Abstract
A two-stage sequential turbocharging system was proposed in order to meet the power output requirements for diesel engine within the altitude range from zero to 5 500 meters. Based on the required power recovery of CA6DL2 engine, the specific parameters of the turbocharging system were calculated and the low-pressure turbocharger was chosen. The software GT-Power was used to calculate the engine's performance at different altitudes. The simulation results show that, due to a good match with the two-stage sequential turbocharging system, the engine power can be recovered to 80 percent at 5 500 meters while keeping no change at sea level.
| Original language | English |
|---|---|
| Pages (from-to) | 397-402 |
| Number of pages | 6 |
| Journal | Binggong Xuebao/Acta Armamentarii |
| Volume | 32 |
| Issue number | 4 |
| Publication status | Published - Apr 2011 |
Keywords
- Diesel engine
- Plateau
- Power machinery engineering
- Simulation
- Two-stage sequential turbocharging