JPH0358047B2 - - Google Patents
Info
- Publication number
- JPH0358047B2 JPH0358047B2 JP12634082A JP12634082A JPH0358047B2 JP H0358047 B2 JPH0358047 B2 JP H0358047B2 JP 12634082 A JP12634082 A JP 12634082A JP 12634082 A JP12634082 A JP 12634082A JP H0358047 B2 JPH0358047 B2 JP H0358047B2
- Authority
- JP
- Japan
- Prior art keywords
- flow rate
- air
- air flow
- detection sensor
- circuit
- 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
Links
- 238000001514 detection method Methods 0.000 claims description 44
- 239000000446 fuel Substances 0.000 description 23
- 238000002347 injection Methods 0.000 description 14
- 239000007924 injection Substances 0.000 description 14
- 238000004891 communication Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 4
- 239000000872 buffer Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 230000003321 amplification Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000003199 nucleic acid amplification method Methods 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F15/00—Details of, or accessories for, apparatus of groups G01F1/00 - G01F13/00 insofar as such details or appliances are not adapted to particular types of such apparatus
- G01F15/02—Compensating or correcting for variations in pressure, density or temperature
- G01F15/022—Compensating or correcting for variations in pressure, density or temperature using electrical means
Landscapes
- 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、所定空気通路内の空気流量を検出す
るようにした空気流量検出装置に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an air flow rate detection device for detecting an air flow rate within a predetermined air passage.
従来より、この種の空気流量検出装置として、
例えば、所定空気通路内に通電により加熱される
熱線を配設し、この熱線への加熱電流の供給を該
熱線が空気通路内の流通空気によつて冷却されて
温度低下するのを補償するように増減制御して、
該熱線の温度を常に所定値に維持することによ
り、この加熱電流の増減によつて生じる出力電圧
の増減変化により通路内の流通空気の質量流量を
検出するようにしたものはよく知られている(例
えば特開昭57−35128号公報等参照)。 Conventionally, as this type of air flow rate detection device,
For example, a hot wire that is heated by electricity is arranged in a predetermined air passage, and the heating current is supplied to the hot wire to compensate for the temperature drop as the hot wire is cooled by the circulating air in the air passage. Control the increase/decrease to
It is well known that the temperature of the heating wire is always maintained at a predetermined value, and the mass flow rate of the circulating air in the passage is detected by the increase/decrease change in the output voltage caused by the increase/decrease in the heating current. (For example, see Japanese Patent Application Laid-Open No. 57-35128, etc.).
しかしながら、上記従来のものでは、加熱電流
によつて生じる出力電圧は空気流量の4乗根に比
例するものであり(上記公報の第2図参照)、こ
のため、検出範囲を広げると、空気流量の大きい
範囲では検出精度が悪くなるという欠点があつ
た。 However, in the above-mentioned conventional device, the output voltage generated by the heating current is proportional to the fourth root of the air flow rate (see Figure 2 of the above-mentioned publication). The disadvantage is that detection accuracy deteriorates in a large range.
そこで、従来、空気通路内の流量空気の質量流
量の検出に依るのに代え、流通空気の流速を検出
することにより空気流量を広範囲にわたつて精度
良く検出し得るようにしたものが提案されてい
る。すなわち、このものは、所定空気通路内にカ
ルマン渦発生柱を配設し、この渦発生柱により発
生するカルマン渦の個数(周波数)が通路内の空
気流速に正比例するのを利用し、このカルマン渦
の発生周波数を上記の如き熱線等の熱量変化検出
センサにより熱量変化として計測することにより
空気流速を検出し、その結果として空気流量を検
出するようにしたものである(例えば特開昭50−
148722号公報等参照)。しかしながら、この提案
のものでは、空気流速の検出に依るものであるた
め、空気流速が一定であれば、実際に空気流量が
空気密度の変化により増減変化している場合であ
つても、常に一定の流量として検出してしまうと
いう欠点がある。すなわち、上記カルマン渦の発
生周波数は空気流速には比例するが、空気密度の
変化に対しては変化しないという欠点がある。 Therefore, instead of relying on the conventional method of detecting the mass flow rate of the flow rate air in the air passage, a method has been proposed in which the air flow rate can be detected accurately over a wide range by detecting the flow velocity of the circulating air. There is. That is, in this method, a Karman vortex generation column is arranged in a predetermined air passage, and the number (frequency) of Karman vortices generated by this vortex generation column is directly proportional to the air flow velocity in the passage. The air flow velocity is detected by measuring the generation frequency of the vortex as a change in heat amount using a heat wire sensor such as the one described above, and the air flow rate is detected as a result.
(See Publication No. 148722, etc.) However, this proposal relies on the detection of air flow velocity, so if the air flow velocity is constant, it will always remain constant even if the air flow rate actually increases or decreases due to changes in air density. The disadvantage is that it is detected as a flow rate of . That is, the generation frequency of the Karman vortex is proportional to the air flow velocity, but there is a drawback that it does not change with respect to changes in air density.
本発明は斯かる点に鑑みてなされたもので、上
記提案の構成に加えて、熱線等の熱量変化検出セ
ンサを本来の質量流量センサとして用いること、
すなわち、流通空気の密度変化に応じて該熱量変
化検出センサの出力の振幅値が大小変化すること
を利用し、この振幅値の変化に基いて、計測した
カルマン渦の発生周波数を補正するようにするこ
とにより、所定空気通路内の空気流量を簡単かつ
広範囲にわたつて精度よく検出し得るようにする
ことを目的とするものである。 The present invention has been made in view of these points, and in addition to the above-mentioned proposed configuration, it includes the use of a heat quantity change detection sensor such as a hot wire as the original mass flow sensor.
That is, by utilizing the fact that the amplitude value of the output of the heat quantity change detection sensor changes in magnitude depending on the density change of the circulating air, the generation frequency of the measured Karman vortex is corrected based on the change in the amplitude value. By doing so, it is an object of the present invention to enable the air flow rate in a predetermined air passage to be detected easily and accurately over a wide range.
その目的を達成するため、本発明では、第1図
に示すように、空気通路内に配設されたカルマン
渦発生柱と、該カルマン渦発生柱により発生する
カルマン渦を熱量変化として検出する熱量変化検
出センサと、該熱量変化検出センサの出力の振幅
値に対応して設定された空気密度の補正値を予め
記憶したメモリと、上記熱量変化検出センサの出
力を受け、該出力の周波数と上記メモリから読み
出した該出力の振幅値に対応する補正値とに基い
て空気流量信号を演算出力する演算回路とからな
り、熱量変化検出センサにより計測したカルマン
渦発生周波数と、該熱量変化検出センサの出力の
振幅値に応じてメモリから読み出した空気密度の
補正値とに基いて、演算回路から空気流量に対応
した空気流量信号を出力するようにしたものであ
る。 In order to achieve this purpose, the present invention uses a Karman vortex generation column disposed in an air passage, and a heat amount that detects the Karman vortex generated by the Karman vortex generation column as a change in heat amount, as shown in FIG. a change detection sensor; a memory storing in advance an air density correction value set corresponding to the amplitude value of the output of the heat amount change detection sensor; It consists of a calculation circuit that calculates and outputs an air flow signal based on a correction value corresponding to the amplitude value of the output read from the memory, and calculates and outputs an air flow signal based on the Karman vortex generation frequency measured by the heat amount change detection sensor and the correction value of the heat amount change detection sensor. Based on the air density correction value read from the memory in accordance with the amplitude value of the output, an air flow rate signal corresponding to the air flow rate is output from the arithmetic circuit.
以下、本発明の実施例を図面に基いて詳細に説
明する。 Embodiments of the present invention will be described in detail below with reference to the drawings.
第2図は、エンジンの燃料噴射式燃料供給装置
を制御するための空気流量の検出に本発明を適用
した場合の実施例を示し、1はエンジン、2はシ
リンダ1a内に摺動自在に配設されたピストン、
3はシリンダ1aに吸気ポート4を介して連通す
る吸気通路、5は吸気ポート4に配設された吸気
弁、6は吸気通路3に配設されシリンダ1a内へ
の空気流量を制御するスロツトル弁、7は吸気通
路3のスロツトル弁6下流に配設された燃料噴射
弁、8はエアクリーナである。 FIG. 2 shows an embodiment in which the present invention is applied to the detection of air flow rate for controlling a fuel injection type fuel supply device of an engine, in which 1 is an engine, and 2 is slidably arranged in a cylinder 1a. installed piston,
3 is an intake passage communicating with the cylinder 1a via the intake port 4; 5 is an intake valve disposed in the intake port 4; and 6 is a throttle valve disposed in the intake passage 3 to control the air flow into the cylinder 1a. , 7 is a fuel injection valve disposed downstream of the throttle valve 6 in the intake passage 3, and 8 is an air cleaner.
また、9は上記吸気通路3のスロツトル弁6上
流に配設されたカルマン渦発生柱であつて、該渦
発生柱9は、第3図に示すように、空気流通方向
(矢印方向)に対して該渦発生柱9下流の上下端
にカルマン渦10,10…を上下交互に規則正し
く2列に発生させるものである。そして、該渦発
生柱9内には空所13が設けられ、該空所11は
渦発生柱9の上下端を連通する連通路12によつ
て吸気通路3と連通しているとともに、該空所1
1内には、所定電流値の加熱電流により常時加熱
されるサーミスタよりなる熱量変化検出センサ1
3が配設されている。よつて、渦発生柱9の上下
端にカルマン渦10,10…が交互に発生する
と、それに伴つて渦発生柱9の上下端に圧力変動
が生じ、これにより吸気通路3の流通空気を連通
路12内を上方から下方に又は下方から上方に向
かつて交互に流通させることにより、熱量変化検
出センサ13を冷却して各カルマン渦10,10
…を熱量変化として検出し、その結果、該検出セ
ンサ13の端子電圧(出力電圧)を第6図実線で
示す如くカルマン渦10,10…の発生周波数で
もつて周期的に変化せしめるように構成されてい
る。そして、上記熱量変化検出センサ13は燃料
噴射制御回路14に接続されている。 Reference numeral 9 denotes a Karman vortex generating column disposed upstream of the throttle valve 6 in the intake passage 3, and as shown in FIG. Karman vortices 10, 10, . . . are generated in two regular rows at the upper and lower ends of the vortex generating column 9, alternating up and down. A cavity 13 is provided in the vortex generating column 9, and the cavity 11 communicates with the intake passage 3 through a communication passage 12 that communicates the upper and lower ends of the vortex generating column 9. Place 1
1 includes a heat amount change detection sensor 1 consisting of a thermistor that is constantly heated by a heating current of a predetermined current value.
3 are arranged. Therefore, when the Karman vortices 10, 10, etc. are generated alternately at the upper and lower ends of the vortex generating column 9, pressure fluctuations occur at the upper and lower ends of the vortex generating column 9, and this causes the circulating air in the intake passage 3 to flow through the communication path. 12 from the top to the bottom or from the bottom to the top, the heat quantity change detection sensor 13 is cooled and each Karman vortex 10, 10 is cooled.
... is detected as a change in heat quantity, and as a result, the terminal voltage (output voltage) of the detection sensor 13 is periodically changed at the generation frequency of the Karman vortices 10, 10, as shown by the solid line in FIG. ing. The heat amount change detection sensor 13 is connected to a fuel injection control circuit 14.
上記燃料噴射制御回路14は、上記熱量変化検
出センサ13からの出力信号をパルス波に波形整
形する波形整形回路15と、該整形回路15のパ
ルス波の周波数と同数の定パルス幅信号よりなる
制御パルスを発生する定パルス幅信号発生回路1
6と、上記熱量変化検出センサ13の出力信号の
振幅値に応じた大きさの電圧信号を発生する振幅
検出回路17と、該検出回路17の電圧信号、す
なわち熱量変化検出センサ13の出力の振幅値に
対応して設定された第4図に示すような空気密度
の補正値(補正係数)を予め記憶したメモリ18
と、上記定パルス幅信号発生回路16の制御パル
スに含む定パルス幅信号の数に、上記振幅検出回
路17の電圧信号に基いて読み出されたメモリ1
8内の補正値を乗算して、補正された数の定パル
ス幅信号よりなる制御パルス(空気流量信号)を
出力する演算回路19と、該演算回路19の空気
流量信号を増幅する増幅回路20とから成り、該
増幅回路20で増幅された空気流量信号を燃料噴
射弁7に出力することにより、該燃料噴射弁7か
ら空気流量信号値に応じた燃料を噴射するように
している。 The fuel injection control circuit 14 includes a waveform shaping circuit 15 that shapes the output signal from the heat quantity change detection sensor 13 into a pulse wave, and a constant pulse width signal of the same number as the frequency of the pulse wave of the shaping circuit 15. Constant pulse width signal generation circuit 1 that generates pulses
6, an amplitude detection circuit 17 that generates a voltage signal having a magnitude corresponding to the amplitude value of the output signal of the heat quantity change detection sensor 13, and an amplitude detection circuit 17 that generates a voltage signal of a magnitude corresponding to the amplitude value of the output signal of the heat quantity change detection sensor 13; A memory 18 that stores in advance air density correction values (correction coefficients) as shown in FIG. 4, which are set corresponding to the values.
and the number of constant pulse width signals included in the control pulse of the constant pulse width signal generation circuit 16 is added to the memory 1 read out based on the voltage signal of the amplitude detection circuit 17.
an arithmetic circuit 19 that outputs a control pulse (air flow rate signal) consisting of the corrected number of constant pulse width signals by multiplying the correction value in 8; and an amplification circuit 20 that amplifies the air flow signal of the arithmetic circuit 19. By outputting the air flow signal amplified by the amplification circuit 20 to the fuel injection valve 7, fuel corresponding to the air flow signal value is injected from the fuel injection valve 7.
次に、上記実施例の作動について説明するに、
吸気通路3内に所定流量の空気が流通すると、カ
ルマン渦発生柱9の上下端には、吸気流量が正比
例した数のカルマン渦10,10…が発生して交
互に規則正しく2列に並ぶ。このため、該渦発生
柱9の上下端に圧力変動が生じて、吸気通路3内
の流通空気が該渦発生柱9の連通路12内を上方
から下方に又は下方から上方に向かつて交互に流
れ、熱量変化検出センサ13はこの流通空気によ
つて周期的に冷却されて、その出力信号が第6図
に実線で示す如くカルマン渦10,10の発生周
波数でもつて周期的に変化する。この出力信号は
燃料噴射制御回路14の波形整形回路15で同一
周波数のパルス波に波形整形されたのち、定パル
ス幅信号発生回路16で上記パルス波の周波数と
同数の定パルス幅信号よりなる制御パルスに変換
される。 Next, to explain the operation of the above embodiment,
When a predetermined flow rate of air flows through the intake passage 3, Karman vortices 10, 10, . For this reason, pressure fluctuations occur at the upper and lower ends of the vortex generating column 9, and the circulating air in the intake passage 3 alternately moves from the top to the bottom or from the bottom to the top in the communication passage 12 of the vortex generation column 9. The flow and heat quantity change detection sensor 13 is periodically cooled by this circulating air, and its output signal changes periodically with the generation frequency of the Karman vortices 10, 10, as shown by the solid line in FIG. This output signal is waveform-shaped into a pulse wave of the same frequency by the waveform shaping circuit 15 of the fuel injection control circuit 14, and then controlled by the constant pulse width signal generation circuit 16 using constant pulse width signals of the same number as the frequency of the pulse wave. converted into pulses.
それと同時に、上記熱量変化検出センサ13の
出力信号は振幅検出回路17に出力され、該検出
回路17で振幅値に応じた大きさの電圧信号に変
換され、この電圧信号に応じた空気密度の補正値
がメモリ18から読み出されて演算回路19に出
力される。そして、演算回路19では、上記定パ
ルス幅信号発生回路16の制御パルスを構成する
定パルス幅信号の数に上記メモリ18からの空気
密度の補正値を乗算することが行なわれて、空気
流量信号が出力される。この空気流量信号は増幅
回路20で増幅されたのち燃料噴射弁7に出力さ
れ、その結果、吸気通路3の吸気流量に応じた燃
料が該燃料噴射弁7から燃料されることになる。 At the same time, the output signal of the heat quantity change detection sensor 13 is output to the amplitude detection circuit 17, where it is converted into a voltage signal of a magnitude corresponding to the amplitude value, and the air density is corrected according to this voltage signal. The value is read from memory 18 and output to arithmetic circuit 19 . Then, in the arithmetic circuit 19, the number of constant pulse width signals constituting the control pulse of the constant pulse width signal generation circuit 16 is multiplied by the air density correction value from the memory 18, and the air flow rate signal is is output. This air flow rate signal is amplified by the amplifier circuit 20 and then output to the fuel injection valve 7, and as a result, fuel corresponding to the intake flow rate of the intake passage 3 is injected from the fuel injection valve 7.
そして、この状態で吸気通路3の流通空気の流
速が一定のまま、例えば吸気温度が低下して空気
密度が高くなると、それに伴い熱量変化検出セン
サ13の冷却効率が高くなり、その出力信号は第
6図破線で示す如く周波数は変化せず振幅値のみ
が大きくなる。このことにより、振幅検出回路1
7の電圧信号値は大きくなり、それに対応してメ
モリ18から読み出される空気密度の補正値も大
きくなり、演算回路19はこの補正値に基いて上
記空気密度の上昇分に応じて大きくなつた空気流
量信号を出力する。その結果、空気密度の上昇に
応じて増量された燃料が燃料噴射弁7から噴射さ
れることになる。よつて、流通空気の流速が一定
であつても、空気密度の変化により空気流量が変
化すれば、この空気流量に対応した適量の燃料を
燃料噴射弁7から噴射することができる。しか
も、熱量変化検出センサ13はカルマン渦発生柱
9の空所11内に配設され、連通路12を介して
吸気通路3と連通しているので、この連通路12
の径を適宜に小さく選定すれば、熱量変化検出セ
ンサ13の質量流量センサとしての質量流量の検
出を精度の良好な範囲内で行うことができ、吸気
通路3の空気流量の補正を正確に行うことができ
る。 In this state, when the flow velocity of the circulating air in the intake passage 3 remains constant, for example, when the intake air temperature decreases and the air density increases, the cooling efficiency of the heat amount change detection sensor 13 increases accordingly, and the output signal is As shown by the broken line in Figure 6, the frequency does not change and only the amplitude value increases. As a result, the amplitude detection circuit 1
The voltage signal value of 7 increases, and the air density correction value read out from the memory 18 also increases accordingly. Based on this correction value, the arithmetic circuit 19 calculates the amount of air that has increased in accordance with the increase in air density. Outputs flow rate signal. As a result, an increased amount of fuel is injected from the fuel injection valve 7 in accordance with the increase in air density. Therefore, even if the flow velocity of the circulating air is constant, if the air flow rate changes due to a change in air density, an appropriate amount of fuel corresponding to this air flow rate can be injected from the fuel injection valve 7. Moreover, since the heat quantity change detection sensor 13 is disposed in the space 11 of the Karman vortex generation column 9 and communicates with the intake passage 3 via the communication passage 12, the communication passage 12
By appropriately selecting a small diameter, the mass flow rate can be detected by the heat quantity change detection sensor 13 as a mass flow rate sensor within a range of accuracy, and the air flow rate in the intake passage 3 can be corrected accurately. be able to.
次に、上記振幅検出回路17の具体的回路を第
5図に示す。 Next, a concrete circuit of the amplitude detection circuit 17 is shown in FIG.
このものは、熱量変化検出センサ13の出力信
号を受けて緩衝するバツフア回路17aと、該バ
ツフア回路17aの出力を両波整流する整流回路
17bと、該整流回路17bの出力を積分する積
分回路17cとからなり、よつて熱量変化検出セ
ンサ13の出力の振幅値に応じた大きさの電圧信
号を得るようにしたものである。 This circuit includes a buffer circuit 17a that receives and buffers the output signal of the heat quantity change detection sensor 13, a rectifier circuit 17b that double-wave rectifies the output of the buffer circuit 17a, and an integration circuit 17c that integrates the output of the rectifier circuit 17b. Therefore, a voltage signal having a magnitude corresponding to the amplitude value of the output of the heat quantity change detection sensor 13 is obtained.
尚、上記実施例では、熱量変化検出センサ13
をカルマン渦発生柱9の空所11に配設してカル
マン渦の発生周波数を計測するようにしたが、そ
の他この熱量変化検出センサ13をカルマン渦発
生柱9の後位に配設してカルマン渦の発生周波数
を計測するようにしてもよいのは勿論である。し
かし、上記実施例の方が、空気流量の補正をより
正確に行い得る点で好ましい。 In the above embodiment, the heat amount change detection sensor 13
is placed in the space 11 of the Karman vortex generating column 9 to measure the generation frequency of the Karman vortex. Of course, it is also possible to measure the frequency at which the vortices occur. However, the above embodiment is preferable in that the air flow rate can be corrected more accurately.
また、上記実施例では、燃料噴射式燃料供給装
置を制御するための空気流量の検出に本発明を適
用した場合について説明したが、本発明はこれに
限定されず、その他、所定通路内の空気流量を検
出しながら所定動作を行うようにしたものに対し
ても同様に適用することができるのは勿論であ
る。この場合、熱量変化検出センサ13の出力の
周波数を一旦アナログ値に変換するようにしたも
のにあつては、変換前の出力の周波数および変換
後のアナログ値の何れか一方をメモリ18の補正
値により補正するようにすればよい。 Further, in the above embodiment, a case has been described in which the present invention is applied to detecting the air flow rate for controlling a fuel injection type fuel supply device, but the present invention is not limited to this. Of course, the present invention can also be similarly applied to devices in which a predetermined operation is performed while detecting the flow rate. In this case, if the frequency of the output of the heat quantity change detection sensor 13 is once converted into an analog value, either the frequency of the output before conversion or the analog value after conversion is used as the correction value in the memory 18. It may be corrected by
以上説明したように、本発明の空気流量検出装
置によれば、吸気通路に配設したカルマン渦発生
柱により生じるカルマン渦の発生周波数を、熱量
変化検出センサの出力に基いて計測するととも
に、このカルマン渦の発生周波数と、上記熱量変
化検出センサの出口の振幅値に対応した空気密度
の補正値とに基いて空気流量信号を出力するよう
にしたので、所定空気通路内の空気流量を流速お
よび質量流量の両面で簡単かつ広範囲にわたつて
精度良く検出することができ、例えば燃料噴射式
燃料供給装置において空気流量に応じた適量の燃
料を噴射させることができる等、実用上各種装置
における空気流量検出に好適なものである。 As explained above, according to the air flow rate detection device of the present invention, the generation frequency of the Karman vortex generated by the Karman vortex generation column disposed in the intake passage is measured based on the output of the heat amount change detection sensor, and Since the air flow rate signal is output based on the generation frequency of the Karman vortex and the air density correction value corresponding to the amplitude value of the exit of the heat quantity change detection sensor, the air flow rate in a given air passage can be determined by the flow velocity and the air density correction value. It is possible to easily and accurately detect both the mass flow rate and the air flow rate in various devices, for example, to inject the appropriate amount of fuel according to the air flow rate in a fuel injection type fuel supply device. It is suitable for detection.
第1図は本発明の構成を示す図、第2図ないし
第6図は本発明の実施例を示し、第2図は燃料噴
射式燃料供給装置における空気流量の検出に本発
明を適用した場合の全体概略構成図、第3図はカ
ルマン渦発生柱の縦断面図、第4図はメモリの記
憶内容を示す図、第5図は振幅検出回路の具体的
回路を示す電気回路図、第6図は熱量変化検出セ
ンサの出力波形図である。
3……吸気通路(空気通路)、9……カルマン
渦発生柱、13……熱量変化検出センサ、18…
…メモリ、19……演算回路。
Fig. 1 shows the configuration of the present invention, Figs. 2 to 6 show embodiments of the present invention, and Fig. 2 shows the case where the present invention is applied to detecting the air flow rate in a fuel injection type fuel supply device. 3 is a vertical cross-sectional view of the Karman vortex generation column, FIG. 4 is a diagram showing the contents of memory, FIG. 5 is an electric circuit diagram showing a specific circuit of the amplitude detection circuit, and FIG. The figure is an output waveform diagram of the heat amount change detection sensor. 3... Intake passage (air passage), 9... Karman vortex generation column, 13... Calorific value change detection sensor, 18...
...Memory, 19...Arithmetic circuit.
Claims (1)
と、該カルマン渦発生柱により発生するカルマン
渦を熱量変化として検出する熱量変化検出センサ
と、該熱量変化検出センサの出力の振幅値に対応
して設定された空気密度の補正値を予め記憶した
メモリと、上記熱量変化検出センサの出力を受
け、該出力の周波数と上記メモリから読み出した
該出力の振幅値に対応する補正値とに基いて空気
流量信号を演算出力する演算回路とからなること
を特徴とする空気流量検出装置。1. A Karman vortex generation column disposed in the air passage, a heat quantity change detection sensor that detects the Karman vortex generated by the Karman vortex generation column as a heat quantity change, and a heat quantity change detection sensor that corresponds to the amplitude value of the output of the heat quantity change detection sensor. Based on a memory that stores in advance a correction value for the air density set by An air flow rate detection device comprising a calculation circuit that calculates and outputs an air flow rate signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12634082A JPS5915816A (en) | 1982-07-19 | 1982-07-19 | Detecting device for flow rate of air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12634082A JPS5915816A (en) | 1982-07-19 | 1982-07-19 | Detecting device for flow rate of air |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5915816A JPS5915816A (en) | 1984-01-26 |
| JPH0358047B2 true JPH0358047B2 (en) | 1991-09-04 |
Family
ID=14932744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12634082A Granted JPS5915816A (en) | 1982-07-19 | 1982-07-19 | Detecting device for flow rate of air |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5915816A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6153517A (en) * | 1984-08-24 | 1986-03-17 | Oval Eng Co Ltd | Flow speed or flow amount meter |
-
1982
- 1982-07-19 JP JP12634082A patent/JPS5915816A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5915816A (en) | 1984-01-26 |
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