JPH03286176A - Fuel injection device for diesel engine - Google Patents
Fuel injection device for diesel engineInfo
- Publication number
- JPH03286176A JPH03286176A JP8788390A JP8788390A JPH03286176A JP H03286176 A JPH03286176 A JP H03286176A JP 8788390 A JP8788390 A JP 8788390A JP 8788390 A JP8788390 A JP 8788390A JP H03286176 A JPH03286176 A JP H03286176A
- Authority
- JP
- Japan
- Prior art keywords
- injection
- valve
- piezoelectric element
- fuel
- fuel injection
- 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
- 238000002347 injection Methods 0.000 title claims abstract description 91
- 239000007924 injection Substances 0.000 title claims abstract description 91
- 239000000446 fuel Substances 0.000 title claims abstract description 51
- 230000001105 regulatory effect Effects 0.000 abstract 2
- 238000010586 diagram Methods 0.000 description 11
- CIWBSHSKHKDKBQ-JLAZNSOCSA-N Ascorbic acid Chemical compound OC[C@H](O)[C@H]1OC(=O)C(O)=C1O CIWBSHSKHKDKBQ-JLAZNSOCSA-N 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 2
- 230000036461 convulsion Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- FNYLWPVRPXGIIP-UHFFFAOYSA-N Triamterene Chemical compound NC1=NC2=NC(N)=NC(N)=C2N=C1C1=CC=CC=C1 FNYLWPVRPXGIIP-UHFFFAOYSA-N 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- WQGWDDDVZFFDIG-UHFFFAOYSA-N pyrogallol Chemical compound OC1=CC=CC(O)=C1O WQGWDDDVZFFDIG-UHFFFAOYSA-N 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Landscapes
- Fuel-Injection Apparatus (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は陸舶用のあらゆる用途向のディーゼルエンジン
用燃料噴射装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a fuel injection device for a diesel engine for all types of land and marine applications.
第4図は従来形ディーゼルエンジンの燃料噴射系の一例
を示したもので、1はジャーキ式燃料噴射ポンプ本体、
2はプランジャバレル、3はプランジャ、4は吐出弁、
5は等圧弁、6は燃料噴射管、7は逆止弁、8は燃料噴
射弁本体、9は噴孔、lOは針弁、11は燃料弁ばねを
示す。これらの図では噴射管6内に残留圧調整用のシス
テムが付加されており、7は残留圧調整用弁で、蓄圧器
12と蓄圧用ポンプ13などからなるシステムが連結さ
れている。Figure 4 shows an example of the fuel injection system of a conventional diesel engine, where 1 is the jerky fuel injection pump body;
2 is a plunger barrel, 3 is a plunger, 4 is a discharge valve,
5 is an equal pressure valve, 6 is a fuel injection pipe, 7 is a check valve, 8 is a fuel injection valve main body, 9 is an injection hole, IO is a needle valve, and 11 is a fuel valve spring. In these figures, a residual pressure adjustment system is added to the injection pipe 6, and 7 is a residual pressure adjustment valve, which is connected to a system consisting of a pressure accumulator 12, a pressure accumulation pump 13, and the like.
次に前記従来例の作用について説明する。Next, the operation of the conventional example will be explained.
燃料カム(図示せず)によってプランジャ3が押し上げ
られると、バレル2内の燃料が圧縮され、吐出弁4を開
いて噴射管6内に送出され、燃料弁8に至ると針弁10
をばね11の押圧力に抗して押し上げて開弁させ、噴孔
9よりエンジンのシリンダ(図示せず)内に噴出し、燃
料は燃焼してエンジン出力が発揮される。When the plunger 3 is pushed up by a fuel cam (not shown), the fuel in the barrel 2 is compressed, opens the discharge valve 4 and is sent into the injection pipe 6, and when it reaches the fuel valve 8, the needle valve 10
The fuel is pushed up against the pressing force of the spring 11 to open the valve, and the fuel is injected from the nozzle hole 9 into the cylinder (not shown) of the engine, whereupon the fuel is combusted and engine output is produced.
この際生ずる二次噴射を防止するため吐出弁4の近くに
逆方向に等圧弁5が設けられており、バレル2の圧力が
低下しておれば、余分の圧力上昇が噴射管6内に生しな
いように等圧別5を開いて噴射管6内の高圧油を所定の
圧力になるまで放出する。一方噴射終了後噴射管6内の
圧力が異常に低下し、場合によっては負圧となるなどの
不具合を防止するために、残留圧調整用の逆止弁7とそ
れにつづく蓄圧器12以下を設けており、必要に応じて
逆止弁7が開閉して、所定の残留圧力になるまで前記逆
止弁7、蓄圧器12、ポンプ13を介して燃料を管6に
供給する。In order to prevent the secondary injection that occurs at this time, an equal pressure valve 5 is provided near the discharge valve 4 in the opposite direction. To prevent this from happening, the isobar 5 is opened and the high pressure oil in the injection pipe 6 is released until it reaches a predetermined pressure. On the other hand, in order to prevent malfunctions such as the pressure inside the injection pipe 6 abnormally decreasing after the end of injection, and in some cases becoming negative pressure, a check valve 7 for adjusting residual pressure and a pressure accumulator 12 and below are provided for adjusting the residual pressure. The check valve 7 is opened and closed as necessary, and fuel is supplied to the pipe 6 via the check valve 7, pressure accumulator 12, and pump 13 until a predetermined residual pressure is reached.
第5図は前記従来例の噴射特性を示したもので主噴射の
みを1回行った場合を示している。FIG. 5 shows the injection characteristics of the conventional example, and shows the case where only the main injection is performed once.
なおさらに、ディーゼルノックを防止する高性能の着火
燃焼を行わせるため、この噴射系でパイロット噴射と主
噴射の二回噴射をつづけて行なう場合には、プランジャ
3を図示しないカムによって二段に分けて上昇させるか
、又はプランジャ3の上部外周部に図示しない逃し用の
溝を設けることによって行なうのが一般に行われており
、第6図に示すようなパイロット噴射と主噴射の二回噴
射が実現されている。Furthermore, in order to perform high-performance ignition combustion to prevent diesel knock, when performing two consecutive injections (pilot injection and main injection) with this injection system, the plunger 3 is divided into two stages by a cam (not shown). Generally, this is done by raising the plunger 3 or by providing a relief groove (not shown) in the upper outer periphery of the plunger 3, thereby realizing two injections, a pilot injection and a main injection, as shown in Fig. 6. has been done.
ところが前述の従来形噴射系において、パイロット噴射
と主噴射を行なうのに、カムとプランジャのいずれで行
なう場合でも幾何学的構成が困難であるため、バイロフ
ト噴射を主噴射に対して最適のタイミングで行なうこと
が困難であり、パイロット噴射の目的であるディーゼル
ノックの防止が、エンジンの運転状態(負荷1回転速度
、気温など)や燃料のセタン価に応し、好ましい状態で
実現することができない欠点があった。However, in the conventional injection system described above, it is difficult to configure the geometry of pilot injection and main injection using either a cam or a plunger. The disadvantage is that it is difficult to perform pilot injection, and the prevention of diesel knock, which is the purpose of pilot injection, cannot be achieved under favorable conditions depending on the engine operating conditions (load rotational speed, temperature, etc.) and the cetane number of the fuel. was there.
本発明の目的は前記従来装置の問題点を解消し、ディー
ゼルノックが最小となるようにコントロールし、パイロ
ット噴射の時期と量を自由に選択できる燃焼噴射装置を
提供するにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a combustion injection system that eliminates the problems of the conventional device, controls diesel knock to a minimum, and allows the timing and amount of pilot injection to be freely selected.
本発明はジャーキ式ディーゼルエンジン用燃料噴射装置
において、燃料噴射弁の開弁圧調整用ばね受と弁本体の
間に圧電素子を介在させ、圧電素子に荷電システムを連
結し、該圧電素子への通電はクランク角が人力されるコ
ントローラ16により適切なタイくングでON、OFF
されるように構成したものである。The present invention provides a fuel injection device for a jerk type diesel engine, in which a piezoelectric element is interposed between a valve opening pressure adjusting spring support of a fuel injection valve and a valve body, a charging system is connected to the piezoelectric element, and a charging system is connected to the piezoelectric element. Electricity is turned on and off by appropriate timing using a controller 16 that manually controls the crank angle.
It is configured so that
噴射管6内は所定の残留圧Prが保たれており、クラン
ク軸と同期して出されるクランク角信号によりバイロフ
ト噴射が必要なタイミングとなると、圧電素子14の駆
動用コントローラ16のスイッチが入り、電源15によ
って電圧が圧電素子14に加えられ、圧電素子14が変
形し、ばね受座111を押し上げるためばね11はちぢ
み、針弁は噴射管6内の残留圧力Prで押し上げられて
開弁し、噴孔9より燃料を噴出する。所定のパイロット
噴射が行われた後はコントローラ16のスイッチがOF
Fとなり、圧電素子14は元の位置にもどり、針弁10
には再びばね11のばね力が加わって閉弁し、主噴射の
待機状態となる。A predetermined residual pressure Pr is maintained inside the injection pipe 6, and when the timing for biloft injection is reached based on a crank angle signal output in synchronization with the crankshaft, the controller 16 for driving the piezoelectric element 14 is switched on. A voltage is applied to the piezoelectric element 14 by the power source 15, the piezoelectric element 14 is deformed, the spring 11 is compressed to push up the spring seat 111, and the needle valve is pushed up by the residual pressure Pr in the injection pipe 6 and opens. Fuel is ejected from the nozzle hole 9. After the predetermined pilot injection is performed, the switch of the controller 16 is turned OFF.
F, the piezoelectric element 14 returns to its original position, and the needle valve 10
The spring force of the spring 11 is applied again to close the valve, and the main injection is in a standby state.
以下第1〜3図を参照し、本発明の一実施例について説
明する。An embodiment of the present invention will be described below with reference to FIGS. 1 to 3.
第1図は実施例の燃料噴射系図、第2図は同パイロット
噴射作動図、第3図は同燃料噴射特性図である。FIG. 1 is a fuel injection system diagram of the embodiment, FIG. 2 is a pilot injection operation diagram, and FIG. 3 is a fuel injection characteristic diagram.
第1図は本発明の構成概要を図示したものである。その
特徴は燃料噴射弁8の中に圧電素子(とくに積層型の圧
電素子)14を設け、これに電圧をかけることにまり針
弁10を押し下げているばね11の押付力を制御し、噴
射管6内の残留圧Prとして貯えられたエネルギを利用
してパイロット噴射を行なわせるものである。FIG. 1 shows an outline of the configuration of the present invention. The feature is that a piezoelectric element (particularly a laminated piezoelectric element) 14 is provided in the fuel injection valve 8, and by applying voltage to this element, the pressing force of the spring 11 that presses down the needle valve 10 is controlled, and the injection pipe The pilot injection is performed using the energy stored as the residual pressure Pr in the fuel tank 6.
噴射系の基本構造は、従来例に示す第4図と類似してお
り、従来例と同一部分については、1はジャーキ式燃料
噴射ポンプ本体、2はプランジャバレル、3はプランジ
ャ、4は吐出弁、5は等圧弁、6は燃料噴射管、7は逆
止弁、8は燃料噴射弁本体、9は噴孔、10は針弁、1
1は燃料弁ばねを示す。これらの図では噴射管6内に残
留圧調整用のシステムが付加されており、7は残留圧調
整用弁で、蓄圧器12と蓄圧用ポンプ13などからなっ
ているシステムが連結されている。The basic structure of the injection system is similar to the conventional example shown in Fig. 4, and the same parts as the conventional example include 1 the jerk type fuel injection pump body, 2 the plunger barrel, 3 the plunger, and 4 the discharge valve. , 5 is an equal pressure valve, 6 is a fuel injection pipe, 7 is a check valve, 8 is a fuel injection valve body, 9 is an injection hole, 10 is a needle valve, 1
1 indicates a fuel valve spring. In these figures, a residual pressure adjustment system is added to the injection pipe 6, and 7 is a residual pressure adjustment valve, which is connected to a system consisting of a pressure accumulator 12, a pressure accumulation pump 13, and the like.
次に本発明の特徴部分としては、燃料噴射弁内でばね受
111と噴射ポンプ本体の間に圧電素子14を、またそ
の駆動用としては電源15とクランク角検出器17より
のクランク角信号が人力するコントローラ16を設け、
該コントローラで適切なタイミングで圧電素子をON、
OFFする構成となっている。従って従来のように幾何
学的制約なしに、電気的制御によってパイロ7)噴射を
行わせるように構成したものである。Next, as a characteristic part of the present invention, a piezoelectric element 14 is provided between the spring receiver 111 and the injection pump main body in the fuel injection valve, and a crank angle signal from a power source 15 and a crank angle detector 17 is used to drive the piezoelectric element 14. A human-powered controller 16 is provided,
The controller turns on the piezoelectric element at an appropriate timing,
It is configured to turn off. Therefore, the structure is such that the pyro injection is performed by electrical control without geometrical constraints as in the conventional case.
次に第2〜3図を参照し前記実施例の作用について説明
する。Next, the operation of the embodiment described above will be explained with reference to FIGS. 2 and 3.
第2図に示すように、燃料噴射管6内は等思弁5と残留
圧調整用弁7および針弁lOの三つの弁で所定の残留圧
Prが保たれており、図示しないクランク軸と同期して
出力されるクランク角信号により、バイロフト噴射が必
要なタイミングに達すると、圧電素子14の駆動用コン
トローラ16のスイッチが入り、電源15によって電圧
が圧電素子14に印加されて圧電素子14が変形し、ば
ね受座111を押し上げる。その結果、ばね11によっ
て押し付けられていた針弁10は押し付は力を失うこと
になり、噴射管6内の残留圧力Prによって針弁は押し
上げられて開弁し、噴孔9より燃料を噴出する。所定の
燃料量が噴出すると、コントローラ16のスイッチがO
FFとなり、圧電素子14は元の位置に戻り、針弁10
には再びばね11の付勢力が加わり閉弁する。As shown in Fig. 2, a predetermined residual pressure Pr is maintained within the fuel injection pipe 6 by three valves: an iso-thinking valve 5, a residual pressure adjustment valve 7, and a needle valve IO, and is synchronized with a crankshaft (not shown). When the necessary timing for biloft injection is reached according to the crank angle signal output from the above, the controller 16 for driving the piezoelectric element 14 is switched on, and a voltage is applied to the piezoelectric element 14 by the power supply 15, causing the piezoelectric element 14 to deform. and push up the spring seat 111. As a result, the needle valve 10 that had been pressed by the spring 11 loses its pressing force, and the needle valve is pushed up and opened by the residual pressure Pr in the injection pipe 6, and fuel is injected from the injection hole 9. do. When a predetermined amount of fuel is ejected, the switch of the controller 16 is turned to O.
FF, the piezoelectric element 14 returns to its original position, and the needle valve 10
The biasing force of the spring 11 is applied again to close the valve.
次いで、図示しないカムが燃料噴射ポンプのプランジャ
3を押し上げ、主噴射が行われるがこの場合、前記圧電
素子の回路はOFFとなっているため、燃料噴射管6内
の油圧が上昇し、針弁10の開弁圧以上になれば、針弁
10が開き再び噴孔9から主噴射が開始される。なお本
発明のパイロット噴射時の詳細は、第3図の噴射特性図
に示すとおりである。Next, a cam (not shown) pushes up the plunger 3 of the fuel injection pump to perform main injection, but in this case, since the circuit of the piezoelectric element is OFF, the oil pressure inside the fuel injection pipe 6 increases, causing the needle valve to close. When the valve opening pressure exceeds 10, the needle valve 10 opens and main injection starts again from the nozzle hole 9. The details of the pilot injection according to the present invention are as shown in the injection characteristic diagram in FIG.
以上のとおり、本発明のバイロフト噴射は電気的人力に
よって制御され、主噴射はカム、プランジャ等の機械式
で制御されることになり、主噴射に対しバイロフト噴射
を任意の望むタイミングと量になるように容易に制御が
できるため、ディーゼルノックを防止できる理想的なデ
ィーゼルエンジン用燃料噴射装置が実現できる。As described above, the viroft injection of the present invention is controlled by electric manual power, and the main injection is controlled by mechanical systems such as cams and plungers, so that the viroft injection can be controlled at any desired timing and amount with respect to the main injection. Since it can be easily controlled, an ideal fuel injection system for diesel engines that can prevent diesel knock can be realized.
本発明は前記のとおり構成したので、第3図に示すよう
な噴射特性が得られ、機関の運転条件や燃料のセタン価
等に最適のバイロフト噴射タイミングと量が実現できス
ムーズな着火燃焼が実現できる。Since the present invention is configured as described above, the injection characteristics shown in Fig. 3 can be obtained, and the optimal viroft injection timing and amount can be realized depending on the engine operating conditions and the cetane number of the fuel, and smooth ignition and combustion can be realized. can.
又その結果ディーゼルノックのない静かで排気公害が少
なく、且熱効果の高い高性能のディーゼルエンジンが実
現できると共に、低セタン価燃料を使用しても、ディー
ゼルノックが防止でき、又多種燃料にも対応可能なディ
ーゼルエンジンを実現できる。As a result, it is possible to realize a high-performance diesel engine that is quiet without diesel knock, has low exhaust pollution, and has high thermal efficiency.It also prevents diesel knock even when using low cetane number fuel, and can be used with a variety of fuels. A compatible diesel engine can be created.
第1〜3図は本発明に係るもので、第1図は燃料噴射系
の構成図、第2図は燃料噴射系の作用説明図、第3図は
同噴射系の燃料噴射特性図、第4〜6図は従来例に係る
もので、第4図は第1図応当図、第5図はパイロット噴
射のない場合の従来形燃料噴射特性図、第6図はバイロ
フト噴射が行われる場合の従来形燃料噴射特性図である
。
8・・・燃料噴射弁、10・・・針弁、11・・・ばね
、14・・・圧電素子、15・・・電源、16・・・コ
ントローラ、111・・・ばね受。
クランク角度e
クランク角度O
第5
図
クラック角度O
第6
図1 to 3 are related to the present invention; FIG. 1 is a configuration diagram of the fuel injection system, FIG. 2 is an explanatory diagram of the operation of the fuel injection system, FIG. 3 is a fuel injection characteristic diagram of the injection system, and FIG. Figures 4 to 6 are related to conventional examples. Figure 4 is a diagram corresponding to Figure 1, Figure 5 is a conventional fuel injection characteristic diagram without pilot injection, and Figure 6 is a diagram of conventional fuel injection characteristics when biloft injection is performed. FIG. 3 is a conventional fuel injection characteristic diagram. 8... Fuel injection valve, 10... Needle valve, 11... Spring, 14... Piezoelectric element, 15... Power source, 16... Controller, 111... Spring receiver. Crank angle e Crank angle O Fig. 5 Crack angle O Fig. 6
Claims (1)
置と自動弁式燃料噴射弁とにより構成されるディーゼル
エンジン用燃料噴射装置において、燃料噴射弁の開弁圧
調整用ばね受と弁本体との間に圧電素子を介在させ、同
圧電素子に荷電システムを連結し、圧電素子への通電を
制御する手段を設けたことを特徴とするディーゼルエン
ジン用燃料噴射装置。In a diesel engine fuel injection device consisting of a jerk-type fuel injection pump, a high-pressure injection pipe, a residual pressure adjustment device, and an automatic valve-type fuel injection valve, the spring bearing for adjusting the opening pressure of the fuel injection valve and the valve body are connected to each other. A fuel injection device for a diesel engine, characterized in that a piezoelectric element is interposed between the piezoelectric elements, a charging system is connected to the piezoelectric element, and means for controlling energization to the piezoelectric element is provided.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2087883A JP2695675B2 (en) | 1990-04-02 | 1990-04-02 | Fuel injection device for diesel engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2087883A JP2695675B2 (en) | 1990-04-02 | 1990-04-02 | Fuel injection device for diesel engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH03286176A true JPH03286176A (en) | 1991-12-17 |
JP2695675B2 JP2695675B2 (en) | 1998-01-14 |
Family
ID=13927272
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2087883A Expired - Fee Related JP2695675B2 (en) | 1990-04-02 | 1990-04-02 | Fuel injection device for diesel engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2695675B2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101303509B1 (en) * | 2012-05-29 | 2013-09-03 | 현대중공업 주식회사 | Hybrid fuel injection equipment for diesel engine |
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JPS57136859U (en) * | 1981-02-18 | 1982-08-26 | ||
JPS6324363U (en) * | 1986-08-01 | 1988-02-17 | ||
JPS63198769A (en) * | 1987-02-13 | 1988-08-17 | Hitachi Ltd | Piezoelectric type fuel injection valve |
JPS63208665A (en) * | 1987-02-24 | 1988-08-30 | Hitachi Ltd | Adjustment of flow rate for piezoelectric type fuel injection valve |
JPS63253168A (en) * | 1987-04-08 | 1988-10-20 | Mitsubishi Heavy Ind Ltd | Fuel injection pump |
-
1990
- 1990-04-02 JP JP2087883A patent/JP2695675B2/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS496043A (en) * | 1971-06-04 | 1974-01-19 | ||
JPS57136859U (en) * | 1981-02-18 | 1982-08-26 | ||
JPS6324363U (en) * | 1986-08-01 | 1988-02-17 | ||
JPS63198769A (en) * | 1987-02-13 | 1988-08-17 | Hitachi Ltd | Piezoelectric type fuel injection valve |
JPS63208665A (en) * | 1987-02-24 | 1988-08-30 | Hitachi Ltd | Adjustment of flow rate for piezoelectric type fuel injection valve |
JPS63253168A (en) * | 1987-04-08 | 1988-10-20 | Mitsubishi Heavy Ind Ltd | Fuel injection pump |
Also Published As
Publication number | Publication date |
---|---|
JP2695675B2 (en) | 1998-01-14 |
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