JPS6111451A - Fuel injection device - Google Patents

Fuel injection device

Info

Publication number
JPS6111451A
JPS6111451A JP13163484A JP13163484A JPS6111451A JP S6111451 A JPS6111451 A JP S6111451A JP 13163484 A JP13163484 A JP 13163484A JP 13163484 A JP13163484 A JP 13163484A JP S6111451 A JPS6111451 A JP S6111451A
Authority
JP
Japan
Prior art keywords
fuel
injection
liquid chamber
pressure
injection port
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
JP13163484A
Other languages
Japanese (ja)
Inventor
Yoshiro Danno
団野 喜朗
Kazuhiro Shiraishi
白石 一洋
Takanao Yokoyama
横山 高尚
Shogo Omori
祥吾 大森
Kiyoshi Hatano
清 波多野
Makoto Shimada
誠 島田
Yoshihiro Konno
紺野 義博
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 Motors Corp
Original Assignee
Mitsubishi Motors 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 Motors Corp filed Critical Mitsubishi Motors Corp
Priority to JP13163484A priority Critical patent/JPS6111451A/en
Publication of JPS6111451A publication Critical patent/JPS6111451A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/08Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/04Injectors peculiar thereto
    • F02M69/041Injectors peculiar thereto having vibrating means for atomizing the fuel, e.g. with sonic or ultrasonic vibrations

Abstract

PURPOSE:To make it possible to minutely control the amount of fuel even at injection of the minimum amount of fuel, by injecting fuel in a liquid chamber having an injection port in the form of fuel drops into a suction passage by driving an electrostrictive vibrator receiving an electric signal. CONSTITUTION:A fuel pump 13 and an air pump 16 are driven to increase a fuel pressure in a liquid chamber 6 to P2 and increase an air pressure in a pressure air chamber 10 to P1. At this time, an injection port 7 continues to be sealed by a liquid membrane G1 of fuel. When a starter is driven, suction pressure P0 in a suction passage 4 becomes negative. Simultaneously, an optimal pulse signal for a starting condition is applied to each piezoelectric device 2, and fuel drops g are injected from each injection port 7 through an opening 9 into the suction passage 4 every time the device 2 receives the pulse signal.

Description

【発明の詳細な説明】 本発明は内燃機関の燃料噴射装置、特に、内燃機関の吸
気路に燃料を噴射する燃料噴射装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel injection device for an internal combustion engine, and more particularly to a fuel injection device for injecting fuel into an intake passage of an internal combustion engine.

車両用の内燃機関はアイドリンクより全負荷運転まで拡
範囲にその運転秋態を変化させる必要があシ、吸入空気
量や燃、料供給量が拡範囲で調整される。この内燃料供
給量を調整する方式の1つとして、ガソリンエンジンの
吸気路に燃料噴射装置を取付け、これにより吸気路中に
燃料を噴射する燃料供給系が知られている。この燃料供
給系は燃料ポンプにより燃料を加圧し、この加圧燃料を
燃料噴射装置内のソレノイド弁の開閉操作により適時噴
射するもので、ソレノイド弁の開口数あるいは開時間を
吸気量や吸気圧、エンジン回転速度等に応じ調整してい
る。
Internal combustion engines for vehicles need to change their operating conditions over a wide range from idle to full load operation, and the amount of intake air and fuel supply are adjusted over a wide range. As one of the methods for adjusting the amount of fuel supplied, a fuel supply system is known in which a fuel injection device is attached to the intake passage of a gasoline engine, and thereby fuel is injected into the intake passage. This fuel supply system pressurizes fuel using a fuel pump, and injects this pressurized fuel at the appropriate time by opening and closing a solenoid valve in the fuel injection device. It is adjusted according to engine speed, etc.

このように、従来の燃料供給系に用いられる燃料噴射装
置は開閉弁としてのソレノイド弁であシ。
As described above, the fuel injection device used in the conventional fuel supply system uses a solenoid valve as an on-off valve.

最小噴射量や最大噴射量をソレノイドの応答特性により
決定される。この場合、燃料噴射装置は最小噴射量に対
する最大噴射量を40乃至80倍に規制されるものが多
く、ダイナミックレンジが狭い傾向にある。これに対し
、エンジン側の要求するダイナミックレンジは100を
越すものが多い。このため、従来はエンジンと燃料噴射
装置のマツチングを行なう際エンジン側の全負荷運転を
可能とするよう、燃料噴射装置の最小噴射量を増加させ
The minimum injection amount and maximum injection amount are determined by the response characteristics of the solenoid. In this case, the maximum injection amount of most fuel injection devices is regulated to be 40 to 80 times the minimum injection amount, and the dynamic range tends to be narrow. On the other hand, the dynamic range required by the engine often exceeds 100. For this reason, conventionally, when matching the engine and fuel injection device, the minimum injection amount of the fuel injection device was increased to enable full load operation on the engine side.

これにより、燃料噴射装置の最大噴射量をエンジン側の
要求するダイナミックレンジが100に相当する噴射量
に合わせている。このため、従来の燃料噴射装置は最小
噴射量の噴射作動時において。
As a result, the maximum injection amount of the fuel injection device is adjusted to the injection amount corresponding to a dynamic range of 100 required by the engine. For this reason, when the conventional fuel injection device injects the minimum injection amount.

微少の燃料量制御を行なうことができないという不具合
がある。本発明は上述の不具合を除去できる燃料噴射装
置を提供することを目的とする。
There is a problem in that minute fuel amount control cannot be performed. An object of the present invention is to provide a fuel injection device that can eliminate the above-mentioned problems.

本発明は上述の目的を達成させるだめ、噴射口を備えた
液室内の燃料を、電気信号を受けた電歪振動子の駆動に
より、内燃機関の吸気路に燃料滴として噴射することを
特徴としたものである。
In order to achieve the above-mentioned object, the present invention is characterized in that fuel in a liquid chamber equipped with an injection port is injected as fuel droplets into an intake path of an internal combustion engine by driving an electrostrictive vibrator that receives an electric signal. This is what I did.

このような燃料噴射装置は電気信号を受ける毎に電歪振
動子が駆動し、燃料を燃料滴化して噴射することよシ最
小噴射量に対する最大噴射量を大きく、即ち、噴射量の
ダイナミックレンジを大キくできる。
In such a fuel injection device, an electrostrictive oscillator is driven every time an electric signal is received, and the fuel is turned into fuel droplets and injected. I can do it big.

第1図には本発明の一実施例としての燃料噴射装置を示
した。この燃料噴射装置は図示しないガソリンエンジン
の吸気管1に取付けられ、電歪振動子としてのピエゾ素
子2を内部に備えた本体3を複数個配列することにより
形成される。なお。
FIG. 1 shows a fuel injection device as an embodiment of the present invention. This fuel injection device is attached to an intake pipe 1 of a gasoline engine (not shown), and is formed by arranging a plurality of main bodies 3 each having a piezo element 2 therein as an electrostrictive vibrator. In addition.

本体3はエンジンへの最大噴射量を確保できるだけの個
数が用いられ、その配列は第4図や第5図に示すように
平面的に配列してもよく、第6図に示すように吸気管1
内の吸気路4に沿って複数列に本体3を配列させてもよ
い。第1図においては複数個の内の1つの本体3を主に
説明する。
The number of main bodies 3 used is sufficient to ensure the maximum injection amount to the engine, and they may be arranged in a plane as shown in Figs. 4 and 5, or in the intake pipe as shown in Fig. 6. 1
The main bodies 3 may be arranged in a plurality of rows along the air intake passages 4 inside. In FIG. 1, one of the main bodies 3 will be mainly explained.

本体3はボデー5と、とのボデー内の液室6と。The main body 3 has a body 5 and a liquid chamber 6 in the body.

液室6の吸気路4との対向側に形成される噴射ロアと、
噴射ロア近傍の液室6側に連通ずる燃料供給室8と、噴
射ロアの出口側の四りを覆うと共に。
an injection lower formed on the opposite side of the liquid chamber 6 to the intake passage 4;
It covers the fuel supply chamber 8 communicating with the liquid chamber 6 near the injection lower and the four sides on the outlet side of the injection lower.

噴射ロアとの対向位置に開口9を形成した加圧空気室1
0とで形成される。液室6はその上壁全体がピエゾ素子
2により形成され、下端に小径の噴射ロアを備え、全体
はほぼ逆円錐状を呈する。ピエゾ素子2は上下面に図示
しない電極が形成され。
A pressurized air chamber 1 having an opening 9 formed at a position facing the injection lower
0. The entire upper wall of the liquid chamber 6 is formed by the piezo element 2, a small diameter injection lower is provided at the lower end, and the entire liquid chamber 6 has a substantially inverted conical shape. The piezo element 2 has electrodes (not shown) formed on the upper and lower surfaces.

これにはコンピュータ11よシ駆動用のパルス信号が印
加される。ここで、第2図Tblに示すように電圧Vの
パルス信号がオフよりオンに立上るとピエゾ素子2は第
2図(alに2点鎖線で示すように歪む。
A pulse signal for driving the computer 11 is applied to this. Here, as shown in FIG. 2 Tbl, when the pulse signal of the voltage V rises from OFF to ON, the piezo element 2 is distorted as shown by the two-dot chain line in FIG. 2 (al).

この際、ピエゾ素子2は電気エネルギを機械エネルギに
変換する。この機械エネルギは液室6の燃料G内に音響
エネルギとして変換されて伝わり。
At this time, the piezo element 2 converts electrical energy into mechanical energy. This mechanical energy is converted into acoustic energy and transmitted into the fuel G in the liquid chamber 6.

結果として燃料が粒子化され、噴射ロアよシ燃料滴tと
して噴射される(第3図(al参照)。なお。
As a result, the fuel becomes particles and is injected as fuel droplets from the injection lower part (see Fig. 3 (al)).

噴射ロアは比較的小径でありピエゾ素子2の非駆動時に
おいて、燃料の液膜G1によりシールされる。
The injection lower has a relatively small diameter and is sealed by a liquid film G1 of fuel when the piezo element 2 is not driven.

この液膜G1は燃料の表面張力の働きによ多形成され、
これは噴射ロアの内外の圧力差を一定値内に保つことに
よ多形成され、これを上回ると、破壊される。燃料供給
室8は路上下に長い液室6に対し直交する方向に形成さ
れ、第3図(alに示すようにピエゾ素子2が非駆動状
態に戻る際、液室6に燃料供給を行なうことができる。
This liquid film G1 is formed due to the surface tension of the fuel,
This is formed by keeping the pressure difference between the inside and outside of the injection lower within a certain value, and if it exceeds this value, it will be destroyed. The fuel supply chamber 8 is formed in a direction perpendicular to the liquid chamber 6 which is long below the road, and supplies fuel to the liquid chamber 6 when the piezo element 2 returns to the non-driving state as shown in FIG. I can do it.

燃料供給室8には燃料管12を介し燃料ポンプ13及び
燃料タンク14が連結される。一方、加圧空気室10は
ボデー5内の最も吸気路4側に形成され、空気管15を
介しエアポンプ16よシ加圧空気を供給される。この加
圧空気室10に流入した加圧空気は開口9より負圧であ
る吸気圧POの吸気路4に流出し、しかも噴射ロアに空
気圧P1を加える。なお、空気圧P1は噴射ロアに液膜
G1′f:形成できればよく、燃料圧P2に等しいかそ
れに近似する値に設定される。ここではPI > P2
に設定されている。なお、第8図に示すように噴射ロア
を加圧空気室10側に対し閉鎖する開閉弁18を取付け
てもよい。この開閉弁18は常閉のソレノイド弁であり
、イグニシロンスイッチ19のオン時にソレノイド20
が駆動し、開閉弁18を閉よシ開位置(第8図に実線で
示す位置)に保持する。なお、開閉弁18は加圧空気室
lo内に装着されたばね21により常時噴射ロア側壁部
に圧接されている。この場合、キーオフ時に液室6を閉
鎖でき、この液室の気体が浸入し、空洞化するととを防
止できる。コンピュータ11は吸気量をエアフローセン
サ17から入力されるパルス信号に基き算出し1図示し
ないセンサよシの入力信号により各運転状態を検出し、
これに応じた最適な空燃比が得られる燃料供給量を算出
する。そして、この燃料供給量に対応した噴射回数を得
るべく、ピエゾ素子2に対し所定の電圧Vのパルスを単
位時間当りにおいて所定回数ずつ出力する。
A fuel pump 13 and a fuel tank 14 are connected to the fuel supply chamber 8 via a fuel pipe 12. On the other hand, the pressurized air chamber 10 is formed closest to the intake path 4 in the body 5 and is supplied with pressurized air from an air pump 16 through an air pipe 15. The pressurized air that has flowed into the pressurized air chamber 10 flows out from the opening 9 into the intake path 4 where the intake pressure PO, which is a negative pressure, applies an air pressure P1 to the injection lower. Note that the air pressure P1 only needs to be able to form a liquid film G1'f on the injection lower, and is set to a value equal to or close to the fuel pressure P2. Here PI > P2
is set to . In addition, as shown in FIG. 8, an on-off valve 18 may be installed to close the injection lower to the pressurized air chamber 10 side. This on-off valve 18 is a normally closed solenoid valve, and when the ignition switch 19 is turned on, the solenoid 20
is driven to hold the on-off valve 18 in the closed and open position (the position shown by the solid line in FIG. 8). The on-off valve 18 is always pressed against the injection lower side wall by a spring 21 mounted in the pressurized air chamber lo. In this case, the liquid chamber 6 can be closed when the key is turned off, thereby preventing gas from entering the liquid chamber and forming a cavity. The computer 11 calculates the intake air amount based on the pulse signal input from the air flow sensor 17, and detects each operating state based on the input signal from a sensor (not shown).
The amount of fuel supplied that provides the optimum air-fuel ratio is calculated accordingly. Then, in order to obtain the number of injections corresponding to this fuel supply amount, pulses of a predetermined voltage V are outputted to the piezo element 2 a predetermined number of times per unit time.

第1図の燃料噴射装置は図示しないエンジンキ−がオン
されることにより作動する。まず、燃料ポンプ13とエ
アポンプ16が駆動し液室6の燃料圧がP2に、加圧空
気室10の空気圧がPlにそれぞれ昇圧し、噴射ロアは
燃料による液膜G1によりシールされ続ける。続いて、
エンジンキーがスタータを駆動させることにより、吸気
路4の吸気圧POは負圧化する。同時にコンピュータ1
1よシ始動状態VC最適なパルス信号が各ピエゾ素子2
に印加され、パルス信号を受ける毎に各噴射ロアより開
口9を通して燃料滴tが吸気路4に噴射される。この場
合、複数個の本体3よりそれぞれ燃料滴9が噴射され、
吸気路4で形成された混合気は図示しない燃焼室で燃焼
し、エンジンが始動する。この後、コンピュータ11は
運転状態に応じ、最適な数のパルス信号を複数個の本体
3に同時に出力し。
The fuel injection system shown in FIG. 1 is activated when an engine key (not shown) is turned on. First, the fuel pump 13 and the air pump 16 are driven to increase the fuel pressure in the liquid chamber 6 to P2 and the air pressure in the pressurized air chamber 10 to Pl, and the injection lower continues to be sealed by the liquid film G1 made of fuel. continue,
When the engine key drives the starter, the intake pressure PO in the intake passage 4 becomes negative pressure. computer 1 at the same time
1, the optimum pulse signal for the starting state VC is applied to each piezo element 2.
is applied, and fuel droplets t are injected into the intake passage 4 from each injection lower through the opening 9 every time a pulse signal is received. In this case, fuel droplets 9 are injected from each of the plurality of main bodies 3,
The air-fuel mixture formed in the intake passage 4 is combusted in a combustion chamber (not shown), and the engine is started. Thereafter, the computer 11 simultaneously outputs an optimal number of pulse signals to the plurality of main bodies 3 according to the operating state.

これによりエンジンが出力を発生し、車両が走行する。This causes the engine to generate power and the vehicle to move.

上述の処において本体3は1つのピエゾ素子2を備え、
パルス毎に1噴射を行なうものであったが、これに代え
、第7図に示すように1本体37内に1つのピエゾ素子
2を備え、その両面に液室6をそれぞれ形成し1両液室
の左右端にそれぞれ噴射ロアを形成し、各噴射ロアを加
圧空気室1oでそれぞれ覆い、各加圧空気室1oの噴射
ロアとの対向位置に開口9をそれぞれ形成してもよい。
In the above, the main body 3 includes one piezo element 2,
Instead of this, one piezo element 2 is provided in one main body 37, and liquid chambers 6 are formed on both sides of the piezo element 2, as shown in FIG. Injection lowers may be formed at the left and right ends of the chamber, each injection lower is covered with a pressurized air chamber 1o, and an opening 9 may be formed in each pressurized air chamber 1o at a position facing the injection lower.

乙の場合、1つの本体3′(ピエゾ素子2)に1パルス
ヲ加える毎に両噴射ロアより1噴射ずつ計2噴射を行な
うことができ1本体の数を半減させることができ、取付
スペースの確保が容易となる。更に、上述の本体3を記
録装置用に用いているインクジェットヘッド、いわゆる
オンデマンド型ヘッドに類似した装置として作成した場
合、その1滴当シの噴射量は少量であるが1本体3の取
付スペースを十分確保できるものであれば、このインク
ジェットヘッドに類似した装置を数十個用いることによ
り本装置を作成できる。更に、−滴の量を十分増量可能
な本体3を用いれば数個の本体により燃料噴射装置を作
成できる。
In the case of B, a total of two injections can be performed, one from both injection lowers each time one pulse is applied to one main body 3' (piezo element 2), and the number of one main body can be halved, securing installation space. becomes easier. Furthermore, if the main body 3 described above is made as a device similar to an inkjet head used in a recording device, a so-called on-demand head, the amount of ejection per drop is small, but the installation space of the main body 3 is small. As long as the inkjet head can be sufficiently secured, the present device can be created by using several dozen devices similar to this inkjet head. Furthermore, by using the main body 3 which can sufficiently increase the amount of droplets, a fuel injection device can be created with several main bodies.

更に、上述の各本体3には加圧空気室1oを備えていた
が、吸気路4が正圧化するターボチャージヤの吐出側に
噴射ロアが対設されるような場合、加圧空気室10を排
除してもよい。
Furthermore, although each of the above-mentioned main bodies 3 was equipped with the pressurized air chamber 1o, in the case where the injection lower is disposed opposite to the discharge side of the turbocharger where the intake path 4 becomes positive pressure, the pressurized air chamber 1o is 10 may be excluded.

このように、本発明による燃料噴射装置はエピゾ素子2
をパルス信号により駆動させるため、毎秒1乃至2万回
程度エピゾ素子2を駆動させることができ、そのダイナ
ミックレンジ自体を非常に大きくとれる。このため、極
微量の噴射量制御が可能で、この点従来より燃費を向上
できる。しかも、ダイナミックレンジが大きいことより
最小より最大噴射量まで適確な噴射量制御が可能となる
In this way, the fuel injection device according to the present invention has the episodic element 2
Since it is driven by a pulse signal, the episodic element 2 can be driven approximately 10,000 to 20,000 times per second, and its dynamic range itself can be very large. Therefore, it is possible to control the amount of injection in an extremely small amount, and in this respect, fuel efficiency can be improved compared to the conventional method. Moreover, since the dynamic range is large, it is possible to accurately control the injection amount from the minimum to the maximum injection amount.

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

第1図は本発明の一実施例としての燃料噴射装置の概略
断面図、第2図及び第3図は同上燃料噴射装置の各々異
なる作動を説明する要部断面図、第4図は同上燃料噴射
装置の本体の配列を表わす概略平面図、第5図は第4図
に示す装置の概略断面図、第6図は同」二本体の他の配
列を表わす概略断面図、第7図及び第8図は本発明の各
々異なる他の実施例としての燃料噴射装置の要部断面図
をそれぞれ示している。 2・・・・ピエゾ素子、4・・・・吸気路、6・・・・
液室、7・・・・噴射口、9・・・・開口、1o・・・
・加圧空気室、G1・・・・液膜、G・・・・燃料。
FIG. 1 is a schematic sectional view of a fuel injection device as an embodiment of the present invention, FIGS. 2 and 3 are sectional views of essential parts explaining different operations of the same fuel injection device, and FIG. 4 is a schematic sectional view of a fuel injection device as an embodiment of the present invention. 5 is a schematic sectional view of the device shown in FIG. 4, FIG. 6 is a schematic sectional view showing another arrangement of the two main bodies, and FIGS. FIG. 8 shows sectional views of essential parts of fuel injection devices as other different embodiments of the present invention. 2...Piezo element, 4...Intake path, 6...
Liquid chamber, 7... Injection port, 9... Opening, 1o...
- Pressurized air chamber, G1...liquid film, G...fuel.

Claims (1)

【特許請求の範囲】 内燃機関の吸気路に対設されると共に燃料の供給を受け
る液室と、電気信号を受けることにより上記液室内の燃
料に振動を伝える電歪振動子と、上記液室に連通すると
共に燃料の液膜によりシール可能な噴射口とを有し、上
記電歪振動子の駆動により上記噴射口を通して吸気路に
燃料 滴を噴射する燃料噴射装置。
[Scope of Claims] A liquid chamber that is disposed opposite to an intake passage of an internal combustion engine and receives fuel supply, an electrostrictive vibrator that transmits vibrations to the fuel in the liquid chamber by receiving an electric signal, and the liquid chamber. and an injection port that is in communication with the injection port and can be sealed by a liquid film of fuel, and injects fuel droplets into an intake passage through the injection port by driving the electrostrictive vibrator.
JP13163484A 1984-06-26 1984-06-26 Fuel injection device Pending JPS6111451A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13163484A JPS6111451A (en) 1984-06-26 1984-06-26 Fuel injection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13163484A JPS6111451A (en) 1984-06-26 1984-06-26 Fuel injection device

Publications (1)

Publication Number Publication Date
JPS6111451A true JPS6111451A (en) 1986-01-18

Family

ID=15062636

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13163484A Pending JPS6111451A (en) 1984-06-26 1984-06-26 Fuel injection device

Country Status (1)

Country Link
JP (1) JPS6111451A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6427010U (en) * 1987-08-07 1989-02-16
US6474566B1 (en) 2000-06-20 2002-11-05 Ngk Insulators, Ltd. Drop discharge device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6427010U (en) * 1987-08-07 1989-02-16
US6474566B1 (en) 2000-06-20 2002-11-05 Ngk Insulators, Ltd. Drop discharge device

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