Abstract
Pre-chamber ignition system has the potential to reduce burn duration of lean-burn gasoline engine combustion and can achieve reduced knock occurrence from the distributed ignition sources. Pre-chamber ignition produces high velocity turbulent jets and these jets often reach sonic velocity and produce shock waves inside the combustion chamber. These shock waves make knock detection difficult with a conventional surface mounted acoustic knock sensor. This paper discusses how an acoustic knock sensor works with pre-chamber ignition and evaluates different cylinder pressure-based knock detection strategies and proposes a method which eliminates the influence of jet induced oscillations on knock detection.
| Original language | English |
|---|---|
| Pages (from-to) | 405-417 |
| Number of pages | 13 |
| Journal | SAE International Journal of Engines |
| Volume | 14 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - 26 Feb 2021 |