JPH02267363A - Fuel injection valve - Google Patents
Fuel injection valveInfo
- Publication number
- JPH02267363A JPH02267363A JP9033989A JP9033989A JPH02267363A JP H02267363 A JPH02267363 A JP H02267363A JP 9033989 A JP9033989 A JP 9033989A JP 9033989 A JP9033989 A JP 9033989A JP H02267363 A JPH02267363 A JP H02267363A
- Authority
- JP
- Japan
- Prior art keywords
- valve
- fuel
- needle valve
- pressure chamber
- back pressure
- 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.)
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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】
[産業上の利用分野]
本発明は燃料噴射弁に関し、特にエンジン回転数および
負荷の広い変化範囲で最適燃料噴射を行なう燃料噴射弁
に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a fuel injection valve, and more particularly to a fuel injection valve that performs optimal fuel injection over a wide range of changes in engine speed and load.
[従来の技術]
車両エンジンの燃料噴射を行なう場合、排気エミッショ
ンの改善や省燃費の点で、噴射初期に噴射量を抑え、あ
るいは特に低速走行時には主噴射に先立ってパイロット
噴射を行なう事が有効である。[Prior art] When injecting fuel into a vehicle engine, it is effective to reduce the amount of injection at the initial stage of injection, or to perform pilot injection prior to main injection, especially when driving at low speeds, in terms of improving exhaust emissions and saving fuel consumption. It is.
そこで例えば特開昭63−120851号公報では、燃
料噴射孔を開閉するニードル弁の背後に背圧室を設ける
とともに、該背圧室への圧力燃料の供給を制御し、燃料
圧で作動せしめられる他のニードル弁を設けて、パイロ
ット噴射を実現した燃料噴射弁が提案されている。Therefore, for example, in Japanese Patent Application Laid-open No. 120851/1985, a back pressure chamber is provided behind a needle valve that opens and closes a fuel injection hole, and the supply of pressurized fuel to the back pressure chamber is controlled so that it is operated by the fuel pressure. A fuel injection valve that realizes pilot injection by providing another needle valve has been proposed.
[発明が解決しようとする課題]
しかしながら、上記従来の燃料噴射弁は、背圧室への加
圧燃料の供給制御を、機械的に作動するニードル弁によ
っている為、エンジン回転数の広い範囲での変化に対応
するのが困難であるという問題がある。[Problems to be Solved by the Invention] However, the conventional fuel injection valve described above uses a mechanically operated needle valve to control the supply of pressurized fuel to the back pressure chamber, so it cannot be used over a wide range of engine speeds. The problem is that it is difficult to respond to changes in
そこで、本発明はかかる課題を解決するもので、エンジ
ンの運転状態の広い変化範囲で常に最適な燃料噴射パタ
ーンを実現できる燃料噴射弁を提供することを目的とす
る。SUMMARY OF THE INVENTION The present invention has been made to solve this problem, and it is an object of the present invention to provide a fuel injection valve that can always achieve an optimal fuel injection pattern over a wide range of changes in engine operating conditions.
[課題を解決するための手段]
本発明の構成を第1図で説明すると、燃料噴射弁は、弁
ハウジング1に設けた燃料噴射孔11を先端弁部21に
より開閉するニードル弁2と、該ニードル弁2の基端2
2面に接して上記弁ハウジング1内に形成され、ニード
ル弁2を閉鎖方向へ付勢する背圧室12と、背圧室12
内に設けられて上記ニードル弁2を閉鎖方向へ付勢する
バネ部材4と、燃料噴射ポンプから送給される加圧燃料
を上記ニードル弁2の受圧面2aに供給してニードル弁
2を開放方向へ作動せしめる第1供給流路13と、上記
加圧燃料を上記背圧室12へ供給する第2供給流路14
と、途中に絞り部151を有し、上記背圧室12の加圧
燃料を排出する排出流路15と、上記第2供給流路14
を開閉する電磁開閉弁3と、上記加圧燃料の送給サイク
ルの所定タイミングで上記電磁開閉弁3を開閉作動せし
める駆動手段5とを具備している。[Means for Solving the Problems] The configuration of the present invention will be explained with reference to FIG. 1. The fuel injection valve includes a needle valve 2 that opens and closes a fuel injection hole 11 provided in a valve housing 1 with a tip valve portion 21, and a needle valve 2 that opens and closes a fuel injection hole 11 provided in a valve housing 1. Base end 2 of needle valve 2
A back pressure chamber 12 formed in the valve housing 1 in contact with two surfaces and urging the needle valve 2 in the closing direction;
A spring member 4 is provided inside to bias the needle valve 2 in the closing direction, and pressurized fuel supplied from the fuel injection pump is supplied to the pressure receiving surface 2a of the needle valve 2 to open the needle valve 2. a first supply passage 13 for operating the pressurized fuel to the back pressure chamber 12; and a second supply passage 14 for supplying the pressurized fuel to the back pressure chamber 12.
, a discharge passage 15 having a constriction part 151 in the middle and discharging the pressurized fuel from the back pressure chamber 12; and the second supply passage 14.
The electromagnetic on-off valve 3 opens and closes the electromagnetic on-off valve 3, and a driving means 5 that opens and closes the electromagnetic on-off valve 3 at a predetermined timing of the pressurized fuel supply cycle.
[作用]
加圧燃料の圧力は送給サイクルの開始より次第に上昇し
、最大に達しな後、次第に低下する。送給サイクルの開
始時には上記電磁開閉弁3は閉じられており、背圧室1
2は加圧燃料が排出流路15により排出されて、低圧と
なっている。[Operation] The pressure of the pressurized fuel gradually increases from the beginning of the feeding cycle, and after reaching the maximum, gradually decreases. At the start of the feeding cycle, the electromagnetic on-off valve 3 is closed, and the back pressure chamber 1 is closed.
2, the pressurized fuel is discharged through the discharge passage 15 and has a low pressure.
この状態で、加圧燃料の圧力が上昇すると、第1供給流
路13を経て上記圧力を受圧面2aに受けたニードル弁
2は、上記バネ部材4の付勢力に抗して開放され、燃料
が噴射される。駆動手段5により適当タイミングで上記
電磁開閉弁3を開放作動せしめると、加圧燃料が第2供
給流路14を経て背圧室12へ供給され、排出流路15
には絞り部151が設けであることにより、背圧室12
の内圧は上昇する。この内圧上昇により、ニードル弁2
は閉鎖方向へ付勢され、−旦これが完全閉鎖し、あるい
はその開度が小さく維持されて、主噴射に先立つパイロ
ット噴射あるいは噴射率の小さい初期噴射が所定量なさ
れる。In this state, when the pressure of the pressurized fuel increases, the needle valve 2, which receives the pressure on the pressure receiving surface 2a through the first supply channel 13, opens against the biasing force of the spring member 4, and the fuel is injected. When the electromagnetic on-off valve 3 is opened at an appropriate timing by the driving means 5, pressurized fuel is supplied to the back pressure chamber 12 via the second supply channel 14, and the fuel is supplied to the back pressure chamber 12 through the second supply channel 14.
Since the throttle part 151 is provided in the back pressure chamber 12
The internal pressure of increases. Due to this increase in internal pressure, the needle valve 2
is biased in the closing direction, and once it is completely closed or its opening degree is kept small, a predetermined amount of pilot injection or initial injection with a small injection rate is performed prior to the main injection.
所定時間後に上記電磁開閉弁3を閉鎖作動せしめると、
背圧室12への加圧燃料供給は停止し、背圧室12内の
加圧燃料は絞り部151を有する排出流路15より漸次
排出されて、背圧室12の内圧が次第に低下する。この
状態で加圧燃料の圧力はさらに上昇するから、ニードル
弁2は再び開放され、あるいはその開度が大きくなって
、主噴射が行われる。When the electromagnetic on-off valve 3 is closed after a predetermined time,
The supply of pressurized fuel to the back pressure chamber 12 is stopped, the pressurized fuel in the back pressure chamber 12 is gradually discharged from the discharge passage 15 having the constriction part 151, and the internal pressure of the back pressure chamber 12 is gradually reduced. In this state, the pressure of the pressurized fuel further increases, so the needle valve 2 is opened again or its opening degree is increased, and main injection is performed.
加圧燃料の圧力が最大近くになった時に、上記電磁開閉
弁3を再び開放作動せしめると、背圧室12の内圧は再
び増大するが、ニードル弁2の受圧面2aに印加されて
いる加圧燃料の圧力が大きい為、ニードル弁2は閉鎖し
ない。所定量の燃料が噴射され、噴射の終了行程でその
圧力が漸次低くなって所定値を下回ると、バネ部材4の
バネ力および背圧室12の内圧により閉鎖方向へ強く付
勢されているニードル弁2は急速に閉鎖し、精度の良い
燃料調量がなされる。If the electromagnetic on-off valve 3 is opened again when the pressure of the pressurized fuel approaches the maximum, the internal pressure in the back pressure chamber 12 increases again, but the pressure applied to the pressure receiving surface 2a of the needle valve 2 increases. Since the pressure of the pressurized fuel is high, the needle valve 2 does not close. When a predetermined amount of fuel is injected and the pressure gradually decreases to below a predetermined value in the final stroke of the injection, the needle is strongly urged in the closing direction by the spring force of the spring member 4 and the internal pressure of the back pressure chamber 12. Valve 2 closes rapidly, providing accurate fuel metering.
加圧燃料の圧力がさらに低下すると、電磁開閉弁3は閉
じられ、背圧室12の加圧燃料が排出流路15より漸次
排出されて、背圧室12の内圧が低下する。この状態で
次の送給サイクルの開始を待つ。When the pressure of the pressurized fuel further decreases, the electromagnetic on-off valve 3 is closed, the pressurized fuel in the back pressure chamber 12 is gradually discharged from the discharge passage 15, and the internal pressure of the back pressure chamber 12 decreases. In this state, wait for the start of the next feeding cycle.
[第1実施例]
第1図において、筒状の弁ハウジング1の下端部には、
先端に燃料噴射孔11を設けた筒状のノズルボデー16
が連結され、ノズルボデー16内には、上下に摺動自在
にニードル弁2が配設されて、その先端弁部21により
上記燃料噴射孔11が開閉される。[First embodiment] In FIG. 1, the lower end of the cylindrical valve housing 1 includes:
A cylindrical nozzle body 16 with a fuel injection hole 11 at its tip
A needle valve 2 is disposed inside the nozzle body 16 so as to be slidable up and down, and the fuel injection hole 11 is opened and closed by the tip valve portion 21 of the needle valve 2 .
上記ニードル弁2の基端に当接せしめた押圧部材22の
端面が臨む弁ハウジング1内には背圧室12が形成され
、該背圧室12内には一端を上記押圧部材22の端面に
当接せしめてコイルバネ4が設けられて、ニードル弁2
を下方の閉鎖方向へ付勢している。A back pressure chamber 12 is formed in the valve housing 1 facing the end surface of the pressing member 22 that is brought into contact with the proximal end of the needle valve 2. A coil spring 4 is provided in contact with the needle valve 2.
is biased downward in the closing direction.
上記弁ハウジング1の側面には加圧燃料の供給ボート1
7が突出形成され、ここへ閃格の燃料噴射ポンプより加
圧燃料が送給される。上記供給ポート17より弁ハウジ
ング1内を下方へ第1供給流路13が設けられて、その
先端は上記ニードル弁2の受圧面2a周りの環状溝に至
っている。上記供給ボート17からは上方へ第2供給流
路14が分岐され、これは途中で下方へ屈曲して上記背
圧室12へ開口している。A pressurized fuel supply boat 1 is provided on the side of the valve housing 1.
7 is formed protrudingly, to which pressurized fuel is fed from a flash-rated fuel injection pump. A first supply passage 13 is provided downward in the valve housing 1 from the supply port 17, and its tip reaches an annular groove around the pressure receiving surface 2a of the needle valve 2. A second supply channel 14 branches upward from the supply boat 17, bends downward midway, and opens into the back pressure chamber 12.
上記弁ハウジング1の上端部には電磁開閉弁3を内設し
た止栓部材18が固着され、上記電磁開閉弁3は、上記
供給流路14の屈曲部に先端弁部を位置せしめた補助ニ
ードル弁31と、これを上方へ吸引する電磁コイル32
より構成されている。A stopper member 18 having an electromagnetic on-off valve 3 installed therein is fixed to the upper end of the valve housing 1. A valve 31 and an electromagnetic coil 32 that attracts the valve upward.
It is composed of
上記補助ニードル弁31の基端は、弁ハウジング1外の
りザーバタンク6へ通じる低圧室19内にあり、この低
圧室19内に設けたコイルバネ33により補助ニードル
弁31は下方へ付勢されて上記供給流路14を閉じてい
る。The base end of the auxiliary needle valve 31 is located in a low pressure chamber 19 communicating with the reservoir tank 6 outside the valve housing 1, and the auxiliary needle valve 31 is biased downward by a coil spring 33 provided in the low pressure chamber 19 to supply the above-mentioned gas. The flow path 14 is closed.
上記電磁コイル32は弁ハウジング1外の駆動回路5に
接続され、駆動回路5は後述する如く、エンジン回転数
およびその負荷状態に応じて、燃料ポンプからの加圧燃
料送給サイクルの所定タイミングで上記電磁コイル32
に通電し、補助ニードル弁31を開放作動せしめる。The electromagnetic coil 32 is connected to a drive circuit 5 outside the valve housing 1, and the drive circuit 5 operates at a predetermined timing in the pressurized fuel supply cycle from the fuel pump depending on the engine rotation speed and its load condition, as will be described later. The electromagnetic coil 32
energizes to open the auxiliary needle valve 31.
上記弁ハウジング1と止栓部材18を貫通して排出流路
15が設けられ、該流路15は上記背圧室12と低圧室
19を連通ずるとともに、途中に絞り部材151が配設
しである。A discharge flow path 15 is provided passing through the valve housing 1 and the stopper member 18, and the flow path 15 communicates the back pressure chamber 12 and the low pressure chamber 19, and a throttle member 151 is disposed in the middle. be.
上記構造の燃料噴射弁の作動を、第2図を参照しつつ、
以下に説明する。The operation of the fuel injection valve having the above structure is explained below with reference to FIG.
This will be explained below.
加圧燃料の圧力は送給サイクルの開始より次第に上昇し
、最大に達した後、次第に低下する(第2図(1))。The pressure of the pressurized fuel gradually increases from the start of the feeding cycle, reaches a maximum, and then gradually decreases (FIG. 2 (1)).
加圧燃料の送給サイクル前には、上記電磁コイル32へ
の通電は停止されており、補助ニードル弁31がコイル
バネ33の付勢力で下方へ押し下げられて第2供給流路
14を閉じている(以下、この状態を電磁開閉弁閉鎖と
いう)。Before the pressurized fuel supply cycle, the electromagnetic coil 32 is de-energized, and the auxiliary needle valve 31 is pushed down by the urging force of the coil spring 33 to close the second supply flow path 14. (Hereinafter, this state will be referred to as the solenoid valve closed).
この状態では、背圧室12は加圧燃料が排出流路15に
より排出されて、低圧となっている(第2図(3))。In this state, the pressurized fuel is discharged from the back pressure chamber 12 through the discharge passage 15, and the pressure in the back pressure chamber 12 is low ((3) in FIG. 2).
ここで燃料送給サイクルが開始され、加圧燃料の圧力が
上昇すると、第1供給流路13を経て上記圧力がニード
ル弁2の受圧面2aに与えられ、ニードル弁2は、上記
バネ部材4の付勢力に抗して開放されて、燃料が噴射さ
れる(第2図(1)A点、同図(4)、(5))。駆動
回路5より適当タイミングで上記電磁コイル32へ通電
すると、補助ニードル弁31がコイルバネ33の付勢力
に抗して上方へ吸引され(第2図B点、同図(2))上
記供給流路14を開放する(以下、この状態を電磁開閉
弁開放という)。When the fuel supply cycle is started and the pressure of the pressurized fuel increases, the pressure is applied to the pressure receiving surface 2a of the needle valve 2 through the first supply flow path 13, and the needle valve 2 It is opened against the urging force of , and fuel is injected (point A in FIG. 2 (1), (4) and (5) in the same figure). When the electromagnetic coil 32 is energized from the drive circuit 5 at an appropriate timing, the auxiliary needle valve 31 is attracted upward against the biasing force of the coil spring 33 (point B in FIG. 2, (2) in the same figure) and the supply flow path is drawn upward. 14 (hereinafter, this state will be referred to as the electromagnetic on-off valve open).
上記電磁開閉弁3が開放されると、加圧燃料が供給流路
14を経て背圧室12へ供給される。排出流路15には
絞り部材151が設けであることにより、背圧室12の
内圧は加圧燃料の流入に伴い上昇する(第2図(3))
。この内圧上昇により、ニードル弁2は閉鎖方向へ付勢
され、−旦これが完全閉鎖する(第2図(4)0点〉。When the electromagnetic on-off valve 3 is opened, pressurized fuel is supplied to the back pressure chamber 12 via the supply channel 14. Since the exhaust flow path 15 is provided with the throttle member 151, the internal pressure of the back pressure chamber 12 increases with the inflow of pressurized fuel (Fig. 2 (3)).
. This increase in internal pressure urges the needle valve 2 in the closing direction, and it is then completely closed (point 0 in FIG. 2 (4)).
かくして、主噴射に先立つパイロット噴射が所定量なさ
れる。Thus, a predetermined amount of pilot injection is performed prior to the main injection.
所定時間後に上記駆動回路は電磁開閉弁3を閉鎮作動せ
しめる(第2図(1)D点、同図(2))。After a predetermined time, the drive circuit closes the electromagnetic on-off valve 3 (point D in FIG. 2 (1), point D in the same figure (2)).
背圧室12への加圧燃料供給は停止し、背圧室12内の
加圧燃料は絞り部材151を設けた排出流路15より漸
次排出されて、背圧室12の内圧は次第に低下する(第
2図(3)〉。この状態で燃料圧はさらに上昇するから
、ニードル弁2は再び開放され(第2図(1)E点、同
図(4)、(5))、主噴射が行われる。The supply of pressurized fuel to the back pressure chamber 12 is stopped, and the pressurized fuel in the back pressure chamber 12 is gradually discharged from the discharge passage 15 provided with the throttle member 151, and the internal pressure of the back pressure chamber 12 gradually decreases. (Figure 2 (3)) In this state, the fuel pressure increases further, so the needle valve 2 is opened again (Figure 2 (1) point E, Figure 2 (4), (5)), and the main injection will be held.
燃料圧が最大近くになった時に、上記電磁開閉弁3を再
び開放作動せしめるとく第2図(1)F点、同図(2)
)、背圧室12の内圧は再び増大するが(第2図(3)
)、ニードル弁2の受圧面2aに印加されている燃料圧
が大きい為、ニードル弁2は閉鎖しない。When the fuel pressure approaches the maximum, the electromagnetic on-off valve 3 is opened again. Point F in Figure 2 (1) and Point F in Figure 2 (2)
), the internal pressure of the back pressure chamber 12 increases again (Fig. 2 (3)
), the needle valve 2 does not close because the fuel pressure applied to the pressure receiving surface 2a of the needle valve 2 is large.
所定量の燃料が噴射され、噴射の終了行程でその圧力が
漸次低くなって所定値を下回ると(第2図(1)G点)
、バネ部材4のバネ力および背圧室12の内圧により閉
鎖方向へ強く付勢されているニードル弁2は急速に閉鎖
し、燃料噴射が即座に停止して精度の良い燃料調量がな
される。When a predetermined amount of fuel is injected and the pressure gradually decreases to below the predetermined value in the end stroke of injection (point G in Figure 2 (1))
The needle valve 2, which is strongly biased in the closing direction by the spring force of the spring member 4 and the internal pressure of the back pressure chamber 12, rapidly closes, and fuel injection is immediately stopped, allowing accurate fuel metering. .
加圧燃料の圧力がさらに低下すると、電磁開閉弁3は閉
じられ(第2図H点、同図(2>)、背圧室12の加圧
燃料が排出流路15の絞り部材151を経て漸次排出さ
れて、背圧室12の内圧が低下する。この状態で次の送
給サイクルの開始を待つ。When the pressure of the pressurized fuel further decreases, the electromagnetic on-off valve 3 is closed (point H in FIG. It is gradually discharged and the internal pressure of the back pressure chamber 12 decreases.In this state, the next feeding cycle is waited for.
かくの如く、上記構造の燃料噴射弁によれば、駆動回路
により作動せしめらせる電磁開閉弁により、車両エンジ
ンの運転状態の変化に応じて、広い範囲でパイロット噴
射と主噴射を最適タイミングで行うことができる。As described above, according to the fuel injection valve having the above structure, the pilot injection and the main injection are performed at the optimum timing over a wide range according to changes in the operating condition of the vehicle engine by means of the electromagnetic on-off valve operated by the drive circuit. be able to.
なお、本実施例で、最初の電磁コイル32への通電量を
調整して、補助ニードル弁31の開度を小さくなせば、
ニードル弁21は完全には閉鎖されず、噴射率の抑えら
れた初期噴射となる。In this embodiment, if the amount of current applied to the first electromagnetic coil 32 is adjusted to reduce the opening degree of the auxiliary needle valve 31,
The needle valve 21 is not completely closed, resulting in initial injection with a suppressed injection rate.
[第2実施例コ
第3図には電磁開閉弁3の他の構造を示す。本実施例で
は、コイルバネ33のバネ力を小さくなすとともに、電
磁コイル32を補助ニードル弁31の基端よりも下方に
設けて、電磁コイル33により上記補助ニードル弁31
を下方へ閉鎖吸引する。[Second Embodiment FIG. 3 shows another structure of the electromagnetic on-off valve 3. In this embodiment, the spring force of the coil spring 33 is reduced, and the electromagnetic coil 32 is provided below the base end of the auxiliary needle valve 31, so that the electromagnetic coil 33
Close and suction downward.
この場合の作動を上記第2図により説明する。The operation in this case will be explained with reference to FIG. 2 above.
加圧燃料の圧力が上昇すると同図のB点で補助ニードル
弁31は押し上げられて開放する。パイロット噴射終了
後、電磁コイル32へ通電すると、補助ニードル弁31
は下方へ吸引されて閉鎖状態となる(第2図り点)。When the pressure of the pressurized fuel increases, the auxiliary needle valve 31 is pushed up and opened at point B in the figure. After the pilot injection is completed, when the electromagnetic coil 32 is energized, the auxiliary needle valve 31
is sucked downward and becomes closed (second target point).
続いてF点で上記電磁コイル32への通電を停止すると
、補助ニードル弁31は燃料圧により再び開放される。Subsequently, when the power supply to the electromagnetic coil 32 is stopped at point F, the auxiliary needle valve 31 is opened again by the fuel pressure.
そして、燃料送給サイクルの終了近くで燃料圧が十分低
下すると(第2図H点〉、補助ニードル弁31はコイル
バネ33により閉鎖される。When the fuel pressure drops sufficiently near the end of the fuel supply cycle (point H in FIG. 2), the auxiliary needle valve 31 is closed by the coil spring 33.
なお、上記各実施例において、バネで付勢されたストッ
パ部材を設けて、パイロット噴射時には、ニードル弁2
の基端が上記ストッパ部材に当接してその上昇が規制さ
れることにより噴射量が抑えられ、燃料圧が上昇する主
噴射時には、ニードル弁2が上記ストッパ部材を押し上
げて上昇し、全開噴射する如き構成も採用できる。In each of the above embodiments, a stopper member biased by a spring is provided so that the needle valve 2 is closed during pilot injection.
The injection amount is suppressed by the base end coming into contact with the stopper member and its rise is restricted, and during main injection when the fuel pressure increases, the needle valve 2 pushes up the stopper member and rises, resulting in a fully open injection. A configuration like this can also be adopted.
[発明の効果]
以上の如く、本発明の燃料噴射弁は、ニードル弁を閉鎖
方向へ付勢する背圧室への加圧燃料の流入を制御する電
磁開閉弁を設けたことにより、広いエンジン運転領域に
おいて、最適な燃料噴射特性を実現できるものである。[Effects of the Invention] As described above, the fuel injection valve of the present invention is equipped with an electromagnetic on-off valve that controls the inflow of pressurized fuel into the back pressure chamber that urges the needle valve in the closing direction, so that it can be used in a wide range of engines. This makes it possible to achieve optimal fuel injection characteristics in the operating range.
第1図および第2図は本発明の第1実施例を示し、第1
図は燃料噴射弁の全体縦断面図、第2図はその作動を示
すタイムチャート、第3図は本発明の第2実施例を示す
燃料噴射弁の全体縦断面図である。
1・・・弁ハウジング
11・・・燃料噴射孔
12・・・背圧室
13・・・第1供給流路
14・・・第2供給流路
15・・・排出流路
151・・・絞り部材(絞り部)
19・・・低圧室
2・・・ニードル弁
2a・・・受圧面
21・・・先端弁部
22・・・押圧部材(基端)
3・・・電磁開閉弁
31・・・補助ニードル弁
32・・・電磁コイル
4・・・コイルバネ(バネ部材)
5・・・駆動回路(駆動手段)
6・・・リザーバタンク
時
間1 and 2 show a first embodiment of the present invention;
2 is a time chart showing its operation, and FIG. 3 is a longitudinal sectional view of the entire fuel injection valve showing a second embodiment of the present invention. 1... Valve housing 11... Fuel injection hole 12... Back pressure chamber 13... First supply channel 14... Second supply channel 15... Discharge channel 151... Throttle Member (throttle part) 19...Low pressure chamber 2...Needle valve 2a...Pressure receiving surface 21...Tip valve part 22...Press member (base end) 3...Solenoid shut-off valve 31...・Auxiliary needle valve 32...Electromagnetic coil 4...Coil spring (spring member) 5...Drive circuit (drive means) 6...Reservoir tank time
Claims (1)
するニードル弁と、該ニードル弁の基端面に接して上記
弁ハウジング内に形成され、ニードル弁を閉鎖方向へ付
勢する背圧室と、背圧室内に設けられて上記ニードル弁
を閉鎖方向へ付勢するバネ部材と、燃料噴射ポンプから
送給される加圧燃料を上記ニードル弁の受圧面に供給し
てニードル弁を開放方向へ作動せしめる第1供給流路と
、上記加圧燃料を上記背圧室へ供給する第2供給流路と
、途中に絞り部を有し、上記圧力室の加圧燃料を排出す
る排出流路と、上記第2供給流路を開閉する電磁開閉弁
と、上記加圧燃料送給サイクルの所定タイミングで、上
記電磁開閉弁を開閉作動せしめる駆動手段とを具備する
燃料噴射弁。a needle valve that opens and closes a fuel injection hole provided in a valve housing with a tip valve portion; a back pressure chamber that is formed in the valve housing in contact with a proximal end surface of the needle valve and biases the needle valve in a closing direction; A spring member provided in a back pressure chamber biases the needle valve in the closing direction, and pressurized fuel supplied from a fuel injection pump is supplied to the pressure receiving surface of the needle valve to operate the needle valve in the opening direction. a first supply flow path that supplies the pressurized fuel to the back pressure chamber; a discharge flow path that has a constriction part in the middle and discharges the pressurized fuel from the pressure chamber; A fuel injection valve comprising: an electromagnetic on-off valve that opens and closes the second supply flow path; and a drive means that opens and closes the electromagnetic on-off valve at a predetermined timing of the pressurized fuel supply cycle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9033989A JPH02267363A (en) | 1989-04-10 | 1989-04-10 | Fuel injection valve |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9033989A JPH02267363A (en) | 1989-04-10 | 1989-04-10 | Fuel injection valve |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02267363A true JPH02267363A (en) | 1990-11-01 |
Family
ID=13995763
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9033989A Pending JPH02267363A (en) | 1989-04-10 | 1989-04-10 | Fuel injection valve |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02267363A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0726390A1 (en) * | 1995-02-11 | 1996-08-14 | Lucas Industries Public Limited Company | Fuel system |
-
1989
- 1989-04-10 JP JP9033989A patent/JPH02267363A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0726390A1 (en) * | 1995-02-11 | 1996-08-14 | Lucas Industries Public Limited Company | Fuel system |
| US5711279A (en) * | 1995-02-11 | 1998-01-27 | Lucas Industries, Plc | Fuel system |
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