JPH01116265A - Fuel injection height correcting device for internal combustion engine - Google Patents

Fuel injection height correcting device for internal combustion engine

Info

Publication number
JPH01116265A
JPH01116265A JP27405987A JP27405987A JPH01116265A JP H01116265 A JPH01116265 A JP H01116265A JP 27405987 A JP27405987 A JP 27405987A JP 27405987 A JP27405987 A JP 27405987A JP H01116265 A JPH01116265 A JP H01116265A
Authority
JP
Japan
Prior art keywords
intake
altitude
fuel injection
internal combustion
combustion 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
JP27405987A
Other languages
Japanese (ja)
Inventor
Toshiyuki Yokoyama
横山 稔之
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.)
Suzuki Motor Corp
Original Assignee
Suzuki 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 Suzuki Motor Corp filed Critical Suzuki Motor Corp
Priority to JP27405987A priority Critical patent/JPH01116265A/en
Publication of JPH01116265A publication Critical patent/JPH01116265A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To prevent air-fuel ratio from fluctuating due to a change of altitude by comparing an intake pressure with a reference pressure, set in the reference altitude, and correcting a fuel injection quantity being based on a difference between both the intake pressure and the reference pressure in the time of required opening of an intake throttle valve. CONSTITUTION:A control circuit 14 inputs in ignition signal from an ignition coil 22 in addition to detection values of an intake pressure sensor 16, intake throttle valve opening sensor 18, intake temperature sensor 20, etc., controlling the opening time of a fuel injection valve 12 to be calculated. The control circuit 14, which sets a reference intake pressure in a reference altitude corresponding to the required opening of an intake throttle valve 10, obtains an altitude being based on a difference between this reference intake pressure and the detection value of, the intake pressure sensor 16 corresponding to the same intake throttle valve opening, correcting the opening time of the fuel injection valve 12.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は内燃機関の燃料噴射高度補正装置に係り、特
に高度変化に応じ内燃機関に噴射供給する燃料量を補正
し得て空燃比の適正化を果たし得る内燃機関の燃料噴射
高度補正装置に関する。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a fuel injection altitude correction device for an internal combustion engine, and in particular, it is capable of correcting the amount of fuel injected and supplied to the internal combustion engine according to changes in altitude, and maintains an appropriate air-fuel ratio. The present invention relates to a fuel injection altitude correction device for an internal combustion engine that can achieve

〔従来の技術〕[Conventional technology]

内燃機関に燃料を供給する装置には、気化器や燃料噴射
装置等がある。燃料噴射装置は、機関負荷や機関回転数
、冷却水温度、吸入空気量、吸気圧力等を燃料噴射量設
定因子とし、機関運転状態に応じて内燃機関に供給する
燃料噴射量を設定している。例えば、特開昭58−13
3433号公報に開示の内燃機関は、内燃機関稼動時の
吸気管内の吸気圧力を絶対圧力として圧力センサにより
検知し、燃料噴射量を設定するものである。
Devices that supply fuel to internal combustion engines include carburetors, fuel injection devices, and the like. The fuel injection system uses engine load, engine speed, cooling water temperature, intake air volume, intake air pressure, etc. as fuel injection amount setting factors, and sets the fuel injection amount supplied to the internal combustion engine according to the engine operating state. . For example, JP-A-58-13
The internal combustion engine disclosed in Japanese Patent No. 3433 uses a pressure sensor to detect the intake air pressure in the intake pipe as an absolute pressure when the internal combustion engine is operating, and sets the fuel injection amount.

この公報に開示の内燃機関は、単一の圧力センサを設け
、内燃機関の電源投入から始動開始までの間、即ち内燃
機関始動中に前記単一の圧力センサの検知した吸気管内
絶対圧力を補正用の燃料噴射量設定因子たる大気圧とし
て制御回路に記憶しておく。内燃機関始動後、即ち内燃
機関稼動中には、前記単一の圧力センサの検知する吸気
管内絶対圧力を主たる燃料噴射量設定因子とし、この主
たる燃料噴射量設定因子により設定される燃料噴射量を
、前記記憶している補正用の燃料噴射量設定因子たる大
気圧により補正し、大気圧変化に対して燃料噴射量を補
正するものである。
The internal combustion engine disclosed in this publication is provided with a single pressure sensor, and corrects the absolute pressure in the intake pipe detected by the single pressure sensor during the period from power-on to the start of the internal combustion engine, that is, during the start of the internal combustion engine. This is stored in the control circuit as atmospheric pressure, which is a fuel injection amount setting factor. After the internal combustion engine is started, that is, while the internal combustion engine is running, the absolute pressure in the intake pipe detected by the single pressure sensor is used as the main fuel injection amount setting factor, and the fuel injection amount set by this main fuel injection amount setting factor is set. The fuel injection amount is corrected based on the atmospheric pressure, which is the stored fuel injection amount setting factor for correction, and the fuel injection amount is corrected in response to changes in atmospheric pressure.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

ところで、内燃機関に吸入される空気は、高度によりそ
の大気圧が変動するものであり、高度が高くなると空気
密度の減少により大気圧は低下する。このため、吸気圧
力を主たる燃料噴射量設定因子として燃料噴射量を設定
し燃料を噴射供給する内燃機関にあっては、高度が高く
なることにより空燃比の薄化を招く不都合がある。
Incidentally, the atmospheric pressure of air taken into an internal combustion engine varies depending on the altitude, and as the altitude increases, the atmospheric pressure decreases due to a decrease in air density. For this reason, internal combustion engines that set the fuel injection amount using the intake pressure as the main fuel injection amount setting factor and inject and supply fuel have the disadvantage that the air-fuel ratio becomes thinner as the altitude increases.

即ち、第4図に示す如く、高度Hと大気圧Pとは逆比例
し、高度Hが高くなると空気密度の減少により大気圧P
は低下する。また、第5図に示す如く、内燃機関の吸気
絞り弁の開度θと吸気通路内の吸気圧力(絶対圧力)P
mとは比例し、吸気絞り弁の開度θが大きくなると吸気
圧力Pmは大きくなる。しかし、吸気絞り弁の開度θが
同じであっても、高度Hが高くなると大気圧Pが低下す
ることにより、基準高度HOである高度Omにおける吸
気圧力Poはこの基準高度Hoよりも高い所定の高度H
nにおいて吸気圧力Pnに低下する。
That is, as shown in Figure 4, altitude H and atmospheric pressure P are inversely proportional, and as altitude H increases, atmospheric pressure P decreases due to the decrease in air density.
decreases. In addition, as shown in Fig. 5, the opening degree θ of the intake throttle valve of the internal combustion engine and the intake pressure (absolute pressure) P in the intake passage
It is proportional to m, and as the opening degree θ of the intake throttle valve increases, the intake pressure Pm increases. However, even if the opening degree θ of the intake throttle valve is the same, as the altitude H increases, the atmospheric pressure P decreases. altitude H
At n, the intake pressure decreases to Pn.

このように、高度Hが高くなることにより低下する吸気
圧力Pmを主たる燃料噴射量設定因子として燃料噴射量
を設定すると、第6図に示す如く、吸気絞り弁の開度θ
が同じであっても、基準高度HOである高度Omにおい
ては吸気圧力Poにより所要の燃料噴射時間TAUoを
得られるが、この基準高度Hoよりも高い所定の高度H
nにおいては前記吸気圧力Poよりも低い吸気圧力Pn
のために、前記所要の燃料噴射時間TAUoよりも短い
燃料噴射時間TAUnL、か得られないことになる。こ
れにより、第7図に示す如く、高度が高くなると燃料噴
射時間TAUが短くなり、空燃比の薄化を招く不都合を
生じた。
In this way, when the fuel injection amount is set using the intake pressure Pm, which decreases as the altitude H increases, as the main fuel injection amount setting factor, as shown in FIG.
Even if they are the same, the required fuel injection time TAUo can be obtained by the intake pressure Po at the altitude Om, which is the reference altitude HO, but at a predetermined altitude H higher than this reference altitude Ho.
n, the intake pressure Pn is lower than the intake pressure Po.
Therefore, the fuel injection time TAUnL, which is shorter than the required fuel injection time TAUo, cannot be obtained. As a result, as shown in FIG. 7, as the altitude increases, the fuel injection time TAU becomes shorter, resulting in a disadvantage that the air-fuel ratio becomes thinner.

このため、空燃比が不適正となり、内燃機関の出力が低
下し、排気ガス有害成分が増加し、また、燃料消費率の
悪化を招く不都合を生じた。
As a result, the air-fuel ratio becomes inappropriate, the output of the internal combustion engine decreases, the harmful components of the exhaust gas increase, and the fuel consumption rate worsens.

この高度が高くなることにより空燃比の薄化を招く不都
合は、前記特開昭58−133433号公報に開示の内
燃機関では解決し得なかった。この公報に開示のものは
、内燃機関始動中に単一の圧力センサの検知した吸気管
内絶対圧力を補正用の燃料噴射量設定因子たる大気圧と
して記憶しておき、内燃機関稼動中に前記単一の圧力セ
ンサの検知する吸気管内絶対圧力を主たる燃料噴射量設
定因子として設定される燃料噴射量を、前記補正用の燃
料噴射量設定因子たる大気圧により補正し、大気圧変化
に対して燃料噴射量を補正するものである。このため、
内燃機関始動中の高度よりも内燃機関始動後の稼動時の
高度が高くなり大気圧が変化した場合に、燃料噴射量を
補正し得ない不都合があった。
This problem of thinning of the air-fuel ratio due to the increase in altitude could not be solved by the internal combustion engine disclosed in Japanese Patent Application Laid-Open No. 58-133433. What is disclosed in this publication is to store the absolute pressure in the intake pipe detected by a single pressure sensor during starting of the internal combustion engine as atmospheric pressure as a fuel injection amount setting factor for correction, and to The fuel injection amount, which is set using the intake pipe absolute pressure detected by the first pressure sensor as the main fuel injection amount setting factor, is corrected by the atmospheric pressure, which is the fuel injection amount setting factor for correction, and the fuel injection amount is adjusted to compensate for changes in atmospheric pressure. This corrects the injection amount. For this reason,
There is a problem in that the fuel injection amount cannot be corrected when the altitude during operation after starting the internal combustion engine is higher than the altitude during starting the internal combustion engine and the atmospheric pressure changes.

〔発明の目的〕[Purpose of the invention]

そこで、この発明の目的は、高度変化に応じ内燃機関に
噴射供給する燃料量を補正し得て空燃比の適正化を果た
し得る内燃機関の燃料噴射高度補正装置を実現すること
にある。
SUMMARY OF THE INVENTION Therefore, an object of the present invention is to realize a fuel injection altitude correction device for an internal combustion engine that can correct the amount of fuel injected and supplied to an internal combustion engine in accordance with changes in altitude and can optimize the air-fuel ratio.

〔問題点を解決するための手段〕[Means for solving problems]

この目的を達成するためにこの発明は、燃料を噴射供給
する内燃機関の吸気圧力を検出する吸気圧力検出手段を
設け、前記内燃機関の吸気絞り弁所要間度状態に対応し
基準高度において設定した基準吸気圧力と前記内燃機関
の吸気絞り弁所要開度状態に対応し所定高度において前
記吸気圧力検出手段の検出する所定吸気圧力との差に応
じ前記内燃機関に噴射供給する燃料量を補正すべく制御
する制御手段を設けたことを特徴とする。
In order to achieve this object, the present invention provides an intake pressure detection means for detecting the intake pressure of an internal combustion engine that injects and supplies fuel, and sets the intake pressure at a reference altitude corresponding to the required time state of the intake throttle valve of the internal combustion engine. To correct the amount of fuel injected and supplied to the internal combustion engine according to the difference between a reference intake pressure and a predetermined intake pressure detected by the intake pressure detection means at a predetermined altitude corresponding to the required opening state of the intake throttle valve of the internal combustion engine. It is characterized by providing a control means for controlling.

〔作用〕[Effect]

この発明の構成によれば、制御手段によって、内燃機関
の吸気絞り弁所要開度状態に対応し基準高度において設
定した基準吸気圧力と、前記内燃機関の吸気絞り弁所要
開度状態に対応し所定高度において吸気圧力検出手段の
検出する所定吸気圧力との差に応じ、内燃機関に噴射供
給する燃料量を補正すべく制御することにより、高度変
化に応じ内燃機関に噴射供給する燃料量を補正する。こ
れにより、空燃比の適正化を果す。
According to the configuration of the present invention, the control means controls the reference intake pressure set at the reference altitude corresponding to the required opening state of the intake throttle valve of the internal combustion engine, and the predetermined standard intake pressure set corresponding to the required opening state of the intake throttle valve of the internal combustion engine. By controlling the amount of fuel injected and supplied to the internal combustion engine to be corrected according to the difference between the intake pressure and the predetermined intake pressure detected by the intake pressure detection means at altitude, the amount of fuel injected and supplied to the internal combustion engine is corrected in accordance with changes in altitude. . This achieves optimization of the air-fuel ratio.

〔実施例〕〔Example〕

次にこの発明の実施例を図に基づいて説明する。 Next, embodiments of the present invention will be described based on the drawings.

第1〜3図は、この発明の実施例を示すものである。第
1・2図において、2は燃料を噴射供給する内燃機関、
4は吸気通路、6は燃焼室、8は排気通路、10は吸気
絞り弁、12は燃料噴射弁、14は制御手段たる制御回
路である。
1 to 3 show embodiments of this invention. In Figures 1 and 2, 2 is an internal combustion engine that injects and supplies fuel;
4 is an intake passage, 6 is a combustion chamber, 8 is an exhaust passage, 10 is an intake throttle valve, 12 is a fuel injection valve, and 14 is a control circuit as a control means.

前記内燃機関2の燃焼室6に指向させて吸気通路4に取
付けた燃料噴射弁12は、制御回路14により動作制御
される。制御回路14には、吸気通路4の吸気圧力を検
出する吸気圧力制御手段たる圧力センサ16と、吸気絞
り弁10の開度状態を検出する開度センサ18と、吸気
通路4の吸気温度を検出する温度センサ20とを接続し
、噴射時期を設定する点火信号を入力する点火コイル2
2を接続している。また、この制御回路14には、図示
しないが、例えば冷却水温度センサや02センサ等のそ
の他のセンサ24を接続している。これら各種センサ1
6〜24から入力する信号により、制御回路14は燃料
噴射弁12を動作制御して内燃機関2に燃料を噴射供給
する。例えば、圧力センサ16の検出する吸気圧力Pm
を主たる燃料噴射量設定因子とし、開度センサ18や温
度センサ20、その他のセンサ24の各検出信号を補正
用の燃料噴射量設定因子として燃料噴射時間TAUを設
定し、点火コイル22からの点火信号により設定する噴
射時期に燃料を噴射すべく前記燃料噴射時間TAUによ
り燃料噴射弁12を動作制御する。
The operation of the fuel injection valve 12 , which is attached to the intake passage 4 and directed toward the combustion chamber 6 of the internal combustion engine 2 , is controlled by a control circuit 14 . The control circuit 14 includes a pressure sensor 16 serving as an intake pressure control means for detecting the intake pressure in the intake passage 4, an opening sensor 18 for detecting the opening state of the intake throttle valve 10, and an opening sensor 18 for detecting the intake air temperature in the intake passage 4. An ignition coil 2 is connected to a temperature sensor 20 to input an ignition signal for setting injection timing.
2 is connected. Further, although not shown, other sensors 24 such as a cooling water temperature sensor and an 02 sensor are connected to the control circuit 14. These various sensors 1
The control circuit 14 controls the operation of the fuel injection valve 12 based on the signals input from the internal combustion engine 2 to inject fuel to the internal combustion engine 2 . For example, the intake pressure Pm detected by the pressure sensor 16
is the main fuel injection amount setting factor, and each detection signal of the opening sensor 18, temperature sensor 20, and other sensors 24 is used as the fuel injection amount setting factor for correction to set the fuel injection time TAU, and the ignition coil 22 is ignited. The operation of the fuel injection valve 12 is controlled according to the fuel injection time TAU in order to inject the fuel at the injection timing set by the signal.

前記圧力センサ16の検出する吸気圧力Pmは、第5図
に示す如く、吸気絞り弁10の開度が同じであっても、
高度が基準高度HOたるOmから所定高度Hnに変化す
ると、吸気圧力POは吸気圧力Pnに低下する。このよ
うに、吸気圧力PmがPoからPnに低下することによ
り、第6図に示す如く、基準高度HOである高度Omに
おいては吸気圧力POにより所要の燃料噴射時間TAU
As shown in FIG. 5, the intake pressure Pm detected by the pressure sensor 16 varies even if the opening degree of the intake throttle valve 10 is the same.
When the altitude changes from Om, which is the reference altitude HO, to the predetermined altitude Hn, the intake pressure PO decreases to the intake pressure Pn. In this way, as the intake pressure Pm decreases from Po to Pn, as shown in FIG. 6, at the altitude Om which is the reference altitude HO, the required fuel injection time TAU
.

を得られるが、この基準高度HOよりも高い所定の高度
Hnにおいては前記吸気圧力POよりも低い吸気圧力P
nのために、前記所要の燃料噴射時間TAUoよりも短
い燃料噴射時間TAUnLか得らhないことになる。こ
れにより、第7図に示す如く、高度が高くなると燃料噴
射時間TAUが短くなり、空燃比の薄化を招く不都合を
生じた。
However, at a predetermined altitude Hn higher than this reference altitude HO, the intake pressure P is lower than the intake pressure PO.
Because of n, it is not possible to obtain a fuel injection time TAUnL shorter than the required fuel injection time TAUo. As a result, as shown in FIG. 7, as the altitude increases, the fuel injection time TAU becomes shorter, resulting in a disadvantage that the air-fuel ratio becomes thinner.

このため、空燃比が不適正となり、内燃機関の出力が低
下し、排気ガス有害成分が増加し、また、燃料消費率の
悪化を招く不都合を生じた。
As a result, the air-fuel ratio becomes inappropriate, the output of the internal combustion engine decreases, the harmful components of the exhaust gas increase, and the fuel consumption rate worsens.

このような不都合を防止するために、この発明では、制
御回路14によって、吸気絞り弁10の所要開度状態θ
に対応して基準高度HOにおける基準吸気圧力POを設
定し、この吸気絞り10の所要開度状態θに対応し基準
高度HOにおいて設定した基準吸気圧力Poと、前記吸
気絞り弁10の所要開度状態θに対応して所定高度Hn
において圧力センサ16の検出する所定吸気圧力Pnと
の差に応じ、内燃機関2に噴射供給する燃料量を補正す
るように制御する。
In order to prevent such inconvenience, in the present invention, the control circuit 14 controls the required opening state θ of the intake throttle valve 10.
The reference intake pressure PO at the reference altitude HO is set corresponding to the required opening state θ of the intake throttle valve 10, and the reference intake pressure Po set at the reference altitude HO corresponding to the required opening state θ of the intake throttle valve 10 and the required opening of the intake throttle valve 10 are set. A predetermined altitude Hn corresponding to the state θ
Control is performed to correct the amount of fuel injected and supplied to the internal combustion engine 2 according to the difference from the predetermined intake pressure Pn detected by the pressure sensor 16.

次に作用を第3図に従って説明する。Next, the operation will be explained according to FIG.

制御がスタート(100)L、内燃機関2を始動(10
1)すると、燃料噴射が開始(102)される。制御回
路14は、圧力センサ16と開度センサ18とから入力
する信号により吸気絞り弁10の開度θと吸気通路4の
吸気圧力Pmとを検出(103)する、設定しである基
準吸気圧力Poと圧力センサ16の検出した所定吸気圧
力Pnとの差(Po−Pn)を計算(104)L、補正
値を計算(105)する。この補正値により内燃機関2
に燃料を噴射(106)する。次いで、内燃機関2が始
動中か否かを判断(107)L、未だ始動中であればス
テップ10.3にジャンプし、前記ステップ103〜1
06を実行する。始動が完了であれば、エンド(10B
)となる。始動完了後の制御においては、前述と同様に
、θとPmとを検出し、(Po−Pn)との差を計算し
、補正値を計算し、補正値により内燃機関2に燃料を噴
射する。
Control starts (100) L, internal combustion engine 2 starts (10
1) Then, fuel injection is started (102). The control circuit 14 detects (103) the opening degree θ of the intake throttle valve 10 and the intake pressure Pm of the intake passage 4 based on the signals inputted from the pressure sensor 16 and the opening sensor 18. The difference (Po-Pn) between Po and the predetermined intake pressure Pn detected by the pressure sensor 16 is calculated (104)L, and a correction value is calculated (105). With this correction value, the internal combustion engine 2
Fuel is injected (106). Next, it is determined whether or not the internal combustion engine 2 is starting (107) L. If it is still starting, the process jumps to step 10.3, and steps 103 to 1 are performed.
Execute 06. If the start is complete, end (10B
). In the control after the start is completed, as described above, θ and Pm are detected, the difference between them is calculated, a correction value is calculated, and fuel is injected into the internal combustion engine 2 based on the correction value. .

即ち、燃料噴射時間TAUは、基準高度Hoである高度
Omにおいて設定しである。この基準高度HOにおける
吸気絞り弁lOの各開度に対応し基準吸気圧力POを設
定する。このときの吸気絞り弁10の開度θに対応する
基準吸気圧力をPO1燃料噴射時間をTAUoとする。
That is, the fuel injection time TAU is set at the altitude Om, which is the reference altitude Ho. A reference intake pressure PO is set corresponding to each opening degree of the intake throttle valve IO at this reference altitude HO. The reference intake pressure corresponding to the opening degree θ of the intake throttle valve 10 at this time is defined as the PO1 fuel injection time TAUo.

基準高度HOから所定高度Hnに高まると、第6図に示
す如く吸気絞り弁10の開度θに対応する吸気圧力がP
nとなり、燃料噴射時間はTAUnになる。この所定高
度Hnにおいては、前記基準高度Hoにおける燃料噴射
時間TAUoと所定高度Hnにおける燃料噴射時間TA
Unとの差(TAUo−TAUn)に相当する燃料噴射
時間が不足し、空燃比が薄化する不都合がある。
When the altitude increases from the reference altitude HO to the predetermined altitude Hn, the intake pressure corresponding to the opening degree θ of the intake throttle valve 10 becomes P as shown in FIG.
n, and the fuel injection time becomes TAUn. At this predetermined altitude Hn, the fuel injection time TAUo at the reference altitude Ho and the fuel injection time TA at the predetermined altitude Hn
There is a disadvantage that the fuel injection time corresponding to the difference from Un (TAUo-TAUn) is insufficient, and the air-fuel ratio becomes lean.

そこで、高度変化により補正した補正燃料噴射時間をT
AUHとし、 TAUH=TAUoX (1+k (Po−Pn))を
満足するkを定める。
Therefore, the corrected fuel injection time T
AUH, and determine k that satisfies TAUH=TAUoX (1+k (Po-Pn)).

ここで、TAUH=TAUoとしないのは、高度変化に
より空気密度および大気温度が変化するので、定数kに
よってこれらを補正するためである。したがって、開度
センサ18の検出する吸気絞り弁10の開度θに基準吸
気圧力Po及び圧力センサ16の検出する所定高度Hn
における所定吸気圧力Pnとの関係から、(Po−Pn
)=0のときは基準高度Hoたる高度Qmであるので、
k−,0となる。
Here, the reason why TAUH is not set as TAUo is that the air density and atmospheric temperature change due to changes in altitude, so these are corrected using the constant k. Therefore, the opening degree θ of the intake throttle valve 10 detected by the opening sensor 18 is equal to the reference intake pressure Po and the predetermined altitude Hn detected by the pressure sensor 16.
From the relationship with the predetermined intake pressure Pn in (Po−Pn
) = 0, the reference altitude Ho is the altitude Qm, so
k-,0.

このように、制御回路14によって、開度センサ18の
検出する吸気絞り弁10の開度θと基準吸気圧力Poお
よび圧力センサ16の検出する所定吸気圧力Pnとの関
係から燃料噴射時間TAUを補正することにより、高地
においては噴射時間を大きくして空燃比の薄化を防止し
、空燃比の適正化を果すことができる。
In this way, the control circuit 14 corrects the fuel injection time TAU based on the relationship between the opening θ of the intake throttle valve 10 detected by the opening sensor 18 and the reference intake pressure Po and the predetermined intake pressure Pn detected by the pressure sensor 16. By doing so, it is possible to increase the injection time at high altitudes, prevent the air-fuel ratio from becoming thinner, and optimize the air-fuel ratio.

このため、内燃機関2の出力を向上することができ、排
気ガス有害成分を低減することができ、また、燃料消費
率を向上することができる。
Therefore, the output of the internal combustion engine 2 can be improved, the harmful components of exhaust gas can be reduced, and the fuel consumption rate can be improved.

〔発明の効果〕〔Effect of the invention〕

このように、この発明によれば、制御手段によって、内
燃機関の吸気絞り弁所要開度状態に対応し基準高度にお
いて設定した基準吸気圧力と、前記内燃機関の吸気絞り
弁所要開度状態に対応し所定高度において吸気圧力検出
手段の検出する所定吸気圧力との差に応じ、内燃機関に
噴射供給する燃料量を補正すべく制御することにより、
高度変化に応じ内燃機関に噴射供給する燃料量を補正す
ることができる。
As described above, according to the present invention, the control means corresponds to the reference intake pressure set at the reference altitude corresponding to the required opening state of the intake throttle valve of the internal combustion engine and the required opening state of the intake throttle valve of the internal combustion engine. By controlling to correct the amount of fuel injected and supplied to the internal combustion engine according to the difference between the intake pressure and the predetermined intake pressure detected by the intake pressure detection means at a predetermined altitude,
The amount of fuel injected and supplied to the internal combustion engine can be corrected according to altitude changes.

これにより、空燃比の適正化を果し得て、内燃機関の出
力向上を果し得て、排気ガス有害成分を低減し得て、ま
た、燃料消費率の向上を果すことができる。
Thereby, the air-fuel ratio can be optimized, the output of the internal combustion engine can be improved, harmful components of exhaust gas can be reduced, and the fuel consumption rate can be improved.

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

第1〜3図はこの発明の実施例を示し、第1図は内燃機
関の燃料噴射高度補正装置の概略構成図、第2図は制御
手段のブロック図、第3図は制御のフローチャートであ
る。第4〜7図は高度変化による空燃比の変動を説明す
る図であり、第4図は高度と大気圧との関係を示す図、
第5図は吸気絞り弁開度と吸気圧力との関係を示す図、
第6図は吸気圧力と燃料噴射時間との関係を示す図、第
7図は高度と空燃比との関係を示す図である。 図において、2は内燃機関、4は吸気通路、8は排気通
路、10は吸気絞り弁、12は燃料噴射弁、14は制御
回路、16は圧力センサ、18は開度センサである。 特許出願人    鈴木自動車工業株式会社代理人 弁
理士  西 郷 義 実 用1図 第2図 第3図 第6図    第7図
1 to 3 show an embodiment of the present invention, FIG. 1 is a schematic configuration diagram of a fuel injection altitude correction device for an internal combustion engine, FIG. 2 is a block diagram of a control means, and FIG. 3 is a flowchart of control. . Figures 4 to 7 are diagrams illustrating fluctuations in air-fuel ratio due to changes in altitude, and Figure 4 is a diagram showing the relationship between altitude and atmospheric pressure.
Figure 5 is a diagram showing the relationship between intake throttle valve opening and intake pressure;
FIG. 6 is a diagram showing the relationship between intake pressure and fuel injection time, and FIG. 7 is a diagram showing the relationship between altitude and air-fuel ratio. In the figure, 2 is an internal combustion engine, 4 is an intake passage, 8 is an exhaust passage, 10 is an intake throttle valve, 12 is a fuel injection valve, 14 is a control circuit, 16 is a pressure sensor, and 18 is an opening sensor. Patent Applicant Suzuki Motor Co., Ltd. Agent Patent Attorney Yoshi Saigo Practical Figure 1 Figure 2 Figure 3 Figure 6 Figure 7

Claims (1)

【特許請求の範囲】[Claims] 燃料を噴射供給する内燃機関の吸気圧力を検出する吸気
圧力検出手段を設け、前記内燃機関の吸気絞り弁所要開
度状態に対応し基準高度において設定した基準吸気圧力
と前記内燃機関の吸気絞り弁所要開度状態に対応し所定
高度において前記吸気圧力検出手段の検出する所定吸気
圧力との差に応じ前記内燃機関に噴射供給する燃料量を
補正すべく制御する制御手段を設けたことを特徴とする
内燃機関の燃料噴射高度補正装置。
An intake pressure detection means for detecting the intake pressure of an internal combustion engine to which fuel is injected and supplied is provided, and a reference intake pressure set at a reference altitude corresponding to the required opening state of the intake throttle valve of the internal combustion engine and the intake throttle valve of the internal combustion engine are provided. A control means is provided for controlling the amount of fuel injected and supplied to the internal combustion engine in accordance with the difference between the intake pressure detected by the intake pressure detection means at a predetermined altitude and the required opening state. Fuel injection altitude correction device for internal combustion engines.
JP27405987A 1987-10-29 1987-10-29 Fuel injection height correcting device for internal combustion engine Pending JPH01116265A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27405987A JPH01116265A (en) 1987-10-29 1987-10-29 Fuel injection height correcting device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27405987A JPH01116265A (en) 1987-10-29 1987-10-29 Fuel injection height correcting device for internal combustion engine

Publications (1)

Publication Number Publication Date
JPH01116265A true JPH01116265A (en) 1989-05-09

Family

ID=17536395

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27405987A Pending JPH01116265A (en) 1987-10-29 1987-10-29 Fuel injection height correcting device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH01116265A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6792614B1 (en) 1999-09-29 2004-09-14 Matsushita Electric Industrial Co., Ltd. Optical disk apparatus and method of installing its spindle motor

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6098329A (en) * 1983-11-02 1985-06-01 Nissan Motor Co Ltd Pressure detector of internal-combustion engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6098329A (en) * 1983-11-02 1985-06-01 Nissan Motor Co Ltd Pressure detector of internal-combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6792614B1 (en) 1999-09-29 2004-09-14 Matsushita Electric Industrial Co., Ltd. Optical disk apparatus and method of installing its spindle motor

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