JPH0450472A - Fuel jet device for internal combustion engine - Google Patents

Fuel jet device for internal combustion engine

Info

Publication number
JPH0450472A
JPH0450472A JP15898990A JP15898990A JPH0450472A JP H0450472 A JPH0450472 A JP H0450472A JP 15898990 A JP15898990 A JP 15898990A JP 15898990 A JP15898990 A JP 15898990A JP H0450472 A JPH0450472 A JP H0450472A
Authority
JP
Japan
Prior art keywords
fuel
air
nozzle
atomization
injection
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
JP15898990A
Other languages
Japanese (ja)
Inventor
Yuki Nakajima
祐樹 中島
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 JP15898990A priority Critical patent/JPH0450472A/en
Priority to US07/709,605 priority patent/US5129381A/en
Priority to DE4119206A priority patent/DE4119206C2/en
Publication of JPH0450472A publication Critical patent/JPH0450472A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To improve atomization of fuel while preventing fuel mists from being mixed with each other by providing jet ports to jet fuel in two different directions, and air jet ports to jet air between them to separate the fuel mists from each other. CONSTITUTION:Jet ports 4a, 4b for jetting fuel in two different directions and air jet ports 8a, 8b for jetting air between them to separate fuel mists form each other are provided. Air for changing jetted fuel into fine grains is jetted from the air jet ports 8a, 8b to be inserted between the fuel mists jetted in the different directions from the two jet ports 4a, 4b. While the two flows of fuel mists are separated from each other, therefore, the fuel can be changed into fine grains.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は内燃機関の燃料噴射装置の改良に関する。[Detailed description of the invention] (Industrial application field) The present invention relates to improvements in fuel injection devices for internal combustion engines.

(従来の技術) 内燃機−の吸気ボートに燃料噴射弁を取付け、噴射燃料
と空気を予混合した混合気を機関に供給する場合、噴射
燃料の微粒化、霧化状態が燃焼特性に大きく関与してく
る。
(Prior art) When a fuel injection valve is attached to the intake boat of an internal combustion engine and a mixture of premixed injected fuel and air is supplied to the engine, the atomization and atomization state of the injected fuel greatly affects the combustion characteristics. It's coming.

そこで、燃料噴射弁から燃料と共に空気(アシストエア
)を噴射して、このアシストエアとの衝突により燃料の
微粒化、霧化の改善を図るようにしたものが、数多く提
案されている。
Therefore, many fuel injection valves have been proposed in which air (assist air) is injected together with fuel from a fuel injection valve, and collision with the assist air atomizes the fuel and improves atomization.

ところで機関の高速化、高出力化をねらって燃焼室に2
つの吸気弁を備え、吸気効率を高める場合、吸気ボート
に設置した燃料噴射弁からは、2つの吸気弁に向けて均
等に燃料を振り分ける必要があり、このため実開平1−
61461号公報には、2方向に分離して燃料噴霧の末
流を形成するようにした燃料噴射弁が提案されている。
By the way, in order to increase the speed and output of the engine, two parts are installed in the combustion chamber.
When equipped with two intake valves to improve intake efficiency, it is necessary to distribute fuel evenly from the fuel injection valve installed on the intake boat toward the two intake valves.
Japanese Patent No. 61461 proposes a fuel injection valve that separates fuel spray into two directions to form tail streams of fuel spray.

2つの噴口(ボート)から燃料を噴射することにより、
燃料の向きを2つの吸気弁に均等に振り分けるのである
が、同時に噴射燃料の微粒化等を図るために、2つの噴
口から噴出する前に、混合室でアシストエアと混合して
いる。
By injecting fuel from two nozzles (boats),
The direction of the fuel is distributed equally to the two intake valves, but at the same time, in order to atomize the injected fuel, it is mixed with assist air in a mixing chamber before being ejected from the two nozzles.

(発明が解決しようとする課題) ところが、このように噴口から燃料が噴出する前にアシ
ストエアと混合すると、噴口を通過する際に燃料の多く
は噴口壁面に付着して壁流となりやすく、噴射燃料の分
流はできても、燃料の微粒化、霧化特性に問題を残した
(Problem to be Solved by the Invention) However, if fuel is mixed with assist air before it is ejected from the nozzle, most of the fuel adheres to the nozzle wall surface when passing through the nozzle and tends to form a wall flow, causing the injection Although the fuel could be separated, problems remained with the atomization and atomization characteristics of the fuel.

したがって噴射燃料の微粒化、霧化特性の改善という点
からは、実開平1−66471号公報にもあるように、
噴口から燃料が噴出した直後に、その周囲からアシスト
エアを噴射する方が、噴口壁面への付着がない分だけ効
果が高いと言える。
Therefore, from the point of view of atomizing the injected fuel and improving the atomization characteristics, as stated in Japanese Utility Model Application No. 1-66471,
It can be said that injecting assist air from around the fuel immediately after it is ejected from the nozzle is more effective since it does not adhere to the nozzle wall.

ところが、この場合、燃料噴霧の周囲から旋回するよう
にアシストエアが噴出するため、燃料噴射方向を2つに
分流することが難しく、2つの吸気弁に向けて均等に燃
料を振り分けることができない。
However, in this case, since the assist air is jetted out in a swirling manner from around the fuel spray, it is difficult to divide the fuel injection direction into two, making it impossible to distribute the fuel evenly toward the two intake valves.

そこで本発明は、燃料噴霧の分流化を損なうことなく微
粒化、霧化を高めた内燃機間の燃料噴射装置を提供する
ことを目的とする。
SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a fuel injection device between internal combustion engines that improves atomization and atomization without impairing the separation of fuel spray.

(課題を解決するための手段) 本発明は、噴口から噴射直後の燃料に高速空気を噴射す
る内燃機関の燃料噴射装置において、少なくとも2つの
異なった方向に燃料を噴射する噴口と、各燃料噴霧を分
離するようにその中間に空気を噴出させる空気噴aとを
備える。
(Means for Solving the Problems) The present invention provides a fuel injection device for an internal combustion engine that injects high-velocity air into fuel immediately after injection from a nozzle. and an air jet a for jetting air between them so as to separate them.

(作用) 2つの噴口から異なる方向に噴出した燃料噴霧の間に割
って入るように、噴射燃料を微粒化するための空気が噴
射され、2つの噴霧を左右に分離しつつ、燃料の微粒化
を図る。
(Operation) Air is injected to atomize the injected fuel between the fuel sprays ejected in different directions from the two nozzles, separating the two sprays left and right and atomizing the fuel. We aim to

(実施例) 以下、本発明の実施例を図面に基づいて説明する。(Example) Embodiments of the present invention will be described below based on the drawings.

第1図、第2図に示すように、燃料噴射弁はインジェク
タ本体1の中央の噴射ノズル2の先端に位置して噴射プ
レート3が配設され、この噴射プレート3には複数の噴
口4a、4bが形成される。
As shown in FIGS. 1 and 2, the fuel injection valve is provided with an injection plate 3 located at the tip of an injection nozzle 2 in the center of an injector body 1, and this injection plate 3 has a plurality of injection ports 4a, 4b is formed.

2つづつの噴口4aと4bは、燃料噴霧を噴射ノズル軸
線に対して所定の傾斜角度で、かつ軸線と直交する平面
において、18o°異なる2方向に指向させるように形
成される。ただしこれらは、2つの吸気弁に対向させる
ように燃料を噴射する場合であり、必要に応じてさらに
噴口数を増加させることもできる。なお、実際の燃料噴
霧は、斜線域で示すように所定の噴射角をもって円錐状
に広がる。
The two injection ports 4a and 4b are formed so as to direct the fuel spray in two directions different by 18 degrees at a predetermined inclination angle to the injection nozzle axis and in a plane perpendicular to the axis. However, these are cases where fuel is injected so as to face two intake valves, and the number of nozzles can be further increased as necessary. Note that the actual fuel spray spreads in a conical shape with a predetermined injection angle, as shown by the shaded area.

インジェクタ本体1の先端には、アダプタ5が取付けら
れ、この内部に形成した環状のエアギヤラリ6にエア通
路7からの空気が導入される。
An adapter 5 is attached to the tip of the injector body 1, and air from an air passage 7 is introduced into an annular air gear gallery 6 formed inside the adapter 5.

噴射ノズル2を取り囲むアダプタ5の内周壁部10には
、一対の主空気噴口8a、8bと、それぞれ2つづつの
副空気噴口9m、9bが形成され、エアギヤラリ6から
の空気を噴出させる。
A pair of main air nozzles 8a, 8b and two auxiliary air nozzles 9m, 9b are formed in the inner circumferential wall 10 of the adapter 5 surrounding the injection nozzle 2, and air from the air gear gallery 6 is jetted out.

主空気噴口8mと8bは互いに対向する位置に配設され
、前記2つの燃料噴霧の中間に位置して、燃料噴霧方向
と直交する方向に空気を噴出するように設定される。た
だし、主空気噴口8a、8bは周囲のエアギヤラリ6が
ら中心に向けて斜めに空気を噴出するため、互いの噴出
空気は燃料噴射ノズル2の中心線上を交差するように通
過し、これらにより2つの燃料噴霧を互いに分離しつつ
燃料との衝突により微粒化、霧化を促進する。
The main air nozzles 8m and 8b are arranged at positions facing each other, located between the two fuel sprays, and set to eject air in a direction perpendicular to the fuel spray direction. However, since the main air nozzles 8a and 8b eject air obliquely toward the center of the surrounding air gear gallery 6, the ejected air from each other passes through the center line of the fuel injection nozzle 2 so as to intersect with each other. It separates the fuel spray from each other and promotes atomization and atomization through collision with the fuel.

副空気噴口9m、9bは各主空気噴口8aと8bをはさ
んでその左右に位置し、ここからの噴出空気流により燃
料噴霧の噴霧角の広がりを抑制しつつ、燃料との衝突に
より微粒化、霧化を高める。
The auxiliary air nozzles 9m and 9b are located on the left and right sides of each main air nozzle 8a and 8b, and the air flow ejected from these suppresses the spread of the spray angle of the fuel spray, while atomizing it by collision with the fuel. , increase atomization.

第3図に示すように、この燃料噴射インジェクタ15は
、吸気マニホールド16に取付られ、吸気ボート17か
ら吸気弁18に向けて燃料を噴射する。
As shown in FIG. 3, this fuel injector 15 is attached to an intake manifold 16 and injects fuel from an intake boat 17 toward an intake valve 18.

前記エア通路7は吸気絞弁19の上流で、かつエアフロ
ーメータ20の下流の位置から分岐し、吸気絞弁19の
上流と下流の圧力差(吸入負圧)に応じて空気を流す、
なお、吸気通路21を流れる空気と、エア通路7を流れ
る空気は燃料噴射インジェクタ15の下流で合流し、し
かも、これらは総てエアフローメータ2oで計量される
ので、混合気の空燃比はアシストエアによって変動する
ことはない、なお、22はエア通路7の流量を制御する
バルブで、機関回転数、吸入負圧、冷却水温等の諸条件
に基づいてアシストエアの流量を制御する。
The air passage 7 branches from a position upstream of the intake throttle valve 19 and downstream of the air flow meter 20, and allows air to flow according to the pressure difference (intake negative pressure) between the upstream and downstream sides of the intake throttle valve 19.
Note that the air flowing through the intake passage 21 and the air flowing through the air passage 7 meet downstream of the fuel injector 15, and all of these are measured by the air flow meter 2o, so the air-fuel ratio of the air-fuel mixture is equal to that of the assist air. Note that 22 is a valve that controls the flow rate of the air passage 7, and controls the flow rate of assist air based on various conditions such as engine speed, suction negative pressure, and cooling water temperature.

以上のように構成され、次に作用について説明すると、
燃料噴射ノズル2がらは機関回転数に同期して燃料が噴
射され、また、エアギヤラリ6がらは吸気ボート17に
作用する吸入負圧に応じて空気が吸引される。
The structure is as described above, and the operation will be explained as follows.
Fuel is injected from the fuel injection nozzle 2 in synchronization with the engine speed, and air is sucked from the air gear gallery 6 in accordance with the negative suction pressure acting on the intake boat 17.

噴射燃料は噴射プレート3の噴口4a、4bにより左右
に分離しつつ、所定の噴射角をもって吸気弁18(2つ
の吸気弁)に向けてそれぞれが円錐状に広がる。
The injected fuel is separated to the left and right by the injection ports 4a and 4b of the injection plate 3, and each spreads conically toward the intake valve 18 (two intake valves) at a predetermined injection angle.

これら噴口4a、4bを取り囲むように配置した主、副
空気噴口8a、8bと9a、9bからは高速のアシスト
エアが噴出する。このうち、主空気噴口8a、8bから
の噴出空気は、左右に分流した燃料噴霧の間に入り、両
噴霧を左右に分離しつつ、高速噴流により燃料の微粒化
、霧化を促進する。
High-speed assist air is ejected from main and sub-air nozzles 8a, 8b and 9a, 9b arranged to surround these nozzles 4a, 4b. Among them, the air ejected from the main air nozzles 8a and 8b enters between the left and right fuel sprays, and while separating the left and right sprays, the high-speed jets promote atomization and atomization of the fuel.

同時に副空気噴口9a、9bから、各燃料噴霧を燃料噴
射ノズル2の中心側から、噴霧角の広がりを抑制しつつ
、高速噴流により微粒化、霧化を促進するように、アシ
ストエアが噴出する。
At the same time, assist air is ejected from the auxiliary air nozzles 9a and 9b from the center side of the fuel injection nozzle 2 so as to suppress the spread of the spray angle and promote atomization and atomization with high-speed jets. .

燃料噴霧は噴射プレート3の噴口4m、4bを出てから
高速のアシストエアと衝突混合するので、燃料の微粒化
が良好で、しかも2つの燃料噴霧を確実に分離するよう
にアシストエアが導入されるので、均等な燃料噴霧が形
成される。
Since the fuel spray collides with high-speed assist air after exiting the nozzles 4m and 4b of the injection plate 3, the fuel is atomized well, and the assist air is introduced in such a way that the two fuel sprays are reliably separated. As a result, a uniform fuel spray is formed.

なお、吸入負圧か一500mm)Igのときの噴出空気
により、300μ−の燃料粒径が20〜30μmm程度
まで微粒化される。
Note that the fuel particle size of 300 μm is atomized to about 20 to 30 μm by the ejected air when the suction negative pressure is 500 mm) Ig.

これらの結果、吸気弁18から燃焼室に微粒化の進んだ
均質的な混合気が流入し、安定した良好な燃焼の実現が
図れる。
As a result, a highly atomized homogeneous air-fuel mixture flows into the combustion chamber from the intake valve 18, and stable and good combustion can be achieved.

なお、主空気噴口8a、8bや副空気噴口9a、9bの
直径や口数は、アシストエアの流量に応じて適正に設定
され、また、副空気噴口9m、9bのねじれ角φも、流
量に対応して適切に設定することができる。
The diameter and number of the main air nozzles 8a, 8b and the auxiliary air nozzles 9a, 9b are set appropriately according to the flow rate of the assist air, and the torsion angle φ of the auxiliary air nozzles 9m, 9b also corresponds to the flow rate. and set it properly.

第4図(A)(B)はそれぞれ主空気噴口8m、8bの
他の実施例を示すもので、2個づつ合計4個の主空気噴
口を、各一対が所定のねじれ角をもつよう対称的に配置
したり、あるいは、2個の主空気噴口8m、8bを燃料
噴霧と直交するように配置したものである。
Figures 4(A) and 4(B) show other embodiments of the main air nozzles 8m and 8b, respectively.The main air nozzles are arranged symmetrically so that each pair has a predetermined helix angle. Alternatively, the two main air nozzles 8m and 8b are arranged perpendicular to the fuel spray.

いずれも副空気噴口9a、9bは無いが、主空気噴口8
a、8bだけでも、最低法必要な燃料の微粒化性能は確
保される。
There are no sub-air nozzles 9a and 9b in either case, but the main air nozzle 8
Even with only a and 8b, the minimum required fuel atomization performance is ensured.

(発明の効果) 以上のように本発明によれば−、少なくとも2つに分流
した燃料噴霧に対して、その間に割り込むように高速の
アシストエアを噴出させるので、燃料噴霧が互いに交わ
るのを防止しつつ、燃料の微粒化、霧化を高めることが
でき、複数の吸気弁についても均等な混合気の供給が可
能となり、燃焼の改善が図れる。
(Effects of the Invention) As described above, according to the present invention, high-speed assist air is ejected to intersect at least two parts of the fuel spray, thereby preventing the fuel sprays from intersecting with each other. At the same time, the atomization and atomization of the fuel can be improved, and even air-fuel mixture can be supplied evenly to a plurality of intake valves, thereby improving combustion.

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

第1図は本発明の実施例を示す燃料噴射インジェクタの
断面図、第2図はそのA−A線断面図、第3図は吸気系
の全体的な断面図、第4図(A)(B)はそれぞれ他の
実施例を示す空気噴口の説明図である。 1・・・インジェクタ本体、2・・・燃料噴射ノズル、
3・・・噴射プレート、4a、4b・・・燃料噴口、5
・・・アダプタ、6・・・エアギヤラリ、8m、8b・
・・主空気噴口、9a、9b・・・副空気噴口。 特許出願人 日産自動車株式会社 第1図
Fig. 1 is a sectional view of a fuel injector showing an embodiment of the present invention, Fig. 2 is a sectional view taken along line A-A, Fig. 3 is an overall sectional view of the intake system, and Fig. 4 (A) ( B) is an explanatory diagram of an air jet port showing other embodiments. 1... Injector body, 2... Fuel injection nozzle,
3... Injection plate, 4a, 4b... Fuel nozzle, 5
...Adapter, 6...Air gear rally, 8m, 8b.
...Main air nozzle, 9a, 9b...Sub air nozzle. Patent applicant Nissan Motor Co., Ltd. Figure 1

Claims (1)

【特許請求の範囲】[Claims] 1. 噴口から噴射直後の燃料に高速空気を噴射する内
燃機関の燃料噴射装置において、少なくとも2つの異な
った方向に燃料を噴射する噴口と、各燃料噴霧を分離す
るようにその中間に空気を噴出させる空気噴口とを備え
ることを特徴する内燃機関の燃料噴射装置。
1. In a fuel injection device for an internal combustion engine that injects high-velocity air into fuel immediately after injection from a nozzle, a nozzle that injects fuel in at least two different directions and air that jets air between them to separate each fuel spray. A fuel injection device for an internal combustion engine, comprising: a nozzle;
JP15898990A 1990-06-18 1990-06-18 Fuel jet device for internal combustion engine Pending JPH0450472A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP15898990A JPH0450472A (en) 1990-06-18 1990-06-18 Fuel jet device for internal combustion engine
US07/709,605 US5129381A (en) 1990-06-18 1991-06-04 Fuel injection system for internal combustion engine
DE4119206A DE4119206C2 (en) 1990-06-18 1991-06-11 Fuel injection device for internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15898990A JPH0450472A (en) 1990-06-18 1990-06-18 Fuel jet device for internal combustion engine

Publications (1)

Publication Number Publication Date
JPH0450472A true JPH0450472A (en) 1992-02-19

Family

ID=15683788

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15898990A Pending JPH0450472A (en) 1990-06-18 1990-06-18 Fuel jet device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0450472A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04292573A (en) * 1991-03-20 1992-10-16 Hitachi Ltd Fuel injection valve
WO1994002736A1 (en) * 1992-07-16 1994-02-03 Unisia Jecs Corporation Fuel injection valve
US5666920A (en) * 1993-02-12 1997-09-16 Nippondenso Co., Ltd. Fuel supply system for use with internal combustion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04292573A (en) * 1991-03-20 1992-10-16 Hitachi Ltd Fuel injection valve
WO1994002736A1 (en) * 1992-07-16 1994-02-03 Unisia Jecs Corporation Fuel injection valve
US5499769A (en) * 1992-07-16 1996-03-19 Unisia Jecs Corporation Fuel injection valve including air promoting atomization
US5666920A (en) * 1993-02-12 1997-09-16 Nippondenso Co., Ltd. Fuel supply system for use with internal combustion engine

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