JPH02286872A - Fuel injection valve - Google Patents

Fuel injection valve

Info

Publication number
JPH02286872A
JPH02286872A JP10815789A JP10815789A JPH02286872A JP H02286872 A JPH02286872 A JP H02286872A JP 10815789 A JP10815789 A JP 10815789A JP 10815789 A JP10815789 A JP 10815789A JP H02286872 A JPH02286872 A JP H02286872A
Authority
JP
Japan
Prior art keywords
fuel
air
injection valve
fuel injection
mixing 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
Application number
JP10815789A
Other languages
Japanese (ja)
Inventor
Toshio Hirota
広田 寿男
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP10815789A priority Critical patent/JPH02286872A/en
Publication of JPH02286872A publication Critical patent/JPH02286872A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To turn fuel into very fine particles by furnishing a mixing chamber for mixing of the fuel and air leading to a fuel passage and an air passage, and providing a ring-shaped jet which leads to this mixing chamber and is so formed as becoming narrower toward the tip. CONSTITUTION:An air atomizing type fuel injection valve 1 is equipped with a mixing chamber 22 for mixing of the fuel and air leading to a fuel passage 24 and an air passage 26. Therein a ring-shaped jet 23 is provided, which leads to this mixing chamber 22 and is formed as narrower toward the tip of the injection valve 1. In this mixing chamber 22 of fuel injection valve 1, the air is mixed with the fuel, which is turned into particulates. The mixture stream is jetted out of the jet 23 and decompressed rapidly, and the fuel is further turned into very fine particles to then be fed to the engine. Thus the performance of the engine can be further enhanced.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、燃料の微粒化性能を向上させた、燃料噴射弁
に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a fuel injection valve with improved fuel atomization performance.

従来の技術 従来の燃料噴射弁としては、例えば、第3図に示すよう
なものがある(実願昭62−171978号等参照)。
2. Description of the Related Art An example of a conventional fuel injection valve is the one shown in FIG. 3 (see Utility Model Application No. 171978/1984).

この燃料噴射弁は、空気噴霧型燃料噴射弁と称されてい
るもので、該燃料噴射弁、Iの噴口部2の近傍に、空気
通路3が開口しており、エアポンプ(第4図参照)から
送られ、エア配管4を通って空気室5に導かれた空気が
、空気通路3がら噴出し、燃料と衝突して微粒化するよ
うになっている。
This fuel injection valve is called an air spray type fuel injection valve, and an air passage 3 is opened near the injection port 2 of the fuel injection valve I, and an air pump (see FIG. 4) The air that is sent from the air pipe 4 and introduced into the air chamber 5 is blown out from the air passage 3, collides with the fuel, and becomes atomized.

第4図には、上記空気噴霧型燃料噴射弁(以下単に燃料
噴射弁と称する)■か使用されている、従来の燃料噴射
弁制御システムを示す。エンジン6の吸気管7に燃料噴
射弁1が設置されている。
FIG. 4 shows a conventional fuel injection valve control system in which the above-mentioned air spray type fuel injection valve (hereinafter simply referred to as a fuel injection valve) is used. A fuel injection valve 1 is installed in an intake pipe 7 of an engine 6.

そして、該燃料噴射弁lに燃料を供給する燃料配管8と
、空気を供給するエアポンプ9及びエア管4、燃料圧力
を一定に保つブレッンヤレギュレータlOによって燃料
噴射弁の制御システムが構成されている。
A fuel injection valve control system is constituted by a fuel pipe 8 that supplies fuel to the fuel injection valve l, an air pump 9 and air pipe 4 that supplies air, and a Brennyer regulator lO that keeps the fuel pressure constant. .

なお、図において、11は水温センサー 12は水温セ
ンサー11の出力により、エアポンプ9の駆動を制御す
るコントロールユニット、13はクランク角センサー 
【4はターボチャージャーである。
In the figure, 11 is a water temperature sensor, 12 is a control unit that controls the drive of the air pump 9 based on the output of the water temperature sensor 11, and 13 is a crank angle sensor.
[4 is a turbocharger.

発明が解決しようとする課題 しかしながら、このような従来の燃料噴射弁Iにあって
は、空気流と燃料流とを衝突させて燃料をmFQ化して
いたので、微粒化性能が十分でなく、例えば、メタノー
ルエンジンの低温始動時などにおいて必要な、極めて小
さい粒径の燃料を得ることができない、という問題点が
あった。
Problems to be Solved by the Invention However, in such a conventional fuel injection valve I, since the air flow and the fuel flow collide to convert the fuel into mFQ, the atomization performance is not sufficient. However, there was a problem in that it was not possible to obtain fuel with an extremely small particle size, which is necessary when starting a methanol engine at a low temperature.

本発明は、このような従来の問題点に着目してなされた
ものであり、その目的とするところは、極めて小さい粒
径の燃料を得ることができる燃料噴射弁を提供しようと
するものである。
The present invention has been made in view of these conventional problems, and its purpose is to provide a fuel injection valve that can obtain fuel with an extremely small particle size. .

課題を解決するための手段 このため本発明は、空気噴霧型燃料噴射弁において、弁
内に設けられた燃料通路及び空気通路に連通ずる燃料と
空気とを混合する混合室と、該混合室に連通し燃料噴射
弁の先端に向かうに従って狭く形成された円環状の噴口
部とを有することを特徴とする。
Means for Solving the Problems Therefore, the present invention provides an air atomizing fuel injection valve including a mixing chamber for mixing fuel and air that communicates with a fuel passage and an air passage provided in the valve; The fuel injection valve is characterized by having an annular nozzle opening that becomes narrower toward the tip of the communicating fuel injection valve.

作用 本願燃料噴射弁は、始動時における燃料の微粒化を促進
するためのものであり、冷却水温が設定値(例えば60
℃)以下のときにエアポンプが作動して加圧された空気
が燃料噴射弁に送られる。
Function The present fuel injection valve is for promoting atomization of fuel at the time of starting, and the cooling water temperature is set at a set value (for example, 60°C).
℃), the air pump operates and pressurized air is sent to the fuel injection valve.

すると、燃料噴射弁の混合室において前記空気は燃料と
混合され燃料は微粒化する。
Then, the air is mixed with fuel in the mixing chamber of the fuel injection valve, and the fuel is atomized.

その後、混合流は、先端に向かって狭く形成された環状
の噴口部より噴射し、急激に減圧され、燃料は極めて小
さい粒径に更に微粒化して、エンジンに供給される。
Thereafter, the mixed flow is injected from an annular injection port formed narrowly toward the tip, and the pressure is rapidly reduced, and the fuel is further atomized to an extremely small particle size and supplied to the engine.

実施例 以下、本発明を図面に基づいて説明する。第1図は、本
発明の一実施例を示す図である。
EXAMPLES Hereinafter, the present invention will be explained based on the drawings. FIG. 1 is a diagram showing an embodiment of the present invention.

まず構成を説明する。ボディ15に燃料流量制御弁16
が、パツキン17及びOリング18により、燃料をシー
ルして固定されている。
First, the configuration will be explained. Fuel flow control valve 16 in body 15
However, the fuel is sealed and fixed by a gasket 17 and an O-ring 18.

また、燃料流量制御弁16.の噴口部I9の下流に、円
筒形状のアウタ部材20と、このアウタ部材20に圧入
により固定された円柱形状のインチ部材2!とによって
、混合室22と円環状の噴口部23とが形成されている
Also, the fuel flow control valve 16. A cylindrical outer member 20 and a cylindrical inch member 2 fixed to the outer member 20 by press-fitting are located downstream of the spout portion I9! A mixing chamber 22 and an annular nozzle portion 23 are formed by these.

混合室22には、燃料通路24と、空気室25から混合
室22へ、旋回空気流を供給する空気通路26とが連通
しており、噴口部23は、先端部に向かうほど狭く形成
されている。なお、27は燃料入口、28は空気入口で
ある。
The mixing chamber 22 communicates with a fuel passage 24 and an air passage 26 that supplies swirling airflow from the air chamber 25 to the mixing chamber 22, and the nozzle portion 23 is formed to become narrower toward the tip. There is. Note that 27 is a fuel inlet and 28 is an air inlet.

第2図には、本発明に係る燃料噴射弁Iが適用される、
燃料噴射弁制御システムの一例を示す。
In FIG. 2, a fuel injection valve I according to the present invention is applied.
An example of a fuel injection valve control system is shown.

エンジン6の吸気管7に燃料噴射弁1が設置されている
。そして、この燃料噴射弁Iに燃料を供給する燃料配管
8と、空気を供給するエアポンプ9及びエア配管4とが
接続されている。
A fuel injection valve 1 is installed in an intake pipe 7 of an engine 6. A fuel pipe 8 that supplies fuel to the fuel injection valve I is connected to an air pump 9 and air pipe 4 that supply air.

そして、絞り弁29上流の吸気管7から、配管30が逆
止弁31を介して、エア配管4に接続され、プレッシャ
レギュレータIOの基準圧配管32も、配管30を介し
てエア配管4に接続されている。
A pipe 30 is connected from the intake pipe 7 upstream of the throttle valve 29 to the air pipe 4 via a check valve 31, and a reference pressure pipe 32 of the pressure regulator IO is also connected to the air pipe 4 via the pipe 30. has been done.

次に第2図を参照して作用を説明する。燃料噴射弁1に
送られた燃料は、燃料流量制御弁16により制御され、
燃料通路24を通り混合室22に噴出する。
Next, the operation will be explained with reference to FIG. The fuel sent to the fuel injection valve 1 is controlled by a fuel flow control valve 16,
The fuel is injected into the mixing chamber 22 through the fuel passage 24 .

一方空気は、水温センサ!■により水温が検出され、設
定値以下たとえば60℃以下のときは、コントロールユ
ニット12の信号により、エアポンプ9が駆動され、エ
ア配管4を通り、空気人口28より燃料噴射弁lに供給
される。供給された空気は、空気室25へ送られ、更に
混合室22へ旋回空気流を供給する空気通路26を通り
、混合室22へ噴出する。
On the other hand, the air is a water temperature sensor! When the water temperature is detected by (2) and is below a set value, for example, 60° C. or below, the air pump 9 is driven by a signal from the control unit 12, and the air is supplied to the fuel injection valve 1 through the air pipe 4 from the air supply 28. The supplied air is sent to the air chamber 25, passes through an air passage 26 that supplies a swirling air flow to the mixing chamber 22, and is ejected into the mixing chamber 22.

混合室22において、燃料流と空気流とが衝突し、燃料
は微粒化され空気と混合する。
In the mixing chamber 22, the fuel flow and the air flow collide, and the fuel is atomized and mixed with the air.

その後、燃料と空気との混合流は、先端部に向かうほど
狭く形成された、環状の噴口部23から噴射される。噴
口部23は、先端部において圧力損失が最大となり、薄
膜となった混合流は、噴射されて急激に減圧され、空気
が膨張し、燃料を極く小さい粒径に微粒化する。
Thereafter, the mixed flow of fuel and air is injected from the annular nozzle 23 that is narrower toward the tip. In the nozzle part 23, the pressure loss is maximum at the tip, and the mixed flow that has become a thin film is injected and the pressure is rapidly reduced, the air expands, and the fuel is atomized to an extremely small particle size.

冷却水温が設定値以上になると、エアポンプ9は停止さ
れる。しかし、空気は、吸気管7より、逆止弁31を介
して配管30を通り、エア配管4へ送られて、燃料噴射
弁lへ空気人口2Bより供給される。
When the cooling water temperature exceeds the set value, the air pump 9 is stopped. However, air is sent from the intake pipe 7, through the check valve 31, through the pipe 30, to the air pipe 4, and then supplied to the fuel injection valve 1 from the air supply 2B.

供給された空気は、低温時と同様に、空気室25、空気
通路26を通り、混合室22へ導入され、燃料と混合す
る。そしてその後、混合流は噴[]部23から噴射され
て、燃料は極く小さい粒径に微粒化される。
The supplied air passes through the air chamber 25 and the air passage 26, is introduced into the mixing chamber 22, and mixes with the fuel, as in the case of low temperature. Thereafter, the mixed flow is injected from the injection part 23, and the fuel is atomized into extremely small particle sizes.

この際、噴口部23は先端が狭く形成されているので、
混合流の膜厚が薄いため、少量の空気で粒径の小さい微
粒化燃料を得ることができる。
At this time, since the tip of the nozzle part 23 is formed narrowly,
Since the film thickness of the mixed flow is thin, atomized fuel with small particle size can be obtained with a small amount of air.

なお、プレッシャレギュレータ10の基準圧配管32か
、エア配管4に接続されており、エア配管4、換言すれ
ば燃料噴射弁1の空気室25の空気圧と、燃料噴射弁1
へ供給される燃料の燃圧との差が一定となるように制御
されているので、常にエンジン6の各運転状態に見合っ
た適正な燃圧が確保され、冷却水温が設定値以上となり
エアポンプが停止しても、精度の良い燃料流潰制御がで
きる。
In addition, it is connected to the reference pressure pipe 32 of the pressure regulator 10 or the air pipe 4, and the air pressure of the air pipe 4, in other words, the air chamber 25 of the fuel injection valve 1 and the fuel injection valve 1
Since the difference between the fuel pressure and the fuel supplied to the engine 6 is controlled to be constant, an appropriate fuel pressure corresponding to each operating state of the engine 6 is always ensured, and the air pump stops when the cooling water temperature exceeds the set value. Accurate fuel spill control is possible even when

また、エアポンプ9を停止しても燃料噴射弁lには空気
が供給されているので、エンジン燃焼室からの吹き返し
により、オイルミストが燃料噴射弁Iの先端に付着する
ことはない。
Furthermore, even when the air pump 9 is stopped, air is still being supplied to the fuel injection valve I, so oil mist does not adhere to the tip of the fuel injection valve I due to blowback from the engine combustion chamber.

発明の効果 本発明は、以上説明してきたように構成されているので
、極めて小さい粒径の燃料を得ることができ、エンジン
性能を一段と向上させることができる。
Effects of the Invention Since the present invention is constructed as described above, it is possible to obtain fuel with an extremely small particle size, thereby further improving engine performance.

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

第1図は本発明の一実施例を示す断面図、第2図は本発
明に係る燃料噴射弁を適用した制御システムの一例を示
す全体構成図、第3図は従来の燃料噴射弁を示す断面図
、第4図は従来の燃料噴射弁制御システムを示す全体構
成図である。 !・・・燃料噴射弁、4・・・エア配管、7・・・吸気
管、9・・エアポンプ、10・・・プレッシャレギュレ
ータ、11・・・水温センサー 12・・・コントロー
ルユニット、I6・・・燃料流量制御弁、22・・・混
合室、23・・・噴口部、24・・・燃料通路、25・
・・空気室、26・・・空気通路、30・・配管、31
・・逆止弁、32・・・基準圧配管。 第1図 1・・燃料噴射弁 16・・燃料通量制御弁 22・・混合室 23・・・噴口部 24・燃料通路 25 空気室 26 ・空気通路
Fig. 1 is a sectional view showing an embodiment of the present invention, Fig. 2 is an overall configuration diagram showing an example of a control system to which the fuel injection valve according to the invention is applied, and Fig. 3 shows a conventional fuel injection valve. The sectional view and FIG. 4 are overall configuration diagrams showing a conventional fuel injection valve control system. ! ...Fuel injection valve, 4...Air piping, 7...Intake pipe, 9...Air pump, 10...Pressure regulator, 11...Water temperature sensor 12...Control unit, I6... Fuel flow control valve, 22... Mixing chamber, 23... Nozzle part, 24... Fuel passage, 25...
...Air chamber, 26...Air passage, 30...Piping, 31
...Check valve, 32...Reference pressure piping. Fig. 1 1...Fuel injection valve 16...Fuel flow control valve 22...Mixing chamber 23...Nozzle port 24/Fuel passage 25 Air chamber 26/Air passage

Claims (1)

【特許請求の範囲】[Claims] (1)空気噴霧型燃料噴射弁において、弁内に設けられ
た燃料通路及び空気通路に連通する燃料と空気とを混合
する混合室と、該混合室に連通し先端に向かうに従って
狭く形成された円環状の噴口部とを有することを特徴と
する燃料噴射弁。
(1) In an air spray type fuel injection valve, there is a mixing chamber for mixing fuel and air that communicates with a fuel passage and an air passage provided in the valve, and a mixing chamber that communicates with the mixing chamber and is formed to become narrower toward the tip. A fuel injection valve characterized by having an annular injection port.
JP10815789A 1989-04-27 1989-04-27 Fuel injection valve Pending JPH02286872A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10815789A JPH02286872A (en) 1989-04-27 1989-04-27 Fuel injection valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10815789A JPH02286872A (en) 1989-04-27 1989-04-27 Fuel injection valve

Publications (1)

Publication Number Publication Date
JPH02286872A true JPH02286872A (en) 1990-11-27

Family

ID=14477401

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10815789A Pending JPH02286872A (en) 1989-04-27 1989-04-27 Fuel injection valve

Country Status (1)

Country Link
JP (1) JPH02286872A (en)

Similar Documents

Publication Publication Date Title
US4361126A (en) Fuel injection valve
US4215549A (en) Turbocharger combustor system
JPS6056908B2 (en) Fuel control device for fuel injection system
US4351304A (en) Fuel injection valve
CA1076900A (en) Fuel supply apparatus for internal combustion engines
CZ296645B6 (en) Apparatus for mixing fuel with air
US4969446A (en) Device at internal combustion engines
JPH021979B2 (en)
US4557241A (en) Fuel injection means having air bleed means
US5245977A (en) Flow proportioning mixer for gaseous fuel and air and internal combustion engine gas fuel mixer system
US3977374A (en) Arrangement for the preparation of the fuel-air mixture for an internal combustion engine
US4955349A (en) Device for preparation of a fuel-air mixture for internal combustion engines
US2349675A (en) Charge forming system for internalcombustion engines with reuse of exhaust gases
JPH02286872A (en) Fuel injection valve
US4489701A (en) Method and fuel supply system for fuel supply to a mixture-compressing internal combustion engine with externally supplied engine
KR950033047A (en) Intake apparatus of internal combustion engine
SE8005147L (en) LIKTRYCKSFORGASARE
JPH02286869A (en) Control system for fuel injection valve
JPS633427Y2 (en)
JP2778384B2 (en) Fuel injection device for internal combustion engine
RU2147074C1 (en) Carburetor jet
JPS63314363A (en) Fuel injection device
JP3264069B2 (en) Fuel injection device for internal combustion engine
JPS59194047A (en) Feeding method of fuel for engine
JPH06129331A (en) Fuel supply system of internal combustion engine