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JPS5914168B2 - Internal combustion engine intake air flow rate detection device - Google Patents
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JPS5914168B2 - Internal combustion engine intake air flow rate detection device - Google Patents

Internal combustion engine intake air flow rate detection device

Info

Publication number
JPS5914168B2
JPS5914168B2 JP53000770A JP77078A JPS5914168B2 JP S5914168 B2 JPS5914168 B2 JP S5914168B2 JP 53000770 A JP53000770 A JP 53000770A JP 77078 A JP77078 A JP 77078A JP S5914168 B2 JPS5914168 B2 JP S5914168B2
Authority
JP
Japan
Prior art keywords
intake air
internal combustion
vortex
combustion engine
flow rate
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
Application number
JP53000770A
Other languages
Japanese (ja)
Other versions
JPS5494074A (en
Inventor
和幸 水田
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP53000770A priority Critical patent/JPS5914168B2/en
Publication of JPS5494074A publication Critical patent/JPS5494074A/en
Publication of JPS5914168B2 publication Critical patent/JPS5914168B2/en
Expired legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Measuring Volume Flow (AREA)

Description

【発明の詳細な説明】 この発明はカルマン渦を利用した内燃機関の吸入空気流
量検出装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an intake air flow rate detection device for an internal combustion engine that utilizes Karman vortices.

内燃機関の燃料噴射システムには吸入空気量の時々刻々
の測定が必要である。
The fuel injection system of an internal combustion engine requires momentary measurement of the amount of intake air.

また吸入空気通路中に渦発生柱を配設し、該渦発生柱の
下流側に生じるカルマン渦を計測して流体流量を計測す
るいわゆる渦流量計は、可動部がないために耐振性に富
み、移動用の内燃機関、特に自動車に適した流量計であ
ると云える。ところで内燃機関の吸入空気は一様な流れ
でなく脈動しているので渦発生柱を設けた場合、安定で
斉整な渦が発生しない。特5 にスロットル弁が全開付
近のマニホールド負圧が約50mmH9以下の小さいと
きは、この脈動が激しく発生する渦の数が不規則となり
流量計として信頼できない欠点がある。この吸入空気の
脈動は、特に多気筒機関におい10て各吸入弁動作の重
なりから生じるもので、負圧のサージパルスが吸入弁の
開いた瞬間に発生する。
In addition, so-called vortex flowmeters, which measure fluid flow rate by arranging a vortex generation column in the intake air passage and measuring the Karman vortices generated downstream of the vortex generation column, have excellent vibration resistance because they have no moving parts. It can be said that this flowmeter is suitable for mobile internal combustion engines, especially automobiles. However, since the intake air of an internal combustion engine does not flow uniformly but pulsates, if a vortex generating column is provided, stable and uniform vortices will not be generated. Particularly, when the manifold negative pressure near the fully open throttle valve is small, about 50 mmH9 or less, the number of vortices generated by this intense pulsation becomes irregular, making it unreliable as a flowmeter. This pulsation of the intake air is caused by the overlapping operation of each intake valve, especially in a multi-cylinder engine, and a negative pressure surge pulse occurs at the moment the intake valve opens.

ス頭ノトル弁が閉じている状態においては、負圧のサー
ジパルスはスロットル弁のオリフィス効果によりそれよ
り上流側では充分減衰されるので渦15流量計の渦は斉
整に発生し流量計として正常にその機能を発揮するが、
スロットル弁の全開付近ではスロットル弁の上流側でも
充分には減衰されず、吸入空気の流れをみたし渦の発生
が不規則となり流量計として信頼できないものとなる。
20この発明は上記の実情に鑑み、スロットル弁の全開
付近においても渦発生柱を通過する空気流の脈動を抑制
し安定した渦を発生させることにより、全運転領域に亘
つて安定した流量検出を可能にしようとするものである
When the head nottle valve is closed, the negative pressure surge pulse is sufficiently attenuated upstream due to the orifice effect of the throttle valve, so the vortices of the vortex 15 flowmeter are generated in unison and the flowmeter operates normally. It performs its functions, but
When the throttle valve is fully open, it is not sufficiently damped even on the upstream side of the throttle valve, which blocks the flow of intake air and generates vortices irregularly, making it unreliable as a flowmeter.
20 In view of the above-mentioned circumstances, this invention suppresses the pulsation of the airflow passing through the vortex generating column and generates a stable vortex even when the throttle valve is fully open, thereby achieving stable flow rate detection over the entire operating range. It attempts to make it possible.

以下図に示すこの発明の25実施例について説明する。
即ち、先ず第1図において1は図示しない内燃機関に吸
入空気を導びく吸入空気導管で、その途中には空気吸入
量を制御するス頭ノトルバルブ2が設けられている。
Hereinafter, 25 embodiments of the present invention shown in the figures will be described.
That is, first, in FIG. 1, reference numeral 1 denotes an intake air conduit that guides intake air to an internal combustion engine (not shown), and a notch valve 2 for controlling the amount of air intake is provided in the middle of the conduit.

3は上記スロットルバルブ230より上流側に吸入空気
の流れに直交するように配設された渦発生柱、4はこの
渦発生柱によつて発生される吸入空気のカルマン渦に対
し超音波を発射する超音波発振子で超音波発生器4aに
より、駆動される。
Reference numeral 3 denotes a vortex generating column arranged perpendicular to the flow of intake air on the upstream side of the throttle valve 230, and 4 emits ultrasonic waves to the Karman vortices of the intake air generated by this vortex generating column. The ultrasonic oscillator is driven by an ultrasonic generator 4a.

5は上記カルマン渦によつて変調され35た上記超音波
発振子4からの超音波を受信する受信子で、この受信子
の出力は処理回路5aによつて周波数−電圧変換されて
カルマン渦の数(周波数)に対応した電圧出力を得るも
のであり、これらによつてカルマン渦の数を検出する検
出器が構成される。
Reference numeral 5 denotes a receiver for receiving the ultrasonic waves from the ultrasonic oscillator 4 modulated by the Karman vortex, and the output of this receiver is frequency-voltage converted by the processing circuit 5a to generate the Karman vortex. A voltage output corresponding to the number (frequency) is obtained, and these constitute a detector that detects the number of Karman vortices.

6は空気室Aを構成するエアタンク、7は上記空気室A
を上記吸入空気導管1の上記検出器より下流側部に連通
する連通パイプである。
6 is an air tank that constitutes air chamber A, and 7 is the air chamber A.
This is a communication pipe that communicates with the downstream side of the detector of the intake air conduit 1.

次にこの様に構成されたものの動作について説明する。
吸入空気導管1に吸入された空気は渦発生柱3の後部に
流量に対応した数のカルマン渦をつくりスロツトルバル
ブ2を経由して内燃機関の吸入弁から吸人される。
Next, the operation of the device configured as described above will be explained.
The air sucked into the intake air conduit 1 creates Karman vortices in the number corresponding to the flow rate at the rear of the vortex generating column 3, and is sucked in from the intake valve of the internal combustion engine via the throttle valve 2.

発生した渦は、超音波発振子4からの超音波に対しその
渦に対応した周波数信号を混人させ、これを受信子5が
受信し処理回路5aによつて空気流量に対応した電圧出
力に変換される。マニ小一ルド負圧の高いときはスロツ
トルバルブが閉じられ一部しか開口していないので、機
関の吸入弁からの負の圧力サージはこ\で反射され、一
部通過した分もその圧力降下で減衰して人口付近のカル
マン渦検出部の吸入空気に影響を及ぼさないのは前述の
通りである。
The generated vortex mixes a frequency signal corresponding to the vortex with the ultrasonic wave from the ultrasonic oscillator 4, which is received by the receiver 5 and converted into a voltage output corresponding to the air flow rate by the processing circuit 5a. converted. When the manifold primary negative pressure is high, the throttle valve is closed and only partially opened, so the negative pressure surge from the engine's intake valve is reflected by this, and the pressure that partially passes through is also reduced. As mentioned above, it is attenuated by descent and does not affect the intake air of the Karman vortex detector near the population.

マニホールド負圧が約50m7!LH9を下廻るころか
らスロツトルバルブの開口面積は大きくなりオリフイス
効果はなくなり、吸入弁の開いた瞬間に生じる負の圧力
サージは吸人空気導管1内を入口方向に向つて減衰しな
がら進行する。ここで、エアタンク6と吸入空気導管1
との圧力は連通パイプ7を通して共鳴しそれら間で進行
波の通過インピーダンスが低下するので、連通パイプ7
の点までで負の圧力サージは吸収減衰されそれ以上入口
側への影響は抑制され、カルマン渦検出部付近の空気流
には干渉しない。こ\で空気室Aの体積、及び連通パイ
プ7の吸入空気導管1に対する開口位置、連通パイプ7
の孔径は実験的に最適値に設定することが望ましい。こ
の場合、エアタンク6は連通パイプ7によつて吸入空気
導管1に連通しているので、スロツトルバルブ2より更
に下流側の負の圧力サージ発生源付近に連通させること
もできるので、効果的な開口位置の設定が可能である。
しかして、マニホールド負圧の高いところからスロツト
ルバルブ全開位置のマニホールド負圧の低い範囲全域に
亘つて吸入空気流の脈動を抑制し斉整なる渦を発生させ
得る。第2図はこの発明の他の実施例を示すもので、2
つの空気室A,Bをタンク6a,6bにより構成し、該
2つの空気室A,Bを連通パイプ7A,7bにより吸入
空気導管1と連通させたものであり、このものにおいて
、互いに異なる共鳴周波数を得ることができるので圧力
サージの減衰効果範囲を増大させることができる。
Manifold negative pressure is approximately 50m7! From around LH9, the opening area of the throttle valve increases and the orifice effect disappears, and the negative pressure surge that occurs at the moment the suction valve opens advances in the intake air conduit 1 toward the inlet while being attenuated. . Here, the air tank 6 and the intake air conduit 1
The pressure between the two resonates through the communicating pipe 7, and the passing impedance of the traveling wave decreases between them.
Up to this point, the negative pressure surge is absorbed and attenuated, and its influence on the inlet side is suppressed beyond that point, and it does not interfere with the air flow near the Karman vortex detection section. Here, the volume of the air chamber A, the opening position of the communication pipe 7 with respect to the intake air conduit 1, and the communication pipe 7
It is desirable to set the pore diameter to the optimum value experimentally. In this case, since the air tank 6 is connected to the intake air conduit 1 through the communication pipe 7, it can also be connected to the vicinity of the negative pressure surge generation source further downstream from the throttle valve 2, so that it can be effectively It is possible to set the opening position.
Therefore, it is possible to suppress the pulsation of the intake air flow and generate a uniform vortex over the entire range from the high manifold negative pressure to the low manifold negative pressure at the fully open position of the throttle valve. FIG. 2 shows another embodiment of this invention.
The two air chambers A and B are composed of tanks 6a and 6b, and the two air chambers A and B are communicated with the intake air conduit 1 through communication pipes 7A and 7b. Therefore, the range of pressure surge damping effect can be increased.

第3図はこの発明の更に別の実施例を示すもので、タン
クを別に設けることなく、径と長さを設定したパイプ8
によつて空気室Aを構成したもので、このものは吸入空
気導管1に対する連通と空気室Aの構成とが同時に行な
い得る。
FIG. 3 shows yet another embodiment of the present invention, in which a pipe 8 with a set diameter and length is provided without a separate tank.
The air chamber A is configured by the air chamber A, which allows communication with the intake air conduit 1 and the configuration of the air chamber A to be performed at the same time.

この実施例のものにあつてもパイプ8の径と長さを適当
に設定することにより上述と同様の作用効果を奏し得る
。以上の如く、この発明によれば、スロツトルバルブの
全開付近のマニホールド負圧が低い範囲においてもカル
マン渦検出部付近の空気流の脈動を抑制し安定した渦を
発生させ得、よつて機関の全運転範囲に亘り安定した流
量検出を可能とし得る。
Even in this embodiment, the same effects as described above can be achieved by appropriately setting the diameter and length of the pipe 8. As described above, according to the present invention, even in a range where the manifold negative pressure near the fully opened throttle valve is low, it is possible to suppress the pulsation of the airflow near the Karman vortex detection part and generate a stable vortex, thereby improving the engine performance. Stable flow rate detection may be possible over the entire operating range.

更には空気室はパイプによつて吸入空気導管に連通させ
たので、その空気導管に対する連通位置の設定も容易と
なり、製造上有益である。又、空気室は空気流の脈動の
大きい上記内燃機関の特定の運転状態において共鳴作用
により吸気脈動を低減するものであるから、上記特定の
運転状態における吸気脈動を効果的に低減できるもので
ある。
Furthermore, since the air chamber is communicated with the intake air conduit through the pipe, it is easy to set the communication position with respect to the air conduit, which is advantageous in manufacturing. Furthermore, since the air chamber reduces intake pulsation through resonance in a specific operating state of the internal combustion engine in which air flow pulsation is large, it is possible to effectively reduce intake pulsation in the specific operating state. .

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

第1図乃至第3図はこの発明の各実施例を示す断面構成
図である。 図中、1は吸入?気導管、2はスロツトルバルブ、3は
渦発生柱、4は超音波発振子、5は受信子、6はエアタ
ンク、A,Bは空気室、7は連通パイプである。
1 to 3 are cross-sectional configuration diagrams showing each embodiment of the present invention. In the diagram, 1 is inhalation? 2 is a throttle valve, 3 is a vortex generation column, 4 is an ultrasonic oscillator, 5 is a receiver, 6 is an air tank, A and B are air chambers, and 7 is a communicating pipe.

Claims (1)

【特許請求の範囲】[Claims] 1 内燃機関の吸入空気通路に吸入空気の流れ方向に対
して略直交するように配設された渦発生柱によつて発生
する吸入空気の渦の数を検出する渦検出器、及び上記渦
発生柱より下流側の上記吸入空気通路に対し、上記渦発
生部での吸気脈動が大きい内燃機関の特定の運転状態に
おいて共鳴作用によつて該吸気脈動を低減させる空気室
を連通させるパイプを備えた内燃機関の吸入空気流量検
出装置。
1. A vortex detector that detects the number of vortices in intake air generated by a vortex generation column arranged in an intake air passage of an internal combustion engine so as to be substantially perpendicular to the flow direction of the intake air, and the vortex generator described above. A pipe is provided that connects the intake air passage downstream of the pillar with an air chamber that reduces intake pulsation through resonance in a specific operating state of an internal combustion engine in which intake pulsation is large in the vortex generating section. Intake air flow rate detection device for internal combustion engines.
JP53000770A 1978-01-06 1978-01-06 Internal combustion engine intake air flow rate detection device Expired JPS5914168B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP53000770A JPS5914168B2 (en) 1978-01-06 1978-01-06 Internal combustion engine intake air flow rate detection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP53000770A JPS5914168B2 (en) 1978-01-06 1978-01-06 Internal combustion engine intake air flow rate detection device

Publications (2)

Publication Number Publication Date
JPS5494074A JPS5494074A (en) 1979-07-25
JPS5914168B2 true JPS5914168B2 (en) 1984-04-03

Family

ID=11482921

Family Applications (1)

Application Number Title Priority Date Filing Date
JP53000770A Expired JPS5914168B2 (en) 1978-01-06 1978-01-06 Internal combustion engine intake air flow rate detection device

Country Status (1)

Country Link
JP (1) JPS5914168B2 (en)

Also Published As

Publication number Publication date
JPS5494074A (en) 1979-07-25

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