JPS63167068A - Advancer for accumulator type fuel injection device - Google Patents

Advancer for accumulator type fuel injection device

Info

Publication number
JPS63167068A
JPS63167068A JP61216901A JP21690186A JPS63167068A JP S63167068 A JPS63167068 A JP S63167068A JP 61216901 A JP61216901 A JP 61216901A JP 21690186 A JP21690186 A JP 21690186A JP S63167068 A JPS63167068 A JP S63167068A
Authority
JP
Japan
Prior art keywords
valve
chamber
pressure
closing
opening
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
JP61216901A
Other languages
Japanese (ja)
Inventor
Masahiro Yamashita
昌宏 山下
Satoshi Torii
鳥井 怜
Masahiro Akeda
正寛 明田
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.)
Kubota Corp
Original Assignee
Kubota Corp
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 Kubota Corp filed Critical Kubota Corp
Priority to JP61216901A priority Critical patent/JPS63167068A/en
Priority to US07/095,459 priority patent/US4807811A/en
Publication of JPS63167068A publication Critical patent/JPS63167068A/en
Pending legal-status Critical Current

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  • High-Pressure Fuel Injection Pump Control (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE:To make it possible to accurately control fuel injection time by connecting a valve closing pressure chamber partitioned by piston united with a needle valve to a suction pump through an opening/closing valve and making it possible to adjust the opening time of the opening/closing valve by a timer mechanism, according to the revolution number of an engine. CONSTITUTION:An accumulator type fuel injection device has a needle valve 3 stored freely in advancement and retreat inside an injection tube 2 and is provided with an accumulation chamber 6 on the injection port 1 side and a valve opening pressure chamber 5 on the opposite side to the injection port 1 by piston 4 formed at the valve axis of this needle valve 3, respectively. The valve opening pressure chamber 5 is connected, through a communication passage, to an injection pump chamber 9 which is pressurized by the operation of a plunger 10. In this case, the valve closing pressure chamber 5 is connected to a suction pump (both are omitted from Fig.) through an opening/closing valve which is adjustable of the starting time to open the valve by timer mechanism according to the revolution number of an engine. And the needle valve 3 is controlled to be opened by lowering the internal pressure of the valve closing pressure chamber 5 with the opening of the opening/closing valve.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、蓄圧式燃料噴射装置の進角装置に関゛し、特
に、簡単な構成で、燃料噴射時期を正確に制御でき、し
かも、小型化を図る上で有利になるようにした蓄圧式燃
料噴射装置の進角装置に関する。
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to an advance device for an accumulator fuel injection device, and in particular, it has a simple configuration, can accurately control the fuel injection timing, and has the following features: The present invention relates to an advance angle device for a pressure accumulation type fuel injection device that is advantageous in achieving downsizing.

また、この発明が適用される蓄圧式燃料噴射装置は、例
えば第3図に示すように、本体B内に形成された燃料通
路の終端部に該燃料通路を開閉する噴射弁3を設けると
ともに、その途中に逆流を防止する逆止弁8を介在させ
て上記噴射弁3と逆止弁8との間に蓄圧室を形成し、逆
止弁8の上流に噴射ポンプ室9とこの噴射ポンプ室9へ
の吸入路11を断続する入口弁12とを存する燃料噴射
装置である。この種の燃料噴射装置はユニットインジェ
クタとして噴射ポンプ室を1個の本体B内に組み合わせ
ることが多いが、これに限定されるわけではなく、例え
ば、本体Bとは別に噴射ポンプ室9等のポンプ部分を設
け、これらを配管で接続することも可能である。
Further, the pressure accumulation type fuel injection device to which the present invention is applied includes, for example, as shown in FIG. A check valve 8 for preventing backflow is interposed in the middle to form a pressure accumulation chamber between the injection valve 3 and the check valve 8, and an injection pump chamber 9 is formed upstream of the check valve 8. This fuel injection device includes an inlet valve 12 that connects and disconnects an intake passage 11 to the fuel injection device 9. This type of fuel injection device often combines an injection pump chamber into one main body B as a unit injector, but the invention is not limited to this. It is also possible to provide sections and connect them with piping.

〈従来技術〉 従来、蓄圧式噴射装置の進角装置としては、例えば、特
開昭49−70031号公報に開示されたものがある。
<Prior Art> Conventionally, as an advance device for a pressure accumulation type injection device, there is one disclosed in, for example, Japanese Unexamined Patent Publication No. 49-70031.

この従来の蓄圧式噴射装置の進角装置は第13図に示す
ように、エンジン已に回転可能に支持させた偏心軸16
にカムフォロア16°を揺動可能に支持させ、エンジン
回転数に対応して偏心軸16の位相を変化させることに
より燃料カム17にカムフォロア16′が当接される位
置を変化させて噴射時期を調節できるようにしである。
As shown in FIG. 13, the advance angle device of this conventional pressure accumulator type injection device has an eccentric shaft 16 which is rotatably supported on the side of the engine.
The cam follower 16' is swingably supported by the engine, and the phase of the eccentric shaft 16 is changed in accordance with the engine speed to change the position where the cam follower 16' contacts the fuel cam 17, thereby adjusting the injection timing. It is possible to do so.

ノズルNと一体に組立られた噴射ポンプPは、カムフォ
ロア16°にブツシュロッド18及びロッカーアーム1
9を介して連動させである。
The injection pump P, which is assembled integrally with the nozzle N, has a bushing rod 18 and a rocker arm 1 at a cam follower 16°.
It is linked via 9.

この従来の蓄圧式噴射装置の進角装置では、噴射ポンプ
Pのプランジャが上昇する時期を変更することによって
逆止弁の上流側の減圧開始のタイミングを調節して噴射
開始時期が調整される。
In this conventional advance device for a pressure accumulation type injection device, the injection start timing is adjusted by changing the timing at which the plunger of the injection pump P rises to adjust the timing at which pressure reduction starts on the upstream side of the check valve.

〈発明が解決しようとする問題点) このような従来の蓄圧式噴射装置の進角装置では、偏心
軸16の位相がエンジン回転数に対応して正逆両方向に
変化されるのが通例である。この偏心軸16の軌跡は所
定の円弧を描き、従って、カムフォロア16°の移動量
は偏心軸2の位相変化に対して正弦的に変化し、エンジ
ン回転数に対して噴射時期をリニアに変化させるために
は、更にカムフォロア16°の位置変化を偏心軸16の
位相変化にリニアに対応させるような補正機構を設ける
必要があるが、このような補正機構を付加することは構
造が複雑になるうえ、大型になる。
(Problems to be Solved by the Invention) In the advance angle device of such a conventional pressure accumulation type injection device, the phase of the eccentric shaft 16 is usually changed in both forward and reverse directions in accordance with the engine rotation speed. . The locus of this eccentric shaft 16 draws a predetermined circular arc, so the amount of movement of the cam follower 16° changes sinusoidally with respect to the phase change of the eccentric shaft 2, and the injection timing changes linearly with respect to the engine rotation speed. In order to achieve this, it is necessary to provide a correction mechanism that linearly corresponds the 16° position change of the cam follower to the phase change of the eccentric shaft 16, but adding such a correction mechanism would complicate the structure and , becomes large.

また、上記のようにブツシュロッド18を介在させる場
合には、カムフォロア16′の位置変化に伴ってブツシ
ュロッド18の傾斜が変化し、ブツシュロッド18とロ
ッカーアーム19との間のクリアランスが変化する。こ
のために、打撃音が発生したり、ロッカーアーム19が
振動したりするうえ、摩耗が進行し易くなり、耐久性を
向上させるうえで不利になるとともに、エンジンの高速
化を図るうえでも不利になる。
Further, when the bushing rod 18 is interposed as described above, the inclination of the bushing rod 18 changes as the position of the cam follower 16' changes, and the clearance between the bushing rod 18 and the rocker arm 19 changes. For this reason, impact noise is generated, the rocker arm 19 vibrates, and wear progresses more easily, which is disadvantageous in terms of improving durability and also disadvantageous in increasing the speed of the engine. Become.

更に、偏心軸16にカムフォロア16を連結させるため
に、カムフォロア16°の基端部を2つ割に形成して、
ボルト等を使用して結合する必要があるので、カムフォ
ロア16′の基端部の構造が不利になる等の問題もある
Furthermore, in order to connect the cam follower 16 to the eccentric shaft 16, the base end of the cam follower 16° is split into two parts.
Since it is necessary to connect using bolts or the like, there are also problems such as disadvantageous structure of the base end of the cam follower 16'.

本発明は、上記の事情を考慮してなされたものであって
、簡単な構成で、燃料噴射時期を正確に制御でき、しか
も、小型化を図る上で有利になるようにした蓄圧式燃料
噴射装置の進角装置を提供することを目的とするもので
ある。
The present invention has been made in consideration of the above circumstances, and is a pressure accumulating fuel injection system that has a simple configuration, can accurately control fuel injection timing, and is advantageous in terms of downsizing. The object of the present invention is to provide an advance angle device for a device.

く問題点を解決するための手段〉 本発明に係る蓄圧式燃料噴射装置の進角装置は、上記の
目的を達成するために、本体内に形成された燃料通路の
終端部に該燃料通路を開閉する噴射弁を設けるとともに
、その途中に逆流を防止する逆止弁を介在させて上記噴
射弁と逆止弁との間に蓄圧室を形成し、逆止弁の上流に
噴射ポンプ室とこの噴射ポンプ室への吸入路を断続する
入口弁とを有する燃料噴射装置の進角装置であって、上
記逆止弁の上流側に上記噴射弁にこれを閉弁方向に付勢
する圧力を作用させるための閉弁圧力室を設け、この閉
弁圧力室に開閉弁を介して吸出ポンプを接続すると共に
、エンジン回転数に対応して上記開閉弁の開弁開始時期
を調整するタイマ機構とを設けたことを特徴とする。
Means for Solving the Problems> In order to achieve the above object, the advance device for a pressure accumulator fuel injection device according to the present invention includes a fuel passage formed in the main body at the terminal end of the fuel passage. In addition to providing an injection valve that opens and closes, a check valve that prevents backflow is interposed in the middle to form a pressure accumulation chamber between the injection valve and the check valve, and an injection pump chamber and this pressure accumulation chamber are provided upstream of the check valve. An advance device for a fuel injection device having an inlet valve that connects and disconnects a suction path to an injection pump chamber, wherein pressure is applied to the upstream side of the check valve to bias the injection valve in the closing direction. A suction pump is connected to the closing pressure chamber via an opening/closing valve, and a timer mechanism is provided to adjust the opening timing of the opening/closing valve in accordance with the engine speed. It is characterized by having been established.

閉弁圧力室と開閉弁とは逆止弁の上流側の上記燃料通路
の部分とは別の通路で接続することも可能であるが、閉
弁圧力室と開閉弁とを上記燃料通路の部分、噴射ポンプ
室及び入口弁を介して接続する方が構造を簡単にでき、
しかも、コンパクトにできるので有利である。
Although it is possible to connect the closing pressure chamber and the opening/closing valve through a passage separate from the part of the fuel passage on the upstream side of the check valve, , connecting via the injection pump chamber and inlet valve makes the structure simpler;
Moreover, it is advantageous because it can be made compact.

この場合、入口弁の上流に燃料供給回路と吸出ポンプと
を切換え接続する切換弁を設ける必要があるが、この切
換弁を開閉弁に兼用することができるので、部品点数を
増加させずにすむので有利である。この切換弁は、一つ
の切換通路を有するローフを回転させるようにしても、
複数の開閉弁を連動させるようにしてもよい。
In this case, it is necessary to provide a switching valve upstream of the inlet valve to switch and connect the fuel supply circuit and the suction pump, but since this switching valve can also be used as an on-off valve, there is no need to increase the number of parts. Therefore, it is advantageous. Even if this switching valve rotates a loaf having one switching passage,
A plurality of on-off valves may be linked.

上記人口弁は、噴射ポンプ室に出塁するプランジャとは
別に設けることも可能であるが、プランジャ内に組込む
ことがコンパクト化及び小型化を図るうえで有利である
Although it is possible to provide the above-mentioned artificial valve separately from the plunger that enters the injection pump chamber, it is advantageous to incorporate it into the plunger in terms of compactness and miniaturization.

また、この人口弁は逆止弁で構成してもよいが、高速運
転時に閉弁時期が早められるおそれがなく、従って、燃
料噴射量の制御が正確にできるスプール弁を用いる方が
有利である。入口弁をプール弁で構成する場合、噴射開
始制御のための吸出しによってスプール室内一端側の容
積が減少し、燃料噴射量に誤差が生ずるおそれがあるの
で、噴射終了後、噴射ポンプのプラジャが上死点に後退
するまでに所定の圧力で入口弁に燃料を供給する定圧補
給回路を接続し、押込ポンプによる燃料供給開始時のス
プールの位置が一定になるようにすることが有利である
Additionally, although this artificial valve may be configured with a check valve, it is advantageous to use a spool valve, which does not have the risk of prematurely closing the valve during high-speed operation and can accurately control the amount of fuel injection. . When the inlet valve is configured with a pool valve, the volume at one end of the spool chamber decreases due to suction for injection start control, which may cause an error in the fuel injection amount. It is advantageous to connect a constant pressure replenishment circuit which supplies fuel to the inlet valve at a predetermined pressure until retraction to dead center, so that the position of the spool at the start of fuel supply by the force pump is constant.

タイマ機構は、動弁装置に付設されるタイマ機構と同様
に構成されたものを使用すればよく、動弁装置のタイマ
機構と兼用することも可能である。
The timer mechanism may be configured similarly to the timer mechanism attached to the valve train, and can also be used as the timer mechanism of the valve train.

更に、噴射管を中心に一例に噴射ポンプ室を、他側に第
2蓄圧室41と第1蓄圧室6とを接続する逆止弁39及
び圧力設定弁40を配置し、第2蓄圧室6を噴射管2の
上部の周囲に配置する場合は、本体内部の通路の形成を
容易にできるとともに、小型化及びコンパクト化を図る
上で有利である。
Furthermore, a check valve 39 and a pressure setting valve 40 connecting the second pressure accumulation chamber 41 and the first pressure accumulation chamber 6 are arranged around the injection pipe, and an injection pump chamber is arranged on the other side to connect the second pressure accumulation chamber 41 and the first pressure accumulation chamber 6. When disposed around the upper part of the injection pipe 2, it is possible to easily form a passage inside the main body, and it is advantageous in terms of miniaturization and compactness.

〈発明の作用〉 上述のように、本発明に係る蓄圧式燃料噴射装置の進角
装置では、閉弁圧力室を開閉弁を介して吸出しポンプに
接続しであるので開閉弁を開弁することにより、閉弁圧
力室の内圧を降下さゼでピストンに作用する差圧を増大
させ、ニードル弁を開弁させることができる。そして、
上記開閉弁の開弁時期をタイマ機構で調節することによ
り、ニードル弁の開弁開始時期を調節できる。このタイ
マ機構は、従来より公知の動弁装置のタイマ機構と同様
に構成すればよいので、エンジン回転数に対して燃料噴
射タイミングを正確にリニアに変化させることが可能で
ある。
<Operation of the Invention> As described above, in the advance angle device of the pressure accumulation type fuel injection device according to the present invention, since the closing pressure chamber is connected to the suction pump via the opening/closing valve, it is not necessary to open the opening/closing valve. By lowering the internal pressure in the valve-closing pressure chamber, the differential pressure acting on the piston can be increased, and the needle valve can be opened. and,
By adjusting the opening timing of the on-off valve using a timer mechanism, the opening timing of the needle valve can be adjusted. Since this timer mechanism may be constructed in the same manner as the timer mechanism of a conventionally known valve train, it is possible to accurately and linearly change the fuel injection timing with respect to the engine speed.

〈発明の効果〉 従って、上述の従来例のように複雑な補正機構を設けず
に、簡単な構成で噴射タイミングを正確にエンジン回転
数にリニアに対応させることができる蓄圧式燃料噴射装
置の進角装置を得られるのである。また、従来の進角装
置がポンプ駆動系に組み込まれているのに対して、ポン
プ駆動系から独立して燃料供給系内で進角装置を構成す
ることができるので、汎用性を高めることができる。更
に、カムフォロア、プッシュロンド、ロッカーアーム等
を設けないので、小型化を図る上で極めて有利になる。
<Effects of the Invention> Therefore, it is possible to develop an accumulator fuel injection device that can accurately and linearly correspond the injection timing to the engine rotational speed with a simple configuration without providing a complicated correction mechanism as in the conventional example described above. You can get a corner device. Additionally, whereas conventional advance angle devices are built into the pump drive system, the advance angle device can be configured within the fuel supply system independently from the pump drive system, increasing versatility. can. Furthermore, since a cam follower, push rod, rocker arm, etc. are not provided, it is extremely advantageous in terms of miniaturization.

〈実施例1〉 以下、本発明の一実施例を図面に基づいて詳細に説明す
る。
<Example 1> Hereinafter, one example of the present invention will be described in detail based on the drawings.

燃料噴射装置はユニットインジェクタUと、これに燃料
を供給する燃料供給回路F及び定圧補給回路Cを有し、
燃料供給回路F及び定圧補給回路Cに共用される燃料タ
ンク20と上記ユニットインジェクタUの間に進角制御
回路Tが設けられる。
The fuel injection device has a unit injector U, a fuel supply circuit F for supplying fuel thereto, and a constant pressure replenishment circuit C,
An advance angle control circuit T is provided between the fuel tank 20, which is shared by the fuel supply circuit F and the constant pressure replenishment circuit C, and the unit injector U.

燃料供給回路F、定圧補給回路C及び進角制御回路Tは
ユニットインジェクタUの入口弁12に切換弁■で切換
え接続される。
The fuel supply circuit F, constant pressure replenishment circuit C, and advance angle control circuit T are switched and connected to the inlet valve 12 of the unit injector U by a switching valve (2).

上記燃料供給回路Fは、燃料タンク20、燃料ポンプ2
1、調圧器22、li量器(ガバナ)23及び押込みポ
ンプ24を存し、エンジン回転数に対応して調量された
所定圧の燃料をユニットインジェクタUに供給するよう
に構成されている。この燃料供給のタイミングは、上記
切換弁■によりて決定される。
The fuel supply circuit F includes a fuel tank 20, a fuel pump 2
1, a pressure regulator 22, a governor 23, and a forced pump 24, and is configured to supply fuel at a predetermined pressure adjusted in accordance with the engine speed to the unit injector U. The timing of this fuel supply is determined by the switching valve (2).

ユニットインジェクタUは、第3図に示すように本体B
と一体に組立てられる噴射管2を有し、この噴射管2の
下端には、複数の噴射口lが開口される。この噴射管2
内にはニードル弁3が、噴射管2を上記噴射口lの近傍
で開閉するように進退可能に配置される。このニードル
弁3の弁軸にハピストン4が形成され、このピストン4
により噴射管2内の噴射口1と反対側の部分に閉弁圧力
室5が、噴射口1例の部分に小容量の第1蓄圧室6がそ
れぞれ区画される。ピストン4と噴射管2の内周面との
間には、閉弁圧力室5と蓄圧室6とを連通させる連通路
7が形成され、ピストン4の蓄圧室6側には、これの端
面に接離され、その周面が噴射管2の内周面に摺接する
逆止弁8が挿入される。上記閉弁圧力室5には連通路2
5を介して噴射ポンプ室9が接続され、この噴射ポンプ
室9にプランジャlOが進退可能に挿入される。このプ
ランジャ10内に噴射ポンプ室9への吸入路11を開閉
する入口弁12が設けられる。
The unit injector U is connected to the main body B as shown in Fig. 3.
It has an injection pipe 2 that is assembled integrally with the injection pipe 2, and a plurality of injection ports 1 are opened at the lower end of the injection pipe 2. This injection pipe 2
A needle valve 3 is disposed inside the injection valve 3 so as to be movable back and forth so as to open and close the injection pipe 2 in the vicinity of the injection port 1. A piston 4 is formed on the valve shaft of this needle valve 3, and this piston 4
As a result, a valve-closing pressure chamber 5 is defined in a portion of the injection pipe 2 opposite to the injection port 1, and a small-capacity first pressure accumulation chamber 6 is defined in a portion of the injection port. A communication passage 7 is formed between the piston 4 and the inner circumferential surface of the injection pipe 2, which communicates the valve-closing pressure chamber 5 with the pressure accumulation chamber 6. A check valve 8 is inserted which is moved toward and away from the valve and whose peripheral surface slides into contact with the inner peripheral surface of the injection pipe 2 . A communication passage 2 is provided in the valve closing pressure chamber 5.
An injection pump chamber 9 is connected through the injection pump chamber 5, and a plunger IO is inserted into the injection pump chamber 9 so as to be movable forward and backward. An inlet valve 12 for opening and closing a suction passage 11 to the injection pump chamber 9 is provided within the plunger 10 .

即ち、プランジャlOは本体Bに上下方向に進退可能に
支持され、その内部にスプール26を収納するスプール
室27が形成される。このスプール26は、下端から上
端の近傍に延びる中空穴28を有し、スプール26及び
プランジャ10の中間高さ部に切換弁Vに連通ずる連通
路29.30が形成される。また、プランジャ10の下
端から所定の位置に噴射ポンプ室9をスプール室27の
下部の蓄圧室43に連通させる弁孔31,32が形成さ
れ、スプール26の周壁には、これの下端から所定の高
さに、弁孔31.32に対応する弁孔33が貫通させで
ある。更に、スプール26の周壁には中空穴28の上端
から周面に通じるバイアス路34が形成されている。こ
のバイアス路34はプランジャ10に形成された通路3
5を介して、スプール室27の上部のバイアス室36と
、本体B内の閉弁バネ室37に連通される。
That is, the plunger lO is supported by the main body B so as to be movable in the vertical direction, and a spool chamber 27 for storing the spool 26 is formed therein. The spool 26 has a hollow hole 28 extending from the lower end to the vicinity of the upper end, and communication passages 29 and 30 communicating with the switching valve V are formed at an intermediate height between the spool 26 and the plunger 10. Further, valve holes 31 and 32 are formed at predetermined positions from the lower end of the plunger 10 to communicate the injection pump chamber 9 with the pressure accumulation chamber 43 at the lower part of the spool chamber 27, and the peripheral wall of the spool 26 is provided with valve holes 31 and 32 at predetermined positions from the lower end of the plunger 10. A valve hole 33 corresponding to the valve hole 31, 32 passes through the height. Furthermore, a bias path 34 is formed in the circumferential wall of the spool 26, leading from the upper end of the hollow hole 28 to the circumferential surface. This bias passage 34 is a passage 3 formed in the plunger 10.
5, it communicates with a bias chamber 36 in the upper part of the spool chamber 27 and a valve-closing spring chamber 37 in the main body B.

閉弁バネ室37は閉弁圧力室5の上方に配置され、この
閉弁バネ室37にはニードル弁3の弁軸の上端が昇降可
能に突入させである。また、この閉弁バネ室37内には
、該弁軸を下方に付勢する閉弁バネ38が挿入されてい
る。
The valve-closing spring chamber 37 is arranged above the valve-closing pressure chamber 5, and the upper end of the valve shaft of the needle valve 3 is inserted into the valve-closing spring chamber 37 so as to be able to rise and fall. Further, a valve closing spring 38 is inserted into the valve closing spring chamber 37 to bias the valve shaft downward.

上記第1蓄圧室6は逆止弁39と圧力設定弁40を介し
て大容漬の第2蓄圧室41に接続される。
The first pressure accumulation chamber 6 is connected to a large-capacity second pressure accumulation chamber 41 via a check valve 39 and a pressure setting valve 40.

この第2蓄圧室6は、本体B内でニードル弁3の弁軸の
上部を取り囲む円環形状に形成される。上記逆止弁39
は、第1M圧室6の内圧が、例えば700〜1000気
圧という高圧になるときに開弁されて、第1蓄圧室6か
ら第2蓄圧室41に燃料を流入するように構成され、圧
力設定弁40は第1蓄圧室6の内圧がニードル弁3の開
弁により閉弁圧よりも高い所定圧まで降下したときに開
弁され、第1蓄圧室6及び第2蓄圧室41の内圧が所定
の閉弁圧(例えば、270気圧)に達したときに閉弁バ
ネ42によって閉弁される。
This second pressure accumulating chamber 6 is formed in the main body B in an annular shape surrounding the upper part of the valve shaft of the needle valve 3. The above check valve 39
is configured such that the valve is opened when the internal pressure of the first M pressure chamber 6 reaches a high pressure of, for example, 700 to 1000 atmospheres, and fuel flows from the first pressure accumulation chamber 6 to the second pressure accumulation chamber 41, and the pressure setting The valve 40 is opened when the internal pressure of the first pressure accumulator 6 drops to a predetermined pressure higher than the valve closing pressure due to the opening of the needle valve 3, and the internal pressures of the first pressure accumulator 6 and the second pressure accumulator 41 are set to a predetermined level. When the valve closing pressure (for example, 270 atmospheres) is reached, the valve is closed by the valve closing spring 42.

尚、上記プランジ中10に形成された両弁孔31.32
の一方の弁孔31は、その他方の弁孔32に比べてはる
かに小径に形成され、かつ、スプール26の下死点から
他方の弁孔32よりも上方に開口されている。
In addition, both valve holes 31 and 32 formed in the plunger 10
One valve hole 31 is formed to have a much smaller diameter than the other valve hole 32, and opens above the other valve hole 32 from the bottom dead center of the spool 26.

上記定圧補給回路Cは燃料供給回路Fの調圧器22の下
流から分岐され、進角制御回路Tは、タイマ機構43に
よって開弁時期が制御される開閉弁としての切換弁■と
、吸出しポンプ45とを備えている。この吸出しポンプ
45はプランジャ室46に進退可能に挿入されたプラン
ジャ47と、プランジャ47をプランジャ室46の容積
が広がる方向に付勢するバネ48とからなり、図示しな
いクランク軸に連動するカム49により駆動される。
The constant pressure replenishment circuit C is branched from the downstream side of the pressure regulator 22 of the fuel supply circuit F, and the advance angle control circuit T includes a switching valve ■ serving as an on-off valve whose opening timing is controlled by a timer mechanism 43, and a suction pump 45. It is equipped with This suction pump 45 consists of a plunger 47 inserted into a plunger chamber 46 so as to be movable back and forth, and a spring 48 that biases the plunger 47 in a direction in which the volume of the plunger chamber 46 increases. Driven.

尚、50は逆止弁8の閉弁バネ、51は逆止弁39の閉
弁バネである。
Note that 50 is a closing spring for the check valve 8, and 51 is a closing spring for the check valve 39.

上記の構成において、燃料がユニットインジェクタUに
供給され始める第12図aの時点では、第3図に示すよ
うに、スプール26は下死点に位置し、プランジャlO
は上死点に位置させられる。
In the above configuration, at the time point in FIG. 12a when fuel starts to be supplied to the unit injector U, the spool 26 is located at the bottom dead center and the plunger lO is located at the bottom dead center as shown in FIG.
is positioned at top dead center.

この時点では、入口弁12は開弁され、逆止弁8、逆止
弁39及び圧力設定弁40は閉弁され、バイアス室36
はスプール26の中空穴28に連通されている。この時
点からプランジャ10を上死点位置させたまま燃料が供
給され始められると、スプール26が下死点から上昇し
、第4図に示すように、バイアス室36とスプール26
内の中空穴28とが遮断され、バイアス室36と蓄圧室
43との圧力がバランスする位置でスプール26は停止
し、燃料供給が終了する。第12図Cの時点で図示しな
いカムがプランジャlOを下降させ始める。これにより
、噴射ポンプ室9の容積が減少し始める。この容積の減
少にともなって噴射ポンプ室9から弁孔31,32を介
して蓄圧室43に燃料が流入し、スプール26が再度上
昇する。このスプール26が上昇する間に閉弁圧力室5
、噴射ポンプ室9及び蓄圧室43の内圧は上昇する。や
がて第5図に示すように、d時点で入口弁12が閉弁さ
れ、蓄圧室43の内圧は一定になる。このd時点で逆止
弁8が開弁されるとともに、プランジャ10の下降はさ
らに続けられ、閉弁圧力室5、噴射ポンプ室9及び第1
蓄圧室6の内圧はさらに上昇し、所定の圧力以上になる
e時点以後第6図に示すように逆止弁39が開弁され、
プランジャ10が下死点に達し、閉弁圧力室5、噴射ポ
ンプ室9、第1蓄圧室6及び第2蓄圧室41の内圧がバ
ランスする1時点で、第7図に示すように、逆止弁8及
び逆止弁39が閉弁される。この後、g時点で切換弁V
を切換えて吸入路11を進角制御回路Tに接続すると、
スプール26の中空穴28及び蓄圧室43の内圧が下降
し、その間にスプール26はバイアス室36と蓄圧室4
3との差圧によって下降し、h時点で第8図に示すよう
に、小径の弁孔31が弁孔33に接続される。これによ
り、hの時点から閉弁圧力室5の内圧が徐々に降下する
一方、蓄圧室43の内圧は閉弁圧力室5の内圧の影響を
受けて昇圧し、スプール26の位置が上昇する。この間
に閉弁圧力室5の内圧が低下して、ニードル弁3に作用
する閉弁ばね室37の内圧及び閉弁バネ38の力に差圧
が打ち勝つ1時点でニードル弁3の開弁が開始される。
At this point, the inlet valve 12 is opened, the check valve 8, the check valve 39, and the pressure setting valve 40 are closed, and the bias chamber 36 is closed.
is in communication with the hollow hole 28 of the spool 26. From this point on, when fuel starts to be supplied with the plunger 10 at the top dead center position, the spool 26 rises from the bottom dead center, and as shown in FIG.
The spool 26 stops at a position where the inner hollow hole 28 is cut off and the pressures of the bias chamber 36 and the pressure accumulation chamber 43 are balanced, and fuel supply ends. At the point in time in FIG. 12C, a cam (not shown) begins to lower the plunger lO. As a result, the volume of the injection pump chamber 9 begins to decrease. As the volume decreases, fuel flows from the injection pump chamber 9 into the pressure accumulation chamber 43 through the valve holes 31 and 32, and the spool 26 rises again. While this spool 26 is rising, the valve pressure chamber 5 is closed.
, the internal pressures of the injection pump chamber 9 and the pressure accumulation chamber 43 rise. Eventually, as shown in FIG. 5, the inlet valve 12 is closed at time d, and the internal pressure of the pressure accumulator 43 becomes constant. At this point d, the check valve 8 is opened, and the plunger 10 continues to descend, closing the pressure chamber 5, the injection pump chamber 9, and the first
The internal pressure of the pressure accumulating chamber 6 further increases, and after the point e when the pressure exceeds a predetermined pressure, the check valve 39 is opened as shown in FIG.
At a point in time when the plunger 10 reaches the bottom dead center and the internal pressures of the valve-closing pressure chamber 5, the injection pump chamber 9, the first pressure accumulation chamber 6, and the second pressure accumulation chamber 41 are balanced, a non-return check is performed as shown in FIG. Valve 8 and check valve 39 are closed. After this, at time g, the switching valve V
When the suction passage 11 is connected to the advance angle control circuit T by switching the
The internal pressure of the hollow hole 28 of the spool 26 and the pressure accumulation chamber 43 decreases, and during that time the spool 26 is moved between the bias chamber 36 and the pressure accumulation chamber 4.
3, and at time h, the small-diameter valve hole 31 is connected to the valve hole 33, as shown in FIG. As a result, the internal pressure of the valve-closing pressure chamber 5 gradually decreases from time h, while the internal pressure of the pressure accumulating chamber 43 increases under the influence of the internal pressure of the valve-closing pressure chamber 5, and the position of the spool 26 rises. During this period, the internal pressure in the valve-closing pressure chamber 5 decreases, and at a point in time when the differential pressure overcomes the internal pressure in the valve-closing spring chamber 37 and the force of the valve-closing spring 38 acting on the needle valve 3, the needle valve 3 starts to open. be done.

ニードル弁3の開弁が開始しても、閉弁圧力室5の内圧
の低下は小径の弁孔31の絞り作用によって緩慢に進行
するので、ニードル弁3の開弁量も僅かであり、第1M
圧室6の内圧の低下は小さく抑えられる。スプール26
の上昇はさらに続き、大径の弁孔32が弁孔33に連通
ずるj時点以降は閉弁圧力室5及び噴射ポンプ室9と蓄
圧室43が大きな弁孔32により連通されるので、閉弁
圧力室5の内圧がさらに減少され、第9図に示すように
ニードル弁3はさらに大きく開弁される。この開弁と同
時に圧力設定弁40が開弁じて、第2蓄圧室41から多
量の燃料が第1蓄圧室6及び噴出口1を介して噴出され
る。第1蓄圧室6及び第2蓄圧室41の内圧が所定値ま
で降下すると、ピストン4に作用する差圧が減少し、閉
弁バネ38及び閉弁バネ室37から弁軸に作用する圧力
がピストン4に作用する差圧より大きくなるに時点では
ニードル弁3が閉弁されて、燃料噴射が終了する。この
後1時点以降にプランジャIOが下死点から上死点に向
かって上昇する。スプール26は、第12図(2)に示
すように燃料噴射終了時までに中間の高さに降下するが
、プランジャ10の上昇時に更に下死点まで降下する。
Even if the needle valve 3 starts to open, the internal pressure in the valve-closing pressure chamber 5 decreases slowly due to the throttling action of the small-diameter valve hole 31, so the opening amount of the needle valve 3 is also small. 1M
The decrease in the internal pressure of the pressure chamber 6 can be suppressed to a small level. Spool 26
continues to rise, and after the point in time when the large diameter valve hole 32 communicates with the valve hole 33, the valve closing pressure chamber 5, injection pump chamber 9, and pressure accumulation chamber 43 are communicated through the large valve hole 32, so the valve closes. The internal pressure of the pressure chamber 5 is further reduced, and the needle valve 3 is opened further as shown in FIG. Simultaneously with this valve opening, the pressure setting valve 40 is opened, and a large amount of fuel is ejected from the second pressure accumulation chamber 41 via the first pressure accumulation chamber 6 and the injection port 1. When the internal pressures of the first pressure accumulation chamber 6 and the second pressure accumulation chamber 41 drop to a predetermined value, the differential pressure acting on the piston 4 decreases, and the pressure acting on the valve shaft from the valve closing spring 38 and the valve closing spring chamber 37 decreases to the piston. When the pressure difference becomes greater than the differential pressure acting on the needle valve 3, the needle valve 3 is closed and the fuel injection is completed. After this, the plunger IO rises from the bottom dead center toward the top dead center after time 1. The spool 26 descends to an intermediate height by the end of fuel injection, as shown in FIG. 12(2), but further descends to the bottom dead center when the plunger 10 rises.

この場合、進角制御回路Tと吸入路11との連通によっ
て、蓄圧室43の内圧が最初のa時点よりも定圧になり
、次に例えば前回と同じ量の燃料が供給されたとすると
、蓄圧室43やこれと連通される噴射ポンプ室9の内圧
が前回よりも低くなり、プランジャlOとこれを駆動す
るカムとの間に隙間が生じ、打撃音等の騒音を発生する
おそれがあるので、上記スプール26が下死点に降下し
終わる前の適当な期間にわたって、切換弁Vを切換えて
、定圧補給回路Cを吸入路11に接続される。
In this case, due to the communication between the advance angle control circuit T and the suction passage 11, the internal pressure of the pressure accumulator 43 becomes more constant than at the initial point a, and then, for example, if the same amount of fuel as last time is supplied, then the pressure accumulator 43 and the injection pump chamber 9 that communicates with it will be lower than before, and there will be a gap between the plunger IO and the cam that drives it, which may cause noise such as impact noise. The constant pressure supply circuit C is connected to the suction passage 11 by switching the switching valve V for an appropriate period before the spool 26 finishes descending to the bottom dead center.

上記一実施例では、弁孔31,32が第1O図(1)に
示すように大小の円孔で形成されているが、例えば第1
0図(2)に示すように、円孔32とこれに連続する細
溝31とで構成してもよく、また、例えば第10図(3
)に示すように小径部31と大径部32とを連続させた
卵形の孔で構成してもよい。
In the above embodiment, the valve holes 31 and 32 are formed of large and small circular holes as shown in FIG.
As shown in FIG. 10 (2), it may be composed of a circular hole 32 and a narrow groove 31 continuous thereto, or, for example, as shown in FIG.
), it may be constructed of an oval-shaped hole in which the small diameter part 31 and the large diameter part 32 are continuous.

また、上記切換弁Vは一つのロータに1本の通路を貫通
させ、このロータをエンジンの回転数と同回転数で回転
させるようにしであるが、このような一体のロークリ式
の切換弁Vに限定されるものではなく、複数の連動弁で
切換弁Vを構成することも可能である。
In addition, the above-mentioned switching valve V has one passage passing through one rotor so that the rotor is rotated at the same rotation speed as the engine, but such an integrated rotor-type switching valve V It is also possible to configure the switching valve V with a plurality of interlocking valves.

更に、第11図に示すように、入口弁工2が逆止弁で構
成され、バイアス室36に代えて開弁バネ52を設け、
第2蓄圧室41を省略したユニットインジェクタU゛を
使用することも可能である。
Furthermore, as shown in FIG. 11, the inlet valve 2 is composed of a check valve, and a valve opening spring 52 is provided in place of the bias chamber 36.
It is also possible to use a unit injector U' in which the second pressure accumulator 41 is omitted.

更に、上述の一実施例では、噴出管2を中心に一例に噴
射ポンプ室9が、他側に第2M圧室41と第1M圧室6
とを接続する逆止弁39及び圧力設定弁40が配置され
、第2N圧室6が噴射管6の上部の周囲に配置されてい
るので、本体内部の通路の形成が容易であり、小型、か
つ、コンパクトに構成できる。
Furthermore, in the above-mentioned embodiment, the injection pump chamber 9 is located around the jet pipe 2, and the second M pressure chamber 41 and the first M pressure chamber 6 are located on the other side.
The check valve 39 and the pressure setting valve 40 that connect the Moreover, it can be configured compactly.

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

第1図は本発明の要部を概略的に示す等価回路図、第2
図は本発明の一実施例の等価回路図、第3図〜第9図は
そのユニットインジェクタの作動状態を順に示す縦断面
図、第10図(1)はプランジャの弁孔を示す正面図、
第10図(2)、第1O図(3)はそれぞれ異なるプラ
ンジャの弁孔を示す正面図、第11図は他のユニットイ
ンジェクタの縦断面図、第12図(1)〜(6)はタイ
ムチャー1・であり、第12図(1)はスプール室下部
の蓄圧室の内圧変化、第12図(2)はスプール位置変
化、第12図(3)はプランジャの位置変化、第12図
(4)は噴射ポンプ室の内圧変化、第12図(5)はニ
ードル弁のリフト量変化、第12図(6)は第1蓄圧室
、第2蓄圧室の内圧変化及び燃料噴射率変化をそれぞれ
示し、第13図は従来例の構成図である。 3・・・噴射弁にニードル弁)、5・・・閉弁圧力室、
6・・・第1蓄圧室、8・・・逆止弁、9・・・噴射ポ
ンプ室、11・・・吸入路、12・・・入口弁、14・
・・吸出ポンプ、15・・・タイマ機構、B・・・本体
、■・・・開閉弁。 第 4 圓 第 5 川 第 6 図 ¥ 7 胆 ]7 帖 2田 第 ? 圓 手続補正書Cヶ六°) 昭和61年11月28日
FIG. 1 is an equivalent circuit diagram schematically showing the main parts of the present invention, and FIG.
The figure is an equivalent circuit diagram of one embodiment of the present invention, FIGS. 3 to 9 are longitudinal sectional views showing the operating states of the unit injector in order, and FIG. 10 (1) is a front view showing the valve hole of the plunger.
Figure 10 (2) and Figure 1O (3) are front views showing the valve holes of different plungers, Figure 11 is a vertical cross-sectional view of another unit injector, and Figures 12 (1) to (6) are time Figure 12 (1) shows the change in the internal pressure of the pressure accumulator at the bottom of the spool chamber, Figure 12 (2) shows the change in the spool position, Figure 12 (3) shows the change in the plunger position, and Figure 12 ( 4) shows the change in the internal pressure of the injection pump chamber, Fig. 12 (5) shows the change in the lift amount of the needle valve, and Fig. 12 (6) shows the change in the internal pressure of the first pressure accumulator chamber and the second pressure accumulator chamber, and the change in the fuel injection rate. 13 is a configuration diagram of a conventional example. 3... Injection valve and needle valve), 5... Valve closing pressure chamber,
6... First pressure accumulation chamber, 8... Check valve, 9... Injection pump chamber, 11... Suction path, 12... Inlet valve, 14...
...Suction pump, 15...Timer mechanism, B...Main body, ■...Opening/closing valve. 4th round 5th river 6th figure¥ 7 bile] 7th chapter 2nd stage ? Amended written amendment C garoku°) November 28, 1986

Claims (1)

【特許請求の範囲】[Claims] 1.本体B内に形成された燃料通路の終端部に該燃料通
路を開閉する噴射弁3を設けるとともに、その途中に逆
流を防止する逆止弁8を介在させて上記噴射弁3と逆止
弁8との間に蓄圧室6を形成し、逆止弁8の上流に噴射
ポンプ室9とこの噴射ポンプ室9への吸入路11を断続
する入口弁12とを有する燃料噴射装置の進角装置であ
って、上記逆止弁8の上流側に上記噴射弁3にこれを閉
弁方向に付勢する圧力を作用させるための閉弁圧力室5
を設け、この閉弁圧力室5に開閉弁Vを介して吸出ポン
プ14を接続すると共に、エンジン回転数に対応して上
記開閉弁Vの開弁開始時期を調整するタイマ機構15を
設けたことを特徴とする、蓄圧式燃料噴射装置の進角装
1. An injection valve 3 for opening and closing the fuel passage is provided at the terminal end of the fuel passage formed in the main body B, and a check valve 8 for preventing backflow is interposed in the middle of the injection valve 3 and check valve 8. An advance device for a fuel injection device which has a pressure accumulation chamber 6 formed between the check valve 8 and an injection pump chamber 9 upstream of the check valve 8 and an inlet valve 12 that connects and disconnects the suction path 11 to the injection pump chamber 9. There is a valve-closing pressure chamber 5 on the upstream side of the check valve 8 for applying pressure to the injection valve 3 in the valve-closing direction.
A suction pump 14 is connected to the closing pressure chamber 5 via an opening/closing valve V, and a timer mechanism 15 is provided for adjusting the opening timing of the opening/closing valve V in accordance with the engine speed. An advance device for a pressure accumulator fuel injection device, characterized by
JP61216901A 1986-09-13 1986-09-13 Advancer for accumulator type fuel injection device Pending JPS63167068A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP61216901A JPS63167068A (en) 1986-09-13 1986-09-13 Advancer for accumulator type fuel injection device
US07/095,459 US4807811A (en) 1986-09-13 1987-09-11 Accumulator fuel injector for diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61216901A JPS63167068A (en) 1986-09-13 1986-09-13 Advancer for accumulator type fuel injection device

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP25308286A Division JPS6394068A (en) 1986-10-23 1986-10-23 Accumulator type fuel injection nozzle

Publications (1)

Publication Number Publication Date
JPS63167068A true JPS63167068A (en) 1988-07-11

Family

ID=16695684

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61216901A Pending JPS63167068A (en) 1986-09-13 1986-09-13 Advancer for accumulator type fuel injection device

Country Status (1)

Country Link
JP (1) JPS63167068A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58192962A (en) * 1982-05-06 1983-11-10 Yanmar Diesel Engine Co Ltd Fuel injection pump for internal-combustion engine
JPS59200055A (en) * 1983-04-25 1984-11-13 Kanesaka Gijutsu Kenkyusho:Kk Fuel injection device for compression firing engine
JPS6187963A (en) * 1984-10-08 1986-05-06 Kanesaka Gijutsu Kenkyusho:Kk Fuel injection device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58192962A (en) * 1982-05-06 1983-11-10 Yanmar Diesel Engine Co Ltd Fuel injection pump for internal-combustion engine
JPS59200055A (en) * 1983-04-25 1984-11-13 Kanesaka Gijutsu Kenkyusho:Kk Fuel injection device for compression firing engine
JPS6187963A (en) * 1984-10-08 1986-05-06 Kanesaka Gijutsu Kenkyusho:Kk Fuel injection device

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