WO2010044361A1 - Engine rpm control device - Google Patents
Engine rpm control device Download PDFInfo
- Publication number
- WO2010044361A1 WO2010044361A1 PCT/JP2009/067456 JP2009067456W WO2010044361A1 WO 2010044361 A1 WO2010044361 A1 WO 2010044361A1 JP 2009067456 W JP2009067456 W JP 2009067456W WO 2010044361 A1 WO2010044361 A1 WO 2010044361A1
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- WO
- WIPO (PCT)
- Prior art keywords
- engine speed
- injection amount
- fuel injection
- deceleration
- control device
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D31/00—Use of speed-sensing governors to control combustion engines, not otherwise provided for
- F02D31/001—Electric control of rotation speed
- F02D31/007—Electric control of rotation speed controlling fuel supply
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/12—Introducing corrections for particular operating conditions for deceleration
Definitions
- the present invention relates to a technology of an engine speed control device, and more particularly to a technology of an engine speed control device for preventing a rapid deceleration of the engine speed with respect to an accelerator operation during deceleration.
- the engine speed command means is composed of an accelerator, and an intermediate target between the deceleration target and the deceleration target is temporarily set to prevent sudden deceleration of the engine speed in response to accelerator operation during deceleration.
- the structure which decelerates to the target rotation speed is known (for example, refer to Patent Document 1). JP 2000-337195 A
- the intermediate point between the engine speed before deceleration and the engine speed that is the deceleration target is set as the intermediate target when sudden deceleration is performed, the difference between the intermediate target and the engine speed before deceleration still increases and the engine still remains.
- the rotational speed may decrease rapidly.
- the present invention provides an engine speed control device that can prevent a sudden decrease in the engine speed even if the engine speed command means performs a rapid deceleration operation.
- the engine speed command means for commanding the target engine speed, the actual engine speed detection means, the engine speed reduction necessity determination means, and the fuel injection at the time of deceleration request
- the engine speed reduction necessity determining means is configured to determine the target engine speed.
- the fuel injection amount correction means Based on the amount of change with respect to time, it is determined whether or not deceleration is required, and when it is determined that deceleration is required by the engine speed reduction determination means, the fuel injection amount correction means The fuel injection amount is calculated based on the correlation characteristic between the target engine speed and the fuel injection amount stored in advance so that the number is decelerated at a predetermined deceleration rate. It was.
- the predetermined deceleration rate is increased over time from the start to the end of deceleration to decelerate.
- the deceleration request determination is canceled and the target engine speed is released. And it is configured to return to the fuel injection amount control by the fuel injection amount calculation means based on the actual engine speed.
- the fuel injection amount calculation based on the fuel injection amount calculated by the fuel injection amount correction means at the time of the deceleration request after the deceleration request determination, and the target engine speed and the actual engine speed.
- the difference from the fuel injection amount calculated by the means becomes equal to or less than a predetermined value
- the deceleration request determination is canceled, and the fuel injection amount control by the fuel injection amount calculation means based on the target engine speed and the actual engine speed is performed. Configured to return.
- the fuel injection amount is calculated based on the correlation characteristic between the target engine speed and the fuel injection amount, or the deceleration rate of the actual engine speed is multiplied from the start of deceleration to the end. Therefore, selection means is provided for setting whether to calculate the fuel injection amount based on the correlation characteristic between the target engine speed and the fuel injection amount so that the fuel injection amount is increased and decelerated over time.
- the engine speed and the fuel injection amount are set so that the engine speed is decelerated at a predetermined deceleration rate even when the operator performs a rapid deceleration operation with the engine speed command means. Since the fuel injection amount is calculated on the basis of the correlation characteristic, a sudden decrease in the engine speed can be prevented.
- the deceleration rate can be suppressed in the early stage of deceleration, so that a sudden decrease in the engine speed at the start of deceleration can be prevented.
- the operator has performed an operation for stopping the rapid deceleration with the engine speed command means, or the sudden deceleration prevention control has been completed. Can be determined based on the actual engine speed to return to normal engine speed control.
- the operator has performed an operation for stopping the rapid deceleration with the engine speed command means, or the sudden deceleration prevention control has been completed. Can be determined based on the calculation result of the fuel injection amount to return to normal engine speed control.
- the operator can arbitrarily select the deceleration rate characteristic, and even if the engine speed command means performs a rapid deceleration operation, it can prevent a sudden decrease in the engine speed. it can.
- the block diagram which shows the structure of the engine which concerns on the Example of this invention The block diagram which similarly shows signal transmission of dash pod control.
- the graph figure similarly showing transition of dash pod control The graph which similarly shows the correlation of an engine speed and fuel injection quantity.
- FIG. 1 is a block diagram showing a configuration of an engine according to an embodiment of the present invention
- FIG. 2 is a block diagram showing signal transmission of dash pod control
- FIG. 3 is a graph showing transition of dash pod control.
- 4 is a graph showing the correlation between the engine speed and the fuel injection amount
- FIG. 5 is a graph showing the transition of the dash pod control
- FIG. 6 is a graph showing the transition of the dash pod control.
- Engine 100 which is an embodiment of the present invention will be described with reference to FIG.
- Engine 100 is an engine that is mounted on a ship and drives propulsion unit 110 as a marine engine.
- the engine 100 includes an engine body 10 and an engine speed control device 20.
- the engine body 10 is a direct injection four-cylinder diesel engine.
- the output shaft 11 of the engine body 10 is connected to the propulsion unit 110.
- a flywheel 12 is provided on the output shaft 11 of the engine body 10.
- the propulsion unit 110 is a unit that drives the propeller 111 through a transmission mechanism (not shown) by driving the output shaft 11.
- the engine body 10 includes a fuel injection pump 21 and injectors 22, 22, 22, 22.
- the fuel is pumped by the fuel injection pump 21 and injected into each cylinder by the injectors 22, 22, 22, 22.
- the fuel injection pump 21 includes an electronic governor mechanism and includes a rack actuator 43.
- the engine speed control device 20 is a device that performs control (hereinafter, dash pod control) for gradually decreasing the target engine speed for safety when there is a deceleration due to a rapid accelerator operation.
- the engine speed control device 20 is configured by connecting an engine control unit (hereinafter referred to as ECU) 40, an accelerator 41, an engine speed sensor 42, a rack actuator 43, and a dip switch 45 as a selection means. Yes.
- the ECU 40 includes an arithmetic device 50 and a storage device 51.
- the accelerator 41 is provided at the steering seat of the ship. Further, the accelerator 41 has a function of instructing the target engine speed Nset to the ECU 40 as an engine speed command means.
- the engine speed sensor 42 is provided in the vicinity of the flywheel 12.
- the engine speed sensor 42 has a function of detecting the actual engine speed Ne and transmitting it to the ECU 40 as actual engine speed detection means.
- the rack actuator 43 is a device that adjusts the fuel injection amount based on a final target injection amount Qfinal calculated by an injection amount calculation unit 61 described later.
- the dip switch 45 has a function of selecting or setting various functions of the engine 100 as selection means.
- the computing device 50 has functions as an injection amount computing unit 61, a rapid deceleration determining unit 62, a deceleration pattern generating unit 63, and a comparison switching unit 64.
- the injection amount calculation unit 61 has a function as fuel injection amount calculation means based on the deviation between the target engine speed Nset and the actual engine speed Ne. More specifically, the injection amount calculation unit 61 calculates the target injection amount Qgov so that the deviation between the target engine speed Nset and the actual engine speed Ne transmitted by the engine speed sensor 42 becomes zero. It has the function to do.
- the rapid deceleration determination unit 62 has a function as a means for determining whether or not the engine speed needs to be reduced. More specifically, it has a function of determining whether or not a rapid decrease has been made from the decrease rate of the target injection amount Qgov from the injection amount calculation unit 61. That is, when the reduction rate ⁇ Qgov (k ⁇ 1) ⁇ Qgov (k) ⁇ / ⁇ t, which is a change amount of the target injection amount Qgov in a minute time, exceeds the threshold value, the rapid deceleration determination flag is established and turned ON It is.
- the accelerator 41 may be configured to determine whether or not a rapid decrease has been made from the deceleration rate of the target engine speed Nset from the accelerator 41. That is, when the deceleration rate ⁇ Nset (k ⁇ 1) ⁇ Nset (k) ⁇ / ⁇ t, which is the amount of change in the target engine speed Nset in a minute time, exceeds the threshold, the rapid deceleration determination flag is established and turned ON. Is.
- the deceleration pattern generation unit 63 and the comparison switching unit 64 have a function as fuel injection amount correction means when deceleration is requested.
- the deceleration pattern generation unit 63 has a function of calculating a corrected target injection amount Qdp using a predetermined deceleration pattern from the deceleration start injection amount Q1 when the rapid deceleration determination flag is turned on.
- the deceleration start injection amount Q1 is the final target injection amount Qfinal in the previous calculation cycle.
- the engine speed when the fuel injection amount is the deceleration start injection amount Q1 is defined as a deceleration start rotation speed N1. It is also possible to set the target injection amount Qgov in the current calculation cycle.
- the deceleration target injection quantity Qdp is calculated by decelerating in a predetermined deceleration pattern until the descent pod control is canceled by the comparison switching unit 64 described later, using the deceleration start injection quantity Q1 as a base point.
- the deceleration pattern will be described later.
- the comparison switching unit 64 inputs the corrected target injection amount Qdp and the target injection amount Qgov calculated by the deceleration pattern generation unit 63, and sets the final target injection amount Qfinal as a target based on ON / OFF of the rapid deceleration determination flag. It has a function of selecting the injection amount Qgov or the corrected target injection amount Qdp. More specifically, the comparison switching unit 64 selects the corrected target injection amount Qdp as the final target injection amount Qfinal when the rapid deceleration determination flag is ON, and the final target when the rapid deceleration determination flag is OFF. The target injection amount Qgov is selected as the injection amount Qfinal.
- the horizontal axis represents the time axis (t), and the vertical axis represents the corrected target injection amount Qdp or the target injection amount selected as the target engine speed Nset for the upper stage and the final target injection quantity Qfinal for the lower stage. Expressed for Qgov.
- the first deceleration pattern P1 shown in FIG. 3 is a deceleration pattern that calculates the fuel injection amount based on the correlation characteristic between the engine speed and the fuel injection amount so as to keep the deceleration rate of the engine speed at a predetermined rate.
- FIG. 4 shows a correlation characteristic between the engine speed and the fuel injection amount. As shown in FIG. 4, there is a correlation between the engine speed and the fuel injection amount. Specifically, the fuel injection amount is proportional to the cube of the engine speed. Based on the correlation characteristic between the engine speed and the fuel injection amount, first, a deceleration rate of the engine speed is obtained using the first deceleration pattern P1, and then converted into a reduction rate of the injection amount to be a correction target. The injection amount Qdp is calculated.
- the first deceleration pattern P1 is stored in advance in the storage device 51 of the ECU 40 as a map.
- FIG. 5 is used to explain another embodiment of the dash pod control.
- the horizontal axis and the vertical axis are the same as those in FIG.
- the second deceleration pattern P2 indicates that the final target engine speed determined by the operation of the accelerator 41 in the later stage of deceleration so that the final target injection quantity Qfinal follows the correlation characteristics between the engine speed and the fuel injection quantity in the first stage of deceleration when a deceleration request is made.
- This is a deceleration pattern that is calculated by reducing the fuel injection amount at a predetermined rate toward the final fuel injection amount Q2 corresponding to N2.
- the second deceleration pattern P2 is stored in advance in the storage device 51 of the ECU 40 as a map.
- FIG. 6 is used to explain another embodiment of the dash pod control.
- the horizontal axis and the vertical axis are the same as those in FIG.
- the third deceleration pattern P3 shown in FIG. 6 is based on the correlation characteristic between the engine speed and the fuel injection amount so that the engine speed is decelerated by increasing the deceleration rate over time from the start to the end of deceleration. This is a deceleration pattern for calculating the fuel injection amount.
- the third deceleration pattern P3 is stored in advance in the storage device 51 of the ECU 40 as a map.
- FIG. 4 shows a correlation characteristic between the engine speed and the fuel injection amount. As shown in FIG. 4, there is a correlation between the engine speed and the fuel injection amount. Specifically, the fuel injection amount is proportional to the cube of the engine speed. Based on the correlation characteristic between the engine speed and the fuel injection amount, first, a deceleration rate of the engine speed is obtained using the third deceleration pattern P3, and then converted into a reduction rate of the injection amount to be a correction target. The injection amount Qdp is calculated.
- the operator operates the accelerator 41 during the dash pod control and changes the engine speed to a value greater than the final engine speed N2.
- the target engine speed Nset becomes equal to or lower than the final engine speed N2 when the dash pod control is completed.
- the difference between the actual engine speed Ne and the target engine speed Nset is predetermined.
- the rapid deceleration determination flag is turned OFF, the dash pod control is canceled, and the final target injection amount Qfinal is returned to the target injection amount Qgov.
- the difference between the corrected target injection amount Qdp and the target injection amount Qgov is a predetermined value.
- the rapid deceleration determination flag is turned OFF, the dash pod control is canceled, and the final target injection amount Qfinal is returned to the target injection amount Qgov.
- the dash pod control will be described.
- a deceleration pattern in another embodiment either the first deceleration pattern P1 or the third deceleration pattern P3 can be selected. In the selection, the operator can arbitrarily select with the DIP switch 45.
- the operator can arbitrarily select the deceleration rate characteristic of the engine 100 when there is a deceleration due to a rapid accelerator operation, so that the operability of the ship is improved.
- the engine control according to the present invention is not limited to marine applications, and can be effectively used in an engine in which an operator makes a deceleration request at the accelerator 41.
- the engine speed control device of the present invention is industrially useful because it can prevent a sudden decrease in the engine speed even if the engine speed command means performs a rapid deceleration operation.
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Abstract
Description
本発明は、エンジン回転数制御装置の技術に関し、特に、減速時のアクセル操作に対するエンジン回転数の急減速を防止するためのエンジン回転数制御装置の技術に関する。 The present invention relates to a technology of an engine speed control device, and more particularly to a technology of an engine speed control device for preventing a rapid deceleration of the engine speed with respect to an accelerator operation during deceleration.
従来、エンジン回転数指令手段をアクセルで構成し、減速時のアクセル操作に対するエンジン回転数の急減速を防止するために減速前と減速目標との中間目標を一時的に設定して、中間目標回転数に減速した後、目標回転数に減速する構成が公知となっている(例えば、特許文献1参照)。
しかし、急減速を行った場合に減速前のエンジン回転数と減速目標となるエンジン回転数との中間点を中間目標とすると、中間目標と減速前のエンジン回転数との差が大きくなり依然としてエンジン回転数が急減する場合がある。 However, if the intermediate point between the engine speed before deceleration and the engine speed that is the deceleration target is set as the intermediate target when sudden deceleration is performed, the difference between the intermediate target and the engine speed before deceleration still increases and the engine still remains. The rotational speed may decrease rapidly.
そこで、本発明はかかる課題に鑑み、エンジン回転数指令手段で急減速操作を行っても、エンジン回転数の急減を防止することができるエンジン回転数制御装置を提供する。 Therefore, in view of such a problem, the present invention provides an engine speed control device that can prevent a sudden decrease in the engine speed even if the engine speed command means performs a rapid deceleration operation.
本発明のエンジン回転数制御装置においては、目標エンジン回転数を指令するエンジン回転数指令手段と、実エンジン回転数検知手段と、エンジン回転数の減速要否判定手段と、減速要求時の燃料噴射量補正手段と、目標エンジン回転数及び実エンジン回転数に基づく燃料噴射量演算手段と、を有するエンジン回転数制御装置において、前記エンジン回転数の減速要否判定手段は、前記目標エンジン回転数の時間に対する変化量より、減速要否判定を判定し、前記エンジン回転数の減速要否判定手段により減速要と判定された場合には、前記燃料噴射量補正手段は、減速要求時に、実エンジン回転数が所定の減速率で減速するように、予め記憶された目標エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出するように構成した。 In the engine speed control device of the present invention, the engine speed command means for commanding the target engine speed, the actual engine speed detection means, the engine speed reduction necessity determination means, and the fuel injection at the time of deceleration request In the engine speed control device having an amount correction means and a fuel injection amount calculation means based on the target engine speed and the actual engine speed, the engine speed reduction necessity determining means is configured to determine the target engine speed. Based on the amount of change with respect to time, it is determined whether or not deceleration is required, and when it is determined that deceleration is required by the engine speed reduction determination means, the fuel injection amount correction means The fuel injection amount is calculated based on the correlation characteristic between the target engine speed and the fuel injection amount stored in advance so that the number is decelerated at a predetermined deceleration rate. It was.
本発明のエンジン回転数制御装置においては、前記所定の減速率を減速開始から終了に掛けて経時的に増加させて減速する。 In the engine speed control device of the present invention, the predetermined deceleration rate is increased over time from the start to the end of deceleration to decelerate.
本発明のエンジン回転数制御装置においては、前記減速要求判定後に実エンジン回転数と目標エンジン回転数との差が所定値以下となった場合は、前記減速要求判定を解除して目標エンジン回転数及び実エンジン回転数に基づく燃料噴射量演算手段による燃料噴射量制御に復帰するように構成した。 In the engine speed control device of the present invention, when the difference between the actual engine speed and the target engine speed is equal to or less than a predetermined value after the deceleration request determination, the deceleration request determination is canceled and the target engine speed is released. And it is configured to return to the fuel injection amount control by the fuel injection amount calculation means based on the actual engine speed.
本発明のエンジン回転数制御装置においては、前記減速要求判定後に減速要求時の前記燃料噴射量補正手段で算出された燃料噴射量と、目標エンジン回転数及び実エンジン回転数に基づく燃料噴射量演算手段で算出された燃料噴射量との差が所定値以下となった場合は、減速要求判定を解除し、目標エンジン回転数と実エンジン回転数に基づく燃料噴射量演算手段による燃料噴射量制御に復帰するように構成した。 In the engine speed control device of the present invention, the fuel injection amount calculation based on the fuel injection amount calculated by the fuel injection amount correction means at the time of the deceleration request after the deceleration request determination, and the target engine speed and the actual engine speed. When the difference from the fuel injection amount calculated by the means becomes equal to or less than a predetermined value, the deceleration request determination is canceled, and the fuel injection amount control by the fuel injection amount calculation means based on the target engine speed and the actual engine speed is performed. Configured to return.
本発明のエンジン回転数制御装置においては、目標エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出するか、または、実エンジン回転数の減速率を減速開始から終了に掛けて経時的に増加させて減速するように、目標エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出するか、を設定する選択手段を設けた。 In the engine speed control device of the present invention, the fuel injection amount is calculated based on the correlation characteristic between the target engine speed and the fuel injection amount, or the deceleration rate of the actual engine speed is multiplied from the start of deceleration to the end. Therefore, selection means is provided for setting whether to calculate the fuel injection amount based on the correlation characteristic between the target engine speed and the fuel injection amount so that the fuel injection amount is increased and decelerated over time.
本発明のエンジン回転数制御装置においては、操作者がエンジン回転数指令手段で急減速操作を行っても、エンジン回転数が所定の減速率で減速するように、エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出するので、エンジン回転数の急減を防止できる。 In the engine speed control device of the present invention, the engine speed and the fuel injection amount are set so that the engine speed is decelerated at a predetermined deceleration rate even when the operator performs a rapid deceleration operation with the engine speed command means. Since the fuel injection amount is calculated on the basis of the correlation characteristic, a sudden decrease in the engine speed can be prevented.
本発明のエンジン回転数制御装置においては、操作者がエンジン回転数指令手段で急減速操作を行っても、減速初期において減速率を抑制できるので、減速開始時のエンジン回転数の急減を防止できる。 In the engine speed control device of the present invention, even if the operator performs a rapid deceleration operation with the engine speed command means, the deceleration rate can be suppressed in the early stage of deceleration, so that a sudden decrease in the engine speed at the start of deceleration can be prevented. .
本発明のエンジン回転数制御装置においては、エンジン回転数の急減を防止する制御中でも、操作者がエンジン回転数指令手段で急減速を中止する操作を行ったことや急減速防止制御の完了したことを実エンジン回転数に基づいて判定して通常のエンジン回転数制御に戻すことができる。 In the engine speed control device of the present invention, even during the control for preventing a sudden decrease in the engine speed, the operator has performed an operation for stopping the rapid deceleration with the engine speed command means, or the sudden deceleration prevention control has been completed. Can be determined based on the actual engine speed to return to normal engine speed control.
本発明のエンジン回転数制御装置においては、エンジン回転数の急減を防止する制御中でも、操作者がエンジン回転数指令手段で急減速を中止する操作を行ったことや急減速防止制御の完了したことを燃料噴射量の算出結果に基づいて判定して通常のエンジン回転数制御に戻すことができる。 In the engine speed control device of the present invention, even during the control for preventing a sudden decrease in the engine speed, the operator has performed an operation for stopping the rapid deceleration with the engine speed command means, or the sudden deceleration prevention control has been completed. Can be determined based on the calculation result of the fuel injection amount to return to normal engine speed control.
本発明のエンジン回転数制御装置においては、減速率特性を操作者が任意に選択することができ、エンジン回転数指令手段で急減速操作を行っても、エンジン回転数の急減を防止することができる。 In the engine speed control device of the present invention, the operator can arbitrarily select the deceleration rate characteristic, and even if the engine speed command means performs a rapid deceleration operation, it can prevent a sudden decrease in the engine speed. it can.
10 エンジン本体
20 エンジン回転数制御装置
40 ECU
41 アクセル
42 エンジン回転数センサー
45 ディップスイッチ
50 演算装置
51 記憶装置
61 噴射量演算部
62 急減速判定部
63 減速パターン生成部
64 比較切替部
100 エンジン
Nset 目標エンジン回転数
Ne 実エンジン回転数
Qgov 目標噴射量
Qdp 補正目標噴射量
Qfinal 最終目標噴射量
P1 第一減速パターン
P2 第二減速パターン
P3 第三減速パターン
10 Engine
41 accelerator 42
次に、発明の実施の形態を説明する。
図1は本発明の実施例に係るエンジンの構成を示す構成図、図2は同じくダッシュポッド制御の信号伝達を示すブロック線図、図3は同じくダッシュポッド制御の推移を示すグラフ図である。図4は同じくエンジン回転数と燃料噴射量の相関関係を示すグラフ図、図5は同じくダッシュポッド制御の推移を示すグラフ図、図6は同じくダッシュポッド制御の推移を示すグラフ図である。
Next, embodiments of the invention will be described.
FIG. 1 is a block diagram showing a configuration of an engine according to an embodiment of the present invention, FIG. 2 is a block diagram showing signal transmission of dash pod control, and FIG. 3 is a graph showing transition of dash pod control. 4 is a graph showing the correlation between the engine speed and the fuel injection amount, FIG. 5 is a graph showing the transition of the dash pod control, and FIG. 6 is a graph showing the transition of the dash pod control.
図1を用いて、本発明の実施形態であるエンジン100について説明する。エンジン100は、船舶に搭載され、舶用エンジンとして推進ユニット110を駆動するエンジンである。また、エンジン100は、エンジン本体10と、エンジン回転数制御装置20と、を備えている。
The
エンジン本体10は、直噴式4気筒ディーゼルエンジンである。エンジン本体10の出力軸11は、推進ユニット110に接続されている。また、エンジン本体10の出力軸11には、フライホイール12が設けられている。推進ユニット110は、出力軸11の駆動によって図示せぬ伝達機構を介してプロペラ111を駆動するユニットである。
The
エンジン本体10は、燃料噴射ポンプ21と、インジェクタ22・22・22・22と、を備えている。燃料は、燃料噴射ポンプ21によって圧送されてインジェクタ22・22・22・22によって各シリンダー内に噴射される。また、燃料噴射ポンプ21は、電子ガバナ機構から構成され、ラックアクチュエータ43を備えている。
The
エンジン回転数制御装置20は、急激なアクセル操作による減速があった場合に、安全のために目標エンジン回転数を漸減させる制御(以下、ダッシュポッド制御)を実施する装置である。エンジン回転数制御装置20は、Engine Control Unit(以下、ECU)40と、アクセル41と、エンジン回転数センサー42と、ラックアクチュエータ43と、選択手段としてのディップスイッチ45とを接続して構成されている。
ECU40は、演算装置50と、記憶装置51とを備えている。
アクセル41は、船舶の操舵席に設けられている。また、アクセル41は、エンジン回転数指令手段として、ECU40に対して目標エンジン回転数Nsetを指令する機能を有する。
エンジン回転数センサー42は、フライホイール12近傍に設けられている。また、エンジン回転数センサー42は、実エンジン回転数検知手段として、実エンジン回転数Neを検出し、ECU40に送信する機能を有する。
ラックアクチュエータ43は、後述する噴射量演算部61により算出される最終目標噴射量Qfinalに基づいて、燃料噴射量を調整する装置である。
ディップスイッチ45は、選択手段として、エンジン100の諸機能についての選択又は設定を行う機能を有する。
The engine
The ECU 40 includes an
The
The engine speed sensor 42 is provided in the vicinity of the
The
The
図2を用いて、ダッシュポッド制御の信号伝達について説明する。演算装置50は、噴射量演算部61、急減速判定部62、減速パターン生成部63、及び比較切替部64としての機能を備えている。
The signal transmission of the dash pod control will be described with reference to FIG. The
噴射量演算部61は、目標エンジン回転数Nsetと実エンジン回転数Neとの偏差に基づく燃料噴射量演算手段としての機能を有する。より具体的には、噴射量演算部61は、目標エンジン回転数Nsetと、エンジン回転数センサー42によって送信される実エンジン回転数Neと、の偏差が0となるように目標噴射量Qgovを算出する機能を有する。
The injection
急減速判定部62は、エンジン回転数の減速要否判定手段としての機能を有する。より具体的には前記噴射量演算部61からの目標噴射量Qgovの減少率から急激な減少がなされたか否かを判定する機能を有する。すなわち目標噴射量Qgovの微少時間での変化量である減少率{Qgov(k-1)-Qgov(k)}/Δtが閾値を越えたとき、急減速判定フラグを成立させてONにするものである。
The rapid
また、アクセル41からの目標エンジン回転数Nsetの減速率から急激な減少がなされたか否かを判定する構成としても良い。すなわち目標エンジン回転数Nsetの微少時間での変化量である減速率{Nset(k-1)-Nset(k)}/Δtが閾値を越えたとき、急減速判定フラグを成立させてONにするものである。
Further, it may be configured to determine whether or not a rapid decrease has been made from the deceleration rate of the target engine speed Nset from the
減速パターン生成部63及び比較切替部64は減速要求時の燃料噴射量補正手段としての機能を有する。前記減速パターン生成部63は、前記急減速判定フラグがONとなった場合に、減速開始時噴射量Q1から所定の減速パターンを用いて補正目標噴射量Qdpを算出する機能を有する。ここで、減速開始時噴射量Q1とは、前回演算サイクルでの最終目標噴射量Qfinalである。また、燃料噴射量が前記減速開始時噴射量Q1であるときのエンジン回転数を減速開始時回転数N1とする。また、現在演算サイクルでの目標噴射量Qgovとすることも可能である。前記減速開始時噴射量Q1を基点とし、後述する比較切替部64によってダッシュポッド制御を解除するまでの間、所定の減速パターンで減速を行い補正目標噴射量Qdpを算出するものである。ここで減速パターンについては後述する。
The deceleration
比較切替部64は、前記減速パターン生成部63において算出された補正目標噴射量Qdpと目標噴射量Qgovを入力し、急減速判定フラグのON/OFFに基づいて、最終目標噴射量Qfinalとして、目標噴射量Qgov又は補正目標噴射量Qdpを選択する機能を有する。より具体的には、比較切替部64は、急減速判定フラグがONの場合には、最終目標噴射量Qfinalとして補正目標噴射量Qdpを選択し、急減速判定フラグOFFの場合には、最終目標噴射量Qfinalとして目標噴射量Qgovを選択する。
The
図3及び図4を用いて、ダッシュポッド制御の実施例について説明する。図3において、横軸については、時間軸(t)を表し、縦軸については、上段が目標エンジン回転数Nset、下段が最終目標噴射量Qfinalとして選択された補正目標噴射量Qdp又は目標噴射量Qgovについて表されている。 Examples of dash pod control will be described with reference to FIGS. In FIG. 3, the horizontal axis represents the time axis (t), and the vertical axis represents the corrected target injection amount Qdp or the target injection amount selected as the target engine speed Nset for the upper stage and the final target injection quantity Qfinal for the lower stage. Expressed for Qgov.
図3に示す第一減速パターンP1は、エンジン回転数の減速率を所定率に保つように、エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出する減速パターンである。
ここで、図4にエンジン回転数と燃料噴射量との相関特性を示す。図4に示すようにエンジン回転数と燃料噴射量との間には相関関係があり、具体的には燃料噴射量はエンジン回転数の三乗に比例するものである。
このようなエンジン回転数と燃料噴射量との相関特性に基づいて、まず、第一減速パターンP1を用いてエンジン回転数の減速率を求め、その後、噴射量の減少率に換算して補正目標噴射量Qdpを算出するものである。
なお、第一減速パターンP1は、マップとして予めECU40の記憶装置51に記憶されている。
The first deceleration pattern P1 shown in FIG. 3 is a deceleration pattern that calculates the fuel injection amount based on the correlation characteristic between the engine speed and the fuel injection amount so as to keep the deceleration rate of the engine speed at a predetermined rate.
FIG. 4 shows a correlation characteristic between the engine speed and the fuel injection amount. As shown in FIG. 4, there is a correlation between the engine speed and the fuel injection amount. Specifically, the fuel injection amount is proportional to the cube of the engine speed.
Based on the correlation characteristic between the engine speed and the fuel injection amount, first, a deceleration rate of the engine speed is obtained using the first deceleration pattern P1, and then converted into a reduction rate of the injection amount to be a correction target. The injection amount Qdp is calculated.
The first deceleration pattern P1 is stored in advance in the
このようにして、エンジン100の異常検知時には、急激なアクセル操作による減速があった場合にエンジン回転数について、減速率を所定率として減速するため、エンジン100の異常検知時に操作者にとって緩やかな減速感を与えることができる。
In this way, when the
図5を用いて、ダッシュポッド制御の別の実施例について説明する。図5において、横軸及び縦軸については、図3と同様であり説明を省略する。 FIG. 5 is used to explain another embodiment of the dash pod control. In FIG. 5, the horizontal axis and the vertical axis are the same as those in FIG.
第二減速パターンP2は、減速要求時に、減速前期では最終目標噴射量Qfinalはエンジン回転数と燃料噴射量との相関特性に沿うように、減速後期はアクセル41の操作により定まる最終到達エンジン回転数N2に応じた最終到達燃料噴射量Q2に向かって所定の割合で燃料噴射量を減量して算出する減速パターンである。なお、第二減速パターンP2は、マップとして予めECU40の記憶装置51に記憶されている。
The second deceleration pattern P2 indicates that the final target engine speed determined by the operation of the
これにより、減速開始時のエンジン回転数の急減を防止しながらも、最終到達エンジン回転数N2への移行も比較的早期に実現できる。 This makes it possible to achieve the transition to the final engine speed N2 relatively early while preventing a sudden decrease in the engine speed at the start of deceleration.
図6を用いて、ダッシュポッド制御の別の実施例について説明する。図6において、横軸及び縦軸については、図3と同様であり説明を省略する。 FIG. 6 is used to explain another embodiment of the dash pod control. In FIG. 6, the horizontal axis and the vertical axis are the same as those in FIG.
図6に示す第三減速パターンP3は、エンジン回転数が減速率を減速開始から終了に掛けて経時的に増加させて減速するように、エンジン回転数と燃料噴射量との相関特性に基づいて燃料噴射量を算出する減速パターンである。なお、第三減速パターンP3は、マップとして予めECU40の記憶装置51に記憶されている。
The third deceleration pattern P3 shown in FIG. 6 is based on the correlation characteristic between the engine speed and the fuel injection amount so that the engine speed is decelerated by increasing the deceleration rate over time from the start to the end of deceleration. This is a deceleration pattern for calculating the fuel injection amount. The third deceleration pattern P3 is stored in advance in the
ここで、図4にエンジン回転数と燃料噴射量との相関特性を示す。図4に示すようにエンジン回転数と燃料噴射量との間には相関関係があり、具体的には燃料噴射量はエンジン回転数の三乗に比例するものである。
このようなエンジン回転数と燃料噴射量との相関特性に基づいて、まず、第三減速パターンP3を用いてエンジン回転数の減速率を求め、その後、噴射量の減少率に換算して補正目標噴射量Qdpを算出するものである。
FIG. 4 shows a correlation characteristic between the engine speed and the fuel injection amount. As shown in FIG. 4, there is a correlation between the engine speed and the fuel injection amount. Specifically, the fuel injection amount is proportional to the cube of the engine speed.
Based on the correlation characteristic between the engine speed and the fuel injection amount, first, a deceleration rate of the engine speed is obtained using the third deceleration pattern P3, and then converted into a reduction rate of the injection amount to be a correction target. The injection amount Qdp is calculated.
このようにして、エンジン100の異常検知時には、急激なアクセル操作による減速があった場合にエンジン回転数について減速率を経時的に増加させて減速するため、操作者にとって緩やかな減速感を与えることができる。
In this way, when an abnormality is detected in the
なお、ダッシュポッド制御中に操作者が、アクセル41を操作して、最終到達エンジン回転数N2より大きいエンジン回転数に変更する状況が考えられる。また、ダッシュポッド制御が完了することにより目標エンジン回転数Nsetが最終到達エンジン回転数N2以下となる状況が考えられる。
Note that it is conceivable that the operator operates the
そこで、ダッシュポッド制御中にアクセル41が操作されて最終到達エンジン回転数N2が大きくなった結果、またはダッシュポッド制御が完了した結果、実エンジン回転数Neと目標エンジン回転数Nsetとの差が所定値以下となった場合は、急減速判定フラグをOFFにして、ダッシュポッド制御を解除し、最終目標噴射量Qfinalを目標噴射量Qgovに戻すものとしている。
Therefore, as a result of the
また、ダッシュポッド制御中にアクセル41が操作されて最終到達エンジン回転数N2が大きくなった結果、またはダッシュポッド制御が完了した結果、補正目標噴射量Qdpと目標噴射量Qgovとの差が所定値以下となった場合は、急減速判定フラグをOFFにして、ダッシュポッド制御を解除し、最終目標噴射量Qfinalを目標噴射量Qgovに戻すものとしている。
Further, as a result of the
このようにして、ダッシュポッド制御における減速後も、アクセル41操作を有効とできるため、船舶の操作性が向上する。
In this way, since the
さらに、ダッシュポッド制御の別実施例について説明する。別実施例における減速パターンは、第一減速パターンP1又は第三減速パターンP3のいずれかを選択できるものとする。選択にあたっては、前記ディップスイッチ45によって、操作者が任意に選択できるものとしている。
Furthermore, another embodiment of the dash pod control will be described. As a deceleration pattern in another embodiment, either the first deceleration pattern P1 or the third deceleration pattern P3 can be selected. In the selection, the operator can arbitrarily select with the
このようにして、エンジン100の異常検知時には、急激なアクセル操作による減速があった場合にエンジン100の減速率特性を操作者が任意に選択することができるため、船舶の操作性が向上する。
In this manner, when an abnormality is detected in the
なお、本発明に係るエンジン制御は舶用用途に限られるものではなく、アクセル41で操作者が減速要求を行うエンジンにおいて有効に利用できる。
It should be noted that the engine control according to the present invention is not limited to marine applications, and can be effectively used in an engine in which an operator makes a deceleration request at the
本発明のエンジン回転数制御装置は、エンジン回転数指令手段で急減速操作を行っても、エンジン回転数の急減を防止することができるので、産業上有用である。
The engine speed control device of the present invention is industrially useful because it can prevent a sudden decrease in the engine speed even if the engine speed command means performs a rapid deceleration operation.
Claims (5)
前記エンジン回転数の減速要否判定手段は、前記目標エンジン回転数の時間に対する変化量から、減速の要否を判定し、前記エンジン回転数の減速要否判定手段により減速が必要であると判定された場合には、前記燃料噴射量補正手段は、実エンジン回転数が所定の減速率で減速するように、予め記憶された目標エンジン回転数と燃料噴射量との相関特性に基づいて、燃料噴射量を算出することを特徴とするエンジン回転数制御装置。 Engine speed command means for instructing the target engine speed, actual engine speed detection means, engine speed reduction necessity determination means, fuel injection amount correction means for requesting deceleration, target engine speed and actual engine speed detection means An engine speed control device having a fuel injection amount calculation means based on the engine speed,
The engine speed reduction necessity determining means determines whether or not deceleration is necessary from the amount of change of the target engine speed with respect to time, and determines that deceleration is required by the engine speed reduction necessity determination means. When the fuel injection amount is corrected, the fuel injection amount correction means determines the fuel injection amount based on the correlation characteristic between the target engine rotation speed and the fuel injection amount stored in advance so that the actual engine rotation speed is reduced at a predetermined deceleration rate. An engine speed control device that calculates an injection amount.
2. The engine speed control device according to claim 1, wherein the fuel injection amount is calculated based on a correlation characteristic between the target engine speed and the fuel injection amount, or the deceleration rate of the actual engine speed is stopped from the start of deceleration. And a selection means for setting whether to calculate the fuel injection amount based on the correlation characteristic between the target engine speed and the fuel injection amount so as to decelerate by increasing over time. Engine speed control device.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2008-267660 | 2008-10-16 | ||
| JP2008267660A JP2010096092A (en) | 2008-10-16 | 2008-10-16 | Engine speed control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2010044361A1 true WO2010044361A1 (en) | 2010-04-22 |
Family
ID=42106525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2009/067456 Ceased WO2010044361A1 (en) | 2008-10-16 | 2009-10-07 | Engine rpm control device |
Country Status (2)
| Country | Link |
|---|---|
| JP (1) | JP2010096092A (en) |
| WO (1) | WO2010044361A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2012044878A2 (en) | 2010-09-30 | 2012-04-05 | Dow Global Technologies Llc | Container modifications to minimize defects during reactive polyurethane flow |
| WO2012041709A1 (en) | 2010-09-29 | 2012-04-05 | Dow Global Technologies Llc | High functionality aromatic polyesters, polyol blends comprising the same and resultant products therefrom |
| WO2013053555A2 (en) | 2011-10-14 | 2013-04-18 | Dow Global Technologies Llc | Hybrid polyester-polyether polyols for improved demold expansion in polyurethane rigid foams |
| US9580539B2 (en) | 2010-04-21 | 2017-02-28 | Dow Global Technologies Llc | Foam insulation unit |
| WO2021045887A1 (en) | 2019-09-02 | 2021-03-11 | Dow Global Technologies Llc | Rigid polyurethane foam made with a hydrocarbon blowing agent and 1,1,1,4,4,4-hexafluorobut-2-ene |
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| US9580539B2 (en) | 2010-04-21 | 2017-02-28 | Dow Global Technologies Llc | Foam insulation unit |
| WO2012041709A1 (en) | 2010-09-29 | 2012-04-05 | Dow Global Technologies Llc | High functionality aromatic polyesters, polyol blends comprising the same and resultant products therefrom |
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| WO2013053555A2 (en) | 2011-10-14 | 2013-04-18 | Dow Global Technologies Llc | Hybrid polyester-polyether polyols for improved demold expansion in polyurethane rigid foams |
| WO2021045887A1 (en) | 2019-09-02 | 2021-03-11 | Dow Global Technologies Llc | Rigid polyurethane foam made with a hydrocarbon blowing agent and 1,1,1,4,4,4-hexafluorobut-2-ene |
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| Publication number | Publication date |
|---|---|
| JP2010096092A (en) | 2010-04-30 |
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