JPH04128532A - Fuel supply controller of internal combustion engine - Google Patents
Fuel supply controller of internal combustion engineInfo
- Publication number
- JPH04128532A JPH04128532A JP24776090A JP24776090A JPH04128532A JP H04128532 A JPH04128532 A JP H04128532A JP 24776090 A JP24776090 A JP 24776090A JP 24776090 A JP24776090 A JP 24776090A JP H04128532 A JPH04128532 A JP H04128532A
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- engine
- intake pipe
- atmospheric pressure
- amount
- 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
Links
Landscapes
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
(L楽土の利用分野)
本発明は、内燃エンジンの燃料供給制御装置に関し、特
に大気圧の影響を受1′jずにスピードデンシティ方式
により燃料供給量を正確に決定するようにし、た内燃ニ
シジンの燃料供給制御装置に関する5、
(従来の技術)
従来、内燃エンシ゛ンの燃料供給量を決定する方式とし
て、吸気管内圧力とエンジン回転数とに基づいて基本燃
料量を算出する、いわゆるスピードデンシティ方式があ
る。Detailed Description of the Invention (Field of Application of L-Rakudo) The present invention relates to a fuel supply control device for an internal combustion engine, and in particular, the present invention relates to a fuel supply control device for an internal combustion engine. 5. Related to the fuel supply control device for internal combustion engine There is a so-called speed density method.
この方式は、第5図に示すように、エンジン回転数を一
定とした場合、吸気管内圧力(負圧)P8とエンジンの
充填効率ηυとの関係が比例関係にあることを利用した
ものであり、あらかじめ記憶手段に記憶されたマツプよ
り吸気管内圧力とエンジン回転数とに応じた燃料の基本
量を検索し、それに応じてエンジンへの燃料供給を行う
ものである。As shown in Figure 5, this method takes advantage of the fact that when the engine speed is constant, there is a proportional relationship between the intake pipe pressure (negative pressure) P8 and the engine charging efficiency ηυ. , the basic amount of fuel corresponding to the intake pipe internal pressure and engine speed is retrieved from a map stored in advance in the storage means, and fuel is supplied to the engine accordingly.
第5図のP8−ηυ特性は、第6図に示す通常タイプの
工ンジ〉、即ち、各気筒51〜54と接続された吸気管
5 ]、 a −54aの集合部55の上流に、スロッ
トル弁56が一つだけ設けられたエンジンにおいて得ら
れる特性でと)る。この従来のエンジンでは、絞り57
を介して集合部55に連通した圧力センサ58によって
、吸気管(集合管)内絶対圧P8を検出している。The P8-ηυ characteristic in FIG. 5 is based on the normal type engine shown in FIG. This is a characteristic obtained in an engine provided with only one valve 56). In this conventional engine, the aperture 57
Absolute pressure P8 inside the intake pipe (collecting pipe) is detected by a pressure sensor 58 that communicates with the collecting part 55 via the intake pipe (collecting pipe).
スロットル弁56の下流側集合部の内部は、大きい容積
のチャンバを有するサージタンクを成しており、従って
その内部の圧力PIIの脈動変化は小さい。このため、
エンジン回転数や空燃比を一定とすれば、充填効率ηt
1(σ基本燃料量)は集合管内圧力pHに略比例した状
態に保たれる。また、大気圧PAが変化した場合(例え
ば高地での運転時)でもスロットル弁全開時(WOT)
の圧力I)いが大気圧PAの低下により低くなる(P、
#PA)だけで、WOT時はもとより、その他の運転状
態でも充填効率+71+と吸気管内圧力Y)8との比例
関係は保たれたままである。従って、かかる通常タイプ
の工〉ジンには」一連のスピードデンシティ方式を適用
することが出来、また、大気圧PAの変化があっても、
それによる排気圧の変化(例えば、内部排気還流(EG
R)量の変化)による影響を無視すれば、大気圧PAの
変化による充填効率ηi)の変化は無く、従って大気圧
PAによる燃料基本量の補正の必要はない。The inside of the downstream collecting section of the throttle valve 56 forms a surge tank having a large volume chamber, and therefore the pulsating changes in the internal pressure PII are small. For this reason,
If the engine speed and air-fuel ratio are constant, the filling efficiency ηt
1 (σ basic fuel amount) is maintained in a state approximately proportional to the pressure pH in the collecting pipe. In addition, even when the atmospheric pressure PA changes (for example, when driving at high altitudes), the throttle valve is fully open (WOT).
The pressure I) decreases due to the decrease in atmospheric pressure PA (P,
#PA) alone, the proportional relationship between the charging efficiency +71+ and the intake pipe pressure Y)8 is maintained not only during WOT but also under other operating conditions. Therefore, a series of speed-density methods can be applied to such ordinary types of machinery, and even if there is a change in atmospheric pressure PA,
Changes in exhaust pressure due to this (for example, internal exhaust gas recirculation (EG)
If the influence of R) (change in amount) is ignored, there is no change in filling efficiency ηi) due to change in atmospheric pressure PA, and therefore there is no need to correct the basic fuel amount based on atmospheric pressure PA.
(発明が解決しようとする課題)
しかしながら、スピードデンジデイ方式による燃料算出
方法を例えば第7図に示すような多連スロットル式のエ
ンジンに適用した場合、次のような問題がおる。かかる
多連スロットル式1ンシ゛ンにおける吸気管内圧力の検
出方法の場合、充填効率ηυと吸気管内圧力PBとの関
係は、上記第5図のような比例関係にはならず、第8図
の実線で示すように通常タイプのエンジンの場合(破線
)に比して同−Ps値に対してη11が低くなる特性を
示すことが、実験により確認されている1、多連スロッ
トル式エンジンは、各気筒71へ74の吸気管71a〜
74aの上流部で且つ集合部75下流側に、夫々スロッ
トル弁71b〜74bが設けられている。各吸気管71
a〜7・4a内の圧力は、各吸気管71a〜74a内の
圧力を絞り71c〜74cを夫々介して取込み、取込ん
だ圧力をバイブ76で集合して圧力ヤンサ77に伝達し
てこれを検出することにより求められる。このように圧
力センサ77は各吸気管内圧力の平均的な値を検出し、
この検出値をもって吸気管内絶対圧P□としている。(Problems to be Solved by the Invention) However, when the fuel calculation method based on the speed density method is applied to, for example, a multiple throttle type engine as shown in FIG. 7, the following problems occur. In the case of such a method of detecting the pressure inside the intake pipe in one-scene multiple throttle type, the relationship between the charging efficiency ηυ and the pressure inside the intake pipe PB is not proportional as shown in FIG. 5 above, but is shown by the solid line in FIG. 8. As shown in the figure, it has been confirmed through experiments that η11 is lower for the same -Ps value than in the case of a normal type engine (dashed line)1. 71 to 74 intake pipe 71a~
Throttle valves 71b to 74b are provided upstream of 74a and downstream of gathering portion 75, respectively. Each intake pipe 71
The pressure in a to 7 and 4a is obtained by taking in the pressure in each intake pipe 71a to 74a through throttles 71c to 74c, respectively, collecting the taken pressure in a vibrator 76, and transmitting it to a pressure jumper 77. Determined by detection. In this way, the pressure sensor 77 detects the average value of the pressure inside each intake pipe,
This detected value is defined as the intake pipe absolute pressure P□.
ところで、多連スロットル式エンジンに上記の方式を採
用した場合、圧力ヤンサ77に伝わる圧力は吸入行程中
の気筒と吸入行程以外の気筒の合成負圧になるが、吸入
行程以外の気筒の圧ツjが大気圧近くになるために合成
圧としては通常のタイプの工〉ジンに比べ大気圧側にず
れた値となる。By the way, when the above method is adopted for a multiple throttle engine, the pressure transmitted to the pressure jumper 77 becomes the composite negative pressure of the cylinder during the intake stroke and the cylinder other than the intake stroke, but the pressure of the cylinder other than the intake stroke Since j is close to atmospheric pressure, the combined pressure is a value that is shifted toward atmospheric pressure compared to normal types of pressure.
従って第8図に示すように、通常タイプのエンジンに比
して同一の吸気管内圧力P、に対する空気の充填効率η
υは低くなるのである。但し、スロットル弁が全開のと
き(WOT)は、吸気管には空気が絞られずに充分な流
量で供給されるので、充填効率η1+は通常タイプのエ
ンジンと同一値になる。Therefore, as shown in Fig. 8, the air filling efficiency η for the same intake pipe internal pressure P is compared to a normal type engine.
υ becomes lower. However, when the throttle valve is fully open (WOT), air is not throttled and is supplied to the intake pipe at a sufficient flow rate, so the filling efficiency η1+ has the same value as a normal type engine.
上記の第8図の特性に沿って従来のスピードデンシティ
方式により吸気管内絶対圧P、A及びエンジン回転数N
eに基づいて基本燃料量Tiを算出するためのマツプを
作成し、これを多連スロットル式エンジンに適用した場
合は下記の不具合を生じる。In line with the characteristics shown in Figure 8 above, the intake pipe absolute pressure P, A and engine speed N are determined by the conventional speed density method.
If a map for calculating the basic fuel amount Ti is created based on e and applied to a multiple throttle engine, the following problems will occur.
例えば、吸気管内絶対圧P、A対基本噴射量工のマツプ
を作成すると、第9図のように、大気圧PAに応じて多
数の特性が必要となる。従って、データの記憶量が多く
なり、コスト高となってしまう。For example, when creating a map of the intake pipe absolute pressure P and A versus the basic injection quantity, a large number of characteristics are required depending on the atmospheric pressure PA, as shown in FIG. Therefore, the amount of data stored increases, resulting in high costs.
しかし、コストを低減するため、従来のように大気圧P
A= 760mm11gとして、吸気管内絶対圧P I
IAに基づいて基本噴射量を算出すると、大気圧PAが
低下した場合にはスロットル弁全開(WOT)以外の運
転領域では吸気管内絶対圧P、Aと要求燃料量との比例
関係が成立せず、第9図のように複雑な関係になるので
、正確な燃料噴量を算出することができない。However, in order to reduce costs, atmospheric pressure P
Assuming that A = 760 mm and 11 g, the absolute pressure in the intake pipe is P I
When calculating the basic injection amount based on IA, when the atmospheric pressure PA decreases, the proportional relationship between the intake pipe absolute pressures P and A and the required fuel amount does not hold in operating ranges other than the throttle valve fully open (WOT). , the relationship is complicated as shown in FIG. 9, making it impossible to calculate an accurate fuel injection amount.
本発明は、上記事情に鑑みて為されたものでおリ、多連
スロ/[・ル式内燃エレン〉のように、吸気管内圧力七
二仙J)出力値に対する空気の充填効ヰ゛が通常々イブ
の内燃エンジンよ一ノ低くなるまうな内燃コごシンにお
いて、大気圧の変化に関らずより正確に且つ簡単に燃料
供給量を算出することのできる内燃工〉ジンの燃料供給
制御装置を提供−計ることを目的とする。The present invention has been made in view of the above circumstances, and it is noted that the air filling effect on the intake pipe internal pressure (72cm) output value is normally A fuel supply control device for an internal combustion engine that can more accurately and easily calculate the fuel supply amount regardless of changes in atmospheric pressure in an internal combustion engine that is much lower than the current internal combustion engine. The purpose is to provide and measure the
(y題を解決するための手段)
上記課題を#決するため、本発明は、内燃エンジンの吸
気管内絶対圧を検出する吸気管内絶対圧検出手段と、入
気圧を検出ずろ大気圧検出手段と、エンジン回転数を検
出するエンジン回転数検出手段と、前記入気圧と吸気管
内絶対圧との差圧を演算づる差圧演算手段と、この差圧
演算手段により演算された差圧とFri記ニジ:5゛ン
回転数と1こ応じて燃料の基本燃料量を算出才乙基本燃
料最算出手段と、l′i′lj記差圧と大気圧とに応し
ごて基本燃料量を補正するための補正値を算出する補正
値算出手段ど、二の補止値により前記基本燃料量を補正
することにより燃料供給量を算出する燃料供給量算出手
段とを備えたものでk)る、
(実施例)
以下、図面に基づいて本発明の一実施例を説町する。(Means for Solving Problem Y) In order to solve the above problems, the present invention provides an intake pipe absolute pressure detection means for detecting the absolute pressure in the intake pipe of an internal combustion engine, an atmospheric pressure detection means for detecting the intake pressure, An engine rotation speed detection means for detecting the engine rotation speed, a differential pressure calculation means for calculating the differential pressure between the inlet air pressure and the absolute pressure in the intake pipe, and a differential pressure calculated by the differential pressure calculation means and the following: Calculating the basic fuel amount according to the rotational speed and the basic fuel calculation means, and correcting the basic fuel amount according to the differential pressure and atmospheric pressure. k) a correction value calculation means for calculating the correction value of the second correction value, and a fuel supply amount calculation means for calculating the fuel supply amount by correcting the basic fuel amount by the second correction value; Example) Hereinafter, one embodiment of the present invention will be explained based on the drawings.
第1図は、本発明の一実施例に係る内燃エンジ〉の燃料
供給料a1装置の全体構成図である。FIG. 1 is an overall configuration diagram of a fuel supply a1 device for an internal combustion engine according to an embodiment of the present invention.
図中、1は多連スロットル式内燃エンジ〉でk)す、各
気筒の吸気管20L流には、夫々スロ7ノ[・ルボデイ
3が設置すらh、その内部にはスロットル弁3′が配さ
れてい己5、スロットル弁3′にはスロットル弁開度(
θ工11 )ヤシ+4が連結されており、当該スロット
ル弁3′の開度に応じた電気信号を出力して電子コント
ロールユニット(A)、”F rEC[1J という)
5に供給する。。In the figure, 1 is a multi-throttle internal combustion engine.In the intake pipe 20L of each cylinder, a throttle body 3 is installed, and a throttle valve 3' is installed inside it. The throttle valve 3' has the throttle valve opening (
θ Engineering 11) Palm +4 is connected, and outputs an electric signal according to the opening degree of the throttle valve 3' to control the electronic control unit (A), called "F rEC [1J"].
Supply to 5. .
燃料噴射弁6はエンジン】とスロットル弁3′との間且
つ吸気v2の図示しない吸気弁の少しJ二数側に各気筒
毎に設けられており、各噴射弁は図示し、ない燃料ポン
プに接続されていると共にECL15に電気的に接続さ
れて当該ECU3からの信号により燃料噴射の開弁時間
が制御される、各吸気¥f2σ)スロソh JL #
3 ’ の直ぐ下流には。The fuel injection valve 6 is provided for each cylinder between the engine] and the throttle valve 3' and a little on the J2 side of the intake valve (not shown) of the intake v2, and each injection valve is connected to a fuel pump (not shown). Each intake ¥f2σ) Sloso h JL # which is electrically connected to the ECL 15 and whose fuel injection valve opening time is controlled by a signal from the ECU 3.
Immediately downstream of 3'.
絞り7aを有するv7が分岐し5、この管7は他の吸気
管2の管7とも接続するバイブ14に接続され、該バイ
ブ14の一端には吸気管内絶対圧(P、、A)センサ8
が接続されており、各吸気管2内の絶対叩1)、は管7
を介して取込まれ、バイブ14で集8され、この絶対圧
センサ8に伝達され、該センサにより電気信号に変換さ
れる。この変換された各吸気管2の平均絶対圧P、Aを
示す絶対圧(P、え)信号は前記ECU3に供給される
。A v7 having a throttle 7a branches 5, and this pipe 7 is connected to a vibrator 14 which also connects to the pipe 7 of the other intake pipe 2, and an intake pipe absolute pressure (P, , A) sensor 8 is installed at one end of the vibrator 14.
are connected, and the absolute tap 1) in each intake pipe 2 is connected to the pipe 7.
The pressure is taken in through the sensor, collected by the vibrator 14, transmitted to the absolute pressure sensor 8, and converted into an electrical signal by the sensor. This converted absolute pressure (P, E) signal indicating the average absolute pressures P and A of each intake pipe 2 is supplied to the ECU 3.
方、エンジン1の図示しないクランク軸の周囲には、エ
ンジン回転数(Ne)センサ9が取付けらilている。On the other hand, an engine rotational speed (Ne) sensor 9 is attached around a crankshaft (not shown) of the engine 1.
エンジン回転数センサ9はエンジン1のクランク軸の1
80度回転毎に所定のクランク角度位置で、即ち各気筒
の吸気行程開始時の五死点(丁DC)に関し所定クラ〉
・り角度前のクランク角度位置で信号パルス(以下rT
DC信号パルス」という)を出力する。このTDC信号
パルスは、ECU3に供給される。又、ECU3は、大
気圧(PA)センサ10が電気的に接続されており、検
出大気圧(PA)信号が供給される。The engine speed sensor 9 is located on the crankshaft of the engine 1.
At a predetermined crank angle position every 80 degree rotation, that is, at a predetermined crank angle position at the start of the intake stroke of each cylinder,
・Signal pulse (hereinafter referred to as rT) at the crank angle position before rT
It outputs a DC signal pulse (referred to as "DC signal pulse"). This TDC signal pulse is supplied to the ECU 3. Further, the ECU 3 is electrically connected to an atmospheric pressure (PA) sensor 10, and is supplied with a detected atmospheric pressure (PA) signal.
EC1J5は各種センサからの人力信号波形を整形り、
!圧しベルを所定レベルに蛯正し、アナロゲ信号値をデ
ジタル信号値に変換する等の機能を有する入力回路5a
、中央演算処理回路(0下rcPLIJ 、!=u”5
)5b、CPTJ5bで実行される各種演算プログラム
及び演算結果等を記憶する記憶手段5c、前記燃料噴射
弁6に駆動信号を供給する出力回路5d等から構成され
る、CPU5bは上述の各センサ及び他の図示しないセ
ンサからの各種エンジンパラメータイコ号に塞づいて2
種々のエンジン運転状態を判別するとともに、エンジン
運転状態に応じ、次式〈1)に基づいて前記丁DC信号
に同期する燃料噴射弁6の燃料噴射時間T。いを演算す
る。尚、この燃料噴射時間T C1kl Tの演算は、
後述するプログラムに基づいて行われる。EC1J5 shapes the waveform of human input signals from various sensors,
! An input circuit 5a having functions such as adjusting the pressure bell to a predetermined level and converting an analog signal value into a digital signal value.
, central processing circuit (0 lower rcPLIJ, !=u”5
) 5b, a storage means 5c for storing various calculation programs and calculation results executed by the CPTJ 5b, an output circuit 5d for supplying a drive signal to the fuel injection valve 6, and the like. 2 due to various engine parameters from sensors not shown in the figure.
The fuel injection time T of the fuel injection valve 6 is determined according to various engine operating states and is synchronized with the DC signal based on the following equation (1) according to the engine operating state. Calculate the value. The calculation of this fuel injection time T C1kl T is as follows:
This is done based on the program described below.
TouT” Tix KrAX Kl+ K2
・ ・ (lンここに、Tiは燃料噴射弁6の噴射時
間T。LITの基本噴射量であり、エンジン回転数Ne
、及び大気圧PAと吸気管内絶対圧P IIAとの差圧
PA−P、Aに応じて設定された図示しないT17:2
ブから読み出される。KPAは本発明に係る大気圧pA
と差圧PA−P、とに応じて決まる補正係数であり、後
述するに、 F Aマツプより読み出される。TouT” Tix KrAX Kl+ K2
・ ・ (In here, Ti is the injection time T of the fuel injection valve 6. It is the basic injection amount of LIT, and the engine rotation speed Ne
, and T17:2 (not shown) set according to the differential pressure PA-P, A between the atmospheric pressure PA and the intake pipe absolute pressure P IIA.
read from the block. KPA is atmospheric pressure pA according to the present invention
This is a correction coefficient determined according to the differential pressure PA-P, and is read out from the FA map, as will be described later.
K、、に、は夫々各種エンジンパラメータ信号に応じて
演算される補正係数及び補正変数であり、エンジン運転
状態に応じた燃費特性、エンジン加速特性等の訃特性の
最適化が図られるような所定値に決定され乙。K, , and K are correction coefficients and correction variables that are calculated according to various engine parameter signals, respectively, and are set to predetermined values to optimize engine performance characteristics such as fuel consumption characteristics and engine acceleration characteristics according to engine operating conditions. The value has been determined.
CPU5bは上述のようにして求めた燃料噴射時間T。The CPU 5b calculates the fuel injection time T obtained as described above.
L、Tに基づいて燃料噴射弁6を開弁させる駆動信号を
出力回路5dを介して燃料噴射弁6に供給する。A drive signal for opening the fuel injection valve 6 based on L and T is supplied to the fuel injection valve 6 via the output circuit 5d.
尚、本実施例においてECU3は、差圧演算手段、基本
性料量算出手段、補正値算出手段及び燃料供給量算出手
段を構成する。In this embodiment, the ECU 3 constitutes a differential pressure calculation means, a basic fuel amount calculation means, a correction value calculation means, and a fuel supply amount calculation means.
次に、本発明に係る燃料供給量の算出方法について説明
する。Next, a method for calculating the fuel supply amount according to the present invention will be explained.
第8図の充填効率ηυと吸気管内絶対圧P、Aとの関係
に基づいて、第3図に示すように、横軸に、大索圧PA
と吸気管内絶対圧PIIAとの差圧をとる。Based on the relationship between the filling efficiency ηυ and the intake pipe absolute pressures P and A in FIG. 8, as shown in FIG.
Calculate the differential pressure between the intake pipe absolute pressure PIIA and the intake pipe absolute pressure PIIA.
すると、PA−P8A=0の点で、全ての特性を揃える
ことができる6PA !〕BA”’O2即ちスロットル
弁全開時は、絶対圧P、Aと基本噴射量Tiとの関係は
、通常のエンジン同様に比例関係になる。Then, 6PA can have all the characteristics at the point where PA-P8A=0! ] BA'''O2, that is, when the throttle valve is fully open, the relationship between the absolute pressures P and A and the basic injection amount Ti is proportional as in a normal engine.
従って、第3図のように、例えばP A= 650+n
mHl(のときのスロットル弁全開時の基本噴射量T1
.、を求めるためには、PA= 760miHgのとき
のスロットル弁全開時の基本噴射量TIAを予め求めて
お1づばよい。即ち、次式(2)によっていかなる大気
圧のときでもスロットル弁全開時の正確な燃料噴射量を
求めることができる。Therefore, as shown in Fig. 3, for example, P A = 650 + n
Basic injection amount T1 when the throttle valve is fully open when mHl (
.. In order to obtain , it is sufficient to obtain in advance the basic injection amount TIA when the throttle valve is fully open when PA = 760 miHg. That is, an accurate fuel injection amount when the throttle valve is fully open can be determined using the following equation (2) at any atmospheric pressure.
L−ム −T l h ” T
l p X!”巴−−−(2)TiA760
+60このことは、以下のことからの
説明できる。L-mu-T l h”T
lpX! “Tomoe---(2) TiA760
+60 This can be explained from the following.
スロットル弁全開時は、スロットル部の開口面積Aは一
定となり、エンジン回転数が一定であれば、空気の流速
t(も一定である。したがって、空気流量Q = A
vも一定となる。When the throttle valve is fully open, the opening area A of the throttle part is constant, and if the engine speed is constant, the air flow rate t (is also constant. Therefore, the air flow rate Q = A
v also becomes constant.
更に、空気重量に=QXρ(ρは空気密度) (3)
また、ρ−ρ。×−P−五×−力− −・ (4
)760 (273÷t)
[ρ0は標準状態での空気密度、tは吸気温度1式(4
)において、吸気温度tの影響を無視すれば、
ム ・・ ・・・(5)p#p0x76
0
式(5)を式(3)に代入すれば、
ム ・(6)
G ” Q xP o x760
となる。よって空気重量Gはムに比例することがわかる
。ここで、空燃比が一定であれば、必要燃料噴射量もW
に比例することになり二のことからも式(2)が正しい
ことが理解できる。Furthermore, air weight = QXρ (ρ is air density) (3)
Also, ρ−ρ. ×−P−5×−force−−・(4
)760 (273÷t) [ρ0 is the air density in the standard state, t is the intake air temperature 1 equation (4
), if the influence of the intake air temperature t is ignored, then (5) p#p0x76
0 Substituting equation (5) into equation (3) gives Mu ・(6) G ” Q x P ox760. Therefore, it can be seen that the air weight G is proportional to Mu. If so, the required fuel injection amount is also W
It can be understood from the second fact that equation (2) is correct.
このように、スロットル弁全開時であれば、大気圧が変
化しても上述の式(2)より、簡単に且つ正確に燃料の
噴射量Tiを算出することができる。しかし、このスロ
ットル弁全開時以外では、スロットル部の開口面積Aが
一定でなくなるため上記式(2)は適用できず、このた
め燃料噴射量を正確に算出できない。In this way, as long as the throttle valve is fully open, even if the atmospheric pressure changes, the fuel injection amount Ti can be easily and accurately calculated using the above equation (2). However, at times other than when the throttle valve is fully open, the opening area A of the throttle section is not constant, so the above equation (2) cannot be applied, and therefore the fuel injection amount cannot be calculated accurately.
例えば、アイドル時の場合を考えると、大気圧PAが低
下するとpA ”BAは小さくなるために、同一吸入空
気量に対して第3図から燃料基本噴射量Tiはより大き
い値に設定されてしまい、従って大気圧が低下すると、
スロットル弁全開時に比して、空燃比が濃くなる傾向に
なる。For example, considering the case of idling, when the atmospheric pressure PA decreases, pA "BA becomes smaller, so the basic fuel injection amount Ti is set to a larger value as shown in Fig. 3 for the same intake air amount. , so when atmospheric pressure decreases,
The air-fuel ratio tends to become richer than when the throttle valve is fully open.
従って1本発明では、差圧P、、−P、AをP、とじて
算出し、この差圧PGに応じてP6の複数の所定ライン
PGNのいずれかを選択し、検出大気圧PAに応じてこ
の選択されたラインPい上に慶)る補正値を大気圧補正
係数K1.Aとして求めるものである。Therefore, in the present invention, the differential pressures P, , -P, and A are calculated by dividing them into P, and one of the plurality of predetermined lines PGN of P6 is selected according to the differential pressure PG, and according to the detected atmospheric pressure PA. The correction value on the selected line P is set as the atmospheric pressure correction coefficient K1. This is what is sought as A.
即ち、第4図のマツプに示すように、上記ラインPいと
して、夫々WOT、パーシャル負荷、アイドルに対応す
る3つのラインP co”” P c)が−例として示
されており、これらのラインは差圧PGが夫々の所定値
を執るときに選択される。差圧P6がこれら所定値間の
値を執るときは補間計算によって適当なラインが決定さ
れる。第4図のマツプ例では、大気圧が760迄m)I
g〜600ロdlの間にあるときは、各ラインPG0〜
PC2は補正係数KPAO値が小さくなて)方向に傾斜
している。これは、差圧P、(=PA−P、A)が同じ
値であってt。That is, as shown in the map of FIG. 4, three lines Pco""Pc) corresponding to WOT, partial load, and idle are shown as examples for the above-mentioned line P, and these lines are selected when the differential pressure PG takes on each predetermined value. When the differential pressure P6 takes a value between these predetermined values, an appropriate line is determined by interpolation calculation. In the example map in Figure 4, the atmospheric pressure is up to 760 m) I
When it is between g~600rodl, each line PG0~
In PC2, the correction coefficient KPAO value decreases and is inclined in the direction of ). This means that the differential pressure P, (=PA-P,A) is the same value and t.
大気圧pAが低ければ、吸入空気量が少なくなるため、
燃料量もそれに応じて減らす必要があるからである。If the atmospheric pressure pA is low, the amount of intake air will be small, so
This is because the amount of fuel needs to be reduced accordingly.
又、大気圧が600 mmHg未満のときは、ラインP
、o−P、、、は、補正係数k PA値0.8.0.7
.0.6に夫々固定される。又、Pcが大きいP、Nラ
イン、即ち大気圧PAと吸気管内絶対圧P IIAとの
差圧が入きL)ラインj:jどKPAの値が小さくなる
ように設定されている。これは、差圧P、が大きくなる
ほど吸入空気量が減少しやすくなるため、燃料量もそれ
に応じて減らす必要があるからである。検出大気圧))
Aが該当するPいライン士の値が補正係数k r Aと
して読み出される。Also, when the atmospheric pressure is less than 600 mmHg, line P
, o-P, , is the correction coefficient k PA value 0.8.0.7
.. Each is fixed at 0.6. In addition, the value of KPA is set to be smaller in the P and N lines where Pc is large, that is, in the L) line where the differential pressure between the atmospheric pressure PA and the intake pipe absolute pressure PIIA is applied. This is because the intake air amount tends to decrease as the differential pressure P increases, so the fuel amount also needs to be reduced accordingly. Detected atmospheric pressure))
The value of the P line to which A corresponds is read out as the correction coefficient krA.
このようにして求めた大気圧補正係数k l’ Aは、
前記式(1)に基づいて、後述するように、差圧r G
及びニレジン回転数Neに応じてT1マツプから読出さ
れた基本燃料噴射1k T iに乗算される。The atmospheric pressure correction coefficient k l' A obtained in this way is
Based on the formula (1), as described later, the differential pressure r G
and the basic fuel injection 1k T i read from the T1 map according to the engine speed Ne.
次に、第2図のプログラムフローチャートに基づき、燃
料噴射量T 、11.1□を算出する手順を述べる。Next, the procedure for calculating the fuel injection amount T, 11.1□ will be described based on the program flowchart shown in FIG.
尚、このプログラムは、TDC信号パルスの発生毎にこ
れに同期して実行される。Note that this program is executed in synchronization with each TDC signal pulse.
まず、ステップS】で、吸気管内絶対圧PIIA、大気
圧PA、及びエンジン回転数Neが検出されると、ステ
ップS2で大気圧PAと吸気管内絶対圧Pいとの差圧P
、:1(=PA−P、A)を算出する。First, in step S], when the intake pipe absolute pressure PIIA, atmospheric pressure PA, and engine speed Ne are detected, in step S2, the differential pressure P between the atmospheric pressure PA and the intake pipe absolute pressure P is detected.
, :1(=PA-P,A) is calculated.
ステップS3では、この差圧P、梵エンジン回転#Ne
とに基づいて、基本噴射量TiをTiマツプより検索す
る。二〇T1マツプは例えば前述した第3図におけるP
A= 760mm1Gの特性に五づいて作成される。In step S3, this differential pressure P, the engine rotation #Ne
Based on this, the basic injection amount Ti is searched from the Ti map. 20T1 map is, for example, P in Fig. 3 mentioned above.
It is created based on the characteristics of A=760mm1G.
次いで、ステップS4で、差圧PI1.の値に基づいて
補正値k PAを求めるべく、第4図のマツプに従って
、P6のラインPcNを設定する。ステップS5では、
この設定したラインPGNと、大気圧PAとに基づいて
、第4図のマツプにより補正係数k PAを読出す。Next, in step S4, the differential pressure PI1. In order to obtain the correction value kPA based on the value of , the line PcN of P6 is set according to the map shown in FIG. In step S5,
Based on the set line PGN and the atmospheric pressure PA, the correction coefficient kPA is read out using the map shown in FIG.
斯くして、燃料の基本噴射量T1及びその補正係数に、
Aの検索を行った徒、ステップS6にて。In this way, the basic injection amount T1 of fuel and its correction coefficient,
After searching for A, in step S6.
11」記式(1)に従って、T1を大気圧補正係数KP
A及び他の補正係数に3.補正変数に、で補正して、燃
料噴射量T。LITを算出し、本プログラムを終了する
。11” According to formula (1), T1 is the atmospheric pressure correction coefficient KP.
3. A and other correction factors. The correction variable is corrected by the fuel injection amount T. Calculate LIT and end this program.
このように本実施例では、大気圧PAが76OnonJ
のときを基準にしたT1マツプに基づいて、大気圧PA
と吸気管内絶対圧pHAとの差圧P9、と、エンジン回
転数Neとに応じた基本噴射量Tiを検索し、そのT1
値を差圧P6と大気圧PAとに基づいて検索した補正値
K PAによって補正するようにしたので、少ない記憶
量で、かつ正確に燃料噴射量T (ILIアの算出を行
うことができる。In this way, in this example, the atmospheric pressure PA is 76OnonJ
Based on the T1 map based on the time of atmospheric pressure PA
Search for the basic injection amount Ti according to the differential pressure P9 between the absolute pressure in the intake pipe and the absolute pressure pHA, and the engine speed Ne, and calculate the basic injection amount Ti according to the engine rotation speed Ne.
Since the value is corrected using the correction value KPA retrieved based on the differential pressure P6 and the atmospheric pressure PA, the fuel injection amount T (ILIa) can be calculated accurately with a small amount of memory.
尚、本実施例では、かかる手法を、多連スロントル式内
燃エンジンに適用したが、これに限られず、スロットル
弁が一つのみ設けられた通常々イブタイプの内燃エンジ
ンであっても、吸気管の集合部容積の小さい内燃エンジ
〉や、吸気弁と排気弁とのバ/Lブオーバラップの大き
い内燃エンジンにおいても適用することができる。In this example, this method was applied to a multiple throttle internal combustion engine, but the invention is not limited to this, and even if the engine is a typical Eve type internal combustion engine with only one throttle valve, the intake pipe The present invention can also be applied to internal combustion engines with a small collecting part volume, and internal combustion engines with a large valve/L valve overlap between the intake valve and the exhaust valve.
(光用の効果)
4゜
上述したように、本発明に依れば、内燃エンジンの吸気
管内絶対圧を検出する吸気管内絶対圧検出手段と、大気
圧を検出する大気圧検出手段と、エンジン回転数を検出
するエンジン回転数検出手段と、前記大気圧と吸気管内
絶対圧との差圧を演算する差圧演算手段と、この差圧演
算手段により演算された差圧と前記エンジン回転数とに
応じて燃料の基本燃料量を算出する基本燃料量算出手段
と、前記差圧と大気圧とに応じて基本燃料量を補正する
だめの補正値を算出する補正値算出手段と、この補正値
により前記基本燃料量を補正することにより燃料供給量
を算出する燃料供給量算出手段とを備えたことにより、
大気圧と吸気管内絶対圧どの差圧と、エンジン回転数と
に応じた基本燃料供給量を検索し、その基本燃料供給量
を差圧と大気圧とに基づいて検索した補正値によって補
正するようにしたので、少ない記憶量でかつ大気圧の変
化に関らず常に正確に、燃料供給量T。1.lTの算出
を行うことができる。(Effect for light) 4. As described above, according to the present invention, the intake pipe absolute pressure detection means for detecting the absolute pressure in the intake pipe of the internal combustion engine, the atmospheric pressure detection means for detecting the atmospheric pressure, and the engine an engine rotation speed detection means for detecting the rotation speed; a differential pressure calculation means for calculating a differential pressure between the atmospheric pressure and the absolute pressure in the intake pipe; and a differential pressure calculated by the differential pressure calculation means and the engine rotation speed. a basic fuel amount calculating means for calculating a basic fuel amount of fuel according to the differential pressure and the atmospheric pressure, a correction value calculating means for calculating a correction value for correcting the basic fuel amount according to the differential pressure and atmospheric pressure, and this correction value. and a fuel supply amount calculation means for calculating the fuel supply amount by correcting the basic fuel amount,
The basic fuel supply amount is searched according to the differential pressure such as atmospheric pressure and the absolute pressure in the intake pipe, and the engine speed, and the basic fuel supply amount is corrected by the correction value searched based on the differential pressure and atmospheric pressure. Therefore, the fuel supply amount T can be determined accurately with a small amount of memory and regardless of changes in atmospheric pressure. 1. Calculation of lT can be performed.
第1図は本発明の一実施例に係る炉材供給制御装置の全
体構成図、第2図は燃料噴射量を算出するためのゴロゲ
ラムを示すフローチャート、第3図は多連スロットル式
内燃エンジンに適用される大気圧PA、差圧P A−P
llAl及び基本噴射量T1間の関係を示す図、第4
図は差圧P、ど大気圧P6とに基づく補正係数KPAの
算出マツプを示ず図、第5図は通常タイプの内燃エンジ
ンにおける吸気管内絶対圧P8Aと空気の充填力率η1
・との関係を示す図、第6図は通常タイプの内燃エンジ
ンの構成を示す略図、第7図は多連フロ、/トル式内燃
エンジンの構成を示す略図、第8図は多連スロットル式
内燃エンジシにおける吸気管内絶対圧P HAと空気の
充填効率ηt・どの関係を示す図、第9図は多連スロッ
トル式内燃エンジンにおける大気圧PAと吸気管内絶対
圧PhAとに応じた基本噴射jlTの算出マツプで、t
−)る4、
] 内燃エンジン22 吸気管、3′ スロットル弁
、5・・EC11(差圧演算手段、基本燃料量算出手段
、補正値算出手段、燃料供給jl算出、f段〕、8 吸
気管内絶対圧ヤシ士、9 ニシジン凹転数七シ妙、10
大気圧ヤシサ、PA 大気圧、)’RA吸気管内絶
対圧、P3.差圧、T1−基本噴射量、丁(l L+
7 燃料噴射量。Fig. 1 is an overall configuration diagram of a reactor material supply control device according to an embodiment of the present invention, Fig. 2 is a flowchart showing a goragelum for calculating the fuel injection amount, and Fig. 3 is a flowchart showing a flowchart for a multi-throttle type internal combustion engine. Applicable atmospheric pressure PA, differential pressure P A-P
4th diagram showing the relationship between llAl and basic injection amount T1
The figure does not show a calculation map for the correction coefficient KPA based on the differential pressure P and the atmospheric pressure P6.
Figure 6 is a schematic diagram showing the configuration of a normal type internal combustion engine, Figure 7 is a diagram showing the configuration of a multiple flow/torque type internal combustion engine, and Figure 8 is a diagram showing the configuration of a multiple throttle type internal combustion engine. A diagram showing the relationship between intake pipe absolute pressure PHA and air filling efficiency ηt in an internal combustion engine. Figure 9 shows the basic injection jlT according to atmospheric pressure PA and intake pipe absolute pressure PhA in a multiple throttle internal combustion engine. In the calculation map, t
-) 4,] Internal combustion engine 22 Intake pipe, 3' Throttle valve, 5...EC11 (differential pressure calculation means, basic fuel amount calculation means, correction value calculation means, fuel supply jl calculation, f stage], 8 Intake pipe Absolute pressure palmist, 9 Nishijin concave rotation number 7shi strange, 10
Atmospheric pressure, PA Atmospheric pressure, )'RA Absolute pressure in the intake pipe, P3. Differential pressure, T1-basic injection amount, d(l L+
7 Fuel injection amount.
Claims (1)
絶対圧検出手段と、大気圧を検出する大気圧検出手段と
、エンジン回転数を検出するエンジン回転数検出手段と
、前記大気圧と吸気管内絶対圧との差圧を演算する差圧
演算手段と、この差圧演算手段により演算された差圧と
前記エンジン回転数とに応じて燃料の基本燃料量を算出
する基本燃料量算出手段と、前記差圧と大気圧とに応じ
て基本燃料量を補正するための補正値を算出する補正値
算出手段と、この補正値により前記基本燃料量を補正す
ることにより燃料供給量を算出する燃料供給量算出手段
とを備えたことを特徴とする内燃エンジンの燃料供給制
御装置。1. Intake pipe absolute pressure detection means for detecting the absolute pressure in the intake pipe of an internal combustion engine; atmospheric pressure detection means for detecting atmospheric pressure; engine rotation speed detection means for detecting engine speed; A differential pressure calculating means for calculating a differential pressure with respect to an absolute pressure; a basic fuel amount calculating means for calculating a basic fuel amount of fuel according to the differential pressure calculated by the differential pressure calculating means and the engine rotation speed; a correction value calculation means for calculating a correction value for correcting the basic fuel amount according to the differential pressure and atmospheric pressure; and a fuel supply for calculating the fuel supply amount by correcting the basic fuel amount using the correction value. 1. A fuel supply control device for an internal combustion engine, comprising: quantity calculation means.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP02247760A JP3105230B2 (en) | 1990-09-18 | 1990-09-18 | Fuel supply control device for internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP02247760A JP3105230B2 (en) | 1990-09-18 | 1990-09-18 | Fuel supply control device for internal combustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH04128532A true JPH04128532A (en) | 1992-04-30 |
| JP3105230B2 JP3105230B2 (en) | 2000-10-30 |
Family
ID=17168257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP02247760A Expired - Fee Related JP3105230B2 (en) | 1990-09-18 | 1990-09-18 | Fuel supply control device for internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3105230B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010058651A1 (en) * | 2008-11-19 | 2010-05-27 | ヤンマー株式会社 | Multi-engine multi-shaft vessel |
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| JPS5885337A (en) * | 1981-11-12 | 1983-05-21 | Honda Motor Co Ltd | Air-fuel ratio atmospheric pressure correction method and device for internal combustion engine |
| JPS58101235A (en) * | 1981-11-20 | 1983-06-16 | Honda Motor Co Ltd | Electronic fuel injection control device of internal- combustion engine with exhaust gas circulation control device |
| JPS58171337A (en) * | 1982-03-30 | 1983-10-08 | 富士重工業株式会社 | Folding type container |
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| JP2010121533A (en) * | 2008-11-19 | 2010-06-03 | Yanmar Co Ltd | Multi-engine multi-shaft vessel |
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| Publication number | Publication date |
|---|---|
| JP3105230B2 (en) | 2000-10-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |