| 摘要 |
A period of time from a point in time at which pilot injection is executed until an equivalence ratio in fuel spray, after exceeding a combustible equivalence ratio, falls below the combustible equivalence ratio is calculated as a physical ignition delay period. A chemical ignition delay period is calculated from the temperature and pressure inside a combustion chamber at a point in time at which the equivalence ratio in the fuel spray reached the combustible equivalence ratio. A total ignition delay period is calculated from the above-calculated ignition delay periods. The oxygen concentration and temperature inside the combustion chamber are adjusted such that the total ignition delay period matches a target ignition delay period.
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