JPS5843669Y2 - fuel injection nozzle - Google Patents

fuel injection nozzle

Info

Publication number
JPS5843669Y2
JPS5843669Y2 JP7805678U JP7805678U JPS5843669Y2 JP S5843669 Y2 JPS5843669 Y2 JP S5843669Y2 JP 7805678 U JP7805678 U JP 7805678U JP 7805678 U JP7805678 U JP 7805678U JP S5843669 Y2 JPS5843669 Y2 JP S5843669Y2
Authority
JP
Japan
Prior art keywords
fuel injection
nozzle
spray
nozzle hole
injection nozzle
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
Application number
JP7805678U
Other languages
Japanese (ja)
Other versions
JPS54179320U (en
Inventor
洋明 中山
Original Assignee
日産デイ−ゼル工業株式会社
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 日産デイ−ゼル工業株式会社 filed Critical 日産デイ−ゼル工業株式会社
Priority to JP7805678U priority Critical patent/JPS5843669Y2/en
Publication of JPS54179320U publication Critical patent/JPS54179320U/ja
Application granted granted Critical
Publication of JPS5843669Y2 publication Critical patent/JPS5843669Y2/en
Expired legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は内燃機関用の燃料噴射ノズルの改良に関するも
のである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement of a fuel injection nozzle for an internal combustion engine.

内燃機関用の燃料噴射ノズルの噴射性能は機関の性能を
決定する。
The injection performance of a fuel injection nozzle for an internal combustion engine determines the performance of the engine.

すなわち、燃焼の良悪を左右する重要な要因である。In other words, it is an important factor that determines the quality of combustion.

特に直接噴射式における燃料噴射ノズル、いわゆるホー
ルノズルではその噴霧が燃焼を決定するといっても過言
ではないほどに重要である。
Particularly in direct injection type fuel injection nozzles, so-called hole nozzles, the spray is so important that it determines combustion.

周知のように燃焼を良くするには燃料と空気との混合を
良くすればよいのだが、ディーゼル機関のように混合す
る期間がきわめて短時間の場合は、いかに燃料粒を燃焼
室全体に一様に分布させるかが問題である。
As is well known, in order to improve combustion, it is necessary to improve the mixing of fuel and air, but when the mixing period is extremely short as in diesel engines, it is difficult to spread the fuel particles uniformly throughout the combustion chamber. The problem is how to distribute it.

ところで、従来より燃焼室の形状を変えたり、燃焼空気
に渦流を与えて混合を良くしようといろいろ試みられて
きたが、従来の燃料噴射ノズルの噴孔は円形であって、
噴霧の断面は円形となるために、どうしても燃料分布に
ムラがあり思うように燃焼改善はできなかった。
By the way, various attempts have been made to improve mixing by changing the shape of the combustion chamber or by creating a vortex in the combustion air, but the injection holes of conventional fuel injection nozzles are circular.
Since the cross section of the spray is circular, the fuel distribution is uneven and combustion cannot be improved as expected.

また近年加工技術、特に放電加工やレーザ加工等の進歩
により、従来ノズル噴孔の加工は円形に限られていたも
のが、従来不可能であった形状のものまで加工可能にな
ってきている。
Furthermore, with recent advances in processing technology, particularly electrical discharge machining, laser processing, etc., it has become possible to process nozzle holes, which were previously limited to circular shapes, to shapes that were previously impossible.

そして、そのような加工技術の進歩によりすでに長円等
の噴孔は考えられているが、しかしこの場合でも噴射さ
れた噴流は先へ行くにつれて1つにまとまる傾向をもつ
から結局略円形に近すいてしまい、均一の分布を得る効
果は十分にはえられなかった。
With the advancement of such processing technology, elongated nozzle holes have already been considered, but even in this case, the ejected jet tends to coalesce into one as it goes forward, so it ends up being approximately circular. As a result, the effect of obtaining uniform distribution could not be sufficiently achieved.

さて第1図イ2口は従来の直接噴射式の場合の噴霧A′
と燃焼室形状を、また第2図は渦流室式の場合の噴霧A
′の分布状態を示すが、いずれの場合も第1図イの「、
第2図の「で示す部分の空気が利用されにくくて燃焼状
態を悪くし、性能向上が計れず、またスモーク悪化の原
因にもなっていた。
Now, Fig. 1 A 2 ports are the spray A' in the case of the conventional direct injection type.
and the shape of the combustion chamber, and Figure 2 shows the spray A in the case of the swirl chamber type.
', but in any case, the distribution state of ',
The air in the area indicated by `` in Figure 2 was difficult to utilize, resulting in poor combustion conditions, making it impossible to improve performance, and causing smoke to worsen.

したがって本考案の目的は燃焼室内の広い範囲に亘って
実質的に一様に燃料を噴射できる燃料噴射ノズルを提供
するにある。
Accordingly, an object of the present invention is to provide a fuel injection nozzle that can inject fuel substantially uniformly over a wide range within a combustion chamber.

以下第3図ないし第5図を参照して本考案の実施例を説
明する。
Embodiments of the present invention will be described below with reference to FIGS. 3 to 5.

第3図は本考案に係るノズル先端部を示し、噴孔の形状
は、中央部分が細長1aで、両側を拡大1b、1bL、
たメガネ形となっている。
FIG. 3 shows the tip of the nozzle according to the present invention.
It is shaped like glasses.

そしてノズルNの中心軸Yに対して噴孔の長手方向の中
心軸Xを角度θをもって配置しである。
The central axis X in the longitudinal direction of the nozzle hole is arranged at an angle θ with respect to the central axis Y of the nozzle N.

通常噴孔はノズルの先端に複数個設けであるが、ここで
角度θとは噴孔を軸Y上に投影した場合の角度であり、
0°と90’との間の値である。
Usually, a plurality of nozzle holes are provided at the tip of the nozzle, and the angle θ here is the angle when the nozzle hole is projected onto the axis Y.
The value is between 0° and 90'.

この角度は燃焼室の構造やスワールの向きやその強弱等
により実験的経験的に設置され、よりよい燃焼作用が得
られる。
This angle is set experimentally and empirically depending on the structure of the combustion chamber, the direction of the swirl, its strength, etc., and better combustion action can be obtained.

第4図イは従来の円形噴孔1′による場合の噴霧A′を
口は従来の長円噴孔1“による場合の噴霧にをそれぞれ
示し、中心付近が一番貫通力が強く、燃料粒密度が濃く
なっている。
Figure 4A shows the spray A' when the conventional circular nozzle hole 1' is used, and the spray A' when the conventional oval nozzle hole 1'' is used.The penetrating force is strongest near the center, and the fuel particles It's getting denser.

円形噴孔1′や長円噴孔1“による場合は、前述のよう
に第1図イの「、第2図の「で示す部分の空気が利用さ
れにくくて燃焼状態が悪く、性能向上が計れず、またス
モークを悪化させる。
In the case of circular nozzle holes 1' and oval nozzle holes 1'', as mentioned above, the air in the areas indicated by ``A'' in Figure 1 and ``in Figure 2'' is difficult to utilize, resulting in poor combustion conditions and poor performance. It cannot be measured and also makes the smoke worse.

第4図ハは本考案のメガネ形噴孔1による場合の噴霧A
を示し、2つの拡大部1b、1bと細長部1aがあるこ
とにより従来の円形噴孔1′のように中心付近の貫通力
が強くなって、その部分の燃料粒密度だけが濃くなるこ
とがなく、図中噴霧Aの断面形状で示す如く、2つの中
心部とその間を結ぶ細長部により適当な噴霧のひろがり
を生じ燃料粒密度は噴霧A全体で一様となって、空気と
燃料の混合が一様に行われる。
Figure 4 (c) shows spray A when using the spectacle-shaped nozzle 1 of the present invention.
, because of the two enlarged parts 1b, 1b and the elongated part 1a, the penetrating force near the center becomes stronger and the density of fuel particles increases only in that part, as in the conventional circular nozzle hole 1'. Instead, as shown in the cross-sectional shape of spray A in the figure, the two central parts and the elongated part connecting them cause the spray to spread appropriately, and the fuel particle density becomes uniform throughout spray A, resulting in a mixture of air and fuel. is done uniformly.

第5図イはスワールSwが吸気管Sから流入する態様を
示している図中Pはピストン、Cは燃焼室である。
FIG. 5A shows the manner in which the swirl Sw flows in from the intake pipe S. In the figure, P is the piston and C is the combustion chamber.

そのために第5図口に示すように好ましい分布状態が得
られる。
Therefore, a preferable distribution state can be obtained as shown in the opening of FIG.

すなわち第5図口は本考案のメガネ形噴孔による場合の
燃焼室内における噴霧Aの分布状態を示し、B部分の空
気が従来の円形噴孔による場合に比べよく利用されてい
ることがわかる。
That is, the opening in FIG. 5 shows the distribution of spray A in the combustion chamber when the spectacle-shaped nozzle hole of the present invention is used, and it can be seen that the air in part B is utilized better than when the conventional circular nozzle hole is used.

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

第1図イ、酬ま従来の円形噴孔による場合の燃焼室内に
おける噴霧の分布状態を示し、イは平面図、口は断面図
である。 第2図は同じく他の形状の燃焼室内における噴霧の分布
状態を示す断面図である。 第3図は本考案に係る噴射弁先端部及びメガネ形噴孔の
平面図である。 第4図イ1口、ハは噴孔より噴射された噴霧の状態を示
し、イは従来の円形噴孔による場合を、口は従来の長円
噴孔による場合をハは本考案に係るメガネ形噴孔による
場合を示す。 第5図イは本考案に係るメガネ形噴孔による場合の燃焼
室の概略図、第5図口は燃焼室における噴霧の分布状態
を示す平面図である。 1・・・・・・メガネ形噴孔、1a・・・・・・噴孔の
細長い中央音医1b・・・・・・噴孔の両側の拡大部。
Figure 1A shows the distribution of spray in the combustion chamber when a conventional circular nozzle hole is used, where A is a plan view and the mouth is a sectional view. FIG. 2 is a sectional view showing the distribution of spray in a combustion chamber of another shape. FIG. 3 is a plan view of the tip of the injection valve and the spectacle-shaped nozzle hole according to the present invention. Fig. 4 A shows the state of the spray injected from the nozzle hole, A shows the state of the spray injected from the nozzle hole, A shows the case with the conventional circular nozzle hole, the mouth shows the case with the conventional oblong nozzle hole, and C shows the state of the spray according to the present invention. The case with a shaped nozzle hole is shown. FIG. 5A is a schematic diagram of a combustion chamber using a spectacle-shaped nozzle according to the present invention, and FIG. 5B is a plan view showing the distribution of spray in the combustion chamber. 1... Spectacle-shaped nozzle hole, 1a... Elongated central sound hole of the nozzle hole 1b... Enlarged portions on both sides of the nozzle hole.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 内燃機関の燃料噴射ノズルにおいて、燃料を燃焼室に噴
射する噴孔の形状を、中央部分が細長で両側を拡大した
メガネ形としかつ、噴孔の長手方向の中心軸を、燃料噴
射ノズルの中心軸に対して角度をもつようにしたことを
、特徴とする燃料噴射ノズル。
In a fuel injection nozzle for an internal combustion engine, the shape of the nozzle hole that injects fuel into the combustion chamber is a glasses shape with an elongated central part and enlarged sides, and the central axis in the longitudinal direction of the nozzle hole is the center of the fuel injection nozzle. A fuel injection nozzle characterized by having an angle with respect to the axis.
JP7805678U 1978-06-09 1978-06-09 fuel injection nozzle Expired JPS5843669Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7805678U JPS5843669Y2 (en) 1978-06-09 1978-06-09 fuel injection nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7805678U JPS5843669Y2 (en) 1978-06-09 1978-06-09 fuel injection nozzle

Publications (2)

Publication Number Publication Date
JPS54179320U JPS54179320U (en) 1979-12-18
JPS5843669Y2 true JPS5843669Y2 (en) 1983-10-03

Family

ID=28994795

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7805678U Expired JPS5843669Y2 (en) 1978-06-09 1978-06-09 fuel injection nozzle

Country Status (1)

Country Link
JP (1) JPS5843669Y2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58143163A (en) * 1982-02-17 1983-08-25 Isuzu Motors Ltd Fuel injection nozzle for engine
JPS58143164A (en) * 1982-02-17 1983-08-25 Isuzu Motors Ltd Fuel injection nozzle for engine
JPS58143162A (en) * 1982-02-17 1983-08-25 Isuzu Motors Ltd Fuel injection nozzle for diezel engine
JP6457797B2 (en) * 2014-11-26 2019-01-23 株式会社Soken Fuel injection nozzle

Also Published As

Publication number Publication date
JPS54179320U (en) 1979-12-18

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