TW552407B - Intake-air pressure detecting method for internal-combustion engine - Google Patents
Intake-air pressure detecting method for internal-combustion engine Download PDFInfo
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五、發明說明(1) 發明所屬技術領域 本發明係有關於用以檢測用 轉參數之進氣壓之進氣M檢測方法、在' 所需之運 :實施直接使用之進氣壓檢測襄置以及::2测方法 置。 “、、铽之控制裝 習知技術 以往内燃機之進氣壓在燃料喷射控制、 或排氣回流控制等各種内燃機之控制用餹期控制 例如’在所謂的「D —J系統」(量測進氣通數,:。 :燃料喷射之系統)之引擎,自進氣壓和引擎轉進,壓:進 擎之燃料室所吸入之進氣量後,依照所計算之^ -引 ,噴射量。可是,在往復式引擎,因伴隨活塞之往^運^ 在進氣發生脈動,進氣壓也隨著變動。因而,益法 , 壓感測器所檢測之進氣壓之值直接用作運轉夂數^ 燃機之控制會變成不安定。 乡 為内 因此,為了檢測排除了進氣壓脈動之影響後用於内燃 機之控制,至目前為止提議了各種技術。 …、 、/在一般之技術上,想到藉著對進氣壓感測器之檢測值 進行「平滑化處理」,將進氣壓脈動伴隨之進氣壓之變動 平滑化。「平滑化處理」係將按照既定之週期取樣之檢測 值平均化之處理,能以「平滑化係數」任意的設定其平均 化之程度。 此外,在特開平1 -3 1 8938號公報也公開一樣之技術之V. Description of the invention (1) The technical field to which the invention belongs The present invention relates to an intake air M detection method for detecting an intake pressure of a rotation parameter, a required operation: implementation of direct-use intake pressure detection, and: : 2 test methods set. ", Control technology of conventional control technology for various internal combustion engines, such as fuel injection control or exhaust gas recirculation control, in the conventional internal combustion engine. For example," in the so-called "D-J system" (measurement of intake air) Flux, :: Fuel injection system) of the engine, from the intake pressure and engine rotation, pressure: the intake amount of intake air into the engine's fuel chamber, according to the calculated ^ -injection, injection volume. However, in a reciprocating engine, the intake air pulsates due to the movement of the piston, and the intake air pressure also changes accordingly. Therefore, with the benefit method, the value of the intake air pressure detected by the pressure sensor is directly used as the operating number ^ The control of the gas turbine becomes unstable. Therefore, various technologies have been proposed so far for detecting and controlling the internal combustion engine after excluding the influence of the intake pressure pulsation. …, // In general technology, it is thought to smooth the fluctuation of the intake pressure accompanying the pulsation of intake pressure by performing a “smoothing process” on the detection value of the intake pressure sensor. The "smoothing process" is a process of averaging the detection values sampled at a predetermined period, and the degree of averaging can be arbitrarily set with the "smoothing coefficient". In addition, Japanese Patent Application Laid-Open No. 1-3 1938 discloses the same technique.
2097-4906-PF(N);Ahddub.p t d 第5頁 五、發明說明(2) 例子。即,在該公 ^ 驅動週期取樣造二之進氣管壓力量測裝置,每隔既定之 所得到之進氣壓:U::器所檢測之進氣壓,對在該取樣 值。而,在内燃播值進行相加平均處理,計算平均 氣壓之計算值’,用,渡運轉時’將該平均值直接作為進 運轉時,使得將利用f料喷射控制。而,在内燃機之定速 平均化後,將:相加平均處理得到之平均值再 計算值’用於燃料噴射:::平::值:接作為進氣壓之 平滑化處理」。:;=::匕檢測值進行「一次之 時理將巧對進氣壓感測器之檢=行,在 ;」,到之計算值作為進氣壓,各自用於:::;: 發明要解決 可是, 法,使平滑 轉時安定, 使平滑化係 轉時之響應 而,在 壓之計算值 該一般之平 實際上燃料 之課題 在以往之一 化係數變大 在過渡運轉 數變小時, 延遲,在定 該以往之公 在定速運轉 滑化處理改 室所取入之 般之利用「 時,進氣壓 時有發生響 進氣壓之計 速運轉時反 報之量測裝 時安定,過 善。可是, 進氣量之相 平滑化處理」之量測方 之叶算值雖然在定速運 應延遲之傾向。反之, 算值雖然改善在過渡運 而有不安定之傾向。 置,如圖13所示,進氣 渡運轉時之響應性也比 在計算值之精度上,和 關丨生不充分,在對於内 2097-4906-PF(N);Ahddub.p t d 第6頁 5524072097-4906-PF (N); Ahddub.p t d page 5 5. Explanation of the invention (2) Examples. That is, the intake pipe pressure measuring device is sampled during the driving cycle, and the intake pressure detected by the U :: device is determined at a predetermined value. On the other hand, the internal combustion broadcast value is added and averaged to calculate the calculated value of the average air pressure ', and the average value is used as the input directly during the operation, so that the fuel injection control will be used. After the constant speed of the internal combustion engine is averaged, the average value obtained by adding the average processing is used to calculate the value ′ for fuel injection ::: flat :: value: used as a smoothing process for the intake pressure ”. : ; = :: Detection value: “Check the intake air pressure sensor at once in a while.”, The calculated values are used as the intake air pressure, which are used for :::; However, the method stabilizes the smooth rotation and makes the smoothing response during the rotation, and the calculated value of the pressure is generally the same as the actual fuel problem. In the past, the coefficient has become larger, the number of transient operations has become smaller, and the delay has been delayed. When setting the conventional usage of the slippery process in the constant speed operation of the conventional modification room, when the intake air pressure occurs, there will be an alarm when the meter responds when the meter is running. However, the measured value of the "smoothing phase of the intake air volume" has a tendency to be delayed even at a constant speed. On the contrary, although the calculation value is improved during the transition period, it tends to be unstable. As shown in Figure 13, the responsiveness of the air intake is also less than the accuracy of the calculated value, and the correlation is not sufficient. In the range of 2097-4906-PF (N); Ahddub.p t d page 6 552407
五、發明說明(3) 燃機之負載之進氣壓計算值之關係,無法得到線性之特 性。 在此’本專利申請人發現,在四行程之往復式弓丨擎, 在進氣之脈動所伴隨之進氣壓之變動,其進氣壓之下限 值丄即在進氣行程之下死點附近之檢測值成為最佳的^映 了實際之進氣量之進氣壓,想到將其用作進氣壓之計算、 值,這已在特願20 00-29343 9之專利申請提案。即,提1 義 一種内燃機之進氣壓檢測方法,在内燃機運轉時,如圖工4 所示,計算伴隨脈動變化之進氣壓之AD值叩“之下限值 pm 1 〇後’將該下限值叩1 〇設為作為進氣壓之計算值之最終 之進氣壓PM。 對於此提案技術,本專利申請人再重複檢討之結果, 得知在運轉中之引擎發生逆吹(bl〇wing-back)等,如在圖 14之時刻tl、t2所示,在AD值pmad之波形混亂之情況,可 能將該混亂所引起之不規則之下限值誤檢測為進氣壓脈動 之下限值pm 1 〇。在發生了這種檢測錯誤之情況,將引擎之 吸入空氣量計算為比實際的多之值,隨著因過渡的計算燃 料喷射量,空氣燃料比貧乏化,可能產生令驅動性或排^ 放射惡化等不良。V. Description of the invention (3) The relationship between the calculated values of the intake pressure of the gas turbine load and the linear characteristics cannot be obtained. The applicant of this patent has found that in a four-stroke reciprocating bow engine, the variation of the intake pressure accompanying the pulsation of the intake air has a lower limit value of the intake pressure, i.e., near the dead point below the intake stroke The detected value becomes the best 进 气 which reflects the actual intake air pressure. It is thought to use it as the calculation and value of the intake air pressure. This has been proposed in Patent Application No. 20 00-29343 9. That is to say, a method for detecting the intake air pressure of an internal combustion engine is provided. When the internal combustion engine is running, as shown in Fig. 4, calculate the AD value of the intake air pressure accompanying the pulsation change "" lower limit value pm 1 0 "and then the lower limit. The value 叩 1 〇 is set as the final intake pressure PM which is the calculated value of the intake pressure. As for the proposed technology, the applicant of this patent repeats the results of the review and learns that the engine is running backblown (blwing-back ), Etc., as shown at times t1 and t2 in FIG. 14, in the case where the waveform of the AD value pmad is chaotic, the irregular lower limit value caused by the chaos may be erroneously detected as the lower limit value pm 1 of the intake pressure pulsation. 〇. In the case of such a detection error, the intake air volume of the engine is calculated to be more than the actual value. As the fuel injection volume is calculated due to the transition, the air-fuel ratio becomes leaner, which may cause driving or exhaustion. ^ Deterioration such as radiation deterioration.
因此,本發明鑑於上述之情況,其目的在於提供一種 内燃機之進氣壓檢測方法,在安定性和響應性優異,使得 可檢測和實際之進氣量之相關性高之進氣壓,防止引擎之 逆吹(blowing-back)等所引起之進氣壓之檢測錯誤。Therefore, in view of the above circumstances, the present invention aims to provide a method for detecting the intake pressure of an internal combustion engine, which is excellent in stability and responsiveness, makes it possible to detect an intake pressure with a high correlation with the actual intake amount, and prevents the engine from reversing Incorrect detection of intake air pressure caused by blowing-back etc.
2097-4906-PF(N);Ahddub.ptd 第7頁 5524072097-4906-PF (N); Ahddub.ptd Page 7 552407
解決課題之方式 為達成上述之目的,如申請專利範圍第1項之發明之 ^燃,之進氣壓檢測方法之主旨為,在内燃機之運轉時計 :進氣壓脈動之下限值*,和該下限值一起計算按照内燃 機之轉速之臨限值,下限值比該臨限值小時將下限值決 為進氣壓之計算值。 、 在内燃機運轉時’因在進氣發生脈動而進氣壓也伴隨 1動’為了内燃機之控制而直接使用該進氣壓時,其控制 變成不安定。在此,在進氣壓脈動之檢測值,已發現其下 限值成為最佳的反映實際之進氣量之進氣壓。 因此,若依據該發明之構造,因計算進氣壓脈動之下 限值後,將其下限值決定為進氣壓之計算值,儘管進氣壓 伴隨脈動,在進氣壓上也得到和進氣量相關之適當之值和 舉動。 又’因下限值比按照内燃機之轉速計算之臨限值小時 將其下限值決定為進氣壓之計算值,例如,因内燃機之逆 吹(blowing —13“1^等,進氣壓脈動之波形混亂,出現不規 則之下限值,也將該不規則之下限值除外,不會決定為進 氣壓之計算值。 為達成上述之目的,如申請專利範圍第2項之發明之 主旨為’在如申請專利範圍第1項之發明之内燃機之進氣 壓檢測方法,藉著自和該下限值一起計算之進氣壓脈動之 上限值減去既定之設定寬計算該臨限值;依照按照在該内 燃機之高負載定速運轉時之該轉速之進氣壓脈動之振幅預The way to solve the problem is to achieve the above-mentioned purpose. For example, the invention of the first invention of the scope of patent application, the main purpose of the intake pressure detection method is, when the internal combustion engine is running: the lower limit of the intake pressure pulsation *, and the lower limit The limit values are calculated together according to the threshold value of the speed of the internal combustion engine. If the lower limit value is smaller than the threshold value, the lower limit value is determined as the calculated value of the intake pressure. "When the internal combustion engine is running" Because the intake pressure fluctuates and the intake pressure is accompanied by 1 movement "When the intake pressure is directly used for the control of the internal combustion engine, the control becomes unstable. Here, in the detected value of the intake pressure pulsation, it has been found that its lower limit value becomes the best intake pressure that reflects the actual intake volume. Therefore, if the lower limit of the intake pressure pulsation is calculated according to the structure of the invention, the lower limit value is determined as the calculated value of the intake pressure. Although the intake pressure is accompanied by the pulsation, the intake pressure is also related to the intake amount. Appropriate values and actions. Also, because the lower limit value is smaller than the threshold value calculated according to the rotational speed of the internal combustion engine, the lower limit value is determined as the calculated value of the intake pressure. For example, due to the back blowing of the internal combustion engine (blowing — 13 "1 ^, etc., The waveform is confusing, and the irregular lower limit value appears. Except for the irregular lower limit value, it will not be determined as the calculated value of the intake pressure. In order to achieve the above purpose, for example, the main purpose of the invention in the second patent application scope is 'In the intake pressure detection method of the internal combustion engine of the invention as claimed in the first item of the patent application range, the threshold is calculated by subtracting a predetermined set width from the upper limit of the intake pressure pulsation calculated together with the lower limit; Prediction based on the amplitude of the intake pressure pulsation at the speed during the high load and constant speed operation of the internal combustion engine
2097-4906-PF(N);Ahddub.ptd 第8頁 552407 五、發明說明(5) 設該設定值。 若依據該發明之構造, 發明之作用以外,以進氣汽=了如申請專利範圍第1項之 上限值低設定寬之低值計^ f動之上限值為基準之只比該 該内燃機之高負载定速運轉時 值。在此,因依照按照在 幅預設該設定寬,得到適合和之該轉速之進氣壓脈動之振 之臨限值。 ϋ依據轉速而變之下限值比較 為達成上述之目的,如申& 主旨為,在如申請專利範圍第^專利範圍第3項之發明之 壓檢測方法,在該内燃機之過、、产員之發明之内燃機之進氣 速計算之臨限值大之第二臨限^運轉時,計算比按照該轉 限值小時將該下限值決定為^氣3 ’該下限值比該第二臨 在内燃機之過渡運轉時,因=^計算值。 運轉時的小,其下限值相對的變氣壓脈動之振幅比定速 之傾向。因此,若依據該發明之 L有下限值比臨限值大 圍第1項之發明之作用以外,在内造,除了如申請專利範 照比臨限值大之第二臨限值和下卩卩…機之過渡運轉時,參 第二臨限值小時,因將下限值決二值之比較,下限值比該 和過渡運轉時對應的檢測進氣壓’為進氣壓之計算值,可 為達成上述之目的,如申請 内燃機之進氣壓檢測裝置之主旨利範圍第4項之發明之 置’檢測内燃機之進氣壓;下限^:進氣壓檢測裝 壓檢測裝置之檢測值計算在該内拗=戽裴置,依照該進氣 之下限值;轉速檢測裝置,撿洲ς機運轉時之進氣壓脈動 、J s亥内燃機之轉速;臨限2097-4906-PF (N); Ahddub.ptd Page 8 552407 V. Description of the invention (5) Set the set value. If based on the structure of the invention, except for the effect of the invention, the intake steam = the low value of the upper limit of the lower limit of the upper limit of the scope of the application for patent application. High load constant speed operation value. Here, since the setting width is preset according to the width, the threshold value of the vibration of the intake pressure pulsation suitable for the rotation speed is obtained.比较 Comparing the lower limit value according to the speed to achieve the above purpose, such as applying & the main purpose is to apply the pressure detection method of the invention as described in the patent application No. ^ patent scope No. 3, Inventor's invention of the internal combustion engine, the threshold value of the calculation of the air intake speed is larger than the second threshold ^ When operating, the calculation ratio is smaller than the turning limit value and the lower limit value is determined to be ^ 3 3 Second, when the internal combustion engine is in transient operation, the calculated value is = ^. During operation, the amplitude of the variable air pressure pulsation relative to the lower limit value tends to be smaller than the constant speed. Therefore, if L according to the invention has the effect that the lower limit value is greater than the threshold value of the invention of item 1 within the scope of the invention, in addition to the second threshold value and the lower limit value,卩 卩 ... When the machine is in transient operation, the second threshold value is small. Because the lower limit value is compared with the second value, the lower limit value is equal to the detected intake air pressure corresponding to the transition time. In order to achieve the above-mentioned purpose, for example, applying the invention of the fourth invention of the air intake pressure detection device of the internal combustion engine to detect the intake pressure of the internal combustion engine; the lower limit ^: the detection value of the air intake pressure detection and installation pressure detection device is calculated in this拗 = 戽 Pei Zhi, according to the lower limit of the intake air; speed detection device, pick up the intake pressure pulsation when the engine is running, the speed of the J shai internal combustion engine; threshold
2097-4906-PF(N);Ahddub.ptd 552407 五、發明說明(β) 計算裝置,計算按照該所檢測之轉速之臨限值;以及進氣 壓決定裝置,該下限值比該臨限值小時將該下限值決定為 進氣壓之計算值。 若依據該發明之構造,在内燃機運轉時,依照進氣壓 檢測裝置之檢測值,利用下限值計算裝置計算進氣壓脈動 之下限值,而且利用臨限值計算裝置計算按照轉速檢、/則裝 置所檢測之轉速臨限值。而,下限值比該臨限值小時’因 進氣壓決定裝置將下限值決定為進氣壓之計算值,儘管進 氣壓伴隨脈動,在進氣壓上也得到和進氣量相關之適‘之 值和舉動。又,因内燃機之逆吹(blowing-back)等’進氣 壓脈動之波形混亂,出現不規則之下限值,也將該不規則 之下限值除外,不會決定為進氣壓之計算值。 為達成上述之目的,如申請專利範圍第5項之發明之 主旨為,在如申請專利範圍第4項之發明之内燃機之進氣 壓檢測裝置,包括:過渡運轉判斷裝置,判斷該内燃機之 過渡運轉;及第二臨限值計算裝置,計算係按照該内燃機 之過渡運轉之臨限值之比該臨限值大之第二臨限值;當判 斷為該内燃機之過渡運轉時,該進氣壓決定裝置選擇替代 該臨限值計算裝置所計算之臨限值之該第二臨限值計算裝 置所計算之第二臨限值,該下限值比該第二臨限值小時將 該下限值決定為進氣壓之計算值。 在内燃機之過渡運轉時,因進氣壓脈動之振幅比定速 運轉時的小,其下限值相對的變大,有下限值比臨限值大 之傾向。因此,若依據該發明之構造,除了如申請專利範2097-4906-PF (N); Ahddub.ptd 552407 V. Description of the invention (β) A calculation device calculates a threshold value based on the detected rotational speed; and an intake pressure determination device, the lower value is lower than the threshold value The lower limit value is determined as the calculated value of the intake pressure in hours. If according to the structure of the invention, when the internal combustion engine is running, according to the detection value of the intake pressure detection device, the lower limit value calculation device is used to calculate the lower limit value of the intake pressure pulsation, and the threshold value calculation device is used to calculate the Threshold of speed detected by the device. However, when the lower limit value is smaller than the threshold value, the lower limit value is determined by the intake pressure determination device as the calculated value of the intake pressure. Although the intake pressure is accompanied by a pulsation, the intake pressure is also appropriately related to the intake amount. Values and moves. In addition, due to the chaotic waveform of the intake air pressure pulsation such as the blow-back of the internal combustion engine, an irregular lower limit value appears. Except for the irregular lower limit value, it is not determined as the calculated intake pressure. In order to achieve the above purpose, the main purpose of the invention of the fifth scope of the patent application is that the intake pressure detection device of the internal combustion engine of the invention of the fourth scope of the patent application includes a transition operation judgment device to judge the transition operation of the internal combustion engine. ; And a second threshold value calculation device, which calculates a second threshold value based on the threshold value of the transition operation of the internal combustion engine that is greater than the threshold value; when it is judged that the transition operation of the internal combustion engine, the intake pressure is determined The device selects a second threshold value calculated by the second threshold value calculation device that replaces the threshold value calculated by the threshold value calculation device. The lower limit value is smaller than the second threshold value and sets the lower limit value. Determined as the calculated value of the intake pressure. During the transient operation of the internal combustion engine, the amplitude of the intake pressure pulsation is smaller than that of the constant-speed operation, and its lower limit value is relatively large, and the lower limit value tends to be larger than the threshold value. Therefore, if according to the structure of the invention,
2097-4906-PF(N);Ahddub.ptd 第10頁 552407 五、發明說明(7) 圍第4項之發明之作用以外 用過渡運轉判斷裝置判斷, 計算之比臨限值計算裝置所 和下限值之比較,下限值比 氣壓決定裝置將下限值決定 運轉時對應的檢測進氣壓。 為達成上述之目的’如 内燃機之控制裝置之主旨為 轉之控制對象之控制裝置, 該内燃機之進氣壓;轉速檢 速;下限值計算裝置,依照 算在該内燃機運轉時之進氣 裝置,計算按照該所檢測之 置’該下限值比該臨限值小 計算值;操作量計算裝置, 值和該轉速之檢測值計算用 量;以及控制裝置,藉著依 制對象,控制該控制量。 若依據該發明之構造, 。十^裝置自進氣壓檢测裝置 進氣壓脈動之下限值。一 算裝置計算按照轉速檢測裝 當下限值比臨限值小時,^ 定為進氣壓之計算值。 ,在内燃機之過渡運 參照利用第二臨轉寸,利 、咏 ^限值計算萝w 计鼻之臨限值大之- 、 該第二臨限值小時=臨限值 為進氣麼之叶丄:,因利用進 <。十异值,可和過渡 申:::2圍第6項之發明之 =使:控制關於内燃機之運 =置:壓檢剛裝置,檢測 /貝j哀置,檢測該内燃機之 該進氣壓檢測裝置之檢測值 壓脈動之下限值;自限值計ΐ 轉速之臨限值;進氣壓決定; 時將該下限值決定為進氣壓^ 依照該所決定之進氣壓之計算 以得到所要之控制量之操作"" 照該所計算之操作量操作該控 在内燃機運轉時,利用下限值 所檢測之進氣壓之檢測值計算 的,在運轉時,利用臨限值計 置檢测之轉速之臨限值。而, 用進氣壓決定裴置將下限值決 ,依照所決定之進氣壓之計算2097-4906-PF (N); Ahddub.ptd Page 10 552407 V. Explanation of the invention (7) Use the transient operation judgment device to judge the calculation of the ratio of the threshold value calculation device in addition to the effect of the invention of item 4 Comparison of the limits. The lower limit ratio is determined by the air pressure determining device, which determines the lower limit value of the corresponding intake air pressure during operation. In order to achieve the above-mentioned purpose, such as the control device of the internal combustion engine, the main purpose is the control device of the control object, the intake pressure of the internal combustion engine; the speed detection; the lower limit calculation device, according to the intake device calculated when the internal combustion engine is operating, Calculate the calculated value according to the detected setting; the lower limit value is smaller than the threshold value; the operation amount calculation device, the value and the detection value of the rotation speed calculation amount; and the control device controls the control amount by depending on the object of control . If constructed according to the invention,. Ten devices from the intake air pressure detection device Lower limit of intake pressure pulsation. A calculation device calculates that when the lower limit value is smaller than the threshold value according to the speed detection device, ^ is set to the calculated value of the intake pressure. In the transition of the internal combustion engine, reference is made to the calculation of the second threshold value, the limit value of the profit, and the value of the threshold. The threshold value of the nose is greater than the threshold value of the second threshold value.丄:, due to the use of <. Ten different values can be applied to the transition: 2: The invention of the 6th item = make: control the operation of the internal combustion engine = set: pressure detection device, detection / detection, detection of the intake pressure of the internal combustion engine The lower limit value of the detected value pressure pulsation of the device; the self-limit value ΐ the threshold value of the rotational speed; the intake pressure is determined; the lower limit value is determined as the intake pressure ^ according to the calculation of the determined intake pressure to obtain the desired Operation of control amount " " Operate according to the calculated operation amount. When the internal combustion engine is running, the control is calculated using the detection value of the detected intake air pressure at the lower limit value. During operation, the threshold value is set to detect Threshold of speed. However, the lower limit value is determined by the intake pressure, and the calculation is based on the determined intake pressure.
552407 五、發明說明(8) 值和轉速之檢測值,利用操作 ' 要之控制量之操作量,利用控制裝算用以得到所 操作控制對象,控制控制量。 错著依照其操作量 因此,將進氣壓脈動之混亂所弓丨 除外,不會決定為進氣壓之計筲值之之不規則之下限值 動之下限值作為進氣壓之計算^取又=將適當之進氣壓脈 而,儘管進氣壓伴隨脈動,抨制旦:制對象之控制。因 照進氣壓之舉動適當的控制^制對象y變成不安定值,按 發明之實施形態 以下參照圖面詳細說明本發 方法及使用該檢測方法之進氣壓檢3 =機之進氣壓檢蜊 壓檢測裝置之内燃機之控制裝置具體進氣 圖1係表不本實施形態之引擎车 貝β 7〜、 ^ ^ ^ ^ Ρ| ^ ^ ^ , 手系統之概略構造圖。車 輛所^載之引擎糸統包括貯存燃料之概 内藏之燃料果2排出燃料槽1所貯存=2槽1。/、,4槽1所 往復式單氣缸引擎3設置燃料噴射存門,:料。在係内燃機之 2“排出之燃料、經㈣料通路5供給喷射器4。所供給之燃^ ,者”器4動作向進氣通路6噴射。經由空氣渡清器自外 邛將空乳取入進氣通路6。進氣通路6所取入之空氣和自噴 射器4所噴射之燃料形成可燃混合氣後被吸入燃料室8。、 在進氣通路6設置利用既定之加速裝置(省略圖示)操 作之節流閥9。藉著節流閥9開閉,調整自進氣通路6吸入 燃料至8之空氣ι(進氣量)。在進氣通路6設置旁通通路 2097-4906-PF(N);Ahddub.ptd 第12頁 552407 五、發明說明(9) 1 0,繞過節流閥9。在旁通通路丨〇設置空轉轉速栌制閥 · (ISC閥)11。ISC閥11係在空轉時,即節流閥9全^時為了 調整單氣缸引擎3之空轉轉速而令動作的。 在燃料室8所設置之火星塞12接受自點火線圈13輸出 - 之點火信號後進行點火動作。兩零件丨2、丨3構成用以向供 給燃料至8之可燃混合軋點火之點火裝置。燃料室8所吸入 之可燃混合氣藉著火星塞1 2之點火動作爆炸•燃燒。燃燒 後之排氣自燃料室8經由排氣通路丨4排向外部/在排氣通 路1 4流動之排氣利用三元觸媒丨5淨化。然後,伴隨在燃料 室8之可燃混合氣之燃燒,藉著活塞丨6運動而曲柄軸丨7轉 春 動’在引擎3得到令車輛行駛之驅動。 在車輛设置用以令引擎3起動之點火開關丨8。在車輛 設置掌官引擎3之各種控制之電子控制裝置(ECU)2〇。作為 車輛用電源之電池19經由點火開關18 *ECU2〇連接。藉著 點火開關18導通’自電池19供給ECU20電力。 在引擎3所设置之各種感測器2 1、2 2、2 3、2 4係用以 檢測關於引擎3之運轉狀態之各種運轉參數的,各自和 ECU20連接。即,在進氣通路6所設置之係進氣壓檢測裝置 之進氣壓感測器2 1檢測在比節流閥9下游側之進氣通路6之 進氣壓pm後,輸出按照該檢測值之電氣信號。在引擎3所 _ 设置之水溫感測器2 2檢測在引擎3之内部流動之冷卻水之 溫度(冷卻水溫)THW後,輸出按照該檢測值之電氣信號。 在引擎3所設置之係轉速檢測裝置之轉速感測器23檢測曲 柄軸17之轉速(引擎轉速)NE後,輸出按照該檢測值之電氣552407 V. Description of the invention (8) The measured value of the value and the rotational speed are obtained by using the operation amount of the control amount required by the operation and using the control device to obtain the control object of the operation and the control amount. Wrongly according to its operating volume, except for the chaos of the intake pressure pulsation, it will not be determined as the irregular lower limit value of the intake pressure value. The lower limit value is used as the calculation of the intake pressure. = Pulse the appropriate intake pressure, although the intake pressure is accompanied by the pulsation, attack the control: control of the target. Due to proper control of the intake air pressure, the control object y becomes unstable. According to the embodiment of the invention, the method of the present invention and the intake air pressure check using the detection method will be described in detail with reference to the drawings below. The specific intake of the control device of the internal combustion engine of the detection device. Figure 1 is a schematic diagram showing the structure of the engine car beta 7 ~, ^ ^ ^ ^ P | ^ ^ ^ of the present embodiment. The engine system contained in the vehicle includes the fuel storage. The built-in fuel fruit 2 is discharged from the fuel tank 1 and stored = 2 tank 1. / 、, 4 tanks, 1 reciprocating single-cylinder engine 3 is provided with fuel injection storage door: feed. In the internal combustion engine 2 "the discharged fuel is supplied to the injector 4 through the fuel passage 5. The supplied fuel ^" is operated to inject the fuel into the intake passage 6. The air milk is taken into the air intake passage 6 from the outside via an air cleaner. The air taken in the intake passage 6 and the fuel injected from the injector 4 form a combustible gas mixture and are drawn into the fuel chamber 8. A throttle valve 9 which is operated by a predetermined acceleration device (not shown) is provided in the intake passage 6. The throttle valve 9 is opened and closed to adjust the air (intake amount) of the fuel sucked in from the intake passage 6 to 8. A bypass passage 2097-4906-PF (N); Ahddub.ptd page 12 552407 is provided in the intake passage 6 5. Description of the invention (9) 1 0, bypass the throttle valve 9. An idle speed control valve (ISC valve) 11 is provided in the bypass path. The ISC valve 11 is actuated during idling, that is, the throttle valve 9 is full time to adjust the idling speed of the single-cylinder engine 3. The spark plug 12 provided in the fuel chamber 8 receives an ignition signal output from the ignition coil 13 and performs an ignition operation. The two parts 丨 2, 丨 3 constitute an ignition device for igniting the combustible mixed rolling supplied with fuel to 8. The combustible mixture inhaled by the fuel chamber 8 is exploded and burned by the ignition action of the spark plug 12. The exhaust gas after combustion is discharged from the fuel chamber 8 to the outside via the exhaust passage 丨 4 / the exhaust gas flowing through the exhaust passage 14 is purified by a ternary catalyst 5. Then, along with the combustion of the combustible mixture in the fuel chamber 8, the crank shaft 丨 7 rotates by the movement of the piston 丨 6 and the spring ′ is driven at the engine 3 to drive the vehicle. The vehicle is provided with an ignition switch 8 for starting the engine 3. The vehicle is provided with an electronic control unit (ECU) 20 for various controls of the engine 3. The battery 19 as a vehicle power source is connected via an ignition switch 18 * ECU20. Power is supplied from the battery 19 to the ECU 20 by turning on the ignition switch 18 '. Various sensors 2 1, 2, 2, 3, 2 and 4 installed in the engine 3 are used to detect various operating parameters related to the operating state of the engine 3, and are connected to the ECU 20 respectively. That is, the intake pressure sensor 21 of the intake pressure detection device provided in the intake passage 6 detects the intake pressure pm of the intake passage 6 on the downstream side of the throttle valve 9 and outputs an electric signal according to the detected value. signal. After the water temperature sensor 2 2 installed in the engine 3 detects the temperature (cooling water temperature) THW of the cooling water flowing inside the engine 3, it outputs an electrical signal according to the detected value. After the rotational speed sensor 23 of the rotational speed detecting device provided in the engine 3 detects the rotational speed (engine rotational speed) NE of the crank shaft 17, it outputs an electrical signal according to the detected value.
552407 五、發明說明(10) :在排氣通路14所設置之氧氣感測器24檢測向排氣通 出之排氣中之氧氣濃度(輸出電壓)0χ後,輸出按照 〇Sx欢測值之電氣信號。該氧氣感測器24用以得到供給引擎 之燃料室8之可燃混合氣之空氣燃料比Α/{?。 Ψ夕^ ί貝^形悲,ECU2〇輸入上述之各種感測器21〜24輸 = 。職〇為了依照這些輸入信號各自執行進 批^:: 燃料喷射控制以及點火時期控制等,各自 K = f '喷射仏⑼闕11以及點火線圈U等。在 值二^ ’ ECU2〇構成本發明之下限值計算裝置、臨限 = 弊;氣壓決定裝置、過渡運轉判斷裝置、第二 =计异凌,、操作量計算裝置以及控制裝置。 檢測之=顏Ϊ軋壓檢測控制係用以依照進氣壓感測器21所 算值之控制。:Ϊ到排除了進氣脈動之影響之進氣壓之計 噴射器Γ之揪料曰射控制係按照引擎3之運轉狀態控制 著按照引擎射時序。點火時期控制係藉 12之點火時_。 ⑮控^點火線圈13 ’控制各火星塞 m \lZ2rt^ I ΐ 4 S ^ £(CPU) 入電路以及外部(RAM)、備用RAM、外部輸 接cpu、_、RAM和借電=Λ4Μ °ECU20構成利用匯流排等連 電路等而成之卜部輸人電路以及外部輸出 種控制之既定==路。_預先記憶關於引擎3之各 備用MM儲存預先?制卜程式。RAM暫時記憶CPU之運算結果。 預先圮k之資料。CPU依照經由輸入電路輸入552407 V. Description of the invention (10): After the oxygen sensor 24 provided in the exhaust passage 14 detects the oxygen concentration (output voltage) in the exhaust gas to the exhaust gas 0x, the output will be based on the measured value of 0Sx. Electrical signal. The oxygen sensor 24 is used to obtain the air-fuel ratio A / {? Of the combustible mixture supplied to the fuel chamber 8 of the engine. After the night, the ECU 20 inputs various sensors 21 ~ 24 as described above. In order to execute batches according to these input signals ^ :: fuel injection control and ignition timing control, etc., K = f 'injection 仏 ⑼ 阙 11 and ignition coil U, etc., respectively. The value ^ 'ECU20 constitutes the lower limit calculation device of the present invention, the threshold = disadvantages; the air pressure determination device, the transition operation determination device, the second = counter Ling, the operation amount calculation device, and the control device. Detecting = Yan Huan rolling detection control is used to control according to the value calculated by the intake pressure sensor 21. : Injection pressure is calculated from the influence of the intake pulsation. The injection control of the injector Γ is controlled according to the operating state of the engine 3 and according to the engine injection timing. The ignition timing control is based on the ignition timing of 12. Control ^ Ignition coil 13 'Control each Mars plug m \ lZ2rt ^ I ΐ 4 S ^ £ (CPU) input circuit and external (RAM), backup RAM, external input cpu, _, RAM and borrowing = Λ4Μ ° ECU20 The predetermined input circuit of the Bubu input circuit and external output control, which are formed by connecting circuits such as bus bars, etc., are established. _Remember in advance each spare MM of the engine 3 to store a pre-production formula. The RAM temporarily stores the operation results of the CPU.圮 k information in advance. CPU input via input circuit
552407 五、發明說明(11) 之各種感測|§ 2 1〜2 4之檢測信號,按照既定之控制程式執 行上述之各種控制等。 其-人,說明E C U 2 0執行之各種控制之中之進氣壓檢測 控制所需之處理内容。在圖2表示進氣壓檢測控制程式之 流程圖。每隔既定期間週期性執行圖2所示之常式。在本 實施形態,ECU20按照「lms」之週期執行此常式。 首先,在步驟1 0 0,ECU20依照轉速感測器23之檢測值 讀入引擎轉速NE之值。 接著’在步驟1 0 1,ECU2 0依照進氣壓感測器2 1所檢測 之進氣壓pm讀入這次之AD值pmad。 然後,在步驟102,ECU20判斷這次之AE^pmad是否大 於上次之AD值pmado。在此判斷結果是否定之情況,設進 氣壓pm未上升’在步驟118 ’ECU20將這次之壓力上升旗標 XPMUP設為「0」後,將處理移往步驟11 9。壓力上升旗標 XPMUP在進氣壓上升之情況設為「1」,在除此以外之情況 設為「0」。 在步驟119,ECU20判斷壓力上升旗標xpmup是否是 「1」。在該判斷結果係否定之情況,設進氣壓pm接著上 次下降,E C U 2 0將處理移往步驟11 4。在該判斷結果係肯定 之情況,設進氣壓pm自上升轉為下降,在步驟120,ECU20 將將上次之AD值pmado設為上限值pmhi後,將處理移往步 驟114。552407 V. Various kinds of sensing of the description of the invention (11) | The detection signals of § 2 1 ~ 2 4 are executed according to the predetermined control program. The person-to-person describes the processing content required for the intake pressure detection control among the various controls performed by E C U 2 0. The flowchart of the intake pressure detection control routine is shown in FIG. The routine shown in FIG. 2 is executed periodically every predetermined period. In this embodiment, the ECU 20 executes this routine at a cycle of "lms". First, in step 100, the ECU 20 reads the value of the engine speed NE according to the detection value of the speed sensor 23. Next, at step 101, the ECU 20 reads the AD value pmad this time according to the intake pressure pm detected by the intake pressure sensor 21. Then, in step 102, the ECU 20 determines whether AE ^ pmad this time is greater than the previous AD value pmado. In this case, if the judgment result is negative, it is assumed that the intake air pressure pm has not risen 'At step 118, the ECU 20 sets the pressure rise flag XPMUP to "0" this time, and then proceeds to step 119. The pressure increase flag XPMUP is set to "1" when the intake pressure is increased, and set to "0" otherwise. In step 119, the ECU 20 determines whether the pressure rising flag xpmup is "1". In the case where the judgment result is negative, it is assumed that the intake air pressure pm then decreases last time, and E C U 2 0 moves the process to step 11 4. In the case where the determination result is affirmative, it is assumed that the intake air pressure pm is changed from rising to falling. In step 120, the ECU 20 sets the previous AD value pmado to the upper limit value pmhi, and then proceeds to step 114.
而,在步驟1 0 2之判斷結果係肯定之情況,設進氣壓 pm上升,在步驟103,ECU20將這次之壓力上升旗標xpMUPHowever, if the judgment result in step 102 is affirmative, it is assumed that the intake air pressure pm is increased. In step 103, the ECU 20 sets the pressure rise flag xpMUP this time.
2097-4906-PF(N);Ahddub.p t d 第15頁 5524072097-4906-PF (N); Ahddub.p t d p. 15 552407
五、發明說明(12) 設為「1」。 XPMUPO是否是「〇」。 氣壓pm接著上次上升, 斷結果係肯定之情況, 理移往步驟1 0 5。 接著,在步驟104,ECU20判斷上次之壓力上升旗標 。在該判斷結果係否定之情況,設進 ’ E C U 2 0將處理移往步驟11 4。在該列 ‘,設進氣壓pm自下降轉為上升,將處 在步驟1 05,ECU20判斷減速判定旗標XGENS0KU是否是 「〇」。減速判定旗標XGENS0KU在引擎3減速運轉時設為 「1」,在除此以外之情況設為「〇」。在本實施形態, ECU20依照本常式所得到之後述之最終之進氣壓pM值之變 化和轉速感測器2 3之檢測值之變化等判斷引擎3是否處於 減速運轉狀態’按照其判斷結果設定減速判定旗標 ' XGENSOKU。在此,在該判斷結果係否定之情況,設為是引 擎3之減速運轉時,ECU20在步驟1〇9將為減速時用而預設 之既定值κρι設為設定寬pmw。該設定寬pmw係為了計算後 述之臨限值pthre而使用之參數。該既定值κρι可設為例如 「1·0(mmHg)」。 而,在步驟1〇5之判斷結果係肯定之情況,設為不是 引擎3之減速運轉時,ECU20將處理移往步驟1〇6。然後, 在步驟106,ECU20判斷加速判定旗標XKAS〇KU是否是 「〇」。加速判定旗標XKASOKU在引擎3加速運轉時設為 「1」,在除此以外之情況設為r Q」。在本實施形態, ECU2 0依照本常式所得到之後述之最終之進氣壓"值之變 化和轉速感測器2 3之檢測值之變化等判斷引擎3是否處於5. Description of the invention (12) Set to "1". Is XPMUPO "0"? The air pressure pm then rises last time, and the result is affirmative. The process moves to step 105. Next, in step 104, the ECU 20 determines the last pressure rising flag. In the case where the judgment result is negative, it is set to 'E C U 2 0 and the process proceeds to step 11 4. In this column ′, it is assumed that the intake air pressure pm changes from falling to rising, and it will be in step 105, and the ECU 20 judges whether the deceleration determination flag XGENS0KU is "0". The deceleration determination flag XGENS0KU is set to "1" when the engine 3 is decelerated, and otherwise set to "0". In this embodiment, the ECU 20 determines whether the engine 3 is in a decelerating operation state such as the final change in the intake air pressure pM value and the change in the detection value of the rotational speed sensor 23 according to this routine. Slowdown judgment flag 'XGENSOKU. Here, in a case where the determination result is negative, it is assumed that the deceleration operation of the engine 3 is performed, and the ECU 20 sets the preset value κρm for the deceleration to the setting width pmw in step 109. The setting width pmw is a parameter used for calculating a threshold value pthre described later. This predetermined value κρι can be set to, for example, "1.0 (mmHg)". If the result of the determination in step 105 is affirmative, and if it is determined that the engine 3 is not decelerating, the ECU 20 moves the processing to step 106. Then, in step 106, the ECU 20 determines whether the acceleration determination flag XKASOKU is "0". The acceleration determination flag XKASOKU is set to "1" when the engine 3 is accelerated, and otherwise set to r Q ". In this embodiment, the ECU 20 determines whether the engine 3 is in the final air pressure " value change and the change in the detection value of the rotational speed sensor 23, which are obtained later according to this routine.
552407 五、發明說明(13) 加速運轉狀態,按照其判斷結果設定加速判定旗標 XKAS0KU。在此,在該判斷結果係否定之情況,設為是引 擎3之加速運轉時,ECU20在步驟1〇8將為加速時用而預設 之既定值KP2設為設定寬pmw。該設定寬pmw係為了計算後 述之臨限值pthre而使用之參數。該既定值KP2可設為比減 速日寸之既定值KP1大之例如「3.0(minHg)」。 而,在步驟1 0 6之判斷結果係肯定之情況,設為是引 擎3之定速運轉時,ECU20將處理移往步驟107。在步驟 107 ’ECU20藉著參照既定之圖計算設定寬pmw。即,ECU20 如圖3所示,藉著參照以引擎轉速NE和設定寬pmw為參數所 預設之資料圖,計算按照這次所讀入之引擎轉速NE之值之 設定寬pmw。在該資料圖之設定寬pmw係依照按照引擎3在 高負載定速運轉時之引擎轉速⑽之進氣壓脈動之振幅預設 的。即,在將節流閥9設為全開之rw〇T(wide Open552407 V. Description of the invention (13) Acceleration running state, set acceleration judgment flag XKAS0KU according to its judgment result. Here, in a case where the determination result is negative, when the acceleration operation of the engine 3 is set, the ECU 20 sets the predetermined value KP2 preset for acceleration at step 108 as the setting width pmw. The setting width pmw is a parameter used for calculating a threshold value pthre described later. The predetermined value KP2 can be set to be larger than the predetermined value KP1 of the deceleration day, for example, "3.0 (minHg)". On the other hand, if the result of the determination in step 106 is affirmative, and if it is set to the constant speed operation of the engine 3, the ECU 20 moves the processing to step 107. At step 107 ', the ECU 20 calculates the set width pmw by referring to the predetermined map. That is, as shown in FIG. 3, the ECU 20 calculates the setting width pmw according to the value of the engine speed NE read this time by referring to the data map preset with the engine speed NE and the setting width pmw as parameters. The setting width pmw in the data chart is preset according to the amplitude of the intake pressure pulsation according to the engine speed at the time of high load and constant speed operation of the engine 3. That is, when the throttle valve 9 is set to rw〇T (wide open
Throttle)」之定速運轉時,如圖4(a)〜(c)所示,進氣壓 pm之振幅按照引擎轉速NE之差異而異。在圖4(a)〜(c)表示 在「lOOOrpm」、「500rpm」以及「2〇〇〇rpm」之情況^振 幅之差異。因此,在本實施形態,依照在該在高負 運轉時因引擎轉速NE之值而異之進氣壓叩之振幅之大小設 定設定寬pmw。 口 狄目乂驟1〇7〜109移往之步驟11(]。^112〇_ 自上^所计异之進氣壓脈動之上限值_hi減去該所 設定寬pmw,計算臨限值pthre。 # 接著,在纟驟⑴,ECU20判斷自下降轉為上升之進桌Throttle) ", as shown in Figs. 4 (a) to (c), the amplitude of the intake pressure pm varies according to the difference in engine speed NE. Figs. 4 (a) to (c) show the difference between the amplitudes at "1000 rpm", "500 rpm", and "2000 rpm". Therefore, in this embodiment, the setting width pmw is set in accordance with the magnitude of the amplitude of the intake pressure 叩, which varies depending on the value of the engine speed NE during high-negative operation. Ordice step 1107 ~ 109 moved to step 11 (). ^ 112〇_ The upper limit of the intake pressure pulsation different from the above ^ _hi minus the set width pmw to calculate the threshold pthre. # Then, in step ECU20, the ECU20 judges that the table turns from falling to rising and enters the table.
552407 五、發明說明(14) 壓pm之上次之AD值pmado是否大於臨限值pthre。在該判斷 結果係肯定之情況,ECU2 0直接將處理移往步驟丨丨4。在該 判斷結果係否定之情況,在步驟11 2,ECU20將上次之AD值 pmado設為進氣壓pm之下限值pm 1 〇。即,從自伴隨脈動之 進氣壓pm連續得到之多個AD值pmad之中計算位於脈動之谷 之下限值pmlo。 接著’在步驟11 3 ’ E C U 2 0將這次所得到之下限值p m 1 〇 設為最後應求得之進氣壓PM。 然後,在自步驟119、120、104、111、113移往之步 驟114 ’ ECU20將這次之AD值pmad設為上次之AD值pmado。 接耆,在步驟115,ECU20判斷這次之壓力上斗後# 是否是。在該判斷結果係肯定之情土 =驟 116,ECU20將上次之壓力上升旗標χρΜυρ〇設為「丨」。在 該判斷結果係否定之情況,在步驟117,ECU2〇將上次之壓 力上升旗標XPMUP0設為「〇」。 專待下一運552407 V. Description of the invention (14) Whether the last AD value pmado of pressing pm is greater than the threshold pthre. In the case where the judgment result is affirmative, ECU20 directly shifts the processing to step 丨 4. In a case where the determination result is negative, in step 112, the ECU 20 sets the last AD value pmado to the lower limit value pm 1 of the intake air pressure pm. That is, the lower limit value pmlo of the valley of the pulsation is calculated from a plurality of AD values pmad obtained continuously from the intake air pressure pm accompanying the pulsation. Next, at step 11 3 'E C U 2 0, the lower limit value p m 1 〇 obtained this time is set to the final intake pressure PM required. Then, in step 114 ', which is moved from steps 119, 120, 104, 111, and 113, the ECU 20 sets the AD value pmad this time to the previous AD value pmado. Then, in step 115, the ECU 20 judges whether or not the pressure is ##. In the case where the judgment result is positive = step 116, the ECU 20 sets the last pressure rising flag χρΜυρ〇 to "丨". If the result of this determination is negative, in step 117, the ECU 20 sets the last pressure increase flag XPPMUP0 to "0". Dedicated to the next transport
於是,ECU20 —度完成本常式之處理後 算週期之時序,再進行自步驟丨〇 〇之處理。 在該常式,使得在引擎3運轉時計算進氣壓pm之脈動 之下限值pmlo後’將該下限值pml〇決定為作為Then, the ECU 20 completes the timing of the calculation cycle after completing the processing of this routine, and then performs the processing from step 丨 00. In this routine, after the pulsation of the intake pressure pm is calculated when the engine 3 is running, the lower limit value pmlo is determined as the lower limit value pml.
控制使用之進氣壓pm之計算值之最終之進氣壓pM。因而 如圖5所不’對於伴隨脈動之進氣細,比較取樣 ,AD iPmad〇和這次之值叩ad後,判斷進氣壓pm之下降 之轉換。然後,將在自上升往下降之轉二之士Control the final intake pressure pM of the calculated value of the intake pressure pm used. Therefore, as shown in Fig. 5, for the intake air with pulsation, compare the sampling, AD iPmad0 and the current value 叩 ad, to determine the transition of the decrease in intake air pressure pm. Then, in the transition from rising to falling
2097-4906-PF(N);Ahddub.ptd 第18頁 552407 五、發明說明(15) pmado計算為上限值pmh i,將在自下降往上升之轉換時之 上次之AD值pmado計算為下限值pml〇後,使得將該下限值 pmlo決定為最終之進氣壓pm之值。2097-4906-PF (N); Ahddub.ptd Page 18 552407 V. Description of the invention (15) pmado is calculated as the upper limit value pmh i, and the last AD value pmado when the conversion from falling to rising is calculated as After the lower limit value pml0, the lower limit value pmlo is determined to be the final intake pressure pm.
在此,在該常式,如圖6所示,自上限值pmhi和設定 寬pmw求臨限值pthre後,當下限值pmi〇比該臨限值pthre 小時’使得將該下限值pm 1 〇決定為係進氣壓pm之計算值之 最終之進氣壓PM之值。因此,如在圖6以圓包圍所示,在 AD值pmad出現不規則之下限值,也在該不規則之下限值大 於臨限值pthre之情況,自下限值pmlo之設定將該不規則 之下限值除外,不會決定為最終之進氣壓PM。 在本實施形態之引擎系統,使用如上述所示檢測之最 終之進氣壓PM進行燃料喷射控制。因此,接著說明該燃料 喷射控制之處理内容。在圖7表示燃料喷射控制之程式之 *程圖。E C U 2 0母隔既定期間週期性的執行該常式。 首先,在步驟200,ECU20依照轉速感測器23之檢測值 讀入引擎轉速NE之值。 在步驟210,ECU20讀入最終之進氣壓pM。即,讀入伴 隨脈動之進氣壓叩之下限值pml0,作為最終之進氣^”之 值0Here, in this routine, as shown in FIG. 6, after the threshold value pthre is obtained from the upper limit value pmhi and the set width pmw, when the lower limit value pmi0 is smaller than the threshold value pthre ', the lower limit value pm is made. 10 is determined as the final intake pressure PM which is the calculated value of the intake pressure pm. Therefore, as shown by a circled circle in FIG. 6, an irregular lower limit value appears in the AD value pmad, and also in the case where the irregular lower limit value is greater than a threshold value pthre. Except for the irregular lower limit, it will not be determined as the final intake pressure PM. In the engine system of this embodiment, fuel injection control is performed using the final intake pressure PM detected as described above. Therefore, the processing content of the fuel injection control will be described next. Fig. 7 shows a flowchart of a fuel injection control routine. E C U 2 0 This routine is executed periodically during a predetermined period of time. First, in step 200, the ECU 20 reads the value of the engine speed NE according to the detection value of the speed sensor 23. In step 210, the ECU 20 reads the final intake pressure pM. That is, the lower limit value pml0 of the intake air pressure accompanied by the pulsation is read as the final intake air value 0 "
产在步驟220,ECU20依照所讀入之引擎轉速㈣之值和 氣壓PM之值計算基本燃料噴射量TAUBSE。ECU2〇藉 e 預先決定之函數資料(喷射量圖)計算該基本燃9 = TAUBSE。在該函數資料自進氣壓pM之值和引擎速二 決定引擎3之燃料室8吸入之進氣量|,按照該進氣量決Produced in step 220, the ECU 20 calculates the basic fuel injection amount TAUBSE based on the read value of the engine speed ㈣ and the value of the air pressure PM. ECU20 uses the function data (injection amount map) determined in advance by e to calculate the basic fuel 9 = TAUBSE. In this function data, the value of the intake air pressure pM and the engine speed determine the intake air volume |
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五、發明說明(16) 基本燃料喷射量TAUBSE。 在步驟2 3 0 ’ E C U 2 0依照水溫感測器2 2之檢測值讀入冷 卻水溫THW之值。然後,在步驟240,ECU20依照所讀入之 冷卻水溫THW之值,按照引擎3之暖機狀態計算用以修正基 本燃料喷射量TAUBSE之暖機修正係數KTHW。 在步驟250 ’ECU20讀入用以修正供給燃料室8之空氣 和燃料之可燃混合氣之空氣燃料比A / ρ之空氣燃料比修正 係數FAF之值。該空氣燃料比修正係數FAF係依昭自 測器24之檢測值讀入之氧氣濃度〇χ之值計算的: ”感 在步驟260,ECU20藉著依照暖機修正係數以㈣及* 燃料比修正係數FAF等修正如上述所計算之基本燃料喷 量TAUBSE ’計算最終之燃料噴射量TAU之值。 、 然後,在步驟270,ECU20藉著依照所計算之最故 料1射量TAU之值控制噴射器4,控制自噴射器4噴射之燃·、、、 料 ΐ 。 “、、 在本實施形態之引擎系統,使用如上述檢 進J壓ΡΜ進行點火時期控制。因&,說明該 ; 之處理内I。圖8表示點火時期控制之程式之 』控制 ECU20每隔既定期間週期性執行該常式。 回 首先,在步驟300,ECU2〇依照轉速感 讀入引擎轉速NE之值。 之檢測值 在步驟310,ECU20讀入最終之進氣壓ρΜ之值。^ =脈動之進氣壓⑽之下限值pral。,作為最終之進。V. Description of the invention (16) Basic fuel injection amount TAUBSE. In step 2 3 0 'E C U 2 0, the value of the cooling water temperature THW is read in accordance with the detection value of the water temperature sensor 22. Then, in step 240, the ECU 20 calculates a warm-up correction coefficient KTHW for correcting the basic fuel injection amount TAUBSE according to the read-in value of the cooling water temperature THW and according to the warm-up state of the engine 3. At step 250 ', the ECU 20 reads the value of the air-fuel ratio correction coefficient FAF for correcting the air-fuel ratio A / ρ of the combustible mixture of the air supplied to the fuel chamber 8 and the fuel. The air-fuel ratio correction factor FAF is calculated based on the value of the oxygen concentration 0χ read from the detection value of the Zhao self-tester 24: "At step 260, the ECU 20 corrects by using the warm-up correction factor to increase the fuel ratio with * The coefficient FAF and the like correct the basic fuel injection amount TAUBSE calculated as described above to calculate the value of the final fuel injection amount TAU. Then, in step 270, the ECU 20 controls the injection in accordance with the calculated value of the most anticipated injection amount TAU. The injector 4 controls the fuel injection from the injector 4. "," In the engine system of this embodiment, the ignition timing control is performed using the J pressure PM as described above. Because of &, explain the processing of I; FIG. 8 shows the routine of the ignition timing control. The control ECU 20 executes this routine periodically at predetermined intervals. First, at step 300, the ECU 20 reads the value of the engine speed NE in accordance with the speed sense. Detection value In step 310, the ECU 20 reads the value of the final intake pressure pM. ^ = Lower limit pral of pulsating intake pressure ⑽. As the final step.
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a…在步驟320,ECU20依照所讀入之引擎轉速NE之值和進 乳f PM之值計算基本點火時期ITBSE。ECU20藉著參照預先 決定之函數資料(點火時期控圖)計算該基本點火時期、 ITBjE。在該函數資料自進氣MpM之值和引擎轉速犯之值 决疋引擎3之燃料室8吸入之進氣量後,按照該進氣量決定 基本點火時期ITBSE。 、 广在步驟330,ECU20依照水溫感測器22之檢測值讀入 部水溫THW之值。然後,在步驟34〇,ECU2〇依照所讀入之7a ... In step 320, the ECU 20 calculates the basic ignition timing ITBSE based on the read value of the engine speed NE and the value of the feeding fPM. The ECU 20 calculates the basic ignition timing and ITBjE by referring to predetermined function data (ignition timing control map). After the function data is determined from the value of the intake air MpM and the value of the engine speed, the amount of intake air taken in by the fuel chamber 8 of the engine 3 is determined, and the basic ignition timing ITBSE is determined according to the intake air amount. In step 330, the ECU 20 reads the value of the water temperature THW according to the detection value of the water temperature sensor 22. Then, in step 34, the ECU 20 reads
冷部水溫THW之值,按照引擎3之暖機狀態計算用以修正基 本點火時期ITBSE之暖機修正係數κι。 土 、▲,步驟350,ECU20藉著依照暖機修正係數以修正如上 述计算之基本點火時期IT B S E,計算最終點火時期I τ。 士然後,在步驟360,ECU20藉著依照所計算之最終點火 時期it之值控制點火線圈13,控制火星塞12之點火時期。 士在以上所說明之本實施形態之引擎系統,在引擎3運 轉π在進氣通路6發生進氣之脈動,進氣壓感測器2 1所 檢測之進氣壓pm伴隨脈動。因而,將伴隨脈動之進氣壓叩 直接用作執行引擎3之各種控制之運轉參數之一時, 控制變成不穩定。The value of the cold water temperature THW is calculated according to the warm-up state of the engine 3 to modify the warm-up correction coefficient κι of the ITBSE during the basic ignition period. At step 350, the ECU 20 calculates the final ignition timing I τ by modifying the basic ignition timing IT B S E calculated as described above in accordance with the warm-up correction coefficient. Then, in step 360, the ECU 20 controls the ignition coil 13 by controlling the ignition coil 13 according to the calculated value of the final ignition period it, and controls the ignition timing of the spark plug 12. In the engine system of this embodiment described above, the pulsation of the intake air occurs in the intake passage 6 while the engine 3 is running π, and the intake pressure pm detected by the intake pressure sensor 21 is accompanied by the pulsation. Therefore, when the intake air pressure 伴随 associated with the pulsation is directly used as one of the operating parameters for performing various controls of the engine 3, the control becomes unstable.
、在此,本專利申請人發現在伴隨脈動之進氣壓pm之檢 測值、,,下限值pmlo成為最佳的反映實際上燃料室8所吸 入之進f量。因此,在本引擎系統執行之進氣壓檢測方 法’使得對於伴隨進氣壓脈動,即脈動之進氣壓pm計算其 下限值Pm丨0後’將其下限值pm 1 〇決定為最終之進氣壓pm。Here, the applicant of this patent has found that the lower limit value pmlo becomes the best reflection of the amount of intake f that is actually absorbed by the fuel chamber 8 at the detected value of the intake air pressure pm accompanied by the pulsation. Therefore, the intake pressure detection method performed in this engine system 'makes the lower limit value pm 1 〇 for the intake pressure pulsation accompanying the pulsation of the intake pressure, that is, the pulsating intake pressure pm, and determines its lower limit value pm 1 〇 as the final intake pressure. pm.
五、發明說明〇8) 因此’儘管伴隨脈動之進氣 _ :和進氣量相關之適當值和舉::::終之進氣壓PM上得 優異’可檢測和實際 a 在穩定性和響應 ㈣。 Λ際之進…相關性高之最終之進氣 在圖9 ( a )、( b )係表示相對 廢之舉動之時序圖。在圖H 、加逮開度之變化之進氣 輝d ’實線表示藉著本實施示進氣塵叩之心值 壓 氣 氣塵⑽二點鏈線表依據以往::”:得到之最終之進 » α化處理之平滑化進 由本時序圖也得知,在二 合無變化之加速開度之舉動,’:”珂和加速完了後’配 在自開始加速至加速完;;止也安定。又,得知 ΡΜ也階段性的迅速的上'、'、$間之過渡運轉時,進氣壓 之平滑化進氣壓之舉動相比將以二點鏈線表示之以往 速完了後之時刻^穩定,而以t貫施形態之進氣壓PM在加 多之時刻t2變成穩定。因此二之平滑化進氣壓在落後很 氣壓檢測方法,可檢測將變雁:=依據本實施形態之進 之時間之進氣壓PM。 I應性改善了兩❹1 U、t2之間 在圖10表示相對於引整 形。由圖形得知,相對於2载之進氣壓之計算特性之圖 載之增加成曲線性增加,二滑,氣壓對於引擎負 線性增加。即,得知本實 Λ施形悲之進氣壓㈣’成 具有線性。這意指相對;=之進氣壓_於引擎Α載 進氣壓PM成線性反應,表=加速裝置之節流闊9之動作 衣π在過渡時檢測之進氣壓PM之響 2097-4906-PF(Ν);Ahddub.p t d 第22頁 552407V. Description of the invention 〇8) Therefore, 'Although the intake air accompanied by pulsation _: an appropriate value and amount related to the intake air volume :::: the final intake air pressure PM is excellent' can be detected and actual a in stability and response Alas. The advancement of Δinterval ... The final intake air with high correlation is shown in Fig. 9 (a) and (b), which is a timing chart showing the relative disuse. In Figure H, the intake air glow d 'with a change in the degree of arrest is shown by the solid line of the two-point linked line table showing the heart pressure of the intake dust by this implementation. Progress »Smoothing progress of the alpha processing is also known from this timing diagram. In the case of the acceleration of the opening without change in the combination, the": "Ke and acceleration are completed" are equipped to accelerate from the beginning to the acceleration; . In addition, it was learned that when the PM is also in a rapid and rapid transition operation between ',', and $, the smoothing of the intake pressure is more stable than the moment when the past speed is completed as indicated by the two-point chain line. At the time t2, the intake air pressure PM in the form of t continuous application becomes stable. Therefore, the second smoothed intake air pressure falls behind the atmospheric pressure detection method, which can detect the change of the geese: = the intake air pressure PM at the time of advancement according to this embodiment. I response is improved between two ❹1 U, t2. Figure 10 shows the relative shaping. It is known from the graph that the increase of the load relative to the calculation characteristic of the intake air pressure at 2 loads increases in a curve, and the second slip, the air pressure increases linearly with the negative of the engine. That is, it is known that the intake air pressure ㈣ 'of this embodiment is linear. This means relative; = the intake air pressure_ linearly reacts with the intake air pressure PM of the engine A, Table = the throttle of the accelerator device 9 of the action clothing π the sound of the intake air pressure PM detected during the transition 2097-4906-PF ( Ν); Ahddub.ptd Page 22 552407
應性提高。因m,得知自進氣MPM換算之進氣量比依 往之平滑化進氣壓換算之進氣量更正確。 象1人 可是’在本實施形態之引擎3,在運轉中發生逆吹 (blowing-back)等時,在進氣通路6之進氣壓脈動之波 混亂’可能該混亂所引起之不規則性下限值和進動 之正常之下限值混合後出現。 動 對於此現象,在本實施形態,計算伴隨脈動之進 pm之AD值pmad之下限值,而且計算按照引擎轉速ne之臨= 值pthre。而,在计算上,當成為下限值之值叩以比臨 限值pthre小時,使得將成為其下限值之❹值叩以決定 係進氣壓pm之計算值之最終之進氣壓pM。因此,例如由 引擎3之逆吹(blowing-back)等,伴隨脈動之進氣壓pm之、 波形混亂,而出現不規則性下限值,也因自正常之下限值 排除該不規則性下限值,不會將不規則性下限值決定 終之進氣壓PM之值。因而,由於引擎3之逆吹 ”、、取 (blowing-back)等,伴隨脈動之進氣壓⑽混亂,也可防止 最終之進氣壓PM之檢測錯誤。 而且,在本實施形態,以和下限值pml〇 一起計算之上 限值pmhi為基準,以比其上限值⑽]^只小既定之設定寬 pmw之值’計真該臨限值pthre。在此,因既定之設定寬 pmw係依照按照在引擎3之高負載定速運轉時之進氣壓脈動 之引擎轉速NE之差異之振幅預設的,在臨限值pthre上, 得到適合和因引擎轉速NE而變之下限值pml〇之比較之值。 因而,由逆吹(blowing-back)等所引起之進氣壓pm之混亂Improved responsiveness. Because of m, it is known that the intake air volume converted from the intake MPM is more accurate than the smoothed air pressure conversion. One person, however, "when blowing-back occurs during operation of the engine 3 of this embodiment, the wave of the intake pressure pulsation in the intake passage 6 is chaotic" may be caused by irregularities caused by the chaos. The limit value appears after mixing with the normal lower limit of precession. For this phenomenon, in this embodiment, the lower limit value of the AD value pmad with the pulsation advance pm is calculated, and the calculation is based on the advent of the engine speed ne = the value pthre. In calculation, when the value of the lower limit value is smaller than the threshold value pthre, it will be the lower value of the lower limit value to determine the final intake pressure pM which is the calculated value of the intake pressure pm. Therefore, for example, the blow-back of the engine 3 and the pulsation of the intake air pressure pm, the waveform is chaotic, and the lower limit of the irregularity occurs, and the lower limit of the irregularity is excluded from the normal lower limit. The limit value does not determine the lower limit value of the irregularity for the final intake air pressure PM. Therefore, due to the “back blowing” of the engine 3, blowing-back, etc., the pulsation of the intake air pressure is turbulent, and the detection error of the final intake air pressure PM can also be prevented. Furthermore, in this embodiment, the lower limit and Calculate the upper limit value pmhi together with the value pml〇 as a reference, and take the value of the set width pmw smaller than the upper limit value ⑽] to calculate the threshold value pthre. Here, because the set width pmw is According to the amplitude preset according to the difference in the engine speed NE of the intake pressure pulsation during high-load constant-speed operation of the engine 3, at the threshold pthre, the lower limit pml suitable and changed by the engine speed NE is obtained. The value of the comparison. Therefore, the confusion of the intake pressure pm caused by blowing-back, etc.
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五、發明說明(20) 之程度因引擎轉速NE之差異而 當的將不規則之下限值除外, PM之檢測錯誤。 變,也因自正常之下限值適 可適當的防止最終之進氣壓 在此,引擎3之過渡運轉時,即,在減速運轉時及加 f運轉時,因進氣壓脈動之振幅比定速運轉時的小,其進 氣壓脈動之下限值pmlo也相對的變大,有其下限值比 臨限值?^1^大之傾向。例如,在引擎3急加速時,如圖u 所示,在時刻tl〜t2,節流閥9急開後之暫時之期間,進氣 壓pm之AD值pmad之脈動波形之振幅比在接在時刻t2以後之 定速運轉時(高負載)之脈動波形的小,其AD值⑽^之下限 值pmlo比臨限值pthre大。因而,在係引擎3之加速正後之 時刻tl〜t2之間,儘管對於引擎3之進氣空氣量增加,所檢 測之隶終之進氣壓PM依然是小值。結果,依照進氣壓μ等 所计异之最終之燃料喷射量T A U變少,空氣燃料比貧乏 化’引擎轉速NE不上升,可能導致發生失速(stumbHng) 專驅動性能之惡化。 因此’在本實施形態,在引擎3之過渡運轉時,參照 與知照引擎轉速N E計算之臨限值(第一臨限值)p f h r e和不 同,而在計算上比其大之別的臨限值(第二臨限值)pthre 和下限值pmlo之比較。即,參照自替代按照引擎轉速NE所 計算之設定寬pmw之在減速時用或加速時用而預設之比設 小之既定值KP1、KP2和上限值pmhi計算之第二臨 限值pthre與下限值pmlo之比較。而,下限值pmlo比該第 二臨限值pthre小時,因將其下限值pmi〇決定為最終之進V. Description of the invention (20) Except the irregular lower limit due to the difference in engine speed NE, the detection of PM is incorrect. The change is also due to the proper lower limit from the normal limit to prevent the final intake pressure here. During the transient operation of engine 3, that is, during deceleration operation and f operation, the amplitude ratio of the intake pressure pulsation is constant. When the operation is small, the lower limit value pmlo of the intake pressure pulsation is also relatively large. Is there a lower limit value than a threshold value? ^ 1 ^ Big tendency. For example, when the engine 3 is rapidly accelerating, as shown in FIG. U, at time t1 to t2, during the temporary period after the throttle valve 9 is suddenly opened, the amplitude ratio of the pulsation waveform of the AD value pmad of the intake pressure pm is connected at the time. When the fixed-speed operation (high load) after t2 has a small pulsating waveform, the AD value ⑽ ^ lower limit value pmlo is larger than the threshold value pthre. Therefore, between the time t1 and t2 immediately after the acceleration of the engine 3, although the intake air volume for the engine 3 increases, the detected final intake pressure PM is still a small value. As a result, the final fuel injection amount T A U calculated in accordance with the intake air pressure μ and the like becomes smaller, and the leaner fuel-air ratio engine speed NE does not increase, which may result in deterioration of the stumbHng driving performance. Therefore, in this embodiment, during the transitional operation of the engine 3, the threshold value (the first threshold value) pfhre which is different from the threshold value calculated from the known engine speed NE is calculated, and is different from the threshold value that is calculated. (Second Threshold) Comparison of pthre and lower limit pmlo. That is, the second threshold value pthre calculated by referring to the preset value KP1, KP2 and the upper limit value pmhi, which are smaller than the set width pmw calculated in accordance with the engine speed NE for use during deceleration or acceleration, is set to be smaller. Comparison with lower limit pmlo. However, the lower limit value pmlo is smaller than the second threshold value pthre, because the lower limit value pmi0 is determined as the final advance.
2097-4906-PF(N);Ahddub.ptd 第24頁 552407 五、發明說明(21) 氣壓PM,可按照過渡運轉時檢測最終之進氣壓PM。因而, 可確實防止在過渡運轉時之最終之進氣壓PM之檢測錯誤。 即,在引擎3之急加速時,如圖1 2所示,臨限值pthre 變成圖11所不之限值pthre大’在時刻tl〜t2之AD值pmad 之下限值pmlo不會變成比其臨限值pthre大。因而,可適 當的掌握剛急加速後急增之A D值p m a d之下限值p m 1 〇。結 果,在係引擎3之剛加速後之時刻11〜12,也可適當的檢測 按如對於引擎3之進氣空氣;之增加而增加之最終之進氣 壓PM。即,可按照引擎3之過渡運轉適當的檢測進氣壓。 而,在本實施形態,因將所適當的檢測之進氣壓取入 燃料喷射篁控制和點火時期控制,可計算適當之進氣量, 可執行和過渡運轉時相稱之適當之燃料喷射控制和適當之 點火時期控制。結果,可在引擎3實現響應性優異之過渡 ,轉。又,例如,在急加速有響應延遲,相對於進氣空氣 里之最終之燃料喷射量TAU變少,空氣燃料比A/F貧乏化不 2 ’在本實施形態,在急加速時,對於進氣空氣量得到適 Μ之最終之燃料喷射量TAU,因空氣燃料比Α/ρ適當化,可 順利的提咼引擎轉速NE,可確保適當之驅動性。 若依據本實施形態之引擎系統,在引擎3 ECU20自進氣壓感測器21所檢 ^ 瞀、社a師ντ饱,則之進亂堡Pm之AD值pmad計 异進氣壓脈動之下限值pml〇。一但p 丁 按照轉速感測器23所檢測之引螌線击 呀,ECU20 ⑽re。此外,下限H之比弓擎轉速NE之值計算臨限值 豆下卩p佶彳4 比臨限值Pthre小時,ECU20將 ,、下限值pmlo決疋為作為進氧 礼堙pm之计异值之最終之進氣2097-4906-PF (N); Ahddub.ptd Page 24 552407 V. Description of the invention (21) Air pressure PM, the final intake pressure PM can be detected according to the transition operation. Therefore, the detection error of the final intake pressure PM during the transient operation can be reliably prevented. That is, during the rapid acceleration of the engine 3, as shown in FIG. 12, the threshold value pthre becomes the limit value pthre not shown in FIG. 11. The lower limit value pmlo of the AD value pmad at time t1 to t2 does not become greater than Its threshold is pthre large. Therefore, it is possible to appropriately grasp the lower limit value p m 1 of the AD value p m a d which increases sharply immediately after the rapid acceleration. As a result, at the moments 11 to 12 immediately after the acceleration of the engine 3, it is also possible to appropriately detect the final intake air pressure PM as the intake air of the engine 3 increases. That is, the intake pressure can be appropriately detected in accordance with the transient operation of the engine 3. However, in this embodiment, since the appropriately detected intake air pressure is taken into the fuel injection control and ignition timing control, an appropriate intake air amount can be calculated, and appropriate fuel injection control and appropriate during the transition operation can be performed. Control of ignition time. As a result, the engine 3 can achieve a transition with excellent responsiveness. In addition, for example, there is a response delay during rapid acceleration, and the final fuel injection amount TAU in the intake air is reduced, and the air-fuel ratio A / F is not depleted. 2 In this embodiment, during rapid acceleration, The final fuel injection amount TAU of the air / air volume is obtained, and the air / fuel ratio A / ρ is appropriately adjusted to smoothly increase the engine speed NE and ensure proper driveability. If the engine system according to this embodiment is detected by the engine 3 ECU20 from the intake pressure sensor 21 ^ 瞀, the company a ντ full, then the AD value pmad into the bunker Pm is the lower limit of the intake pressure pulsation pml〇. Once p D is hit by the lead wire detected by the speed sensor 23, the ECU 20 ⑽re. In addition, the lower limit value of the ratio of the engine speed NE to the threshold value is calculated. The lower limit value p 卩 4 is smaller than the threshold value Pthre, and the ECU 20 determines the lower limit value pmlo as the value of the oxygen intake ceremony pm. Final air intake
552407 五、發明說明(22) 壓PM〇ECU20依昭該所沐田 ^ .. λΤΓ ^ …、斤、疋之最終之進氣壓ΡΜ之值和引擎 終點火時期Ιτ,作為摔彳U最 料喷射量TAU及最 ^ΤΛΠ ΤΤ々乍為刼作1。然後,藉著ECU20依照這此 餘作里T A U、IΤ各自#告丨1哈&一 >丨+ A 役利赁射态4及點火線圈1 3等,執行煥 料喷射控制及點火時期控制。 囤寻執仃燃 以之因此^自/半隨脈動之進氣壓⑽之⑽值叩以之中將因引 ^AD ^pmad ^ ^ ^ ^ =之不規則之下限值除外,只將適當之下限 最終之進^刪,取入喷射器4及點火線圈13等之控制乍為 =此’儘官進氣壓pm伴隨脈動並在其脈動發生混亂,也 备的求作為操作量之最終之燃料喷射量TAU及最終點火時 期IT之值按照進氣壓pm之舉動適當的控制喷射器4及點 火線圈1 3等。結果,可執行安定性和響應性優異之燃 ^控制,點火時期控制,可執行和實際之進氣量之相關性 同、,氣壓脈動之混亂之影響小之正確之燃料喷射控制及 點火時期控制。同時,可執行不會受到引擎3之逆吹 (blowing-back)等影響之安定之控制。 此外’本發明未限定為上述之實施形態,在不超出本 發明之主旨之範圍也可如以下所示實施。 ° (1)在上述之實施形態,在包含單氣缸引擎3之引擎系 統將本發明之進氣壓檢測方法、進氣壓檢測裝置以及内燃 機之控制裝置等具體化,但是也可在包含氣缸數為2氣缸、、、 或3氣缸、或者3氣缸以上之引擎之引擎系統具體化但, 因若氣缸數愈多進氣脈動之振幅也愈小,可說本發明之效552407 V. Description of the invention (22) The pressure of PM〇ECU20 according to the Zhaotian Institute ^ .. λΤΓ ^…, the final intake pressure PM value of the catty, 疋 and the engine end fire period Ιτ, as the most expected injection of 彳 U The amount of TAU and the maximum ^ ΛΛΤΤΤ is the first operation. Then, the ECU 20 executes the glow injection control and the ignition timing control in accordance with the remaining TAU and IT # 1, 1H & A, and + A, and a firing state 4 and an ignition coil 13. . The value of the ^ self-semi- / semi-pulsating intake air pressure will not be included in the search for the value of ^ AD ^ pmad ^ ^ ^ ^ =, except for the appropriate lower limit The final entry of the lower limit is ^ deleted. The control of taking in the injector 4 and the ignition coil 13 is as follows: This' exhaustible intake pressure pm is accompanied by pulsation and chaos occurs in its pulsation. It is also prepared to be the final fuel injection for the operating amount. The value of the amount TAU and the final ignition timing IT are appropriately controlled in accordance with the behavior of the intake pressure pm, the injector 4 and the ignition coil 13 and so on. As a result, it is possible to perform ignition control and ignition timing control with excellent stability and responsiveness, and perform correct fuel injection control and ignition timing control with the same correlation with the actual intake air volume and little influence of the fluctuation of the air pressure pulsation. . At the same time, it can perform stable control without being affected by the blow-back of the engine 3. In addition, the present invention is not limited to the above-mentioned embodiments, and may be implemented as shown below without departing from the spirit of the present invention. ° (1) In the embodiment described above, the engine system including the single-cylinder engine 3 embodies the intake pressure detection method, the intake pressure detection device, and the control device of the internal combustion engine of the present invention. However, the number of cylinders may be two. The engine system of a cylinder, a three-cylinder, or an engine with three or more cylinders is embodied. However, if the number of cylinders is larger, the amplitude of the intake pulsation is smaller, so the effect of the present invention can be said.
2097-4906-PF(N);Ahddub.ptd 第26頁 552407 五、發明說明(23) 果在氣缸數卜3之引擎特別有效。 (2 )在上述之實施形態, 、,、 控制將本發明具體化,但b 燃^料噴射控制及點火時期 將進氣壓作為運轉參數H 限定為這些控制,也可用於 ^ 一使排氣回流控制等別的控制。 發明之效果 若依據申請專利範園第1 和響應性優異,可檢測和實際之Ί之構造,在安定性 壓,而且可防止内燃機之逆^ 孔里之相關性高之進氣 進氣壓之檢測錯誤。 0Wlng —back)等所引起之 ⑴〇wln“ack)等二卜,内^機之逆吹 若依撼防止進氣壓之檢測錯誤。 專利範圍第!項之發明之效果==構造’除了申請 運轉,當的進行進氣壓之檢測。 t照内燃機之過渡 右依據申請專利範圍第4項之發止 和響應性優異,可檢 之構泣,在女定性 壓,而且可防止引擎量之相關性高之進氣 氣壓之檢測錯誤之逆—ng-back)等所引起之進 運轉適當的進行進氣按照内燃機之過渡 第27頁 552407 五、發明說明(24) 若依據申請專利範圍第6項之發明之構造,在安定性 和響應性優異,可檢測和實際之進氣量之相關性高之進氣 壓,同時可執行不受内燃機之逆吹(blowing-back)等影響 之安定之控制。2097-4906-PF (N); Ahddub.ptd page 26 552407 V. Description of the invention (23) It is particularly effective in engines with cylinder number bu 3. (2) In the embodiment described above, the control embodies the present invention, but b fuel injection control and ignition timing limit the intake pressure as the operating parameter H to these controls, and can also be used to make exhaust gas return Controls and other controls. If the effect of the invention is based on the patent application No. 1 and excellent responsiveness, it can detect the structure that is practical and realistic, and it can detect the pressure of the internal combustion engine with high stability and prevent the reverse of the internal combustion engine. error. 0Wlng —back), etc., such as ⑴〇wln "ack) and so on, the back blowing of the internal machine can prevent the detection error of the intake air pressure. The effect of the invention in the scope of the patent item == structure except for the application operation According to the transition of the internal combustion engine, according to the fourth item of the scope of the patent application, the start and stop and responsiveness are excellent, and the detectable structure is qualitative pressure in the female, and it can prevent the high correlation of the engine volume. Incorrect detection of intake air pressure — reverse-ng-back) etc. Intake operation is properly performed. Intake is performed in accordance with the transition of the internal combustion engine. The structure is excellent in stability and responsiveness, it can detect the intake air pressure with high correlation with the actual intake air volume, and at the same time it can perform stable control without being affected by the blow-back of the internal combustion engine.
2097-4906-PF(N);Ahddub.ptd 第28頁 552407 圖式簡單說明 圖1係表示一實施形態之引擎系統之概略構 圖2係表示進氣壓檢測控制之程式之流程圖。回 圖。圖3係表示相對於引擎轉度之設定寬度之關係之資料 圖4(a)〜(c)係表示進氣壓脈動波形之差異 圖5係表示伴隨脈動之進氣壓之AD值等之、w形。 圖6係表示伴隨脈動之進氣壓之心值等之說=。 圖7係表示燃料喷射控制之程式之流 圖。 圖8係表示點火時期控制之程 =。 圖9(a)、⑻係表示相對於加 之舉動之時序圖。 開度之、交化之進氣壓 圖1 〇係表示相對於引擎負載 形。 戟之進氣壓之計算特性之圖 圖11係表示在加速運轉時之 時序圖。 之進氣塵之AD值等之舉動之 圖1 2係表示在加速運轉時之 時序圖。 f之礎氣壓之AD值等之舉動之 圖1 3係表示以往之進氣壓之 時序圖。 孔1之檢測值和計算值之舉動之 圖14係表示以往之進氣壓檢剛方法之時序圖。 符號說明 3引擎(内燃機) 1 2火星塞(控制對象) b進氣通路 1 3 點火線圈(控制對象)2097-4906-PF (N); Ahddub.ptd Page 28 552407 Brief Description of Drawings Figure 1 shows the general structure of an engine system in an embodiment. Figure 2 shows the flowchart of the intake pressure detection control program. Back to figure. Figure 3 shows the relationship between the set width with respect to engine rotation. Figures 4 (a) ~ (c) show the differences in the intake pressure pulsation waveforms. Figure 5 shows the AD values of the intake pressure with pulsations. . FIG. 6 shows the values of the heart rate of the intake pressure accompanying the pulsation. Fig. 7 is a flowchart showing a program of fuel injection control. Fig. 8 shows the process of ignition timing control. Fig. 9 (a) and IX are timing charts showing the relative actions. The degree of opening and the combined intake air pressure are shown in Figure 10, relative to the engine load. Fig. 11 is a timing chart of the calculation characteristic of the intake air pressure of the halberd. Figure 12 shows the timing diagram of the air intake dust AD value during acceleration operation. Behavior of the AD value of the basic pressure of f, etc. Fig. 13 is a timing chart showing the conventional intake pressure. Fig. 14 is a timing chart showing a conventional method for detecting the intake pressure. Explanation of Symbols 3 Engine (Internal Combustion Engine) 1 2 Spark Plug (Control Object) b Intake Path 1 3 Ignition Coil (Control Object)
IHII 2097-4906-PF(N);Ahddub.ptd 第29頁 552407 圖式簡單說明 2 3轉速感測器(轉速檢測裝置) 4喷射器(燃料喷射閥、控制對象) 2 1進氣壓感測器(進氣壓檢測裝置) 2 0 ECU(下限值計算裝置、臨限值計算裝置、進氣壓 決定裝置、過渡運轉判斷裝置、第二臨限值計算裝置、操 作量計算裝置以及控制裝置) 2097-4906-PF(N);Ahddub.ptd 第30頁IHII 2097-4906-PF (N); Ahddub.ptd Page 29 552407 Brief description of drawings 2 3 Speed sensor (speed detection device) 4 Injector (fuel injection valve, control object) 2 1 Intake pressure sensor (Intake pressure detection device) 2 0 ECU (lower limit value calculation device, threshold value calculation device, intake pressure determination device, transient operation determination device, second threshold value calculation device, operation amount calculation device, and control device) 2097- 4906-PF (N); Ahddub.ptd Page 30
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KR101534712B1 (en) * | 2013-12-17 | 2015-07-08 | 현대자동차 주식회사 | Method and system for diagnosing and correcting boost pressure sensor and air flow sensor by signal of combustion pressure sensor |
CN104533644A (en) * | 2014-12-20 | 2015-04-22 | 河南机电高等专科学校 | Fuel oil controller |
JP6862870B2 (en) * | 2017-02-01 | 2021-04-21 | スズキ株式会社 | Internal combustion engine control device |
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