JPS5815620B2 - Diesel engine injection start detection method and device - Google Patents
Diesel engine injection start detection method and deviceInfo
- Publication number
- JPS5815620B2 JPS5815620B2 JP12762777A JP12762777A JPS5815620B2 JP S5815620 B2 JPS5815620 B2 JP S5815620B2 JP 12762777 A JP12762777 A JP 12762777A JP 12762777 A JP12762777 A JP 12762777A JP S5815620 B2 JPS5815620 B2 JP S5815620B2
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- JP
- Japan
- Prior art keywords
- component
- cylinder
- diesel engine
- injection start
- waveform
- Prior art date
- 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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Links
- 238000002347 injection Methods 0.000 title claims description 28
- 239000007924 injection Substances 0.000 title claims description 28
- 238000001514 detection method Methods 0.000 title description 3
- 239000000446 fuel Substances 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims 1
- 239000000284 extract Substances 0.000 claims 1
- 230000003111 delayed effect Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000004397 blinking Effects 0.000 description 3
- 230000010354 integration Effects 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
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- Combined Controls Of Internal Combustion Engines (AREA)
Description
【発明の詳細な説明】
本発明はディーゼルエンジンの噴射始め検出方法及びそ
の装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method and apparatus for detecting the start of injection in a diesel engine.
従来、燃料噴射ポンプを使用したディーゼルエンジンに
おける該ポンプと噴射ノズルとの間の高圧パイプに圧電
素子からなるピックアップを外装して、尚該エンジンの
回転数を検出する方法及び装置はあったが、当該エンジ
ンの噴射始め時期を検出する方法及び装置はなかった。Conventionally, there have been methods and devices for detecting the rotational speed of a diesel engine using a fuel injection pump by mounting a pickup made of a piezoelectric element on a high-pressure pipe between the pump and the injection nozzle. There was no method or device for detecting the injection start timing of the engine.
というのは、上記の如く高圧パイプに圧電素子を外装し
て該パイプに生ずる圧力変化を電気信号として取出した
としても、噴射始め時期に対応する電気信号成分が微弱
で、かつ、多くのノイズが電気信号に含まれているため
に、噴射始め時期成分のみを正確に単離することが困難
であったからである。This is because even if a piezoelectric element is mounted on a high-pressure pipe as described above and the pressure changes occurring in the pipe are extracted as an electrical signal, the electrical signal component corresponding to the injection start time is weak and contains a lot of noise. This is because it is difficult to accurately isolate only the injection start timing component because it is included in the electrical signal.
本発明の目的とするところは上記困難を克服して噴射始
め時期を正確に検出することができるも1のを提供せん
とするにある。SUMMARY OF THE INVENTION An object of the present invention is to overcome the above-mentioned difficulties and to provide a system capable of accurately detecting the injection start timing.
以下図面に即して本発明実施の1例を説明する。An example of implementing the present invention will be described below with reference to the drawings.
第1図は本発明にかかる検出装置のブロック図であり、
第2図は第1図に示した各経路A−Vにおける電気信号
の各波形図を示すものであり、第1、図にしたがって本
発明を順次説明していく。FIG. 1 is a block diagram of a detection device according to the present invention,
FIG. 2 shows each waveform diagram of the electrical signals on each path AV shown in FIG. 1, and the present invention will be sequentially explained according to the first diagram.
(1)まず、第1図に示すように、噴射始め時期を検出
すべきディーゼルエンジンE。(1) First, as shown in FIG. 1, a diesel engine E whose injection start timing should be detected.
の噴射係統、例えば圧力バイブにチタンサンバリウム等
の圧電素子からなるメインピックアップ1及びサブピッ
クアップ2を取付ける。A main pickup 1 and a sub-pickup 2 made of piezoelectric elements such as titanium sambarium are attached to the injection system, for example, a pressure vibrator.
即ち、4気筒e1〜e4からなり、el 、 e3.
e4. e2の順番で各気筒が圧縮−噴射−爆発の1サ
イクルを繰返すディーゼルエンジンの場合には、該エン
ジンの基準気筒となるelの圧力バイブにメインピック
アップ1を、また該基準気筒e1の直前に1サイクルを
行なう前段気筒であるe2の圧力バイブにサブピックア
ップ2をそれぞれ外装して取付ける3(2)エンジンE
。That is, it consists of four cylinders e1 to e4, el, e3.
e4. In the case of a diesel engine in which each cylinder repeats one cycle of compression-injection-explosion in the order of e2, the main pickup 1 is placed on the pressure vibrator of el, which is the reference cylinder of the engine, and the main pickup 1 is placed immediately before the reference cylinder e1. 3 (2) Engine E where the sub-pickup 2 is mounted externally to the pressure vibrator of e2, which is the front stage cylinder that performs the cycle.
.
が稼動すると、メイン及びサブピックアップ1,2は両
気筒el 、 e2の圧力バイブに生ずる圧力変化に対
応して第2図A及びBに示す如き高周波電圧波形を呈す
る電気信号を出力する。When the main and sub-pickups 1 and 2 operate, the main and sub-pickups 1 and 2 output electric signals exhibiting high-frequency voltage waveforms as shown in FIGS. 2A and 2B in response to pressure changes occurring in the pressure vibrators of both cylinders el and e2.
ここで、第2図中、A1は基準気筒e、の圧力バイブに
おいて当該燃料噴射始め時期に生ずる圧力変化に対応し
た噴射始め時期の電気信号成分(以下始め成分という。Here, in FIG. 2, A1 is an electric signal component (hereinafter referred to as the "start component") at the injection start time corresponding to a pressure change that occurs at the fuel injection start time in the pressure vibrator of the reference cylinder e.
)、可は当該燃料噴射直後噴射ノズルの管路を閉塞した
際に圧力バイブにおいて生ずる大きな圧力変化に対応し
た電気信号成分(以下路り成分という。), OK is an electrical signal component corresponding to a large pressure change that occurs in the pressure vibrator when the pipe line of the injection nozzle is closed immediately after the fuel injection (hereinafter referred to as the "road component").
)で電気信号の成分のうち最も顕著である。) is the most prominent component of the electrical signal.
A22 A32A4は他の各気筒e27e32e4にお
ける圧力変化の影響で基準気筒e1の圧力バイブ中に生
ずる圧力変化に対応した各電気信号成分(以下ノイズ成
分という。A22 A32A4 are electrical signal components (hereinafter referred to as noise components) corresponding to pressure changes that occur during the pressure vibration of the reference cylinder e1 due to the influence of pressure changes in the other cylinders e27e32e4.
)である。ノイズ成分はこれらの他に種々内在するが、
それらは省略した。). There are various other noise components in addition to these, but
They have been omitted.
また、B2は前段気筒e2の圧力変化に対応した始め成
分、B2は同じ終り成分、B1. B3. B4は各気
筒el 、 e3. e4のノイズ成分である。Further, B2 is the beginning component corresponding to the pressure change of the front stage cylinder e2, B2 is the same end component, B1. B3. B4 is for each cylinder el, e3. This is the noise component of e4.
そこで本発明においてはAI(始め成分)を確保せんと
するものであるが、これがB10とA′1の間にあり、
しかもX、に近い時点にあることに着目して以下の操作
を行うものである。Therefore, in the present invention, the aim is to secure AI (starting component), which is between B10 and A'1,
Moreover, the following operation is performed by paying attention to the fact that the point is close to X.
メインピックアップ1の上記出力信号は、始め成分A1
及び終り成分A/1の各周波数帯域に対してそれぞれ共
振する異なる周波数帯域を持つ2つのフィルタ3及び4
に、他方、サブピックアップ2の上記出力信号は上記フ
ィルタ4と同等の周波数帯域を持つフィルタ13にそれ
ぞれ入力させる。The above output signal of main pickup 1 has a starting component A1.
and two filters 3 and 4 having different frequency bands that resonate with each frequency band of the end component A/1.
On the other hand, the output signals of the sub-pickup 2 are respectively input to filters 13 having the same frequency band as the filter 4.
(3)−1上記フィルタ4を通過したメインピックアッ
プ1の出力信号AはCの如き終り成分べを強調された波
形となる。(3)-1 The output signal A of the main pickup 1 which has passed through the filter 4 has a waveform such as C, in which the final component is emphasized.
この波形Cを高入力インピーダンスアンプ5で増巾後、
再度具なるフィルタ6でノイズ除去を行なわせ、高入力
インピーダンスアンプ7で増巾させてDの如き波形にさ
せる。After amplifying this waveform C with the high input impedance amplifier 5,
Noise is removed again using a filter 6, and amplified using a high input impedance amplifier 7 to obtain a waveform like D.
この波形りを検波器8、波形整形器9を経てノイズ除去
及び波形を低周波変換させて波形整形し、Eの如き単発
波形にさせ、さらに、該単発パルス波形Eをワンショッ
トマルチバイブレーク10によってFの如き方形波に変
換する。This waveform is passed through a detector 8 and a waveform shaper 9 to remove noise and convert the waveform to a low frequency to shape the waveform into a single waveform like E. Furthermore, the single pulse waveform E is processed by a one-shot multi-by-break 10. Convert to a square wave like F.
■ かくて、この方形波Fは基準気筒e1の終り成分X
1に対応するものであるから、FとFの間隔は該気筒e
1の1サイクルの周期に相当することになる。■Thus, this square wave F is the end component X of the reference cylinder e1.
1, the interval between F and F is equal to that of the cylinder e.
This corresponds to the period of one cycle of 1.
そこで、この方形波Fを電流回路11に入力させ、該回
路11をして気筒e1の周期と等しくなるディーゼルエ
ンジンE。Therefore, this square wave F is inputted into the current circuit 11, and the cycle of the circuit 11 becomes equal to the period of the cylinder e1 in the diesel engine E.
の回転数を出力せしめ、該出力をもって回転計12に当
該回転数を表示させる。The rotational speed is outputted, and the rotational speed is displayed on the tachometer 12 based on the output.
(4)他方、フィルタ13を通過したサブピックアップ
2の出力信号は終り成分紙を強調されたGの如き波形と
なり、続いて、前記(3)−Iと同様に、高入力インピ
ーダンスアンプ14、フィルタ15、アンプ16、検波
器17、波形整形器18及びワンショットマルチバイブ
レーク19をそれぞれ通過して各波形H,Iを経てJの
如き方形波に変換させる。(4) On the other hand, the output signal of the sub-pickup 2 that has passed through the filter 13 becomes a waveform such as G with the final component emphasized, and then, as in (3)-I above, the output signal is passed through the high input impedance amplifier 14 and filtered. 15, an amplifier 16, a detector 17, a waveform shaper 18, and a one-shot multi-by-break 19, and convert the waveforms H and I into square waves such as J.
この方形波Jは前段気筒e2の終り成分B′2に対応す
るものであるから、JとJの間隔は該気筒e2の1サイ
クルの周期に相当することになる。Since this square wave J corresponds to the end component B'2 of the preceding cylinder e2, the interval between J and J corresponds to the period of one cycle of the cylinder e2.
したがって、この方形波Jを使用してもディーゼルエン
ジンE。Therefore, even if this square wave J is used, the diesel engine E.
の回転数を得ることができる。(5)−I 前記(3
)−I及び(4)で得た両方形波F及びJをフリップフ
ロップ20に入力すると、該フリップフロップ20は、
前段気筒e2の終り成分B′2に相当する方形波Jの立
上りでONL、他方の基準気筒e、の終り成分A1に相
当する立上りでOFFして、Kの如き方形波を出力する
。rotation speed can be obtained. (5)-I Above (3)
)-I and both the waveforms F and J obtained in (4) are input to the flip-flop 20, the flip-flop 20 becomes
It turns ON at the rising edge of the square wave J corresponding to the end component B'2 of the preceding cylinder e2, turns OFF at the rising edge corresponding to the end component A1 of the other reference cylinder e, and outputs a square wave like K.
この方形波には前段気筒e2の終り成分から基準気筒e
、の終り成分までの期間に相当するものであって、この
期間中に基準気筒e1の始め成分A1が必ず存在するは
ずである。This square wave includes the end component of the previous stage cylinder e2 to the reference cylinder e.
, and the beginning component A1 of the reference cylinder e1 must exist during this period.
■ この方形波Kを回転同調型積分回路21で積分して
Lの如き三角波を作り、さらに、該三角波りを分割回路
22に入力せしめて前記方形波Kを2分割したMの如き
方形波を作り、該方形波Mを比較制御器23の一方の入
力端へ印加させる。■ This square wave K is integrated by the rotationally tuned integration circuit 21 to create a triangular wave like L, and then this triangular wave is input to the dividing circuit 22 to divide the square wave K into two, which generates a square wave like M. The square wave M is applied to one input terminal of the comparison controller 23.
(6)−I ひるかえって、他方のフィルタ3に入力
した基準気筒e1の出力信号Aは該フィルタ3で始め成
分A1を強調されたNの如き波形となる。(6)-I On the contrary, the output signal A of the reference cylinder e1 inputted to the other filter 3 becomes a waveform such as N in which the component A1 is initially emphasized in the filter 3.
この波形Nを高入力インピーダンスアンプ24及び25
でOの如き波形に増巾し、さらに、検波器26及び波形
整形器27でPの如き波形に検波整形し、該整形波Pを
コンパレータ28に入力させる。This waveform N is converted into high input impedance amplifiers 24 and 25.
The waveform is amplified into a waveform such as O, and further detected and shaped into a waveform such as P by a detector 26 and a waveform shaper 27, and the shaped wave P is input to a comparator 28.
■ このコンパレータ28は、前記(5)−IIの回転
同調型積分回路21から該コンパレータ28に入力され
る積分三角波りと上記■の整形波Pとを比較して、Pの
レベルをLのレベルと同程度にすべく制御回路30によ
り上記Iの高入力インピーダンスアンプ25の増中度を
制御させる。■ This comparator 28 compares the integral triangular wave input to the comparator 28 from the rotation-tuned integration circuit 21 of (5)-II with the shaped wave P of (2) above, and sets the level of P to the level of L. The control circuit 30 controls the degree of increase in the high input impedance amplifier 25 of the above I in order to maintain the same level as the above.
その目的はPの波形のうち特に相並ぶ前方の信号のふら
つきを防止し、常に必要な所定のレベルの安定な波形を
得るためである。The purpose of this is to prevent waveforms in the waveforms of P, especially in the adjacent front signals, and to always obtain a stable waveform at a required predetermined level.
この制御はいわゆるautomatic feed b
ack gain controlと称せられるもので
ある。This control is called automatic feed b.
This is called ack gain control.
■ コンパレータ28で比較判別して調整した整形波P
をさらにアンプ29でQの如き波形に増巾して、該波形
Qをフリップフロップ31及びゲート回路32の各入力
端にそれぞれ印加させる。■ Shaped wave P adjusted by comparing with comparator 28
is further amplified into a waveform such as Q by an amplifier 29, and the waveform Q is applied to each input terminal of a flip-flop 31 and a gate circuit 32, respectively.
(7)シかるに、前記(6)−1のフリップフロップ3
1の他の入力端には前記(3)−1で得られた方形波F
を印加させる。(7) Finally, the flip-flop 3 of (6)-1 above.
1 is connected to the square wave F obtained in (3)-1 above.
is applied.
該フリップフロップ31は波形Qの始め成分A1に当る
立上りでONし、方形波Fの立下りでOFFして、Rの
如き方形波を出力する。The flip-flop 31 turns on at the rising edge of the first component A1 of the waveform Q, turns off at the falling edge of the square wave F, and outputs a square wave like R.
この方形波Rは始め成分A1と終り成分A1との間隔に
相当するものである。This square wave R corresponds to the interval between the starting component A1 and the ending component A1.
次に、この方形波Rを前記(5)−IIの比較制御器2
3における他方の入力端に印加させる。Next, this square wave R is transferred to the comparison controller 2 of (5)-II.
3 to the other input terminal.
18)−I 該比較制御器23は、前記(5)−II
の2分割方形波Mの中に前記(力の方形波Rが重なるか
否かを比較して重なった場合にのみSの如き一定電圧を
前記(6)−1のゲート回路32の入力端に印加させる
。18)-I The comparison controller 23 performs the above (5)-II
It is compared whether or not the force square waves R overlap in the two-divided square wave M, and only when they overlap, a constant voltage such as S is applied to the input terminal of the gate circuit 32 of (6)-1. Apply.
このM内にRが重なるということは、前記(6)−1で
得られた波形Qの持つ始め成分A1がB10とXlとの
中間点とA/1との間にあるということ、すなわち、基
準気筒の終り成分A′1に寄ったところに存在すること
を意味している。The fact that R overlaps within M means that the initial component A1 of the waveform Q obtained in (6)-1 is between A/1 and the midpoint between B10 and Xl, that is, This means that it exists near the end component A'1 of the reference cylinder.
■ 次に、ゲート回路32は、電圧波Sが印加されてい
る時で、かつ、前記(6)−Iの波形Qのパルスが入力
した場合にTの如きトリガ波を出力する。(2) Next, the gate circuit 32 outputs a trigger wave such as T when the voltage wave S is applied and the pulse of the waveform Q of (6)-I is input.
つまり、このゲート回路32は基準気筒e1の始め成分
A1が基準気筒e1の終り成分X1の直前にあると判別
された場合(上記■の比較制御器23による。That is, this gate circuit 32 operates when it is determined that the start component A1 of the reference cylinder e1 is immediately before the end component X1 of the reference cylinder e1 (by the comparison controller 23 in (2) above).
)に限り、当該始め成分に対応したトリガ信号を出力す
るのである。), the trigger signal corresponding to the starting component is output.
■ 続いて、該トリガ波Tをワンショットマルチバイブ
レーク33に入力して基準気筒e1の始め成分に相当す
るトリガ信号でUの如きパルス波を出力させる。(2) Subsequently, the trigger wave T is input to the one-shot multi-by-break 33 to output a pulse wave such as U with a trigger signal corresponding to the starting component of the reference cylinder e1.
この際、パイブレーク33の時定数を適当に定めておけ
ば、始め成分に続く基準気筒e1の終り成分に相当する
トリが信号を除去させることができる。At this time, if the time constant of the pie break 33 is appropriately determined, the signal of the bird corresponding to the end component of the reference cylinder e1 following the start component can be removed.
かくして、基準気筒e1の始め成分はこのパルス信号U
として他のノイズ成分及び終り成分を除去して正確に単
離されたことになる。Thus, the initial component of the reference cylinder e1 is this pulse signal U.
This means that other noise components and end components have been removed and accurately isolated.
(9)−1前記パルス信号波形Uを遅延回路34に入力
して自由に遅延できるようになす。(9)-1 The pulse signal waveform U is input to the delay circuit 34 so that it can be delayed freely.
■ この遅延回路34を経たパルス信号波形Uを反転回
路35で■の如く負電位波形に変換させ、この波形■で
タイミングライト36を点滅させる。(2) The pulse signal waveform U that has passed through the delay circuit 34 is converted into a negative potential waveform as shown in (2) by the inverting circuit 35, and the timing light 36 is made to blink with this waveform (2).
かくして、このタイミングライト36の点滅周期は上記
信号波Uが遅延回路34で遅延されていない場合には基
準気筒e1の燃料噴射始め時期の周期に同期(全く一致
している。Thus, if the signal wave U is not delayed by the delay circuit 34, the blinking cycle of the timing light 36 is synchronized with (exactly coincides with) the cycle of the fuel injection start timing of the reference cylinder e1.
)して繰返えすことになる。) and then repeat.
■ しかるに、通常、ディーゼルエンジン凡のフライホ
イールEfには第一段気筒elの上死点を表示するマー
クmが基準マークMに対向して刻設されている。(2) However, normally, a mark m indicating the top dead center of the first stage cylinder el is engraved on the flywheel Ef of a diesel engine, facing the reference mark M.
そこで、上記■のように遅延させないでタイミングライ
ト36を点滅させた場合には、該点滅が噴射始め時期と
同期しているから上死点マークmは停止して見えるか、
両者が全く一致しているので該マークmは基準マークM
に合わずその手前に停止した状態となる。Therefore, if the timing light 36 is made to blink without delay as in (①) above, the top dead center mark m will appear to have stopped because the blinking is synchronized with the injection start time, or
Since the two match exactly, the mark m is the reference mark M.
The vehicle does not meet this point and comes to a halt before that point.
■ 次に、上記パルス信号波Uを遅延回路34で遅延し
てタイミングライト36の点滅時期を全体的に遅延させ
ていくと、上死点マークmが基準マークMに次第に近づ
いていき、所定の遅延度で両マークm 、 rr(が完
全に一致する。■Next, when the above-mentioned pulse signal wave U is delayed by the delay circuit 34 and the blinking timing of the timing light 36 is delayed as a whole, the top dead center mark m gradually approaches the reference mark M, and a predetermined point is reached. Both marks m and rr (completely match in terms of delay).
■ 上記遅延回路34におけるパルス信号波Uの遅延度
を電流回路37で取出し、その値を遅角メータ38に表
示する。(2) The degree of delay of the pulse signal wave U in the delay circuit 34 is taken out by the current circuit 37, and the value is displayed on the delay angle meter 38.
このメーク38に表示される値は基準気筒e1の噴射始
め時期が該気筒e1の上死点の何度手前にあるかを示す
ものである。The value displayed on the make 38 indicates how many degrees before the top dead center of the reference cylinder e1 the injection start timing is.
以上説明する如く本発明によればディーゼルエンジンの
燃料噴射始め時期を電気信号として検出することができ
る。As described above, according to the present invention, the fuel injection start timing of a diesel engine can be detected as an electrical signal.
しかも、燃料噴射直後Lγ生ずる圧力変化や、他の気筒
による圧力変化等のノイズ成分の影響を完全に除去する
ものとしたので、当該検出が極めて正確である。Furthermore, since the influence of noise components such as pressure changes occurring immediately after fuel injection and pressure changes caused by other cylinders is completely removed, the detection is extremely accurate.
また、電気信号として検出するものであるから、その後
の処理、例えば回転数の表示、遅延角メータによる上死
点に対する位置表示等が極めて簡単に行なうことができ
る。Furthermore, since it is detected as an electrical signal, subsequent processing, such as displaying the number of revolutions and displaying the position relative to top dead center using a delay angle meter, can be performed very easily.
図面は本発明実施の1例を示すもので、第1図は本発明
装置のブロック図、第2図A〜■は第1図に示した各経
路A〜■における各波形図である。
上図中、各符号は次のものを示す。
1:メインピックアップ、2:サブピックアップ、3,
4,13,6,15:フィルタ、5,7゜14.16,
24,25,29:高入力インピーダンスアンプ、8,
17,26:検波器、9゜18.27:波形整形器、1
0,19,33:ワンショットマルチバイブレーク、1
1,37:’を光回路、12:回転計、20,31:フ
リップフロップ、21:回転同調型積分回路器、22:
分割回路、23:比較制御器、28:コンパレータ、3
0:制御回路、32:ゲート回路、34:遅延回路、3
5:反転器、36:タイミングライト、38:遅延角メ
ータ、Eo:ディーゼルエンジン、e1〜e4:ディー
ゼルエンジンの気筒、Ef:フライホイール。The drawings show one example of carrying out the present invention; FIG. 1 is a block diagram of the apparatus of the present invention, and FIGS. In the above figure, each symbol indicates the following. 1: Main pickup, 2: Sub pickup, 3,
4, 13, 6, 15: Filter, 5, 7° 14.16,
24, 25, 29: High input impedance amplifier, 8,
17, 26: Detector, 9° 18.27: Waveform shaper, 1
0, 19, 33: One shot multi-bye break, 1
1, 37:' optical circuit, 12: rotation meter, 20, 31: flip-flop, 21: rotation-tuned integration circuit, 22:
Division circuit, 23: Comparison controller, 28: Comparator, 3
0: Control circuit, 32: Gate circuit, 34: Delay circuit, 3
5: Inverter, 36: Timing light, 38: Delay angle meter, Eo: Diesel engine, e1 to e4: Diesel engine cylinder, Ef: Flywheel.
Claims (1)
き基準気筒と該気筒の直前でサイクルを繰返す前段気筒
とを選定して該一気筒の燃料噴射ノズルに通ずる圧力バ
イブ等に生ずる圧力変化を電気信号として同時に各別に
取出し、基準気筒における始め成分A1が前段気筒にお
ける終り成分B2と基準気筒における終り成分A1との
間にありかつA1がA1に近い時点にあることに着目し
て、前記両路り成分B′2とA′、の時間的間隔を2分
割してそのA1に近い方の2分割時間間隔内に求める始
め成分A1が入っている時に該始め成分A1によるパル
ス電気信号を出力させるようにしたことを特徴とするデ
ィーゼルエンジンの噴射始め検出方法。 2 ディーゼルエンジンの燃料噴射始め時期を検出すべ
き基準気筒と該気筒の直前でサイクルを繰返す前段気筒
とを選定して該一気筒の燃料噴射ノズルに通ずる圧力パ
イ°プ等に生ずる圧力変化を電気信号として同時に各別
に取出す装置と前段気筒における終り成分B2と基準気
筒における終り成分A1との時間的間隔を2分割する装
置と、さらに基準気筒における噴射始め成分A、を検出
しこれが前記路り成分A1に近い方の2分割時間間隔内
に入っている時に該噴射始め成分A1による電気信号を
出力させる装置とを備えたことを特徴とするディーゼル
エンジンの噴射始め検出装置。[Scope of Claims] 1 Select a reference cylinder in which the fuel injection start timing of a diesel engine is to be detected and a pre-stage cylinder whose cycle is repeated immediately before that cylinder, and generate a pressure vibration etc. that communicates with the fuel injection nozzle of the one cylinder. The pressure changes are simultaneously taken out as electrical signals for each separately, noting that the starting component A1 in the reference cylinder is between the ending component B2 in the preceding cylinder and the ending component A1 in the reference cylinder, and that A1 is close to A1. , the time interval between the two path components B'2 and A' is divided into two, and when the desired starting component A1 is included in the two-divided time interval that is closer to A1, the pulse electricity generated by the starting component A1 is generated. A method for detecting the start of injection in a diesel engine, characterized by outputting a signal. 2 Select a reference cylinder in which the timing of starting fuel injection in a diesel engine is to be detected and a pre-stage cylinder that repeats the cycle just before that cylinder, and electrically measure pressure changes occurring in a pressure pipe leading to the fuel injection nozzle of that one cylinder. A device that simultaneously extracts each component as a signal, a device that divides the time interval between the end component B2 in the preceding cylinder and the end component A1 in the reference cylinder into two, and a device that detects the injection start component A in the reference cylinder and detects this as the road component. An apparatus for detecting the start of injection for a diesel engine, comprising: a device for outputting an electric signal according to the injection start component A1 when the injection start component A1 is within a two-divided time interval that is closer to A1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12762777A JPS5815620B2 (en) | 1977-10-26 | 1977-10-26 | Diesel engine injection start detection method and device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12762777A JPS5815620B2 (en) | 1977-10-26 | 1977-10-26 | Diesel engine injection start detection method and device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5462417A JPS5462417A (en) | 1979-05-19 |
| JPS5815620B2 true JPS5815620B2 (en) | 1983-03-26 |
Family
ID=14964752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12762777A Expired JPS5815620B2 (en) | 1977-10-26 | 1977-10-26 | Diesel engine injection start detection method and device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5815620B2 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57212367A (en) * | 1981-06-22 | 1982-12-27 | Hitachi Zosen Corp | Method and apparatus for detecting operation timing in fuel injection system |
| JPS57212366A (en) * | 1981-06-22 | 1982-12-27 | Hitachi Zosen Corp | Method of detecting operation timing in fuel injection series and system therefor |
| JPS58133472A (en) * | 1982-02-04 | 1983-08-09 | Nissan Motor Co Ltd | Fuel injection timing measuring device for diesel engine |
| JPS58174153A (en) * | 1982-04-06 | 1983-10-13 | Nissan Motor Co Ltd | Injection timing sensing device of engine |
| JPS58214667A (en) * | 1982-06-08 | 1983-12-13 | Hitachi Zosen Corp | How to detect fuel injection system operation |
-
1977
- 1977-10-26 JP JP12762777A patent/JPS5815620B2/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5462417A (en) | 1979-05-19 |
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