JP5779532B2 - Engine electronic governor - Google Patents

Engine electronic governor Download PDF

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JP5779532B2
JP5779532B2 JP2012073157A JP2012073157A JP5779532B2 JP 5779532 B2 JP5779532 B2 JP 5779532B2 JP 2012073157 A JP2012073157 A JP 2012073157A JP 2012073157 A JP2012073157 A JP 2012073157A JP 5779532 B2 JP5779532 B2 JP 5779532B2
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value
speed deviation
rotational speed
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JP2013204484A (en
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正徳 藤原
正徳 藤原
保生 藤井
保生 藤井
一成 辻野
一成 辻野
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Kubota Corp
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本発明は、エンジンの電子ガバナに関し、詳しくは、回転数偏差が微小範囲に収まった後に発生することがある、周期的な回転数変動の狭小ピークを回避することができる、エンジンの電子ガバナに関する。   The present invention relates to an engine electronic governor, and more particularly, to an engine electronic governor capable of avoiding a narrow peak of periodic rotational speed fluctuation that may occur after the rotational speed deviation falls within a minute range. .

従来、エンジンの電子ガバナとして、制御手段が、回転数偏差演算手段と、PID制御またはPI制御の制御値演算手段と、電流制御部と、アクチュエータ駆動回路とを備え、回転数偏差演算手段で目標回転数と実回転数との回転数偏差を演算し、この回転数偏差に基づいて、制御値演算手段がPID制御またはPI制御の制御値を演算し、この制御値に基づいて、電流制御部がアクチュエータ駆動回路のアクチュエータ電流を制御し、このアクチュエータ駆動電流でアクチュエータを駆動し、このアクチュエータで燃料噴射ポンプの燃料調量部を調量することにより、回転数偏差を所定範囲内に収束させるものがある(例えば、特許文献1参照)。
また、制御手段がディザ電流重畳手段を備え、このディザ電流重畳手段でアクチュエータ駆動電流にディザ電流を重畳させるものがある(特許文献2参照)。
後者には、ディザ電流によりアクチュエータの出力部を微小振動させ、これに追従する燃料調量部の微小振動により、燃料調量部の応答性を高めることができる利点がある。
2. Description of the Related Art Conventionally, as an electronic governor of an engine, a control means includes a rotation speed deviation calculation means, a control value calculation means for PID control or PI control, a current control unit, and an actuator drive circuit. A rotational speed deviation between the rotational speed and the actual rotational speed is calculated, and based on this rotational speed deviation, a control value calculating means calculates a control value for PID control or PI control, and based on this control value, a current control unit Controls the actuator current of the actuator drive circuit, drives the actuator with this actuator drive current, and controls the fuel metering part of the fuel injection pump with this actuator, thereby converging the rotational speed deviation within a predetermined range (For example, refer to Patent Document 1).
Further, there is a control means that includes a dither current superimposing means, and the dither current superimposing means superimposes the dither current on the actuator drive current (see Patent Document 2).
The latter has an advantage that the output of the actuator is minutely vibrated by the dither current, and the response of the fuel metering unit can be enhanced by the minute vibration of the fuel metering unit following the dither current.

特開2011−74771号公報(図2参照)JP 2011-74771 A (see FIG. 2) 特開2009−85062号公報(図1参照)JP 2009-85062 A (see FIG. 1)

《問題》 回転数偏差が微小範囲に収まった後に、周期的な回転数変動の狭小ピークが発生することがある。
PID制御またはPI制御の制御値演算手段とディザ電流重畳手段とを組み合わせると、図5に示すように、回転数偏差ΔRの絶対値|ΔR|が微小範囲LRに収まった後に、周期的な回転数変動の狭小ピーク(P)が発生することがある。
このような狭小ピーク(P)の発生は、周波数変動に直結し、例えばエンジン発電機に用いた場合には、電圧と周波数の安定性等の性能が低下し、電灯をちらつかせる等の不具合が生じる。
<< Problem >> After the rotational speed deviation falls within a very small range, a narrow peak of periodic rotational speed fluctuation may occur.
When the control value calculating means for PID control or PI control and the dither current superimposing means are combined, as shown in FIG. 5, after the absolute value | ΔR | of the rotational speed deviation ΔR falls within the minute range LR, A narrow peak (P) with a number variation may occur.
The occurrence of such a narrow peak (P) is directly linked to frequency fluctuations. For example, when it is used for an engine generator, performance such as stability of voltage and frequency is lowered, and there is a problem such as flickering of an electric lamp. Arise.

本発明の課題は、回転数偏差が微小範囲に収まった後に発生することがある、周期的な回転数変動の狭小ピークを回避することができる、エンジンの電子ガバナを提供することにある。   An object of the present invention is to provide an electronic governor for an engine that can avoid a narrow peak of periodic rotational speed fluctuations that may occur after the rotational speed deviation falls within a very small range.

(請求項1に係る発明の前提となる発明特定事項)
図3に例示するように、制御手段(1)が、回転数偏差演算手段(2)と、PID制御またはPI制御の制御値演算手段(3)と、電流制御部(4)と、アクチュエータ駆動回路(5)とを備え、回転数偏差演算手段(2)で目標回転数と実回転数との回転数偏差を演算し、この回転数偏差に基づいて、制御値演算手段(3)がPID制御またはPI制御の制御値を演算し、この制御値に基づいて、電流制御部(4)がアクチュエータ駆動回路(5)のアクチュエータ駆動電流を制御し、このアクチュエータ駆動電流でアクチュエータ(6)を駆動し、このアクチュエータ(6)で燃料噴射ポンプ(7)の燃料調量部(8)を調量することにより、回転数偏差ΔRを所定範囲内に収束させるとともに、
制御手段(1)がディザ電流重畳手段(9)を備え、このディザ電流重畳手段(9)でアクチュエータ駆動電流にディザ電流を重畳させるようにした、エンジンの電子ガバナ。
(Invention-specific matters on which the invention of claim 1 is based )
As illustrated in FIG. 3 , the control means (1) includes a rotation speed deviation calculation means (2), a control value calculation means (3) for PID control or PI control, a current control section (4), and an actuator drive. A circuit (5), and a rotational speed deviation calculating means (2) calculates a rotational speed deviation between the target rotational speed and the actual rotational speed, and based on the rotational speed deviation, the control value calculating means (3) The control value of control or PI control is calculated, and based on this control value, the current control unit (4) controls the actuator drive current of the actuator drive circuit (5), and the actuator (6) is driven by this actuator drive current. By adjusting the fuel metering section (8) of the fuel injection pump (7) with this actuator (6), the rotational speed deviation ΔR is converged within a predetermined range,
An electronic governor for an engine, wherein the control means (1) includes dither current superimposing means (9), and the dither current superimposing means (9) superimposes the dither current on the actuator drive current.

(周期的な回転数変動の狭小ピークが発生する原因)
PID制御またはPI制御の制御値演算手段とディザ電流重畳手段とを組み合わせた場合、回転数偏差が微小範囲に収まった後に、周期的な回転数変動の狭小ピークが発生する原因について、本願発明の発明者らは、研究の結果、次の知見を得た。
すなわち、図1を参照して説明すると、目標回転数がある値に設定された場合、燃料噴射ポンプ(7)の燃料圧送周期とディザ電流による燃料調量部(8)の振動周期が同期することがある。この場合、燃料圧送のために作動が拘束された燃料調量部(8)がアクチュエータ(6)の出力部(13)の振動に追従せず、燃料調量部(8)の調量位置が適正位置からずれ、微小回転数偏差(例えば、1rpm以下の回転数偏差)が定常的に残ることがある。この微小回転数偏差を放置しておくと、図5に示すように、積分値Iが累積し、この積分値Iを相殺する制御の結果、周期的な回転数変動の狭小ピーク(P)が発生する。
本願発明の発明者らは、この知見に基づき、本願発明に至った。
(Cause of narrow peaks of periodic rotational speed fluctuations)
When the control value calculation means for PID control or PI control and the dither current superposition means are combined, the cause of the occurrence of a narrow peak of periodic rotational speed fluctuation after the rotational speed deviation is within a very small range is described in the present invention. As a result of the research, the inventors have obtained the following knowledge.
That is, referring to FIG. 1, when the target rotational speed is set to a certain value, the fuel pumping cycle of the fuel injection pump (7) and the vibration cycle of the fuel metering unit (8) by the dither current are synchronized. Sometimes. In this case, the fuel metering unit (8) whose operation is restricted for fuel pumping does not follow the vibration of the output unit (13) of the actuator (6), and the metering position of the fuel metering unit (8) is Deviation from an appropriate position may cause a minute rotational speed deviation (for example, rotational speed deviation of 1 rpm or less) to remain constantly. If this minute rotational speed deviation is left unattended, as shown in FIG. 5, the integral value I is accumulated, and as a result of control for canceling out this integral value I, a narrow peak (P) of periodic rotational speed fluctuations is obtained. Occur.
The inventors of the present invention have arrived at the present invention based on this finding.

(請求項1に係る発明の特徴となる発明特定事項)
図3、図4に例示するように、制御手段(1)が、積分値変動率判定手段(3a)と、積算キャンセル手段(10)とを備え、制御値演算手段(3)で演算した積分値Iの積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回っている間は、これを積分値変動率判定手段(3a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルする、ことを特徴とするエンジンの電子ガバナ。
(Invention-specific matters that characterize the invention according to claim 1 )
As illustrated in FIGS. 3 and 4, the control means (1) includes an integral value fluctuation rate determination means (3a) and an integration cancellation means (10), and the integration calculated by the control value calculation means (3). While the absolute value | ΔI / ΔT | of the integral value fluctuation rate ΔI / ΔT of the value I is below the predetermined reference fluctuation rate value SI, it is based on the fact that the integral value fluctuation rate judging means (3a) has judged this. An electronic governor for an engine, wherein the integration canceling means (10) cancels the integration of the integral value I by the control value calculating means (3).

請求項1に係る発明は、次の効果を奏する。
《効果》 回転数偏差が微小範囲に収まった後に発生することがある、周期的な回転数変動の狭小ピークを回避することができる。
図3、図4に例示するように、制御手段(1)が、積分値変動率判定手段(3a)と、積算キャンセル手段(10)とを備え、制御値演算手段(3)で演算した積分値Iの積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回っている間は、これを積分値変動率判定手段(3a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルするので、微小回転数偏差に基づく積分値Iが累積せず、この積分値Iを相殺する制御の結果生じていた、周期的な回転数変動の狭小ピークの発生が起こらない。このため、回転数偏差が微小範囲LRに収まった後に発生することがある、周期的な回転数変動の狭小ピークを回避することができる。
The invention according to claim 1 has the following effects.
<Effect> It is possible to avoid a narrow peak of periodic rotational speed fluctuations that may occur after the rotational speed deviation falls within a very small range.
As illustrated in FIGS. 3 and 4, the control means (1) includes an integral value fluctuation rate determination means (3a) and an integration cancellation means (10), and the integration calculated by the control value calculation means (3). While the absolute value | ΔI / ΔT | of the integral value fluctuation rate ΔI / ΔT of the value I is below the predetermined reference fluctuation rate value SI, it is based on the fact that the integral value fluctuation rate judging means (3a) has judged this. Thus, since the integration canceling means (10) cancels the integration of the integral value I by the control value calculating means (3), the integral value I based on the minute rotation speed deviation is not accumulated, and the integral value I is canceled. As a result, the occurrence of a narrow peak of periodic rotational speed fluctuation does not occur. For this reason, it is possible to avoid a narrow peak of periodic rotational speed fluctuation that may occur after the rotational speed deviation falls within the minute range LR.

本発明の参考形態に係るエンジンの電子ガバナのブロック図である。It is a block diagram of the electronic governor of the engine which concerns on the reference form of this invention. 図1の電子ガバナの制御によるエンジン回転数のグラフである。It is a graph of the engine speed by control of the electronic governor of FIG. 本発明の実施形態に係るエンジンの電子ガバナのブロック図である。It is a block diagram of the electronic governor of the engine which concerns on embodiment of this invention. 図3の電子ガバナの制御によるエンジン回転数のグラフである。It is a graph of the engine speed by control of the electronic governor of FIG. 従来技術に係るエンジンの電子ガバナの制御によるエンジン回転数と積分値のグラフである。It is a graph of the engine speed and integral value by control of the electronic governor of the engine which concerns on a prior art.

図1、図2は本発明の参考形態に係るエンジンの電子ガバナを説明する図、図3、図4は本発明の実施形態に係るエンジンの電子ガバナを説明する図であり、この参考形態と実施形態では、ディーゼルエンジンの電子ガバナについて説明する。 1 and 2 illustrate an electronic governor for an engine according to the reference embodiment of the present invention, FIG. 3, FIG. 4 is a diagram illustrating an electronic governor for an engine according to an embodiment of the present invention, and this reference embodiment In the embodiment , an electronic governor of a diesel engine will be described.

まず、参考形態について説明する。
このディーゼルエンジンの電子ガバナは、エンジン発電機に用いている。
図1、図2に示すように、制御手段(1)が、回転数偏差演算手段(2)と、PID制御方式の制御値演算手段(3)と、電流制御部(4)と、アクチュエータ駆動回路(5)とを備え、回転数偏差演算手段(2)で目標回転数と実回転数との回転数偏差を演算し、この回転数偏差に基づいて、制御値演算手段(3)がPID制御の制御値を演算し、この制御値に基づいて、電流制御部(4)がアクチュエータ駆動回路(5)のアクチュエータ駆動電流を制御し、このアクチュエータ駆動電流でアクチュエータ(6)を駆動し、このアクチュエータ(6)で燃料噴射ポンプ(7)の燃料調量部(8)を調量することにより、回転数偏差ΔRを所定範囲内に収束させるとともに、制御手段(1)がディザ電流重畳手段(9)を備え、このディザ電流重畳手段(9)でアクチュエータ駆動電流にディザ電流を重畳させるようにしている。
First, a reference form will be described.
This diesel engine electronic governor is used for an engine generator.
As shown in FIGS. 1 and 2, the control means (1) includes a rotation speed deviation calculating means (2), a PID control type control value calculating means (3), a current control section (4), and an actuator drive. A circuit (5), and a rotational speed deviation calculating means (2) calculates a rotational speed deviation between the target rotational speed and the actual rotational speed, and based on the rotational speed deviation, the control value calculating means (3) The control value of the control is calculated, and based on this control value, the current controller (4) controls the actuator drive current of the actuator drive circuit (5), and drives the actuator (6) with this actuator drive current. By adjusting the fuel metering section (8) of the fuel injection pump (7) with the actuator (6), the rotational speed deviation ΔR is converged within a predetermined range, and the control means (1) is a dither current superimposing means ( 9), and this dither current superimposing means (9) The dither current is superimposed.

図1に示すように、回転数偏差演算手段(2)には、目標回転数検出手段(19)と実回転数検出手段(20)を接続している。目標回転数検出手段(19)は、アクセルペダルの位置を検出して、エンジンの目標回転数を検出するポテンショメータである。実回転数検出手段(20)は、エンジンの実回転数を検出するピックアップコイルである。   As shown in FIG. 1, a target rotational speed detecting means (19) and an actual rotational speed detecting means (20) are connected to the rotational speed deviation calculating means (2). The target engine speed detecting means (19) is a potentiometer that detects the target engine speed by detecting the position of the accelerator pedal. The actual rotational speed detection means (20) is a pickup coil that detects the actual rotational speed of the engine.

図1に示すように、制御値演算手段(3)は、比例項演算部(14)と積分項演算部(11)と微分項演算部(15)とを備えている。
制御値演算手段(3)は、回転数偏差に基づく制御値のPID演算式の演算を行う。
PID演算式は、次の通りである。
制御値=Kp×(回転数偏差)+Ki×(偏差の累積値)+Kd×(前回偏差との差)
ここで、Kp×(回転数偏差)は比例項、Ki×(偏差の累積値)は積分項、Kd×(前回偏差との差)は微分項、Kpは比例ゲイン、Kiは積分ゲイン、Kdは微分ゲインである。
制御値演算手段(3)は、微分項演算部(15)のないPI制御の演算手段であってもよい。
As shown in FIG. 1, the control value computing means (3) includes a proportional term computing unit (14), an integral term computing unit (11), and a differential term computing unit (15).
The control value calculation means (3) calculates the PID calculation formula of the control value based on the rotational speed deviation.
The PID arithmetic expression is as follows.
Control value = Kp × (rotational speed deviation) + Ki × (cumulative deviation value) + Kd × (difference from previous deviation)
Here, Kp × (rotational speed deviation) is a proportional term, Ki × (cumulative deviation) is an integral term, Kd × (difference from previous deviation) is a differential term, Kp is a proportional gain, Ki is an integral gain, Kd Is the differential gain.
The control value calculation means (3) may be a PI control calculation means without the differential term calculation unit (15).

図1に示すように、アクチュエータ(6)は、リニアソレノイドである。
燃料噴射ポンプ(7)はボッシュ式の列形燃料噴射ポンプである。
燃料調量部(8)は燃料調量ラック(16)である。
燃料調量ラック(16)は、付勢スプリング(17)によって燃料増量側に付勢され、アクチュエータ(6)の出力部(13)で受け止められている。
アクチュエータ(6)の出力部(13)がソレノイドの電磁力で本体側に引かれると、付勢スプリング(17)の付勢力で、燃料調量ラック(16)が燃料増量側に駆動される。アクチュエータ(6)の出力部(13)が戻しスプリング(18)の付勢力で本体側から押し出されると、燃料調量ラック(16)が燃料減量側に駆動される。
アクチュエータ(6)の非通電時は、出力部(13)が戻しスプリング(18)の付勢力で本体側から押し出され、燃料調量ラック(16)が燃料無噴射位置に保持される。
As shown in FIG. 1, the actuator (6) is a linear solenoid.
The fuel injection pump (7) is a Bosch type row fuel injection pump.
The fuel metering unit (8) is a fuel metering rack (16).
The fuel metering rack (16) is urged toward the fuel increase side by the urging spring (17) and is received by the output portion (13) of the actuator (6).
When the output portion (13) of the actuator (6) is pulled toward the main body by the electromagnetic force of the solenoid, the fuel metering rack (16) is driven to the fuel increase side by the biasing force of the biasing spring (17). When the output portion (13) of the actuator (6) is pushed out from the main body side by the urging force of the return spring (18), the fuel metering rack (16) is driven to the fuel reduction side.
When the actuator (6) is not energized, the output section (13) is pushed out from the main body side by the urging force of the return spring (18), and the fuel metering rack (16) is held at the no fuel injection position.

図1、図2に示すように、制御手段(1)が、回転数偏差判定手段(2a)と積算キャンセル手段(10)とを備え、所定時間Δtの回転数偏差ΔRの平均値ΔRavの絶対値|ΔRav|が所定の基準偏差値SRを下回っている間は、これを回転数偏差判定手段(2a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルする。この実施形態では、基準偏差値SRは、微小範囲LRよりも小さい値で、1rpm未満の値としている。この基準偏差値SRは、適用するシステムに応じて適正な値を選択すればよい。回転数偏差ΔRが微小範囲LRに入っている場合には、所定時間Δtの回転数偏差ΔRの平均値ΔRavの絶対値|ΔRav|が所定の基準偏差値SRを下回るように、基準偏差値SRを設定しておく。
図1、図2に例示するように、この参考形態では、制御手段(1)が、回転数偏差判定手段(2a)と積算キャンセル手段(10)とを備え、所定時間Δtの回転数偏差ΔRの平均値ΔRavの絶対値|ΔRav|が所定の基準偏差値SRを下回っている間は、これを回転数偏差判定手段(2a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルするので、微小回転数偏差に基づく積分値Iが累積せず、この積分値Iを相殺する制御の結果生じていた、周期的な回転数変動の狭小ピークの発生が起こらない。このため、回転数偏差が微小範囲LRに収まった後に発生することがある、周期的な回転数変動の狭小ピークを回避することができる。
As shown in FIG. 1 and FIG. 2, the control means (1) includes a rotation speed deviation determination means (2a) and an integration cancellation means (10), and the absolute value of the average value ΔRav of the rotation speed deviation ΔR over a predetermined time Δt. While the value | ΔRav | is below the predetermined reference deviation value SR, the integration canceling means (10) controls the control value calculating means (3) based on the fact that the rotation speed deviation judging means (2a) has determined this value. Cancel the integration of the integral value I. In this embodiment, the reference deviation value SR is a value smaller than the minute range LR and less than 1 rpm. As this reference deviation value SR, an appropriate value may be selected according to the system to be applied. When the rotational speed deviation ΔR is in the minute range LR, the reference deviation value SR is set such that the absolute value | ΔRav | of the average value ΔRav of the rotational speed deviation ΔR for the predetermined time Δt is less than the predetermined reference deviation value SR. Is set in advance.
As illustrated in FIGS. 1 and 2, in this reference form, the control means (1) includes a rotation speed deviation determination means (2a) and an integration cancellation means (10), and the rotation speed deviation ΔR for a predetermined time Δt. While the absolute value | ΔRav | of the average value ΔRav is below the predetermined reference deviation value SR, the integration canceling means (10) controls based on the determination by the rotational speed deviation determining means (2a). Since the integration of the integral value I by the value calculation means (3) is canceled, the integral value I based on the minute rotation speed deviation does not accumulate, and the periodic rotation speed that has occurred as a result of the control that cancels out this integral value I has occurred. Narrow peaks of fluctuation do not occur. For this reason, it is possible to avoid a narrow peak of periodic rotational speed fluctuation that may occur after the rotational speed deviation falls within the minute range LR.

図2のグラフは、縦軸がエンジン回転数、横軸が時間であり、負荷投入により、実回転数が目標回転数から下降した後、目標回転数に復帰する過程を示しており、所定時間Δtの回転数偏差ΔRの平均値ΔRavの絶対値|ΔRav|が所定の基準偏差値SRを下回っている間は、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルするため、その間、制御値演算手段(3)では、絶対値|ΔRav|が所定の基準偏差値SRを下回った下回り開始時点の積分値Iで制御値の演算を行う。   The graph of FIG. 2 shows a process in which the vertical axis represents the engine speed and the horizontal axis represents time, and the process returns to the target speed after the actual speed decreases from the target speed by applying a load. While the absolute value | ΔRav | of the average value ΔRav of the rotation speed deviation ΔR of Δt is below a predetermined reference deviation value SR, the integration canceling means (10) integrates the integral value I by the control value calculating means (3). In the meantime, in the control value calculation means (3), the control value is calculated with the integral value I at the time of starting to fall below the absolute value | ΔRav | below the predetermined reference deviation value SR.

次に実施形態について説明する。
図3、図4に示すように、制御手段(1)が、積分値変動率判定手段(3a)と、積算キャンセル手段(10)とを備え、制御値演算手段(3)で演算した積分値Iの積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回っている間は、これを積分値変動率判定手段(3a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルする。回転数偏差ΔRの絶対値|R|が微小範囲LRに入っている場合には、制御値演算手段(3)で演算した積分値Iの積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回るように、基準変動率値SIを設定しておく。ΔTは所定時間、ΔIは所定時間ΔTにおける積分値Iの変動値である。
Next, an embodiment will be described.
As shown in FIGS. 3 and 4, the control means (1) includes an integral value fluctuation rate determination means (3a) and an integration cancellation means (10), and the integral value calculated by the control value calculation means (3). While the absolute value | ΔI / ΔT | of the integral value fluctuation rate ΔI / ΔT of I is below a predetermined reference fluctuation rate value SI, it is based on the fact that the integral value fluctuation rate judgment means (3a) has judged this. The integration canceling means (10) cancels the integration of the integral value I by the control value calculating means (3). When the absolute value | R | of the rotational speed deviation ΔR is within the minute range LR, the absolute value | ΔI / ΔT of the integrated value fluctuation rate ΔI / ΔT of the integrated value I calculated by the control value calculating means (3). The reference fluctuation rate value SI is set so that | is less than a predetermined reference fluctuation rate value SI. ΔT is a predetermined time, and ΔI is a fluctuation value of the integral value I at the predetermined time ΔT.

図4のグラフは、縦軸がエンジン回転数、横軸が時間であり、負荷投入により、実回転数が目標回転数から下降した後、目標回転数に復帰する過程を示しており、積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回っている間は、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルするため、その間、制御値演算手段(3)では、絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回った下回り開始時点の積分値Iで制御値の演算を行う。
他の構成は、参考形態と同じであり、図3、4中、参考形態と同じ要素には、図1、図2と同じ符号を付しておく。
The graph of FIG. 4 shows a process in which the vertical axis represents the engine speed and the horizontal axis represents time, and the process returns to the target speed after the actual speed decreases from the target speed by applying a load. While the absolute value | ΔI / ΔT | of the fluctuation rate ΔI / ΔT is below the predetermined reference fluctuation rate value SI, the integration canceling means (10) cancels the integration of the integral value I by the control value calculating means (3). Therefore, in the meantime, in the control value calculation means (3), the control value is calculated with the integral value I at the time of starting to fall below the absolute value | ΔI / ΔT | being lower than the predetermined reference fluctuation rate value SI.
Other configurations are the same as those of the reference embodiment , and in FIGS. 3 and 4, the same reference numerals as those of FIGS.

(1) 制御手段
(2) 回転数偏差演算手段
(2a) 回転数偏差判定手段
(3) 制御値演算手段
(3a) 積分値変動率判定手段
(4) 電流制御部
(5) アクチュエータ駆動回路
(6) アクチュエータ
(7) 燃料噴射ポンプ
(8) 燃料調量部
(9) ディザ電流重畳手段
(10) 積算キャンセル手段
(11) 積分項演算部
Δt 所定時間
ΔR 回転数偏差
|ΔRav| 回転数偏差の平均値の絶対値
SR 基準偏差値
I 積分値
ΔI/ΔT 積分値変動率
|ΔI/ΔT| 積分値変動率の絶対値
SI 基準変動率値
(1) Control means
(2) Speed deviation calculation means
(2a) Speed deviation judging means
(3) Control value calculation means
(3a) Integral value fluctuation rate determination means
(4) Current controller
(5) Actuator drive circuit
(6) Actuator
(7) Fuel injection pump
(8) Fuel metering section
(9) Dither current superposition means
(10) Integration cancellation means
(11) Integral term calculation unit Δt Predetermined time ΔR Rotational speed deviation | ΔRav | Absolute value SR of standard deviation of rotational speed SR Standard deviation value I Integral value ΔI / ΔT Integral value fluctuation rate | ΔI / ΔT | Integral value fluctuation rate Absolute value SI standard fluctuation rate value

Claims (1)

制御手段(1)が、回転数偏差演算手段(2)と、PID制御またはPI制御の制御値演算手段(3)と、電流制御部(4)と、アクチュエータ駆動回路(5)とを備え、回転数偏差演算手段(2)で目標回転数と実回転数との回転数偏差を演算し、この回転数偏差に基づいて、制御値演算手段(3)がPID制御またはPI制御の制御値を演算し、この制御値に基づいて、電流制御部(4)がアクチュエータ駆動回路(5)のアクチュエータ駆動電流を制御し、このアクチュエータ駆動電流でアクチュエータ(6)を駆動し、このアクチュエータ(6)で燃料噴射ポンプ(7)の燃料調量部(8)を調量することにより、回転数偏差ΔRを所定範囲内に収束させるとともに、
制御手段(1)がディザ電流重畳手段(9)を備え、このディザ電流重畳手段(9)でアクチュエータ駆動電流にディザ電流を重畳させるようにした、エンジンの電子ガバナにおいて、
制御手段(1)が、積分値変動率判定手段(3a)と、積算キャンセル手段(10)とを備え、制御値演算手段(3)で演算した積分値Iの積分値変動率ΔI/ΔTの絶対値|ΔI/ΔT|が所定の基準変動率値SIを下回っている間は、これを積分値変動率判定手段(3a)が判定したことに基づいて、積算キャンセル手段(10)が制御値演算手段(3)による積分値Iの積算をキャンセルする、ことを特徴とするエンジンの電子ガバナ。
The control means (1) includes a rotation speed deviation calculation means (2), a control value calculation means (3) for PID control or PI control, a current control section (4), and an actuator drive circuit (5). The rotation speed deviation calculating means (2) calculates the rotation speed deviation between the target rotation speed and the actual rotation speed, and based on this rotation speed deviation, the control value calculation means (3) calculates the control value for PID control or PI control. Based on this control value, the current control section (4) controls the actuator drive current of the actuator drive circuit (5), drives the actuator (6) with this actuator drive current, and this actuator (6) By metering the fuel metering section (8) of the fuel injection pump (7), the rotational speed deviation ΔR is converged within a predetermined range,
In the electronic governor of the engine, the control means (1) includes a dither current superimposing means (9), and the dither current superimposing means (9) superimposes the dither current on the actuator drive current.
The control means (1) includes an integral value fluctuation rate determination means (3a) and an integration cancellation means (10), and the integral value fluctuation rate ΔI / ΔT of the integral value I calculated by the control value calculation means (3). While the absolute value | ΔI / ΔT | is below the predetermined reference fluctuation rate value SI, the integration canceling means (10) controls the control value based on the fact that the integral value fluctuation rate judging means (3a) has judged this. An electronic governor for an engine, wherein the integration of the integral value I by the computing means (3) is canceled.
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