JPS6327093Y2 - - Google Patents

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Publication number
JPS6327093Y2
JPS6327093Y2 JP1982025820U JP2582082U JPS6327093Y2 JP S6327093 Y2 JPS6327093 Y2 JP S6327093Y2 JP 1982025820 U JP1982025820 U JP 1982025820U JP 2582082 U JP2582082 U JP 2582082U JP S6327093 Y2 JPS6327093 Y2 JP S6327093Y2
Authority
JP
Japan
Prior art keywords
fuel
fuel injection
engine
needle valve
detection means
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
JP1982025820U
Other languages
Japanese (ja)
Other versions
JPS58130081U (en
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 filed Critical
Priority to JP2582082U priority Critical patent/JPS58130081U/en
Publication of JPS58130081U publication Critical patent/JPS58130081U/en
Application granted granted Critical
Publication of JPS6327093Y2 publication Critical patent/JPS6327093Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は内燃機関の燃料噴射装置に関する。[Detailed explanation of the idea] The present invention relates to a fuel injection device for an internal combustion engine.

例えばデイーゼル機関等のように燃焼室内に燃
料を噴射する内燃機関では、スワール強さと燃料
噴射ノズルの噴口数が燃料噴霧と吸入空気の混合
に大きく影響し、噴口数が多い場合はスワールを
小さくし噴口数が少ない場合はスワールを強化す
るのが良好な混合を得られ燃焼性を良好にするの
に好ましい。
For example, in internal combustion engines such as diesel engines that inject fuel into the combustion chamber, the swirl strength and the number of nozzles in the fuel injection nozzle greatly affect the mixing of the fuel spray and intake air. When the number of nozzles is small, it is preferable to strengthen the swirl in order to obtain good mixing and improve combustibility.

ところが、スワールの強さは機関回転速度全域
に亘つて一定ではなく機関回転速度の上昇に伴つ
て強くなる傾向にあるので、低・中・高のいずれ
かの機関回転域にスワール量を合せば、他の機関
回転域でマツチングできない。例えば、機関中回
転域でマツチングをとると、高回転域ではスワー
ルが強過ぎて噴霧燃料が重なつてしまい逆に低回
転域ではスワールが弱く充分に噴霧燃料が拡散せ
ずいずれも最適な燃焼が得られなかつた。
However, the strength of the swirl is not constant over the entire engine speed range, but tends to become stronger as the engine speed increases, so if you adjust the swirl amount to one of the low, medium, and high engine speed ranges, , matching is not possible in other engine speed ranges. For example, if matching is done in the middle engine speed range, the swirl will be too strong in the high speed range and the sprayed fuel will overlap, while in the low speed range the swirl will be weak and the sprayed fuel will not be sufficiently diffused, resulting in optimal combustion. was not obtained.

このため機関回転速度に応じてスワール量を変
え全回転域で最適なスワールが得られるようにし
た可変スワール機構等が提案されている(実公昭
51−7365号等)が、この場合、吸気通路の絞り装
置により空気の充填効率の低下を招き出力損失を
生じるばかりか、装置が複雑となり実用化が難し
いという問題があつた。また、異なる設定圧の複
数個の針弁と同数の群に形成され、それぞれ対応
する針弁のリフトのみにより燃料を噴射する複数
個の噴口群を備えた噴射ノズルが提案されている
(実開昭51−582165号等)。
For this reason, variable swirl mechanisms have been proposed that change the amount of swirl according to the engine speed to obtain the optimum swirl over the entire rotation range (Jikkosho).
No. 51-7365, etc.), but in this case, the throttle device in the intake passage not only reduces the air filling efficiency and causes output loss, but also makes the device complicated and difficult to put into practical use. In addition, an injection nozzle has been proposed that has a plurality of needle valves with different set pressures and a plurality of nozzle groups that inject fuel only by the lift of the corresponding needle valves. (Sho 51-582165, etc.)

本考案は異なる燃料噴射口が針弁を介して連通
する2つの燃料通路を有する燃料噴射ノズルを機
関燃焼室に臨設し、機関低回転時には燃料噴射口
の多い燃料通路側に、機関中・高回転時には燃料
噴射口の少ない燃料通路側に、それぞれ燃料を切
り換え供給し、実質的に噴口数を可変とすること
により、従来の問題点を解消することを目的とす
る。
In this invention, a fuel injection nozzle having two fuel passages in which different fuel injection openings communicate through a needle valve is installed in the engine combustion chamber, and when the engine is running at low speeds, the fuel injection nozzle with many fuel injection openings is placed on the side of the fuel passage where there are many fuel injection openings. The purpose of this invention is to solve the conventional problems by switching and supplying fuel to the fuel passage side where there are fewer fuel injection ports during rotation, thereby making the number of injection ports substantially variable.

以下、本考案の実施例を図面に基づいて詳細に
説明する。
Hereinafter, embodiments of the present invention will be described in detail based on the drawings.

第1図において、1はシリンダヘツド、2はシ
リンダブロツク、3はピストン、4は燃焼室であ
る。5は燃焼室4に臨設した燃料噴射ノズルで、
燃料噴射ポンプ6から供給された燃料を燃焼室4
内に噴射する。前記噴射ノズル5の構成について
は後で詳述する。7は機関回転速度を検出して出
力する機関回転速度検出手段としての回転速度セ
ンサで、このセンサ7からの出力によつて燃料供
給切換手段としての切換弁8を切換操作し噴射ノ
ズル5に設けた2つの燃料通路の一方を燃料噴射
ポンプ6に連通するようになつている。
In FIG. 1, 1 is a cylinder head, 2 is a cylinder block, 3 is a piston, and 4 is a combustion chamber. 5 is a fuel injection nozzle installed in the combustion chamber 4;
Fuel supplied from the fuel injection pump 6 is supplied to the combustion chamber 4.
Inject inside. The configuration of the injection nozzle 5 will be explained in detail later. Reference numeral 7 denotes a rotation speed sensor as an engine rotation speed detection means for detecting and outputting the engine rotation speed, and the output from this sensor 7 switches a switching valve 8 as a fuel supply switching means, which is installed in the injection nozzle 5. One of the two fuel passages is connected to a fuel injection pump 6.

前記燃料噴射ノズル5の構成を第2図及び第3
図に基づいて説明する。
The structure of the fuel injection nozzle 5 is shown in FIGS. 2 and 3.
This will be explained based on the diagram.

図において、燃料噴射ノズル5のノズルホルダ
11とノズルボデイ12はノズルナツト13によ
つて一体に締付固定されている。ノズルボデイ1
2の先端には複数の燃料噴射口14が形成されて
おり、該噴射口14の配置は第3図Bに示す如く
ノズルボデイ12の軸心を中心とする内外2つの
同心円上に設けられ、内側には4つ、外側には5
つの噴射口14が略等間隔に位置している。そし
て、ノズルホルダ11及びノズルボデイ12の内
部に前記外側の5つの噴射口14Aを開閉する第
1針弁15が嵌挿され、この第1針弁15に前記
内側の噴射口14Bを開閉する第2針弁16が嵌
挿されている。
In the figure, a nozzle holder 11 and a nozzle body 12 of a fuel injection nozzle 5 are tightened and fixed together by a nozzle nut 13. Nozzle body 1
A plurality of fuel injection ports 14 are formed at the tip of the nozzle body 12. As shown in FIG. 4 on the outside, 5 on the outside
The two injection ports 14 are located at approximately equal intervals. A first needle valve 15 that opens and closes the five outer injection ports 14A is fitted into the nozzle holder 11 and nozzle body 12, and a second needle valve 15 that opens and closes the inner injection ports 14B is inserted into the first needle valve 15. A needle valve 16 is inserted.

一方、ノズルホルダ11の上端部には、上下に
凹部17A,17Bが設けられた第1アジヤスト
スクリユ17が螺合している。このアジヤストス
クリユ17の下部凹部17B内壁と第1針弁15
の頂壁との間に第1スプリング18が介装され第
1針弁15を常時閉弁方向に付勢している。また
第1アジヤストスクリユ17の上部凹部17Aに
は第2アジヤストスクリユ19が螺合し、ナツト
20により固定されている。前記第1及び第2ア
ジヤストスクリユ17,19を貫通する第2針弁
16の上部外周にはスプリングシート21が嵌合
しており、このスプリングシート21と第2アジ
ヤストスクリユ19頂部内壁に固定したスプリン
グシート22との間に第2スプリング23が介装
され第2針弁16を常時閉弁方向に付勢してい
る。尚、第2針弁16外周には前記スプリングシ
ート21を係止する係止部をなすリング状部材2
4が第2針弁16と一体に取り付けられている。
On the other hand, a first adjuster screw 17 having upper and lower recesses 17A and 17B is screwed into the upper end of the nozzle holder 11. The inner wall of the lower recess 17B of the adjusting screw 17 and the first needle valve 15
A first spring 18 is interposed between the first needle valve 15 and the top wall of the first needle valve 15 to always bias the first needle valve 15 in the valve closing direction. Further, a second adjusting screw 19 is screwed into the upper recessed portion 17A of the first adjusting screw 17 and fixed with a nut 20. A spring seat 21 is fitted to the upper outer periphery of the second needle valve 16 that passes through the first and second adjusting screws 17 and 19, and the spring seat 21 and the inner wall of the top of the second adjusting screw 19 are fitted. A second spring 23 is interposed between the second needle valve 16 and a spring seat 22 fixed to the second needle valve 16 to always bias the second needle valve 16 in the valve closing direction. Incidentally, on the outer periphery of the second needle valve 16, there is a ring-shaped member 2 that forms a locking portion for locking the spring seat 21.
4 is integrally attached to the second needle valve 16.

また、ノズルホルダ11には第1及び第2の2
つの燃料導入口25,26が形成され、第1燃料
導入口25はノズルホルダ11及びノズルボデイ
12を通して形成された第1燃料通路27を介し
て第3図Aに示す第1針弁15とノズルボデイ1
2との間の燃料溜り28に連通し、更に、この燃
料溜り28から燃料通路31及び第1針弁15を
介して外側の燃料噴射口14Aに連通する。一
方、第2燃料導入口26は燃料通路29を介して
第3図Aに示すように第1針弁15と第2針弁1
6との間の燃料溜り30に連通し、この燃料溜り
30から燃料通路32及び第2針弁16を介して
内側の燃料噴射口14Bに連通する。
Further, the nozzle holder 11 has a first and a second two.
Two fuel inlet ports 25 and 26 are formed, and the first fuel inlet port 25 connects the first needle valve 15 and the nozzle body 1 shown in FIG.
This fuel reservoir 28 communicates with the outer fuel injection port 14A via the fuel passage 31 and the first needle valve 15. On the other hand, the second fuel inlet 26 is connected to the first needle valve 15 and the second needle valve 1 through a fuel passage 29 as shown in FIG. 3A.
The fuel reservoir 30 communicates with the inner fuel injection port 14B via the fuel passage 32 and the second needle valve 16.

次に作用を説明する。 Next, the effect will be explained.

機関回転速度が低速時には、回転速度センサ7
がこれを検出して出力し、この出力によつて切換
弁8が駆動して燃料噴射ポンプ6と燃料噴射ノズ
ル5の第1燃料導入口25とを連通する。これに
より、噴射ポンプ6からの燃料は第1燃料導入口
25を介して燃料噴射ノズル5内へ供給され、燃
料通路27を介して燃料溜り28へ導かれる。こ
の燃料溜り28内の燃料圧力が第1スプリング1
8のセツト荷重以上になると第1針弁15が第1
スプリング18に抗して上動し、外側の5つの燃
料噴射口14Aから燃焼室4内に燃料を噴射す
る。
When the engine rotation speed is low, the rotation speed sensor 7
detects this and outputs it, and this output drives the switching valve 8 to communicate the fuel injection pump 6 and the first fuel inlet 25 of the fuel injection nozzle 5. Thereby, fuel from the injection pump 6 is supplied into the fuel injection nozzle 5 via the first fuel inlet 25 and guided to the fuel reservoir 28 via the fuel passage 27. The fuel pressure in this fuel reservoir 28 is the first spring 1
When the load exceeds the set load of 8, the first needle valve 15
It moves upward against the spring 18 and injects fuel into the combustion chamber 4 from the five outer fuel injection ports 14A.

一方、機関回転速度が中・高速になると、回転
速度センサ7からの出力によつて切換弁8が切換
わり、燃料噴射ポンプ6と第2燃料導入口26と
を連通する。このため、噴射ポンプ6からの燃料
は第2燃料導入口26を介して燃料噴射ノズル5
へ供給される。第2燃料導入口26から供給され
た燃料は燃料通路29を介して第1針弁15と第
2針弁16との間の燃料溜り30へ導入される。
この燃料溜り30内の燃料圧力が第2スプリング
23のセツト荷重以上に達すると、第2針弁16
が第2スプリング23に抗して上動し内側の4つ
の燃料噴射口14Bから燃焼室4内に燃料が噴射
される。
On the other hand, when the engine rotational speed becomes medium or high, the switching valve 8 is switched according to the output from the rotational speed sensor 7, and the fuel injection pump 6 and the second fuel inlet 26 are communicated with each other. Therefore, the fuel from the injection pump 6 passes through the second fuel inlet 26 to the fuel injection nozzle 5.
supplied to Fuel supplied from the second fuel inlet 26 is introduced into a fuel reservoir 30 between the first needle valve 15 and the second needle valve 16 via the fuel passage 29.
When the fuel pressure in this fuel reservoir 30 reaches the set load of the second spring 23 or more, the second needle valve 16
moves upward against the second spring 23, and fuel is injected into the combustion chamber 4 from the four inner fuel injection ports 14B.

このようにスワールの弱い機関低速時には、多
くの噴射口から燃料を噴射させてスワールの不足
を補い噴霧燃料を拡散し易くしているので燃料と
空気との混合が良好となり、良好な燃焼が得られ
る。一方、機関高速時のようにスワールが強過ぎ
る時には、燃料を噴射する噴射口を少なくして噴
霧燃料の重なりを少なくし効率良く燃料を拡散さ
せるので、良好な燃焼が得られる。更に、吸気系
の通路断面積を絞る必要がないので、空気充填効
率を損なうことはなく充分な空気量を確保するこ
とができることは言うまでもない。
In this way, at low engine speeds with weak swirl, fuel is injected from many injection ports to compensate for the lack of swirl and make it easier to spread the atomized fuel, resulting in better mixing of fuel and air, resulting in better combustion. It will be done. On the other hand, when the swirl is too strong, such as when the engine is running at high speed, the number of injection ports for injecting fuel is reduced to reduce the overlap of the atomized fuel and efficiently diffuse the fuel, resulting in good combustion. Furthermore, since there is no need to reduce the cross-sectional area of the passage in the intake system, it goes without saying that a sufficient amount of air can be secured without impairing air filling efficiency.

尚、燃料噴射口の数は本実施例のものに限定さ
れるものではない。
Note that the number of fuel injection ports is not limited to that of this embodiment.

以上述べたように本考案によれば、機関回転速
度に応じて燃料噴射ノズルの実質的な噴射口数を
可変とし、低速時には中・高速時よりも多い噴射
口から燃料を噴射するよう構成したので、低速時
スワールが弱い場合でも噴霧燃料の拡散が充分と
なり良好な燃焼を得ることができる。従つて、ス
ワールを強化するために絞り装置を設ける必要も
なく空気充填効率を損なうことなく機関の全回転
速度域において最適な燃焼を得ることができる。
As described above, according to the present invention, the actual number of injection ports of the fuel injection nozzle is made variable according to the engine rotation speed, and fuel is injected from more injection ports at low speeds than at medium and high speeds. Even when the swirl is weak at low speeds, the atomized fuel can be sufficiently diffused and good combustion can be achieved. Therefore, there is no need to provide a throttling device to enhance swirl, and optimum combustion can be obtained in the entire rotational speed range of the engine without impairing air filling efficiency.

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

第1図は本考案の1実施例を示す簡略構成図、
第2図は燃料噴射ノズルの一部断面構成図、第3
図Aは第2図のノズルの先端を示す拡大断面図、
第3図BはA図中のA矢視図である。 5……燃料噴射ノズル、6……燃料噴射ポン
プ、7……回転速度センサ、8……切換弁、14
……燃料噴射口、15……第1針弁、16……第
2針弁、25……第1燃料導入口、26……第2
燃料導入口、27,29……燃料通路。
FIG. 1 is a simplified configuration diagram showing one embodiment of the present invention;
Figure 2 is a partial cross-sectional configuration diagram of the fuel injection nozzle;
Figure A is an enlarged sectional view showing the tip of the nozzle in Figure 2;
FIG. 3B is a view taken along arrow A in FIG. 5...Fuel injection nozzle, 6...Fuel injection pump, 7...Rotational speed sensor, 8...Switching valve, 14
...Fuel injection port, 15...First needle valve, 16...Second needle valve, 25...First fuel inlet, 26...Second
Fuel inlet, 27, 29... fuel passage.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 異なる数の燃料噴射口が針弁を介して連通する
2つの燃料通路を有し機関燃焼室に臨設された燃
料噴射ノズルと、機関回転速度を検出して出力す
る機関回転速度検出手段と、燃料噴射ポンプから
燃料を供給する燃料通路を前記検出手段の出力に
応じて切り換える燃料供給切換手段と、を備え、
前記切換手段によつて、前記検出手段が機関低回
転速度を検出した時に燃料噴射口の多い燃料通路
側に切り換え、前記検出手段が機関中・高回転速
度を検出した時に燃料噴射口の少ない燃料通路側
に切り換える構成としたことを特徴とする内燃機
関の燃料噴射装置。
a fuel injection nozzle provided in an engine combustion chamber and having two fuel passages through which different numbers of fuel injection ports communicate via needle valves; an engine rotation speed detection means for detecting and outputting an engine rotation speed; a fuel supply switching means for switching a fuel passage through which fuel is supplied from the injection pump according to the output of the detection means;
The switching means switches to the fuel passage side with many fuel injection ports when the detection means detects a low engine speed, and switches to the fuel passage side with fewer fuel injection ports when the detection means detects a middle/high engine speed. A fuel injection device for an internal combustion engine, characterized in that the fuel injection device is configured to switch to the passage side.
JP2582082U 1982-02-26 1982-02-26 Internal combustion engine fuel injection system Granted JPS58130081U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2582082U JPS58130081U (en) 1982-02-26 1982-02-26 Internal combustion engine fuel injection system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2582082U JPS58130081U (en) 1982-02-26 1982-02-26 Internal combustion engine fuel injection system

Publications (2)

Publication Number Publication Date
JPS58130081U JPS58130081U (en) 1983-09-02
JPS6327093Y2 true JPS6327093Y2 (en) 1988-07-22

Family

ID=30037782

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2582082U Granted JPS58130081U (en) 1982-02-26 1982-02-26 Internal combustion engine fuel injection system

Country Status (1)

Country Link
JP (1) JPS58130081U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2750715B2 (en) * 1988-12-12 1998-05-13 株式会社ゼクセル Fuel injection nozzle

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5447028A (en) * 1977-09-01 1979-04-13 Sulzer Ag Jet valve for reciprocating internal combustion engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5447028A (en) * 1977-09-01 1979-04-13 Sulzer Ag Jet valve for reciprocating internal combustion engine

Also Published As

Publication number Publication date
JPS58130081U (en) 1983-09-02

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