JPS63189669A - Fuel injector for diesel engine - Google Patents
Fuel injector for diesel engineInfo
- Publication number
- JPS63189669A JPS63189669A JP2087887A JP2087887A JPS63189669A JP S63189669 A JPS63189669 A JP S63189669A JP 2087887 A JP2087887 A JP 2087887A JP 2087887 A JP2087887 A JP 2087887A JP S63189669 A JPS63189669 A JP S63189669A
- Authority
- JP
- Japan
- Prior art keywords
- passage
- fuel
- fuel injection
- injection nozzle
- 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.)
- Pending
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 60
- 238000002347 injection Methods 0.000 claims abstract description 46
- 239000007924 injection Substances 0.000 claims abstract description 46
- 238000002485 combustion reaction Methods 0.000 claims description 6
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 abstract description 20
- 239000007789 gas Substances 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Landscapes
- Fuel-Injection Apparatus (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は燃料噴射ノズルの噴射特性を改善して排ガス中
の窒素酸化物の低減および騒音の低減を図ったディーゼ
ルエンジンの燃料噴射装置に関するものである。Detailed Description of the Invention (Field of Industrial Application) The present invention relates to a fuel injection device for a diesel engine that improves the injection characteristics of a fuel injection nozzle to reduce nitrogen oxides in exhaust gas and noise. It is.
(従来技術)
この種の技術として従来はえ燃料噴射ノズル内の燃料供
給圧力の上昇に従ってニードルパルプとノズルシートと
の間に形成されるノズル開孔を流過して吐出される燃料
が該ニードルパルプのリフト量に伴い変化するディーゼ
ルエンジンの燃料噴射方法において、上記燃料はニード
ルパルプのリフ)13増大と共に初期状態で増加された
後、減少され、その後増量されて増大吐出量に達するよ
うにされたものがある。(特開昭59−190470号
公報)
つまり、ニードルパルプのリフト量によりノズル間孔面
積を変えて2段階の噴射特性をもたせたものであるが、
エンジンが高回転になるとニードルパルプのリフト量変
化が非常に早くなるためノズル開口面積が殆ど一様とな
り、上記のような2段階の噴射特性が得られなくなって
、窒素酸化物の低減などを期待出来な(なるという問題
があるまた、2つの燃料噴射ポンプにより位相をずらし
て燃料を供給することにより燃料噴射ノズルの噴射特性
の改善を図ることも考えられるが、複数の燃料噴射ポン
プが必要となるためコストアップとなる問題があった。(Prior Art) As a conventional technology of this kind, as the fuel supply pressure in the fly fuel injection nozzle increases, the fuel flows through the nozzle opening formed between the needle pulp and the nozzle seat and is discharged from the needle. In a diesel engine fuel injection method that changes with the lift amount of pulp, the fuel is increased in an initial state as the needle pulp lift (13) increases, then is decreased, and then increased to reach an increased discharge amount. There is something. (Japanese Unexamined Patent Publication No. 59-190470) In other words, the nozzle hole area is changed depending on the lift amount of the needle pulp to provide two-stage injection characteristics.
When the engine rotates at high speeds, the lift amount of the needle pulp changes very quickly, so the nozzle opening area becomes almost uniform, making it impossible to obtain the two-stage injection characteristics described above, which is expected to reduce nitrogen oxides. It is also possible to improve the injection characteristics of the fuel injection nozzle by supplying fuel out of phase with two fuel injection pumps, but this would require multiple fuel injection pumps. Therefore, there was a problem of increased costs.
(発明の目的)
本発明はエンジンの高回転域においても燃料噴射ノズル
の2段階の噴射特性が得られて窒素酸化物の低減などを
期待でき、また構造簡単で安価なディーゼルエンジンの
燃料噴射装置を提供することを目的とするものである。(Objective of the Invention) The present invention provides a fuel injection device for a diesel engine that can be expected to reduce nitrogen oxides by obtaining two-stage injection characteristics of the fuel injection nozzle even in the high rotational range of the engine, and that is simple in structure and inexpensive. The purpose is to provide the following.
(発明の構成)
上記の目的を達成するための本発明は、燃料噴射ポンプ
から燃焼室の燃料噴射ノズルに至る燃料供給通路におい
て、該燃料供給通路のうち少なくとも一部を径の大きい
第1通路と径の小さい第2通路とからなる並列通路とし
、かつ第1通路が第2通路よりも所定長さだけ長くされ
たものである(実施例)
以下図面にもとづいて本発明の詳細な説明する。(Structure of the Invention) To achieve the above object, the present invention provides that, in a fuel supply passage leading from a fuel injection pump to a fuel injection nozzle of a combustion chamber, at least a part of the fuel supply passage is connected to a first passage having a large diameter. and a second passage with a small diameter, and the first passage is made longer than the second passage by a predetermined length (Example) The present invention will be described in detail below based on the drawings. .
(1)は燃料噴射ポンプ、(2)は燃焼室の燃料噴射ノ
ズル、(3)は燃料噴射ポンプ(1)から燃料噴射ノズ
ル(2)に至り配設された燃料供給通路である。(1) is a fuel injection pump, (2) is a fuel injection nozzle in the combustion chamber, and (3) is a fuel supply passage arranged from the fuel injection pump (1) to the fuel injection nozzle (2).
燃料供給通路(3)は少なくとも一部に径の大きい第1
通路(4)と径の小さい第2通路(5)とからなる並列
通路を形成し、また第1通路(4)はU字状のベンド部
(4a)を有しており第2通路(5)よりも所定長さC
1)だけ長くなっている。The fuel supply passage (3) has at least a portion of the first passage having a large diameter.
A parallel passage consisting of a passage (4) and a second passage (5) with a small diameter is formed, and the first passage (4) has a U-shaped bend part (4a) and the second passage (5) has a U-shaped bend portion (4a). ) than the predetermined length C
1) is longer.
この所定長さC1>は噴射燃料が上記各通路(4)、
(5)内を圧力波として伝播する速度(V)およびエ
ンジンの希望回転数(n)における先行圧力波と遅行圧
力波との差の希望クランク角度(α)によって決定でき
る。This predetermined length C1> is such that the injected fuel is in each of the passages (4),
(5) It can be determined by the desired crank angle (α) of the difference between the leading pressure wave and the lagging pressure wave at the velocity (V) at which the pressure wave propagates in the engine and the desired engine speed (n).
たとえば、燃料が軽油の場合の伝播速度v−=1400
m/s、エンジンの希望回転数n=250Qrpm、希
望クランク角度α=2°とすると、また、主噴射となる
上記第1通路(4)の全噴射に対する燃料供給量の割合
は通路の径の大きさにより8周整できる。For example, when the fuel is light oil, the propagation velocity v-=1400
m/s, the desired engine speed n = 250 Qrpm, and the desired crank angle α = 2°. Also, the ratio of the fuel supply amount to the total injection of the first passage (4), which is the main injection, is determined by the diameter of the passage. Depending on the size, it can be trimmed 8 times.
次に燃料供給通路(3)の各部位での圧力波の動きをみ
ると、第1図に示すA、B、Cの各点における圧力波は
それぞれ第2.第3.第4図に示すグラフによって表さ
れる。Next, looking at the movement of pressure waves at each part of the fuel supply passage (3), the pressure waves at each point A, B, and C shown in FIG. Third. This is represented by the graph shown in FIG.
すなわち、燃料供給通路(3)のA点における圧力波は
通路が分岐する以前であるから第2図に示すように1つ
の大きい波形を表わし、B点では第3図に示すように通
路が分岐したのち燃料噴射ノズル(2)に入る直前の波
形が表わされ、符号(5)で示す通路長さの短い第2通
路(5)内の圧力波と符号(4)で示す長い第1通路(
4)内の圧力波とが重ねて示され後者の方が時間(1)
だけ遅れていることがわかる。ここで、この時間(1)
はノズルからの燃料噴射から着火までに要する時間に合
わせることが望ましい。That is, since the pressure wave at point A of the fuel supply passage (3) is before the passage branches, it shows one large waveform as shown in Fig. 2, and at point B, the passage branches as shown in Fig. 3. After that, the waveform immediately before entering the fuel injection nozzle (2) is shown, and the pressure wave in the second passage (5) with a short passage length (5) and the long first passage (4) are shown. (
The pressure waves in 4) are shown superimposed on each other, and the latter is shown to be faster at time (1).
I can see that you are late. Here, this time (1)
It is desirable to match the time required from fuel injection from the nozzle to ignition.
ノズル内の0点では第4図に示すように2つの圧力波が
重なり合って、初めに小さく後で大きい波形のいわゆる
2段階の噴射特性が示されているこのようなノズル内で
の圧力波に伴ない噴射率のグラフも第4図に示す圧力波
と略同様の波形のいわゆる後立ちとなるものである。At the 0 point inside the nozzle, two pressure waves overlap as shown in Figure 4, showing a so-called two-stage injection characteristic with a small waveform at first and a large waveform later. The graph of the accompanying injection rate also has a so-called trailing waveform that is substantially similar to the pressure wave shown in FIG.
これにより、第2通路(5)から供給さえる少量の燃料
によって着火が行われ、着火した燃料に時間(1)だけ
遅れて第1通路(4)から供給される多量の燃料によっ
て徐々に燃焼が進行する。As a result, ignition is performed by a small amount of fuel supplied from the second passage (5), and combustion is gradually started by a large amount of fuel supplied from the first passage (4) with a delay of time (1) after the ignited fuel. proceed.
従って爆発的な燃焼が起こらないので、高温高圧時に多
量に発生するNOX (窒素酸化物)の発生量が抑制さ
れると共に、燃焼室内の爆発に伴う騒音も低減される。Therefore, explosive combustion does not occur, so the amount of NOX (nitrogen oxides) that is generated in large quantities at high temperatures and high pressures is suppressed, and the noise associated with explosions within the combustion chamber is also reduced.
なお、第1図に示す場合は燃料供給通路(3)の略全域
に亘って並列通路が形成されているが、U字状のベンド
部(4a)の直前までを単一通路にしても燃料噴射ノズ
ル(2)へ入る前で第1゜第2通路(4)、 (5)
を合流させるようにして、もよい。In addition, in the case shown in Fig. 1, a parallel passage is formed over almost the entire area of the fuel supply passage (3), but even if the part just before the U-shaped bend part (4a) is made into a single passage, the fuel The first and second passages (4) and (5) before entering the injection nozzle (2).
It is good to have them merge.
(発明の効果)
本発明によれば燃料噴射ポンプから燃料、噴射ノズルに
至る燃料供給通路の少なくとも一部を長さ及び太さの異
なる2つの通路からなる並列通路としたものであるから
、エンジンの高回転域における燃料噴射ノズル内での供
給燃料の圧力波および噴射率が2段階の噴射特性を表わ
し、排ガス中の窒素酸化物の低減および騒音の低減が期
待できる。また従来のように燃料噴射ポンプやノズルに
ついて手を加えることがないため低コストで所期の目的
を達成できるものである。(Effects of the Invention) According to the present invention, at least a part of the fuel supply passage from the fuel injection pump to the fuel injection nozzle is formed into a parallel passage consisting of two passages having different lengths and thicknesses. The pressure waves and injection rate of the supplied fuel within the fuel injection nozzle in the high rotation range of the engine exhibit a two-stage injection characteristic, which can be expected to reduce nitrogen oxides in exhaust gas and noise. In addition, unlike conventional methods, there is no need to modify the fuel injection pump or nozzle, so the desired purpose can be achieved at low cost.
第1図は本発明に係るディーゼルエンジンの燃料噴射装
置の一実施例を示す説明図、第2図乃至第4図は燃料供
給通路の異なる各部位での供給燃料の圧力波のグラフを
示す図である。
(1) ・・燃料噴射ポンプ (2)・・燃料噴射ノ
ズル (3)・・燃料供給通路 (4)・・第1通路
(5)・・第2通路
特 許出願人 マツダ株式会社
代理人弁理士 三 原 隆
(外1名)
第1図
第2図 第3図 第4図FIG. 1 is an explanatory diagram showing one embodiment of the fuel injection device for a diesel engine according to the present invention, and FIGS. 2 to 4 are diagrams showing graphs of pressure waves of supplied fuel at different parts of the fuel supply passage. It is. (1) Fuel injection pump (2) Fuel injection nozzle (3) Fuel supply passage (4) First passage
(5)...Second Passage Patent Applicant: Takashi Mihara, Patent Attorney, Mazda Motor Corporation (1 other person) Figure 1 Figure 2 Figure 3 Figure 4
Claims (1)
供給通路において、該燃料供給通路のうち少なくとも一
部を径の大きい第1通路と径の小さい第2通路とからな
る並列通路とし、かつ第1通路が第2通路よりも所定長
さだけ長くされたことを特徴とするディーゼルエンジン
の燃料噴射装置。In the fuel supply passage leading from the fuel injection pump to the fuel injection nozzle of the combustion chamber, at least a part of the fuel supply passage is a parallel passage consisting of a first passage with a large diameter and a second passage with a small diameter, and A fuel injection device for a diesel engine, characterized in that a passage is longer than a second passage by a predetermined length.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2087887A JPS63189669A (en) | 1987-01-30 | 1987-01-30 | Fuel injector for diesel engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2087887A JPS63189669A (en) | 1987-01-30 | 1987-01-30 | Fuel injector for diesel engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63189669A true JPS63189669A (en) | 1988-08-05 |
Family
ID=12039445
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2087887A Pending JPS63189669A (en) | 1987-01-30 | 1987-01-30 | Fuel injector for diesel engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63189669A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2776701A1 (en) * | 2011-11-07 | 2014-09-17 | Liebherr-Machines Bulle SA | Injection system |
-
1987
- 1987-01-30 JP JP2087887A patent/JPS63189669A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2776701A1 (en) * | 2011-11-07 | 2014-09-17 | Liebherr-Machines Bulle SA | Injection system |
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