JPS60108546A - Fuel injection device of engine - Google Patents
Fuel injection device of engineInfo
- Publication number
- JPS60108546A JPS60108546A JP58213881A JP21388183A JPS60108546A JP S60108546 A JPS60108546 A JP S60108546A JP 58213881 A JP58213881 A JP 58213881A JP 21388183 A JP21388183 A JP 21388183A JP S60108546 A JPS60108546 A JP S60108546A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- injection
- injection valve
- intake
- 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
Links
- 238000002347 injection Methods 0.000 title claims abstract description 114
- 239000007924 injection Substances 0.000 title claims abstract description 114
- 239000000446 fuel Substances 0.000 title claims abstract description 94
- 230000035939 shock Effects 0.000 abstract description 6
- 239000010419 fine particle Substances 0.000 abstract 1
- 230000001133 acceleration Effects 0.000 description 10
- 238000002485 combustion reaction Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 238000000889 atomisation Methods 0.000 description 4
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000004043 responsiveness Effects 0.000 description 2
- 239000002828 fuel tank Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10006—Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
- F02M35/10026—Plenum chambers
- F02M35/10045—Multiple plenum chambers; Plenum chambers having inner separation walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1015—Air intakes; Induction systems characterised by the engine type
- F02M35/10177—Engines having multiple fuel injectors or carburettors per cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/108—Intake manifolds with primary and secondary intake passages
- F02M35/1085—Intake manifolds with primary and secondary intake passages the combustion chamber having multiple intake valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/112—Intake manifolds for engines with cylinders all in one line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/04—Injectors peculiar thereto
- F02M69/042—Positioning of injectors with respect to engine, e.g. in the air intake conduit
- F02M69/044—Positioning of injectors with respect to engine, e.g. in the air intake conduit for injecting into the intake conduit downstream of an air throttle valve
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、エンジンの燃料噴射装置の改良に関するもの
である。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an improvement in a fuel injection device for an engine.
(従来技術)
エンジンの各気筒に対して2つの燃料噴射弁を配設し、
エンジンの負荷等の運転状態に応じて各燃料@側弁から
の燃料噴射用を制御し、第1噴則弁からは低吸気口域を
含む全運転領域で燃料を噴射し、第2噴射弁からは高吸
気W域で燃料を噴射するようにして、低負荷域から高負
荷域に至るまで精度の良い燃料供給制御を実現するよう
にした燃料−射装置は、例えば実公昭57−50536
号に見られるように公知である。(Prior art) Two fuel injection valves are arranged for each cylinder of the engine,
The fuel injection from each fuel @ side valve is controlled according to the engine load and other operating conditions, and the first injection valve injects fuel in the entire operating range including the low intake area, and the second injection valve For example, a fuel injection device that injects fuel in a high intake W range to achieve accurate fuel supply control from a low load range to a high load range is known as, for example, the Japanese Utility Model Publication No. 57-50536.
It is well known as shown in No.
上記のような燃料噴射装置では、高負荷時にd3ける多
凶の燃料噴射を1本の燃1f3I nA射弁で行うと、
低負荷時の少量の燃料噴射を行うときの精度が低下する
のに対し、低流量域での供給精度の良い第1噴射弁で低
負荷域の燃料噴射を行う一方、この第1噴射弁では供給
できない高流量域では第2噴側弁からも燃料噴射を行う
ようにしたものである。In the above-mentioned fuel injection device, if the dangerous fuel injection at d3 is performed with one fuel 1f3I nA injector during high load,
Accuracy decreases when injecting a small amount of fuel at low load, whereas the first injector, which has good supply accuracy in the low flow rate range, injects fuel in the low load range. In a high flow rate range where fuel cannot be supplied, fuel is also injected from the second injection side valve.
しかして、吸入空気母の増大に応じて燃料噴射量を増大
するために、第1噴射弁による燃料噴射に加えてM2噴
射弁による燃料噴射を行うについて、前記先行例のよう
に、各噴射弁における燃圧が一定のものでは、全領域に
おいて良好な噴射特性を得ることは困難で低負荷時の供
給精度を向上すると、第2噴射弁の噴射開始時に切換シ
ョックが発生し、運転性に悪影響を与える恐れがある。Therefore, in order to increase the fuel injection amount in accordance with the increase in the intake air carrier, in order to perform fuel injection by the M2 injector in addition to the fuel injection by the first injector, each injector If the fuel pressure is constant, it is difficult to obtain good injection characteristics over the entire range.If the supply accuracy at low loads is improved, a switching shock will occur at the start of injection from the second injector, which will have a negative impact on drivability. There is a risk of giving.
すなわち、低噴射硲域では、燃圧が高いと所定最(少舟
)の燃料噴射を行う時間が短(なってその制御性が低下
することから、低い燃圧の方が噴射時間が長くなって制
御性に優れる反面、燃圧が低いと高噴射領域に移行して
第2噴射弁からの噴射を開始したときに、吸気通路に噴
射された燃料が燃焼室に流入するまでの時間遅れが発生
して、一時的にリーンな空燃比の混合気の供給によって
エンジン出力が低下して運転性にショックを与えるもの
であり、また、燃圧を上昇すると切換時のショックの軽
減とともに燃料の微粒化を促進して燃焼性の向上が図れ
るものである。In other words, in the low injection range, when the fuel pressure is high, the time to perform the predetermined maximum (small) fuel injection is short (and the controllability is reduced), so when the fuel pressure is low, the injection time is longer and the controllability is reduced. On the other hand, when the fuel pressure is low, there is a time delay before the fuel injected into the intake passage flows into the combustion chamber when the fuel injection range shifts to the high injection range and injection from the second injector starts. , temporarily supplying a mixture with a lean air-fuel ratio reduces engine output and causes a shock to drivability.In addition, increasing the fuel pressure reduces the shock during switching and promotes fuel atomization. It is possible to improve combustibility.
(発明の目的)
本発明は上記事情に鑑み、Mlおよび俯2咄射弁による
燃料噴射において燃料の供給精瓜の向上と、切換時のシ
ョック低減の要望を同時に満足するようにして良好な燃
焼性を得るようにしたエンジンの燃料噴射装置を提供す
ることを目的とするものである。(Object of the Invention) In view of the above-mentioned circumstances, the present invention aims to improve fuel injection by simultaneously satisfying the demands of improving fuel supply efficiency and reducing shock during switching in fuel injection using Ml and two-pressure injection valves, thereby achieving good combustion. The object of the present invention is to provide a fuel injection device for an engine that achieves improved performance.
(発明の構成)
本発明のエンジンのm判@別装置は、低吸気量域を含む
全運転領域で燃料を噴射−4る第1噴射弁と、高吸気量
域で燃料を噴射づる第2噴射弁とを備えたものにおいて
、上記第2噴射弁の燃圧を第1噴射弁の燃圧より高く設
定したことを特徴とするものである。(Structure of the Invention) The M size @ separate device for the engine of the present invention includes a first injection valve that injects fuel in the entire operating range including the low intake air amount area, and a second injection valve that injects fuel in the high intake air amount area. The fuel injection valve is characterized in that the fuel pressure of the second injection valve is set higher than the fuel pressure of the first injection valve.
(発明の効果)
本発明によれば、低吸気m域では燃圧の低い第1噴射弁
によって精度の良い燃料噴射を行うとともに、高吸気量
域では燃圧の高い第2噴射弁からも燃料噴射を行うよう
にして燃料微粒化を促進づる一方、この第11114射
弁に加えて第2噴射弁からも燃料を噴射する切換時にお
ける噴射燃料の飛散距離が大ぎく燃料遅れを改善し応答
性を向上することができ、この切換時のショック低減が
実現できるものである。(Effects of the Invention) According to the present invention, in the low intake air amount region, the first injector with low fuel pressure injects fuel with high precision, and in the high intake amount region, the second injector with high fuel pressure also injects fuel. While this promotes fuel atomization, the scattering distance of the injected fuel when switching to inject fuel from the second injector in addition to the 11114th injector is too large, improving fuel delay and improving responsiveness. This makes it possible to reduce the shock at the time of switching.
(実施例)
」ス下、図面により本発明の実施態様を詳細に説明する
。(Example) Embodiments of the present invention will be described in detail below with reference to the drawings.
第1図は2つの吸気ボートを備えたエンジンの全体構成
図で、エンジン1の各気筒の燃焼室2に対し、2つのM
lおよび第2の吸気ボート3および4が開口するととも
に、2つの第1および第2の排気ボート5および6がそ
れぞれ開口している。Figure 1 is an overall configuration diagram of an engine equipped with two intake boats.
1 and the second intake boats 3 and 4 are open, and the two first and second exhaust boats 5 and 6 are open, respectively.
上記吸気ボート3.4には吸入空気を供給する吸気通路
7が接続されている。この吸気通路7は上流端にエアク
リーナ8を有し、このエアクリーナ8の下流側に吸気量
を検出する吸入空気筒検出手段9(エアフローメータ)
が介装され、この吸入中気門検出手段9より下流側の吸
気通路7が、第1の吸気通路7aと第2の吸気通路7b
とに分岐形成されている。第1の吸気通路78は拡張寮
7Gを介して各燃焼室2の第1の吸気ボート3にそれぞ
れ接続される一方、第2の吸気通路7bは拡張室7dを
介して各燃焼室2の第2の吸気ボート4にそれぞれ接続
されている。An intake passage 7 for supplying intake air is connected to the intake boat 3.4. This intake passage 7 has an air cleaner 8 at its upstream end, and an intake air cylinder detection means 9 (air flow meter) downstream of this air cleaner 8 for detecting the amount of intake air.
is interposed, and the intake passage 7 on the downstream side of the spiracle detection means 9 during intake has a first intake passage 7a and a second intake passage 7b.
It is branched into two parts. The first intake passage 78 is connected to the first intake boat 3 of each combustion chamber 2 via the expansion dormitory 7G, while the second intake passage 7b is connected to the first intake boat 3 of each combustion chamber 2 via the expansion chamber 7d. 2 intake boats 4, respectively.
上記第1の吸気通路7aの入口部分(Sは、この第1の
吸気通路7aを流れる吸気量を制御づる第1の絞り弁1
0が介設されると七もに、上記第2の吸気通路7bの入
口部分には、この第2の吸気通路7bを流れる吸気量を
制御づる第2の絞り弁11が介設され、両絞り弁”10
.11はスnツトル操作に連係して開閉作動される。第
1の絞り弁10は低負荷時から開いて負荷の」−昇に伴
って全開状態となり、第2の絞り弁11は第1の絞り弁
10が設定開度以上となったときに開き始め負荷の上昇
とともに全開状態となるものである。The inlet portion of the first intake passage 7a (S is the first throttle valve 1 that controls the amount of intake air flowing through the first intake passage 7a).
0, a second throttle valve 11 is provided at the entrance of the second intake passage 7b to control the amount of intake air flowing through the second intake passage 7b. Throttle valve"10
.. 11 is opened and closed in conjunction with the throttle operation. The first throttle valve 10 opens when the load is low and becomes fully open as the load increases, and the second throttle valve 11 begins to open when the opening of the first throttle valve 10 reaches or exceeds the set opening. It becomes fully open as the load increases.
上記第1の吸気通路7aには低吸気5H域を含む全運転
領域で燃料を噴射する第1噴射弁12が各気筒に対して
それぞれ配設されるとともに、上記第2の吸気通路7b
には高吸気量域で燃料を噴則づる第2噴躬弁13が各気
筒に対してそれぞれ配設されている。この第1および笹
2噴射弁12゜13にはコントロールユニット14(マ
イクロコンピュータ)からの燃料制御信号として燃料噴
射パルスが出力され、その噴射パルス幅に応じた所定口
の燃料噴射を行う。In the first intake passage 7a, a first injection valve 12 for injecting fuel in all operating ranges including the low intake 5H range is disposed for each cylinder, and in the second intake passage 7b.
A second injection valve 13 for injecting fuel in a high intake air amount region is provided for each cylinder. A fuel injection pulse is output as a fuel control signal from the control unit 14 (microcomputer) to the first and second injection valves 12 and 13, and fuel is injected at a predetermined port according to the width of the injection pulse.
上記コントロールユニット14には前記吸入空気量検出
手段9からの吸気量信号が入力されるとともに、回転数
センサー15からエンジン回転数信号が入ツノされ、両
信号に対応して燃料噴射口および時期(噴射回数)を演
算して所定時期に所定パルス幅を有する燃料噴射パルス
を各噴射弁12゜13に出ノjする。The control unit 14 receives an intake air amount signal from the intake air amount detecting means 9, and also receives an engine rotation speed signal from the rotation speed sensor 15. The fuel injection pulse having a predetermined pulse width is output to each injection valve 12 and 13 at a predetermined time by calculating the number of injections.
そして、上記高温嶽域用の第2噴劃弁13の燃圧は低流
量域用の第1噴射弁12の燃圧より高く設定されている
。すなわち、第2図に第1噴射弁12および第2噴射弁
13に対する燃料系統を示し、燃料タンク16の燃料は
、燃料ポンプ17からフィルター18を介して燃料供給
通路19によって並列に接続された第1噴射弁12およ
び第2噴射弁13に供給されるものであり、第1噴射弁
12と第2噴射弁13との間には絞り20が介装されて
、この第2噴射弁13側の圧力が第1噴射弁12側の圧
力より」:昇可能にしている。吸気圧力に対応して噴射
圧力を調整刃−るプレッシャレギュレータ21.22は
、第1噴射弁12に対するプレッシャレギュレータ21
の設定圧より第2噴射弁13に対するプレッシャレギュ
レータ22の設定圧が高くされ、これにより第2噴射弁
13の燃圧が所定値だ(プ第1噴射弁12より高くなる
ように設(プられている。The fuel pressure of the second injection valve 13 for the high temperature region is set higher than the fuel pressure of the first injection valve 12 for the low flow region. That is, FIG. 2 shows a fuel system for the first injection valve 12 and the second injection valve 13, and the fuel in the fuel tank 16 is supplied from a fuel pump 17 via a filter 18 to a fuel supply passage 19 connected in parallel. This is supplied to the first injection valve 12 and the second injection valve 13, and a throttle 20 is interposed between the first injection valve 12 and the second injection valve 13. The pressure can be increased from the pressure on the first injection valve 12 side. The pressure regulators 21 and 22 that adjust the injection pressure in accordance with the intake pressure are the pressure regulators 21 and 22 for the first injection valve 12.
The set pressure of the pressure regulator 22 for the second injector 13 is set higher than the set pressure of the first injector 12. There is.
第3図は上記コン]・ロールユニット14の動作を説明
するだめのフローチャー1・であり、スタート後、ステ
ップS1で運転状態に対応づ−る燃料噴射量を演算する
ものであって、吸入空気量検出手段9による吸入空気m
oa 、回転数センサー15によるエンジン回転数N1
定数K、補正係数αなどから燃F31 @射パルス幅τ
(噴射時間)をめる。FIG. 3 is a flowchart 1 for explaining the operation of the control unit 14. After the start, in step S1, the fuel injection amount corresponding to the operating condition is calculated. Intake air m by air amount detection means 9
oa, engine rotation speed N1 determined by rotation speed sensor 15
From constant K, correction coefficient α, etc., fuel F31 @ injection pulse width τ
Increase (injection time).
なお、補正係数αは冷間時等の補正を行うためのもので
あり、加算補正値τ0は燃料噴射パルスが第1もしくは
第2噴削弁12.”13に出力されても、実際に燃料の
噴射が開始されるまでに一定時間を要することから、こ
の立上りの時間を補正するためのものである。また、τ
aは冷間補正等を加味した基本噴射時間であり、τbは
加速増最時間である。Note that the correction coefficient α is used to correct for cold times, etc., and the additional correction value τ0 is used when the fuel injection pulse is the first or second injection valve 12. 13, it takes a certain amount of time for fuel injection to actually start, so this purpose is to correct this rise time. Also, τ
a is the basic injection time taking cold correction etc. into consideration, and τb is the maximum acceleration increase time.
続いて、第2噴射弁13の燃料噴射を開始する設定パル
ス幅τVを読出しくS2)、前記ステップS1で演算し
た噴射パルス幅τa十τbがこの設定パルス幅τV以上
かどうかを判断しくS3)、この判断がNo(低吸気■
域)のときには非同期加速スイッチがオンかどうかを判
断しくS4)、非同期加速スイッチがオン(YES)と
なっている大ぎな加速状態のときにはステップS5で非
同期噴射を行う一方、この非同期加速スイッチがオフ(
No>のときには非同期噴射を行うことなく、第1噴劃
弁12用の噴射パルスτpと第2噴射弁13用の噴射パ
ルスτSとを演算する(S6)。Next, the set pulse width τV for starting fuel injection from the second injector 13 is read out (S2), and it is determined whether the injection pulse width τa + τb calculated in step S1 is greater than or equal to the set pulse width τV (S3). , this judgment is No (low intake ■
If the asynchronous acceleration switch is on (YES), it is determined whether the asynchronous acceleration switch is on (S4), and when the asynchronous acceleration switch is on (YES) and there is a large acceleration state, asynchronous injection is performed in step S5, while this asynchronous acceleration switch is off. (
No>, the injection pulse τp for the first injection valve 12 and the injection pulse τS for the second injection valve 13 are calculated without performing asynchronous injection (S6).
上記低吸気聞域では、第2噴射弁13用の噴射パルスτ
Sが零に設定されており、この第2噴射弁13から−の
燃料噴射を行うことなく、第1噴射弁12のみによって
ステップS1でめた噴射パルス幅τpの制御信号によっ
て第1噴射弁12を駆動して燃料噴射を行う(810)
。In the above-mentioned low intake air region, the injection pulse τ for the second injection valve 13 is
S is set to zero, and the first injector 12 is controlled by the control signal of the injection pulse width τp determined in step S1 only by the first injector 12 without injecting negative fuel from the second injector 13. to perform fuel injection (810)
.
一方、上記ステップS3の判断がYESで高吸気置載の
ときには、同様に非同期加速スイッチがオンかどうかを
判断しくS7)、非同期加速スイッチがオン(YES>
となっている大きな加速状態のときにはステップS8で
非同期噴射を行う一方、非同期加速スイッチがオフ(N
o)のときには非同期噴射を行うことなく、第1噴剣弁
12用の噴射パルスτpと第2噴躬弁13用の噴射パル
スτSとを演算しくS9)、この制御信号によって第1
および第2噴射弁12.13を駆動して燃料噴射を行う
(S 10)。なお、この例では、第1噴射弁12と第
2噴射弁13とは同舟(半分ずつ)の燃料を噴射するよ
うに設定されている。On the other hand, if the determination in step S3 is YES and the high intake air is placed, it is similarly determined whether the asynchronous acceleration switch is on (S7), and the asynchronous acceleration switch is on (YES>
When the acceleration state is large, asynchronous injection is performed in step S8, while the asynchronous acceleration switch is turned off (N
o), the injection pulse τp for the first injection valve 12 and the injection pulse τS for the second injection valve 13 are calculated without performing asynchronous injection (S9), and this control signal causes the first injection pulse to be calculated.
Then, the second injection valve 12.13 is driven to perform fuel injection (S10). In this example, the first injection valve 12 and the second injection valve 13 are set to inject the same amount of fuel (half each).
上記燃料噴射において、高噴射量域で非同期噴射を行う
場合の噴射パルスτp、τSの出力は、第4図に示すよ
うになる。In the above fuel injection, the outputs of the injection pulses τp and τS when performing asynchronous injection in a high injection amount range are as shown in FIG.
第5図は変形例を示すものであって、この例においては
エンジン1の各気筒2には1つの吸気ボー1−3と排気
ポート5とが形成され、吸気ボート3に1つの吸気通路
7が接続され、絞り弁10より下流の拡張室7Cからそ
れぞれ各気筒2に接続された吸気通路7に燃焼v2に近
い下流側に第11111躬弁12が、これより上流側に
第2噴射弁13がそれぞれ配設され、この第1噴射弁1
2および第2噴射弁13に前例と同様のフントロールユ
ニッ]・14によって燃料噴射パルスが出力され、その
噴11JfM、切換時期が制御されるもので、その他は
前例と同様に設けられ、第2噴射弁13の燃圧が第1噴
射弁12の燃圧より高く設定されている。FIG. 5 shows a modified example, in which each cylinder 2 of the engine 1 is formed with one intake bow 1-3 and an exhaust port 5, and the intake boat 3 has one intake passage 7. is connected to the intake passage 7 connected to each cylinder 2 from the expansion chamber 7C downstream of the throttle valve 10, the 11111st valve 12 is connected to the downstream side near the combustion v2, and the second injection valve 13 is connected to the upstream side of this. are arranged respectively, and this first injection valve 1
2 and the second injection valve 13, a fuel injection pulse is outputted by the same fuel injection valve 14 as in the previous example, and its injection 11JfM and switching timing are controlled. The fuel pressure of the injection valve 13 is set higher than the fuel pressure of the first injection valve 12.
なa5、上記実施例において、第1図および第5図に示
すように第1噴射弁12は比較的燃焼室2に近い吸気通
路7の下流側部分に配設し、この第1噴躬弁12から噴
射された燃料が速やかに燃焼室2に供給されるようにし
て、吸気量の増減に対する燃料の応答性を良好にしてい
るものであり、一方、第2噴射弁13は第1噴射弁12
より上流側の吸気通路7に配設して噴QJ燃料と吸気と
の混合、微粒化を良好にして、霧化を促進するようにし
ているものである。a5. In the above embodiment, as shown in FIGS. 1 and 5, the first injection valve 12 is disposed in the downstream portion of the intake passage 7 relatively close to the combustion chamber 2, and this first injection valve The fuel injected from the first injector 12 is quickly supplied to the combustion chamber 2 to improve the responsiveness of the fuel to increases and decreases in the amount of intake air. 12
It is disposed in the intake passage 7 on the more upstream side to improve mixing and atomization of the injected QJ fuel and intake air, thereby promoting atomization.
また、第1の吸気通路7aを流れる吸気量を制御する第
1の絞り弁10は、第1図のように第1の吸気通路7a
の入口部に介設するほか、第2の絞り弁11より上流側
の吸気通路7に介設しても同様の制御作用が得られる。Further, the first throttle valve 10 that controls the amount of intake air flowing through the first intake passage 7a is connected to the first intake passage 7a as shown in FIG.
In addition to intervening at the inlet of the second throttle valve 11, the same control effect can be obtained by interposing it in the intake passage 7 upstream of the second throttle valve 11.
さらに、第1噴射弁12と第2噴射弁13との燃圧を変
更する構造としては、上記第2図に示すもののほか、例
えば別系統にしてそれぞれ燃料ポンプを配設するなど公
知の技術が適宜採用可能である。Furthermore, as a structure for changing the fuel pressure between the first injection valve 12 and the second injection valve 13, in addition to the structure shown in FIG. Adoptable.
第1図は本発明の一実施例におけるエンジンの燃料噴射
装置の概略構成図、
第2図は噴射弁に対する燃料供給系統を示す系統図、
第3図はコントロールユニットのフローチャート図、
第4図は第3図によって噴射弁に出力される燃料噴射パ
ルスの一例を示す説明図、
第5図は変形例におけるエンジンの燃料噴射装置の1駅
路構成図である。
1・・・・・・エンジン 2・・・・・・燃焼室3.4
・・・・・・吸気ボート
7.7a、7b・・・・・・吸気通路
10.11・・・・・・絞り弁
12・・・・・・第1噴射弁 13・・・・・・第2噴
射弁14・・・・・・コントロールユニット17・・・
・・・燃料ポンプ
21.22・・・・・・プレッシャレギュレータ第1図
0645” 4p<bpp b
1N2図
114図
rs m■
iIB図
@5図FIG. 1 is a schematic configuration diagram of an engine fuel injection device according to an embodiment of the present invention, FIG. 2 is a system diagram showing a fuel supply system to an injection valve, FIG. 3 is a flowchart diagram of a control unit, and FIG. FIG. 3 is an explanatory diagram showing an example of the fuel injection pulse output to the injection valve, and FIG. 5 is a one-stop configuration diagram of the engine fuel injection device in a modified example. 1...Engine 2...Combustion chamber 3.4
...Intake boat 7.7a, 7b ...Intake passage 10.11 ... Throttle valve 12 ... First injection valve 13 ... Second injection valve 14...Control unit 17...
...Fuel pump 21.22...Pressure regulator Fig. 1 0645"4p<bpp b 1N2 Fig. 114 Fig. rs m ■ iIB Fig. @ Fig. 5
Claims (1)
1噴躬弁と、高吸気量域で燃料を噴射する第2噴射弁と
を備えたエンジンの燃料噴射装置において、上記第2噴
射弁の燃圧を第1噴射弁の燃圧より高く設定したことを
特徴とするエンジンの燃料噴射装置。(1) In an engine fuel injection device comprising a first injection valve that injects fuel in the entire operating range including a low intake area, and a second injection valve that injects fuel in a high intake air amount area, A fuel injection device for an engine, characterized in that the fuel pressure of two injection valves is set higher than the fuel pressure of a first injection valve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58213881A JPS60108546A (en) | 1983-11-14 | 1983-11-14 | Fuel injection device of engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58213881A JPS60108546A (en) | 1983-11-14 | 1983-11-14 | Fuel injection device of engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS60108546A true JPS60108546A (en) | 1985-06-14 |
JPH0137585B2 JPH0137585B2 (en) | 1989-08-08 |
Family
ID=16646558
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58213881A Granted JPS60108546A (en) | 1983-11-14 | 1983-11-14 | Fuel injection device of engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60108546A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63179148A (en) * | 1987-01-20 | 1988-07-23 | Mazda Motor Corp | Fuel control device for fuel injection type engine |
JP2011058435A (en) * | 2009-09-10 | 2011-03-24 | Toyota Motor Corp | Fuel injection device for internal combustion engine |
-
1983
- 1983-11-14 JP JP58213881A patent/JPS60108546A/en active Granted
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63179148A (en) * | 1987-01-20 | 1988-07-23 | Mazda Motor Corp | Fuel control device for fuel injection type engine |
JP2011058435A (en) * | 2009-09-10 | 2011-03-24 | Toyota Motor Corp | Fuel injection device for internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
JPH0137585B2 (en) | 1989-08-08 |
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