JPH0241688B2 - - Google Patents

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Publication number
JPH0241688B2
JPH0241688B2 JP55139803A JP13980380A JPH0241688B2 JP H0241688 B2 JPH0241688 B2 JP H0241688B2 JP 55139803 A JP55139803 A JP 55139803A JP 13980380 A JP13980380 A JP 13980380A JP H0241688 B2 JPH0241688 B2 JP H0241688B2
Authority
JP
Japan
Prior art keywords
air
flow rate
passage
flow
internal combustion
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 - Lifetime
Application number
JP55139803A
Other languages
Japanese (ja)
Other versions
JPS5764109A (en
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 filed Critical
Priority to JP55139803A priority Critical patent/JPS5764109A/en
Publication of JPS5764109A publication Critical patent/JPS5764109A/en
Publication of JPH0241688B2 publication Critical patent/JPH0241688B2/ja
Granted legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01FMEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/68Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using thermal effects

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)

Description

【発明の詳細な説明】 本発明は内燃機関の空気流量測定装置に関し、
特に、熱線式空気流量計により内燃機関の空気通
路を通る吸入空気量を測定する空気流量測定装置
に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an air flow rate measuring device for an internal combustion engine.
In particular, the present invention relates to an air flow measuring device that measures the amount of intake air passing through an air passage of an internal combustion engine using a hot wire air flow meter.

従来、内燃機関の吸入空気量を測定するため種
種の方式が用いられているが、その中で、熱線式
空気流量計を用いる方式は一般的に応答性が良く
かつ空気の質量流量が測定できるので、気圧補正
を必要としない等の理由で広く用いられている。
これについては特公昭49−48893号、特開昭47−
19227号、および特開昭51−64134号に記載され公
知となつている。
Conventionally, various methods have been used to measure the amount of intake air in internal combustion engines, but among these methods, methods using hot wire air flowmeters generally have good response and can measure the mass flow rate of air. Therefore, it is widely used because it does not require atmospheric pressure correction.
Regarding this, JP-A-49-48893, JP-A-47-
No. 19227 and Japanese Patent Application Laid-Open No. 51-64134 and is well known.

しかし、熱線式空気流量計を用いた流量測定装
置では、応答性を良くするためにその熱容量を小
さくしなければならず、検知部が微細な構造とな
り耐久性に劣るという欠点があつた。特に、内燃
機関が不調であるときに生ずるバツクフアイアー
によつて基本的な損傷を受け易いという欠点があ
つた。また、バツクフアイアー時だけでなく、エ
ンジンの回転により脈動が激しい時には給気が逆
流する場合があり、一方、熱線式空気流量計の性
質として逆流の場合も整流と同様に出力するの
で、このような逆流が生じる場合には実際の吸入
空気量よりも多い値を検知しこれに基づいた信号
を出力するので、測定値が不正確になるという欠
点もあつた。
However, a flow measuring device using a hot wire air flowmeter has the disadvantage that its heat capacity must be reduced in order to improve responsiveness, and the sensing portion has a fine structure, resulting in poor durability. In particular, they have the disadvantage of being susceptible to fundamental damage from backup fire that occurs when the internal combustion engine is malfunctioning. In addition, not only during backfire, but also when there is intense pulsation due to engine rotation, supply air may flow backwards.On the other hand, due to the nature of hot wire air flowmeters, even if there is a backward flow, it will output the same as if it were rectified. When a backflow occurs, a value larger than the actual amount of intake air is detected and a signal based on this is output, which has the disadvantage that the measured value becomes inaccurate.

本発明の目的は以上のような従来技術の欠点を
解消し、内燃機関の運転状態のいかんにかかわら
ず安定した高精度な測定を行いうる内燃機関の空
気流量測定装置を提供することである。特に、内
燃機関の吸入空気流が伴う場合の測定精度を向上
させた空気流量測定装置を提供することに主目的
がある。
SUMMARY OF THE INVENTION An object of the present invention is to provide an air flow rate measuring device for an internal combustion engine that can eliminate the drawbacks of the prior art as described above and perform stable and highly accurate measurements regardless of the operating state of the internal combustion engine. In particular, the main objective is to provide an air flow rate measuring device with improved measurement accuracy when accompanied by an intake air flow of an internal combustion engine.

すなわち、本発明によれば、内燃機関の給気通
路を通る吸入空気量を測定する空気流量測定装置
において、給気通路を横切る方向に突出するよう
取付けられた流速測定管の上流側側面に空気取入
口を設けるとともに下流側側面に空気出口を設
け、前記流速測定管内を長さ方向に延在する仕切
壁により前記空気取入口から前記空気出口へ通じ
る空気通路を形成し、該空気通路内に設置された
流速測定用抵抗体を有する熱線式流量計を設ける
ことを特徴とする内燃機関の空気流量測定装置が
提供される。
That is, according to the present invention, in an air flow rate measuring device that measures the amount of intake air passing through an air supply passage of an internal combustion engine, air is placed on the upstream side of a flow rate measuring tube that is attached to protrude in a direction across the air supply passage. An air intake port is provided and an air outlet is provided on the downstream side surface, an air passageway leading from the air intake port to the air outlet is formed by a partition wall extending in the length direction within the flow velocity measuring tube, and an air passageway is formed in the air passageway. An air flow rate measuring device for an internal combustion engine is provided, which is characterized in that it includes a hot wire flow meter having a flow rate measuring resistor installed therein.

以下図面を参照して本発明の作動原理および各
種の好的実施例について説明する。
The operating principle and various preferred embodiments of the present invention will be explained below with reference to the drawings.

第1図は本発明の作動原理の説明図である。 FIG. 1 is an explanatory diagram of the operating principle of the present invention.

第1図において、主空気通路である給気通路1
にバイパス路(バイパス空気通路)20を形成
し、該バイパス路内に熱線式流量計の流速測定用
抵抗体6を設置する形式の空気流量測定装置にお
いて、内燃機関の吸入空気流が逆流する場合の前
記バイパス路20内の空気の流れは次のようにな
る。なお、第1図中の矢印Xは逆流時の空気の流
れ方向を示す。
In Figure 1, air supply passage 1 which is the main air passage
In an air flow measuring device of the type in which a bypass passage (bypass air passage) 20 is formed in the bypass passage and a flow rate measuring resistor 6 of a hot wire flowmeter is installed in the bypass passage, when the intake air flow of the internal combustion engine flows backward. The air flow in the bypass passage 20 is as follows. Note that the arrow X in FIG. 1 indicates the flow direction of air during backflow.

第1図において給気通路1内の空気の流れを非
圧縮性の一次元流と仮定し、その摩擦損失を無視
すると次のような関係式が得られる。
In FIG. 1, assuming that the air flow in the air supply passage 1 is an incompressible one-dimensional flow and ignoring its friction loss, the following relational expression is obtained.

∂u/∂t+u∂u/∂x=−1/p∂p/∂x …(1) ∂/∂x(uA)=0 …(2) ここで、Aは通路断面積、uは空気流速、pは
圧力、ρは空気密度、xは基準点から流れ方向に
沿つた距離、tは時間をそれぞれ示し、式(1)は運
動方程式を、式(2)は連続の式を示す。
∂u/∂t+u∂u/∂x=-1/p∂p/∂x...(1) ∂/∂x(u A )=0...(2) Here, A is the passage cross-sectional area and u is the air In the flow velocity, p is the pressure, ρ is the air density, x is the distance along the flow direction from the reference point, and t is the time, Equation (1) shows the equation of motion, and Equation (2) shows the equation of continuity.

式(1)を第1図中のバイパス空気通路20の空気
入口Aから空気出口Bまで積分すると、 pB(t)−pA(t)/ρ=l1du/dt …(3) となる。ここでl1は点Aから点Bまでの距離であ
る。
When formula (1 ) is integrated from the air inlet A to the air outlet B of the bypass air passage 20 in FIG. Become. Here l 1 is the distance from point A to point B.

式(3)より、逆流時には点Bの圧力は点Aの圧力
より高くなるため、バイパス空気通路20内の空
気の流れは矢印Yのようになる。この場合、熱線
式空気流量計では逆流の時にも整流の時と同様の
信号が出力されるので、理想的には逆流の時流速
測定用抵抗体(熱線)6が設置されるバイパス空
気通路20内の空気流速を零にする必要がある。
そのためには、点Aと点Bとの圧力差がほゞ零で
ある必要がある。このことは、式(3)より、点Aか
ら点Bまでの距離l1を小さくしできるだけ零に近
づけることを意味する。
According to equation (3), the pressure at point B becomes higher than the pressure at point A during backflow, so the air flow in the bypass air passage 20 is as shown by arrow Y. In this case, since the hot wire air flow meter outputs the same signal as during rectification even during reverse flow, ideally the bypass air passage 20 where the resistor (hot wire) 6 for measuring flow velocity during reverse flow is installed. It is necessary to reduce the air flow velocity inside to zero.
For this purpose, the pressure difference between point A and point B needs to be almost zero. According to equation (3), this means that the distance l 1 from point A to point B is made small and as close to zero as possible.

しかし、逆流時の点Aと点Bとの圧力差を完全
に零にすることは難しい。このため、圧力差があ
つてバイパス空気通路20内の空気が動かないよ
うにする方法が考えられる。そのためには、バイ
パス空気通路20内の空気の慣性を大きくすれば
良い。すなわち、バイパス空気通路20の長さを
ある程度長く確保するか、またはバイパス空気通
路20内にサージタンクを設けることにより、空
気の慣性を大きくすることができる。
However, it is difficult to completely reduce the pressure difference between points A and B during backflow to zero. For this reason, a method can be considered to prevent the air in the bypass air passage 20 from moving due to the pressure difference. To achieve this, it is sufficient to increase the inertia of the air within the bypass air passage 20. That is, by ensuring a certain length of the bypass air passage 20 or by providing a surge tank within the bypass air passage 20, the inertia of the air can be increased.

本発明は以上の作動原理を考慮してなされたも
のであり、本発明の特徴は、バイパス空気通路ま
たはこれに相当する空気通路内に熱線式流速計の
流速側定用抵抗体(熱線)を設置するものにおい
て、バイパス空気通路の入口と出口との間の給気
通路1内における直線距離l1を小さくし、かつ、
該バイパス空気通路内の空気の慣性を所定値以上
に維持することである。
The present invention has been made in consideration of the above operating principle, and the feature of the present invention is that a constant resistor (hot wire) on the flow velocity side of a hot wire type anemometer is installed in the bypass air passage or an air passage equivalent to this. In the installation, the linear distance l 1 in the air supply passage 1 between the inlet and outlet of the bypass air passage is made small, and
The objective is to maintain the inertia of the air within the bypass air passage above a predetermined value.

この場合、前記空気通路の途中にサージタンク
室を設ければ、該空気通路内の空気の慣性をいつ
そう大きくすることができる。
In this case, if a surge tank chamber is provided in the middle of the air passage, the inertia of the air within the air passage can be greatly increased.

以下第2図ないし第10図を参照して本発明の
各種の実施例を説明する。
Various embodiments of the present invention will be described below with reference to FIGS. 2 to 10.

第2図および第3図は本発明の内燃機関の空気
流量測定装置の一実施例を示す図である。
FIGS. 2 and 3 are diagrams showing an embodiment of the air flow measuring device for an internal combustion engine according to the present invention.

第2図において、給気通路1内には上方から矢
印Z方向に空気が流入し下方に位置する内燃機関
へ流入する。なお、内燃機関への空気の供給は図
示の給気通路1の下流側に設置された気化器の絞
り弁(図示せず)を介して行なわれる。
In FIG. 2, air flows into the air supply passage 1 from above in the direction of arrow Z and flows into the internal combustion engine located below. Note that air is supplied to the internal combustion engine through a throttle valve (not shown) of a carburetor installed downstream of the air supply passage 1 shown.

給気通路1の側壁には、通路断面積を小さくし
て空気の流速分布を一様にするためのベンチユリ
2が設けられている。該ベンチユリ2の部分の給
気通路1の壁には、該給気通路を横切る方向に突
出するよう取付けられた流速測定管3が設置され
ている。該流速測定管の上流側側面には空気取入
口4が形成され、下流側端面2は空気出口10が
形成されている。流速測定管3内は長さ方向に延
在する仕切壁22により上流側部分および下流側
部分に仕切られており、該仕切壁22により前記
空気取入口4から前記空気出口10へ通じる比較
的長い空気通路5が形成されている。
A bench lily 2 is provided on the side wall of the air supply passage 1 to reduce the cross-sectional area of the passage and make the air flow velocity distribution uniform. A flow rate measuring tube 3 is installed on the wall of the air supply passage 1 in the area of the bench lily 2 so as to protrude in a direction across the air supply passage. An air intake port 4 is formed on the upstream side surface of the flow rate measuring tube, and an air outlet 10 is formed on the downstream end surface 2. The inside of the flow rate measuring tube 3 is partitioned into an upstream portion and a downstream portion by a partition wall 22 extending in the length direction, and the partition wall 22 allows a relatively long pipe to connect from the air intake port 4 to the air outlet 10. An air passage 5 is formed.

前記空気通路5内部すなわち図示の場合該空気
通路5の右端折返し部は、熱線式空気流量計の流
速測定用抵抗体6および温度補償用抵抗体7が設
置されている。また、空気通路5内の流速測定用
抵抗体6の上流側には整流格子23が設けられて
いる。なお、符号8は熱線式空気流量計の電子回
路を示し、この電子回路は前記流速測定用抵抗体
6および温度補償用抵抗体7に電気的に接続さ
れ、これらからの信号を受けて空気流量を演算す
る。また、符号9は前記電子回路8をおおう電子
回路カバーを示す。
Inside the air passage 5, that is, in the case of illustration, at the right end folded portion of the air passage 5, a flow rate measuring resistor 6 and a temperature compensating resistor 7 of a hot wire air flow meter are installed. Further, a rectifying grid 23 is provided on the upstream side of the flow rate measuring resistor 6 in the air passage 5. Reference numeral 8 indicates an electronic circuit of the hot-wire air flowmeter, which is electrically connected to the flow rate measuring resistor 6 and temperature compensation resistor 7, and receives signals from these to determine the air flow rate. Calculate. Further, reference numeral 9 indicates an electronic circuit cover that covers the electronic circuit 8.

第2図において、前記空気取入口4には全圧
(動圧+静圧)は加わるようになつており、前記
空気出口10は流れに平行な開口面を有し静圧の
みが加わるようになつている。こうすることによ
り、流速測定管3の空気取入口4および空気出口
10の間には、空気流の動圧のみが作用するよう
に構成されている。また、整流格子23を設ける
ことにより、空気通路5内の空気流が整流され、
熱線式流量計における測定信号の精度が改善され
ると共に流速測定用の抵抗体6と温度補償用抵抗
体7の破損を防止する効果がある。
In FIG. 2, the air intake port 4 is configured to receive total pressure (dynamic pressure + static pressure), and the air outlet 10 has an opening surface parallel to the flow so that only static pressure is applied. It's summery. By doing so, only the dynamic pressure of the air flow acts between the air intake port 4 and the air outlet 10 of the flow rate measuring tube 3. Furthermore, by providing the rectifying grid 23, the air flow within the air passage 5 is rectified.
This has the effect of improving the precision of the measurement signal in the hot wire flowmeter and preventing damage to the flow velocity measuring resistor 6 and the temperature compensating resistor 7.

以上説明した第2図および第3図に示す実施例
によれば、第1図中に示した距離l1、第2図にお
ける空気取入口4と空気出口の間隔を最小限にす
ることができ、しかも流速測定管3の上流側に向
けて空気取入口4を設けたので吸入気の動圧のみ
を取り入れることができ、正流成分のみを精度良
く測定できる。さらに、流速測定用抵抗体6と空
気取入口4との間の距離を大きくすることができ
るので、慣性が大きくなり、パルス状の圧力変動
の伝達を吸収したり、又はおくらせて、流速測定
用抵抗体6部分が逆流にならないから、内燃機関
の運転状態のいかんにかかわらず安定した高精度
な流量測定を行なうことができる。特に、内燃機
関への吸入空気流が逆流を伴なう場合でも空気出
口10が逆流に直面しないので、逆流成分が切り
捨てられ、吸入空気量の測定精度を大幅に向上さ
せることができる。
According to the embodiment shown in FIGS. 2 and 3 described above, the distance l 1 shown in FIG. 1 and the distance between the air intake port 4 and the air outlet in FIG. 2 can be minimized. Moreover, since the air intake port 4 is provided toward the upstream side of the flow rate measurement tube 3, only the dynamic pressure of the intake air can be taken in, and only the forward flow component can be measured with high accuracy. Furthermore, since the distance between the flow velocity measuring resistor 6 and the air intake port 4 can be increased, the inertia is increased, and the transmission of pulse-like pressure fluctuations can be absorbed or slowed down, and the flow velocity can be measured. Since the resistor 6 portion does not cause backflow, stable and highly accurate flow rate measurement can be performed regardless of the operating state of the internal combustion engine. In particular, even if the intake air flow to the internal combustion engine is accompanied by a backflow, the air outlet 10 does not face the backflow, so the backflow component is discarded, and the accuracy of measuring the amount of intake air can be significantly improved.

第4図および第5図は第2図および第3図の空
気通路5内にサージタンク室11を設けた第二実
施例を示す図である。この実施例はサージタンク
室11を設けた点のみで第2図および第3図の実
施例と異なり、その他の構造はすべて実質上同じ
である。
FIGS. 4 and 5 are views showing a second embodiment in which a surge tank chamber 11 is provided in the air passage 5 of FIGS. 2 and 3. FIG. This embodiment differs from the embodiments shown in FIGS. 2 and 3 only in that a surge tank chamber 11 is provided, and all other structures are substantially the same.

サージタンク室11を設けることにより、空気
通路5内の空気の慣性をさらに増大させることが
でき、もつて、吸入空気流の脈動流の平坦化を行
うことにより流量測定の精度をいつそう向上させ
ることができる。
By providing the surge tank chamber 11, it is possible to further increase the inertia of the air in the air passage 5, and by flattening the pulsating flow of the intake air flow, the accuracy of flow rate measurement is further improved. be able to.

第6図および第7図は本発明の内燃機関の空気
流量測定装置の第三実施例を示す図である。この
実施例は、第4図および第5図の実施例において
流速測定管3を給気通路1を横切つて反対側壁部
(ベンチユリ2の壁部)内へ延在させ、両端で固
定しその機械的強度の向上が図られている。この
場合、空気取入口4は流速測定管の上流側壁面に
形成され、空気出口10は給気通路1内の空気流
にほぼ平行な側面に形成されている。図示のごと
く、これら空気取入口および空気出口は給気通路
のほぼ中央部に形成されている。この場合も空気
取入口4には全圧(動圧+静圧)が作用するが、
空気出口10には静圧のみが作用するようにされ
ている。
6 and 7 are diagrams showing a third embodiment of the air flow measuring device for an internal combustion engine according to the present invention. In this embodiment, the flow rate measuring tube 3 is extended across the air supply passage 1 into the opposite wall (the wall of the bench lily 2) in the embodiments shown in FIGS. 4 and 5, and is fixed at both ends. Efforts are being made to improve mechanical strength. In this case, the air intake port 4 is formed on the upstream side wall surface of the flow rate measuring tube, and the air outlet 10 is formed on the side surface substantially parallel to the air flow in the air supply passage 1. As shown in the figure, the air intake port and air outlet are formed approximately in the center of the air supply passage. In this case as well, total pressure (dynamic pressure + static pressure) acts on the air intake port 4,
Only static pressure acts on the air outlet 10.

また、測定管3の空取入口4および空気出口1
0の左側部分、すなわち抵抗体6,7の反対側の
空間はサージタンクとしての役目もすることがで
きる。
In addition, the air intake port 4 and the air outlet 1 of the measuring tube 3
The left side of 0, that is, the space opposite the resistors 6 and 7, can also serve as a surge tank.

第6図および第7図の実施例のその他の構造は
第4図および第5図に示した実施例と実質上同じ
であり、対応部分はそれぞれ同一符号で示されて
いる。
The rest of the structure of the embodiment of FIGS. 6 and 7 is substantially the same as the embodiment shown in FIGS. 4 and 5, and corresponding parts are designated by the same reference numerals.

第8図および第9図は本発明の内燃機関の空気
流量測定装置の第四実施例を示す図である。この
実施例は第6図および第7図に示した実施例と
は、空気出口10を流速測定管3の下流側(第8
図中下側)の側面に形成した点で相違しており、
その他の構成は実質上同じである。この実施例に
よれば、空気出口10の逆流時の動圧が加わるよ
うにされており、このため、空気流の逆流分をさ
し引いた出力を得ることができる。すなわち、逆
流発生時にはこの逆流の影響をとり入れて流速測
定用抵抗体6による流量(正流方向)測定値を現
実の流量値に理想的に近づけることができる。
FIGS. 8 and 9 are diagrams showing a fourth embodiment of the air flow measuring device for an internal combustion engine according to the present invention. This embodiment differs from the embodiments shown in FIGS. 6 and 7 in that the air outlet 10 is located on the downstream side (the
The difference is that it is formed on the side (lower side in the figure).
The other configurations are substantially the same. According to this embodiment, dynamic pressure is applied when the air flows backward through the air outlet 10, so that an output obtained by subtracting the backward flow of the air flow can be obtained. That is, when a backflow occurs, the influence of this backflow can be taken into account to ideally bring the flow rate (forward flow direction) measured value by the flow rate measuring resistor 6 closer to the actual flow rate value.

第8図および第9図の実施例に対して、第2図
ないし第7図に示した実施例では、空気出口10
には静圧のみを作用させたので逆流発生時にはそ
の影響を阻止し(逆流値を全て零にする)逆流に
よる測定誤差を防止するという効果があつたが、
第8図および第9図の第四実施例では積極的に逆
流の影響をとり入れて正流から逆流分だけさし引
いて理想的に真実の流量を測定しようとするもの
である。
In contrast to the embodiments of FIGS. 8 and 9, in the embodiments shown in FIGS. 2 to 7, the air outlet 10
Since only static pressure was applied to the sensor, it had the effect of blocking the influence of backflow when it occurs (setting all backflow values to zero) and preventing measurement errors due to backflow.
In the fourth embodiment shown in FIGS. 8 and 9, the influence of backflow is actively taken into account and the backflow is subtracted from the normal flow to ideally measure the true flow rate.

上記の「正流から逆流分だけさし引」の意味を
述べよう。第8図において、仕切壁22に添つて
設けられた空気通路5は十分な長さがあり、合せ
てサージタンク室11が併設されているから、通
路内の空気の慣性も十分大きくなつている。従つ
て、空気出口10にパルス状の逆流が侵入しても
通路内の粘性抵抗と、サージタンク室11による
圧力波の吸収作用によつて、伝達おくれを生じ、
流速測定用抵抗体6部分においては正流を零にす
る迄にならない。換言すれば、正流から逆流を差
引いた成分が残るようになつている。
Let's explain the meaning of "subtracting the reverse flow from the forward flow" above. In Fig. 8, the air passage 5 provided along the partition wall 22 has a sufficient length, and the surge tank chamber 11 is also attached, so that the inertia of the air within the passage is sufficiently large. . Therefore, even if a pulsed backflow enters the air outlet 10, a transmission delay occurs due to the viscous resistance in the passage and the pressure wave absorption effect by the surge tank chamber 11.
In the flow velocity measuring resistor 6 portion, the forward flow cannot be reduced to zero. In other words, a component obtained by subtracting the reverse flow from the forward flow remains.

従つて、空気取入口4と、空気出口10との間
隔が極めて短くしたことから逆流の静圧の差が僅
少となり、上記逆流の静圧の差による空気通路5
内の逆流がほとんど無くなる。
Therefore, since the distance between the air intake port 4 and the air outlet 10 is extremely short, the difference in the static pressure of the backflow becomes very small, and the air passage 5 due to the difference in the static pressure of the backflow becomes small.
Internal backflow is almost eliminated.

流速測定用抵抗体6は、正流と逆流の判別が出
来ない検出端であるから、逆流が侵入したときに
正流が増大した如く検出するので、換言すれば逆
流=誤差なのである。従つて、誤差原因である上
記逆流が上記検出端に達しないように構成された
のが本願発明である。
The flow rate measuring resistor 6 is a detection end that cannot distinguish between forward flow and reverse flow, so when reverse flow enters, it detects as if the forward flow has increased. In other words, reverse flow = error. Therefore, the present invention is configured such that the backflow, which is the cause of the error, does not reach the detection end.

そして逆流が吸収作用によつて小さくなつたこ
と、上記空気通路5などの空気の慣性を増大させ
たことと相俟つて精度の良い内燃機関の空気流量
測定装置が出来たのである。
Together with the fact that the backflow is reduced by the absorption effect and the inertia of the air in the air passage 5 is increased, an accurate air flow measuring device for an internal combustion engine has been created.

第10図は以上説明した各種実施例の流速測定
管3の断面形状を例示する図である。第10図A
は縦長の長方形断面の測定管を使用しその上下に
ほぼ正方形断面の空気通路5を形成する場合を示
し、第10図Bは円形チユーブを使用しこれを仕
切壁22で上下の半円形断面の空気通路5に仕切
つた例であり、第10図Cは流線形断面の測定管
3を使用して給気通路1内の流れのみだれの防止
を図つたものである。
FIG. 10 is a diagram illustrating the cross-sectional shape of the flow rate measuring tube 3 of the various embodiments described above. Figure 10A
10B shows a case in which a vertically long measuring tube with a rectangular cross section is used and air passages 5 with a substantially square cross section are formed above and below it, and FIG. This is an example in which the air passage 5 is partitioned, and FIG. 10C shows an example in which a measuring tube 3 having a streamlined cross section is used to prevent the flow inside the air supply passage 1 from becoming sloppy.

以上の説明から明らかなごとく、逆流への測定
誤差を防止することができ、もつて精度の高い流
量測定を行ない得る内燃機関の空気流量測定装置
が得られる。
As is clear from the above description, it is possible to obtain an air flow measuring device for an internal combustion engine that can prevent measurement errors due to backflow and can perform highly accurate flow measurement.

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

第1図は本発明の内燃機関の空気流量測定装置
の作動原理を示す説明図、第2図は本発明の内燃
機関の空気流量測定装置の第一実施例を示す縦断
面図、第3図は第2図中線−から見た端面
図、第4図は本発明の内燃機関の空気流量測定装
置の第二実施例の要部を示す縦断面図、第5図は
第4図中の線−に沿つて見た端面図、第6図
は本発明の内燃機関の空気流量測定装置の第三実
施例の要部を示す縦断面図、第7図は第6図中の
線−に沿つて見た端面図、第8図は本発明の
内燃機関の空気流量測定装置の第四実施例の要部
を示す縦断面図、第9図は第8図中の線−に
沿つて見た端面図、第10図はバイパス路を構成
する流速測定管の断面形状の3つの例を示す断面
図、 1…給気通路、2…ベンチユリー、3…流速測
定管、4…空気取入口、5…空気通路、6…流速
測定用抵抗体、7…温度補償用抵抗体、10…空
気出口、11…サージタンク室、22…仕切壁、
23…整流格子。
FIG. 1 is an explanatory diagram showing the operating principle of the air flow measuring device for an internal combustion engine according to the present invention, FIG. 2 is a longitudinal sectional view showing a first embodiment of the air flow measuring device for an internal combustion engine according to the present invention, and FIG. 2 is an end view taken from the middle line - in FIG. 2, FIG. 4 is a longitudinal cross-sectional view showing the main part of the second embodiment of the air flow measuring device for an internal combustion engine of the present invention, and FIG. 6 is a longitudinal cross-sectional view showing the main part of the third embodiment of the air flow measuring device for an internal combustion engine of the present invention, and FIG. 7 is an end view taken along the line - in FIG. 6. 8 is a longitudinal cross-sectional view showing the main part of the fourth embodiment of the air flow measuring device for an internal combustion engine of the present invention, and FIG. 9 is an end view taken along the line - in FIG. 8. FIG. 10 is a sectional view showing three examples of the cross-sectional shape of the flow rate measuring tube constituting the bypass passage, 1...Air supply passage, 2...Venture, 3...Flow rate measuring tube, 4...Air intake port, 5... Air passage, 6... Resistor for flow rate measurement, 7... Resistor for temperature compensation, 10... Air outlet, 11... Surge tank chamber, 22... Partition wall,
23... Rectifier grid.

Claims (1)

【特許請求の範囲】 1 内燃機関の給気通路を通る吸入空気量を測定
する空気流量測定装置において、前記給気通路を
横切る方向に突出するよう流速測定管を設け、こ
の管の上流側に空気取入口を、下流側に空気出口
を設け、前記流速測定管内の長さ方向に延在する
仕切壁により前記空気取入口から前記空気出口へ
通じる空気通路を形成し、該空気通路内に設置さ
れた流速測定用抵抗体を有する熱線式流量計を設
けることを特徴とする内燃機関の空気流量測定装
置。 2 特許請求の範囲第1項記載の空気流量測定装
置において、前記空気通路内の前記流速測定用抵
抗体の上流側に整流格子を設けることを特徴とす
る内燃機関の空気流量測定装置。 3 特許請求の範囲第1項または第2項記載の空
気流量測定装置において、前記空気通路の途中に
サージタンク室を設けて該空気通路内の空気の慣
性を大きくすることを特徴とする内燃機関の空気
流量測定装置。
[Scope of Claims] 1. In an air flow measuring device for measuring the amount of intake air passing through an air supply passage of an internal combustion engine, a flow rate measuring tube is provided so as to protrude in a direction across the air supply passage, and a flow rate measuring tube is provided on the upstream side of this tube. An air intake port is provided on the downstream side, an air outlet is provided on the downstream side, an air passage is formed from the air intake port to the air outlet by a partition wall extending in the length direction within the flow rate measuring tube, and the air passage is installed within the air passage. 1. An air flow rate measuring device for an internal combustion engine, comprising a hot wire flowmeter having a resistor for measuring flow rate. 2. The air flow rate measuring device for an internal combustion engine according to claim 1, wherein a rectifying grid is provided upstream of the flow rate measuring resistor in the air passage. 3. The air flow rate measuring device according to claim 1 or 2, wherein an internal combustion engine is characterized in that a surge tank chamber is provided in the middle of the air passage to increase the inertia of the air in the air passage. air flow measuring device.
JP55139803A 1980-10-08 1980-10-08 Measuring equipment for air flow rate of internal combustion engine Granted JPS5764109A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55139803A JPS5764109A (en) 1980-10-08 1980-10-08 Measuring equipment for air flow rate of internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55139803A JPS5764109A (en) 1980-10-08 1980-10-08 Measuring equipment for air flow rate of internal combustion engine

Publications (2)

Publication Number Publication Date
JPS5764109A JPS5764109A (en) 1982-04-19
JPH0241688B2 true JPH0241688B2 (en) 1990-09-19

Family

ID=15253792

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55139803A Granted JPS5764109A (en) 1980-10-08 1980-10-08 Measuring equipment for air flow rate of internal combustion engine

Country Status (1)

Country Link
JP (1) JPS5764109A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3130624A1 (en) * 1981-08-01 1983-02-17 Robert Bosch Gmbh, 7000 Stuttgart AIR MEASURING DEVICE
JPH03205514A (en) * 1990-01-08 1991-09-09 Japan Electron Control Syst Co Ltd Air flow rate detector for internal combustion engine

Also Published As

Publication number Publication date
JPS5764109A (en) 1982-04-19

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