JPS6022042A - Apparatus for detecting engine temperature - Google Patents

Apparatus for detecting engine temperature

Info

Publication number
JPS6022042A
JPS6022042A JP12877183A JP12877183A JPS6022042A JP S6022042 A JPS6022042 A JP S6022042A JP 12877183 A JP12877183 A JP 12877183A JP 12877183 A JP12877183 A JP 12877183A JP S6022042 A JPS6022042 A JP S6022042A
Authority
JP
Japan
Prior art keywords
engine
temperature
sensor
output
detection
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
JP12877183A
Other languages
Japanese (ja)
Inventor
Yuji Nakajima
雄二 中島
Akito Yamamoto
明人 山本
Katsunori Oshiage
勝憲 押上
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP12877183A priority Critical patent/JPS6022042A/en
Publication of JPS6022042A publication Critical patent/JPS6022042A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/24Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
    • F02D41/26Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using computer, e.g. microprocessor
    • F02D41/28Interface circuits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D41/222Safety or indicating devices for abnormal conditions relating to the failure of sensors or parameter detection devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
  • Testing Of Engines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 (産業上の利用分野) この発明は、内燃機関用の電子式燃料供給■制御装量等
に好適な機関の温度検出装置に係わり、特に1幾関の暖
(戊申に温度ゼンザ巽常が発イ1;シたような場合、セ
ンサー異常発生後についても、比較的実際の機関温度に
近い値の出力を発するようにした装置に関する。
Detailed Description of the Invention (Field of Industrial Application) The present invention relates to an engine temperature detection device suitable for electronic fuel supply/control amount for internal combustion engines, and in particular, This invention relates to a device that outputs an output that is relatively close to the actual engine temperature even after a sensor abnormality occurs in the event that a temperature change occurs.

(発明の背景) 従来、特願昭56−.78725“号公報、97452
号公報等においては、内燃機関用の電子式燃判供給量制
御装買が開示されている。この電子式燃利供給聞制御装
置は、機関の回転数を示1′機閏lj]転数信号および
吸入空気mを示1吸入空気吊18号等を用いて機関に供
給ずべき基本燃料mを算出し、更に機関の冷却木調ある
いは曲調を示す機関温痘信号、吸入空気温度を表わづ吸
入空気温信号。
(Background of the invention) Conventionally, patent applications filed in 1982-. Publication No. 78725, 97452
In the above publications, an electronic fuel feed rate control device for an internal combustion engine is disclosed. This electronic fuel supply control device indicates the engine rotational speed, 1' engine leap lj] rotation speed signal, and the intake air m, 1 indicates the basic fuel m to be supplied to the engine using an intake air hanger No. 18, etc. In addition, an engine temperature signal indicating the engine cooling tone or tune, and an intake air temperature signal indicating the intake air temperature.

(層間がアイドル状態であるかどうかを示すアイドル接
勲信号等を用いて、前述の基本燃料量を補正し、この補
正された燃料量に応じて機関に燃料を供給りるちのであ
る。
(The above-mentioned basic fuel amount is corrected using an idle signal indicating whether or not the interlayer is in an idling state, and fuel is supplied to the engine according to this corrected fuel amount.

また、従来特開昭5 /!−141926丹公報には、
前記電子式燃利供給吊制(l′II装置に好適な機関の
湿度検出装置が開示され−Cいる。この渇麿検出H同は
、譬層間の温痘を検出]るヒンザに異常が生じた場合、
センナ異常発生後については、予め設定された一定値(
例えば、暖機完了後の通常機関温石)の温1良信号を出
力するようにしたもので、これを電子式燃料供給量制御
装置にJ用ずれば、機関温度センザの異常に起因し−C
11;旧カ温度に対応覆る燃判供給徂補正分に誤りが生
り゛ることを低減づることかでさた。
In addition, the conventional Japanese Patent Application Publication No. 5/1999/! -141926 Tan Publication states,
An engine humidity detection device suitable for the electronic fuel supply restriction (l'II device) is disclosed. If
After the Senna abnormality occurs, a preset constant value (
For example, it is designed to output a temperature 1 good signal (normal engine temperature sensor) after warm-up is completed, and if this is used in an electronic fuel supply amount control device, it will detect -C due to an abnormality in the engine temperature sensor.
11; It was possible to reduce the possibility of errors occurring in the correction of the fuel supply level corresponding to the old temperature.

しかしながら、このにうな従来の機関の温度検出装置に
あっては、機関湯面センリーに異常が生じIこ場合、そ
の後一定温度1−3(例えば、暖機後の定常状態にA3
4)る正常な検出温度)に相当覆る信号を出ツノするた
め、第1図に示づ機関温度が上界しつつある暖機中にセ
ンサ異常が発生づると、第2図に示す如く、温1良検出
装置の出力は突然に温度Δ]だ多用」シ、この結果図中
点線C゛示づ実際の機関温度との間には大きな誤差を生
じる。
However, in this conventional engine temperature detection device, if an abnormality occurs in the engine hot water level sensor, then the temperature will be constant at 1-3 (for example, A3 in the steady state after warm-up).
4) Since the sensor outputs a signal that is considerably higher than the normal detected temperature, as shown in Fig. 1, if a sensor abnormality occurs during warm-up when the engine temperature is rising, as shown in Fig. 2, The output of the temperature 1/good detection device suddenly becomes Δ], and as a result, a large error occurs between the output and the actual engine temperature shown by the dotted line C in the figure.

従って、このような温度検出装置の出ツノで燃料供給量
を補正するように構成した場合、暖機中であるために未
だI幾関の瀧瓜が低いにも拘わらず、既に暖機が完了し
″′C機関の温度が充分上昇しIζらのと誤認され、機
関低温時の燃料増量補正が行われないため、空燃比の低
下によって排気浄化性。
Therefore, if the configuration is such that the fuel supply amount is corrected based on the output of the temperature detection device, the warm-up has already been completed even though the temperature of the I-temperature is still low due to the warm-up process. The temperature of the ``C engine has risen sufficiently and it is mistaken for Iζ etc., and the fuel amount increase correction is not performed when the engine temperature is low, so the air-fuel ratio decreases and the exhaust purification performance decreases.

tW機性、運転性が低下し、更にはエンジンストールが
発生し易くなる等の問題点があった。
There were problems such as deterioration of tW functionality and drivability, and furthermore, engine stalling was more likely to occur.

(発明の目的) この発明↓ま、このような従来の問題点に着(コしてな
されIζもので、その目的とづるところは、(段間の暖
(戊申に機関湿度センサに異常が生じた場合、異常発生
後についても実際の(層間温度に近い信号を出力し続【
プるJ:うにした温度検出装胃を提供Jることにある。
(Purpose of the Invention) This invention was made in response to such conventional problems. If this occurs, a signal close to the actual interlayer temperature will continue to be output even after the abnormality has occurred.
Puru J: The aim is to provide a temperature sensor equipped with a sea urchin.

(発明の構成) 第3図は、このlFr明の構成を説明づるためのクレー
ム対応図である。
(Structure of the Invention) FIG. 3 is a claim correspondence diagram for explaining the structure of this IFr light.

同図において、温麿ヒンリ100は、機関の湿度を直接
にまたは冷却媒体、潤滑油等の温度をfrし°(間接的
に検出するものである。
In the same figure, Onmaro Hinri 100 detects the humidity of the engine directly or indirectly detects the temperature of the cooling medium, lubricating oil, etc.

−ll′i記憶手段101は、前記センサ100の最新
の検出出力を一時的に記1 !lるもので必る。
-ll'i Storage means 101 temporarily records the latest detection output of the sensor 100. It's a must have.

じン(〕゛異常検出手段102は、前記しンリ゛100
の検出出力にλ(づいて、センサの異常を判定りるもの
である。
The abnormality detection means 102 detects the
Based on the detection output of λ, abnormality of the sensor is determined.

(;笈関回転数検出手段103は、図示しない機関の回
転数を検出するものCある。
(The engine rotation speed detection means 103 is a device C that detects the rotation speed of an engine (not shown).

1層間状態判定手段10/Iは、前記Lンリ異常が検出
され!ことき、前記一時記憶された異常直前の[ンザ出
力の値に丼づいて、レン1)異常発生時が(段間の暖機
中か暖Ijl後かを判定覆るものである。
The first interlayer state determining means 10/I detects the above-mentioned L error! At this time, it is determined whether the abnormality occurred during (during warm-up between stages or after warm-up Ijl) based on the temporarily stored value of the output immediately before the abnormality.

出力選択手段105は、前記センナ100が正常と判定
されたときには、センサの実際の検出値を機関の温度と
しで出力する一方、前記センサーが異常でかつセンナ異
常発生後が暖機中と判定されたどきには、センナ異常発
生後については、セン号異常発生直前のセンV検出値と
レン+J異常発生後の機関回転数積算値とで決定される
各時点にJ3りる所定の予測検出値を、実際の検出値の
替わりに機関の温度として出tJターるちのである。
The output selection means 105 outputs the actual detected value of the sensor as the engine temperature when the senna 100 is determined to be normal, while it is determined that the sensor is abnormal and the engine is being warmed up after the senna abnormality occurs. After the Senna abnormality occurs, the predetermined predicted detection value J3 is determined at each point in time, which is determined by the SEN V detection value immediately before the SEN abnormality occurs and the integrated engine speed value after the SEN + J abnormality occurs. is output as the engine temperature instead of the actual detected value.

(実施例の説明) 以下に、本発明の好適な一実施例を第4図以下の図面を
参照しながら詳細に説明゛する。
(Description of Embodiment) A preferred embodiment of the present invention will be described in detail below with reference to the drawings from FIG. 4 onwards.

第4図は本発明に係わる温度検出装置を採用した電子式
燃料供給量制御装同全体のシステム構成を示すブ1コッ
ク図である。同図に示づ如く、この電子式燃料供給量制
御装置は、システムプログラム等を格納したROM1と
、ソー。1:ング1リア等としで利用されるRAM2と
、I10インターフJイス3と、これらを統括制御層る
C l) U 4とからなるマイクロコンビコータを主
体としで構成されている。
FIG. 4 is a block diagram showing the overall system configuration of an electronic fuel supply amount control device employing the temperature detection device according to the present invention. As shown in the figure, this electronic fuel supply amount control device includes a ROM 1 that stores system programs, etc. The system is mainly composed of a micro combi coater consisting of a RAM 2 which is used as a backing, an I10 interface Jice 3, and a C1) U4 which serves as an overall control layer for these.

110インターフエイス3には、機関回転数センリ5の
出力、I層間温度センリ6の出力d3J:び基本燃わ1
供給吊の鋒出およびその補正に必要な各科の廿ン→ノ(
例え1.(,1アフローセンリ等)からの伝りが供給さ
れている。
110 interface 3 contains the output of the engine speed sensor 5, the output of the I layer temperature sensor 6 d3J: and the basic combustion 1.
廿→ノ(
Example 1. (, 1 Aflosenri, etc.) is supplied.

ここで、機関回転数センサ5としでは、例えば′公知の
クランク角ヒン暑すからの出力パルスを一定I+、)間
ごとに01数りるカウンタ等で(j4成Jることができ
る。
Here, as the engine speed sensor 5, for example, output pulses from a well-known crank angle sensor can be calculated by a counter that increments 01 every time.

また、機関温石センサ6は、この例ぐは機関の冷IJI
媒体通路の所定部位に配置されたリーミスタ等からなる
感温抵抗素子6′1ど、この感温抵抗素子61と固定抵
抗62との合成抵抗値ど、固定抵抗63とで基W、雷電
圧cを分圧’J−7,) 、J:うにした分圧回路と、
抵抗6/Iど二1ンデン4ノロ5とで構成され、前記分
JJ回路のノイズ出力成分を除去する積分回路とく・構
成され、機関σ2温度に対応したアナ■」グミ圧Viを
出力覆るように構成され−(いる。
In addition, the engine warm stone sensor 6 is connected to the cold IJI of the engine, for example.
A temperature sensitive resistance element 6'1, such as a reamister or the like, disposed at a predetermined portion of the medium path, a combined resistance value of this temperature sensitive resistance element 61 and a fixed resistance 62, a fixed resistance 63, a base W, and a lightning voltage c. A voltage dividing circuit with a voltage division 'J-7, ) , J:
It is composed of a resistor 6/I, 21, 4, 5, and an integral circuit that removes the noise output component of the JJ circuit. It is composed of - (is.

ここで、このil;i度センリ−6の出力電圧viと機
関の温度との間には、例えば第6図に示ず関係が設定さ
れており、すなわち第6図の例では(大関温度の変化し
得る範囲を1°L= THとすれば、正常な湿aセンザ
6の出力Viの値は、VL−V’Hの箱間〇直線的に変
化づるように設定されている。
Here, for example, a relationship not shown in FIG. 6 is set between the output voltage vi of the sensor 6 and the engine temperature, that is, in the example of FIG. If the range of variation is 1°L=TH, the value of the output Vi of the normal humidity a sensor 6 is set to vary linearly between the boxes of VL-V'H.

また、不揮発性メ王す7は、CPU4からの制御でRE
AD−WRIT’E可能に構成されており、かつCP 
U 4に対する電源が断たれた後も、記憶情報を保持す
るような構成となつでいる。具体的には、例えばFΔM
O8,MΔS、MNO3′8の半導体不揮発性メ[りを
使用したり、あるいはイクニツションスイッチを経由す
ることなくバッテリからの電源C直接バックアップされ
た]でΔM等で構成することができる。
In addition, the non-volatile menu 7 is controlled by the CPU 4.
AD-WRIT'E is possible and CP
The configuration is such that the stored information is retained even after the power to U4 is cut off. Specifically, for example, FΔM
It can be configured as ΔM, etc. by using semiconductor nonvolatile memory such as O8, MΔS, and MNO3'8, or by directly backing up the power supply C from the battery without going through an ignition switch.

また、温度センサ異常警報装置8は、ブヂーあるいは音
声合成LSIとスピーカの組合は等の聴覚警報手段、ラ
ンプ、0R−r等の視覚警報手段その仙触覚的な警報手
段管種々の構成を採用づることがCき、要するに温度セ
ンサ6に異常が生じlζ場合これを直ちにあるいは所定
の操作に応じて警報するものである。
Further, the temperature sensor abnormality alarm device 8 employs various configurations including auditory alarm means such as a combination of a boogie or a voice synthesis LSI and a speaker, a visual alarm means such as a lamp, an 0R-r, and a tactile alarm means. In other words, if an abnormality occurs in the temperature sensor 6, an alarm is issued immediately or in response to a predetermined operation.

また、燃料噴射弁駆動回路9は、1710インター゛ノ
]イス3からの所定の信号に応じて、燃料用0・1弁用
の駆動コイル10を駆動づるものである。
Further, the fuel injection valve drive circuit 9 drives the drive coil 10 for the fuel 0/1 valve in response to a predetermined signal from the 1710 interface 3.

なお、燃r3+噴射弁の具体的な構成は種々公知である
ため説明は省略づ−る。
It should be noted that various specific configurations of the fuel r3+ injection valve are well known, and therefore description thereof will be omitted.

次に、第5図はこの電子弐瘤目z1供給吊制御装置の動
作に必要なシステムブ[1グラムの構成を示す′ノロー
ブrr −t−’P ilうり、以下にこのフロー11
?−1−に従って、この実施例装置の動作を系統的に説
明する。’ch J3、このブ]二1グラムは所定時間
ごとに起iFIノされるプログラムC1いわゆる115
間同期手法を用いている。
Next, FIG. 5 shows the system block necessary for the operation of this electronic second eye z1 supply suspension control device.
? -1-, the operation of this embodiment device will be systematically explained. 'ch J3, this block] 21g is a program C1 so-called 115 that is started every predetermined time.
An inter-synchronization method is used.

j、す゛、ステップ〈1)では、1,10インターフ]
、イス3を介して、1段間回転数レン1す5の出力。
j, su゛, step <1), 1,10 interf]
, the output of the inter-stage rotation speed lens 1-5 via the chair 3.

++l r!El温1良レンリ6の出力おにび前述した
各種センサからの出力がマイクロニ」ンビ」−夕に読込
J、れ、これらの読込まれlζ各データはCP LJ、
 4を介してRAM2のワーキングエリアに設けられた
該貫層る各レジスタに記10される。
++l r! The outputs from the various sensors mentioned above are read in from the micro-minimum unit 6, and each of these read data is CP LJ,
4 to each register provided in the working area of the RAM 2.

ごこC,l段間温度しンリ−6の出力は、現在温度レジ
スタr< 1− +に、J、た機関回転数センサ5の出
力は現在回転数レジスタRNに記憶されるものとする。
It is assumed that the output of the inter-stage temperature sensor 6 is stored in the current temperature register r<1-+, and the output of the engine rotation speed sensor 5 is stored in the current rotation speed register RN.

次いで、ステップ(2>、(3)では、現在渇磨レジス
タ1(11の記憶内容で示される現在渇爪T1が、機関
湿度センサ6が正常な場合に検出し得る下限温a −r
 Lよりも低いか、J3よび上限渦電1’ HJ:りも
高いかの判定が行なわれる。
Next, in steps (2>, (3)), the current thirst T1 indicated by the stored contents of the current thirst register 1 (11) is set to the lower limit temperature a - r that can be detected when the engine humidity sensor 6 is normal.
A determination is made as to whether it is lower than L or higher than J3 and upper limit eddy current 1'HJ:.

ここで、1層間温度レンサ6が正常な場合には、これら
のステップ(2>、(3)の実行結果は何れもNoどな
り、続いてステップ(4)が実行されて、2スデージシ
フトレジスタとして機能づるF IFO(First 
in J:1rsl Qut)スタックには現在瀧麿レ
ジスタR−1−+の記憶内容がブツシュされる。
Here, if the first interlayer temperature sensor 6 is normal, the execution results of these steps (2> and (3) are both No, and then step (4) is executed and the second stage shift register FIFO (First
in J:1rsl Qut) The contents of the current Takimaro register R-1-+ are written to the stack.

これに対して、機関温度センサ−6が異常な場合には、
ステップ(2)またはステップ(3)の何れかが必ずY
ESとなり、続いてステップ(5)が実行されて、不揮
発性メモリ7内に設けられたセン+Jn常フラグF T
は1″にセラ1〜される。
On the other hand, if the engine temperature sensor 6 is abnormal,
Either step (2) or step (3) must be Y.
ES, and then step (5) is executed, and the sen+Jn normal flag F T provided in the non-volatile memory 7 is
is set to 1''.

従つ11以後マイクロコンピユータの電源が断たれたと
しr::ら、センサ異常フラグFTの内容は保持され、
例えば整備工揚笠で111両を整備づる際に所定のシス
テムプログラムによってこのセン1す異常フラグFTの
内容を読み出Uば、子の時点にif5い(1ンサ異常が
見られなくとも、過去にセン1)異常が発生し/ご場合
には、そのことを整備の際に発見することができる。
Therefore, if the power to the microcomputer is cut off after 11, the contents of the sensor abnormality flag FT are retained.
For example, when a mechanic lifts 111 cars and reads out the contents of this sensor 1 abnormality flag FT using a predetermined system program, it is possible to read out the contents of this sensor 1 abnormality flag FT at the time of child maintenance (even if no sensor abnormality is observed in the past). 1) If an abnormality occurs, it can be discovered during maintenance.

次いで、ステップ(6)が実行されると、直前渦電レジ
スタR−raには、FIFOスタックから胱i)出され
たヒンリ訳常直前の検出篇1度データが転送される。
Next, when step (6) is executed, the immediately preceding detection data taken out from the FIFO stack is transferred to the immediately preceding eddy current register R-ra.

次いで、ステップ(7)が実行されると、irl前温度
レジしタR’I’ oの記憶内容C示されるセン1ノ屓
常ii!i前の4iJI I!J瀧度1−0が、畷(幾
完了後の機関湿度−[Sよりも低いか否かに基づいて、
センザ異常光生Il″jが暖1j!i完了前1なわら暖
機中であるかどうかの判定が行なわれる。
Next, when step (7) is executed, the memory contents of the irl pre-temperature register R'I'o are shown as the result of the sensor 1! i before 4iJI I! Based on whether J Taki degree 1-0 is lower than Nawate (engine humidity after completion - [S),
It is determined whether or not the sensor abnormal light output Il''j is being warmed up since it is 1 before the completion of warming 1j!i.

ここC′、センサ異常フラグが暖機完了後であった場合
には、ステップ(,7)の実行結果はNOどなり、続い
てステップ(8)が尖1jされて、現在温度レジスタR
’1− +には、暖機完了1殺の通常温度Tsに相当J
る1′−夕が転送され、次いでステップ(4)の実行と
ともに、この現在温度レジスタR−r +の内容はFI
FOスタックへとブツシュされる。
Here, C', if the sensor abnormality flag is after the completion of warm-up, the execution result of step (, 7) will be NO, then step (8) will be executed, and the current temperature register R will be returned.
'1-+ corresponds to the normal temperature Ts at the end of warm-up completion J
1'-T is transferred, and then with the execution of step (4), the contents of this current temperature register R-r+ are transferred to FI
Pushed onto the FO stack.

これに対して、センサ異常フラグが暖(戊申であった場
合、ステップ(7)の実行11I!i果はYESとなり
、続いてステップ(9)が実行されて機関温度予測処理
が行なわれる。
On the other hand, if the sensor abnormality flag is warm (warm), the result of step (7) is YES, and step (9) is then executed to perform engine temperature prediction processing.

この機関温度予測処理では、直前温度レジスタR王0に
記憶されたセンサ異常発生直前の温度下。と機関回転数
レジスタRNに記憶された機関回転数Nとに基づいて、
次式により現在の機関の予測温度がめられる。
In this engine temperature prediction process, the temperature is below the temperature immediately before the occurrence of sensor abnormality, which is stored in the immediately preceding temperature register R0. Based on the engine speed N stored in the engine speed register RN,
The current predicted temperature of the engine can be determined by the following equation.

予測温度−TO+に−N・・・(1) ここで、上r;dの(1)式は、第7図に実線で示す如
く、暖機中の機関温度は機関回転数偵算賄に比例して直
線的に増加すると見なした上で決定されたもので、また
係数にの値はステップ(1)で行なわれる各入力情報読
込周JilJ等に基づいて実験的に定められるものであ
る。
Predicted temperature -TO+ -N...(1) Here, equation (1) for r; d above is based on the engine temperature during warm-up as shown by the solid line in Figure 7. It is determined based on the assumption that it increases linearly in proportion, and the value of the coefficient is determined experimentally based on the reading frequency of each input information performed in step (1). .

イして、(1)式でめられた1幾関の予測温1良(,1
、現(J:温度レジスタ1チー1°1に記憶される。
Then, the predicted temperature of 1, which is determined by equation (1), is 1 good (,1
, current (J: stored in temperature register 1 1° 1).

次いで、ステップ(10)が実行されると、現在湯度レ
ジスタR−「+の記憶内容で示される機関の予測温度が
、暖機完了後の一定温1良1− s以上であるかfiか
に基づいC,機関の暖機が完了したか否かの予測が行な
われる。
Next, when step (10) is executed, it is determined whether the predicted temperature of the engine indicated by the stored contents of the current hot water temperature register R-"+ is equal to or higher than the constant temperature 1-s after warm-up is completed. Based on C, a prediction is made as to whether or not warm-up of the engine has been completed.

ここで、機関の1敗(幾が完了したしのと予測された場
合に【jl、ステップ(10)の実行結果はYESとな
り、続いてステップ(8)が実行されて、現在温度レジ
スタ1<T1には暖I幾完了後の(層間温度USに相当
づるデータが書込まれる。
Here, if it is predicted that the engine will have one loss (1), the execution result of step (10) will be YES, then step (8) will be executed, and the current temperature register 1 < Data corresponding to the interlayer temperature US after the completion of warming I is written in T1.

これに灼して、暖機中と予測された場合には、ステップ
(10)の実行結果はNOとなり、続い−(“スーテッ
プ(4)が実行されて、F I F Oスタックには予
測された現在の機1′!!温度に相当づるi−タが1ツ
シコされる。
If it is predicted that it is warming up, the execution result of step (10) will be NO, and then -("Step (4) will be executed, and the predicted One i-ta corresponding to the temperature of the current machine 1'!! is sent.

このJ、うに、Ifi l!Q tilt反Uンリー6
が正常な場合にLet、現在潟)貨レジスタR−I’ 
+には常に実際の検出温度に相当°す゛るデータが書込
まれる。
This J, Uni, Ifil! Q tilt anti-unley 6
If it is normal, let, current lag) currency register R-I'
+ is always written with data corresponding to the actual detected temperature.

これに対して、センサ異常が翔生じた場合には、センサ
異常フラグが暖機中か暖機完了後かに応じて次のような
2つの動作が行なわれる。
On the other hand, when a sensor abnormality occurs, the following two operations are performed depending on whether the sensor abnormality flag is set during warm-up or after warm-up is completed.

゛づなわら、センサ異常が暖(火中に発生した場合には
、第7図に示1如く、センリ異常発生後畷機完了が予測
されるまCの間は、回転数積算値に比例して直線的増加
層る予測渇1立を出力し、他方暖機が完了したものと予
測された11こおいては、暖機完了後の通常温度Tsに
相当する信号を出力Jることになる。
However, if the sensor abnormality occurs during a warm fire, as shown in Figure 7 (1), during the period C when the sensor abnormality is predicted to be completed, it will be proportional to the cumulative rotational speed. In the case of 11 where warm-up is predicted to be completed, a signal corresponding to the normal temperature Ts after warm-up is output is output. .

また、センサ異常が暖機完了後に発生した場合には、セ
ンサ異常発生直後から暖機完了後の通常温度1−sに相
当する信号を出力づることになる。
Further, if a sensor abnormality occurs after the completion of warm-up, a signal corresponding to the normal temperature 1-s after the completion of warm-up is output immediately after the sensor abnormality occurs.

従って、第7図に実線で示り一子1111機関濡度と点
線で示寸実際の機関温度との誤差は充分小さなlif&
に制限され、センサ異常発生後についても実際q)lj
la関温疫に近い(直を出力し続tプることになる。
Therefore, the error between the Ichiko 1111 engine wetness indicated by the solid line in Fig. 7 and the actual engine temperature indicated by the dotted line is sufficiently small.
is limited to q) lj even after sensor abnormality occurs.
It's close to La Seki's fever (it will output direct and continue to be output).

次いで、ステップ(11)〜(15)にa3い1、電子
式燃料供給開制御処理がT5なわれる訳であるが、この
処理については4Φ々の文献にJ3いて既に公知くある
ため一例を挙げて曲中に説明づる。
Next, in steps (11) to (15), the electronic fuel supply opening control process is performed at T5, but since this process is already known in the literature of 4Φ, I will give an example. It is explained during the song.

スーフップ(11)では、y;(本哨用単相当パルス幅
11)の演iが行なJつれる。この演掠においてtよ、
−Lアノ0− t?ンリの出力に阜づい(吸入空気mQ
を512めるとともに、機関回転数センサーに基づいて
機関回転数Nをめ、これらに基づいて1吸気゛F(?に
吸入される空気量Q / Nをit n t−’、更に
燃料哨用ブrの流量特性を8慮して、Q/Nに比例する
ように基本パルス幅1pを決定りる。
In the super-fup (11), the operation i of y; (main sentry single equivalent pulse width 11) is performed. In this play, T.
-L Anno 0- t? (intake air mQ)
512, determine the engine speed N based on the engine speed sensor, and based on these, calculate the amount of air Q / N taken into 1 intake ゛F (?), and further calculate the fuel flow rate. The basic pulse width 1p is determined in proportion to Q/N, taking into consideration the flow rate characteristics of the pulse r.

次いで、ステップ(12)では、(j1関湿度増n1補
正係数1<TWがめられる。この(層間温I良増ω補i
t係数1<TWをめるために、前述した現在温度レジス
タR王1の記憶j゛−夕が使用される。この補正係数の
しl的は、機関冷温時におい(、燃焼安定化のために燃
料を増呈し、排気浄化性、暖機性、j車QV、’ l!
Iを改善し、エンジンスト−ルの発生を防止りるものC
ある。
Next, in step (12), it is determined that (j1 relative humidity increase n1 correction coefficient 1<TW).
In order to determine the t coefficient 1<TW, the memory of the current temperature register R1 described above is used. The purpose of this correction coefficient is when the engine is cold and hot (increasing fuel for combustion stabilization, exhaust purification, warm-up performance, vehicle QV, 'l!
Things that improve I and prevent engine stalls C
be.

次いで、ステップ(13)ではその仙各種の補正係数の
演件が行な4つれる。その他の補正係数としては次のよ
うなものがある。
Next, in step (13), four calculations are performed for each type of correction coefficient. Other correction coefficients include the following.

1<AS:始動時増1B補正 KAt;アイドル後増量 K 14 R;混合比補正 KFC:フューエル・カッ1〜 ]−8;電圧補正 次いで、ステップ(14)では、以」−求めら、れた基
本哨射吊相当パルス幅1” pと台秤の補正係数とに基
づいて、次式により通常の噴IJJ fllのパルス幅
1°outがめられる。
1<AS: Increase at startup 1B correction KAt; Increase after idling K 14 R; Mixture ratio correction KFC: Fuel cut 1~ ]-8; Voltage correction Next, in step (14), Based on the basic sentry suspension equivalent pulse width 1'' p and the correction coefficient of the platform scale, the pulse width 1° out of the normal injection IJJ flll can be calculated from the following equation.

T Oすt −= T 11 ・ (1+l<TW →
−K A S 十 K Δ 1+1< 間 尺 ) ・
 K F C・ α −ト Ts=’Ie<イj効噴射
吊)+13 次いで、ステップ(15)では、以上求められた出力パ
ルス幅1−outに基づいて、燃料nQ川用御信号を燃
料噴射弁駆動回路9に出力し、これに基づいて燃料噴射
弁のコイル10が駆動され、機関に対して所望の燃お1
吊が供給されることにhる。
T Ost −= T 11 ・ (1+l<TW →
-K A S 1 K Δ 1+1
K F C・α-t Ts='Ie<Ij effect injection suspension)+13 Next, in step (15), the fuel nQ river control signal is used to inject the fuel based on the output pulse width 1-out obtained above. Based on the output to the valve drive circuit 9, the coil 10 of the fuel injection valve is driven, and the desired fuel level is delivered to the engine.
I'm glad that the suspension will be provided.

次いで、ステップ(16)では、前記不揮発性メモリ7
に設けられlζセンサ異常フラグFrがII I II
にレッt−6れでいるか否かの判定が行なわ1する。
Next, in step (16), the non-volatile memory 7
II II II
A determination is made as to whether or not the number is t-6.

ここで・、センリ眉常が過去に発生した場合、スj−ツ
7(16)の実行結果はY E’Sとなり、続いてスラ
ップ(17)が実行され−〔、温石レン(う異常警報装
置F!r8に対して所゛定の警報出力が発せられ、これ
に基づい−C腎報装置8によっ−C温麿レし9に?シ常
が生じlこことを視覚的、聴覚的あるいは触覚的に報知
りることになる。
Here, if an abnormality alarm has occurred in the past, the execution result of SJ-TS 7 (16) will be Y E'S, and then Slap (17) will be executed. A predetermined alarm output is issued to the device F!r8, and based on this, the -C kidney reporting device 8 causes an alarm to occur in the -C temperature range 9. Or, it will be tactile information.

かくして、この実施例ににれば、機関温度Lンリに異常
が生じたll[j合、直営発生後についても、実際の機
関温度に近い温度を出力し続すさせることができる1゜ t〃っ−(、これを公知の電子式燃利唱射吊制御装置門
に適用し、か′つ(層間濡1廊増吊補正係数KTWの(
ン出に必要な機関?!11麿の検出手段どして使用覆れ
ば、仮に暖(戊申に1幾関温1復ヒン1すに異常が生じ
た明白に−6、補1係数1<TWのずれを最小に留め、
機関温度に応じて正常な補正処理を行なわせることがで
きる。
Thus, according to this embodiment, when an abnormality occurs in the engine temperature L, it is possible to continue outputting a temperature close to the actual engine temperature even after the occurrence of the direct operation. (, Applying this to the well-known electronic fuel injection suspension control device gate, and ()
What institutions are needed for the project? ! 11 If we were to use a different detection means, it would be obvious that an abnormality had occurred in the warmer temperature (-6). ,
It is possible to perform normal correction processing according to the engine temperature.

更に、温度センサに異常が生じたときには、これを直ち
に運転化に警告できるととしに、整備上場等において過
去の温度センサの異常をも確認でさる。
Furthermore, if an abnormality occurs in the temperature sensor, this can be immediately alerted to operation, and past abnormalities in the temperature sensor can also be confirmed during maintenance listings, etc.

なお、前記実施例を説明Jるのに用いたプログラムは所
定時間ごとに起動するいわゆる時間同期プログラムであ
るが、これに代えて所定(層間回転角度ごとにプログラ
ムを起動りる角度同期プログラムであっても良い。
The program used to explain the above embodiment is a so-called time synchronized program that starts at predetermined time intervals, but instead of this, an angle synchronized program that starts a program at predetermined (interlayer rotation angles) may be used. It's okay.

その場合、予測温度をめる前記(1)式に代えて、下記
のように予測温度がめられる。
In that case, the predicted temperature can be calculated as follows instead of the above equation (1) for calculating the predicted temperature.

予測温度−TO+l(d・・・(2) つまり、所定機関回転角度ごとの温度上昇が定数Kdで
あり、づなわち暖機中の予測温度は1層間回転数積篩値
に比例しで直線的に上テvしていく。
Predicted temperature - TO + l (d... (2) In other words, the temperature rise for each predetermined engine rotation angle is a constant Kd, that is, the predicted temperature during warm-up is proportional to the interlayer rotation speed product sieve value and is a straight line. I will continue to improve my skills.

なJ3、定数K dの値は、プログラム起動周111、
づなわち何度ごとにプログラムを起動1−るか等に基づ
いて実験的にめられるものである。まIこ、前記実施例
では、機関温度センサの最新の検出用ツノを一時的に記
憶するl〔めの手段として、PIFOスタックを用いた
が、これに代えてI10インターフ「イス3の外部に2
ステージシフ1−レジスタを段り、このシフトレジスタ
にJ−って(層間渇度eンリ−6の出力を一〇・Y的に
記イ彦Jるようにしても1q<、更に機関記麿ヒンリ6
の出力側を2系統に分岐しで、一方については直接にI
10インターノ1イス3に入力するどどL)に、他方に
ついてはアブ[]グ近延回路を介しく若干)1y延した
後同様に110インターフ]−イス3にへカし、センリ
ー異常が生じた01点で前記遅延された検出信号を読込
むようにしても良い。
J3, the value of the constant Kd is the program startup cycle 111,
In other words, this can be determined experimentally based on how often the program is started. In the above embodiment, the PIFO stack was used as a means for temporarily storing the latest detection horn of the engine temperature sensor, but instead of this, the 2
Even if you set up a stage shift 1 register and record the output of the interlayer thirst level 6 as 10/Y in this shift register, 1q<, and further engine memory. Hinri 6
The output side of the is branched into two systems, and one is directly connected to
10 interno 1 is input to chair 3), and the other one goes through the ab[]g Chikanobu circuit a little) 1y) and then similarly goes to 110 interno 1 - chair 3, causing a sentry abnormality. The delayed detection signal may be read at the 01 point.

また、1jlJ +iE実施例では、eンリの検出出力
に基づいて、eンリ−の異常を判定する手段として、【
?ンリの検出11r1が所定の上下限1fif)IQ 
1− H、’l−Lがら外れることを判定りるJ、うに
しlζが、これに代えし−1,限5ノ、たけ下限の一方
だ()を兄て¥シ常を判定1ノでも良く、更にはセン(
J−の検出用ツノの変化率が所定の(10を越えたこと
に基づいて51<常を判定りるようにしCも良い。
In addition, in the 1jlJ+iE embodiment, [
? IQ
1- J, sea urchin lζ, which determines that H, 'l-L is out of range, replaces -1, limit 5 no, one of the lower limits () and determines ¥shi always 1 node. But it's fine, and even better (
It is also possible to determine whether 51<normally based on the fact that the rate of change of the detection horn of J- exceeds a predetermined value (10).

また、1)う記実施例−r IJ: 、機関の回転数を
検出するだめの手段として、クランク角センVと子の出
力をカウントするカウンタでIR成したが、これについ
−(もディストリビュータに段t)られだ光学式ロータ
リエンコーダからの信号に基づ゛い′て(爪間の回転数
を検出しても良い。
In addition, 1) Embodiment-r IJ: As a means of detecting the engine rotational speed, an IR was constructed using a crank angle sensor V and a counter that counts the child's output. Step t) Based on the signal from the rotary optical rotary encoder (the number of rotations between the pawls may be detected).

また、前記実施例では、センザ異常発生直前のセンリ゛
検出値どセンリ直営発生後の機関回転数積算値とで各時
点における所定の検出値を予測覆るlこめの手段として
、実験的に定められた直線を表わす数式に回転数を代入
するという方法を使用したが、これに代えて各回転数積
算値ど当該積n値に対応する(股間温度どの関係を予め
デープルに作成し、いわゆるテーブルルックアップの手
法を用いて機関温度を予測しても良いことは勿論であり
、更にこの実施例では暖機中にJ3りる機関温度が直線
的に上昇するものど仮定しlζが、これを実際の検出曲
線に近イ11〕でラープルを作成し、より精密な近似予
測を行なうことができることは勿論である。
In addition, in the above-mentioned embodiment, the sensor detection value immediately before the sensor abnormality occurs and the integrated value of the engine rotation speed after the sensor abnormality occurs are used to predict and overturn the predetermined detection value at each point in time. We used a method of substituting the number of revolutions into a mathematical formula representing a straight line, but instead of this, each integrated value of number of revolutions corresponds to the product n value. It is of course possible to predict the engine temperature using the above method, and furthermore, in this example, it is assumed that the engine temperature rises linearly during warm-up. Of course, it is possible to create a curve near the detection curve 11] and perform more accurate approximate predictions.

また、1)IC実施例では本発明に係わる温度検出装置
を電了式燃お1供給吊制御装置に適用したが、本発明1
4首の適用はこれに限定されるしのCはなく、例えば機
1nの温度に応じて冷ノJJ 77ンの起動時1+11
を制御りるJ、うにした冷N1水温麿制御システム、イ
の他暖(戊申の1幾関湿痕に応じC何らかの出力を制御
づるJ:うなす゛べでのシステムに応用りることが可能
である。
In addition, 1) In the IC example, the temperature detection device according to the present invention was applied to an electric lighting type fuel 1 supply suspension control device, but the present invention 1
The application of 4 necks is not limited to this and there is no C. For example, depending on the temperature of the machine 1n, when starting the cold JJ 77n 1+11
A cold N1 water temperature control system that controls the water temperature, and a warm water temperature control system that controls some kind of output depending on the humidity level of the water temperature control system. It is.

(発明の効果) 以−1の実施例の説明でも明らかなJζうに、この発明
にJ、れば暖機中に機関温麿ヒンリに異常が生じ!ごよ
うな」9合、直営発生1ねについ’Cbl戊関の湿1身
に比較的近い出力を発生し続けることができ、従つくこ
れを例えば公知の電子式燃利供給吊制御装置にa31J
る(層間温度増爪補正係教紳出のための(層間湿麿検出
手段どしく使用Jれは′、暖I戊申に(層間温度じンリ
“に異常が生じても、機関温度増ff!補’+I’ t
ui fy>に〜える形管を可及的に低減させ、従来の
)11A麿検出装置で問題となっ1.:空燃比の稀薄化
に起因りる111気浄化性、暖1幾1!l 、運転性の
低]・を防止し、更に(,1エンジンスト−ルの発生も
防止できるという効果がある。
(Effects of the Invention) As is clear from the explanation of Example 1 below, if this invention is used, an abnormality will occur in the engine temperature during warm-up! In the 9th stage, it is possible to continue to generate an output relatively close to that of the CBL Bozeki for each directly operated generator, and this can be applied to a well-known electronic fuel supply suspension control system, for example, on the A31J.
(In order to correct the interstitial temperature increase, please use the interstitial humidity detection means properly.) !Supplementary '+I' t
ui fy > to reduce the number of shaped tubes as much as possible, and eliminate problems with conventional) 11A detection devices.1. : 111 air purification properties due to the dilution of the air-fuel ratio, making it warmer! This has the effect of preventing poor drivability] and also preventing the occurrence of engine stall.

【図面の簡単な説明】 第1図は機関温度セン勺が正常な場合にお1)る回転数
積算値と(層間潴麿検出値との関係を示リグラフ、f1
52図は従来の機関温度検出装置にJjlプる回転数積
算値と補正出力値との関係示Jグラフ、第3図は本発明
を説明覆るだめのクレーム対応図、第4図は本発明を適
用した電子式燃判供給晴制御共同のシステム構成を示1
−ブロック図、第5図は本発明を適用した電子式燃料供
給量制御装置Tfの制御用マイコンで実行されるシステ
ムプ1]グラムの構成を示タフローヂ1F−ト、第6図
は温麿ヒンサの出力と1層間温度との関係を示Jグラフ
、第7図は本発明に係わる温度検出装置NにJjける回
転数積算値と温度出力との関係を示Jグラフである。 1・・・RO,M 2・・・RAM 3・・・I10インターフlイス 4・・・CPLI 5・・・1;31関回転数センυ 6・・・・・・・・・(層間温度センザ7・・・・・・
・・・不揮発性メしり 8・・・・・・・・・温度センリー異常警報装置9・・
・・・・・・・燃料噴射弁駆動回路10・・・・・・燃
1′8I噴射弁のコイル100・・・温石センザ 101・・・一時記憶手段 102・・・セン勺異常検出手段 103・・・1層間回転数検出手段 104・・・機関状態判定手段 105・・・出力選択手段 特v1出願人 1]産自動車株式会社 第5図
[Brief explanation of the drawings] Figure 1 is a graph showing the relationship between the integrated rotational speed value (1) and the interlayer detection value when the engine temperature sensor is normal.
Fig. 52 is a J graph showing the relationship between the integrated rotational speed value and the corrected output value applied to a conventional engine temperature detection device, Fig. 3 is a diagram corresponding to claims that do not cover the present invention, and Fig. 4 is a graph showing the relationship between the integrated rotational speed value and the corrected output value applied to a conventional engine temperature detection device. The system configuration of the applied electronic fuel supply and clearing control system is shown below.
-Block diagram, Fig. 5 shows the configuration of the system program executed by the control microcomputer of the electronic fuel supply amount control device Tf to which the present invention is applied. FIG. 7 is a J graph showing the relationship between the rotational speed integrated value and temperature output of the temperature detecting device N according to the present invention. 1...RO, M 2...RAM 3...I10 interface 4...CPLI 5...1; 31 function rotation speed sensor υ 6......(interlayer temperature Senza 7...
...Non-volatile meter 8...Temperature sensor abnormality alarm device 9...
...Fuel injection valve drive circuit 10 ... Fuel 1'8I injection valve coil 100 ... Warm stone sensor 101 ... Temporary storage means 102 ... Temperature abnormality detection means 103 ... 1-layer rotational speed detection means 104 ... Engine state determination means 105 ... Output selection means Special v1 Applicant 1] San Jidosha Co., Ltd. Figure 5

Claims (1)

【特許請求の範囲】[Claims] (1)機関の温石を直接にまたは冷却媒体、潤滑油等の
温度を介して間接的に検出づ°るセンサと;前記センサ
の最新の検出出力を一時的に記憶づる一時開1n手段と
; 前記センサの検出出力に基づいてセンサの異常を判定り
るセンサ異常判定手段と: l!、l!門の回転数を検出づるための機関回転数検出
手段と; 前記レンリ巽常が検出されたとさ、前記一時開10され
た異常直前のセンサ出力の値に基づいて、レンリ゛異常
発生時が機関の暖機中か暖機後かを判定Jる機関状態判
定手段と: 前記セン1ノが1常なときには、センサの実際の検出値
を機関の&i度として出力づ゛る一方、前記セン1ノが
異常でか−)センサ異常発生時が暖機中と判定されたと
きには、センサ異常発生後については、センサー異常発
生直前のセンサ検出値とヒンサ異常発生後の機関回転数
積粋値とで決定される各時点におりる所定の予測検出値
を、実際の検出値の替わりに(層間の温度として出力づ
る出力選択手段とを具備することを特徴と・する機関の
温度検出装置。
(1) A sensor that detects the hot stone of the engine directly or indirectly through the temperature of the cooling medium, lubricating oil, etc.; Temporary opening means that temporarily stores the latest detection output of the sensor; Sensor abnormality determination means for determining abnormality of the sensor based on the detection output of the sensor; and: l! ,l! an engine rotational speed detection means for detecting the rotational speed of the gate; an engine state determining means for determining whether the engine is being warmed up or after warming up; If it is determined that the engine is warming up when the sensor abnormality occurs, the sensor detection value immediately before the sensor abnormality occurs and the integral value of the engine rotation speed after the sensor abnormality occur. 1. A temperature detection device for an engine, comprising an output selection means for outputting a predetermined predicted detected value at each determined time point as an interlayer temperature instead of an actual detected value.
JP12877183A 1983-07-15 1983-07-15 Apparatus for detecting engine temperature Pending JPS6022042A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12877183A JPS6022042A (en) 1983-07-15 1983-07-15 Apparatus for detecting engine temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12877183A JPS6022042A (en) 1983-07-15 1983-07-15 Apparatus for detecting engine temperature

Publications (1)

Publication Number Publication Date
JPS6022042A true JPS6022042A (en) 1985-02-04

Family

ID=14993059

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12877183A Pending JPS6022042A (en) 1983-07-15 1983-07-15 Apparatus for detecting engine temperature

Country Status (1)

Country Link
JP (1) JPS6022042A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01100346A (en) * 1987-10-14 1989-04-18 Daihatsu Motor Co Ltd Fail-safe system for water temperature sensor failure
JPH01110859A (en) * 1987-10-23 1989-04-27 Daihatsu Motor Co Ltd Fuel control method at time of pressure sensor trouble
JPH0272343U (en) * 1988-11-17 1990-06-01
JPH03294642A (en) * 1990-04-09 1991-12-25 Nissan Motor Co Ltd Control device for engine
US5694897A (en) * 1996-01-26 1997-12-09 Denso Corporation Water temperature sensor failure detecting device for idle speed control system
JPH09329060A (en) * 1996-06-10 1997-12-22 Toyota Motor Corp Hybrid vehicle catalyst temperature control device
US7272942B2 (en) * 2003-04-30 2007-09-25 Air Products And Chemicals, Inc. Method and system for purifying exhaust gas

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01100346A (en) * 1987-10-14 1989-04-18 Daihatsu Motor Co Ltd Fail-safe system for water temperature sensor failure
JPH01110859A (en) * 1987-10-23 1989-04-27 Daihatsu Motor Co Ltd Fuel control method at time of pressure sensor trouble
JPH0272343U (en) * 1988-11-17 1990-06-01
JPH03294642A (en) * 1990-04-09 1991-12-25 Nissan Motor Co Ltd Control device for engine
US5694897A (en) * 1996-01-26 1997-12-09 Denso Corporation Water temperature sensor failure detecting device for idle speed control system
JPH09329060A (en) * 1996-06-10 1997-12-22 Toyota Motor Corp Hybrid vehicle catalyst temperature control device
US7272942B2 (en) * 2003-04-30 2007-09-25 Air Products And Chemicals, Inc. Method and system for purifying exhaust gas

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