JPH0240041A - Fuel injection control device for 2-cycle direct injection engine - Google Patents
Fuel injection control device for 2-cycle direct injection engineInfo
- Publication number
- JPH0240041A JPH0240041A JP63191119A JP19111988A JPH0240041A JP H0240041 A JPH0240041 A JP H0240041A JP 63191119 A JP63191119 A JP 63191119A JP 19111988 A JP19111988 A JP 19111988A JP H0240041 A JPH0240041 A JP H0240041A
- Authority
- JP
- Japan
- Prior art keywords
- air
- cylinder
- fuel
- scavenging
- 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
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 65
- 238000002347 injection Methods 0.000 title claims abstract description 35
- 239000007924 injection Substances 0.000 title claims abstract description 35
- 230000002000 scavenging effect Effects 0.000 claims abstract description 52
- 238000002485 combustion reaction Methods 0.000 claims description 7
- 238000004364 calculation method Methods 0.000 claims description 5
- 238000000034 method Methods 0.000 abstract description 3
- 239000000203 mixture Substances 0.000 description 12
- 238000010586 diagram Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 235000010724 Wisteria floribunda Nutrition 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/18—Circuit arrangements for generating control signals by measuring intake air flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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
本発明は、インジェクタにより筒内へ燃料を直接噴射す
る2サイクル直噴エンジンにおける燃料噴射制御装置に
関し、詳しくは、掃気時の空気吹き抜けを加味して燃料
噴射量を定める方式に関する。The present invention relates to a fuel injection control device for a two-stroke direct injection engine in which fuel is directly injected into a cylinder by an injector, and more particularly to a method of determining a fuel injection amount by taking into account air blow-through during scavenging.
2サイクルエンジンでは、掃気ポートから給気して掃気
する際に、新気の一部の吹き抜けを生じる。このとき、
新気が燃料を含んだ混合気の場合は、燃料の吹き抜けを
招いて好ましくない。そこで、かかる燃料の吹き抜けを
防ぐため、空気のみにより掃気作用してその後にインジ
ェクタにより燃料供給する方式が提案されている。
そこで従来、上記インジェクタ付2サイクルエンジンに
関しては、例えば特開昭62−11.3819号公報の
先行技術かある。ここで、給気系として空気のみの糸路
とインジェクタにより燃料噴射される混合気の糸路とを
有し、空気のみで掃気した後に、エンジン回転数とエア
フローメータとの検出値で算出した燃料をインジェクタ
から供給して混合気を生成し、この混合気を筒内に流入
することが示されている。In a two-stroke engine, when air is supplied from the scavenging port for scavenging, some fresh air blows through. At this time,
If the fresh air is an air-fuel mixture containing fuel, this is undesirable because it causes fuel to blow through. Therefore, in order to prevent such fuel from blowing through, a method has been proposed in which only air is used for scavenging, and then fuel is supplied by an injector. Conventionally, regarding the above-mentioned two-stroke engine with an injector, there is a prior art, for example, disclosed in Japanese Patent Application Laid-open No. 11.3819/1983. Here, the air supply system has a thread path for only air and a thread path for the mixture injected by the injector, and after scavenging with air only, the fuel is calculated based on the engine rotation speed and the value detected by the air flow meter. is supplied from the injector to generate a mixture, and this mixture is shown to flow into the cylinder.
ところで、上記先行技術のものは、2種類の掃気系路を
有し、短時間の掃気時にこれらの2系路から給気する構
成であるから、構造か複雑化すると共に給気制御が煩雑
化する難点かあり、この点で筒内直噴式の方が好ましい
。
また、インジェクタからの燃料の算出にエアフローメー
タの検出値をそのまま用いているので以下の問題がある
。即ち、エアフローメータの検出値の空気の一部は掃気
時に吹き抜けて混合気形成に関与しないなめ、この吹き
抜けを加味しないで燃料を算出すると、必然的に筒内混
合気の空燃比を正確に制御できない。
本発明は、かかる点に鑑みてなされたもので、その目的
とするところは、筒内直噴式においてインジェクタの燃
料噴射量を空気の吹き抜けを加味して正確に制御できる
2サイクル直噴エンジンの燃料噴射制御装置を提供する
ことにある。By the way, the prior art described above has two types of scavenging system paths and is configured to supply air from these two paths during short-time scavenging, which makes the structure complicated and the air supply control complicated. In this respect, the in-cylinder direct injection type is preferable. Furthermore, since the detected value of the air flow meter is directly used to calculate the amount of fuel from the injector, there are the following problems. In other words, some of the air detected by the air flow meter blows through during scavenging and does not contribute to mixture formation, so if fuel is calculated without taking this blow-through into account, it is inevitable that the air-fuel ratio of the cylinder mixture will be accurately controlled. Can not. The present invention has been made in view of the above points, and its object is to provide fuel for a two-stroke direct injection engine that can accurately control the amount of fuel injected by an injector by taking into account air blow-through in a direct-in-cylinder injection type. An object of the present invention is to provide an injection control device.
上記目的を達成するため、本発明の燃料噴射制御装置は
、2サイクルエンジン本体の燃焼室に燃料噴射するイン
ジェクタを取付り、シリングの掃気ポートには空気のみ
給気する掃気ポンプを連設する2ザイクル直噴エンジン
において、アクセル開度とエンジン回転数とによる各運
転条件での掃気時の空気の吹き抜け率を定める吹き抜け
決定部と、上記吹き抜け率とエアフローメータによる吸
入空気量で筒内空気量を算出する筒内空気算出部と、上
記筒内空気量、上記エンジン回転数に基づいて燃料噴射
量を定める燃料噴射量決定部とを備えるものである。In order to achieve the above object, the fuel injection control device of the present invention is provided with an injector that injects fuel into the combustion chamber of a two-stroke engine main body, and a scavenging pump that supplies only air to the Schilling scavenging port. Seikle direct injection engines have a blow-through determination section that determines the blow-through rate of air during scavenging under various operating conditions based on the accelerator opening degree and engine speed, and a blow-through determining section that determines the amount of air in the cylinder based on the blow-through rate and the amount of intake air determined by the air flow meter. The cylinder air calculation unit includes a cylinder air calculation unit that calculates the cylinder air amount, and a fuel injection amount determination unit that determines the fuel injection amount based on the cylinder air amount and the engine rotation speed.
上記構成に基つき、各運転条件において掃気時の空気の
吹き抜け率か設定されることで、実際の筒内空気量か算
出され、この筒内空気量とエンジン回転数とに応じた燃
料噴射量か正確に定まって、筒内混合気の空燃比がi&
適副制御れるようになる。Based on the above configuration, by setting the air blow-through rate during scavenging under each operating condition, the actual amount of air in the cylinder is calculated, and the amount of fuel injection is determined according to this amount of air in the cylinder and the engine speed. is determined accurately, and the air-fuel ratio of the in-cylinder mixture is i&
You will be able to control your subordinates appropriately.
以下、本発明の一実施例を図面に基づいて説明する。
第1図において、2サイクルエンジンの全体の構成につ
いて述べると、符号1は2サイクルエンジンの本体であ
り、シリング2にピストン3か往復動可能に挿入され、
クランク室4のクランク軸5に対し偏心したコンロッド
6によりピストン3が連結し、クランク軸5にはピスト
ン3の往復動慣性力を相殺するようにバランサ7か設け
られる。
燃焼室8の頂部には点火プラグ9と筒内直接噴射式のイ
ンジェクタ10とが取付けられている。
シリング2にはピストン3によって所定のタイミンクで
開閉される排気ポート11が開口し、この排気ポート1
1と連通ずる排気管12に触媒装置13゜排気チャンバ
14.マフラー15か配設される。また、シリング2の
排気ポート11の位置から略90度すれな位置(または
排気ポート11に対向した位置)には、ピストン3によ
って所定のタイミングで開閉する掃気ポート16が開口
し、との掃気ポート16に掃気系が設けられる。
上記インジェクタ10は2流体式であって、所定の燃料
を貯えた後に加圧空気で押圧し、燃料と空気とを混合し
た状態で直接噴射するものである。
そこで、インジェクタ10の燃料通路20かフィルタ2
1、燃料ポンプ22を介して燃料タンク23に連通し、
燃料通路20の途中に調圧弁24か設けられ、常に一定
の低い燃圧(上記加圧空気より若干高い圧力)を生じる
。また、インジェクタ10の空気通路25には調圧弁2
6.アキュムレータ27.コンプレッサ28が連結し、
加圧空気を生じるようになっている。
そして、予め燃料パルスにより所定の燃料をインジェク
タ10に貯え、排気ポート11の閉じた後に空気パルス
で加圧空気を燃料に付与して噴射する。
次いで、掃気ポート16の掃気系について述べると、掃
気ポート16と連通する掃気管30に掃気ポート16開
閉時の掃気圧力波を吸収する掃気チャンバ31、掃気を
冷却するインタークーラ32を介して容積型の掃気ポン
プ33が連設される。また、掃気ポンプ33の上流のエ
アクリーナ34側とインタークーラ32の下流との・間
にはバイパス通路35が連通し、このバイパス通路35
に負荷制御用の制御弁36が設けられている。
掃気ポンプ33は伝動手段37によりクランク軸5に連
結し、エンジン出力により常にポンプを駆動して掃気圧
を生じるようになっている。
制御系について述べると、アクセルペダル40が開度変
更手段41を介して制御弁36に、アクセル開度に対し
制御弁36の開度を反比例的に開閉するように連結す、
る。また、各運転条件を定めるエンジン回転数Nとアク
セル開度φのエンジン回転数センサ42.アクセル開
ーナ34の直下流には吸入空気量Qを計測するエアフロ
ーメータ44が取付けられている。そしてエンジン回転
数センサ42,アクセル開度センサ43,エアフローメ
ータ44の信号は制御ユニット45に入力して処理され
、制御ユニット45からインジェクタ10に燃料,空気
パルスの信号を、点火プラグ9に点火信号を出力するよ
うになっている。
第2図において制御ユニット45について述べる。
先ず、エンジン回転数センサ42,アクセル開度センサ
43のエンジン回転数N,アクセル開度φが入力する運
転条件判定部46を有し、この各運転条件の信号が吹き
抜け決定部47に入力する。ここでマツプ設定部48に
は、各運転条件で予め実験的に定めた第3図のようなア
クセル開度φに対して増大関数の吹き抜け率eのマツプ
が記憶され、吹き抜け決定部47ではこのマツプを参照
して掃気時の空気の吹き抜け率Cを定める。
この吹き抜け率eとエアフローメータ4の吸入空気量Q
は筒内空気量算出部49に入力し、筒内空気量Q′をQ
’−e−Qにより算出する。筒内空気量Q′とエンジン
回転数Nとは燃料噴射量決定部50に入力し、マツプ設
定部51の目標空燃比に応じた係数αを用いて燃料噴射
量T1を、TQ′/N・αにより求め、駆動部52によ
り燃料噴射量Tiに応じた燃料,空気パルス信号をイン
ジェクタに出力するように構成される。
次いで、このように構成された2サイクル直噴エンジン
の作用について述べる。
先ず、掃気ポンプ33から吐出してインタークーラ32
により冷却される給気は、常にバイパス通路35により
吸気側に戻るように循環し、制御弁36でこの戻り量を
制限した分の掃気量がシリンダ2側に導入されることに
なる。ここで、アクセル開度φに対し制御弁36の開度
θは反比例的に設定され、アクセル開度φが小さい場合
は制御弁36の開度により多く戻されて掃気量か少なく
なるのであり、こうしてポンプ損失を生じることなくア
クセル開度φに応じた掃気量に調整される。
そこで、第1図のようにピストン3か下死点付近に位置
して排気ポート11と共に掃気ポート16を開くと、ア
クセル開度に応じた掃気量が掃気ポンプ33により加圧
され、インタークーラ32で冷却されて掃気ポート16
よりシリンダ2の内部に流入する。そして、この掃気に
より排気ポート11から残留ガスを押し出して掃気作用
するのであり、こうして短時間に空気のみの新気がシリ
ンダ2に導入される。そして、ピストン3の上昇時に掃
気ポート16 排気ポート11が閉じることで、上記
掃気が終了して圧縮行程に移行する。また、排気ポート
11が閉じた後にあらかじめ燃料パルスによりインジェ
クタ10に貯えられた所定の燃料が、空気パルスによる
加圧空気で噴射して混合気を生成する。
そして、上死点直前で点火プラク9により着火されるこ
とで燃焼するか、この場合に掃気ポート16から流入す
る掃気流に燃焼室8の頂部のインジェクタ10から適切
なタイミングおよび時間で噴射される燃料が乗り、適切
に配置された点火プラグ位置に導かれることで、点火プ
ラグ9の付近か濃い混合気になり、これにより成層燃焼
されるのである。この燃焼による爆発後にビスl〜ン3
は下降して膨脂行程に移り、排気ポート11が開いてシ
リンダ内圧により成る程度の排気が行われ、更に下死点
付近で上述のように掃気作用を件う掃気行程に戻るので
あり、こうしてエンジンを運転する。
一方、上記エンジン運転時に、第4図のフローチャート
図で示すようにエンジン回転数センサ42。
アクセル開度センサ43,エアフローメータ44でエン
ジン回転数N,アクセル開度φ,吸入空気量Qが検出さ
れ、吹き抜け決定部47で各運転条件での掃気時の空気
の吹き抜け率eがマツプを参照して定められる。そして
筒内空気量算出部49で吹き抜け率eと吸入空気量Qと
により掃気後の実際の筒内空気量Q′が算出され、燃料
噴射決定部50で筒内空気量Q′、エンジン回転数N、
目標空燃比の係数αの要素により燃料噴射量Tiか求め
られ、これに基づきインジェクタ10から燃料噴射され
る。
そこで、筒内混合気の空燃比は常に目標の一定値になり
、この空燃比の混合気の増減により負荷制御されること
になる。
なお、運転条件の決定の負荷要素にアクセル開度に代っ
てエアフローメータの吸入空気量を用いることもできる
。また、燃料噴射量の決定はマツプまたは演算式のいず
れを用いてもよい。そして、インジェクタは高圧1流体
式でもよい。Hereinafter, one embodiment of the present invention will be described based on the drawings. In FIG. 1, the overall structure of the two-stroke engine is described. Reference numeral 1 is the main body of the two-stroke engine, and a piston 3 is inserted into a sill 2 so as to be able to reciprocate.
The piston 3 is connected to the crank chamber 4 by a connecting rod 6 eccentric to the crankshaft 5, and a balancer 7 is provided on the crankshaft 5 so as to offset the reciprocating inertia of the piston 3. A spark plug 9 and an in-cylinder direct injection type injector 10 are attached to the top of the combustion chamber 8. An exhaust port 11 is opened in the cylinder 2 and is opened and closed at a predetermined timing by a piston 3.
An exhaust pipe 12 communicating with the catalytic device 13 and the exhaust chamber 14. 15 mufflers are installed. In addition, a scavenging port 16 that opens and closes at a predetermined timing by the piston 3 is opened at a position approximately 90 degrees away from the exhaust port 11 of the cylinder 2 (or a position facing the exhaust port 11). A scavenging system is provided at 16. The injector 10 is of a two-fluid type, which stores a predetermined amount of fuel and then presses it with pressurized air to directly inject the fuel and air in a mixed state. Therefore, the fuel passage 20 of the injector 10 or the filter 2
1. communicates with the fuel tank 23 via the fuel pump 22;
A pressure regulating valve 24 is provided in the middle of the fuel passage 20 to always produce a constant low fuel pressure (slightly higher pressure than the pressurized air). In addition, a pressure regulating valve 2 is provided in the air passage 25 of the injector 10.
6. Accumulator 27. The compressor 28 is connected,
It is designed to produce pressurized air. Then, a predetermined amount of fuel is stored in the injector 10 in advance by a fuel pulse, and after the exhaust port 11 is closed, pressurized air is applied to the fuel by an air pulse and the fuel is injected. Next, the scavenging system of the scavenging port 16 will be described. A scavenging pipe 30 that communicates with the scavenging port 16 is connected to a displacement type via a scavenging chamber 31 that absorbs scavenging pressure waves when the scavenging port 16 is opened and closed, and an intercooler 32 that cools the scavenging air. A scavenging pump 33 is installed in series. Further, a bypass passage 35 communicates between the air cleaner 34 side upstream of the scavenging pump 33 and the downstream side of the intercooler 32.
A control valve 36 for load control is provided. The scavenging pump 33 is connected to the crankshaft 5 by a transmission means 37, and the engine output constantly drives the pump to generate scavenging pressure. Regarding the control system, the accelerator pedal 40 is connected to the control valve 36 via the opening degree changing means 41 so that the opening degree of the control valve 36 is opened and closed in inverse proportion to the accelerator opening degree.
Ru. Also, an engine rotation speed sensor 42 that measures the engine rotation speed N and accelerator opening degree φ that determines each operating condition. An air flow meter 44 for measuring the amount of intake air Q is attached immediately downstream of the accelerator opener 34. The signals from the engine speed sensor 42, accelerator opening sensor 43, and air flow meter 44 are input to the control unit 45 and processed, and the control unit 45 sends fuel and air pulse signals to the injector 10 and ignition signals to the spark plug 9. It is designed to output . The control unit 45 will be described in FIG. First, there is a driving condition determining section 46 which inputs the engine speed N of the engine speed sensor 42, the accelerator opening φ of the accelerator opening sensor 43, and the signals of these driving conditions are input to the blow-through determining section 47. Here, the map setting section 48 stores a map of the blow-through rate e of the increasing function with respect to the accelerator opening φ, as shown in FIG. Determine the air blow-through rate C during scavenging with reference to the map. This blow-through rate e and the intake air amount Q of the air flow meter 4
is input to the cylinder air amount calculating section 49, and the cylinder air amount Q' is calculated as Q
Calculated by '-e-Q. The cylinder air amount Q' and the engine speed N are input to the fuel injection amount determination section 50, and the fuel injection amount T1 is determined by using the coefficient α according to the target air-fuel ratio of the map setting section 51, TQ'/N. α, and the driving unit 52 is configured to output fuel and air pulse signals to the injector according to the fuel injection amount Ti. Next, the operation of the two-stroke direct injection engine configured as described above will be described. First, the scavenging air is discharged from the scavenging pump 33 and sent to the intercooler 32.
The supply air cooled by the exhaust gas is always circulated back to the intake side through the bypass passage 35, and the amount of scavenged air is introduced into the cylinder 2 side by limiting this return amount with the control valve 36. Here, the opening degree θ of the control valve 36 is set in inverse proportion to the accelerator opening degree φ, and when the accelerator opening degree φ is small, more is returned to the opening degree of the control valve 36 and the amount of scavenging air decreases. In this way, the scavenging amount is adjusted to correspond to the accelerator opening degree φ without causing pump loss. Therefore, when the piston 3 is located near the bottom dead center and the scavenging port 16 is opened together with the exhaust port 11 as shown in FIG. The scavenging air is cooled by the scavenging port 16.
It flows into the inside of the cylinder 2. This scavenging air pushes out residual gas from the exhaust port 11 to perform a scavenging action, and in this way, fresh air consisting only of air is introduced into the cylinder 2 in a short period of time. Then, when the piston 3 rises, the scavenging port 16 and the exhaust port 11 close, thereby completing the scavenging and moving to the compression stroke. Further, after the exhaust port 11 is closed, a predetermined fuel stored in the injector 10 in advance by a fuel pulse is injected with pressurized air by an air pulse to generate an air-fuel mixture. Then, it is ignited by the ignition plaque 9 just before top dead center and combusted, or in this case, it is injected from the injector 10 at the top of the combustion chamber 8 into the scavenging air flow flowing in from the scavenging port 16 at appropriate timing and time. When the fuel is introduced and guided to the appropriately placed spark plug position, a rich air-fuel mixture is created near the spark plug 9, resulting in stratified combustion. After the explosion caused by this combustion,
descends and moves to the fat expansion stroke, the exhaust port 11 is opened and exhaust is performed to the extent that the cylinder internal pressure is used, and then near the bottom dead center the cylinder returns to the scavenging stroke where the scavenging action is performed as described above. Run the engine. On the other hand, when the engine is operating, as shown in the flowchart of FIG. 4, the engine rotation speed sensor 42 is activated. The engine speed N, accelerator opening φ, and intake air amount Q are detected by the accelerator opening sensor 43 and air flow meter 44, and the blow-through determining unit 47 determines the air blow-through rate e during scavenging under each operating condition by referring to a map. It is determined as follows. Then, the cylinder air amount calculating section 49 calculates the actual cylinder air amount Q' after scavenging from the blow-through rate e and the intake air amount Q, and the fuel injection determining section 50 calculates the cylinder air amount Q' and the engine rotation speed. N,
The fuel injection amount Ti is determined by the factor of the coefficient α of the target air-fuel ratio, and the fuel is injected from the injector 10 based on this. Therefore, the air-fuel ratio of the in-cylinder air-fuel mixture always remains at a constant target value, and the load is controlled by increasing or decreasing the air-fuel ratio of the air-fuel mixture. Note that the intake air amount measured by the air flow meter may be used instead of the accelerator opening degree as the load element for determining the operating conditions. Furthermore, the fuel injection amount may be determined using either a map or an arithmetic expression. The injector may be of a high-pressure single fluid type.
以上述べてきたように、本発明によれば、2サイクル直
噴エンジンのインジェクタからの燃料噴射量を、掃気時
の空気の吹き抜けを加味して筒内空気量を求め、これに
基づいて決定するので、燃料噴射量と共に筒内混合気空
燃比を正確に制御でき、燃費、エミッション、走行性を
常に良好に行い得る。
さらに、空気の吹き抜け率を定めるので、筒内空気量の
算出が容易化する。As described above, according to the present invention, the amount of fuel injected from the injector of a two-stroke direct injection engine is determined based on the amount of air in the cylinder, which is obtained by taking into account the air blow-through during scavenging. Therefore, it is possible to accurately control the in-cylinder mixture air-fuel ratio as well as the fuel injection amount, and it is possible to always maintain good fuel efficiency, emissions, and running performance. Furthermore, since the air blow-through rate is determined, calculation of the amount of air in the cylinder is facilitated.
第1図は本発明の2サイクル直噴エンジンの燃料噴射制
御装置の実施例を示す全体構成図、第2図は制御系のブ
ロック図、
第3図は空気吹き抜け率のマツプを示す図、第4図は作
用のフローチャー1〜図である。
1・・・エンジン本体、2・・・シリンダ、8・・・燃
焼室、10・・・インジェクタ、16・・・掃気ポート
、33・・・掃気ポンプ、42・・・エンジン回転数セ
ンサ、43・・・アクセル開度センサ、44・・・エア
フローメータ、45・・・制御ユニット、47・・・空
気吹き抜け決定部、49・・・筒内空気凰算出部、50
・・・燃料噴射決定部
特許出願人 富士重工業株式会社代理人 弁理士
小 橋 信 浮
量 弁理士 村 井 進FIG. 1 is an overall configuration diagram showing an embodiment of the fuel injection control device for a two-stroke direct injection engine of the present invention, FIG. 2 is a block diagram of the control system, FIG. 3 is a diagram showing a map of the air blow-through rate, and FIG. Figure 4 shows the flowchart 1 to 1 of the operation. DESCRIPTION OF SYMBOLS 1... Engine body, 2... Cylinder, 8... Combustion chamber, 10... Injector, 16... Scavenging port, 33... Scavenging pump, 42... Engine speed sensor, 43 ... Accelerator opening sensor, 44... Air flow meter, 45... Control unit, 47... Air blow-through determining section, 49... Cylinder air flow calculation section, 50
...Fuel Injection Decision Department Patent Applicant Fuji Heavy Industries Co., Ltd. Agent Patent Attorney Makoto Kobashi Ukasa Patent Attorney Susumu Murai
Claims (1)
ジェクタを取付け、シリンダの掃気ポートには空気のみ
給気する掃気ポンプを連設する2サイクル直噴エンジン
において、 アクセル開度とエンジン回転数とによる各運転条件での
掃気時の空気の吹き抜け率を定める吹き抜け決定部と、
上記吹き抜け率とエアフローメータによる吸入空気量で
筒内空気量を算出する筒内空気算出部と、上記筒内空気
量,上記エンジン回転数に基づいて燃料噴射量を定める
燃料噴射量決定部とを備えることを特徴とする2サイク
ル直噴エンジンの燃料噴射制御装置。[Claims] In a 2-stroke direct injection engine in which an injector for injecting fuel is attached to the combustion chamber of the 2-stroke engine body, and a scavenging pump for supplying only air is connected to the scavenging port of the cylinder, a blow-through determination unit that determines an air blow-through rate during scavenging under various operating conditions according to the rotation speed;
A cylinder air calculation section that calculates the cylinder air amount based on the blow-through rate and the intake air amount measured by the air flow meter, and a fuel injection amount determination section that determines the fuel injection amount based on the cylinder air amount and the engine rotation speed. A fuel injection control device for a two-stroke direct injection engine, comprising:
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63191119A JPH0240041A (en) | 1988-07-29 | 1988-07-29 | Fuel injection control device for 2-cycle direct injection engine |
| DE3924771A DE3924771A1 (en) | 1988-07-29 | 1989-07-26 | FUEL INJECTION CONTROL SYSTEM FOR A TWO-STROKE COMBUSTION ENGINE |
| GB8917307A GB2221774B (en) | 1988-07-29 | 1989-07-28 | Fuel injection control system for a two-stroke engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63191119A JPH0240041A (en) | 1988-07-29 | 1988-07-29 | Fuel injection control device for 2-cycle direct injection engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0240041A true JPH0240041A (en) | 1990-02-08 |
Family
ID=16269182
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63191119A Pending JPH0240041A (en) | 1988-07-29 | 1988-07-29 | Fuel injection control device for 2-cycle direct injection engine |
Country Status (3)
| Country | Link |
|---|---|
| JP (1) | JPH0240041A (en) |
| DE (1) | DE3924771A1 (en) |
| GB (1) | GB2221774B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05263708A (en) * | 1992-03-18 | 1993-10-12 | Hitachi Ltd | Air flow meter for internal combustion engine |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104813011A (en) * | 2012-11-29 | 2015-07-29 | 丰田自动车株式会社 | Controls for engines with superchargers |
| FR3044713B1 (en) | 2015-12-08 | 2017-12-01 | Continental Automotive France | METHOD AND DEVICE FOR DETERMINING THE FLOW OF AIR ENTERING THE INTAKE MANIFOLD OF A TWO-STROKE ENGINE |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57203821A (en) * | 1981-06-09 | 1982-12-14 | Yamaha Motor Co Ltd | Two-cycle engine equipped with scavenging pump |
| JPS61152935A (en) * | 1984-12-26 | 1986-07-11 | Fuji Heavy Ind Ltd | Air-fuel ratio controlling device |
| IT1215330B (en) * | 1987-01-09 | 1990-02-08 | Piaggio & C Spa | LOW PRESSURE FUEL INJECTION APPARATUS IN A TWO STROKE ENGINE. |
| JPH0658071B2 (en) * | 1987-01-27 | 1994-08-03 | トヨタ自動車株式会社 | Air-fuel ratio controller for two-cycle internal combustion engine |
| US4823755A (en) * | 1987-01-27 | 1989-04-25 | Toyota Jidosha Kabushiki Kaisha | Fuel injection system for an internal combustion engine |
-
1988
- 1988-07-29 JP JP63191119A patent/JPH0240041A/en active Pending
-
1989
- 1989-07-26 DE DE3924771A patent/DE3924771A1/en not_active Ceased
- 1989-07-28 GB GB8917307A patent/GB2221774B/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05263708A (en) * | 1992-03-18 | 1993-10-12 | Hitachi Ltd | Air flow meter for internal combustion engine |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8917307D0 (en) | 1989-09-13 |
| GB2221774A (en) | 1990-02-14 |
| DE3924771A1 (en) | 1990-02-01 |
| GB2221774B (en) | 1992-08-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5020504A (en) | Fuel injection control system for a two-cycle engine | |
| US5085193A (en) | Fuel injection control system for a two-cycle engine | |
| US4984540A (en) | Fuel injection control system for a two-cycle engine | |
| US5054444A (en) | Fuel injection control system for a two-cycle engine | |
| US4957089A (en) | Fuel injection control system for a two-cycle engine | |
| JPH02169818A (en) | Two cycle engine | |
| US5035223A (en) | Fuel injection control system for an internal combustion engine | |
| US4907549A (en) | Scavenging system for a two-stroke-cycle engine | |
| US5031594A (en) | Idle speed control system for a two-cycle engine | |
| US4969435A (en) | Idle speed control system for a two-cycle engine | |
| US5690063A (en) | Engine control system | |
| US5613468A (en) | Fuel injection control | |
| JPH0264248A (en) | Engine braking device for two cycle direct injection engine | |
| JPH04179847A (en) | Fuel injection controlling apparatus | |
| JPH04370343A (en) | Idle rotation speed control device for two-cycle engine | |
| US4981127A (en) | Fuel injection control system for a two-cycle engine | |
| JPH0240041A (en) | Fuel injection control device for 2-cycle direct injection engine | |
| JP3006221B2 (en) | Idling control system for in-cylinder injection internal combustion engine | |
| US5022367A (en) | Engine brake system of a two-cycle engine for a motor vehicle | |
| JPH0264239A (en) | Engine braking device for two cycle direct injection engine | |
| JPH033935A (en) | Fuel injection control device for two-cycle direct injection engine | |
| JPH02238168A (en) | Two cycle direct injection type engine | |
| JPH01280659A (en) | Load control device for 2-cycle engine | |
| JP3010077B2 (en) | Fuel injection control device for two-cycle multi-cylinder engine | |
| JPS59122757A (en) | Idle rotation controller for internal-combustion engine |