Control device for compression-ignition engine
A control device for a compression-ignition engine in which partial compression-ignition combustion including spark ignition (SI) combustion performed by combusting a portion of a mixture gas inside a cylinder by spark-ignition followed by compression ignition (CI) combustion performed by causing the remaining mixture gas to self-ignite is executed at least within a part of an engine operating range is provided, which includes a detector configured to detect a given parameter that changes as combustion progresses inside the cylinder, an A/F (air-fuel ratio) controller configured to change an air-fuel ratio of air to fuel introduced into the cylinder, and a combustion controller configured to determine combustion stability based on the detected parameter of the detector and control the A/F controller to reduce the air-fuel ratio when it is confirmed that during the partial compression-ignition combustion the combustion stability is low.
1. A control device for a compression-ignition engine in which partial compression-ignition combustion including spark ignition (SI) combustion performed by combusting a portion of a mixture gas inside a cylinder by spark-ignition followed by compression ignition (CI) combustion performed by causing the remaining mixture gas inside the cylinder to self-ignite is executed at least within a part of an operating range of the engine, comprising:
a detector configured to detect a given parameter that changes as combustion progresses inside the cylinder;
an A/F (air-fuel ratio) controller configured to change an air-fuel ratio of air to fuel introduced into the cylinder; and
a combustion controller configured to determine combustion stability based on the detected parameter of the detector and control the A/F controller to reduce the air-fuel ratio when it is confirmed that during the partial compression-ignition combustion the combustion stability is low, wherein
the combustion controller identifies based on the detected parameter of the detector, a given mass combustion timing at which a given mass ratio of part of fuel supplied to the cylinder in one combustion cycle combusts, and determines the combustion stability based on the identified given mass combustion timing.
2. The device of claim 1 , wherein the combustion controller identifies a first mass combustion timing at which a given first mass ratio of fuel combusts and a second mass combustion timing at which a second mass ratio that is higher than the first mass ratio combusts, and determines the combustion stability based on a variation in combustion speed between cycles calculated based on the first and second mass combustion timings.
3. A control device for a compression-ignition engine in which partial compression-ignition combustion including spark ignition (SI) combustion performed by combusting a portion of a mixture gas inside a cylinder by spark-ignition followed by compression ignition (CI) combustion performed by causing the remaining mixture gas inside the cylinder to self-ignite is executed at least within a part of an operating range of the engine, comprising:
a detector configured to detect a given parameter that changes as combustion progresses inside the cylinder;
an A/F (air-fuel ratio) controller configured to change an air-fuel ratio of air to fuel introduced into the cylinder; and
a combustion controller configured to determine combustion stability based on the detected parameter of the detector and control the A/F controller to reduce the air-fuel ratio when it is confirmed that during the partial compression-ignition combustion the combustion stability is low, wherein
the combustion controller selects, as a combustion mode of the partial compression-ignition combustion, one of a first mode in which the partial compression-ignition combustion is performed in an environment in which the air-fuel ratio is higher than a stoichiometric air-fuel ratio and a second mode in which the partial compression-ignition combustion is performed in an environment in which a gas-fuel ratio is higher than the stoichiometric air-fuel ratio and the air-fuel ratio is substantially the stoichiometric air-fuel ratio, and when it is confirmed during the partial compression-ignition combustion in the first mode, that the combustion stability is low, the combustion controller switches the combustion mode from the first mode to the second mode, the gas-fuel ratio being a ratio of a total gas including exhaust gas recirculation (EGR) gas to fuel inside the cylinder.
4. The device of claim 3 , wherein the combustion controller controls a timing of the spark ignition so that a combustion center of gravity of the partial compression-ignition combustion in the first mode and a combustion center of gravity of the partial compression-ignition combustion in the second mode are located at the same position when an engine speed and an engine load are the same in the first mode and the second mode.
5. The device of claim 1 , wherein the combustion controller identifies a start timing that is a start timing of the CI combustion based on the detected parameter of the detector and determines the combustion stability based on a variation in the start timing between cycles.
6. The device of claim 1 , wherein the detector is an in-cylinder pressure sensor configured to detect pressure inside the cylinder as the parameter.