JP3516583B2 - Diesel engine fuel injection system - Google Patents

Diesel engine fuel injection system

Info

Publication number
JP3516583B2
JP3516583B2 JP01167098A JP1167098A JP3516583B2 JP 3516583 B2 JP3516583 B2 JP 3516583B2 JP 01167098 A JP01167098 A JP 01167098A JP 1167098 A JP1167098 A JP 1167098A JP 3516583 B2 JP3516583 B2 JP 3516583B2
Authority
JP
Japan
Prior art keywords
injection
main
fuel injection
preliminary
fuel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP01167098A
Other languages
Japanese (ja)
Other versions
JPH11210588A (en
Inventor
正寛 明田
哲也 小坂
裕三 梅田
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 JP01167098A priority Critical patent/JP3516583B2/en
Publication of JPH11210588A publication Critical patent/JPH11210588A/en
Application granted granted Critical
Publication of JP3516583B2 publication Critical patent/JP3516583B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、ディーゼルエンジ
ンの燃料噴射装置に関する。
TECHNICAL FIELD The present invention relates to a fuel injection device for a diesel engine.

【0002】[0002]

【従来の技術】ディーゼルエンジンの燃料噴射装置の従
来技術として、予備噴射と主噴射とが行われるように構
成したものがある。主噴射前に予備噴射を行い、主噴射
による燃焼を改善するためである。この種の燃料噴射装
置には、燃料噴射ポンプのプランジャが予備噴射用突起
によってリフトされる最大リフト寸法が、主噴射用突起
によってリフトされる最大リフト寸法よりも短く設定さ
れたものや、予備噴射量が主噴射量よりも多いもの等が
ある。
2. Description of the Related Art As a conventional technique of a fuel injection device for a diesel engine, there is one which is configured to perform a preliminary injection and a main injection. This is because the preliminary injection is performed before the main injection to improve combustion by the main injection. In this type of fuel injection device, the maximum lift dimension by which the plunger of the fuel injection pump is lifted by the preliminary injection projection is set shorter than the maximum lift dimension by the main injection projection, and the preliminary injection For example, the amount is larger than the main injection amount.

【0003】[0003]

【発明が解決しようとする問題点】上記従来技術には次
の問題点がある。燃料噴射ポンプのプランジャが予備噴
射用突起によってリフトされる最大リフト寸法が、主噴
射用突起によってリフトされる最大リフト寸法よりも短
く設定されている場合には、予備噴射と主噴射の終了条
件が相違するため、予備噴射と主噴射の終了時に行われ
る吸い戻し弁による燃料の吸い戻し条件が相違し、予備
噴射終了時に燃料噴射管の残圧が低下することがある。
このため、噴射が欠落したり、噴射タイミングが狂うこ
とがあり、円滑な運転を行うことができない。
Problems to be Solved by the Invention The above-mentioned prior art has the following problems. If the maximum lift size for lifting the plunger of the fuel injection pump by the preliminary injection projection is set shorter than the maximum lift size for lifting by the main injection projection, the pre-injection and main injection end conditions are Because of the difference, the conditions for sucking back the fuel by the suction return valve performed at the end of the preliminary injection and the main injection are different, and the residual pressure of the fuel injection pipe may decrease at the end of the preliminary injection.
Therefore, the injection may be lost or the injection timing may be misaligned, and smooth operation cannot be performed.

【0004】予備噴射量が主噴射量よりも多い場合に
は、過早着火が起こり、適性な出力が得られない。ま
た、多くの予備噴射燃料が一時に自発火するので、激し
いノッキングを起こすことがある。
If the preliminary injection amount is larger than the main injection amount, pre-ignition occurs and an appropriate output cannot be obtained. In addition, a large amount of pre-injected fuel spontaneously ignites at one time, which may cause severe knocking.

【0005】本発明の課題は、上記問題点を解決するこ
とにある。
An object of the present invention is to solve the above problems.

【0006】[0006]

【課題を解決するための手段】主要な請求項1の発明の
構成は、次の通りである(図3・図4参照)。燃料噴射
として、予備噴射(1)と主噴射(2)とが行われるように
構成した、ディーゼルエンジンの燃料噴射装置におい
て、1の燃料噴射カム(3)に1の予備噴射用突起(4)と
1の主噴射用突起(5)とが設けられ、燃料噴射ポンプ
(7)のプランジャ(21)が予備噴射用突起(4)によって
リフトされる最大リフト寸法が、主噴射用突起(5)によ
ってリフトされる最大リフト寸法と実質的に同一と
れ、 予備噴射用突起(4)と主噴射用突起(5)とが異なる
形状とされ、予備噴射用突起(4)によるプランジャ(2
1)のリフト速度が主噴射用突起(5)によるプランジャ
(21)のリフト速度よりも遅く設定されているもの。
The main constitution of the invention of claim 1 is as follows (see FIGS. 3 and 4 ). In a fuel injection device for a diesel engine configured to perform a preliminary injection (1) and a main injection (2) as fuel injection, one fuel injection cam (3) has one preliminary injection protrusion (4). And a main injection projection (5) for the fuel injection pump
(7) the plunger (21) of maximum lift dimensioned to be lifted by the projections for preinjection (4), the maximum lift dimension substantially the same, which is lifted by a main injection projections (5)
Is, projections for preinjection (4) and the projection for the main injection (5) is different from
The plunger (2
The lift speed of 1) is the plunger due to the main injection projection (5)
It is set slower than the lift speed of (21).

【0007】[0007]

【発明の作用及び効果】(請求項1の発明) 請求項1の発明は、次の作用効果を奏する(図3・図4
参照)。燃料噴射ポンプ(7)のプランジャ(21)が予備
噴射用突起(4)によってリフトされる最大リフト寸法
が、主噴射用突起(5)による最大リフト寸法と実質的に
同一とされるので、予備噴射(1)と主噴射(2)の終了条
件が実質的に同一とされ、或いは極めて近くなり、予備
噴射と主噴射の終了時に行われる吸い戻し弁による燃料
の吸い戻し条件が実質的に同一とされ、或いは極めて近
くなり、予備噴射終了時に燃料噴射管の残圧が低下する
不備を防止できる。このため、これに起因する噴射の欠
落や、噴射タイミングの狂いを防止でき、円滑な運転を
行うことができる。
Action and Effect of the Invention (Invention of Claim 1) The invention of Claim 1 has the following action and effect ( FIGS. 3 and 4).
reference). Since the maximum lift dimension by which the plunger (21) of the fuel injection pump (7) is lifted by the preliminary injection projection (4) is substantially the same as the maximum lift dimension by the main injection projection (5), The end conditions for injection (1) and main injection (2) are substantially the same or very close to each other, and the conditions for sucking back fuel by the suction return valve performed at the end of pre-injection and main injection are substantially the same. Therefore, it is possible to prevent the deficiency that the residual pressure of the fuel injection pipe decreases at the end of the preliminary injection. Therefore, it is possible to prevent the missing of the injection and the deviation of the injection timing due to this, and it is possible to perform the smooth operation.

【0008】1サイクル中の必要噴射量を予備噴射(1)
と主噴射(2)の2回に分割して噴射することができ、1
サイクル中に1回の噴射のみを行う場合に比べ、1噴射
当たりの燃料吐出量が少なくて済み、小型小能力の安価
な燃料噴射ポンプ(7)を用いることができる。また、予
備噴射用突起(4)によるプランジャ(21)のリフト速度
が主噴射用突 起(5)によるプランジャ(21)のリフト速
度よりも遅く設定されているので、予備噴射量が主噴射
量よりも少なくなり、過早着火やノッキングの抑制がよ
り効果的に行われる。
Pre-injection of the required injection amount in one cycle (1)
And the main injection (2) can be divided into two injections.
Compared to the case where only one injection is performed during a cycle, the amount of fuel discharged per injection is small, and a small-sized and low-capacity fuel injection pump (7) can be used. In addition,
Lift speed of the plunger (21) by the projection (4) for injection
Lift speed of the plunger (21) by collision force for the main injection (5)
Since it is set later than
It is less than the amount, and it is possible to suppress premature ignition and knocking.
More effectively.

【0009】[0009]

【0010】[0010]

【0011】[0011]

【0012】(請求項2の発明)請求項2 の発明は、請求項1の発明の作用効果に加え、
次の作用効果を奏する(図3・図4参照)。予備噴射用
突起(4)と主噴射用突起(5)とが、相互反対側に配置さ
れているので、これらを十分に離して配置することがで
き、燃料噴射カム(3)のカムプロフィールの設計や製作
を容易に行うことができる。
(Invention of Claim 2 ) The invention of Claim 2 has the function and effect of the invention of Claim 1 ,
The following operational effects are achieved (see FIGS. 3 and 4 ). Since the pre-injection protrusion (4) and the main-injection protrusion (5) are arranged on the opposite sides, they can be arranged sufficiently apart from each other, and the cam profile of the fuel injection cam (3) It can be designed and manufactured easily.

【0013】(請求項3の発明)請求項3 の発明は、請求項1または請求項2の発明の作
用効果に加え、次の作用効果を奏する(図3・図4
照)。予備噴射(1)が吸気工程の前半に開始され、主噴
射(2)が圧縮工程の後半に開始されるので、予備噴射
(1)から主噴射(2)までの期間が長く、気化した予備噴
射燃料が燃焼室(6)全体に行き渡った後に主噴射(2)が
行われる。このため、主噴射(2)による燃焼火炎が燃焼
室(6)全体に伝播し、空気の利用率が高くなり、不完全
燃焼による黒煙の発生が抑制される。
(Invention of Claim 3 ) The invention of claim 3 has the following effect in addition to the effect of the invention of claim 1 or claim 2 (see FIGS. 3 and 4 ). Since the preliminary injection (1) is started in the first half of the intake stroke and the main injection (2) is started in the latter half of the compression stroke, the preliminary injection is performed.
The period from (1) to the main injection (2) is long, and the main injection (2) is performed after the vaporized preliminary injection fuel has spread to the entire combustion chamber (6). Therefore, the combustion flame generated by the main injection (2) propagates to the entire combustion chamber (6), the utilization rate of air is increased, and the generation of black smoke due to incomplete combustion is suppressed.

【0014】(請求項4の発明)請求項4 の発明は、請求項1から請求項3のいずれかの
発明の作用効果に加え、次の作用効果を奏する(図3・
図4参照)。予備噴射(1)と主噴射(2)とが単一の噴射
経路を介して行われるので、燃料噴射装置の構造が簡素
化され、その製造コストが安くなるとともに、その故障
が起こりにくい。
(Invention of Claim 4 ) The invention of claim 4 has the following effect in addition to the effect of any one of claims 1 to 3 ( Fig. 3 ) .
( See FIG. 4 ). Since the preliminary injection (1) and the main injection (2) are performed via a single injection path, the structure of the fuel injection device is simplified, the manufacturing cost thereof is reduced, and the failure thereof is unlikely to occur.

【0015】予備噴射(1)が燃焼室(6)に直接に行われ
るので、気化した燃料を含まない空気を燃焼室(6)に吸
気できる。このため、空気の充填効率が高まり、不完全
燃焼による黒煙の発生を抑制できる。
Since the pre-injection (1) is directly performed in the combustion chamber (6), the vaporized fuel-free air can be sucked into the combustion chamber (6). Therefore, the efficiency of filling air is increased, and the generation of black smoke due to incomplete combustion can be suppressed.

【0016】(請求項5の発明)請求項5 の発明は、請求項4の発明の作用効果に加え、
次の作用効果を奏する(図3参照)。燃焼室(6)が直接
噴射式とされ、予備噴射(1)と主噴射(2)とがピストン
(11)のキャビティ(12)内に向けて行われるので、噴
射燃料によるシリンダ(17)の内周面の潤滑油の洗い流
しが抑制され、ピストン(11)の焼き付きが抑制され
る。
(Invention of Claim 5 ) The invention of Claim 5 has, in addition to the function and effect of the invention of Claim 4 ,
The following operational effects are achieved (see FIG. 3 ). The combustion chamber (6) is a direct injection type, and the preliminary injection (1) and the main injection (2) are pistons.
Since it is carried out into the cavity (12) of (11), the washing out of the lubricating oil on the inner peripheral surface of the cylinder (17) by the injected fuel is suppressed, and the seizure of the piston (11) is suppressed.

【0017】(請求項6の発明)請求項6 の発明は、請求項4の発明の作用効果に加え、
次の作用効果を奏する(図4参照)。燃焼室(6)が副室
式とされ、予備噴射(1)と主噴射(2)とが副燃焼室(1
3)で行われ、予備噴射(1)と主噴射(2)の際、副燃焼
室(13)と主燃焼室(14)との連通孔(15)がピストン
(11)の頂面(16)に向けられているので、噴射燃料に
よるシリンダ(17)の内周面の潤滑油の洗い流しが抑制
され、ピストン(11)の焼き付きが抑制される。
(Invention of Claim 6 ) According to the invention of Claim 6 , in addition to the function and effect of the invention of Claim 4 ,
The following operational effects are obtained (see FIG. 4 ). The combustion chamber (6) is of a sub-chamber type, and the preliminary injection (1) and the main injection (2) are the sub-combustion chamber (1).
3), and during the preliminary injection (1) and the main injection (2), the communication hole (15) between the auxiliary combustion chamber (13) and the main combustion chamber (14) forms the piston.
Since it is directed to the top surface (16) of (11), the washing out of the lubricating oil on the inner peripheral surface of the cylinder (17) by the injected fuel is suppressed, and the seizure of the piston (11) is suppressed.

【0018】[0018]

【参考例】本発明の参考例を図面に基づいて説明する。
図1は本発明の第1参考例を説明する図である。この
考例では、直接噴射式の多気筒エンジンが用いられてい
る。
Reference Example A reference example of the present invention will be described with reference to the drawings.
FIG. 1 is a diagram illustrating a first reference example of the present invention. This ginseng
In the example , a direct injection multi-cylinder engine is used.

【0019】このエンジンは、次のように構成されてい
る。図1(A)に示すように、シリンダ(17)にピスト
ン(11)が内嵌され、ピストン(11)の頂面(16)にキ
ャビィティ(12)が設けられ、このキャビィティ(12)
内が燃焼室(6)とされている。シリンダ(17)にシリン
ダヘッド(18)が組み付けられ、このシリンダヘッド
(18)に燃料噴射ノズル(9)が取り付けられている。図
中の符号(19)は吸気弁である。
This engine is constructed as follows. As shown in FIG. 1A, a piston (11) is fitted in a cylinder (17), and a cavity (12) is provided on a top surface (16) of the piston (11).
The inside is a combustion chamber (6). The cylinder head (18) is assembled to the cylinder (17).
A fuel injection nozzle (9) is attached to (18). Reference numeral (19) in the drawing is an intake valve.

【0020】このエンジンの燃料噴射装置は、次のよう
に構成されている。図1(A)に示すように、燃料噴射
ポンプ(7)に燃料噴射管(8)が接続され、この燃料噴射
管(8)の先端に燃料噴射ノズル(9)が接続されている。
燃料噴射ポンプ(7)は燃料噴射カム(3)によって駆動さ
れる。図1(B)に示すように、燃料噴射として、予備
噴射(1)と主噴射(2)とが行われる。
The fuel injection system of this engine is constructed as follows. As shown in FIG. 1A, a fuel injection pipe (8) is connected to the fuel injection pump (7), and a fuel injection nozzle (9) is connected to the tip of this fuel injection pipe (8).
The fuel injection pump (7) is driven by the fuel injection cam (3). As shown in FIG. 1B, a preliminary injection (1) and a main injection (2) are performed as fuel injection.

【0021】図1(A)に示すように、1の燃料噴射カ
ム(3)に1の予備噴射用突起(4)と1の主噴射用突起
(5)とが設けられ、燃料噴射ポンプ(7)のプランジャ
(21)が予備噴射用突起(4)によってリフトされる最大
リフト寸法が、主噴射用突起(5)によってリフトされる
最大リフト寸法と実質的に同一とされている。予備噴射
用突起(4)と主噴射用突起(5)とは実質的に同一形状と
されている。
As shown in FIG. 1A, one fuel injection cam (3) has one preliminary injection protrusion (4) and one main injection protrusion.
(5) and are provided, and the plunger of the fuel injection pump (7)
The maximum lift dimension by which (21) is lifted by the preliminary injection projection (4) is substantially the same as the maximum lift dimension by which the main injection projection (5) is lifted. The preliminary injection protrusion (4) and the main injection protrusion (5) have substantially the same shape.

【0022】予備噴射用突起(4)と主噴射用突起(5)と
が、燃料噴射カム(3)の回転中心(10)を間に挟んで、
相互反対側に配置されている。図1(B)に示すよう
に、予備噴射(1)が吸気工程の前半に開始され、主噴射
(2)が圧縮工程の後半に開始される。予備噴射(1)は排
気弁(図外)が閉弁された直後に開始され、吸気工程の
前半で終了する。主噴射(2)は圧縮工程が終了する上死
点の手前で開始され、その上死点の後で終了する。図1
(A)に示すように、1の燃焼室(6)への予備噴射(1)
と主噴射(2)とが燃料噴射ポンプ(7)に接続された1の
燃料噴射管(8)と、この燃料噴射管(8)に接続された1
の燃料噴射ノズル(9)とを介して、燃焼室(6)に直接に
行われる。予備噴射(1)と主噴射(2)とはピストン(1
1)のキャビティ(12)内に向けて行われる。
The preliminary injection projection (4) and the main injection projection (5) sandwich the rotation center (10) of the fuel injection cam (3) between them,
Located on opposite sides of each other. As shown in FIG. 1 (B), the preliminary injection (1) is started in the first half of the intake stroke, and the main injection is performed.
(2) is started in the latter half of the compression process. The preliminary injection (1) starts immediately after the exhaust valve (not shown) is closed and ends in the first half of the intake stroke. The main injection (2) starts before the top dead center where the compression process ends and ends after the top dead center. Figure 1
As shown in (A), preliminary injection (1) into the combustion chamber (6) of 1
And one main injection (2) are connected to the fuel injection pump (7) and one fuel injection pipe (8) and one connected to this fuel injection pipe (8)
Directly into the combustion chamber (6) via the fuel injection nozzle (9). The preliminary injection (1) and the main injection (2) are
It is performed toward the inside of the cavity (12) of 1).

【0023】燃料噴射ポンプ(7)は、次のように構成さ
れている。図1(A)に示すように、燃料噴射ポンプ
(7)は逃げ孔式の列型ポンプである。バレル(20)にプ
ランジャ(21)が内嵌されている。プランジャ(21)は
燃料噴射カム(3)によってリフトされ、戻しバネ(22)
によって戻される。プランジャ(21)のリフト側にはプ
ランジャ室(23)が設けられている。バレル(20)の周
囲に燃料溜め室(24)が設けられている。バレル(20)
の周壁に燃料入口(25)と逃げ孔(26)とが設けられ、
これらを介してプランジャ室(23)と燃料溜め室(24)
とが連通されている。プランジャ(21)に斜め溝(27)
が設けられている。斜め溝(27)は縦溝(28)でプラン
ジャ室(23)と連通されている。プランジャ(21)は燃
料調量ラック(29)を介してガバナ部(図外)に連動連
結されている。プランジャ室(23)の吐出口には吸い戻
し弁(30)が設けられ、プランジャ室(23)は吸い戻し
弁(30)を介して燃料噴射管(8)と連通する。
The fuel injection pump (7) is constructed as follows. As shown in FIG. 1 (A), the fuel injection pump
(7) is an escape hole type row pump. A plunger (21) is fitted in the barrel (20). The plunger (21) is lifted by the fuel injection cam (3) and the return spring (22)
Returned by A plunger chamber (23) is provided on the lift side of the plunger (21). A fuel storage chamber (24) is provided around the barrel (20). Barrel (20)
A fuel inlet (25) and an escape hole (26) are provided on the peripheral wall of the
Through these, the plunger chamber (23) and the fuel storage chamber (24)
And are in communication. Diagonal groove (27) on the plunger (21)
Is provided. The oblique groove (27) communicates with the plunger chamber (23) by a vertical groove (28). The plunger (21) is interlockingly connected to the governor section (not shown) via a fuel metering rack (29). A suction return valve (30) is provided at the discharge port of the plunger chamber (23), and the plunger chamber (23) communicates with the fuel injection pipe (8) through the suction return valve (30).

【0024】予備噴射(1)と主噴射(2)とは、次のよう
にして行われる。プランジャ(21)が燃料噴射カム(3)
の主噴射用突起(5)でリフトされた後、戻しバネ(22)
によって戻されると、バレル(20)内のプランジャ室
(23)が負圧になり、燃料溜め室(24)内の燃料が燃料
入口(25)からプランジャ室(23)に吸入される。予備
噴射用突起(4)でプランジャ(21)が下死点からリフト
され、プランジャ(21)の周面で燃料入口(25)と逃げ
孔(26)とが閉じられると、プランジャ室(23)の燃料
油圧が上昇し、吸い戻し弁(30)が開弁され、プランジ
ャ室(23)から燃料噴射管(8)に燃料が吐出され、予備
噴射(1)が開始される。プランジャ(21)が更にリフト
され、斜め溝(27)で逃げ孔(26)が開かれると、プラ
ンジャ室(23)の燃料が縦溝(28)と斜め溝(27)と逃
げ孔(26)とを順に介して燃料溜め室(24)から逃げ、
プランジャ室(23)の燃料油圧が低下し、吸い戻し弁
(30)が閉弁され、その閉弁の際、燃料噴射管(8)内の
燃料の一部がプランジャ室(23)に吸い戻され、予備噴
射(1)が終了される。同じ動作により、主噴射用突起
(5)で主噴射(2)が行われる。予備噴射量と主噴射量と
は実質的に同一となる。
The preliminary injection (1) and the main injection (2) are performed as follows. Plunger (21) is the fuel injection cam (3)
After being lifted by the main injection protrusion (5) of the return spring (22)
Plunger chamber in barrel (20) when returned by
(23) becomes negative pressure, and the fuel in the fuel storage chamber (24) is sucked into the plunger chamber (23) from the fuel inlet (25). When the plunger (21) is lifted from the bottom dead center by the preliminary injection projection (4) and the fuel inlet (25) and the escape hole (26) are closed on the peripheral surface of the plunger (21), the plunger chamber (23) The fuel oil pressure increases, the suction return valve (30) is opened, the fuel is discharged from the plunger chamber (23) to the fuel injection pipe (8), and the preliminary injection (1) is started. When the plunger (21) is further lifted and the escape hole (26) is opened in the oblique groove (27), the fuel in the plunger chamber (23) is fed into the vertical groove (28), the oblique groove (27) and the escape hole (26). Escape from the fuel sump (24) through the and
The fuel pressure in the plunger chamber (23) has dropped and the suction valve
The valve (30) is closed, and when the valve is closed, part of the fuel in the fuel injection pipe (8) is sucked back into the plunger chamber (23) and the preliminary injection (1) is ended. By the same operation, the main injection projection
The main injection (2) is performed at (5). The preliminary injection amount and the main injection amount are substantially the same.

【0025】図2に示す第2参考例では、燃焼室(6)が
副室式とされ、予備噴射(1)と主噴射(2)とが副燃焼室
(13)で行われ、予備噴射(1)と主噴射(2)の際、副燃
焼室(13)と主燃焼室(14)との連通孔(15)がピスト
ン(11)の頂面(16)に向けられている。他の構造及び
機能は、第1実施形態と同じである。図2中、第1実施
形態と同一の要素には、図1と同一の符号を付してお
く。
In the second reference example shown in FIG. 2, the combustion chamber (6) is of the auxiliary chamber type, and the preliminary injection (1) and the main injection (2) are the auxiliary combustion chamber.
(13), during the pre-injection (1) and the main injection (2), the communication hole (15) between the auxiliary combustion chamber (13) and the main combustion chamber (14) forms the top surface of the piston (11) ( 16). Other structures and functions are the same as those in the first embodiment. 2, the same elements as those in the first embodiment are designated by the same reference numerals as those in FIG.

【0026】[0026]

【発明の実施の形態】図3に示す第1実施形態では、予
備噴射用突起(4)と主噴射用突起(5)とが異なる形状と
されている。すなわち、プランジャ(21)のリフトに用
いる予備噴射用突起(4)のリフト面が、主噴射用突起
(5)のリフト面よりも、基礎円から緩やかに上昇してい
る。このため、予備噴射用突起(4)によるプランジャ
(21)のリフト速度が主噴射用突起(5)によるプランジ
ャ(21)のリフト速度よりも遅く設定される。このた
め、予備噴射(1)に際しては、プランジャ室(21)のリ
フトによるプランジャ室(23)の燃料油圧の上昇速度が
低下し、予備噴射(1)の開始が遅れ、予備噴射量が主噴
射量よりも少なくなる。他の構造及び機能は、第1参考
と同じである。図3中、第1参考例と同一の要素には
図1と同一の符号を付しておく。
BEST MODE FOR CARRYING OUT THE INVENTION In the first embodiment shown in FIG. 3, the preliminary injection projection (4) and the main injection projection (5) have different shapes. That is, the lift surface of the preliminary injection projection (4) used for lifting the plunger (21) is the main injection projection.
It rises more slowly from the base circle than the lift surface in (5). Therefore, the plunger with the preliminary injection projection (4)
The lift speed of (21) is set slower than the lift speed of the plunger (21) by the main injection projection (5). Therefore, in the pre-injection (1), the rising speed of the fuel oil pressure in the plunger chamber (23) due to the lift of the plunger chamber (21) decreases, the start of the pre-injection (1) is delayed, and the pre-injection amount is the main injection amount. Less than the amount. For other structures and functions, refer to the first reference
Same as the example . 3, the same elements as those of the first reference example are designated by the same reference numerals as those of FIG.

【0027】図4に示す第2実施形態では、図2の第2
参考例と同様、燃焼室(6)が副室式とされ、予備噴射
(1)と主噴射(2)とが副燃焼室(13)で行われ、予備噴
射(1)と主噴射(2)の際、副燃焼室(13)と主燃焼室
(14)との連通孔(15)がピストン(11)の頂面(16)
に向けられている。また、図3の第1実施形態と同様、
予備噴射用突起(4)と主噴射用突起(5)とが異なる形状
とされている。すなわち、プランジャ(21)のリフトに
用いる予備噴射用突起(4)のリフト面が、主噴射用突起
(5)のリフト面よりも、基礎円から緩やかに上昇してい
る。他の構造及び機能は、第1・第2参考例及び第1実
施形態と同じである。図4中、これらと同一の要素には
図1〜図3と同一の符号を付しておく。
[0027] In the second embodiment shown in FIG. 4, first in Fig 2
As in the reference example , the combustion chamber (6) is of the sub-chamber type, and the preliminary
(1) and the main injection (2) are performed in the auxiliary combustion chamber (13), and during the preliminary injection (1) and the main injection (2), the auxiliary combustion chamber (13) and the main combustion chamber
The communication hole (15) with (14) is the top surface (16) of the piston (11).
Is directed to. Further, similar to the first embodiment of FIG.
The preliminary injection protrusion (4) and the main injection protrusion (5) have different shapes. That is, the lift surface of the preliminary injection projection (4) used for lifting the plunger (21) is the main injection projection.
It rises more slowly from the base circle than the lift surface in (5). Other structures and functions are the same as those of the first and second reference examples and the first actual example.
It is the same as the embodiment . In FIG. 4, the same elements as these are denoted by the same reference numerals as those in FIGS.

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

【図1】本発明の第1参考例を説明する図で、図1
(A)は燃料噴射装置の縦断面図、図1(B)は1サイ
クル中の噴射タイミングと噴射率を説明する図である。
FIG. 1 is a diagram illustrating a first reference example of the present invention.
1A is a vertical cross-sectional view of a fuel injection device, and FIG. 1B is a diagram illustrating injection timing and injection rate during one cycle.

【図2】本発明の第2参考例を説明する図で、図2
(A)は図1(A)相当図、図2(B)は図1(B)相
当図である。
FIG. 2 is a diagram illustrating a second reference example of the present invention.
1A is a view corresponding to FIG. 1A, and FIG. 2B is a view corresponding to FIG.

【図3】本発明の第1実施形態を説明する図で、図3
(A)は図1(A)相当図、図3(B)は図1(B)相
当図である。
FIG. 3 is a diagram for explaining the first embodiment of the present invention, and FIG.
1A is a view corresponding to FIG. 1A, and FIG. 3B is a view corresponding to FIG.

【図4】本発明の第2実施形態を説明する図で、図4
(A)は図1(A)相当図、図4(B)は図1(B)相
当図である。
FIG. 4 is a diagram for explaining the second embodiment of the present invention.
1A is a view corresponding to FIG. 1A, and FIG. 4B is a view corresponding to FIG.

【符号の説明】[Explanation of symbols]

(1)…予備噴射、(2)…主噴射、(3)…燃料噴射カム、
(4)…予備噴射用突起、(5)…主噴射用突起、(6)…燃
焼室、(7)…燃料噴射ポンプ、(8)…燃料噴射管、(9)
…燃料噴射ノズル、(10)…回転中心、(11)…ピスト
ン、(12)…キャビティ、(13)…副燃焼室、(14)…
主燃焼室、(15)…連通孔、(16)…頂面、(21)…プ
ランジャ。
(1) ... Preliminary injection, (2) ... Main injection, (3) ... Fuel injection cam,
(4) ... Projection for preliminary injection, (5) ... Projection for main injection, (6) ... Combustion chamber, (7) ... Fuel injection pump, (8) ... Fuel injection pipe, (9)
... Fuel injection nozzle, (10) ... Center of rotation, (11) ... Piston, (12) ... Cavity, (13) ... Sub-combustion chamber, (14) ...
Main combustion chamber, (15) ... communication hole, (16) ... top surface, (21) ... plunger.

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI F02M 61/14 F02M 61/14 310P (56)参考文献 特開 平10−18940(JP,A) 特開 平9−158810(JP,A) 特開 昭61−112724(JP,A) 実開 昭63−121772(JP,U) (58)調査した分野(Int.Cl.7,DB名) F02M 45/06 F02B 19/08 F02D 1/02 301 F02M 59/10 F02M 59/20 F02M 59/26 310 F02M 61/14 310 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 7 Identification code FI F02M 61/14 F02M 61/14 310P (56) References JP 10-18940 (JP, A) JP 9-158810 ( JP, A) JP 61-112724 (JP, A) Actually developed 63-121772 (JP, U) (58) Fields investigated (Int.Cl. 7 , DB name) F02M 45/06 F02B 19/08 F02D 1/02 301 F02M 59/10 F02M 59/20 F02M 59/26 310 F02M 61/14 310

Claims (6)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 燃料噴射として、予備噴射(1)と主噴射
(2)とが行われるように構成した、ディーゼルエンジン
の燃料噴射装置において、 1の燃料噴射カム(3)に1の予備噴射用突起(4)と1の
主噴射用突起(5)とが設けられ、燃料噴射ポンプ(7)の
プランジャ(21)が予備噴射用突起(4)によってリフト
される最大リフト寸法が、主噴射用突起(5)によってリ
フトされる最大リフト寸法と実質的に同一とされ、 予備噴射用突起(4)と主噴射用突起(5)とが異なる形状
とされ、予備噴射用突起(4)によるプランジャ(21)の
リフト速度が主噴射用突起(5)によるプランジャ(21)
のリフト速度よりも遅く設定されているもの。
1. A pre-injection (1) and a main injection as fuel injection
In a fuel injection device for a diesel engine configured so that (2) and (2) are performed, one fuel injection cam (3) has one preliminary injection protrusion (4) and one main injection protrusion (5). The maximum lift dimension of the plunger (21) of the fuel injection pump (7) lifted by the preliminary injection projection (4) is substantially the same as the maximum lift dimension of the main injection projection (5). And the preliminary injection projection (4) and the main injection projection (5) have different shapes.
And the plunger (21) by the preliminary injection projection (4)
Plunger (21) with lift speed due to the main injection projection (5)
It is set to be slower than the lift speed of.
【請求項2】 請求項1に記載したディーゼルエンジン
の燃料噴射装置において、予備噴射用突起(4)と主噴射
用突起(5)とが、燃料噴射カム(3)の回転中心(10)を
間に挟んで、相互反対側に配置されているもの。
2. The fuel injection device for a diesel engine according to claim 1 , wherein the pre-injection projection (4) and the main-injection projection (5) define a rotation center (10) of the fuel injection cam (3). Those placed on opposite sides of each other, sandwiched between them.
【請求項3】 請求項1または請求項2に記載したディ
ーゼルエンジンの燃料噴射装置において、予備噴射(1)
が吸気工程の前半に開始され、主噴射(2)が圧縮工程の
後半に開始されるもの。
3. A fuel injection device for a diesel engine according to claim 1 or 2 , wherein preliminary injection (1)
Is started in the first half of the intake stroke, and main injection (2) is started in the second half of the compression stroke.
【請求項4】 請求項3に記載したディーゼルエンジン
の燃料噴射装置において、1の燃焼室(6)への予備噴射
(1)と主噴射(2)とが燃料噴射ポンプ(7)に接続された
1の燃料噴射管(8)と、この燃料噴射管(8)に接続され
た1の燃料噴射ノズル(9)とを介して、燃焼室(6)に直
接に行われるようにしたもの。
4. The fuel injection device for a diesel engine according to claim 3 , wherein preliminary injection into one combustion chamber (6).
One fuel injection pipe (8) in which (1) and main injection (2) are connected to a fuel injection pump (7), and one fuel injection nozzle (9) connected to this fuel injection pipe (8) It is designed to be directly conducted to the combustion chamber (6) via and.
【請求項5】 請求項4に記載したディーゼルエンジン
の燃料噴射装置において、燃焼室(6)が直接噴射式とさ
れ、予備噴射(1)と主噴射(2)とがピストン(11)のキ
ャビティ(12)内に向けて行われるもの。
5. The fuel injection device for a diesel engine according to claim 4 , wherein the combustion chamber (6) is of a direct injection type, and the preliminary injection (1) and the main injection (2) are cavities of a piston (11). (12) Things to be done inward.
【請求項6】 請求項4に記載したディーゼルエンジン
の燃料噴射装置において、燃焼室(6)が副室式とされ、
予備噴射(1)と主噴射(2)とが副燃焼室(13)で行わ
れ、予備噴射(1)と主噴射(2)の際、副燃焼室(13)と
主燃焼室(14)との連通孔(15)がピストン(11)の頂
面(16)に向けられているもの。
6. The fuel injection device for a diesel engine according to claim 4 , wherein the combustion chamber (6) is of a sub chamber type,
The preliminary injection (1) and the main injection (2) are performed in the auxiliary combustion chamber (13), and during the auxiliary injection (1) and the main injection (2), the auxiliary combustion chamber (13) and the main combustion chamber (14) The communication hole (15) with is directed to the top surface (16) of the piston (11).
JP01167098A 1998-01-23 1998-01-23 Diesel engine fuel injection system Expired - Fee Related JP3516583B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP01167098A JP3516583B2 (en) 1998-01-23 1998-01-23 Diesel engine fuel injection system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP01167098A JP3516583B2 (en) 1998-01-23 1998-01-23 Diesel engine fuel injection system

Publications (2)

Publication Number Publication Date
JPH11210588A JPH11210588A (en) 1999-08-03
JP3516583B2 true JP3516583B2 (en) 2004-04-05

Family

ID=11784432

Family Applications (1)

Application Number Title Priority Date Filing Date
JP01167098A Expired - Fee Related JP3516583B2 (en) 1998-01-23 1998-01-23 Diesel engine fuel injection system

Country Status (1)

Country Link
JP (1) JP3516583B2 (en)

Also Published As

Publication number Publication date
JPH11210588A (en) 1999-08-03

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