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JP2522409B2 - Fuel injection control device for two-cycle internal combustion engine - Google Patents
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JP2522409B2 - Fuel injection control device for two-cycle internal combustion engine - Google Patents

Fuel injection control device for two-cycle internal combustion engine

Info

Publication number
JP2522409B2
JP2522409B2 JP1243305A JP24330589A JP2522409B2 JP 2522409 B2 JP2522409 B2 JP 2522409B2 JP 1243305 A JP1243305 A JP 1243305A JP 24330589 A JP24330589 A JP 24330589A JP 2522409 B2 JP2522409 B2 JP 2522409B2
Authority
JP
Japan
Prior art keywords
air
fuel injection
valve
fuel ratio
injection time
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.)
Expired - Fee Related
Application number
JP1243305A
Other languages
Japanese (ja)
Other versions
JPH03107553A (en
Inventor
雄彦 広瀬
憲一 野村
辰夫 小林
啓 野村
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.)
Toyota Motor Corp
Original Assignee
Toyota 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP1243305A priority Critical patent/JP2522409B2/en
Publication of JPH03107553A publication Critical patent/JPH03107553A/en
Application granted granted Critical
Publication of JP2522409B2 publication Critical patent/JP2522409B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two

Landscapes

  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は2サイクル内燃機関の燃料噴射制御装置に関
する。
The present invention relates to a fuel injection control device for a two-cycle internal combustion engine.

〔従来の技術〕[Conventional technology]

2サイクル内燃機関では機関シリンダ内に供給された
吸入空気の全てが燃焼に寄与せず、一部の吸入空気は燃
焼に寄与することなく排気通路内に吹き抜ける。従って
機関シリンダ内に供給される吸入空気量を求めてこの吸
入空気量から空燃比が目標空燃比となるように燃料噴射
量を決定すると一部の吸入空気が吹き抜けるために機関
シリンダ内の実際の空燃比は目標空燃比よりもリッチ側
となり、機関シリンダ内の実際の空燃比を目標空燃比に
一致させることができない。
In a two-cycle internal combustion engine, all of the intake air supplied to the engine cylinder does not contribute to combustion, and some intake air blows into the exhaust passage without contributing to combustion. Therefore, if the amount of intake air supplied to the engine cylinder is determined and the fuel injection amount is determined from this intake air amount so that the air-fuel ratio becomes the target air-fuel ratio, a part of the intake air will blow through, and the actual The air-fuel ratio becomes richer than the target air-fuel ratio, and the actual air-fuel ratio in the engine cylinder cannot match the target air-fuel ratio.

ところで吸入空気の吹き抜け量は機関の運転状態に応
じて変化するが特定の定常運転状態における吹き抜け量
は一定となる。従って種々の定常運転状態における吹き
抜け量を予め実験により求めておけば現在の機関の運転
状態がわかれば吸入空気の吹き抜け量がわかることにな
る。
By the way, the blow-through amount of intake air changes according to the operating state of the engine, but the blow-through amount in a specific steady operating state is constant. Therefore, if the blow-through amount in various steady operation states is obtained in advance by experiments, the blow-through amount of the intake air can be known if the current operating state of the engine is known.

そこで種々の定常運転状態における機関シリンダ内に
供給される吸入空気量と吹き抜け量とを実測して新気捕
捉係数{(吸入空気量−吹き抜け量)/吸入空気量}、
即ち機関シリンダ内に残る新気の割合を予め実験により
求め、この実験により求めた新気捕捉係数を予め記憶し
ておき、機関の運転状態を検出してこの運転状態に対応
する新気捕捉係数を求めると共に吸入空気量を測定し、
測定された吸入空気量と新気捕捉係数から実際に燃焼に
寄与する吸入空気量を求め、この吸入空気量から空燃比
が目標空燃比となるように燃料噴射量を決定するように
した2サイクル内燃機関が公知である(特開昭63−1832
31号公報から特開昭63−183236号公報までを参照)。こ
れらの2サイクル内燃機関では実際に燃焼に寄与する吸
入空気量に対して燃料噴射量が定められるので機関シリ
ンダ内の実際の空燃比を目標空燃比に一致せしめること
ができる。
Then, the intake air amount and the blow-through amount supplied into the engine cylinder in various steady operation states are measured to measure the fresh air trapping coefficient {(intake air amount-blowing amount) / intake air amount},
That is, the ratio of the fresh air remaining in the engine cylinder is previously obtained by an experiment, the fresh air trapping coefficient obtained by this experiment is stored in advance, and the fresh air trapping coefficient corresponding to this operating state is detected by detecting the operating state of the engine. And measure the amount of intake air,
Two cycles in which the intake air amount that actually contributes to combustion is obtained from the measured intake air amount and the fresh air capture coefficient, and the fuel injection amount is determined from this intake air amount so that the air-fuel ratio becomes the target air-fuel ratio. Internal combustion engines are known (Japanese Patent Laid-Open No. 63-1832).
31 to JP-A-63-183236). In these two-cycle internal combustion engines, the fuel injection amount is determined with respect to the intake air amount that actually contributes to combustion, so that the actual air-fuel ratio in the engine cylinder can be made to match the target air-fuel ratio.

〔発明が解決しようとする課題〕[Problems to be Solved by the Invention]

ところが定常運転時における吸入空気の吹き抜け量と
過渡運転時における吸入空気の吹き抜け量は異なり、過
渡状態が激しくなるほど定常運転時の吹き抜け量との差
が大きくなる。従って上述の2サイクル内燃機関のよう
に過渡運転時であっても定常運転時の吹き抜け量に基い
て燃料噴射量を計算すると過渡運転時には実際に燃焼に
寄与する吸入空気量が異なってくるために機関シリンダ
内の実際の空燃比を目標空燃比に一致させることができ
ないという問題がある。
However, the blow-through amount of intake air during steady operation differs from the blow-through amount of intake air during transient operation, and the difference between the blow-through amount during steady operation increases as the transient state becomes more severe. Therefore, when the fuel injection amount is calculated based on the amount of blow-through during steady operation even during transient operation such as in the above-described two-cycle internal combustion engine, the intake air amount that actually contributes to combustion differs during transient operation. There is a problem that the actual air-fuel ratio in the engine cylinder cannot match the target air-fuel ratio.

〔課題を解決するための手段〕[Means for solving the problem]

上記問題点を解決するために本発明によれば第1図の
発明の構成図に示されるように定常運転時における機関
シリンダ内の実際の空燃比が予め定められた目標空燃比
となるように定常運転状態に応じた燃料噴射時間を記憶
した燃料噴射時間記憶手段Aと、過渡運転状態を検出す
る過渡運転状態検出手段Bと、過渡運転時に機関シリン
ダ内の実際の空燃比が上述の標空燃比となるように過渡
運転状態に応じた上述の燃料噴射時間に対する補正値を
記憶した補正値記憶手段Cと、上述の燃料噴射時間と補
正値から機関の運転状態に応じた実際の燃料噴射時間を
計算する燃料噴射時間計算手段Dとを具備している。
In order to solve the above problems, according to the present invention, as shown in the configuration diagram of the invention of FIG. 1, the actual air-fuel ratio in the engine cylinder during steady operation becomes a predetermined target air-fuel ratio. Fuel injection time storage means A that stores the fuel injection time according to the steady operating state, transient operating state detecting means B that detects the transient operating state, and the actual air-fuel ratio in the engine cylinder during the transient operating state is the above-mentioned space. A correction value storage unit C that stores a correction value for the above-mentioned fuel injection time according to the transient operating state so as to obtain a fuel ratio, and an actual fuel injection time according to the operating state of the engine from the above-mentioned fuel injection time and the correction value. And a fuel injection time calculation means D for calculating

〔作 用〕[Work]

過渡運転時には期間シリンダ内の実際の空燃比が目標
空燃比となるように燃料噴射時間が補正値によって補正
される。
During the transient operation, the fuel injection time is corrected by the correction value so that the actual air-fuel ratio in the period cylinder becomes the target air-fuel ratio.

〔実施例〕〔Example〕

第2図に2サイクル内燃機関の全体図を示す。第2図
を参照すると、1はシリンダブロック、2はシリンダブ
ロック1内において往復動するピストン、3はシリンダ
ブロック1上に固締されたシリンダヘッド、4はピスト
ン2とシリンダヘッド3間に形成された燃焼室、5は給
気弁、6は給気ポート、7は排気弁、8は排気ポート、
9は燃焼室4内に向けて燃料も圧縮空気と共に噴射する
エアブラスト弁を夫々示す。図面には示さないがシリン
ダヘッド3の内壁面中央部には点火栓が配置される。給
気ポート6は給気枝管10を介してサージタンク11に連結
され、サージタンク11は機関駆動の機械式過給機12、給
気ダクト13およびエアフローメータ14を介してエアクリ
ーナ15に連結される。給気ダクト13内にはスロットル弁
16が配置される。
FIG. 2 shows an overall view of the two-cycle internal combustion engine. Referring to FIG. 2, 1 is a cylinder block, 2 is a reciprocating piston in the cylinder block 1, 3 is a cylinder head fixed on the cylinder block 1, and 4 is formed between the piston 2 and the cylinder head 3. Combustion chamber, 5 air supply valve, 6 air supply port, 7 exhaust valve, 8 exhaust port,
Reference numerals 9 respectively denote air blast valves that inject fuel into the combustion chamber 4 together with compressed air. Although not shown in the drawings, an ignition plug is disposed at the center of the inner wall surface of the cylinder head 3. The air supply port 6 is connected to a surge tank 11 via an air supply branch pipe 10, and the surge tank 11 is connected to an air cleaner 15 via an engine-driven mechanical supercharger 12, an air supply duct 13 and an air flow meter 14. It Throttle valve in the air supply duct 13
16 are placed.

第3図にエアブラスト弁9の拡大断面図を示す。第3
図を参照するとエアブラスト弁9のハウジング30内には
まっすぐに延びる圧縮空気通路31が形成され、この圧縮
空気通路31の先端部には燃焼室4(第2図)内に位置す
るノズル口32が形成される。圧縮空気通路31内には開閉
弁33が配置され、この開閉弁33の外端部にはノズル口32
の開閉制御をする弁体34が一体形成される。ハウジング
30内には開閉弁33と共軸的に配置されかつ圧縮ばね35に
よって開閉弁33に向けて付勢された可動コア36と、可動
コア36を吸引するためのソレノイド37が配置される。開
閉弁33の内端部は圧縮ばね38によって可動コア36の端面
に当接せしめられており、圧縮ばね38のばね力は圧縮ば
ね35のばね力よりも強いので通常ノズル口32は開閉弁33
の弁体34によって閉鎖されている。ソレノイド37が付勢
されると可動コア36が開閉弁33の方向に移動し、その結
果開閉弁33の弁体34がノズル口32を開口せしめる。一
方、圧縮空気通路31からは圧縮空気通路31から斜めに延
びる圧縮空気通路39が分岐され、この圧縮空気通路39は
圧縮空気供給口40に連結される。ハウジング30には燃料
噴射弁41が取付けられ、この燃料噴射弁41のノズル孔42
からは燃料が圧縮空気通路39内に向けて噴射される。
FIG. 3 shows an enlarged sectional view of the air blast valve 9. Third
Referring to the figure, a straight compressed air passage 31 is formed in the housing 30 of the air blast valve 9, and a nozzle port 32 located in the combustion chamber 4 (Fig. 2) is formed at the tip of the compressed air passage 31. Is formed. An on-off valve 33 is disposed in the compressed air passage 31, and a nozzle port 32 is provided at an outer end of the on-off valve 33.
A valve body 34 for controlling the opening and closing of the valve is integrally formed. housing
A movable core 36 coaxially arranged with the on-off valve 33 and urged toward the on-off valve 33 by the compression spring 35 and a solenoid 37 for sucking the movable core 36 are arranged in the inside 30. The inner end of the on-off valve 33 is brought into contact with the end face of the movable core 36 by a compression spring 38, and the spring force of the compression spring 38 is stronger than that of the compression spring 35.
It is closed by the valve body 34. When the solenoid 37 is energized, the movable core 36 moves in the direction of the on-off valve 33, and as a result, the valve element 34 of the on-off valve 33 opens the nozzle port 32. On the other hand, a compressed air passage 39 that extends obliquely from the compressed air passage 31 is branched from the compressed air passage 31, and the compressed air passage 39 is connected to a compressed air supply port 40. A fuel injection valve 41 is attached to the housing 30, and a nozzle hole 42 of the fuel injection valve 41 is provided.
From there, fuel is injected into the compressed air passage 39.

第2図に示されるようにエアフローメータ14とスロッ
トル弁16間の給気ダクト13からはエアブラスト用空気通
路17が分岐され、このエアブラスト用空気通路17は機関
駆動のベーンポンプ18および圧縮空気通路19を介して圧
縮空気分配室20に連結される。この圧縮空気分配室20は
各気筒に対して夫々設けられたエアブラスト弁9の圧縮
空気供給口40に連結される。圧縮空気通路19内には圧縮
空気分配室20内の圧縮空気圧を予め定められた一定圧に
維持するための調圧弁21が配置され、余分な圧縮空気は
圧縮空気返戻通路22を介して給気ダクト13内に返戻され
る。従ってエアブラスト弁9の圧縮空気通路31,39は一
定圧の圧縮空気によって満たされている。
As shown in FIG. 2, an air blast air passage 17 is branched from the air supply duct 13 between the air flow meter 14 and the throttle valve 16, and the air blast air passage 17 includes an engine-driven vane pump 18 and a compressed air passage. It is connected to the compressed air distribution chamber 20 via 19. The compressed air distribution chamber 20 is connected to a compressed air supply port 40 of an air blast valve 9 provided for each cylinder. In the compressed air passage 19, a pressure regulating valve 21 for maintaining the compressed air pressure in the compressed air distribution chamber 20 at a predetermined constant pressure is arranged, and excess compressed air is supplied through a compressed air return passage 22. It is returned into the duct 13. Therefore, the compressed air passages 31, 39 of the air blast valve 9 are filled with compressed air of a constant pressure.

第4図に給気弁5および排気弁7の開弁期間、燃料噴
射弁41からの燃料噴射期間および開閉弁33の弁体34の開
弁期間、即ちエアブラスト弁9の開弁期間を示す。第4
図に示されるように第2図に示す実施例では排気弁7が
給気弁5よりも先に開弁し、先に閉弁する。また、第4
図に示されるように開閉弁33の弁体34が開弁する前に、
即ちエアブラスト弁9が開弁する前に燃料噴射弁41から
圧縮空気通路39内の圧縮空気内に向けて燃料が噴射され
る。次いでエアブラスト弁9が開弁するとノズル口32か
ら噴射燃料が圧縮空気と共に燃焼室4内に噴射される。
一方、第2図に示されるように排気弁7側の給気弁5の
開口を給気弁5の全開弁期間に亘って覆うマスク壁23が
シリンダヘッド3の内壁面上に形成される。従って給気
弁5が開弁すると新気は給気ポート6から排気弁7と反
対側の給気弁5の開口を通って燃焼室4内に供給され
る。その結果新気は矢印Sで示すように燃焼室4の周壁
面に沿って流れ、斯くして良好なループ掃気が行なわれ
ることになる。
FIG. 4 shows the opening period of the supply valve 5 and the exhaust valve 7, the period of fuel injection from the fuel injection valve 41, and the opening period of the valve body 34 of the on-off valve 33, that is, the opening period of the air blast valve 9. . Fourth
As shown in the drawing, in the embodiment shown in FIG. 2, the exhaust valve 7 opens before the intake valve 5 and closes before the intake valve 5. Also, the fourth
Before the valve element 34 of the on-off valve 33 opens as shown in the figure,
That is, the fuel is injected from the fuel injection valve 41 into the compressed air in the compressed air passage 39 before the air blast valve 9 opens. Next, when the air blast valve 9 is opened, the injected fuel is injected into the combustion chamber 4 from the nozzle port 32 together with the compressed air.
On the other hand, as shown in FIG. 2, a mask wall 23 is formed on the inner wall surface of the cylinder head 3 to cover the opening of the air supply valve 5 on the exhaust valve 7 side for the full opening period of the air supply valve 5. Therefore, when the air supply valve 5 is opened, fresh air is supplied from the air supply port 6 into the combustion chamber 4 through the opening of the air supply valve 5 opposite to the exhaust valve 7. As a result, the fresh air flows along the peripheral wall surface of the combustion chamber 4 as shown by the arrow S, and thus good loop scavenging is performed.

第2図に示されるようにエアブラスト弁9は電子制御
ユニット50の出力信号に基いて制御される。この電子制
御ユニット50は双方向性バス51によって相互に接続され
たROM(リードオンリメモリ)52と、RAM(ランダムアク
セスメモリ)53と、CPU(マイクロプロセッサ)54と、
入力ポート55と、出力ポート56を具備する。エアフロー
メータ14は吸入空気量に比例した出力電圧を発生し、こ
の出力電圧はAD変換器57を介して入力ポート55に入力さ
れる。また、スロットル弁16にはスロットル弁開度を検
出するスロットルセンサ24が取付けられ、このスロット
ルセンサ24の出力信号がAD変換器58を介して入力ポート
55に入力される。更に入力ポート55には機関回転数を表
す回転数センサ25の出力信号が入力される。一方、出力
ポート56は対応する駆動回路59,60を介してエアブラス
ト弁9のソレノイド37および燃料噴射弁41に接続され
る。
As shown in FIG. 2, the air blast valve 9 is controlled based on the output signal of the electronic control unit 50. The electronic control unit 50 includes a ROM (read only memory) 52, a RAM (random access memory) 53, a CPU (microprocessor) 54,
It has an input port 55 and an output port 56. The air flow meter 14 generates an output voltage proportional to the amount of intake air, and this output voltage is input to an input port 55 via an AD converter 57. A throttle sensor 24 for detecting the throttle valve opening is attached to the throttle valve 16, and the output signal of this throttle sensor 24 is input through an AD converter 58 to an input port.
Entered in 55. Further, the output signal of the rotation speed sensor 25 representing the engine rotation speed is input to the input port 55. On the other hand, the output port 56 is connected to the solenoid 37 and the fuel injection valve 41 of the air blast valve 9 via the corresponding drive circuits 59 and 60.

本発明においては燃料噴射時間TAUは次式に基いて計
算される。
In the present invention, the fuel injection time TAU is calculated based on the following equation.

TAU=K・TP・Fb・C TP=Tb・Fa ここでKは定数、 Tbは基本燃料噴射時間 Faは新気捕捉係数、即ち筒内空気残留率 Fbは過渡補正係数、 Cは機関冷却水温等による補正係数である。TAU = K ・ TP ・ Fb ・ C TP = Tb ・ Fa where K is a constant, Tb is the basic fuel injection time Fa is a fresh air capture coefficient, that is, the cylinder air residual rate Fb is a transient correction coefficient, and C is the engine cooling water temperature. It is a correction coefficient based on the above.

基本燃料噴射時間Tbは機関負荷Q/N(機関シリンダ内
に供給される吸入空気量Q/機関回転数N)と機関回転数
Nの関数であり、機関シリンダ内に供給された吸入空気
全部が吹き抜けることなくシリンダ内に残留すると仮定
したときに機関シリンダ内の空燃比を目標空燃比とする
のに必要な燃料噴射時間を表わしている。
The basic fuel injection time Tb is a function of the engine load Q / N (intake air amount Q supplied to the engine cylinder / engine speed N) and the engine speed N, and the total intake air supplied to the engine cylinder is It represents the fuel injection time required to bring the air-fuel ratio in the engine cylinder to the target air-fuel ratio, assuming that the air-fuel ratio remains in the cylinder without being blown through.

一方、筒内空気残留率Faは定常運転時における吸入空
気の吹き抜け量を実測して得られる実験値であり、この
筒内空気残留率Faは{(機関シリンダ内に供給された吸
入空気量Q−吹き抜け量)/機関シリンダ内に供給され
た吸入空気量Q}により定義される。この筒内空気残留
率Faは定常運転時における機関負荷Q/Nと機関回転数N
の関数となる。
On the other hand, the in-cylinder air residual rate Fa is an experimental value obtained by actually measuring the amount of blown-in intake air during steady operation, and this in-cylinder air residual rate Fa is {(intake air amount Q supplied to the engine cylinder Q -Blow-through amount) / intake air amount Q} supplied into the engine cylinder. This in-cylinder air residual ratio Fa is the engine load Q / N and engine speed N during steady operation.
Is a function of.

従って基本燃料噴射時間Tbに筒内空気残留率Faを乗算
した燃料噴射時間TPは定常運転時において機関シリンダ
内の実際の空燃比を目標空燃比とするのに必要な燃料噴
射時間を表わしており、以下この燃料噴射時間TPを吹き
抜けを考慮した基本燃料噴射時間と称する。この吹き抜
けを考慮した基本燃料噴射時間TPは第5図に示されるよ
うに機関負荷Q/Nと機関回転数Nとの関数としてマップ
の形で予めROM52内に記憶されている。従って機関が定
常運転されている限り、第5図に示すマップに基いて燃
料噴射時間を計算すれば機関シリンダ内の実際の空燃比
を目標空燃比に維持することができる。
Therefore, the fuel injection time TP, which is obtained by multiplying the basic fuel injection time Tb by the in-cylinder air residual ratio Fa, represents the fuel injection time required to set the actual air-fuel ratio in the engine cylinder to the target air-fuel ratio during steady operation. Hereinafter, this fuel injection time TP will be referred to as a basic fuel injection time in consideration of blow through. The basic fuel injection time TP considering this blow-through is stored in advance in the ROM 52 in the form of a map as a function of the engine load Q / N and the engine speed N, as shown in FIG. Therefore, as long as the engine is operating steadily, the actual air-fuel ratio in the engine cylinder can be maintained at the target air-fuel ratio by calculating the fuel injection time based on the map shown in FIG.

ところが過渡運転時に第5図に示すマップに基いて燃
料噴射時間を計算すると機関シリンダ内の実際の空燃比
が目標空燃比からずれてしまう。以下その理由について
説明する。即ち、機関負荷が高くなると排気通路内の圧
力、即ち背圧が高くなり、吹き抜け量はこの背圧の影響
を大きく受ける。従って例えば機関加速運転時において
スロットル弁16の開度の増大に対応して背圧が上昇すれ
ば機関シリンダ内の実際の空燃比が目標空燃比からずれ
ることはない。しかしながら実際には機関加速運転時に
おいてスロットル弁16の開度が増大しても背圧がただち
に上昇せず、従って加速が開始されると同一スロットル
弁開度における定常運転時よりも吹き抜け量が増大する
ことになる。この吹き抜け量の増大率は加速の度合が大
きくなるほど大きくなる。吹き抜け量が増大すれば機関
シリンダ内の実際の空燃比が目標空燃比に対してリッチ
側となるので機関シリンダ内の実際の空燃比を目標空燃
比とするには加速の度合が大きくなるほど燃料噴射時間
を短かくしてやらなければならない。これに対して機関
減速運転時にはスロットル弁16開度が小さくなってもた
だちに背圧が低下せず、従って吹き抜け量が減少する。
吹き抜け量が減少すれば機関シリンダ内の実際の空燃比
が目標空燃比に対してリーン側となるので減速運転時に
機関シリンダ内の実際の空燃比を目標空燃比とするには
減速の度合が大きくなるほど燃料噴射時間を長くしてや
らなければならない。
However, when the fuel injection time is calculated based on the map shown in FIG. 5 during the transient operation, the actual air-fuel ratio in the engine cylinder deviates from the target air-fuel ratio. The reason will be described below. That is, when the engine load increases, the pressure in the exhaust passage, that is, the back pressure, increases, and the blow-through amount is greatly affected by this back pressure. Therefore, for example, if the back pressure increases in response to an increase in the opening degree of the throttle valve 16 during engine acceleration operation, the actual air-fuel ratio in the engine cylinder does not deviate from the target air-fuel ratio. However, in actuality, the back pressure does not immediately increase even when the opening degree of the throttle valve 16 increases during engine acceleration operation, and therefore when acceleration starts, the blow-through amount increases compared to during steady operation at the same throttle valve opening degree. Will be done. The rate of increase in the blow-through amount increases as the degree of acceleration increases. If the amount of blow-through increases, the actual air-fuel ratio in the engine cylinder becomes richer than the target air-fuel ratio.Therefore, in order to make the actual air-fuel ratio in the engine cylinder the target air-fuel ratio, the fuel injection increases as the degree of acceleration increases. I have to shorten the time. On the other hand, during engine deceleration operation, the back pressure does not immediately decrease even when the opening of the throttle valve 16 becomes small, and therefore the blow-through amount decreases.
If the amount of blow-through decreases, the actual air-fuel ratio in the engine cylinder becomes leaner than the target air-fuel ratio, so the degree of deceleration is large in order to make the actual air-fuel ratio in the engine cylinder the target air-fuel ratio during deceleration operation. Indeed, the fuel injection time must be lengthened.

そこで過渡運転時に機関シリンダ内の実際の空燃比が
目標空燃比となるように基本燃料噴射時間TPを補正する
ために過渡補正係数Fbが導入されている。第6図はこの
過渡補正係数Fbの一例を示している。第6図では過渡状
態を表わすものとしてスロットル弁16開度の変化率ΔT
を用いており、スロットル弁16開度の変化率ΔTが正の
方向に大きくなるにつれて、即ち加速の度合が大きくな
るにつれて過渡補正係数Fbが小さくなり、スロットル弁
16開度の変化率ΔTが負の方向に大きくなるにつれて、
即ち減速の度合が大きくなるにつれて過渡補正係数Fbが
大きくなる。第6図に示す関係は予めROM52内に記憶さ
れている。なお、過渡状態を表わすものとしてスロット
ル弁16開度の変化率ΔTを用いる代りにスロットル弁16
下流の吸入空気圧の変化率ΔPを用いることもできる。
Therefore, the transient correction coefficient Fb is introduced to correct the basic fuel injection time TP so that the actual air-fuel ratio in the engine cylinder becomes the target air-fuel ratio during transient operation. FIG. 6 shows an example of this transient correction coefficient Fb. In FIG. 6, the change rate ΔT of the opening of the throttle valve 16 is shown as a transient state.
The transient correction coefficient Fb decreases as the rate of change ΔT of the opening of the throttle valve 16 increases in the positive direction, that is, as the degree of acceleration increases.
16 As the rate of change ΔT of the opening increases in the negative direction,
That is, the transient correction coefficient Fb increases as the degree of deceleration increases. The relationship shown in FIG. 6 is stored in advance in the ROM 52. It should be noted that instead of using the rate of change ΔT of the opening of the throttle valve 16 to represent the transient state, the throttle valve 16
It is also possible to use the change rate ΔP of the downstream intake air pressure.

第7図はスロットル弁16開度の変化率ΔTを計算する
ためのルーチンを示しており、このルーチンは一定時間
毎の割込みによって実行される。
FIG. 7 shows a routine for calculating the rate of change ΔT of the opening of the throttle valve 16 and this routine is executed by interruption at regular time intervals.

第7図を参照するとこのルーチンではステップ70にお
いてスロットルセンサ24の出力信号に基き現在のスロッ
トル弁開度TAから前回の割込みルーチンにおけるスロッ
トル開度TA1を減算することによってスロットル開度の
変化率ΔTが求められる。
Referring to FIG. 7, in this routine, in step 70, the throttle opening change rate ΔT is subtracted from the current throttle valve opening TA based on the output signal of the throttle sensor 24 by the throttle opening TA 1 in the previous interruption routine. Is required.

第8図は燃料噴射時間を計算するためのルーチンを示
しており、このルーチンは一定クランク角度毎の割込み
によって実行される。
FIG. 8 shows a routine for calculating the fuel injection time, and this routine is executed by interruption every constant crank angle.

第8図を参照するとまず始めにステップ80においてエ
アフローメータ14および回転数センサ25の出力信号から
第5図に示すマップに基いて吹き抜けを考慮した基本燃
料噴射時間TPが計算される。次いでステップ81では機関
冷却水温等による補正係数Cが計算され、次いでステッ
プ82では第7図のルーチンで求められた最新のスロット
ル弁開度変化率ΔTから第6図に示す関係に基いて過渡
補正係数Fbが計算される。次いでステップ83では次式に
基いて実際の燃料噴射時間TAUが計算される。
Referring to FIG. 8, first, at step 80, the basic fuel injection time TP considering blow-through is calculated from the output signals of the air flow meter 14 and the rotation speed sensor 25 based on the map shown in FIG. Next, at step 81, the correction coefficient C by the engine cooling water temperature etc. is calculated, then at step 82, the transient correction is made from the latest throttle valve opening change rate ΔT obtained in the routine of FIG. 7 based on the relationship shown in FIG. The coefficient Fb is calculated. Next, at step 83, the actual fuel injection time TAU is calculated based on the following equation.

TAU=K・TP・Fb・C 〔発明の効果〕 過渡運転時であっても機関シリンダ内の実際の空燃比
を目標空燃比に維持することができる。
TAU = K / TP / Fb / C [Effect of the invention] Even during transient operation, the actual air-fuel ratio in the engine cylinder can be maintained at the target air-fuel ratio.

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

第1図は発明の構成図、第2図は2サイクル内燃機関の
全体図、第3図はエアブラスト弁の拡大側面断面図、第
4図は給排気弁の開弁期間、エアブラスト弁の開弁期間
等を示す栓図、第5図は吹き抜けを考慮した基本燃料噴
射時間を示す図、第6図は過渡補正係数を示す図、第7
図はスロットル弁開度変化率を計算するためのフローチ
ャート、第8図は燃料噴射時間を計算するためのフロー
チャートである。 4……燃焼室、5……給気弁、 9……エアブラスト弁、16……スロットル弁、 24……スロットルセンサ。
FIG. 1 is a block diagram of the invention, FIG. 2 is an overall view of a two-cycle internal combustion engine, FIG. 3 is an enlarged side sectional view of an air blast valve, and FIG. 4 is an opening period of an air supply / exhaust valve, an air blast valve. FIG. 5 is a plug diagram showing a valve opening period, etc., FIG. 5 is a diagram showing a basic fuel injection time in consideration of blow-through, FIG. 6 is a diagram showing a transient correction coefficient,
FIG. 8 is a flowchart for calculating the throttle valve opening change rate, and FIG. 8 is a flowchart for calculating the fuel injection time. 4 ... Combustion chamber, 5 ... Air supply valve, 9 ... Air blast valve, 16 ... Throttle valve, 24 ... Throttle sensor.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 野村 啓 愛知県豊田市トヨタ町1番地 トヨタ自 動車株式会社内 (56)参考文献 特開 昭63−208635(JP,A) ─────────────────────────────────────────────────── --- Continuation of the front page (72) Inventor Kei Nomura 1 Toyota-cho, Toyota-shi, Aichi Toyota Motor Co., Ltd. (56) Reference JP-A-63-208635 (JP, A)

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】定常運転時における機関シリンダ内の実際
の空燃比が予め定められた目標空燃比となるように定常
運転状態に応じた燃料噴射時間を記憶した燃料噴射時間
記憶手段と、過渡運転状態を検出する過渡運転状態検出
手段と、過渡運転時に機関シリンダ内の実際の空燃比が
上記目標空燃比となるように過渡運転状態に応じた上記
燃料噴射時間に対する補正値を記憶した補正値記憶手段
と、上記燃料噴射時間と補正値から機関の運転状態に応
じた実際の燃料噴射時間を計算する燃料噴射時間計算手
段とを具備した2サイクル内燃機関の燃料噴射制御装
置。
1. A fuel injection time storage means for storing fuel injection time according to a steady operation state so that an actual air-fuel ratio in an engine cylinder during a steady operation becomes a predetermined target air-fuel ratio, and a transient operation. A transient operation state detecting means for detecting the state, and a correction value memory for storing a correction value for the fuel injection time according to the transient operation state so that the actual air-fuel ratio in the engine cylinder during the transient operation becomes the target air-fuel ratio. A fuel injection control device for a two-cycle internal combustion engine, comprising: a fuel injection time calculation means for calculating an actual fuel injection time according to an operating state of the engine from the fuel injection time and the correction value.
JP1243305A 1989-09-21 1989-09-21 Fuel injection control device for two-cycle internal combustion engine Expired - Fee Related JP2522409B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1243305A JP2522409B2 (en) 1989-09-21 1989-09-21 Fuel injection control device for two-cycle internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1243305A JP2522409B2 (en) 1989-09-21 1989-09-21 Fuel injection control device for two-cycle internal combustion engine

Publications (2)

Publication Number Publication Date
JPH03107553A JPH03107553A (en) 1991-05-07
JP2522409B2 true JP2522409B2 (en) 1996-08-07

Family

ID=17101858

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1243305A Expired - Fee Related JP2522409B2 (en) 1989-09-21 1989-09-21 Fuel injection control device for two-cycle internal combustion engine

Country Status (1)

Country Link
JP (1) JP2522409B2 (en)

Also Published As

Publication number Publication date
JPH03107553A (en) 1991-05-07

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