JP2003184708A - Method for measuring fuel injection start timing in engine - Google Patents

Method for measuring fuel injection start timing in engine

Info

Publication number
JP2003184708A
JP2003184708A JP2001386503A JP2001386503A JP2003184708A JP 2003184708 A JP2003184708 A JP 2003184708A JP 2001386503 A JP2001386503 A JP 2001386503A JP 2001386503 A JP2001386503 A JP 2001386503A JP 2003184708 A JP2003184708 A JP 2003184708A
Authority
JP
Japan
Prior art keywords
fuel injection
fuel
start timing
injection start
pressure
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.)
Granted
Application number
JP2001386503A
Other languages
Japanese (ja)
Other versions
JP3773444B2 (en
Inventor
Manabu Yamanishi
学 山西
Susumu Kubota
奨 窪田
Kengo Adachi
健吾 足達
Kimihiro Yoshida
公博 吉田
Hisao Tsujii
久雄 辻井
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kubota Corp
Original Assignee
Kubota Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Kubota Corp filed Critical Kubota Corp
Priority to JP2001386503A priority Critical patent/JP3773444B2/en
Publication of JP2003184708A publication Critical patent/JP2003184708A/en
Application granted granted Critical
Publication of JP3773444B2 publication Critical patent/JP3773444B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for measuring a fuel injection start timing capable of automatically measuring of fuel injection start timing accurately in a short time and measuring all engines in a line without increasing the number of operators. <P>SOLUTION: A crack shaft is rotated by external power under a condition that fuel is compressed at designated pressure and is fed to a fuel injection pump mounted on a crank case. A change of fuel feeding pressure P nearby a fuel injection start timing is detected by comparing with crankshaft angles θand the fuel injection start timing is measured by automated analysis of detected data. An approximate line L in a fuel feeding pressure rising area and an average value P1 line in a stable pressure after the rise are computed, and a crankshaft angles θs at intersection points of these lines is defined as the fuel injection start timing. <P>COPYRIGHT: (C)2003,JPO

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、ディーゼル型のエ
ンジンに装備される燃料噴射ポンプの燃料噴射開始時期
を計測する方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for measuring a fuel injection start timing of a fuel injection pump mounted on a diesel engine.

【0002】[0002]

【従来の技術】ディーゼル型のエンジンに装備される燃
料噴射ポンプは、クランクケースのポンプ取付座にシム
を介して連結されており、クランクケース側のカム軸軸
心とポンプ取付座との寸法誤差が大きかったり、厚さの
違うシムが組込まれたりすると、カム軸軸心と燃料噴射
ポンプとの寸法距離が変化して燃料噴射開始時期が適正
状態からずれてしまい、排ガスに悪影響をおよぼすこと
になる。そこで、エンジンに燃料噴射ポンプを組付けた
状態で燃料噴射開始時期が許容範囲内にあるか否かを計
測して不良品の摘出を行い、性能の安定したエンジンだ
けを市場に供給するようにしている。
2. Description of the Related Art A fuel injection pump mounted on a diesel engine is connected to a pump mounting seat of a crankcase via a shim, and a dimensional error between a camshaft axial center of the crankcase and the pump mounting seat. If the size is large or a shim with a different thickness is installed, the dimensional distance between the cam shaft axis and the fuel injection pump will change, and the fuel injection start timing will deviate from the proper state, adversely affecting exhaust gas. Become. Therefore, with the fuel injection pump installed in the engine, it is determined whether the fuel injection start timing is within the allowable range, the defective product is extracted, and only the engine with stable performance is supplied to the market. ing.

【0003】従来の燃料噴射開始時期の計測方法はエン
ジン組立てラインとは別にオフラインで行われており、
先ず、シリンダヘッドが組付けられていないエンジンの
ピストン上面にダイヤルゲージを当てた状態でクランク
軸を手動で回転させ、燃料噴射開始時期の基準角度とな
るピストントップ位置を検出する。
The conventional method of measuring the fuel injection start timing is performed off-line separately from the engine assembly line.
First, the crankshaft is manually rotated while the dial gauge is in contact with the upper surface of the piston of the engine in which the cylinder head is not assembled, and the piston top position that is the reference angle of the fuel injection start timing is detected.

【0004】次に、油圧ポンプによって燃料噴射ポンプ
に燃料を所定の圧力で圧送した状態でクランク軸を手動
で回転させ、燃料噴射ポンプの第1気筒出口から燃料が
1秒間に2〜3滴流出することを目視で確認し、その時
のピストントップ位置角度を基準としたクランク軸角度
を燃料噴射開始時期としていた。
Next, the crankshaft is manually rotated while the fuel is pumped to the fuel injection pump by the hydraulic pump at a predetermined pressure, and a few drops of the fuel flow out from the first cylinder outlet of the fuel injection pump per second. That is, the crankshaft angle based on the piston top position angle at that time was used as the fuel injection start timing.

【0005】[0005]

【発明が解決しようとする課題】上記した従来の計測方
向では、1台当たりの計測所要時間が専用治具の脱着を
含めて約5分かかっており、インラインで全台数の計測
を行うためには多くの作業者を必要となるものであっ
た。例えば、タクトタイム50秒のインラインで全数の
計測を行うとすると、5人の増員が必要となるものであ
った。
In the above-mentioned conventional measuring direction, the time required for measurement per one unit is about 5 minutes including the attachment and detachment of the dedicated jig, and it is necessary to measure all the units inline. Required a lot of workers. For example, if the total number is to be measured in-line with a tact time of 50 seconds, it is necessary to increase the number of employees by five.

【0006】また、目視確認による計測形態を採用して
いたために、作業者の感覚によって計測結果にばらつき
(作業者の感覚で±1°以上)が発生しやすく、エンジ
ン品質を向上するためには更に精度の高い計測が望まれ
ている。
Further, since the measurement form by visual confirmation is adopted, the measurement result is likely to vary (± 1 ° or more depending on the operator's feeling) depending on the operator's feeling, and in order to improve the engine quality. Higher precision measurement is desired.

【0007】本発明は、このような点に着目してなされ
たものであって、燃料噴射開始時期の自動計測を短時間
で精度良く行うことができ、多くの作業者の増員を要す
ることなくインラインでの全台数の計測が可能となる燃
料噴射開始時期計測方向を提供することを主たる目的と
するものである。
The present invention has been made paying attention to such a point, and the automatic measurement of the fuel injection start timing can be accurately performed in a short time, without increasing the number of workers. Its main purpose is to provide a fuel injection start timing measurement direction that enables in-line measurement of the total number of fuel injection units.

【0008】[0008]

【課題を解決するための手段】請求項1に係る発明のエ
ンジンの燃料噴射開始時期計測方法は、クランクケース
に組付けられた燃料噴射ポンプに、燃料を所定圧で圧送
した状態でクランク軸を外部動力によって回転させ、燃
料噴射開始時期付近における供給燃料圧力の変化をクラ
ンク軸角度に対比して検出し、検出データの自動解析に
よって燃料噴射開始時期を計測することを特徴とする。
According to a first aspect of the present invention, there is provided a fuel injection start timing measuring method for an engine, wherein a crankshaft is fed to a fuel injection pump assembled in a crankcase while the fuel is being pumped at a predetermined pressure. It is characterized in that it is rotated by external power, a change in the supplied fuel pressure near the fuel injection start timing is detected in comparison with the crankshaft angle, and the fuel injection start timing is measured by automatic analysis of the detection data.

【0009】請求項2に係る発明のエンジンの燃料噴射
時期計測方法は、請求項1の発明において、燃料噴射開
始時期付近における供給燃料圧力の波形解析により燃料
噴射開始時期を計測することを特徴とする。
The fuel injection timing measuring method for an engine according to a second aspect of the present invention is characterized in that, in the first aspect of the invention, the fuel injection start timing is measured by analyzing the waveform of the supplied fuel pressure near the fuel injection start timing. To do.

【0010】請求項3に係る発明のエンジンの燃料噴射
時期計測方法は、請求項2の発明において、供給燃料圧
力の立上り領域の近似直線と、立上り後の圧力安定領域
の平均値直線との交点におけるクランク軸角度を燃料噴
射開始時期とすることを特徴とする。
According to a third aspect of the present invention, there is provided an engine fuel injection timing measuring method according to the second aspect of the invention, wherein an intersection of an approximate straight line of a rising region of the supplied fuel pressure and an average straight line of a pressure stable region after rising. Is used as the fuel injection start timing.

【0011】本発明に係る燃料噴射開始時期計測方法に
よると、クランクケースに組付けられた燃料噴射ポンプ
に、供給燃料圧力の検出手段を備えた燃料供給手段を接
続するとともに、クランク軸の角度計測手段をセットし
て、クランク軸をモータなどの外部駆動手段によって低
速で回転させ、クランク軸角度に対する供給燃料圧力の
変動データを検出収集し、この検出データを自動的に解
析して燃料噴射開始時期を割り出す。
According to the fuel injection start timing measuring method of the present invention, the fuel injection pump assembled to the crankcase is connected to the fuel supply means having the means for detecting the supplied fuel pressure, and the crankshaft angle is measured. Means, the crankshaft is rotated at a low speed by an external drive means such as a motor, and the fluctuation data of the supplied fuel pressure with respect to the crankshaft angle is detected and collected, and the detected data is automatically analyzed to determine the fuel injection start timing. Figure out.

【0012】ここで、図2に示すボッシュ形の燃料噴射
ポンプにおける供給燃料圧力の変動について考察する
と、燃料噴射ポンプ5の燃料供給口bに所定の圧力(リ
リーフ弁で設定)で燃料を供給した状態でポンプ駆動用
のカム23を低速で回転させると、プランジャ24が上
死点まで上昇して1回の燃料送出を終えたのち下降する
行程では、燃料供給管路27の燃料が燃料吸入口aから
プランジャ24内に吸入される燃料吸入段階となるの
で、図9(イ)に示すように、燃料供給管路27の供給
燃料圧力は設定圧力より低くなる。そして、プランジャ
24が上昇行程に入ると、プランジャバレル25の燃料
吸入口aがプランジャ24で次第に閉じられることにな
り、燃料供給管路27の供給燃料圧力は次第に上昇して
ゆく。そして、プランジャ24が燃料吸入口aを完全に
閉じた時点から燃料噴射(圧送)行程となり、プランジ
ャバレル25内に閉じ込められた燃料が加圧され、デリ
バリーバルブを押し開いて送出されてゆく。この燃料噴
射行程においてはプランジャバレル25の燃料吸入口a
はプランジャ24によって閉じられたままとなるので、
燃料供給管路27の供給燃料圧力は設定された圧力に保
たれる。そして、上昇するプランジャ24の傾斜溝が燃
料吸入口aに連通して燃料噴射行程が終了すると、燃料
供給管路27の供給燃料圧力は低下し始める。
Considering the fluctuation of the supplied fuel pressure in the Bosch type fuel injection pump shown in FIG. 2, the fuel is supplied to the fuel supply port b of the fuel injection pump 5 at a predetermined pressure (set by a relief valve). When the cam 23 for driving the pump is rotated at a low speed in this state, the fuel in the fuel supply line 27 is drawn into the fuel intake port during the stroke in which the plunger 24 ascends to the top dead center and finishes one fuel delivery. Since the fuel is sucked into the plunger 24 from a, the fuel pressure supplied to the fuel supply line 27 becomes lower than the set pressure, as shown in FIG. 9A. Then, when the plunger 24 enters the ascending stroke, the fuel inlet a of the plunger barrel 25 is gradually closed by the plunger 24, and the fuel pressure supplied to the fuel supply line 27 gradually increases. Then, the fuel injection (pressure feeding) process starts from the time when the plunger 24 completely closes the fuel intake port a, the fuel trapped in the plunger barrel 25 is pressurized, and the delivery valve is pushed open to be delivered. In this fuel injection stroke, the fuel inlet a of the plunger barrel 25
Remains closed by the plunger 24,
The fuel pressure supplied to the fuel supply line 27 is maintained at the set pressure. Then, when the rising inclined groove of the plunger 24 communicates with the fuel intake port a and the fuel injection stroke ends, the fuel supply pressure in the fuel supply conduit 27 starts to decrease.

【0013】上記した燃料噴射ポンプの作動において、
燃料噴射開始時期はプランジャバレル25の燃料吸入口
aが上昇するプランジャ24によって閉じられた時点で
あり、この時、燃料供給管路27の供給燃料圧力は立上
がりが終了して所定の圧力に安定する時である。つま
り、燃料供給管路27の供給燃料圧力の変動波形を検出
して、圧力の立上がり領域から設定圧力の安定領域への
変曲点Aをとらえれば、その点のクランク軸角度θs が
燃料噴射開始時期となるのである。
In the operation of the above fuel injection pump,
The fuel injection start timing is the time when the fuel intake port a of the plunger barrel 25 is closed by the ascending plunger 24. At this time, the fuel pressure supplied to the fuel supply conduit 27 ends at the rise and stabilizes at a predetermined pressure. It's time. In other words, if the fluctuation waveform of the fuel pressure supplied to the fuel supply line 27 is detected and the inflection point A from the rising region of the pressure to the stable region of the set pressure is detected, the crankshaft angle θs at that point will start fuel injection. It is time.

【0014】しかし、供給燃料圧力の実際の変動波形
は、図9(ロ)に示すように、圧力の立上がり領域から
設定圧力の安定領域への変曲部位は曲線波形となり、か
つ、安定領域の波形も多少の変動を含むものであり、変
曲点を直接に把握することはできないものである。
However, the actual fluctuation waveform of the supplied fuel pressure is, as shown in FIG. 9B, the inflection portion from the rising region of the pressure to the stable region of the set pressure is a curved waveform, and the stable region The waveform also includes some fluctuations, and the inflection point cannot be directly grasped.

【0015】そこで、本発明方法では、立上がり領域の
波形を検出データに基づいた演算によって直線Lに近似
するとともに安定領域の平均値P1 を演算し、得られた
近似直線Lと平均値P1 の直線との交点を求めて前記変
曲点Aとして把握し、この点のクランク軸角度θs を燃
料噴射開始時期としているのである。
Therefore, in the method of the present invention, the waveform of the rising region is approximated to the straight line L by the calculation based on the detected data, the average value P1 of the stable region is calculated, and the obtained straight line of the approximate line L and the average value P1 is calculated. The intersection point with and is grasped as the inflection point A, and the crankshaft angle θs at this point is taken as the fuel injection start timing.

【0016】[0016]

【発明の実施の形態】図1に、本発明による燃料噴射開
始時期計測方法を実施するための概略構成を示すブロッ
ク図であり、図中の1はシリンダヘッドが未だ組付けら
れていないディーゼル・エンジンのクランクケース、2
はクランク軸、3はクランクケース1の複数の気筒に組
込まれたピストン、4は所定の気筒におけるピストン3
の上面に作用する接触式の変位センサ、5はクランクケ
ース1の側部に組付けられた燃料噴射ポンプ、6はクラ
ンク軸2を外部から強制回転させるモータ、7はモータ
5に組付けられたロータリエンコーダなどの回転セン
サ、8は燃料供給タンク、9は燃料供給タンク内の燃料
を燃料噴射ポンプ5に圧送するモータ駆動式の燃料供給
ポンプ、10は燃料供給圧を設定維持するリリーフ弁、
11は圧送される燃料の圧力を検出する圧力センサ、1
2は燃料噴射ポンプ4における所定の気筒出口4aから
送出された燃料を回収する燃料回収タンク、13は燃料
還元用ポンプ、14は燃料フィルタ、であり、前記変位
センサ4、圧力センサ11、および、ロータリエンコー
ダ7からの検出データがD/ A変換器15、アンプ16
を介してマイコン利用の演算装置17にそれぞれ入力さ
れるようになっている。
1 is a block diagram showing a schematic configuration for carrying out a fuel injection start timing measuring method according to the present invention, in which 1 denotes a diesel engine to which a cylinder head is not yet attached. Engine crankcase, 2
Is a crankshaft, 3 is a piston incorporated in a plurality of cylinders of the crankcase 1, and 4 is a piston 3 in a predetermined cylinder.
Of the contact type acting on the upper surface of the fuel cell, 5 is a fuel injection pump mounted on the side of the crankcase 1, 6 is a motor for forcibly rotating the crankshaft 2 from the outside, and 7 is mounted on the motor 5. A rotation sensor such as a rotary encoder, 8 is a fuel supply tank, 9 is a motor-driven fuel supply pump that pumps the fuel in the fuel supply tank to the fuel injection pump 5, and 10 is a relief valve that sets and maintains the fuel supply pressure,
Reference numeral 11 is a pressure sensor for detecting the pressure of the fuel to be pumped, 1
Reference numeral 2 is a fuel recovery tank for recovering fuel delivered from a predetermined cylinder outlet 4a of the fuel injection pump 4, 13 is a fuel reduction pump, 14 is a fuel filter, and the displacement sensor 4, the pressure sensor 11, and The detection data from the rotary encoder 7 is the D / A converter 15 and the amplifier 16.
Are input to the arithmetic unit 17 using the microcomputer via.

【0017】図2に、前記燃料噴射ポンプ5の概略構造
が示されている。燃料噴射ポンプ5は、クランクケース
1の一部に形成された取付座に噴射時期調整用のガスケ
ットシム21を介して搭載連結されるとともに、クラン
クケー1ス内に支承したカム軸22が図示しないクラン
ク軸2にギヤ連動されている。燃料噴射ポンプ5自体は
周知のボッシュ形のものが利用されており、カム軸22
に備えたカム23の回転によってプランジャ24が押し
上げ駆動されることで、プランジャ24がプランジャバ
レル25の燃料吸入口aを遮断した時点からプランジャ
バレル25内の燃料Fが加圧され、デリバリーバルブ2
6を押し開いて送出されるものであり、プランジャ24
がプランジャバレル25の燃料吸入口aを遮断した時点
が噴射開始時期となっている。
FIG. 2 shows a schematic structure of the fuel injection pump 5. The fuel injection pump 5 is mounted and connected to a mounting seat formed in a part of the crankcase 1 via a gasket shim 21 for adjusting injection timing, and a camshaft 22 supported in the crankcase 1 is not shown. It is geared to the crankshaft 2. As the fuel injection pump 5 itself, a well-known Bosch type is used.
When the plunger 24 is pushed up by the rotation of the cam 23 provided for the plunger 24, the fuel F in the plunger barrel 25 is pressurized from the time when the plunger 24 blocks the fuel intake port a of the plunger barrel 25, and the delivery valve 2
6 is pushed out and delivered, and the plunger 24
The injection start time is when the fuel intake port a of the plunger barrel 25 is blocked.

【0018】この発明は、上記噴射開始時期を自動計測
するための方法であり、以下にその詳細を図7のフロー
チャートを参照しながら説明する。
The present invention is a method for automatically measuring the above injection start timing, and the details thereof will be described below with reference to the flowchart of FIG.

【0019】先ず、ワークとしてのクランクケース1
は、クランク軸2、ピストン3群、燃料噴射ポンプ5、
カム軸22、および、カム軸駆動用のギヤ類が組付けら
れるとともに、シリンダヘッドが組付けられていない上
方開放状態でエンジン組立てライン中の計測エリアに搬
入されてくる。ワークが所定の位置に到着すると、自動
的にクランク軸2の軸端にカップリング18を介してモ
ータ6が接続されるとともに、燃料噴射ポンプ5の燃料
供給口bおよび燃料送出口cに燃料供給管27および燃
料回収管28が作業者によって接続される。また、計測
用に予め設定してある気筒(例えば第1気筒)の上に変
位センサ4が搬入され、その気筒のピストン3の上面に
変位センサ4の検出端が下降接触される。
First, the crankcase 1 as a work
Is a crankshaft 2, a group of pistons 3, a fuel injection pump 5,
The camshaft 22 and the gears for driving the camshaft are assembled, and the camshaft 22 is carried into the measurement area in the engine assembly line in an upper open state where the cylinder head is not assembled. When the work reaches a predetermined position, the motor 6 is automatically connected to the shaft end of the crankshaft 2 via the coupling 18, and the fuel is supplied to the fuel supply port b and the fuel delivery port c of the fuel injection pump 5. The pipe 27 and the fuel recovery pipe 28 are connected by an operator. Further, the displacement sensor 4 is carried into a cylinder (for example, the first cylinder) preset for measurement, and the detection end of the displacement sensor 4 is brought into downward contact with the upper surface of the piston 3 of the cylinder.

【0020】次に、モータ6によってクランク軸2が低
速(例えば10rpm )で回転され計測が開始される。ク
ランク軸2が回転されるのに伴って上下に変位するピス
トン3の上面高さが計測されるとともに、クランク軸2
の角度θが回転センサ7で計測され(♯1)、ピストン
3が上限に到達した時点のクランク軸角度(ピストント
ップ位置角度θ0 )が演算により割り出される(♯
2)。なお、図8に示すように、ピストントップ位置角
度θ0 は、ピストントップ位置付近において同一の高さ
検出値をもたらすクランク軸角度θ1 ,θ2 の2等分位
置として算出される。
Next, the crankshaft 2 is rotated at a low speed (for example, 10 rpm) by the motor 6, and the measurement is started. The height of the upper surface of the piston 3, which is displaced vertically as the crankshaft 2 is rotated, is measured, and
Is measured by the rotation sensor 7 (# 1), and the crankshaft angle (piston top position angle θ0) at the time when the piston 3 reaches the upper limit is calculated (#).
2). As shown in FIG. 8, the piston top position angle θ0 is calculated as a bisected position of the crankshaft angles θ1 and θ2 that provide the same height detection value near the piston top position.

【0021】ピストントップ位置角度θ0 が検出される
と、燃料を所定の圧(例えば30kgf/cm2)で圧送しなが
らクランク軸2を低速(例えば10rpm )で回転させ、
燃料噴射開始時期前後の範囲での供給燃料の圧力変化
を、クランク軸角度に対比させて圧力センサ11で検出
し、この検出データの以下の波形解析によって噴射開始
時期を割り出す。
When the piston top position angle θ 0 is detected, the crankshaft 2 is rotated at a low speed (eg 10 rpm) while the fuel is being pumped at a predetermined pressure (eg 30 kgf / cm 2 ),
The pressure change of the supplied fuel in the range before and after the fuel injection start timing is detected by the pressure sensor 11 in comparison with the crankshaft angle, and the injection start timing is determined by the following waveform analysis of the detection data.

【0022】先ず、計測開始角度から計測終了角度まで
の噴射開始時期計測範囲において、クランク軸角度θと
供給燃料圧力Pとがサンプリングされ(♯3)、サンプ
リングされた供給燃料圧力データは予め設定したポイン
ト数(例えば31ポイント)で移動平均され、図3に示
す変動波形が求められる(♯4)。
First, the crankshaft angle θ and the supplied fuel pressure P are sampled (# 3) in the injection start timing measurement range from the measurement start angle to the measurement end angle, and the sampled supply fuel pressure data is set in advance. The moving average is calculated by the number of points (for example, 31 points), and the fluctuation waveform shown in FIG. 3 is obtained (# 4).

【0023】次に、供給燃料圧力Pが立上り変化する領
域を過ぎた後の圧力変化が比較的安定している領域にお
ける定範囲(平均値取得角度範囲)の供給燃料圧力の平
均値P1 が演算される(♯5)。なお、この場合、燃料
噴射ポンプ5のコントロールラック(図示せず)は任意
の位置でもよいが、コントロールラックを最大燃料供給
量位置にセットしてプランジャの有効ストロークを長く
とることで、平均値取得角度範囲を長く得て平均演算処
理を精度よく行うことができる。
Next, an average value P1 of the supplied fuel pressures in a constant range (average value acquisition angle range) is calculated in a region where the pressure change after the supplied fuel pressure P rises and changes is relatively stable. (# 5). In this case, the control rack (not shown) of the fuel injection pump 5 may be located at any position, but by setting the control rack at the maximum fuel supply amount position and lengthening the effective stroke of the plunger, the average value can be obtained. It is possible to obtain a long angle range and accurately perform the average calculation process.

【0024】次に、供給燃料圧力Pの立上り変化する領
域での波形を直線近似するための演算を行う。この演算
においては、前記平均値P1 から予め設定した圧力差分
づつ差し引いた値が近似直線計算用圧力として設定した
ポイント数(例えば6ポイント)求め、各ポイントごと
のクランク軸角度を読み込む(♯6)。次に、最小2乗
法を用いて供給燃料圧力Pの立上り領域での近似直線L
を以下のように演算する(♯7)。
Next, an operation for linearly approximating the waveform in the region where the supply fuel pressure P rises and changes is performed. In this calculation, a value obtained by subtracting the preset pressure difference from the average value P1 is obtained as the number of points (for example, 6 points) set as the approximate straight-line calculation pressure, and the crankshaft angle for each point is read (# 6). . Next, using the method of least squares, the approximate straight line L in the rising region of the supplied fuel pressure P
Is calculated as follows (# 7).

【0025】すなわち、クランク軸角度をx軸、供給燃
料圧力をy軸とし、サンプリングした6ポイントのクラ
ンク軸角度xと近似直線計算用圧力yをそれぞれ、 ( x1 ,y1),( x2 ,y2),( x3 ,y3),( x4 ,
y4),( x5 ,y5),( x6 ,y6) 近似直線Lの式を y= kx+ y0 とすると、比例定数
kおよびy軸切片y0は、 k =(6・ C1-A2・C2 )/ (6・ A1-A22) y0=(A3・C2-A2・C1 )/ (6・ A1-A22) となる。ここで、A1 ,A2 ,C1 ,C2 は次式から求
めることができる。 A1=x12+x22+ x32+ x42+ x52+ x62 A2=x1+x2+x3+x4+x5+x6 C1=x1・y1+x2・y2+x3・y3+x4・y4+x5・y5+x6・y
6 C2=y1+y2+y3+y4+y5+y6
That is, with the crankshaft angle as the x-axis and the supplied fuel pressure as the y-axis, the sampled 6-point crankshaft angle x and the approximate straight-line calculation pressure y are (x1, y1), (x2, y2), respectively. , (X3, y3), (x4,
y4), (x5, y5), (x6, y6) If the equation of the approximate straight line L is y = kx + y0, the proportional constant k and the y-axis intercept y0 are k = (6 · C1-A2 · C2) / (6 · A1−A2 2 ) y 0 = (A3 · C2−A2 · C1) / (6 · A1−A2 2 ) Here, A1, A2, C1 and C2 can be obtained from the following equations. A1 = x1 2 + x2 2 + x3 2 + x4 2 + x5 2 + x6 2 A2 = x1 + x2 + x3 + x4 + x5 + x6 C1 = x1 ・ y1 + x2 ・ y2 + x3 ・ y3 + x4 ・ y4 + x5 / y5 + x6 / y
6 C2 = y1 + y2 + y3 + y4 + y5 + y6

【0026】以上のようにして近似直線Lが求められる
と、この近似直線Lのy値に上記平均値P1 を代入し、
その時の近似直線Lのx値を求め、このx値(クランク
軸角度)を燃料噴射開始時期θs とするのである(♯
8)。
When the approximate straight line L is obtained as described above, the average value P1 is substituted for the y value of the approximate straight line L,
The x value of the approximate straight line L at that time is obtained, and this x value (crankshaft angle) is used as the fuel injection start timing θs (#
8).

【0027】以上の計測方法を用いた燃料噴射開始時期
計測テストの結果を以下に例示する。図6は、計測条件
を示す図表であり、ガスケットシム21の厚さを4種類
(0.5mm,0.55mm,0.6mm,0.75mm )に変えるとともに、供
給燃料圧力を28〜32kgf/cm2 の範囲で3段階に変え
て行っている。また、図5は、供給燃料圧力の変動波形
の実測データ、また、図6は、テスト結果を示してい
る。なお、参考のために従来の目視計測も同時に行って
おり、この目視計測には、図1において、燃料回収管路
28中に設けた透明筒部29を目視して、燃料が1秒間
に2〜3滴流下し始めたことが確認された時点を燃料噴
射開始時期としており、図6のデータは、同一条件で複
数回目視計測を行って平均したものである。
The results of the fuel injection start timing measurement test using the above measuring method will be illustrated below. FIG. 6 is a chart showing the measurement conditions, in which the thickness of the gasket shim 21 is changed to four types (0.5 mm, 0.55 mm, 0.6 mm, 0.75 mm) and the supply fuel pressure is in the range of 28 to 32 kgf / cm 2 . I am changing it in 3 steps. Further, FIG. 5 shows the measured data of the fluctuation waveform of the supplied fuel pressure, and FIG. 6 shows the test result. For reference, the conventional visual measurement is also performed at the same time. For this visual measurement, the transparent tubular portion 29 provided in the fuel recovery conduit 28 is visually observed in FIG. The fuel injection start timing is the time when it is confirmed that the flow of 3 to 3 drops has started to flow, and the data in FIG. 6 is the average obtained by performing visual measurement a plurality of times under the same conditions.

【0028】テストの結果をみると、燃料供給圧力を2
8〜32kgf/cm2 で変化させても、燃料噴射開始時期の
自動計測精度を確保できることが認識できた。また、シ
ム厚さを変えることで燃料噴射開始時期が変化するが、
同じシム厚さの場合には燃料供給圧力波形のばらつきは
極めて小さいことが確認された。
The test result shows that the fuel supply pressure is 2
It was recognized that automatic measurement accuracy of the fuel injection start timing can be ensured even if the fuel injection rate is changed at 8 to 32 kgf / cm 2 . Also, the fuel injection start timing changes by changing the shim thickness,
It was confirmed that the variation of the fuel supply pressure waveform was extremely small when the shim thickness was the same.

【0029】[0029]

【発明の効果】以上の説明から明らかなように、本発明
方法によれば、作業者は計測用器材の脱着操作、あるい
は、それの補助を行うだけで、計測演算はすべて自動で
行うので、1台当たりの測所要時間は短いものとなり、
インラインに導入しても計測のための作業者の増員は少
なくてすむ。しかも、計測そのものに人的要因が含まれ
ないので精度の高い計測が可能となり、エンジンの品質
向上および品質安定化に有効となる。
As is apparent from the above description, according to the method of the present invention, the operator only performs the detaching operation of the measuring instrument or the assist thereof, and all the measurement calculations are automatically performed. The time required for measurement per unit is short,
Even if it is introduced inline, the number of workers for measurement can be reduced. Moreover, since the measurement itself does not include human factors, highly accurate measurement is possible, which is effective for improving the quality and stabilizing the quality of the engine.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明方法を実施する計測構造の概略構成図FIG. 1 is a schematic configuration diagram of a measurement structure for carrying out the method of the present invention.

【図2】燃料噴射ポンプの一部を示す縦断面図FIG. 2 is a vertical sectional view showing a part of a fuel injection pump.

【図3】供給燃料圧力の変動波形を示す線図FIG. 3 is a diagram showing a fluctuation waveform of supply fuel pressure.

【図4】計測テストの条件を示す図表[Figure 4] Chart showing the conditions of measurement test

【図5】各種条件のもとに実測された供給燃料圧力の変
動波形を示す線図
FIG. 5 is a diagram showing fluctuation waveforms of the supplied fuel pressure actually measured under various conditions.

【図6】測定テストの結果を示す図表FIG. 6 is a chart showing the results of measurement tests.

【図7】燃料噴射開始時期検出用の基本フローチャートFIG. 7 is a basic flowchart for detecting fuel injection start timing.

【図8】ピストントップ位置検出手段を説明する線図FIG. 8 is a diagram illustrating a piston top position detecting means.

【図9】(イ)供給燃料圧力の理論上の変動波形 (ロ)供給燃料圧力の実際の変動波形FIG. 9 (a) The theoretical fluctuation waveform of the supplied fuel pressure (B) Actual fluctuation waveform of supplied fuel pressure

【符号の説明】[Explanation of symbols]

1 クランクケース 2 クランク軸 5 燃料噴射ポンプ P 燃料供給圧力 P1 平均値 L 近似直線 θ クランク軸角度 θs クランク軸角度(燃料噴射開始時期) 1 crankcase 2 crankshaft 5 Fuel injection pump P Fuel supply pressure P1 average value L approximate straight line θ Crankshaft angle θs Crankshaft angle (fuel injection start timing)

───────────────────────────────────────────────────── フロントページの続き (72)発明者 足達 健吾 大阪府堺市石津北町64番地 株式会社クボ タ堺製造所内 (72)発明者 吉田 公博 大阪府堺市石津北町64番地 株式会社クボ タ堺製造所内 (72)発明者 辻井 久雄 大阪府堺市石津北町64番地 株式会社クボ タ堺製造所内 Fターム(参考) 3G084 BA15 CA00 DA21 DA27 FA17 FA38    ─────────────────────────────────────────────────── ─── Continued front page    (72) Inventor Kengo Adachi             64 Ishizukitamachi, Sakai City, Osaka Prefecture Kubo Co., Ltd.             Ta Sakai Factory (72) Inventor Kimihiro Yoshida             64 Ishizukitamachi, Sakai City, Osaka Prefecture Kubo Co., Ltd.             Ta Sakai Factory (72) Inventor Hisao Tsujii             64 Ishizukitamachi, Sakai City, Osaka Prefecture Kubo Co., Ltd.             Ta Sakai Factory F-term (reference) 3G084 BA15 CA00 DA21 DA27 FA17                       FA38

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 クランクケースに組付けられた燃料噴射
ポンプに、燃料を所定圧で圧送した状態でクランク軸を
外部動力によって回転させ、燃料噴射開始時期付近にお
ける供給燃料圧力の変化をクランク軸角度に対比して検
出し、検出データの自動解析によって燃料噴射開始時期
を計測することを特徴とするエンジンの燃料噴射開始時
期計測方法。
1. A fuel injection pump mounted on a crankcase, wherein a crankshaft is rotated by an external power in a state where fuel is pumped at a predetermined pressure, and a change in supplied fuel pressure near a fuel injection start timing is measured by a crankshaft angle. The method for measuring the fuel injection start timing of an engine, characterized by measuring the fuel injection start timing by automatically analyzing the detected data.
【請求項2】 燃料噴射開始時期付近における供給燃料
圧力の波形解析により燃料噴射開始時期を計測すること
を特徴とする請求項1記載のエンジンの燃料噴射開始時
期計測方法。
2. The fuel injection start timing measuring method for an engine according to claim 1, wherein the fuel injection start timing is measured by analyzing a waveform of the supplied fuel pressure in the vicinity of the fuel injection start timing.
【請求項3】 供給燃料圧力の立上り領域の近似直線
と、立上り後の圧力安定領域の平均値直線との交点にお
けるクランク軸角度を燃料噴射開始時期とすることを特
徴とする請求項2記載のエンジンの燃料噴射開始時期計
測方法。
3. The crankshaft angle at the intersection of the approximate straight line of the rising region of the supplied fuel pressure and the average straight line of the pressure stable region after rising is used as the fuel injection start timing. Engine fuel injection start timing measurement method.
JP2001386503A 2001-12-19 2001-12-19 Engine fuel injection start timing measurement method Expired - Lifetime JP3773444B2 (en)

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Application Number Priority Date Filing Date Title
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JP2003184708A true JP2003184708A (en) 2003-07-03
JP3773444B2 JP3773444B2 (en) 2006-05-10

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008128152A (en) * 2006-11-24 2008-06-05 Nissan Diesel Motor Co Ltd Inspection device for fuel injection device for vehicle
CN103541847A (en) * 2013-10-19 2014-01-29 福州大学 Method and device for discriminating oil injection time of diesel engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008128152A (en) * 2006-11-24 2008-06-05 Nissan Diesel Motor Co Ltd Inspection device for fuel injection device for vehicle
CN103541847A (en) * 2013-10-19 2014-01-29 福州大学 Method and device for discriminating oil injection time of diesel engine
CN103541847B (en) * 2013-10-19 2015-11-18 福州大学 A kind of diesel engine oil injection time method of discrimination and device

Also Published As

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