JP6604319B2 - Gas physical quantity measuring device - Google Patents
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- JP6604319B2 JP6604319B2 JP2016245507A JP2016245507A JP6604319B2 JP 6604319 B2 JP6604319 B2 JP 6604319B2 JP 2016245507 A JP2016245507 A JP 2016245507A JP 2016245507 A JP2016245507 A JP 2016245507A JP 6604319 B2 JP6604319 B2 JP 6604319B2
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本発明は、赤外吸収法を用いて内燃機関の燃焼室内のガスの物理量を計測するガス物理量計測装置に関する。 The present invention relates to a gas physical quantity measuring apparatus that measures a physical quantity of a gas in a combustion chamber of an internal combustion engine using an infrared absorption method.
従来から、点火プラグ、および燃焼室に燃料を噴射するインジェクタを備えた火花点火式筒内直噴エンジンが知られている。このようなエンジンにおいては、燃料を噴射するタイミング、燃料噴射量等をより精密に制御することが可能になった。その結果、燃焼室内の実際の空燃比等をより精密に計測することが求められるようになり、燃焼室を通過させた赤外光の透過率を計測することによって、赤外光を吸収した被計測ガスの濃度を算出する燃料濃度計測装置が提案されている(例えば、特許文献1参照)。 Conventionally, a spark ignition type in-cylinder direct injection engine including an ignition plug and an injector for injecting fuel into a combustion chamber is known. In such an engine, it becomes possible to control the timing of fuel injection, the amount of fuel injection, and the like more precisely. As a result, it has become necessary to measure the actual air-fuel ratio in the combustion chamber more precisely, and by measuring the transmittance of infrared light that has passed through the combustion chamber, A fuel concentration measuring device that calculates the concentration of a measurement gas has been proposed (see, for example, Patent Document 1).
従来の赤外線を用いた内燃機関の燃料濃度又は空燃比(A/F)の計測では、計測システムにおける、振動、光源(レーザ)の発振振動、受光器の受光感度の変動、電気ノイズ等、様々な要因により高周波ノイズが発生する。 Conventional measurement of fuel concentration or air-fuel ratio (A / F) of an internal combustion engine using infrared rays includes various vibrations, oscillation oscillation of a light source (laser), fluctuation of light receiving sensitivity of a light receiver, electric noise, etc. in a measurement system. High frequency noise is generated due to various factors.
図1(a)にクランク角位相に対して赤外光を受光した光伝導素子の出力電圧を示し、図1(b)に各周波数におけるパワースペクトル密度を示す。空燃比は、エンジンの回転数に比例した周期、図1(b)に示す例では20Hz程度で変動するので、空燃比の変動周期に対応する20Hz近傍のスペクトル成分が最も密度が高くなっている。一方で、空燃比の変動周期よりも高い周波数(1kHz〜)の成分も含まれているが、これは上述した高周波ノイズに対応する成分であると考えられる。つまり、図1(a)に示す計測波形には高周波ノイズが重畳していると考えられ、これら計測値をそのまま使用して空燃比を算出すると、誤差が大きくなる。 FIG. 1A shows the output voltage of the photoconductive element that receives infrared light with respect to the crank angle phase, and FIG. 1B shows the power spectral density at each frequency. Since the air-fuel ratio fluctuates at a cycle proportional to the engine speed, which is about 20 Hz in the example shown in FIG. 1B, the spectral component near 20 Hz corresponding to the fluctuating cycle of the air-fuel ratio has the highest density. . On the other hand, although the component of the frequency (1 kHz-) higher than the fluctuation cycle of an air fuel ratio is also included, this is considered to be a component corresponding to the high frequency noise mentioned above. That is, it is considered that high-frequency noise is superimposed on the measurement waveform shown in FIG. 1A, and if these measurement values are used as they are, the error becomes large.
そのため計測精度をさらに高めるためには、この高周波ノイズをローパスフィルタ処理等によって除去する必要がある。 Therefore, in order to further improve the measurement accuracy, it is necessary to remove this high-frequency noise by low-pass filter processing or the like.
しかしながら、従来技術では、点火時期(SA)直後などの点火することで燃料が瞬時に酸化し、空燃比が急変する急変部においては、赤外線の透過率から算出した空燃比に対してローパスフィルタ処理を行うと空燃比の急変部の値の影響が大きくなるため、空燃比が急変する直前の点火時期付近の空燃比の算出値も急変部の値側に大きくシフトして誤差が大きくなるという課題がある。 However, in the prior art, in the sudden change portion where the fuel is instantly oxidized by ignition such as immediately after the ignition timing (SA) and the air-fuel ratio changes suddenly, the low-pass filter processing is performed on the air-fuel ratio calculated from the infrared transmittance. Since the influence of the value of the sudden change portion of the air-fuel ratio becomes large when the engine is operated, the calculated value of the air-fuel ratio near the ignition timing immediately before the sudden change of the air-fuel ratio is greatly shifted to the value side of the sudden change portion, resulting in a large error. There is.
図2に、従来の計測方法におけるクランク角位相に対する受光素子の透過電圧の生データ、およびローパスフィルタ処理後のデータを示す。これは、ローパスフィルタ処理のカットオフ周波数が低くなるに従って、点火時期付近の計測値は生データに比べて大きくなっていく様子を示している。 FIG. 2 shows raw data of the transmission voltage of the light receiving element with respect to the crank angle phase in the conventional measurement method, and data after the low-pass filter processing. This shows that the measured value near the ignition timing becomes larger than the raw data as the cut-off frequency of the low-pass filter processing becomes lower.
本発明は、このような課題に鑑みてなされたもので、その目的とするところは、赤外吸収法を用いた内燃機関の燃焼室内のガスの物理量の計測において、点火時期までの測定データに点火時期までの測定データを時間反転したものを点火時期以降の測定データとして結合した結合データを生成し、結合データに対してローパスフィルタ処理を行うことにより、測定データに重畳した高周波ノイズを除去し、高周波ノイズ除去前よりも高精度に点火時期までのガスの物理量を計測することができるガス物理量計測装置を提供することにある。 The present invention has been made in view of such a problem, and an object of the present invention is to use measurement data up to the ignition timing in measurement of a physical quantity of gas in a combustion chamber of an internal combustion engine using an infrared absorption method. By combining the measurement data up to the ignition timing with time reversal combined as measurement data after the ignition timing, low-pass filter processing is performed on the combined data to remove high-frequency noise superimposed on the measurement data. An object of the present invention is to provide a gas physical quantity measuring apparatus capable of measuring a physical quantity of gas until ignition timing with higher accuracy than before removing high frequency noise.
上記の課題を解決するために、本発明は、内燃機関の燃焼室に赤外光を照射して前記燃焼室内を通過した前記赤外光の透過率を計測し、計測された前記赤外光の透過率に基づき前記燃焼室内のガスの物理量を算出するガス物理量計測装置であって、前記計測された赤外光の透過率に基づき点火時期まで算出されたクランク角位相に対する前記ガスの物理量である第1のデータを生成し、前記点火時期を起点として前記第1のデータを時間反転させた第2のデータを生成し、前記第1のデータに前記点火時期以降のデータとして前記第2のデータを結合した結合データにローパスフィルタ処理を行って第3のデータを生成し、前記第3のデータに基づき前記燃焼室内のガスの物理量を算出することを特徴とする。 In order to solve the above problems, the present invention irradiates a combustion chamber of an internal combustion engine with infrared light, measures the transmittance of the infrared light that has passed through the combustion chamber, and measures the measured infrared light. A gas physical quantity measuring device for calculating a physical quantity of gas in the combustion chamber based on the transmittance of the gas, wherein the physical quantity of the gas with respect to the crank angle phase calculated until the ignition timing based on the measured transmittance of infrared light The first data is generated, the second data obtained by reversing the time of the first data with the ignition timing as a starting point is generated, and the second data as the data after the ignition timing is generated in the first data. Low-pass filter processing is performed on the combined data obtained by combining the data to generate third data, and a physical quantity of the gas in the combustion chamber is calculated based on the third data.
請求項2に記載の発明は、請求項1に記載のガス物理量計測装置において、前記赤外光の波長は3.3〜3.5μmであり、前記ガスの物理量は空燃比であることを特徴とする。
The invention according to
請求項3に記載の発明は、請求項1に記載のガス物理量計測装置において、前記赤外光の波長は1.2〜1.4μmであり、前記ガスの物理量はガス温度であることを特徴とする。
The invention according to
請求項4に記載の発明は、請求項1に記載のガス物理量計測装置において、前記赤外光の波長は4.3〜4.5μmであり、前記ガスの物理量は二酸化炭素濃度であることを特徴とする。 According to a fourth aspect of the present invention, in the gas physical quantity measuring device according to the first aspect, the wavelength of the infrared light is 4.3 to 4.5 μm, and the physical quantity of the gas is a carbon dioxide concentration. Features.
本発明は、赤外吸収法を用いた内燃機関の燃焼室内のガスの物理量の計測において、点火時期までの測定データに点火時期までの測定データを時間反転したものを点火時期以降の測定データとして結合した結合データを生成し、結合データに対してローパスフィルタ処理を行うことにより、測定データに重畳した高周波ノイズを除去し、高周波ノイズ除去前よりも高精度に点火時期までのガスの物理量を計測することができる。 In the measurement of the physical quantity of the gas in the combustion chamber of the internal combustion engine using the infrared absorption method, the present invention is obtained by inverting the measurement data up to the ignition timing with the measurement data up to the ignition timing as measurement data after the ignition timing. Generate combined data and perform low-pass filter processing on the combined data to remove high-frequency noise superimposed on the measurement data and measure the physical quantity of gas up to the ignition timing with higher accuracy than before removing high-frequency noise can do.
以下、本発明の実施の形態について、詳細に説明する。 Hereinafter, embodiments of the present invention will be described in detail.
図3に、本発明の一実施形態に係るガス物理量計測装置の構成を示す。ガス物理量計測装置は、被計測物理量に対応する周波数の赤外光を出射する光源301と、赤外光を内燃機関の燃焼室まで導き、燃焼室内を通過した赤外光を外部に導く光導波路302と、燃焼室内を透過した赤外光を受光して光強度を電気信号として出力する受光素子303と、受光素子から出力された電気信号を処理して空燃比を算出する演算部304とを備えている。尚、本発明では、演算部304以外の光源301から受光素子303までの構成は、内燃機関の燃焼室内を通過した赤外光の光強度を電気信号として出力可能なものであれば他の構成で代替可能である。
FIG. 3 shows a configuration of a gas physical quantity measuring device according to one embodiment of the present invention. The gas physical quantity measuring device includes a
図4に、本発明の一実施形態に係るガス物理量計測装置の動作を説明するフロー図を示す。赤外吸収法を用いた内燃機関の燃焼室内のガス物理量計測装置において、燃焼室内を通過した赤外光の点火時期までの透過率を計測する(S401)。計測された赤外光の透過率から、図5(a)に示すようなクランク角位相に対する空燃比の第1のデータを生成する(S402)。算出したクランク角位相に対する空燃比の点火時期(SA)を確認し(S403)、クランク角位相に対する空燃比の第1のデータを、点火時期を起点として時間反転させた第2のデータ、すなわち、クランク角位相に対する空燃比の第1のデータを点火時期で折り返し、点火時期を起点としてクランク角位相を逆の順序で並び替えるように空燃比を並べ替えた第2のデータを生成する。そして、点火時期までの第1のデータに点火時期以降のデータとして第2のデータを結合して図5(b)に示すような結合データを生成する(S404)。折り返しデータに対してローパスフィルタ処理を行って第3のデータを生成し(S405)、図5(c)に示すような高周波ノイズを除去した空燃比を算出する(S406)。 FIG. 4 is a flowchart for explaining the operation of the gas physical quantity measuring device according to the embodiment of the present invention. In the gas physical quantity measuring device in the combustion chamber of the internal combustion engine using the infrared absorption method, the transmittance of the infrared light that has passed through the combustion chamber until the ignition timing is measured (S401). From the measured infrared light transmittance, first data of air-fuel ratio with respect to the crank angle phase as shown in FIG. 5A is generated (S402). The air-fuel ratio ignition timing (SA) with respect to the calculated crank angle phase is confirmed (S403), and the first data of the air-fuel ratio with respect to the crank angle phase is time-reversed with the ignition timing as a starting point, that is, First data of the air-fuel ratio with respect to the crank angle phase is turned back at the ignition timing, and second data is generated by rearranging the air-fuel ratio so that the crank angle phase is rearranged in the reverse order starting from the ignition timing. Then, the first data up to the ignition timing is combined with the second data as data after the ignition timing to generate combined data as shown in FIG. 5B (S404). Low-pass filter processing is performed on the return data to generate third data (S405), and an air-fuel ratio from which high-frequency noise as shown in FIG. 5C is removed is calculated (S406).
図6に、1サイクルの計測例として、クランク角位相に対する空燃比の生データと、クランク角位相に対する空燃比の本発明によるローパスフィルタ処理後のデータを示す。このときの点火時期における空燃比は、従来方法による計測値が12.6であったのに対し、本発明による計測値では12.3であった。 FIG. 6 shows raw data of the air-fuel ratio with respect to the crank angle phase and data after the low-pass filter processing according to the present invention of the air-fuel ratio with respect to the crank angle phase as measurement examples of one cycle. The air-fuel ratio at the ignition timing at this time was 12.6 as measured by the conventional method, but 12.3 as measured according to the present invention.
また、表1は、200サイクル分のデータを元に従来の計測方法(ローパスフィルタ処理無し)と本発明の計測方法で算出した点火時期における空燃比の平均、分散、標準偏差、最小値、最大値を示す。 Table 1 shows the average, variance, standard deviation, minimum value, maximum value of air-fuel ratio at the ignition timing calculated by the conventional measurement method (without low-pass filter processing) based on the data for 200 cycles and the measurement method of the present invention. Indicates the value.
表1は、本発明では、これまでローパスフィルタ処理を行うと計測誤差が大きくなる急変部近傍の値についても、誤差を抑制しながらローパスフィルタ処理を行うことを可能にし、高周波ノイズを含む生データよりもばらつきの小さい空燃比の計測が可能であることを示している。 Table 1 shows that in the present invention, it is possible to perform low-pass filter processing while suppressing errors even for values in the vicinity of sudden change portions where measurement errors become large when low-pass filter processing has been performed so far, and raw data including high-frequency noise. It is shown that the air-fuel ratio can be measured with less variation than the above.
ここまで空燃比を計測する場合について説明してきたが、使用する赤外光の周波数を変えることによって計測対象となるガスの物理量を変えることができる。空燃比を計測するのに適した波長は3.3〜3.5μmであり、例えば燃焼室内のガス温度を計測するのには1.2〜1.4μm、燃焼室内の二酸化炭素濃度を計測するのには4.3〜4.5μmの波長が適している。本発明においても、使用する赤外光の周波数を変えることによって様々なガスの物理量を計測することができ、使用する赤外光の波長に関わらず同様の効果を奏することができる。 The case where the air-fuel ratio is measured has been described so far, but the physical quantity of the gas to be measured can be changed by changing the frequency of the infrared light to be used. The wavelength suitable for measuring the air-fuel ratio is 3.3 to 3.5 μm. For example, 1.2 to 1.4 μm is used to measure the gas temperature in the combustion chamber, and the carbon dioxide concentration in the combustion chamber is measured. For this, a wavelength of 4.3 to 4.5 μm is suitable. Also in the present invention, the physical quantity of various gases can be measured by changing the frequency of the infrared light used, and the same effect can be obtained regardless of the wavelength of the infrared light used.
301 光源
302 光導波路
303 受光素子
304 演算部
301
Claims (4)
前記計測された赤外光の透過率に基づき点火時期まで算出されたクランク角位相に対する前記ガスの物理量である第1のデータを生成し、前記点火時期を起点として前記第1のデータを時間反転させた第2のデータを生成し、前記第1のデータに前記点火時期以降のデータとして前記第2のデータを結合した結合データにローパスフィルタ処理を行って第3のデータを生成し、前記第3のデータに基づき前記燃焼室内のガスの物理量を算出することを特徴とするガス物理量計測装置。 Irradiate the combustion chamber of the internal combustion engine with infrared light to measure the transmittance of the infrared light that has passed through the combustion chamber, and based on the measured transmittance of the infrared light, determine the physical quantity of the gas in the combustion chamber. A gas physical quantity measuring device to calculate,
Generating first data that is a physical quantity of the gas with respect to a crank angle phase calculated up to an ignition timing based on the measured transmittance of infrared light, and time-reversing the first data with the ignition timing as a starting point Second data is generated, low-pass filter processing is performed on combined data obtained by combining the first data with the second data as data after the ignition timing, and third data is generated. 3. A gas physical quantity measuring device that calculates a physical quantity of gas in the combustion chamber based on the data of No. 3.
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