CN102691585A - Motor control apparatus - Google Patents
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- CN102691585A CN102691585A CN2012100807261A CN201210080726A CN102691585A CN 102691585 A CN102691585 A CN 102691585A CN 2012100807261 A CN2012100807261 A CN 2012100807261A CN 201210080726 A CN201210080726 A CN 201210080726A CN 102691585 A CN102691585 A CN 102691585A
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- 238000002347 injection Methods 0.000 claims abstract description 211
- 239000007924 injection Substances 0.000 claims abstract description 211
- 230000004913 activation Effects 0.000 claims description 2
- 239000003607 modifier Substances 0.000 claims 4
- 238000004880 explosion Methods 0.000 abstract description 87
- 238000000034 method Methods 0.000 description 141
- 230000008569 process Effects 0.000 description 140
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 101
- 239000001301 oxygen Substances 0.000 description 101
- 229910052760 oxygen Inorganic materials 0.000 description 101
- 238000001514 detection method Methods 0.000 description 37
- 238000005474 detonation Methods 0.000 description 19
- 238000002485 combustion reaction Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 239000000243 solution Substances 0.000 description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000000498 cooling water Substances 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 230000003197 catalytic effect Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 230000006870 function Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000010485 coping Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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Abstract
本发明提供一种发动机控制装置,其既能够削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器或进气压传感器等压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。其中,初始喷射量计算部(108a)考虑了进行高地修正后的空气密度修正系数MAS,计算发动机(1)的启动时燃料喷射量的初始值TISI,作为比与发动机温度TW相应的基本燃料喷射量少的燃料喷射量,燃料增加控制部(108b)通过依次增加该空气密度修正系数MAS,来使发动机(1)的启动时燃料喷射量TIS依次增加,完爆后喷射量计算部(108c)在发动机(1)完爆后,考虑由燃料增加控制部108b依次增加的空气密度修正系数MAS来计算发动机(1)完爆后的燃料喷射量TI。
The present invention provides an engine control device that can reduce the data capacity required for high-altitude correction of the fuel injection amount without using a pressure sensor such as an atmospheric pressure sensor or an intake pressure sensor, achieve good startability, and suppress unnecessary The amount of fuel injected by the fuel. Among them, the initial injection amount calculation unit (108a) considers the air density correction coefficient MAS after the height correction, and calculates the initial value TISI of the fuel injection amount at the start of the engine (1), as the basic fuel injection value corresponding to the engine temperature TW. For small fuel injection quantities, the fuel increase control unit (108b) sequentially increases the air density correction coefficient MAS to sequentially increase the fuel injection quantity TIS at the start of the engine (1), and the post-explosion injection quantity calculation unit (108c) After the complete explosion of the engine (1), the fuel injection amount TI after the complete explosion of the engine (1) is calculated in consideration of the air density correction coefficient MAS sequentially increased by the fuel increase control unit 108b.
Description
技术领域 technical field
本发明涉及发动机控制装置,尤其涉及控制车辆等移动体的发动机的燃料喷射量的发动机控制装置。The present invention relates to an engine control device, and more particularly to an engine control device for controlling the fuel injection amount of an engine of a mobile body such as a vehicle.
背景技术 Background technique
近年来,在车辆等移动体中,为了避免机械结构的复杂化且以与油门操作部件的操作对应的自由度高的形式来控制对发动机的燃料供给量,而采用具备燃料喷射控制机构的发动机控制装置,该燃料喷射控制机构一边以电子方式控制对发动机的燃料供给量一边从喷油器喷射燃料。In recent years, in mobile bodies such as vehicles, in order to avoid complicating the mechanical structure and to control the amount of fuel supplied to the engine with a high degree of freedom corresponding to the operation of the accelerator operating member, engines equipped with fuel injection control mechanisms have been adopted. The fuel injection control means injects fuel from the injector while electronically controlling the fuel supply amount to the engine.
另外,在这样的发动机中,当车辆等移动体位于高地时,根据大气压降低、吸入空气量减少的情况,混合气中的燃料量相对过剩,混合气没必要地变化为较浓状态。这样当混合气没必要地成为较浓状态时,不仅这样的车辆等的驾驶性能出现变化,还有可能连废气的化学物质成分比也出现不必要的变化,并且消耗没必要的燃料。In addition, in such an engine, when a mobile body such as a vehicle is located on a high ground, the amount of fuel in the air-fuel mixture is relatively excessive due to a decrease in atmospheric pressure and a decrease in the amount of intake air, and the air-fuel mixture becomes unnecessarily rich. In this way, when the air-fuel mixture becomes unnecessarily rich, not only the drivability of such vehicles and the like may change, but also the chemical component ratio of the exhaust gas may change unnecessarily, and fuel may be consumed unnecessarily.
因此,提出有如下的发动机控制装置结构:即使在根据车辆等移动体的高度使大气压降低且吸入空气量减少的情况下,也可利用简便的结构来实现与这样的车辆等位于低地时同样的空燃比,并且不需要增设检测大气压的压力传感器,可利用现有的压力传感器来求出实际的高度及大气压,并且提供与实际的高度及大气压相应的燃料喷射量。Therefore, an engine control device structure has been proposed that can achieve the same performance as when such a vehicle is located on a low ground with a simple structure even when the atmospheric pressure is lowered depending on the height of a mobile body such as a vehicle and the amount of intake air is reduced. Air-fuel ratio, and there is no need to add a pressure sensor to detect atmospheric pressure, the existing pressure sensor can be used to obtain the actual altitude and atmospheric pressure, and provide the fuel injection amount corresponding to the actual altitude and atmospheric pressure.
在这样的状况下,关于电子控制燃料喷射装置,专利文献1公开了如下的结构:具备发动机转速检测传感器、节流阀传感器以及检测发动机的吸入空气量的质量空气量传感器,通过比较前次的发动机参数和当前的发动机参数,不使用大气压传感器就能够检测高度。Under such circumstances, regarding an electronically controlled fuel injection device, Patent Document 1 discloses a structure including an engine speed detection sensor, a throttle valve sensor, and a mass air volume sensor for detecting the intake air volume of the engine. Engine parameters and current engine parameters, altitude can be detected without using the barometric pressure sensor.
另外,关于发动机的燃料控制装置,专利文献2公开了如下的结构:具备以绝对值来检测发动机的进气歧管压力的压力传感器,将这样的压力传感器的检测压力用作发动机转动前的大气压。In addition, Patent Document 2 discloses a fuel control device for an engine that includes a pressure sensor that detects the intake manifold pressure of the engine as an absolute value, and uses the detected pressure of the pressure sensor as the atmospheric pressure before the engine is turned. .
【专利文献1】日本专利第02936749公报[Patent Document 1] Japanese Patent No. 02936749
【专利文献2】日本特公平07-037773号公报[Patent Document 2] Japanese Patent Publication No. 07-037773
但是,根据本发明人的研究,在专利文献1所公开的结构中,需要设置检测发动机的吸入空气量的质量空气量传感器本身,因此结构比较烦杂,而且,为了比较发动机参数,还需要预先准备各种映射数据,对于整个控制装置,应该准备的数据量显著增加,结构变得烦杂,并且强烈地显示出难以实现低成本化的倾向。However, according to the research of the present inventors, in the structure disclosed in Patent Document 1, it is necessary to install the mass air sensor itself for detecting the intake air amount of the engine, so the structure is more complicated, and in order to compare engine parameters, it is necessary to prepare in advance. For various map data, the amount of data to be prepared for the entire control device increases remarkably, the structure becomes complicated, and there is a strong tendency that it is difficult to achieve cost reduction.
另外,根据专利文献2所公开的结构,需要设置以绝对值来检测发动机的进气歧管压力的压力传感器本身,所以结构烦杂且强烈地显示出难以实现低成本化的倾向。In addition, according to the structure disclosed in Patent Document 2, it is necessary to provide the pressure sensor itself for detecting the intake manifold pressure of the engine as an absolute value, so the structure is complicated and the cost reduction tends to be strongly difficult.
即,目前所处的现状是期待提供如下所述的发动机控制装置:既能够削减燃料喷射量的高地修正所需的数据容量而不采用各种压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。That is, the current situation is to provide an engine control device that can reduce the data volume required for high-altitude correction of the fuel injection amount without using various pressure sensors, and can achieve good startability and can Fuel injection of unnecessary fuel quantity is suppressed.
发明内容 Contents of the invention
本发明是根据以上的研究而做出的,其目的在于提供如下所述的发动机控制装置:既能够削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器或进气压传感器等压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。The present invention has been made based on the above studies, and its object is to provide an engine control device capable of reducing the data volume required for high-altitude correction of the fuel injection amount without using a pressure sensor such as an atmospheric pressure sensor or an intake pressure sensor. , and good startability can be realized, and fuel injection of an unnecessary fuel amount can be suppressed.
为了达成以上的目的,本发明的第一方面的技术方案是一种发动机控制装置,其具备:初始喷射量计算部,其考虑进行高地修正后的规定的第1空气密度修正系数,计算发动机启动时的初始燃料喷射量,作为比与上述发动机温度相应的基本燃料喷射量少的初始燃料喷射量;燃料增加控制部,其通过依次增加上述第1空气密度修正系数,来使上述初始燃料喷射量依次增加;以及完爆后喷射量计算部,在与上述发动机启动后上述发动机的转速变为完爆基准值以上的情况对应的上述发动机的完爆之后,考虑由上述燃料增加控制部依次增加的空气密度修正系数,来计算上述发动机的完爆后的燃料喷射量。In order to achieve the above object, the technical solution of the first aspect of the present invention is an engine control device, which includes: an initial injection amount calculation unit that considers a predetermined first air density correction coefficient after the height correction, and calculates the engine start-up The initial fuel injection amount at the time of the engine temperature is an initial fuel injection amount smaller than the basic fuel injection amount corresponding to the above-mentioned engine temperature; the fuel increase control unit sequentially increases the above-mentioned first air density correction coefficient to make the above-mentioned initial fuel injection amount increase sequentially; and the post-complete explosion injection amount calculation part, after the complete explosion of the above-mentioned engine corresponding to the situation where the rotational speed of the above-mentioned engine becomes more than the complete explosion reference value after the above-mentioned engine startup, considers the fuel increase control part sequentially increased The air density correction coefficient is used to calculate the fuel injection quantity after the complete explosion of the above-mentioned engine.
另外,本发明除了该第1方面的技术方案之外还提供如下的第2方面的技术方案:该发动机控制装置还具备空气密度修正系数计算部,其在上述发动机完爆之后,考虑由上述燃料增加控制部依次增加的空气密度修正系数,来计算第2空气密度修正系数,上述完爆后喷射量计算部考虑上述第2空气密度修正系数,来计算上述发动机完爆后的燃料喷射量。In addition, in addition to the technical solution of the first aspect, the present invention also provides the following technical solution of the second aspect: the engine control device further includes an air density correction coefficient calculation unit, which considers the air density correction coefficient calculation unit after the above-mentioned engine is completely detonated, and the air density generated by the above-mentioned fuel is considered. The second air density correction coefficient is calculated by increasing the air density correction coefficient sequentially increased by the control unit, and the post-detonation injection quantity calculation unit considers the second air density correction coefficient to calculate the fuel injection quantity of the engine after complete explosion.
另外,本发明除了该第2方面的技术方案之外还提供如下的第3方面的技术方案:上述空气密度修正系数计算部在安装于上述发动机的排气系统上的氧传感器激活且与来自上述氧传感器的输出值相应的氧传感器反馈修正系数收敛之前,将由上述燃料增加控制部依次增加的空气密度修正系数设定为上述第2空气密度修正系数。In addition, in addition to the technical solution of the second aspect, the present invention also provides the following technical solution of the third aspect: the air density correction coefficient calculation unit activates the oxygen sensor installed on the exhaust system of the above-mentioned engine and communicates with the oxygen sensor from the above-mentioned Before the oxygen sensor feedback correction coefficient corresponding to the output value of the oxygen sensor converges, the air density correction coefficient sequentially increased by the fuel increase control unit is set as the second air density correction coefficient.
另外,本发明除了该第3方面的技术方案之外还提供如下的第4方面的技术方案:上述空气密度修正系数计算部在上述氧传感器激活且上述氧传感器反馈修正系数收敛之后,当上述氧传感器反馈修正系数的偏差变为规定值以上时,进一步考虑上述氧传感器反馈修正系数来计算上述第2空气密度修正系数。In addition, in addition to the technical solution of the third aspect, the present invention also provides the following technical solution of the fourth aspect: the air density correction coefficient calculation unit, after the oxygen sensor is activated and the oxygen sensor feedback correction coefficient converges, when the oxygen When the deviation of the sensor feedback correction coefficient becomes more than a predetermined value, the above-mentioned second air density correction coefficient is calculated by further considering the above-mentioned oxygen sensor feedback correction coefficient.
根据本发明第1方面的技术方案的发动机控制装置,具备:初始喷射量计算部,其考虑进行高地修正后的规定第1空气密度修正系数,计算发动机启动时的初始燃料喷射量,作为比与发动机的温度相应的基本燃料喷射量少的初始燃料喷射量;燃料增加控制部,其通过依次增加第1空气密度修正系数,来使初始燃料喷射量依次增加;以及完爆后喷射量计算部,其在与发动机启动后发动机的转速为完爆基准值以上的情况对应的发动机完爆之后,考虑由燃料增加控制部依次增加的空气密度修正系数,来计算发动机完爆后的燃料喷射量,由此既能够削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器及进气压传感器等压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。The engine control device according to the technical solution of the first aspect of the present invention is provided with: an initial injection amount calculation unit which considers a predetermined first air density correction coefficient after the height correction, and calculates the initial fuel injection amount at the time of starting the engine as a ratio and The initial fuel injection amount corresponding to the temperature of the engine is less than the basic fuel injection amount; the fuel increase control unit sequentially increases the initial fuel injection amount by sequentially increasing the first air density correction coefficient; and the post-explosion injection amount calculation unit It calculates the fuel injection amount after the engine is completely detonated by considering the air density correction coefficient sequentially increased by the fuel increase control part after the engine detonation corresponding to the case where the engine speed is above the detonation reference value after the engine is started. This can reduce the data capacity required for the height correction of the fuel injection amount without using a pressure sensor such as an atmospheric pressure sensor and an intake pressure sensor, achieve good startability, and suppress unnecessary fuel injection of the fuel amount.
另外,根据本发明第2方面的技术方案的发动机控制装置,还具备空气密度修正系数计算部,其在发动机完爆之后,考虑由燃料增加控制部依次增加的空气密度修正系数来计算第2空气密度修正系数,完爆后喷射量计算部考虑第2空气密度修正系数来计算发动机的完爆后的燃料喷射量,由此可实现良好的启动性,并且能够更可靠地抑制发动机在完爆后的不必要的燃料量的燃料喷射。In addition, the engine control device according to the technical solution of the second aspect of the present invention further includes an air density correction coefficient calculation unit that calculates the second air density correction coefficient in consideration of the air density correction coefficient that is sequentially increased by the fuel increase control unit after the engine has completely exploded. Density correction coefficient, post-detonation injection quantity calculation unit considers the second air density correction coefficient to calculate the fuel injection quantity after detonation of the engine, thereby achieving good startability and more reliably preventing the engine from detonating after detonation. Fuel injection of an unnecessary amount of fuel.
另外,根据本发明第3方面的技术方案的发动机控制装置,空气密度修正系数计算部在安装于发动机的排气系统上的氧传感器激活且与来自氧传感器的输出值相应的氧传感器反馈修正系数收敛之前,将由燃料增加控制部依次增加的空气密度修正系数设定为第2空气密度修正系数,由此可实现良好的启动性,并且能够根据氧传感器的工作状态来抑制发动机完爆后的不必要的燃料量的燃料喷射。In addition, according to the engine control device of the third aspect of the present invention, the air density correction coefficient calculation unit activates the oxygen sensor mounted on the exhaust system of the engine and feeds back the correction coefficient of the oxygen sensor corresponding to the output value from the oxygen sensor. Before converging, the air density correction coefficient sequentially increased by the fuel increase control unit is set as the second air density correction coefficient, thereby achieving good startability and suppressing engine failure after complete explosion according to the operating state of the oxygen sensor. Fuel injection of necessary fuel quantity.
另外,根据本发明第4方面的技术方案的发动机控制装置,空气密度修正系数计算部在氧传感器激活且氧传感器反馈修正系数收敛之后,当氧传感器反馈修正系数的偏差为规定值以上时,进一步考虑氧传感器反馈修正系数来计算第2空气密度修正系数,由此可实现良好的启动性,并且能够根据氧传感器的工作状态来更可靠地抑制发动机的完爆后的不必要的燃料量的燃料喷射。In addition, according to the engine control device according to the fourth aspect of the present invention, the air density correction coefficient calculation unit further calculates when the deviation of the oxygen sensor feedback correction coefficient is greater than or equal to a predetermined value after the oxygen sensor is activated and the oxygen sensor feedback correction coefficient converges. Considering the feedback correction coefficient of the oxygen sensor to calculate the second air density correction coefficient, it is possible to achieve good startability, and it is possible to more reliably suppress the unnecessary amount of fuel after the engine is completely detonated according to the operating state of the oxygen sensor. injection.
附图说明 Description of drawings
图1是示出本发明实施方式中的发动机控制装置以及应用该发动机控制装置的发动机的结构的示意图。FIG. 1 is a schematic diagram showing the configuration of an engine control device and an engine to which the engine control device is applied in an embodiment of the present invention.
图2是示出本实施方式中的发动机控制装置的控制处理的流程图。具体地说,(a)是示出该发动机控制处理的整体流程的流程图,(b)是示出(a)所示的发动机控制处理中的启动时燃料喷射量计算处理流程的流程图。FIG. 2 is a flowchart showing control processing of the engine control device in the present embodiment. Specifically, (a) is a flow chart showing the overall flow of the engine control process, and (b) is a flow chart showing the flow of start-time fuel injection amount calculation processing in the engine control process shown in (a).
图3是示出图2的(a)所示的发动机控制处理中的完爆后空气密度修正系数计算处理流程的流程图。3 is a flowchart showing the flow of post-explosion air density correction coefficient calculation processing in the engine control processing shown in (a) of FIG. 2 .
图4是用于说明本实施方式中的发动机控制处理的具体例的时序图,(a)是示出空气密度修正系数MAS、MA以及氧传感器反馈修正系数MG、MGR的时序图,(b)是示出发动机转速NE以及燃料喷射量TIS、TI的时序图。4 is a time chart for explaining a specific example of engine control processing in this embodiment, (a) is a time chart showing air density correction coefficients MAS, MA and oxygen sensor feedback correction coefficients MG, MGR, (b) It is a time chart showing the engine speed NE and the fuel injection amounts TIS, TI.
符号说明Symbol Description
1…发动机1…Engine
2…气缸体2…Cylinder block
3…水温传感器3…Water temperature sensor
4…活塞4…piston
5…连杆5…connecting rod
6…曲轴6… crankshaft
7…曲轴转角传感器7…Crank angle sensor
8…气缸盖8…Cylinder head
9…燃烧室9…combustion chamber
10…火花塞10…spark plug
11…进气通路11...intake passage
12…进气阀12…intake valve
13…喷油器13…Injector
14…节流阀14...throttle valve
15…节流阀开度传感器15...Throttle valve opening sensor
16…排气通路16...exhaust passage
17…排气阀17...exhaust valve
18…催化剂转换器18…catalytic converter
19…氧传感器19…oxygen sensor
100…发动机控制装置100…Engine control unit
101…曲轴转角信号检测部101...Crankshaft angle signal detection unit
102…节流阀开度检测部102...Throttle valve opening detection unit
103…氧传感器输出检测部103...Oxygen sensor output detection unit
104…发动机温度检测部104...Engine temperature detection unit
105…存储器105...memory
105a…ROM105a...ROM
105b…RAM105b...RAM
105c…EEPROM105c...EEPROM
106…发动机转速计算部106...Engine speed calculation department
107…空气密度修正系数计算部107...Air density correction coefficient calculation department
108…燃料喷射量控制部108...Fuel injection amount control unit
108a…初始喷射量计算部108a...Initial injection amount calculation unit
108b…燃料增加控制部108b... Fuel increase control unit
108c…完爆后喷射量计算部108c...Calculation Department of Injection Quantity after Explosion
109…点火正时控制部109…Ignition timing control unit
具体实施方式 Detailed ways
下面,适当参照附图来详细说明本发明实施方式中的发动机控制装置。Hereinafter, an engine control device in an embodiment of the present invention will be described in detail with appropriate reference to the drawings.
[发动机的结构][Structure of the engine]
首先,参照图1来详细说明应用了本发明实施方式中的发动机控制装置的发动机结构。First, the structure of an engine to which the engine control device in the embodiment of the present invention is applied will be described in detail with reference to FIG. 1 .
图1是示出本实施方式中的发动机控制装置以及应用了该发动机控制装置的发动机的结构的示意图。FIG. 1 is a schematic diagram showing the configuration of an engine control device in the present embodiment and an engine to which the engine control device is applied.
如图1所示,发动机1是装备在省略图示的车辆等移动体中的汽油发动机等内燃机,典型地,包括具有多个气缸的气缸体2。此外,为了便于说明,在图中仅示出1个气缸。As shown in FIG. 1 , the engine 1 is an internal combustion engine such as a gasoline engine installed in a mobile body such as a vehicle (not shown), and typically includes a cylinder block 2 having a plurality of cylinders. In addition, for convenience of explanation, only one cylinder is shown in the figure.
用于冷却发动机1的冷却水在气缸体2的侧壁内流通,形成省略图示的冷却水通路。在这样的冷却水通路中设置有水温传感器3。水温传感器3检测流过冷却水通路的冷却水的温度即发动机1的温度,并将该检测值作为电压信号输出至发动机控制装置100。此外,在发动机1是空冷式的情况下,可设置适合检测发动机1的温度的温度传感器来代替水温传感器3。Cooling water for cooling the engine 1 flows through the side wall of the cylinder block 2 to form a cooling water passage (not shown). A
在气缸体2的内部配置有活塞4。活塞4经由连杆5与曲轴6连接。在该曲轴6的附近设置有曲轴转角传感器7。曲轴转角传感器7检测曲轴6的旋转角度,并将该检测值作为电压信号输出至发动机控制装置100。A
在气缸体2的上部安装有气缸盖8。活塞4与气缸盖8之间的空间构成燃烧室9。A
在气缸盖8中设置有对燃烧室9内的混合气进行点火的火花塞10。通过发动机控制装置100控制对省略图示的点火线圈的通电来控制该火花塞10的点火动作。An ignition plug 10 for igniting the air-fuel mixture in the
另外,在气缸盖8上安装有与燃烧室9连通的进气通路11。在燃烧室9与进气通路11的连接部上设置有进气阀12。在进气通路11上设置有向其内部喷射燃料的喷油器13。另外,在进气通路11中,在喷油器13的上游侧设置有节流阀14。在节流阀14的附近设置有节流阀开度传感器15。节流阀开度传感器15检测节流阀14的开度并将该检测值作为电压信号输出至发动机控制装置100。此外,也可在气缸盖8上设置喷油器13,使得直接向燃烧室9内喷射燃料。In addition, an
另外,在气缸盖8上安装有与燃烧室9连通的排气通路16。在燃烧室9与排气通路16的连接部设置有排气阀17。在排气通路16上设置有用于净化发动机1的废气的催化剂转换器18。在排气通路16中的催化剂转换器18的上游设置有氧传感器19。氧传感器19检测发动机1的废气中的氧气浓度,并将该检测值作为电压信号输出至发动机控制装置100。In addition, an
[发动机控制装置的结构][Structure of engine control unit]
接着,参照图1更详细地说明本发明实施方式中的发动机控制装置的结构。Next, the configuration of the engine control device in the embodiment of the present invention will be described in more detail with reference to FIG. 1 .
如图1所示,发动机控制装置100典型地构成为具备微型计算机来进行运算处理的电子控制装置(ECU:Electric Control Unit),并由在车辆等移动体上装备的省略图示的电池提供电力,进行工作。该发动机控制装置100具备:曲轴转角信号检测部101、节流阀开度检测部102、氧传感器输出检测部103、发动机温度检测部104、存储器105、发动机转速计算部106、空气密度修正系数计算部107、燃料喷射量控制部108以及点火正时控制部109。此外,这样的曲轴转角信号检测部101、节流阀开度检测部102、氧传感器输出检测部103、发动机温度检测部104、发动机转速计算部106、空气密度修正系数计算部107、燃料喷射量控制部108以及点火正时控制部109作为运算处理的功能模块分别被示出。另外,空气密度修正系数计算部107也可设置为燃料喷射量控制部108的内部的功能模块。As shown in FIG. 1 , the
具体地说,曲轴转角信号检测部101读入从曲轴转角传感器7输出的电压信号,根据该电压信号来检测曲轴6的旋转角度,并将该检测值输出至发动机转速计算部106。节流阀开度检测部102根据从节流阀开度传感器15输出的电压信号来检测节流阀14的开度,并将该检测值输出至燃料喷射量控制部108。Specifically, the crank angle
氧传感器输出检测部103读入从氧传感器19输出的电压信号,根据该电压信号来检测氧传感器输出电压VG,并且分别根据该氧传感器输出电压VG来执行氧传感器19的激活判断、氧传感器反馈修正系数MG的计算、氧传感器反馈修正系数MG的收敛判断以及氧传感器反馈修正系数MG的偏差判断,将它们的计算值以及判断结果输出至空气密度修正系数计算部107。此外,氧传感器输出检测部103可只具备读入从氧传感器19输出的电压信号来检测氧传感器输出电压VG的功能,在此情况下,只要另外设置分别执行氧传感器19的激活判断、氧传感器反馈修正系数MG的计算、氧传感器反馈修正系数MG的收敛判断以及氧传感器反馈修正系数MG的偏差判断并将它们的计算值以及判断结果输出至空气密度修正系数计算部107的计算判断功能模块即可。The oxygen sensor
发动机温度检测部104读入从水温传感器3输出的电压信号,根据该电压信号来检测发动机1的温度,并将该检测值输出至燃料喷射量控制部108。The engine
存储器105具备:ROM(Read Only Memory:只读存储器)105a、RAM(RandomAccess Memory:随机存取存储器)105b、EEPROM(Electronically Erasable andProgrammable Read Only Memory:电可插可编程只读存储器)105c等各种存储器。ROM105a存储用于控制发动机1的各种控制程序及用于控制发动机1的控制数据等各种数据。作为各种控制数据,例如可列举与发动机转速和节流阀开度对应的基本燃料喷射量的映射数据、与发动机温度对应的基本燃料喷射量的映射数据、用于判断发动机1的完爆状态的基准转速值(完爆基准值)以及进行高地修正后的空气密度修正系数MAS(第1空气密度修正修正系数)的值等。另外,作为在RAM105b及EEPROM105c中存储的各种数据,可列举发动机控制装置100所算出的各种计算值的数据或发动机控制装置100所设定的各种标志的值等。此外,该存储器105也可以另外设置在发动机控制装置100的外部。The
发动机转速计算部106根据从曲轴转角信号检测部101输出的曲轴6的旋转角度的检测值来算出发动机1的转速,并将该计算值分别输出至燃料喷射量控制部108以及点火正时控制部109。The engine rotation
空气密度修正系数计算部107利用来自氧传感器输出检测部103的计算值以及判断结果这样的各种输出值和存储在存储器105内的各种数据,主要算出发动机1在完爆后的空气密度修正系数即完爆后空气密度修正系数MA(第2空气密度修正系数),并将该计算值分别输出至燃料喷射量控制部108以及点火正时控制部109。The air density correction
燃料喷射量控制部108具备初始喷射量计算部108a、燃料增加控制部108b以及完爆后喷射量计算部108c来作为该运算处理的功能模块,通过发动机1启动、到达完爆状态、且维持该完爆状态的过程,来控制喷油器13的燃料喷射量。此外,在发动机1启动、到达完爆的过程中,初始喷射量计算部108a以及燃料增加控制部108b在燃料喷射量控制部108按照启动时燃料喷射量的初始值TISI及启动时燃料喷射量TIS从喷油器13喷出燃料时发挥功能,在发动机1的完爆之后,完爆后喷射量计算部108c在燃料喷射量控制部108按照发动机完爆后的燃料喷射量TI从喷油器13喷出燃料时发挥功能。The fuel injection
点火正时控制部109通过控制对省略图示的点火线圈的通电状态,来控制火花塞10的点火动作。The ignition
[发动机控制处理][Engine Control Processing]
具有以上这种结构的发动机控制装置100通过执行以下所示的发动机控制处理,既可削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器或进气压传感器等压力传感器,又能实现良好的启动性,并且抑制不必要的燃料量的燃料喷射。以下,参照图2以及图3所示的流程图,来详细说明执行该发动机控制处理时的发动机控制装置100的动作。The
图2(a)是示出本实施方式中的发动机控制处理的整体流程的流程图。FIG. 2( a ) is a flowchart showing the overall flow of engine control processing in this embodiment.
图2(a)所示的发动机控制处理在车辆等移动体的点火开关从断开状态切换至导通状态的时刻开始,发动机控制处理进入到步骤S1的处理。此外,针对发动机1的每次旋转而反复开始执行该发动机控制处理。另外,可通过发动机控制装置100读出并执行存储在存储器105的ROM105a内的控制程序来实现该发动机控制处理。The engine control process shown in FIG. 2( a ) starts when the ignition switch of a mobile body such as a vehicle is switched from the off state to the on state, and the engine control process proceeds to the process of step S1 . In addition, this engine control process is repeatedly started and executed every rotation of the engine 1 . In addition, this engine control process can be realized by the
在步骤S1的处理中,发动机转速计算部106根据从曲轴转角信号检测部101输出的表示曲轴6的旋转角度的检测值来算出发动机1的转速NE,将表示该计算出的发动机转速NE的电信号分别输出至燃料喷射量控制部108以及点火正时控制部109,其中,该曲轴转角信号检测部101被输入来自曲轴转角传感器7的电压信号。由此,步骤S1的处理结束,发动机控制处理进入到步骤S2的处理。In the process of step S1, the engine rotation
在步骤S2的处理中,节流阀开度检测部102根据从节流阀开度传感器15输出的电压信号来检测节流阀14的开度TH,将表示所检测出的节流阀14的开度TH的电信号输出至燃料喷射量控制部108。由此,步骤S2的处理结束,发动机控制处理进入到步骤S3的处理。In the process of step S2, the throttle
在步骤S3的处理中,发动机温度检测部104根据从水温传感器3输出的电压信号来检测发动机1的温度TW,并将表示所检测出的发动机1的温度TW的电信号输出至燃料喷射量控制部108。由此,步骤S3的处理结束,发动机控制处理进入到步骤S4的处理。In the process of step S3, the engine
在步骤S4的处理中,燃料喷射量控制部108判别通过步骤S1的处理来算出的发动机转速NE是否是规定的基准转速(完爆基准值)以上。这里,将该基准转速预先设定为比发动机1启动时的转速大规定量的值,并存储到ROM105a内,燃料喷射量控制部108读出并使用存储在ROM105a中的该值。在判别结果是发动机转速NE小于规定的基准转速时,燃料喷射量控制部108判断为发动机1没有完爆,发动机控制处理进入到步骤S5的处理。另一方面,在判别结果是发动机转速NE为规定的基准转速以上时,燃料喷射量控制部108判断为发动机1完爆,发动机控制处理进入到步骤S6的处理。In the process of step S4, the fuel injection
在步骤S5的处理中,燃料喷射量控制部108执行启动时燃料喷射量计算处理,在该启动时燃料喷射量计算处理中,算出发动机启动时、具体地说是从发动机1起动开始到完爆为止的期间的燃料喷射量。在后面,参照图2(b)所示的流程图来详细叙述该启动时燃料喷射量计算处理。由此,步骤S5的处理结束,一系列的发动机控制处理结束。In the process of step S5, the fuel injection
另一方面,在步骤S6的处理中,氧传感器输出检测部103接收从氧传感器19输出的电压信号,根据该电压信号检测氧传感器输出电压VG。由此,步骤S6的处理结束,发动机控制处理进入到步骤S7的处理。On the other hand, in the process of step S6, the oxygen sensor
在步骤S7的处理中,氧传感器输出检测部103根据通过步骤S6的处理检测出的氧传感器输出电压VG的值,来判别是否检测出与发动机1的废气中的氧气浓度相应变化的氧传感器输出电压VG,由此来判别氧传感器19是否已激活。在判别结果是没有检测出该氧传感器输出电压VG时,氧传感器输出检测部103判断为氧传感器19没有激活,发动机控制处理进入到步骤S9的处理。另一方面,在判别结果是检测出该氧传感器输出电压VG时,氧传感器输出检测部103判断为氧传感器19已激活,发动机控制处理进入到步骤S8的处理。In the process of step S7, the oxygen sensor
在步骤S8的处理中,氧传感器输出检测部103在例如氧传感器输出电压VG是规定值以上(例如0.45伏以上)时减小氧传感器反馈修正系数MG,在氧传感器输出电压VG小于规定值(例如小于0.45伏)时增大氧传感器反馈修正系数MG,由此与发动机1的废气中的氧气浓度对应地算出氧传感器反馈修正系数MG,使得发动机1的空燃比达到理论空燃比,并将表示所计算出的氧传感器反馈修正系数MG的电信号输出至空气密度修正系数计算部107。由此,步骤S8的处理结束,发动机控制处理进入到步骤S9的处理。In the process of step S8, the oxygen sensor
在步骤S9的处理中,空气密度修正系数计算部107执行完爆后空气密度修正系数计算处理,在该完爆后空气密度修正系数计算处理中,算出发动机1在完爆后的空气密度修正系数即完爆后空气密度修正系数MA(第2空气密度修正系数)。在后面,参照图3所示的流程图来详细地叙述该完爆后空气密度修正系数计算处理。由此,步骤S9的处理结束,发动机控制处理进入到步骤S10的处理。In the process of step S9, the air density correction
在步骤S10的处理中,完爆后喷射量计算部108c从ROM105a读出与发动机转速NE和节流阀开度TH对应的基本燃料喷射量的映射数据,并根据该映射数据来算出与通过步骤S1以及步骤S2的处理获得的发动机转速NE和节流阀开度TH对应的基本燃料喷射量。接着,完爆后喷射量计算部108c通过将这样算出的基本燃料喷射量与在步骤S9的处理中由空气密度修正系数计算部107所算出的完爆后空气密度修正系数MA相乘,来算出发动机1在完爆后的燃料喷射量即完爆后燃料喷射量TI。然后,燃料喷射量控制部108根据完爆后喷射量计算部108c所算出的完爆后燃料喷射量TI来控制喷油器13的燃料喷射量,实施从喷油器13喷出燃料的完爆后燃料喷射。由此,步骤S10的处理结束,一系列的发动机控制处理结束。此外,作为该基本燃料喷射量的映射数据的发动机控制参数,可列举发动机转速NE以及节流阀开度TH来作为能够实现简便且可靠的控制的参数,但不局限于此,可根据需要适当取舍地选择采用其它发动机控制参数。In the process of step S10, the post-explosion injection
[启动时燃料喷射量计算处理][Fuel injection amount calculation processing at startup]
接着,参照图2(b)所示的流程图来详细说明执行该发动机控制处理中的启动时燃料喷射量计算处理时的发动机控制装置100的动作。Next, the operation of the
图2(b)是示出图2(a)所示的发动机控制处理中的启动时燃料喷射量计算处理流程的流程图。FIG. 2( b ) is a flowchart showing the flow of start-time fuel injection amount calculation processing in the engine control processing shown in FIG. 2( a ).
图2(b)所示的启动时燃料喷射量计算处理是在图2(a)所示的步骤S4的处理中判断为发动机1没有完爆的时刻开始的,启动时燃料喷射量计算处理进入到步骤S21的处理。The start-up fuel injection amount calculation process shown in FIG. 2( b) is started when it is determined that the engine 1 has not fully exploded in the process of step S4 shown in FIG. 2( a), and the start-up fuel injection amount calculation process enters The process proceeds to step S21.
在步骤S21的处理中,燃料喷射量控制部108读出在RAM105b等中存储的初始值计算完毕标志的值,并判别该值是否为1,由此来判别启动时燃料喷射量的初始值TISI是否已经算出。在判别结果是初始值计算完毕标志的值为1时,燃料喷射量控制部108判断为启动时燃料喷射量的初始值TISI已经算出,启动时燃料喷射量计算处理进入到步骤S24的处理。另一方面,在判别结果是初始值计算完毕标志的值为0时,燃料喷射量控制部108判断为启动时燃料喷射量的初始值TISI没有计算完毕,启动时燃料喷射量计算处理进入到步骤S22的处理。In the process of step S21, the fuel injection
在步骤S22的处理中,初始喷射量计算部108a从ROM105a读出与发动机温度TW对应的基本燃料喷射量的映射数据,根据该映射数据来算出与利用步骤S3的处理获得的发动机温度TW对应的基本燃料喷射量,并且从ROM105a读出进行高地修正后的空气密度修正系数MAS(第1空气密度修正修正系数)的值,然后将计算出的基本燃料喷射量与该进行高地修正后的空气密度修正系数MAS的值相乘,由此算出启动时燃料喷射量的初始值TISI。并且,初始喷射量计算部108a将该计算出的启动时燃料喷射量的初始值TISI的值存储到RAM105b等内。根据此处理,仅将发动机1启动时的初始燃料喷射量设定为比与发动机温度TW相应的基本燃料喷射量少的燃料喷射量。此外,作为该基本燃料喷射量的映射数据的发动机控制参数,可列举发动机温度TW来作为能够实现简便且可靠的控制的参数,但不局限于此,还可以根据需要适当取舍地选择采用其它发动机控制参数。In the processing of step S22, the initial injection
这里,将进行高地修正后的空气密度修正系数MAS与基本燃料喷射量相乘的原因是,考虑到车辆等移动体位于高地处而启动发动机1的情况,将启动发动机1时的初始燃料喷射量,作为适合在车辆等移动体位于低地处而启动发动机1时使发动机1完爆的发动机启动时的初始燃料喷射量、即比与发动机温度TW对应的基本燃料喷射量少的值,由此,实际上能够可靠地获得在高地处启动发动机1时最适合完爆的燃料喷射量。换言之,如果将在高地处的发动机启动时的初始燃料喷射量设定得过大,则发动机1虽然容易完爆,但混合气不需要继续维持在较浓状态,从而无法获得高地处的最适当的燃料喷射量,所以为了不产生这样的状况而采用已应对的结构。由此,步骤S22的处理结束,启动时燃料喷射量计算处理进入到步骤S23的处理。此外具体地说,这里认为高地是标高2000m左右,作为进行高地修正后的空气密度修正系数MAS,采用可提供在相当于标高2000m的位置处启动发动机1时使发动机1完爆所需的发动机启动时的初始燃料喷射的值,在此情况下,将该值例如设定为0.8。Here, the reason for multiplying the air density correction coefficient MAS after the height correction by the basic fuel injection amount is that the initial fuel injection amount at the time of starting the engine 1 is taken into account when the engine 1 is started when a mobile body such as a vehicle is located , as the initial fuel injection amount at the time of starting the engine suitable for causing the engine 1 to explode completely when the engine 1 is started when a mobile body such as a vehicle is located in a low place, that is, a value smaller than the basic fuel injection amount corresponding to the engine temperature TW, whereby, It is actually possible to reliably obtain the fuel injection amount most suitable for complete explosion when starting the engine 1 at a high place. In other words, if the initial fuel injection amount when starting the engine at high altitudes is set too large, although the engine 1 is likely to explode, the mixture does not need to be kept in a rich state, so that the optimum fuel injection at high altitudes cannot be obtained. Therefore, in order not to produce such a situation, a coping structure is adopted. Thereby, the process of step S22 ends, and the start-time fuel injection amount calculation process proceeds to the process of step S23. In addition, specifically, it is considered that the highland is about 2000m above sea level, and as the air density correction coefficient MAS after the highland correction, the engine starting pressure required to start the engine 1 when starting the engine 1 at a position equivalent to 2000m above sea level is used to complete the explosion of the engine 1. In this case, the value is set to 0.8, for example.
在步骤S23的处理中,燃料喷射量控制部108将初始值计算完毕标志的值设定为1并存储到RAM105b等内,该初始值计算完毕标志表示已算出启动时燃料喷射量的初始值TISI的情况。由此,步骤S23的处理结束,启动时燃料喷射量计算处理进入到步骤S28的处理。In the process of step S23, the fuel injection
另一方面,在步骤S24的处理中,燃料喷射量控制部108从ROM105a读出进行高地修正后的空气密度修正系数MAS的值,或者利用前次的步骤S26的处理来读出在RAM105b等中存储的已经增加的空气密度修正系数MAS的值,判别所读出的值是否是规定值以上。在判别结果是所读出的值为规定值以上时,启动时燃料喷射量计算处理进入到步骤S25的处理。另一方面,在判别结果是所读出的值小于规定值时,启动时燃料喷射量计算处理进入到步骤S26的处理。这里,将所判别的规定值设定为1,该值1是在从发动机1启动时到完爆时的过程中混合气不会因没必要地增加启动时燃料喷射量而没必要地成为较浓状态的空气密度修正系数MAS的值。On the other hand, in the process of step S24, the fuel injection
在步骤S25的处理中,燃料喷射量控制部108将进行高地修正后的空气密度修正系数MAS的值设定为1,并将所设定的进行高地修正后的空气密度修正系数MAS的值存储到RAM105b等内。通过利用该处理将空气密度修正系数MAS的值设定为1,来抑制在从发动机1启动时到完爆时的过程中混合气没必要地成为较浓状态的情况。由此,步骤S25的处理结束,启动时燃料喷射量计算处理进入到步骤S27的处理。In the process of step S25, the fuel injection
在步骤S26的处理中,燃料增加控制部108b从ROM105a中读出进行高地修正后的空气密度修正系数MAS的值,或者利用前次的步骤S26的处理读出在RAM105b等中存储的已经增加的空气密度修正系数MAS的值,并将该值与小于1的规定值相加,从而增加进行高地修正后的空气密度修正系数MAS的值,并将该已经增加的空气密度修正系数MAS的值存储到RAM105b等内。根据此处理,进行高地修正后的空气密度修正系数MAS按照发动机1的每次旋转依次增加规定值来进行更新。由此,步骤S26的处理结束,启动时燃料喷射量计算处理进入到步骤S27的处理。这里,用于相加的比1小的规定值依赖于从发动机1启动开始到完爆为止的时间等并考虑应该增加几次来决定,例如只要设定为比1充分小的0.03的值即可。In the process of step S26, the fuel
在步骤S27的处理中,初始喷射量计算部108a利用步骤S25的处理或步骤S26的处理来读出在RAM105b等中存储的已经增加的空气密度修正系数MAS的值,并且利用步骤S22的处理读出在RAM105b等中存储的启动时燃料喷射量的初始值TISI,然后使这些值相乘,由此来算出从启动时燃料喷射量的初始值TISI依次增加的启动时燃料喷射量TIS,将所计算出的启动时燃料喷射量TIS的值存储到RAM105b等内。通过该处理,启动时燃料喷射量TIS根据在步骤S26的处理中依次增加的空气密度修正系数MAS,按照发动机1的每次旋转依次增加并进行更新。由此,步骤S27的处理结束,启动时燃料喷射量计算处理进入到步骤S28的处理。In the process of step S27, the initial injection
在步骤S28的处理中,燃料喷射量控制部108利用步骤S22的处理读出在RAM105b等中存储的启动时燃料喷射量的初始值TISI,或者利用步骤S27的处理读出在RAM105b等中存储的启动时燃料喷射量TIS的值,并根据此值来控制喷油器13的燃料喷射量,实施从喷油器13喷出燃料的启动时燃料喷射。由此,步骤S28的处理结束,一系列的启动时燃料喷射量计算处理结束,图2(a)所示的一系列的发动机控制处理也一并结束。In the processing of step S28, the fuel injection
[完爆后空气密度修正系数计算处理][Calculation and processing of air density correction coefficient after explosion]
接着,参照图3所示的流程图,来详细说明执行图2(a)所示的发动机控制处理中的完爆后空气密度修正系数计算处理时的发动机控制装置100的动作。Next, the operation of the
图3是示出图2(a)所示的发动机控制处理中的完爆后空气密度修正系数计算处理的流程的流程图。3 is a flowchart showing the flow of post-explosion air density correction coefficient calculation processing in the engine control processing shown in FIG. 2( a ).
图3所示的流程图是在图2(a)所示的步骤S7的处理中判别为氧传感器19没有激活的时刻或者图2(a)所示的步骤S8的处理已结束的时刻开始的,完爆后空气密度修正系数计算处理进入到步骤S31的处理。The flowchart shown in FIG. 3 is started when it is determined that the
在步骤S31的处理中,燃料喷射量控制部108读出在RAM105b等中存储的完爆后空气密度修正系数计算完毕标志的值,并判别该值是否为1,由此来判别发动机1在完爆以后的空气密度修正系数即完爆后空气密度修正系数MA(第2空气密度修正系数)是否已经算出。在判别结果是完爆后空气密度修正系数计算完毕标志的值为1时,燃料喷射量控制部108判断为完爆后空气密度修正系数MA已经算出,完爆后空气密度修正系数计算处理进入到步骤S34的处理。另一方面,在判别结果是完爆后空气密度修正系数计算完毕标志的值为0时,燃料喷射量控制部108判断为完爆后空气密度修正系数MA没有计算完毕,完爆后空气密度修正系数计算处理进入到步骤S32的处理。In the process of step S31, the fuel injection
在步骤S32的处理中,空气密度修正系数计算部107在图2(b)所示的步骤S26的处理中读出存储于RAM105b等内的已经增加的空气密度修正系数MAS的值,将该值设定为完爆后空气密度修正系数MA的值,并将该设定值存储到RAM105b等内。由此,步骤S32的处理结束,完爆后空气密度修正系数计算处理进入到步骤S33的处理。In the process of step S32, the air density correction
在步骤S33的处理中,燃料喷射量控制部108将完爆后空气密度修正系数计算完毕标志的值设定为1,并将该值存储到RAM105b等内。由此,步骤S33的处理结束,完爆后空气密度修正系数计算处理进入到步骤S38的处理。In the process of step S33, the fuel injection
另一方面,在步骤S34的处理中,氧传感器输出检测部103算出氧传感器反馈修正系数MG的最大、最小峰值之间的移动平均值,并判别该移动平均值的变动量是否处于规定范围内,由此来判别氧传感器反馈修正系数MG是否已经收敛。在判别结果是氧传感器反馈修正系数MG的变动量不在规定范围内时,氧传感器输出检测部103判断为氧传感器反馈修正系数MG没有收敛,一系列的完爆后空气密度修正系数计算处理结束,图2(a)所示的一系列发动机控制处理也一并结束。另一方面,在判别结果是氧传感器反馈修正系数MG的变动量处于规定范围内时,氧传感器输出检测部103判断为氧传感器反馈修正系数MG已收敛,完爆后空气密度修正系数计算处理进入到步骤S35的处理。此外,考虑到氧传感器19的种类及氧传感器输出检测部103的分辨率等来适当设定该规定范围、即其上限值以及下限值,并预先存储到ROM105a内,从ROM105a读出并使用这些值。On the other hand, in the process of step S34, the oxygen sensor
在步骤S35的处理中,氧传感器输出检测部103将已收敛的氧传感器反馈修正系数MG设定为收敛后氧传感器反馈修正系数MGR,算出收敛后氧传感器反馈修正系数MGR与在完爆后空气密度修正系数MA的值恰当时收敛后氧传感器反馈修正系数MGR应取的值即1.0倍之间的偏差,并判别所算出的偏差值是否是规定值以上。在判别结果是偏差值小于规定值时,一系列的完爆后空气密度修正系数计算处理结束,图2(a)所示的一系列的发动机控制处理也一并结束。另一方面,在判别结果是偏差值为规定值以上时,氧传感器输出检测部103将表示收敛后氧传感器反馈修正系数MGR的值的电信号输出至空气密度修正系数计算部107,完爆后空气密度修正系数计算处理进入到步骤S36的处理。这里,只要将对偏差值进行比较的规定值设定为如下这样的值即可,该值是为了更正完爆后空气密度修正系数MA的值成为没必要地增大燃料喷射量而使混合气没必要地变为较浓状态的值的状态所需的充分的值,这里设定为0.07的值,其中,所述完爆后空气密度修正系数MA的值是在步骤S32的处理及步骤S36的处理中设定的。In the process of step S35, the oxygen sensor
在步骤S36的处理中,空气密度修正系数计算部107利用步骤S32的处理或前次的步骤S36的处理来读出在RAM105b等中存储的完爆后空气密度修正系数MA的值,将该值与在步骤S35的处理中输出的收敛后氧传感器反馈修正系数MGR的值相乘后所得的值设定为完爆后空气密度修正系数MA的值,将表示该设定值的电信号输出至燃料喷射量控制部108、具体地说是完爆后喷射量计算部108c,并且将该设定值存储到RAM105b等内。根据该处理,将完爆后空气密度修正系数MA的值修正并更新为不会有因燃料喷射量没必要地增加而使混合气没必要地成为较浓状态这一情况的程度的值、即适合于当前车辆等移动体所处的高度的值。由此,步骤S36的处理结束,完爆后空气密度修正系数计算处理进入到步骤S37的处理。In the process of step S36, the air density correction
在步骤S37的处理中,氧传感器输出检测部103将自身所保持的氧传感器反馈修正系数MG以及收敛后氧传感器反馈修正系数MGR的值复位为1,为下次处理做准备。由此,步骤S37的处理结束,完爆后空气密度修正系数计算处理进入到步骤S38的处理。In the processing of step S37 , the oxygen sensor
在步骤S38的处理中,空气密度修正系数计算部107根据在步骤S36的处理中获得的完爆后空气密度修正系数MA的值来算出大气压PA的值,并将计算值存储到RAM105b等内。存储于存储器105内的大气压PA的值被使用于在车辆等移动体内设置的显示装置上的显示及各种控制中。由此,步骤S38的处理结束,一系列的完爆后空气密度修正系数计算处理结束。In the process of step S38, the air density correction
[具体例][specific example]
最后,参照图4来详细说明以上的发动机控制处理的具体例。Finally, a specific example of the above engine control processing will be described in detail with reference to FIG. 4 .
图4是用于说明本实施方式中的发动机控制处理的具体例的时序图,图4(a)示出空气密度修正系数MAS、MA以及氧传感器反馈修正系数MG、MGR的时序图,图4(b)示出发动机转速NE以及燃料喷射量TIS、TI的时序图。此外,在本具体例中,为了便于说明,而使发动机启动后的节流阀14的开度固定。FIG. 4 is a time chart for explaining a specific example of engine control processing in this embodiment. FIG. (b) shows a timing chart of the engine speed NE and the fuel injection amounts TIS, TI. In addition, in this specific example, for convenience of description, the opening degree of the
(1)时刻T=T0(1) Time T=T0
在图4所示的时刻T=T0时,当点火开关从断开状态切换至导通状态来启动发动机时,针对发动机1的每次旋转来反复开始发动机控制处理。这样,在已开始发动机控制处理的时刻,初始喷射量计算部108a将与发动机温度TW对应的基本燃料喷射量和与相当于标高2000m的高地对应地进行高地修正后的空气密度修正系数MAS(本具体例中的值是0.8)相乘,来算出启动时燃料喷射量的初始值TISI。然后,燃料喷射量控制部108根据初始喷射量计算部108a所算出的启动时燃料喷射量的初始值TISI来控制喷油器13的燃料喷射量,使燃料开始从喷油器13喷出。At time T=T0 shown in FIG. 4 , when the ignition switch is switched from the off state to the on state to start the engine, the engine control process is repeatedly started for every revolution of the engine 1 . In this way, when the engine control process is started, the initial injection
(2)期间T=T0~T1(2) Period T=T0~T1
接着,在期间T=T0~T1中,燃料增加控制部108b针对发动机1的每次旋转依次增加进行高地修正后的空气密度修正系数MAS的值,初始喷射量计算部108a通过将该已经增加的空气密度修正系数MAS与启动时燃料喷射量的初始值TISI相乘,来依次增加并算出启动时燃料喷射量TIS。然后,燃料喷射量控制部108根据初始喷射量计算部108a所算出的启动时燃料喷射量TIS来控制喷油器13的燃料喷射量,使燃料从喷油器13喷出。Next, during the period T=T0 to T1, the fuel
(3)期间T=T1~T2(3) Period T=T1~T2
接着,当在时刻T=T1判断为发动机1已完爆时,空气密度修正系数计算部107将在时刻T=T1之前依次增加的已增加完毕的空气密度修正系数MAS的时刻T=T1时的值(本具体例中是0.87)设定为完爆后空气密度修正系数MA的值,完爆后喷射量计算部108c通过将与发动机转速NE以及节流阀开度TH对应的基本燃料喷射量和完爆后空气密度修正系数MA相乘来算出完爆后燃料喷射量TI。然后,燃料喷射量控制部108根据完爆后喷射量计算部108c所算出的完爆后燃料喷射量TI来控制喷油器13的燃料喷射量,使燃料从喷油器13喷出。此外,该燃料喷射量的控制本身经过时刻T=T2,维持到时刻T=T3。Next, when it is determined at time T=T1 that the engine 1 has fully exploded, the air density correction
(4)期间T=T2~T3(4) Period T=T2~T3
接着,当在时刻T=T2从氧传感器19开始输出与发动机1的旋转相应的电压信号时,在到时刻T=T3为止的期间,氧传感器输出检测部103在判断出氧传感器19的激活之后,算出氧传感器反馈修正系数MG的最大、最小峰值之间的移动平均值,并判别该移动平均值的变动量是否处于规定范围内,由此来判别氧传感器反馈修正系数MG是否已收敛,在氧传感器反馈修正系数MG收敛之后,算出收敛后氧传感器反馈修正系数MGR与规定值10倍的偏差Δx,并判别所算出的偏差Δx是否是规定值0.07以上。Next, when the
(5)时刻T=T3以后(5) After time T=T3
接着,当在时刻T=T3判断为偏差Δx是规定值0.07以上时,空气密度修正系数计算部107将当前的完爆后空气密度修正系数MA的值与收敛后氧传感器反馈修正系数MGR的值相乘后所得的值设定并更新为完爆后空气密度修正系数MA的值,完爆后喷射量计算部108c通过将基本燃料喷射量与这样更新后的完爆后空气密度修正系数MA相乘来算出完爆后燃料喷射量TI。此时,将完爆后空气密度修正系数MA的值修正为适合当前车辆等移动体所处的高度的值。具体地说,在期间T=T2~T3中,因为完爆后空气密度修正系数MA的值是0.87、且收敛后氧传感器反馈修正系数MGR的值是0.92,所以可知:当将它们相乘时约为0.8,当前车辆等移动体处在相当于标高2000m的高地,而且可知已将完爆后空气密度修正系数MA的值修正为适合相当于标高2000m的高度的值。并且在时刻T=T3以后,燃料喷射量控制部108根据完爆后喷射量计算部108c所算出的完爆后燃料喷射量TI来控制喷油器13的燃料喷射量,使燃料从喷油器13喷出。此时,发动机转速NE在规定的空转转速下稳定。Next, when it is determined at time T=T3 that the deviation Δx is greater than or equal to the predetermined value 0.07, the air density correction
由以上说明可知,在本实施方式的发动机控制处理中,初始喷射量计算部108a考虑到进行高地修正后的空气密度修正系数MAS,计算发动机1的启动时燃料喷射量的初始值TISI作为比与发动机温度TW相应的基本燃料喷射量少的燃料喷射量,燃料增加控制部108b通过依次增加空气密度修正系数MAS,来使发动机1的启动时燃料喷射量TIS从启动时燃料喷射量的初始值TISI依次增加,完爆后喷射量计算部108c在发动机1完爆后,考虑利用燃料增加控制部108b依次增加的空气密度修正系数MAS来算出发动机1的完爆后燃料喷射量TI,所以既可削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器或进气压传感器等压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。As can be seen from the above description, in the engine control process of the present embodiment, the initial injection
另外,在本实施方式的发动机控制处理中,空气密度修正系数计算部107在发动机1完爆之后,考虑利用燃料增加控制部108b依次增加的空气密度修正系数MAS来算出完爆后空气密度修正系数MA,完爆后喷射量计算部108c考虑该完爆后空气密度修正系数MA来算出发动机1的完爆后燃料喷射量TI,所以可实现良好的启动性,并且能够更可靠地抑制发动机1在完爆后的不必要的燃料量的燃料喷射。In addition, in the engine control process of the present embodiment, the air density correction
另外,在本实施方式的发动机控制处理中,空气密度修正系数计算部107在安装于发动机1的排气系统上的氧传感器19激活且与来自氧传感器19的输出值相应的氧传感器反馈修正系数MG收敛之前,将利用燃料增加控制部108b依次增加的空气密度修正系数MAS设定为完爆后空气密度修正系数MA,所以能够实现良好的启动性,并且可根据氧传感器19的动作状态来抑制发动机1在完爆后的没必要的燃料量的燃料喷射。In addition, in the engine control process of the present embodiment, the air density correction
另外,在本实施方式的发动机控制处理中,空气密度修正系数计算部107在氧传感器19激活且氧传感器反馈修正系数MG收敛之后,当该收敛后氧传感器反馈修正系数MGR的偏差为规定值以上时,进一步考虑收敛后氧传感器反馈修正系数MGR来算出完爆后空气密度修正系数MA,所以可实现良好的启动性,并且能够根据氧传感器19的动作状态来更可靠地抑制发动机1在完爆后的不必要的燃料量的燃料喷射。In addition, in the engine control process of the present embodiment, after the
此外,在本发明中,部件的种类、配置、个数等不局限于上述实施方式,理所当然地,在不脱离本发明主旨的范围内可适当地进行变更,可将其结构要素适当置换为能起到同等作用效果的要素等。In addition, in the present invention, the type, arrangement, number, etc. of components are not limited to the above-mentioned embodiments, and of course, can be appropriately changed without departing from the gist of the present invention, and the constituent elements can be appropriately replaced by elements with the same effect.
工业上的可利用性Industrial availability
如以上所说明的那样,在本发明中,可提供这样的发动机控制装置:其既能削减燃料喷射量的高地修正所需的数据容量而不采用大气压传感器或进气压传感器等压力传感器,又能实现良好的启动性,并且能够抑制不必要的燃料量的燃料喷射。根据其普遍通用的特性,可期待着能够广泛应用于车辆等移动体的发动机中。As described above, in the present invention, it is possible to provide an engine control device that can reduce the data volume required for high-altitude correction of the fuel injection amount without using a pressure sensor such as an atmospheric pressure sensor or an intake pressure sensor, and can Good startability is achieved, and fuel injection of an unnecessary fuel amount can be suppressed. Due to its universal properties, it is expected to be widely used in engines of moving bodies such as vehicles.
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JP2012202255A (en) | 2012-10-22 |
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