JPS63106356A - Fuel feed device for engine - Google Patents

Fuel feed device for engine

Info

Publication number
JPS63106356A
JPS63106356A JP25347986A JP25347986A JPS63106356A JP S63106356 A JPS63106356 A JP S63106356A JP 25347986 A JP25347986 A JP 25347986A JP 25347986 A JP25347986 A JP 25347986A JP S63106356 A JPS63106356 A JP S63106356A
Authority
JP
Japan
Prior art keywords
fuel injection
fuel
air
injection valve
engine
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.)
Pending
Application number
JP25347986A
Other languages
Japanese (ja)
Inventor
Noboru Hashimoto
昇 橋本
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor 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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP25347986A priority Critical patent/JPS63106356A/en
Publication of JPS63106356A publication Critical patent/JPS63106356A/en
Pending legal-status Critical Current

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  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE:To enhance the economy of fuel consumption and the output power of an engine, by providing an auxiliary air supply means for feeding directed air into injected fuel, in the vicinity of the fuel injection part of a fuel injection valve, and by enabling the feed direction of the auxiliary air to be changed in accordance with the operating condition of the engine. CONSTITUTION:In an engine in which a fuel injection valve 21 is disposed in a secondary air passage 9 in an intake-air pipe 10 in the vicinity of a fuel combustion chamber, the fuel injection valve 21 is attached to the injection valve attaching part 22 of the intake-air pipe 10 through the intermediary of a receptacle 23. Further, an assist air supply device 24 including an assist air passage 25 is disposed between the fuel injection valve attaching part 22 and a section upstream of a throttle valve. This supply device 24 is adapted to selectively feed air into assist air introduction parts 27, 28 in the fuel injection valve attaching part 22 under the control of a three- way solenoid valve 26. These introduction parts 27, 28 are arranged to be communicated with first and second ring grooves 21, 32 formed respectively in a communication hole 34 facing in opposite to the direction of fuel injection and a communication hole facing in the direction of fuel injection which are formed in the receptacle 23.

Description

【発明の詳細な説明】 (産業上の利用分野) この発明は、燃料噴射弁の燃料噴射部近傍にアシストエ
アを供給するようなエンジンの燃料供給装置に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a fuel supply device for an engine that supplies assist air to the vicinity of a fuel injection portion of a fuel injection valve.

(従来技術) 従来、燃焼室もしくは燃焼室近傍の吸気通路に、燃料を
供給する燃料噴射弁を設け、この燃料噴射弁で燃料を直
接供給するエンジンの燃料供給装置では、燃焼室と燃料
噴射弁の噴口との距離が短いことその他に起因して、気
化器タイプの燃料供給装置に比較して、燃料の気化霧化
が悪い問題点があった。
(Prior art) Conventionally, a fuel injection valve for supplying fuel is provided in the combustion chamber or an intake passage near the combustion chamber, and in an engine fuel supply system that directly supplies fuel with this fuel injection valve, the combustion chamber and the fuel injection valve are Due to the short distance from the nozzle, etc., there was a problem in that fuel vaporization was poor compared to a carburetor type fuel supply device.

このため従来、例えば、特開昭59−7772号公報に
記載のように、上述の燃料噴射弁の燃料噴射部近傍に、
エアフローメータ下流部で、かつスロットル弁上流側の
エア(アシストエア)を供給する空気通路を設けて、こ
の空気通路からのアシストエアにより燃料の気化霧化を
向上するように成したエンジンの燃料供給装置が既に発
明されている。
For this reason, conventionally, for example, as described in Japanese Unexamined Patent Publication No. 59-7772, near the fuel injection part of the above-mentioned fuel injection valve,
An engine fuel supply system in which an air passage is provided downstream of the air flow meter and upstream of the throttle valve to supply air (assist air), and the assist air from this air passage improves fuel vaporization and atomization. A device has already been invented.

しかし、この従来装置においては、燃料の気化霧化およ
び空気とのミキシングの向上を図ることができる利点が
ある反面、上述のアシストエアの供給方向が、燃料噴射
方向に対して直交づる方向であるから、特に加速時にお
いては、噴射燃料に対するアシストエアの衝突弁だけ燃
料供給が遅れて、加速応答性が悪くなる問題点を有して
いた。
However, although this conventional device has the advantage of improving fuel vaporization and mixing with air, the above-mentioned assist air supply direction is perpendicular to the fuel injection direction. Therefore, especially during acceleration, the fuel supply is delayed by the collision valve of the assist air with respect to the injected fuel, resulting in a problem that the acceleration response becomes poor.

(発明の目的) この発明は、エンジンの運転状態に応じてアシストエア
の供給方向を変更することで、燃費の向上や、加速応答
性の向上等の運転状態に応じた性能の向上を図ることが
できるエンジンの燃料供給装置の提供を目的とする。
(Purpose of the Invention) The present invention aims to improve performance according to the driving conditions, such as improving fuel efficiency and acceleration response, by changing the supply direction of assist air according to the driving conditions of the engine. The purpose is to provide an engine fuel supply system that can perform

(発明の構成) この発明は、燃焼室もしくは吸気通路に、燃料を供給す
る燃料噴射弁と、上記燃料噴射弁の燃料噴射部近傍に、
該燃料噴射弁により噴射された燃料に指向エアを供給す
る補助エア供給手段と、燃料の噴射方向に対する補助エ
アの供給方向を、運転状態に応じて変速制御する制御手
段とを備えたエンジンの燃料供給装置であることを特徴
とする。
(Structure of the Invention) The present invention provides a fuel injection valve that supplies fuel to a combustion chamber or an intake passage, and a fuel injection valve near a fuel injection part of the fuel injection valve.
Fuel for an engine, comprising: auxiliary air supply means for supplying directional air to fuel injected by the fuel injection valve; and control means for controlling the supply direction of the auxiliary air with respect to the fuel injection direction in accordance with operating conditions. It is characterized by being a supply device.

(発明の効果) この発明によれば、上述の制御手段で運転状態に応じた
燃料の霧化状態の変更ができ、運転状態に応じた性能の
向上を図ることができる。
(Effects of the Invention) According to the present invention, the atomization state of the fuel can be changed according to the operating state using the above-mentioned control means, and the performance can be improved depending on the operating state.

(実施例) この発明の一実施例を以下図面に基づいて詳述する。(Example) An embodiment of the present invention will be described in detail below based on the drawings.

図面は、エンジンの燃料供給装置を示し、第1図におい
て、エアクリーナ1の浄化空気出口にエア70−メータ
2を接続し、このエア70−メータ2の後位にはスロッ
トルボディ3を連通している。
The drawing shows a fuel supply system for an engine. In FIG. 1, an air 70-meter 2 is connected to the purified air outlet of an air cleaner 1, and a throttle body 3 is connected to the rear of the air 70-meter 2. There is.

そして、上述のスロットルボディ3内のスロットルチャ
ンバ4にスロットル弁5を配設すると共に、スロットル
ボディ3外には上述のスロットル弁5の開度を検出する
スロットル開度センサ6を配設している。
A throttle valve 5 is disposed in the throttle chamber 4 within the throttle body 3, and a throttle opening sensor 6 for detecting the opening of the throttle valve 5 is disposed outside the throttle body 3. .

また上述のスロットルボディ3の後位には、燃焼室7に
供給される混合気に同燃焼室7における周方向のスワー
ルを与えるスワール生成手段としての1次通路8と、2
次通路9とを備えた1ユアルインダクシヨンシステムD
ISの吸気管10を接続している。
Further, at the rear of the above-mentioned throttle body 3, there is a primary passage 8 as a swirl generating means for giving the air-fuel mixture supplied to the combustion chamber 7 a circumferential swirl in the combustion chamber 7;
1 user induction system D with next passage 9
The IS intake pipe 10 is connected.

上述の低負荷用の1次通路8と、高負荷用の2次通路9
とからなる吸気ボート11には吸気弁12を配設する一
方、排気ポート13には排気弁14を配設している。
The above-mentioned primary passage 8 for low loads and secondary passage 9 for high loads
An intake valve 12 is disposed in the intake boat 11 consisting of the above, and an exhaust valve 14 is disposed in the exhaust port 13.

上述の各ボート11.13を形成したシリンダヘッド1
5の下部にシリンダブロック16を取付け、このシリン
ダブロック16内にピストン17を配設している。
Cylinder head 1 forming each boat 11.13 mentioned above
A cylinder block 16 is attached to the lower part of the cylinder block 5, and a piston 17 is disposed within the cylinder block 16.

さらに前述の吸気管10における2次通路9内には、ア
クチュエータ18でI7!!閉操作される開閉弁19を
配設する一方、前述の排気ポート13には排気マニホル
ド20を接続している。
Further, in the secondary passage 9 of the above-mentioned intake pipe 10, an actuator 18 is connected to I7! ! An on-off valve 19 that is closed is provided, and an exhaust manifold 20 is connected to the exhaust port 13 described above.

ところで、前述の燃焼室7近傍の吸気通路としての吸気
管10の2次通路9には燃料を供給する燃料噴射弁21
をl!!設している。
By the way, a fuel injection valve 21 that supplies fuel is connected to the secondary passage 9 of the intake pipe 10 as an intake passage near the combustion chamber 7.
l! ! It is set up.

上述の燃料噴射弁21は第2図に示す如く、吸気管10
の噴射弁取付部22にソケット23を介して配設する一
方、この燃料噴射弁21の燃料噴射部近傍と、エアフロ
−メータ2下流部およびスロットル弁5上流部間との間
にはアシストエア供給装置24を配設している。
The above-mentioned fuel injection valve 21 is connected to the intake pipe 10 as shown in FIG.
is installed in the injection valve mounting part 22 of the fuel injection valve 21 via a socket 23, while assist air is supplied between the vicinity of the fuel injection part of the fuel injection valve 21 and the downstream part of the air flow meter 2 and the upstream part of the throttle valve 5. A device 24 is provided.

このアシストエア供給装置i!24は、上述のエアフロ
−メータ2下流部とスロットル弁5h流部との問からア
シストエアを導出するアシストエア通路25と、このア
シストエア通路25の先端に取付けた3方ソレノイド弁
26と、この3方ソレノイド弁26の操作により噴射弁
取付部22におけるアシストエア導入路27.28に選
択的にエアを供給する第1通路2つおよび第2通路30
とを備えている。
This assist air supply device i! Reference numeral 24 denotes an assist air passage 25 that leads out assist air from the downstream part of the air flow meter 2 and the downstream part of the throttle valve 5h, a three-way solenoid valve 26 attached to the tip of this assist air passage 25, and Two first passages and a second passage 30 that selectively supply air to the assist air introduction passages 27 and 28 in the injection valve mounting portion 22 by operating the three-way solenoid valve 26.
It is equipped with

上述のアシストエア導入路27.28はソケット23の
外周部に形成した第1および第2の各輪溝31.32に
それぞれ連通し、一方の第1輪溝31には、同ソケット
23内の孔部33と連通し、かつ燃料の噴射方向(第2
図の矢印a方向)と対向する方向の連通孔34を穿設し
、他方の第2通路30には、ソケット23内の孔部33
と連通し、かつ燃料の噴射方向と略同方向に向く連通孔
35を穿設している。
The above-mentioned assist air introduction passages 27 and 28 communicate with the first and second annular grooves 31 and 32 formed on the outer periphery of the socket 23, respectively. communicates with the hole 33 and in the fuel injection direction (second
A communication hole 34 is formed in the direction opposite to the arrow a direction in the figure, and the other second passage 30 is provided with a hole 33 in the socket 23.
A communication hole 35 is provided which communicates with the fuel and faces substantially the same direction as the fuel injection direction.

ところで、CPU40は第1図に示す吸入空気組信号、
スロットル開度信号、エンジン回転数信号、クランク角
信号、アクセル位置信号の入力に基づいてROM3Bに
格納されたプログラムに沿って、開開弁19用のアクチ
ュエータ18、燃料噴射弁21および3方ソレノイド弁
26を駆動制御し、またRAM39は加速判定アクセル
微分値K(第3図参照)などの必要なデータを記憶づる
By the way, the CPU 40 receives the intake air group signal shown in FIG.
The actuator 18 for the opening/opening valve 19, the fuel injection valve 21, and the three-way solenoid valve are activated in accordance with the program stored in the ROM 3B based on the input of the throttle opening signal, engine speed signal, crank angle signal, and accelerator position signal. 26, and a RAM 39 stores necessary data such as acceleration determination accelerator differential value K (see FIG. 3).

ここで、上述のCPLJ40は減速時に3方ソレノイド
弁26を操作してアシストエア通路25と第1通路29
とを連通ずることで、燃料の噴射方向に対する補助エア
の供給方向を、噴射方向と対向する方向に制御する一方
、加速時には3方ソレノイド弁26の操作で、アシスト
エア通路25と第2通路30とを連通させて、燃料の噴
射方向に対する補助エアの供給方向を、噴射方向と同方
向に変更制御する。
Here, the above-mentioned CPLJ 40 operates the three-way solenoid valve 26 during deceleration to control the assist air passage 25 and the first passage 29.
By communicating with the assist air passage 25 and the second passage 30, the direction in which the auxiliary air is supplied with respect to the fuel injection direction is controlled in the direction opposite to the injection direction. The supply direction of the auxiliary air relative to the fuel injection direction is controlled to be changed to the same direction as the injection direction.

このように構成したエンジンの燃料供給装置の動作を第
3図のフローチャートを参照して説明する。
The operation of the engine fuel supply system configured as described above will be explained with reference to the flowchart shown in FIG.

第1ステツプ41で、CI) U 40は入力されるア
クセル位置信号に基づいて、アクセル位置をモニターす
る。
In a first step 41, the CI U 40 monitors the accelerator position based on the input accelerator position signal.

次に第2ステツプ42で、CPtJ40はアクセル微分
値Itつまりアクセル変化率を演算する。
Next, in a second step 42, the CPtJ 40 calculates the accelerator differential value It, that is, the accelerator change rate.

次に第3ステツプ43で、CPU40は上述の演算結果
としてのアクセル微分値tが予め設定した加速判定アク
セル微分値によりも大か否か、換言すればエンジンの運
転状態が加速状態にあるかを判定する。
Next, in a third step 43, the CPU 40 determines whether the accelerator differential value t as the result of the above calculation is larger than a preset acceleration judgment accelerator differential value, in other words, whether the engine operating state is in an accelerating state. judge.

上述の第3ステツプ43で、t>Kと判定した際には次
の第4ステツプ44に移行する一方、t≦にと判定した
際には別の第5ステツプ45に移行する。
In the third step 43 described above, when it is determined that t>K, the process proceeds to the next fourth step 44, while when it is determined that t≦, the process proceeds to another fifth step 45.

上述の第4ステツプ44で、CPU40は第2図に示す
3方ソレノイド弁26を操作してアシストエア通路25
と第2通路30とを連通させる。
In the fourth step 44 described above, the CPU 40 operates the three-way solenoid valve 26 shown in FIG.
and the second passage 30 are communicated with each other.

この結果、アシストエア通路25からの補助エアは各要
素26.30.28.35をこの順に介して燃料噴射方
向と同方向に供給されるので、t〉Kの加速時において
は主として加速応答性の向上を図ることができる効果が
ある。
As a result, since the auxiliary air from the assist air passage 25 is supplied in the same direction as the fuel injection direction through each element 26, 30, 28, 35 in this order, during acceleration at t>K, the acceleration response is mainly affected. This has the effect of improving the

一方、前述の第5ステツプ45では、CPU40は第2
図の3方ソレノイド弁26を操作してアシストエア通路
25と第1通路29とを連通させる。
On the other hand, in the fifth step 45 described above, the CPU 40
The three-way solenoid valve 26 shown in the figure is operated to connect the assist air passage 25 and the first passage 29.

この結果、アシストエア通路25からの補助エアは各要
素26.29,27.34をこの順に介して燃料噴射方
向に対向する方向から供給されるので、t≦にの非加速
時においては主として燃費の向上を図ることができる効
果がある。
As a result, since the auxiliary air from the assist air passage 25 is supplied from the direction opposite to the fuel injection direction via each element 26, 29, 27, 34 in this order, the main fuel consumption is This has the effect of improving the

尚、本実施例においては、加速時と非速時とでアシスト
エアの供給方向を変更するもののみ示したが、低負荷運
転時、アシストエアを燃料の噴射方向と対向する方向に
、高負荷運転時、アシストエアを燃料の噴射方向と同方
向に変更しても良く、それにより、低負荷運転時におけ
る燃費の向上と、高負荷運転時における充填効率の低下
の防止を図ることができる。
In this example, only the direction in which the assist air is supplied is changed between acceleration and non-speed operation. During operation, the assist air may be changed in the same direction as the fuel injection direction, thereby improving fuel efficiency during low load operation and preventing a decrease in filling efficiency during high load operation.

この発明の構成と、上述の実施例との対応において、 この発明の吸気通路は、実施例の2次通路9に対応し、 以下同様に、 補助エア供給手段は、アシストエア供給装置24に対応
し、 !制御手段は、CPU40に対応するも、この発明は、
上述の実施例の構成のみに限定されるものではない。
In the correspondence between the structure of this invention and the above-described embodiments, the intake passage of this invention corresponds to the secondary passage 9 of the embodiment, and similarly, the auxiliary air supply means corresponds to the assist air supply device 24. death, ! Although the control means corresponds to the CPU 40, the present invention
The present invention is not limited to the configuration of the embodiment described above.

【図面の簡単な説明】[Brief explanation of the drawing]

図面はこの発明の一実施例を示し、 第1図はエンジンの燃料供給装置を示す系統図、第2図
は第1図の要部の拡大新面図、 第3図はアシストエア供給処理を示すフローチャートで
ある。 2・・・エアフローメータ 5・・・スロットル弁7・
・・燃焼室      9・・・2次通路21・・・燃
料噴射弁 24・・・アシストエア供給装置 40・・・CPU 倉、2図 第31’ZI
The drawings show an embodiment of the present invention; Fig. 1 is a system diagram showing an engine fuel supply system, Fig. 2 is an enlarged new view of the main part of Fig. 1, and Fig. 3 shows an assist air supply process. FIG. 2... Air flow meter 5... Throttle valve 7.
...Combustion chamber 9...Secondary passage 21...Fuel injection valve 24...Assist air supply device 40...CPU warehouse, Figure 2, No. 31'ZI

Claims (1)

【特許請求の範囲】[Claims] 1.燃焼室もしくは吸気通路に、燃料を供給する燃料噴
射弁と、 上記燃料噴射弁の燃料噴射部近傍に、該燃 料噴射弁により噴射された燃料に指向エア を供給する補助エア供給手段とを備えたエ ンジンの燃料供給装置であって、 燃料の噴射方向に対する補助エアの供給方 向を、運転状態に応じて変更制御する制御 手段を備えた エンジンの燃料供給装置。
1. A fuel injection valve that supplies fuel to a combustion chamber or an intake passage, and an auxiliary air supply means that supplies directional air to the fuel injected by the fuel injection valve near the fuel injection part of the fuel injection valve. What is claimed is: 1. A fuel supply device for an engine, the device comprising: control means for changing and controlling the direction of supply of auxiliary air with respect to the direction of fuel injection according to operating conditions.
JP25347986A 1986-10-23 1986-10-23 Fuel feed device for engine Pending JPS63106356A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25347986A JPS63106356A (en) 1986-10-23 1986-10-23 Fuel feed device for engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25347986A JPS63106356A (en) 1986-10-23 1986-10-23 Fuel feed device for engine

Publications (1)

Publication Number Publication Date
JPS63106356A true JPS63106356A (en) 1988-05-11

Family

ID=17251958

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25347986A Pending JPS63106356A (en) 1986-10-23 1986-10-23 Fuel feed device for engine

Country Status (1)

Country Link
JP (1) JPS63106356A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5148788A (en) * 1991-06-19 1992-09-22 Hitachi America, Ltd. Air-assist fuel injection system
WO1993008384A2 (en) * 1991-06-19 1993-04-29 Hitachi America, Ltd Air-assist fuel injection system
JPH08502723A (en) * 1992-07-27 1996-03-26 ハイブライドン インコーポレイテッド Oligonucleotide alkylphosphonothioate

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5148788A (en) * 1991-06-19 1992-09-22 Hitachi America, Ltd. Air-assist fuel injection system
WO1993008384A2 (en) * 1991-06-19 1993-04-29 Hitachi America, Ltd Air-assist fuel injection system
WO1993008384A3 (en) * 1991-06-19 1993-05-27 Hitachi Ltd Air-assist fuel injection system
JPH08502723A (en) * 1992-07-27 1996-03-26 ハイブライドン インコーポレイテッド Oligonucleotide alkylphosphonothioate

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