Schematic Diagram - Variable Vane Operation
A = LOW ENGINE SPEED; B = INTERMEDIATE ENGINE SPEED; C = MAXIMUM ENGINE SPEED.
| ITEM | DESCRIPTION |
|---|---|
| 1 | Powertrain Control Module (PCM) |
| 2 | Variable Geometry Turbocharger (VGT) vane actuator |
| 3 | Turbine housing |
| 4 | Variable vanes |
| 5 | Compressor wheel |
Low Engine Speed. At low engine speeds the volume of exhaust gas is low so the vanes are moved towards the closed position to reduce the turbine inlet area. This reduction causes an increase in the gas velocity into the turbine wheel thereby increasing wheel speed and charge air pressure.
Intermediate Engine Speed. As the engine speed increases and the volume of exhaust gas increases the vanes are moved towards the open position to increase the turbine inlet area and maintain the gas velocity.
Maximum Engine Speed. At maximum engine speed the vanes are almost fully open to maintain the gas velocity into the turbine wheel. The maximum position of the VGT vanes is also an emergency default position in the event of an electrical fault. This lowers the chance of engine damage due to excessive charge air pressure.
When the vehicle is driven at high altitudes, the ambient pressure reduces causing the compressor wheel to rotate faster to achieve the same charge air pressure. To prevent the turbine wheel from over-speeding under these conditions, the PCM protects the turbocharger by opening the vanes further to reduce the turbine wheel speed. This is known as the altitude margin of the turbocharger, which occurs at altitudes above 2000 meters. Below 2000 meters altitude compensation is not necessary. The PCM uses an internal barometric pressure sensor to monitor altitude.