JPS5827873A - Excess fuel discharge device for fuel injection pump - Google Patents
Excess fuel discharge device for fuel injection pumpInfo
- Publication number
- JPS5827873A JPS5827873A JP12568681A JP12568681A JPS5827873A JP S5827873 A JPS5827873 A JP S5827873A JP 12568681 A JP12568681 A JP 12568681A JP 12568681 A JP12568681 A JP 12568681A JP S5827873 A JPS5827873 A JP S5827873A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- injection
- free piston
- injection pump
- valve body
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M41/00—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
- F02M41/08—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
- F02M41/14—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons
- F02M41/1405—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons pistons being disposed radially with respect to rotation axis
- F02M41/1411—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons pistons being disposed radially with respect to rotation axis characterised by means for varying fuel delivery or injection timing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M41/00—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
- F02M41/08—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
- F02M41/14—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons
- F02M41/1405—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons pistons being disposed radially with respect to rotation axis
- F02M41/1411—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined rotary distributor supporting pump pistons pistons being disposed radially with respect to rotation axis characterised by means for varying fuel delivery or injection timing
- F02M41/1422—Injection being effected by means of a free-piston displaced by the pressure of fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/20—Varying fuel delivery in quantity or timing
- F02M59/32—Varying fuel delivery in quantity or timing fuel delivery being controlled by means of fuel-displaced auxiliary pistons, which effect injection
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
本発明はディーゼルエンジン等に用いられる燃料噴射ポ
ンプに係シ、特に、その余剰燃料排出装置に関するもの
である。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel injection pump used in a diesel engine or the like, and particularly to a surplus fuel discharge device thereof.
第1図は従来の燃料噴射ポンプの断面図である。FIG. 1 is a sectional view of a conventional fuel injection pump.
エンジンと同期的に回転している駆動シャフト(図示さ
れていない]によってロータlは回転させられるが、こ
の四−夕1の左端部を横に貫通する孔には一対のプラン
ジャ2が収容されている。A rotor 1 is rotated by a drive shaft (not shown) rotating synchronously with the engine, and a pair of plungers 2 are accommodated in a hole passing through the left end of the rotor 1 laterally. There is.
このプランジャ2の外側にはロー2シユー8およびロー
ラ9が設置されておシ、これらのプランジャ2.ローラ
シュー8およびローラ9はロータ1と共に回転する。A row 2 shoe 8 and a roller 9 are installed on the outside of the plunger 2. Roller shoes 8 and rollers 9 rotate together with rotor 1.
ロー29の外周のカムリング3は最外側のハウジング1
0内に装着されている。ま九、ロータ1はハウジング1
0に固定されているスリーブホルダ41内に取シ付けら
れているスリーブ42の内部で回転運動を行っている。The cam ring 3 on the outer periphery of the row 29 is the outermost housing 1
It is installed in 0. Nine, rotor 1 is housing 1
The sleeve 42 is mounted in a sleeve holder 41 which is fixed at 0, and rotates inside the sleeve 42.
一一タlの内部は第1加圧室4と第2加圧1i16とに
区分され、その間にフリーピストン5が介在しておシ、
第2加圧I!6の右端はストッパ7で封止されている。The inside of the tank is divided into a first pressurizing chamber 4 and a second pressurizing chamber 1i16, with a free piston 5 interposed between them.
Second pressurization I! The right end of 6 is sealed with a stopper 7.
また、第2加圧宣6はロータ1の牛径方向に形成された
吐出通路23に連通し、第2放射通路12はスリーブ4
2の第2固定通路14に対応して設けられている。Further, the second pressure release 6 communicates with a discharge passage 23 formed in the radial direction of the rotor 1, and the second radial passage 12 communicates with the sleeve 4.
It is provided corresponding to the second fixed passage 14 of No. 2.
一方、第1加圧室4に連通している第1放射通路11は
スリーブ42の第1固定通路13に対応して設けられ、
第1加圧室4の下部には溢流口29が設けられ、溢流通
路30,311−通って排出通1632に接続している
。On the other hand, the first radiation passage 11 communicating with the first pressurizing chamber 4 is provided corresponding to the first fixed passage 13 of the sleeve 42,
An overflow port 29 is provided in the lower part of the first pressurizing chamber 4, and is connected to the discharge passage 1632 through overflow passages 30, 311-.
スリーブ42に形成し九第1固定通路13.第2固定通
路14の開口部はjll電磁弁15.第2電磁弁16の
弁体17の先増に夫々対向しておシ、この第1電磁弁1
5と第2電磁弁16はケース18に収容した;イル19
と固定磁極20.ばね21で構成されている。なお、ス
リーブホルダ41の中央部には燃料供給口43が形成さ
れ、これよシ導入された燃料は電磁弁15.16の弁体
17の収容室およびロータ1内に充満している。A ninth first fixing passage 13 is formed in the sleeve 42. The opening of the second fixed passage 14 is connected to the jll solenoid valve 15. The valve body 17 of the second solenoid valve 16 is located opposite to the first solenoid valve 1.
5 and the second solenoid valve 16 were housed in a case 18;
and fixed magnetic pole 20. It is composed of a spring 21. A fuel supply port 43 is formed in the center of the sleeve holder 41, and the fuel introduced through this port fills the accommodation chamber of the valve body 17 of the solenoid valve 15, 16 and the rotor 1.
なお、22はコイル19の端子であ夛、24は出力通路
で6シ、25は接続口でめる。また、27はスリーブホ
ルダ41の端部に固定した環状の永久磁石をもつ検出器
でめシ、その中側にはロータ1に取シ付けたパルサ26
が挿入されている。In addition, 22 is a terminal of the coil 19, 24 is an output path, and 25 is a connection port. Further, 27 is a female detector having an annular permanent magnet fixed to the end of the sleeve holder 41, and a pulser 27 attached to the rotor 1 is located inside the detector.
is inserted.
パルサ26は周辺に突起部を設けた磁性体で、ロータ1
と共にパルサ26が回転すると、磁路が断続されるので
検出端子28より回転信号を出力する。これによってロ
ータlの回転位置と速度を検出することができる。The pulsar 26 is a magnetic material with protrusions around its periphery, and is attached to the rotor 1.
When the pulser 26 rotates at the same time, the magnetic path is interrupted and a rotation signal is output from the detection terminal 28. This allows the rotational position and speed of the rotor I to be detected.
このように構成された燃料噴射ポンプの動作について第
2図〜第7図によって説明する。これらの図の左側は第
1図のIf−It断面図に相当するもので、燃料ポンプ
の状態を示している。iた、右側の図は回転するロータ
1とロータ1を収容しているスリーブ42との燃料流路
の関係および7リーピストン5の位置が示されている。The operation of the fuel injection pump configured in this way will be explained with reference to FIGS. 2 to 7. The left side of these figures corresponds to the If-It sectional view of FIG. 1, and shows the state of the fuel pump. In addition, the diagram on the right side shows the relationship of the fuel flow path between the rotating rotor 1 and the sleeve 42 housing the rotor 1, and the position of the 7-lead piston 5.
第2図は噴射燃料の供給開始時の状態で、プランジャ2
a、 2bは外側に移動中である。第2図(a)ではカ
ムリング3の内面の縮小径部よ〕大径部へ移行しておシ
、第1加圧室4が減圧されるのでフリーピスト15は矢
印方向に移動して第2加圧室8t−減圧する。したがっ
て第2放射通路12とM2固定通M14を介して噴射燃
料を吸入する。Figure 2 shows the state at the start of the supply of injected fuel, and the plunger 2
a, 2b are moving outward. In FIG. 2(a), the reduced diameter portion of the inner surface of the cam ring 3 moves to the larger diameter portion, and as the first pressurizing chamber 4 is depressurized, the free piston 15 moves in the direction of the arrow and moves to the second pressurizing chamber 4. Pressure chamber 8t - Depressurize. Therefore, the injected fuel is sucked through the second radiation passage 12 and the M2 fixed passage M14.
なおこの時は弁体17bは開放されているので加圧され
た燃料が第2加圧室6内に流入する。即ち、この場合は
噴射するための燃料を吸入している段階である。Note that at this time, since the valve body 17b is open, pressurized fuel flows into the second pressurizing chamber 6. That is, in this case, fuel for injection is being sucked.
第3図は噴射燃料の吸入が完了し噴射時期調整燃料の供
給を開始した状態を示し、この時はフリーピストンは一
時停止して弁体171が開弁した時点である。なお、第
3vA(a)に示すごとくローラ9はカムリング3の大
きな内径部を回転するのでプランジャ2は更に第1加圧
室4を減圧し、第1固定通路13.第1放射通路1lt
−介して噴射時期調整燃料を吸入する。なお、弁体17
a、17bは同時に開弁して燃料を導入するようにする
こともできる。FIG. 3 shows a state in which the intake of the injected fuel has been completed and the supply of the injection timing adjustment fuel has started, and at this time the free piston has temporarily stopped and the valve body 171 has opened. Note that as the roller 9 rotates around the large inner diameter portion of the cam ring 3, the plunger 2 further depressurizes the first pressurizing chamber 4, and the first fixed passage 13. 1st radiation passage 1lt
-The injection timing adjustment fuel is taken in through the In addition, the valve body 17
It is also possible to open valves a and 17b at the same time to introduce fuel.
第4図は噴射時期調整燃料の供給が終了した状1It−
示し、プランジャ2とフリーピストン5は停止し、弁体
17は共に閉じている。Figure 4 shows the state 1It- when the injection timing adjustment fuel supply has finished.
As shown, the plunger 2 and the free piston 5 are stopped, and the valve body 17 is both closed.
第5図は燃料噴射開始状Mを示し、このときはローラ9
がカムリング3の縮小内径部に導びかれるのでプランジ
ャ2は接近し始める。したがってフリーピストン5は矢
印右方向に移動して第2加圧室6内の燃料を吐出通路2
3.出口通l&24を介して第1図の接続口25に圧送
する。接続口25に取シ付けたパイプは気筒に連通して
いるので所定量の燃料が気筒に供給される。FIG. 5 shows a fuel injection start state M, in which the roller 9
is guided to the reduced inner diameter of the cam ring 3, so the plunger 2 begins to approach. Therefore, the free piston 5 moves in the right direction of the arrow to transfer the fuel in the second pressurizing chamber 6 to the discharge passage 2.
3. It is pumped via outlet port 1&24 to connection port 25 in FIG. Since the pipe attached to the connection port 25 communicates with the cylinder, a predetermined amount of fuel is supplied to the cylinder.
第6図は燃料噴射を終了して余剰燃料の排出開始状l!
1f:示し、フリーピストン5が右側極@盲で移動する
と溢流口29が露出するので、加圧されている余剰の燃
料は溢流通路30を介してtIt出する。なお、この燃
料は第1図のスリーブホルダ41の溢流通路31を通っ
て低圧部へ流出する。Figure 6 shows the start of exhaustion of excess fuel after fuel injection has ended!
1f: As shown, when the free piston 5 moves to the right side, the overflow port 29 is exposed, so the pressurized surplus fuel flows out through the overflow passage 30. Note that this fuel flows out to the low pressure section through the overflow passage 31 of the sleeve holder 41 shown in FIG.
即ち、第1図はこの時の状態を示している。That is, FIG. 1 shows the state at this time.
第7図は余剰燃料の排出を終了した状態を示してお9、
フリーピストン5ti一時停止しているがこれから第2
図の状態に移行して噴射燃料を吸入しようとしている。Figure 7 shows the state after the discharge of excess fuel9.
Free piston 5ti has stopped temporarily, but the second one will start soon.
It is about to move to the state shown in the figure and inhale the injected fuel.
上記の説明で理解されることは、ロータ1が90″回転
する間に一連の燃料吸入噴射操作が行われる。なお、こ
の場合のエンジンは4気筒の例を示しているので、ロー
タ1が1回転する間にすべての気筒に燃料が噴射される
。を九、第1加圧室4に吸入される燃料は所謂噴射時期
を崗整するための燃料であ夛、実際に噴射されるものは
#f2加圧室6に吸入された燃料である。What is understood from the above explanation is that a series of fuel intake and injection operations are performed while the rotor 1 rotates 90''. Note that the engine in this case is a 4-cylinder engine, so the rotor 1 is Fuel is injected into all cylinders during rotation. 9. The fuel sucked into the first pressurizing chamber 4 is a lot of fuel for adjusting the injection timing, and what is actually injected is #f2 is the fuel sucked into the pressurizing chamber 6.
このように作動する従来の燃料噴射ポンプは、第2加圧
室6の燃料が噴射された後で余剰な燃料を排出するが、
このとき溢出口29の開口面積が急速に増加しないので
、フリーピストン5を強制的にオーパース)0−りさせ
るのに時間を要する。The conventional fuel injection pump that operates in this manner discharges excess fuel after the fuel in the second pressurizing chamber 6 is injected.
At this time, since the opening area of the overflow port 29 does not increase rapidly, it takes time to force the free piston 5 to open.
したがって、第2加圧1i16に導入する次期噴射燃料
を余分に吸入し、フリーピストン5の動き、を不安定に
する。Therefore, the next injection fuel to be introduced into the second pressurization 1i16 is excessively sucked in, making the movement of the free piston 5 unstable.
また、この導入燃料量は余剰燃料の溢流速度によっても
変化するので、ロータ1の回転数十噴射/時期決定燃料
量の影響を受けて噴射の安定性を欠くことになるという
欠点をもっていた。Furthermore, since the amount of introduced fuel changes depending on the overflow speed of surplus fuel, there is a drawback that the injection stability is affected by the number of revolutions of the rotor 1 and the amount of fuel determined at the injection timing.
本発明は従来技術の欠点を解消して安定し九燃料噴射量
を得ることができる燃料噴射ポンプの余剰燃料排出装置
を提供することを目的とし、その特徴とするところは、
燃料噴射期間の終了時期にフリーピストンが移動すると
共に開弁し、噴射時期制御用の燃料を急速に流出させる
弁機構をフリーピストンに設は九ことにおる。An object of the present invention is to provide a surplus fuel discharge device for a fuel injection pump that can eliminate the drawbacks of the prior art and provide a stable fuel injection amount, and is characterized by:
The free piston is provided with a valve mechanism that opens as the free piston moves at the end of the fuel injection period and rapidly allows fuel for injection timing control to flow out.
第8図は本発明の一実施例である燃料噴射ポンプの要部
断面図で6D%第1図と同じ部分には同一符号を付しで
ある。この場合はフリーピストン50内に移動可能な弁
体51を収容しているが、弁体51とフリーピストン5
0とは気密に嵌合しているので、第1加圧室4から第2
加圧室6への燃料の移動は生じない、を九、7リーピス
トン50内に収容した弁体51の鍔部はリング54に係
止されたばね53で押されて弁座に密着し、燃料の流通
を阻止している。FIG. 8 is a sectional view of a main part of a fuel injection pump according to an embodiment of the present invention, and the same parts as in FIG. 1 are given the same reference numerals. In this case, a movable valve body 51 is housed in the free piston 50, but the valve body 51 and the free piston 5
0 is airtightly fitted, so that the first pressure chamber 4 can be
The flange of the valve body 51 accommodated in the piston 50 is pressed by the spring 53 secured to the ring 54 and comes into close contact with the valve seat, so that the fuel does not move to the pressurizing chamber 6. It is blocking the distribution of.
しかるにフリーピストン50が右方に移動して噴射終了
余剰燃料排出の段階になると、弁体51の先端がストッ
パ7の先端に接触して弁体51の鍔が弁座から離れて排
出口52よシgi流通路30に余剰燃料が渡れる。この
場合の溢流口29およびaa通路30は第1図のものよ
〕も大径の孔としであるので、これを介して急速に余剰
燃料を流出させることができる。However, when the free piston 50 moves to the right and reaches the stage where injection is completed and surplus fuel is discharged, the tip of the valve body 51 comes into contact with the tip of the stopper 7, and the collar of the valve body 51 separates from the valve seat and exits from the discharge port 52. Surplus fuel can cross over to the fuel flow path 30. In this case, the overflow port 29 and the aa passage 30 are larger-diameter holes than those in FIG. 1, so that excess fuel can rapidly flow out through these holes.
例えば弁体51の鍔が接触しているシート部の径を4■
とし、弁体51とシート部との隙間が0.1■であると
すると、燃料が流通する流路断面積は、L26■倉とな
る。しかも、この流路を通った燃料はこれ以上の断面積
をもっている排出口52および溢流口29.溢l51I
逸路30から容易に迅速に排出することができる。For example, the diameter of the seat portion that the flange of the valve body 51 is in contact with is 4mm.
Assuming that the gap between the valve body 51 and the seat portion is 0.1 cm, the cross-sectional area of the flow path through which fuel flows will be L26 cm. Furthermore, the fuel that has passed through this flow path has a larger cross-sectional area than the exhaust port 52 and the overflow port 29. Overflow l51I
It can be easily and quickly discharged from the escape route 30.
これに対して従来のフリーピストン5では、溢流口29
の直径を3sIとし、フリーピストン5がα6■移動し
て溢流部を作り九としてもα998謹8の面積としかな
らない。On the other hand, in the conventional free piston 5, the overflow port 29
If the diameter of the free piston 5 is 3sI, and if the free piston 5 moves α6■ to create an overflow part, the area will only be α998min8.
即ち、本実施例の場合はフリーピストン50の僅かな移
動で迅速に余剰燃料の排出が可能となる。That is, in the case of this embodiment, surplus fuel can be quickly discharged by a slight movement of the free piston 50.
なお、噴射の終夛はフリーピストン50の定まった位置
で行われるので、排出口52が溢流口29に対向するよ
うに選定することが容易である。Note that since the end of the injection is performed at a fixed position of the free piston 50, it is easy to select the discharge port 52 to face the overflow port 29.
本実施例の余剰燃料排出装置は、内部に鍔付きの弁体を
設定してフリーピストンの最大移動時にはストッパに弁
体が接触するように構成し、鍔がシート部から僅かに離
れた状態でも比較的多量の余剰燃料を短時間で排出する
ことができる。したがって、第2加圧塞よシ噴出される
燃料量の精度も向上する。更に、吐出通路23の開弁前
後でフリーピストン50が右方に圧力を受ける面積の増
大が行われるので、余剰燃料排出時の振動現象が抑制さ
れ、噴射弁までの高圧管内圧力を急速に低下安定させる
ので、2次噴射等の防止に役立ち、燃料噴射の安定性を
向上させることができる等の効果が得られる。The surplus fuel discharge device of this embodiment is configured such that a valve body with a flange is set inside so that the valve body contacts the stopper when the free piston moves at its maximum, and even when the flange is slightly separated from the seat part. A relatively large amount of surplus fuel can be discharged in a short time. Therefore, the accuracy of the amount of fuel injected by the second pressurized plug is also improved. Furthermore, since the area where the free piston 50 receives pressure to the right before and after opening the discharge passage 23 is increased, the vibration phenomenon when excess fuel is discharged is suppressed, and the pressure inside the high-pressure pipe up to the injection valve is rapidly reduced. Since it is stabilized, it helps to prevent secondary injection and the like, and effects such as being able to improve the stability of fuel injection can be obtained.
本発明の燃料噴射ポンプの余剰燃料排出装置は、余剰燃
料の排出処理を迅速に行うことが可能となシ、安定した
燃料噴射量を得ることができるという効果が得られる。The surplus fuel discharge device for a fuel injection pump according to the present invention has the advantage that surplus fuel can be discharged quickly and a stable fuel injection amount can be obtained.
第1図は従来の燃料噴射ポンプの断面図、第2図〜第7
図は第1図の燃料噴射ポンプの動作説明図、第8図は本
発明の一実施例である燃料噴射ポンプの要部断面図であ
る。
1・・・ロータ、2・・・プランジャ、3・・・カムリ
ング、4・・・第1加圧室、5.50・・・フリーピス
トン、6・・・M2加EE’M、?・・・ストッパ、8
・・・ローラシュー、9・・・ローラ、10・・・ハウ
ジング、11・・・第1放射通路、12・・・第2放射
通路、13・・・第1固定通路、14・・・第2固定通
路、15= 16・・・電磁弁、17・・・弁体、23
・・・吐出通路、24−・・出力通路、25・・・接続
口、26・・・パルサ、27・・・検出器、29−・・
溢流口、30.31・・・溢流通路、32・・・排出通
路、41・・・スリーブホルダ、42・・・スリーブ、
43・・・燃料供給口、51・・・弁体、52・・・排
出口、53・・・第 l 閉
第 2 区
(0、)(?ジ
第 5 鼎Figure 1 is a sectional view of a conventional fuel injection pump, Figures 2 to 7
This figure is an explanatory view of the operation of the fuel injection pump shown in FIG. 1, and FIG. 8 is a sectional view of a main part of the fuel injection pump which is an embodiment of the present invention. 1... Rotor, 2... Plunger, 3... Cam ring, 4... First pressurizing chamber, 5.50... Free piston, 6... M2 application EE'M,? ...Stopper, 8
...Roller shoe, 9...Roller, 10...Housing, 11...First radiation passage, 12...Second radiation passage, 13...First fixed passage, 14...No. 2 fixed passage, 15 = 16... solenoid valve, 17... valve body, 23
...Discharge passage, 24-...Output passage, 25...Connection port, 26...Pulser, 27...Detector, 29-...
Overflow port, 30. 31... Overflow passage, 32... Discharge passage, 41... Sleeve holder, 42... Sleeve,
43...Fuel supply port, 51...Valve body, 52...Discharge port, 53...1th closed 2nd section (0,) (?ji 5th ding)
Claims (1)
、このフリーピストンで仕切られ九一方の室には噴射量
に関係する燃料を供給し、他方の室には噴射時期に関係
する燃料を供給するごとく構成した燃料噴射ポンプにお
いて、燃料噴射期間の終了時期に上記フリーピストンが
移動すると共に開弁し、噴射時期制御用の燃料を急速に
流出させる弁機構を上記フリーピストンに設けたことt
−特徴とする燃IP+噴射ポンプの余剰燃料排出装置。 2、上記弁機構が、上記噴射量に関係する燃、科を収容
した室に移動可能な弁体の先熾を突出させ、上記燃料噴
射期間の終了時期に上記弁体がストッパに接触して弁座
よ〕離れ、上記噴射時期に関係する燃料を溢流口よ〕流
出させる機構である特許請求の範囲第1項記載の燃料噴
射ポンプの余剰燃料排出装置。[Claims] 1. A movable 7-Lee piston is installed in a high-pressure fuel chamber, which is partitioned by this free piston, and one chamber is supplied with fuel related to the injection amount, and the other chamber is In a fuel injection pump configured to supply fuel related to injection timing, the free piston moves and opens at the end of the fuel injection period, and the valve mechanism is configured to rapidly flow out fuel for injection timing control. What is provided on the free piston?
- Features a fuel IP + injection pump surplus fuel discharge device. 2. The valve mechanism causes a tip of a movable valve body to protrude into a chamber containing fuel related to the injection amount, and the valve body contacts a stopper at the end of the fuel injection period. 2. The surplus fuel discharge device for a fuel injection pump according to claim 1, which is a mechanism for separating fuel related to the injection timing from the valve seat and flowing out the fuel related to the injection timing from the overflow port.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12568681A JPS5827873A (en) | 1981-08-10 | 1981-08-10 | Excess fuel discharge device for fuel injection pump |
| EP82106366A EP0071800A3 (en) | 1981-08-10 | 1982-07-15 | Fuel injection pump for internal combustion engine having improved excess fuel discharger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12568681A JPS5827873A (en) | 1981-08-10 | 1981-08-10 | Excess fuel discharge device for fuel injection pump |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5827873A true JPS5827873A (en) | 1983-02-18 |
| JPH02544B2 JPH02544B2 (en) | 1990-01-08 |
Family
ID=14916166
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12568681A Granted JPS5827873A (en) | 1981-08-10 | 1981-08-10 | Excess fuel discharge device for fuel injection pump |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP0071800A3 (en) |
| JP (1) | JPS5827873A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5835260A (en) * | 1981-08-28 | 1983-03-01 | Hitachi Ltd | Distribution-type fuel injection pump |
| JPS5853669A (en) * | 1981-09-28 | 1983-03-30 | Hitachi Ltd | Fuel injection pump device for internal-combustion engine |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1162494A (en) * | 1966-03-22 | 1969-08-27 | Cav Ltd | Liquid Fuel Injection Pumping Apparatus for Supplying Fuel to Internal Combustion Engines. |
| US3489093A (en) * | 1968-09-11 | 1970-01-13 | Cav Ltd | Liquid fuel pumping apparatus |
| US3704963A (en) * | 1971-02-03 | 1972-12-05 | Stanadyne Inc | Fuel pump |
| US4185779A (en) * | 1978-01-16 | 1980-01-29 | The Bendix Corporation | Fuel injector |
-
1981
- 1981-08-10 JP JP12568681A patent/JPS5827873A/en active Granted
-
1982
- 1982-07-15 EP EP82106366A patent/EP0071800A3/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| EP0071800A3 (en) | 1984-01-18 |
| EP0071800A2 (en) | 1983-02-16 |
| JPH02544B2 (en) | 1990-01-08 |
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