 Starion/Conquest used the TD05-12A
      however with a 8cm2 (080) exhaust housing. The Japanese market
      4G63 SOHC 2.0 Starion used a TC05-12A (same size turbine wheel
      as US) however with the much smaller 6cm2 (060) exhaust housing. |  | 
  
    |  | TC06 turbine 8cm2 (080) housing
      on the left and TD05 8cm2 (080) housing on the right. | 
  
    |  | TC06 turbine 8cm2 (080) housing
      as used on 4G63 2.0 SOHC 8 valve Australian spec Starions. | 
  
    |  | TD05 turbine 8cm2 (080) housing
      as used on G54B 2.6 US Starion/Conquests
      . Notice smaller diameter. Entry slot
      into involute is also 1mm narrower. | 
  
    |  | Another shot TC06 on the left
      TD05 on the right. | 
  
    |  | TC06 turbine wheel on the left
      and TD05 turbine wheel on the right | 
  
    |   | There are minor differences
      between early and late TC06 turbine housings. However the centre
      cartridge is the same and is interchangable providing the correct
      cover plate is used.
      (Note: to change the cover plate the
      turbo centre cartridge has to be pulled apart) | 
  
    | 
 | 
  
    | Special Stuff |  | 
  
    |  | Ralliart TD06-19C turbo used
      on factory Pajero/Starion G54B 2.6 litre 330hp spec race engine.
      This is the same turbo used on 1988 Paris-Dakar Ralliart Pajero.
      These turbo's were used by the factory
      teams only and were not for sale.
      Wastegate actuator has only a 300
      Kpa (0.3 bar) spring. Boost was controlled by the ECU. This could
      be changed in the cockpit by means of a switch. | 
  
    |  | 1988 Paris-Dakar Ralliart Pajero!
      Full kevlar body spaceframe construction
      200Km/h + on the sand! | 
  
    |  | Side view. Note lack of water
      cooled centre bearing housing. | 
  
    |  | Rear view. A separate pipe was
      used for the wastegate and joined the main exhaust about a metre
      down the engine pipe. | 
  
    |  | This view shows there is no
      provision for wastegate passage to main exhaust outlet so seperate
      dump pipe for wastegate must be used. | 
  
    |  | This is the Ralliart exhaust
      G54B 2.6 manifold shown with the turbo above. Notice size of
      turbo outlet. | 
  
    |  | This is a standard 2.6 G54B
      turbo exhaust manifold.(notice weld repair) | 
  
    |  | This view shows the sealing
      ring from the standard G54B manifold above you can see how much
      bigger the Ralliart manifold turbo outlet is.
      ID on standard manifold is 43.2mm.
      Ralliart manifold is 54.2mm. | 
  
    |  |  | 
  
    |  | This is exhaust manifold
      from 4G63 2.0 SOHC engine. Turbo outlet is exactly the same size
      as stock G54B. | 
  
    | 
 | 
  
    | Turbo Testing
      I did some testing before and after
      fitting the Ralliart TD06-19C. The first graph shows data recorded
      using the "high flowed" TD05. Compressor housing was
      modified and a Garrett compressor wheel was fitted. Turbine side
      was stock. My horsepower has increased by somewhere around (I
      say around because the previous best with the TD05 was 180HP
      and the test was done in 4th gear) 40HP at the wheels with NO
      other changes other than to connect the different exhaust flange.
      I'm running a ported Magna head, Camtech cam (Camtech is an Australian
      cam company), full 3" exhaust, standard ECU, standard airflow
      meter. Being an engineer I decided to do some data logging to
      see what the difference was between the turbos. See graphs below.
      Due to my limited budget I purchased low cost DAQ gear that could
      only sample at about 6-8 samples a second that's why the graphs
      have steps but the info is still there to see. There is no RPM
      trace on the graphs so I added some RPM markers. |  | 
  
    |  | Starion on the dyno at MRC Dyno
      located in Sydney Australia. | 
  
    |     | Engine bay pic with TD06 turbo
      fitted. | 
  
    |  | TD05
      Dynosheet | 
  
    |  | TD06-19C
      Dynosheet | 
  
    |  | NOTE: TDO5 was "high flowed"
      and fitted with a Garrett compressor wheel by previous owner.
      Turbine side was untouched. | 
  
    |  | Note it is making 221 HP on
      only 13 psi. | 
  
    | The main difference between the turbos was:1) Reduction of exhaust manifold backpressure by 0.5 bar (7.25
      psi) @ 6000 RPM!!!!
 Uncorked!!!!
 2) Reduction in compressor outlet temperature
      of approx 20 degrees CNote: this is with a lot higher airflow as well.
 Another discovery is the major restriction
      between the turbo outlet and the inlet manifold. There is about
      a 3.8 psi pressure drop through the TBI (with 220HP airflow)
      noted as "A" in the graph. The engine wants to really rev now pulls hard
      to 6500 RPM even with the boost dropping off as shown in the
      graphs. Note the wastegate is connected to the "hard pipe"
      so keeps the pressure constant there.
     |  | 
  
    |  | Briefcase DAQ system I built
      using 3 bar Delco MAP sensors, M&W Uego wideband controller
      (not shown) and ICP i7000 modules. | 
  
    |  | I wrote the software using Borland
      Delphi. | 
  
    |  | Another run with a fraction
      more boost and the wastegate hose relocated to the inlet manifold
      (was in cross-over pipe).
      Note: abrupt roll off at 6500 RPM
      is dyno operator backing off. | 
  
    |  | HKS EVCIV fitted boost increased
      to17 psi with factory air cleaner removed and POD filter (no
      airflow meter) and Haltech F3. | 
  
    |  | POD filter could be installed
      better but was installed quickly for dyno run. | 
  
    |  | Magna MPI
installed | 
  
    |  |   Magna MPI
dyno sheet.
 This does not tell
 the whole story the
 drivability is vastly
 better compared to
 the stock TBI setup.
 |