JPS614860A - Injection-rate meter - Google Patents
Injection-rate meterInfo
- Publication number
- JPS614860A JPS614860A JP12295784A JP12295784A JPS614860A JP S614860 A JPS614860 A JP S614860A JP 12295784 A JP12295784 A JP 12295784A JP 12295784 A JP12295784 A JP 12295784A JP S614860 A JPS614860 A JP S614860A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- pressure
- solenoid valve
- injection
- capacity chamber
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M65/00—Testing fuel-injection apparatus, e.g. testing injection timing ; Cleaning of fuel-injection apparatus
- F02M65/001—Measuring fuel delivery of a fuel injector
Abstract
Description
【発明の詳細な説明】 本発明は噴射率計に関する。[Detailed description of the invention] The present invention relates to an injection rate meter.
第1図に従来の噴射率測定装置の構造を示す。FIG. 1 shows the structure of a conventional injection rate measuring device.
図において、01は噴射率針本体、02は取付金物、0
3はノズルホルダ、04は測定管、05は圧力計測用ヒ
ズミヶゞ−ジであシ22図示ないアンプによシ圧力値が
計測される。o6は針弁、07は放出管である。測定管
o4はノズルからの噴射が続く期間中にその圧力波が返
ってこないように十分に長く設定されている。In the figure, 01 is the injection rate needle body, 02 is the mounting hardware, 0
3 is a nozzle holder, 04 is a measuring tube, and 05 is a pressure measuring strain gauge. 22 The pressure value is measured by an amplifier (not shown). o6 is a needle valve, and 07 is a discharge pipe. The measuring tube o4 is set long enough so that its pressure wave does not return during the duration of the injection from the nozzle.
液体を満たした一様断面の管内に液体を注入すると、そ
の注入量に応じて圧力上昇が起こる。即ち。When a liquid is injected into a liquid-filled tube with a uniform cross-section, a pressure increase occurs depending on the amount injected. That is.
Δp=ρaV 、 ? == q/A・”・Δp−ρ
a−q/A即ち、Δ、ア。Δp=ρaV, ? == q/A・”・Δp−ρ
a-q/A, that is, Δ, a.
ここに、Δp:圧力上昇 k19/cm2ρ:液体の密
度 kg/an4・2
a:液体中の音速 〜優
V二液体中の流速 卿優
q:流量 (Yn3/5ee
A:管断面積 crn2
の原理を応用したものである。Here, Δp: Pressure rise k19/cm2ρ: Liquid density kg/an4・2 a: Sound velocity in liquid ~YuV2 Flow velocity in liquid q: Flow rate (Yn3/5ee A: Principle of pipe cross-sectional area crn2 This is an application of
噴射率の計測につき説明すると2図示しない噴射ポンプ
から噴射管を通してノズルo3の先端噴孔部から高圧で
噴射される。このとき測定管04内には燃料が充満して
お9.噴射される流量に応じて流速の変化が起きる。こ
の流速の変化は即ち管内の圧力変化として現われる。こ
れを圧力計測用ヒズミケ゛−ジで検出することによシ噴
射時の開側の噴射率が計測される。To explain the measurement of the injection rate, ink is injected at high pressure from the tip of the nozzle o3 through the injection pipe from an injection pump (not shown). At this time, the measuring tube 04 is filled with fuel.9. Changes in flow velocity occur depending on the injected flow rate. This change in flow rate appears as a change in pressure within the pipe. By detecting this with a pressure measuring strain cage, the injection rate on the open side during injection can be measured.
ここで針弁06の作用としては噴射量と同量を放出管0
7から放出させるだめのもので、絞りすぎると放出量が
少なくなシ、測定管04の圧力が上がシ過ぎると同時に
正確な噴射率とならない。Here, the action of the needle valve 06 is to send the same amount as the injection amount to the discharge pipe 0.
7, and if it is narrowed too much, the amount of discharge will be small, and if the pressure in the measuring tube 04 is too high, the injection rate will not be accurate.
また、絞シを拡きすぎると放出量が多くなシ測定管04
内に空洞を生じ、これも正確な噴射率とならない。In addition, if the diaphragm is expanded too much, the amount of emission will be large.Measurement tube 04
This creates a cavity within the cylinder, which also prevents the injection rate from being accurate.
上記のものは正確な噴射率を測るには針弁の絞りを適正
にする必要があり、この調節にはかなシの熟練を要する
。また、ノズル取付部及び測定管は断面変化がなく正確
に一様なものでなくてはならず非常に高価なものであシ
、その取付、取扱にも非常に面倒である。In order to accurately measure the injection rate with the above, it is necessary to adjust the throttle of the needle valve appropriately, and this adjustment requires a great deal of skill. In addition, the nozzle mounting portion and the measuring tube must be precisely uniform without any change in cross section, and are very expensive, and their installation and handling are also very troublesome.
本発明の目的は上記の点に着目し、取付、取扱が簡単で
、製作費の安い噴射重訂を提供することであシ、その特
徴とするところは、液体を充満させた容器と、同容器内
に液体を噴射する装置と。The purpose of the present invention is to focus on the above-mentioned points, and to provide an injection refill that is easy to install and handle, and is inexpensive to manufacture. A device that injects liquid into a container.
同容器内の圧力を計測する圧力計と、同容器内の液体を
電磁弁で排出する装置と、燃料ポンプカム軸の1回転に
つき1パルスの基準トリガ・ぐルスを発生する装置と、
同装置のトリガパルス信号が入力する上記電磁弁のコン
トローラと、上記圧力計の出力信号と上記トリガパルス
信号とが入力され噴射率を算出するコンピュータとから
なることである。A pressure gauge that measures the pressure inside the container, a device that discharges the liquid in the container using a solenoid valve, and a device that generates a reference trigger pulse of one pulse per revolution of the fuel pump camshaft.
It consists of a controller for the electromagnetic valve to which the trigger pulse signal of the device is input, and a computer to which the output signal of the pressure gauge and the trigger pulse signal are input and calculates the injection rate.
この場合は、従来の一様管内での流速の変化による圧力
上昇から噴射率を求めるのではなく、一様容積中に燃料
を噴射し容積室内の圧力上昇の変化率を求めることによ
シ噴射率の計測を行うようにしている。In this case, instead of determining the injection rate from the pressure rise due to a change in flow velocity in a conventional uniform pipe, the injection rate is determined by injecting fuel into a uniform volume and determining the rate of change in the pressure rise within the volume chamber. We are trying to measure the rate.
本発明は間欠的に吐出される液体の刻々の流量変化を計
測する装置全般に適用できる。The present invention can be applied to any device that measures momentary changes in the flow rate of liquid that is intermittently discharged.
以下図面を参照して本発明による実施例につき説明する
。Embodiments of the present invention will be described below with reference to the drawings.
第2図は本発明による1実施例の噴射率計測装置を示す
説明図である。−
図において、1は本体で、その内部に容積室2がある。FIG. 2 is an explanatory diagram showing an injection rate measuring device according to an embodiment of the present invention. - In the figure, 1 is a main body, inside which is a volume chamber 2.
3は燃料噴射弁、4は電磁弁、5は圧力ピッファツジ、
6は圧力信号アンプである。7は背圧調整弁本体で、8
は弁、9はばねである。3 is a fuel injection valve, 4 is a solenoid valve, 5 is a pressure pipe,
6 is a pressure signal amplifier. 7 is the back pressure regulating valve body, 8
is a valve, and 9 is a spring.
10は図示しない燃料ポンプカム軸回転角と同期するト
リガノクルス発生装置、11は電磁弁4のコントローラ
、12はマイクロコンピュータで。10 is a trigger nozzle generator synchronized with the rotation angle of a fuel pump camshaft (not shown); 11 is a controller for the solenoid valve 4; and 12 is a microcomputer.
その構成要素を第4図に示す。破線内に示したクロック
信号発信器、 A74)変換器、噴射率演算器(dq/
dt)、D//A変換器及び回転角演算器、噴射率演算
器(dq/dθ) 、 D/A変換器からなる。このう
ち、クロック信号発信器、 A/D変換器、噴射率演算
器(dq/dt ) 、 D/A変換器が基本構成で以
下のものも必要に応じてつけ加えるもので図中さらに破
線でかこみ符号120で示した。Its components are shown in FIG. Clock signal generator, A74) converter, injection rate calculator (dq/
dt), a D//A converter, a rotation angle calculator, an injection rate calculator (dq/dθ), and a D/A converter. Of these, the clock signal generator, A/D converter, injection rate calculator (dq/dt), and D/A converter are the basic components, and the following items are added as necessary and are further enclosed by broken lines in the figure. It is indicated by the reference numeral 120.
上記構成の場合の作用について述べる。The operation in the case of the above configuration will be described.
まず、初期状態として容積室2の中には燃料が充満して
おシ、電磁弁4は閉の状態にある。このとき2図示しな
い燃料ポンプの回転によシ燃料が吐出声れると、燃料噴
射弁3から燃料が噴射される。すると、容積室2内の燃
料の圧力は噴射された量に見合って上昇する。これを圧
力ピッファツジ5で検出し、アンゾロで増巾すると第3
図(C)に見られるように噴射と同時に圧力上昇を検知
できる。この出力信号はマイクロコンぎユータ12へ入
力される。また、トリガパルス発生装置10からは1回
転1ノやルスの基準トリガパルスが発生される。このト
リガ信号は電磁弁のコントローラ11及びマイクロコン
ピュータ12へ入力される。First, in the initial state, the volume chamber 2 is filled with fuel and the solenoid valve 4 is in a closed state. At this time, when fuel is discharged due to the rotation of a fuel pump (not shown), fuel is injected from the fuel injection valve 3. Then, the pressure of the fuel within the volume chamber 2 increases in proportion to the injected amount. Detecting this with pressure pizzazzi 5 and amplifying it with Anzoro, the third
As shown in Figure (C), the pressure increase can be detected at the same time as injection. This output signal is input to the microcomputer 12. Further, the trigger pulse generator 10 generates a reference trigger pulse of 1 pulse per revolution. This trigger signal is input to the solenoid valve controller 11 and microcomputer 12.
電磁弁コントローラは基準信号から設定されたΔt1の
時間後に電磁弁4を開き、容積室2内に噴射された燃料
を放出し、さらにΔt2時間時間開じる。電磁弁4が開
くと背圧調整弁7の設定圧力以上で放出が起こり、再度
初期の状態に戻る。The solenoid valve controller opens the solenoid valve 4 after a time of Δt1 set from the reference signal, releases the fuel injected into the volume chamber 2, and further opens the solenoid valve for a time of Δt2. When the solenoid valve 4 opens, discharge occurs when the pressure exceeds the set pressure of the back pressure regulating valve 7, and the initial state is returned again.
第4図によシマイクロコンピュータの作用につき説明す
る。The operation of the microcomputer will be explained with reference to FIG.
増巾器(圧力信号アン7’)6からの圧力信号はコンピ
ュータに設置されたクロック信号発信器の微小時間ごと
に圧力信号がディノタル値化される( A/D変換器)
。この値の遂次変化分を求め(噴射率演算器)、これか
らD/A変換を行いアナログ値として噴射率(ciq、
/at g3/see )が出力される。The pressure signal from the amplifier (pressure signal amplifier 7') 6 is converted into a digital value every minute by a clock signal generator installed in the computer (A/D converter).
. The successive changes in this value are determined (injection rate calculation unit), which is then subjected to D/A conversion and the injection rate (ciq,
/at g3/see) is output.
符号120で示した部分は必要に応じて噴射率(dq/
dθmm’/deg )i出力させるもので、トリガパ
ルス発生装置10の信号からクロック信号を角度に演算
しく回転角演算器)、さきに演算された噴射率dq/d
tをdq/dθに変換しく噴射率演算器dq/dθ)。The part indicated by reference numeral 120 indicates the injection rate (dq/
dθ mm'/deg
The injection rate calculator converts t into dq/dθ).
恥変換して出力される。It is shamefully converted and output.
上述の場合には次の効果がある。The above case has the following effects.
以上のように燃料の放出、閉止は電磁弁によシ行われる
ので2面倒な針弁の絞シを調整する必要が々く、取扱が
非常に簡単になる。また高精度の部品も少なく製作も安
価である。As described above, since fuel is discharged and closed by the electromagnetic valve, there is no need to adjust the needle valve's throttle, which is a tedious task, and the handling becomes very simple. It also has fewer high-precision parts and is inexpensive to manufacture.
さらに、マイクロコンピュータで即時に噴射率が出力さ
れるので、噴射現象の解明に有効である。Furthermore, since the injection rate is immediately output by the microcomputer, it is effective in elucidating injection phenomena.
第1図は従来の噴射率針を示す説明図、第2図は本発明
による1実施例の噴射率計測装置を示す説明図、第3図
は第2図の装置の作動時のトリが信号、クロック信号、
容積室圧力、噴射率、針弁リフト、噴圧圧力を示す線図
、第4図はマイクロコンピュータの構成2作用を示す説
明図である。
2・・・容積室、3・・・燃料噴射弁、4・・・電磁弁
、5・・・圧力ビックアップ、10・・・トリガパルス
発生装置、11・・・電磁弁コントローラ、12・・・
マイクロコンピュータ。
Oγ
″A=1旧Fig. 1 is an explanatory diagram showing a conventional injection rate needle, Fig. 2 is an explanatory diagram showing an injection rate measuring device according to an embodiment of the present invention, and Fig. 3 is an explanatory diagram showing a signal when the device in Fig. 2 is activated. , clock signal,
A diagram showing the volume chamber pressure, injection rate, needle valve lift, and injection pressure, and FIG. 4 is an explanatory diagram showing the operation of configuration 2 of the microcomputer. 2... Volume chamber, 3... Fuel injection valve, 4... Solenoid valve, 5... Pressure kick-up, 10... Trigger pulse generator, 11... Solenoid valve controller, 12...・
microcomputer. Oγ ″A=1 old
Claims (1)
する装置と,同容器内の圧力を計測する圧力計と,同容
器内の液体を電磁弁で排出する装置と,燃料ポンプカム
軸の1回転につき1パルスの基準トリガパルスを発生す
る装置と,同装置のトリガパルス信号が入力する上記電
磁弁のコントローラと,上記圧力計の出力信号と上記ト
リガパルス信号とが入力され噴射率を算出するコンピュ
ータとからなることを特徴とする噴射率計。1. A container filled with liquid, a device to inject liquid into the container, a pressure gauge to measure the pressure in the container, a device to discharge the liquid in the container using a solenoid valve, and one part of the fuel pump camshaft. A device that generates a reference trigger pulse of one pulse per rotation, a controller for the solenoid valve to which the trigger pulse signal of the device is input, and an output signal of the pressure gauge and the trigger pulse signal are input to calculate the injection rate. An injection rate meter comprising a computer.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12295784A JPS614860A (en) | 1984-06-16 | 1984-06-16 | Injection-rate meter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12295784A JPS614860A (en) | 1984-06-16 | 1984-06-16 | Injection-rate meter |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS614860A true JPS614860A (en) | 1986-01-10 |
Family
ID=14848811
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12295784A Pending JPS614860A (en) | 1984-06-16 | 1984-06-16 | Injection-rate meter |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS614860A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5985371A (en) * | 1996-12-05 | 1999-11-16 | Shin-Etsu Chemical Co., Ltd. | Primer compositions |
FR2795139A1 (en) * | 1999-06-18 | 2000-12-22 | Efs Sa | Device for instantaneous analysis of flow of fuel injector used in heat engine for testing and set-up |
WO2006104176A1 (en) * | 2005-03-29 | 2006-10-05 | National University Corporation Gunma University | Instantaneous flow measuring instrument of gas fuel injector |
WO2007100415A1 (en) * | 2006-02-28 | 2007-09-07 | Caterpillar Inc. | Valve-testing system and method |
EP1746394A3 (en) * | 2005-07-20 | 2008-03-12 | AEA S.r.l. | Method for measuring the quantity of fluid ejected by an injector and device to effect said measuring |
EP2295788A1 (en) * | 2009-08-06 | 2011-03-16 | Continental Automotive GmbH | Method and arrangement for determining a mass flow of an injection process of an injection valve |
-
1984
- 1984-06-16 JP JP12295784A patent/JPS614860A/en active Pending
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5985371A (en) * | 1996-12-05 | 1999-11-16 | Shin-Etsu Chemical Co., Ltd. | Primer compositions |
FR2795139A1 (en) * | 1999-06-18 | 2000-12-22 | Efs Sa | Device for instantaneous analysis of flow of fuel injector used in heat engine for testing and set-up |
WO2000079125A1 (en) * | 1999-06-18 | 2000-12-28 | Efs Sa | Device for instantaneous ad hoc analysis of an injection flow provided by an injection system used in a heat engine |
WO2006104176A1 (en) * | 2005-03-29 | 2006-10-05 | National University Corporation Gunma University | Instantaneous flow measuring instrument of gas fuel injector |
US7845216B2 (en) | 2005-03-29 | 2010-12-07 | National University Corporation Gunma University | Instantaneous flow rate measurement instrument of gaseous fuel injector |
EP1746394A3 (en) * | 2005-07-20 | 2008-03-12 | AEA S.r.l. | Method for measuring the quantity of fluid ejected by an injector and device to effect said measuring |
WO2007100415A1 (en) * | 2006-02-28 | 2007-09-07 | Caterpillar Inc. | Valve-testing system and method |
US7357020B2 (en) | 2006-02-28 | 2008-04-15 | Caterpillar Inc. | Valve-testing system and method employing a fluid-transfer system with a reservoir |
EP2295788A1 (en) * | 2009-08-06 | 2011-03-16 | Continental Automotive GmbH | Method and arrangement for determining a mass flow of an injection process of an injection valve |
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