JPS6141977Y2 - - Google Patents

Info

Publication number
JPS6141977Y2
JPS6141977Y2 JP7698478U JP7698478U JPS6141977Y2 JP S6141977 Y2 JPS6141977 Y2 JP S6141977Y2 JP 7698478 U JP7698478 U JP 7698478U JP 7698478 U JP7698478 U JP 7698478U JP S6141977 Y2 JPS6141977 Y2 JP S6141977Y2
Authority
JP
Japan
Prior art keywords
engine
fuel injection
timing
injection pump
advance
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
Application number
JP7698478U
Other languages
Japanese (ja)
Other versions
JPS54177417U (en
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 filed Critical
Priority to JP7698478U priority Critical patent/JPS6141977Y2/ja
Publication of JPS54177417U publication Critical patent/JPS54177417U/ja
Application granted granted Critical
Publication of JPS6141977Y2 publication Critical patent/JPS6141977Y2/ja
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 本考案は、各気筒に対する燃料の供給を、燃料
噴射ポンプによつて行うようにした燃料噴射式の
エンジンに関するものである。
[Detailed Description of the Invention] The present invention relates to a fuel injection type engine in which fuel is supplied to each cylinder by a fuel injection pump.

一般に、この種のエンジンにおいて噴射供給し
た燃料が燃焼を完了するまでには、エンジンの回
転数によつて多少の差があるものの略一定の時間
が必要である。それ故に、この種の燃料噴射エン
ジンにおける燃料噴射ポンプには、例えば実公昭
51−21231号公報に記載されているようにエンジ
ンから当該燃料噴射ポンプへの動力伝達の途中に
遠心式等の噴射時期進角機構を設けて、前記燃料
噴射ポンプによる燃料の噴射時期を、エンジンの
回転数に比例して進角するようにしていることは
周知の通りである。
Generally, in this type of engine, a substantially constant amount of time is required for the injected fuel to complete combustion, although it varies somewhat depending on the engine speed. Therefore, for example, the fuel injection pump in this type of fuel injection engine is
As described in Japanese Patent No. 51-21231, an injection timing advance mechanism such as a centrifugal type is provided in the middle of power transmission from the engine to the fuel injection pump, and the injection timing of the fuel by the fuel injection pump is controlled by the engine. It is well known that the angle is advanced in proportion to the number of revolutions.

しかし、エンジンにおける吸・排気弁をカム軸
によつて開閉する時期は、エンジンの回転数に拘
わらず常に一定であるから、前記のように燃料噴
射ポンプによる燃料の噴射時期のみを進角機構に
てエンジンの回転数に応じて可変することは、エ
ンジンにおける吸・排気弁が開閉する時期と燃料
噴射の時期との位相の関係が刻々変化することに
なつて、両者の最適な位相関係が広い回転域にわ
たつて得られず、従つてエンジンの回転数に対す
る発生トルクは、両者の最適位相関係を呈するよ
うな特定の回転数で最高になり、これ以外の回転
数では発生トルクが急に低下すると言うように、
発生トルク曲線が比較的尖つた形状になるのであ
つた。
However, the timing at which the intake and exhaust valves in the engine are opened and closed by the camshaft is always constant regardless of the engine speed, so as mentioned above, only the timing of fuel injection by the fuel injection pump is controlled by the advance mechanism. The fact that the engine speed varies according to the engine speed means that the phase relationship between the opening/closing timing of the intake/exhaust valves in the engine and the fuel injection timing changes from moment to moment, and the optimal phase relationship between the two is wide. Therefore, the generated torque with respect to the engine speed is highest at a certain speed where the optimum phase relationship between the two is exhibited, and the generated torque suddenly decreases at other speeds. As they say,
The generated torque curve had a relatively sharp shape.

本考案は、この問題を解消することを目的とす
るもので、この目的を達成するために、エンジン
から、当該エンジンに対する燃料噴射ポンプへの
動力伝達部に、前記燃料噴射ポンプによる燃料の
噴射時期をエンジンの回転数に比例して進角する
ようにした進角機構を設けて成る燃料噴射式エン
ジンにおいて、前記エンジンにおける吸・排気弁
を開閉するカム軸に、前記進角機構の出力側から
動力伝達するように構成したものである。
The purpose of the present invention is to solve this problem, and in order to achieve this purpose, the power transmission part from the engine to the fuel injection pump for the engine has a timing control for the injection of fuel by the fuel injection pump. In a fuel injection engine equipped with an advance mechanism that advances the angle in proportion to the engine rotational speed, a camshaft that opens and closes intake and exhaust valves in the engine is provided with a camshaft from the output side of the advance mechanism. It is configured to transmit power.

以下本考案の実施例を図面について説明する
と、図において1は、クランクケース3の下部に
オイルパン4を備えたシリンダブロツク2の上面
に、燃料噴射弁6付きシリンダヘツド5を取付け
て成るエンジンを示し、該エンジン1のシリンダ
ブロツク2におけるクランクケース3内には、タ
ペツト9、押棒10及び動弁機構(図示せず)を
介してシリンダヘツド5における吸・排気弁(図
示せず)を開閉するためのカム軸8が、前記エン
ジン1におけるクランク軸7と平行に設けられ、
また、前記クランクケース3の外側には、シリン
ダヘツド5における燃料噴射弁6に燃料を供給す
るための燃料噴射ポンプ11が、シリンダブロツ
ク2に取付く歯車ケース12を介して設けられて
いる。
Embodiments of the present invention will be described below with reference to the drawings. In the drawings, reference numeral 1 shows an engine consisting of a cylinder head 5 with a fuel injection valve 6 attached to the upper surface of a cylinder block 2 which is provided with an oil pan 4 at the bottom of a crankcase 3. In the crankcase 3 of the cylinder block 2 of the engine 1, intake and exhaust valves (not shown) in the cylinder head 5 are opened and closed via a tappet 9, a push rod 10, and a valve mechanism (not shown). A camshaft 8 is provided parallel to the crankshaft 7 in the engine 1,
Further, on the outside of the crankcase 3, a fuel injection pump 11 for supplying fuel to the fuel injection valve 6 in the cylinder head 5 is provided via a gear case 12 attached to the cylinder block 2.

前記燃料噴射ポンプ11における入力軸13に
は、従来公知の遠心式等の進角機構14を設け、
該進角機構14の入力軸に、前記クランク軸7の
回転を、スプロケツト15,16及びその間に巻
き掛けしたチエン17にて1/2に減速して伝達す
る一方、前記進角機構14の出力側を、燃料噴射
ポンプ11の入力軸13に連結すると共に、互い
に噛合する同じ歯数の歯車18,19を介して、
前記吸・排気弁を開閉するためのカム軸8に動力
伝達するように構成する。
The input shaft 13 of the fuel injection pump 11 is provided with a conventionally known centrifugal advance mechanism 14,
The rotation of the crankshaft 7 is reduced to 1/2 and transmitted to the input shaft of the advance angle mechanism 14 by the sprockets 15 and 16 and the chain 17 wound between them, while the output of the advance angle mechanism 14 is transmitted to the input shaft of the advance angle mechanism 14. The side is connected to the input shaft 13 of the fuel injection pump 11, and via gears 18 and 19 having the same number of teeth that mesh with each other,
It is configured to transmit power to a camshaft 8 for opening and closing the intake and exhaust valves.

この構成において、エンジン1の回転数が早く
なれば、進角機構14がその出力側の位相を回転
数に比例して進角方向に進ませるように作動する
から、燃料噴射ポンプ11における燃料噴射の時
期は、低回転時よりも早い時期に進角されると同
時に、カム軸8による吸・排気弁の開閉の時期を
低回転時よりも早い時期に進角されることにな
り、また、エンジン1の回転数が遅くなれば、進
角機構14によつて燃料噴射の時期が高い回転時
よりも遅角されると共に、吸・排気弁の回転の時
期も遅角されると言うように、燃料の噴射時期及
び吸・排気弁の開閉時期は、一定の位相関係を保
つた状態のまま、エンジンの回転数に応じて、進
角又は遅角に制御されるのである。
In this configuration, when the rotation speed of the engine 1 increases, the advance angle mechanism 14 operates to advance the phase on the output side in the advance direction in proportion to the rotation speed, so that the fuel injection in the fuel injection pump 11 The timing of is advanced earlier than when the rotation speed is low, and at the same time, the timing of opening and closing of the intake and exhaust valves by the camshaft 8 is advanced earlier than when the rotation speed is low. As the rotation speed of the engine 1 becomes lower, the timing of fuel injection is retarded by the advance mechanism 14 compared to when the rotation speed is high, and the timing of rotation of the intake and exhaust valves is also retarded. The fuel injection timing and the opening/closing timing of the intake and exhaust valves are controlled to be advanced or retarded depending on the engine speed while maintaining a constant phase relationship.

なお、前記進角機構14を、吸・排気弁の開閉
用カム軸8等のように、燃料噴射ポンプ11以外
の箇所に設けて、その出力側から、燃料噴射ポン
プ11及び吸・排気弁の開閉用カム軸3に動力伝
達するように構成しても良いのである。
Note that the advance mechanism 14 is provided at a location other than the fuel injection pump 11, such as the camshaft 8 for opening/closing the intake/exhaust valves, and the advance mechanism 14 is provided at a location other than the fuel injection pump 11, such as the camshaft 8 for opening/closing the intake/exhaust valves. It may be configured to transmit power to the opening/closing camshaft 3.

以上の通り本考案によれば、燃料噴射の時期を
エンジンの回転数に比例して進角制御するに際し
て、エンジンにおける吸・排気弁の開閉時期を
も、同時に進角でき、両者の位相関係を全回転域
にわたつて略一定に保持できるから、エンジンに
おける発生トルク曲線は、従来の尖つたものに比
べてなだらかになり、発生トルクを広い回転域に
わたつて向上できるのである。
As described above, according to the present invention, when the fuel injection timing is advanced in proportion to the engine speed, the opening and closing timings of the intake and exhaust valves in the engine can also be advanced at the same time, and the phase relationship between the two can be adjusted. Since it can be held substantially constant over the entire rotation range, the generated torque curve in the engine becomes gentler than the conventional sharp curve, and the generated torque can be improved over a wide rotation range.

しかも、エンジンにおける吸・排気弁の開閉時
期を、エンジンの回転数に比例して進角する進角
機構を、燃料噴射ポンプにおける進角機構と供用
するので、両方に別々の進角機構を設ける必要が
なく一つの進角機構で済み、構造が簡単になつて
安価に提供できると共に、取付けスペースの増大
延いてはエンジンの大型化を回避できるのであ
る。
Moreover, the advance mechanism that advances the opening and closing timing of the intake and exhaust valves in the engine in proportion to the engine speed is shared with the advance mechanism in the fuel injection pump, so separate advance mechanisms are provided for both. This eliminates the need for a single advance angle mechanism, which simplifies the structure and can be provided at low cost, and also avoids an increase in installation space and, in turn, an increase in the size of the engine.

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

図面は本考案の実施例を示し、第1図はエンジ
ンの一部切欠側面図、第2図は動力伝達部の平面
図である。 1……エンジン、2……シリンダブロツク、5
……シリンダヘツド、6……燃料噴射弁、7……
クランク軸、8……吸・排気弁の開閉用カム軸、
11……燃料噴射ポンプ、14……進角機構。
The drawings show an embodiment of the present invention, with FIG. 1 being a partially cutaway side view of the engine, and FIG. 2 being a plan view of the power transmission section. 1...Engine, 2...Cylinder block, 5
...Cylinder head, 6...Fuel injection valve, 7...
Crankshaft, 8...Camshaft for opening and closing intake and exhaust valves,
11... Fuel injection pump, 14... Advance angle mechanism.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] エンジンから、当該エンジンに対する燃料噴射
ポンプへの動力伝達部に、前記燃料噴射ポンプに
よる燃料の噴射時期をエンジンの回転数に比例し
て進角するようにした進角機構を設けて成る燃料
噴射式エンジンにおいて、前記エンジンにおける
吸・排気弁を開閉するカム軸に、前記進角機構の
出力側から動力伝達するように構成したことを特
徴とする燃料噴射式エンジン。
A fuel injection type comprising an advance mechanism that advances the timing of fuel injection by the fuel injection pump in proportion to the engine rotation speed, in a power transmission section from the engine to the fuel injection pump for the engine. 1. A fuel injection engine characterized in that the engine is configured such that power is transmitted from the output side of the advance angle mechanism to a camshaft that opens and closes intake and exhaust valves in the engine.
JP7698478U 1978-06-05 1978-06-05 Expired JPS6141977Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7698478U JPS6141977Y2 (en) 1978-06-05 1978-06-05

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7698478U JPS6141977Y2 (en) 1978-06-05 1978-06-05

Publications (2)

Publication Number Publication Date
JPS54177417U JPS54177417U (en) 1979-12-14
JPS6141977Y2 true JPS6141977Y2 (en) 1986-11-28

Family

ID=28992764

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7698478U Expired JPS6141977Y2 (en) 1978-06-05 1978-06-05

Country Status (1)

Country Link
JP (1) JPS6141977Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60112644U (en) * 1983-12-31 1985-07-30 いすゞ自動車株式会社 Internal combustion engine advance device

Also Published As

Publication number Publication date
JPS54177417U (en) 1979-12-14

Similar Documents

Publication Publication Date Title
US6250266B1 (en) Variable valve timing mechanism for engine
JPH086568B2 (en) Engine valve operation control device
US5199393A (en) Timing apparatus for a four-stroke engine with camshafts running at differentiated angular rotation
US8635988B2 (en) Variable valve device for internal combustion engine
JPS6141977Y2 (en)
JPS61252836A (en) 4-cycle engine
JP2738745B2 (en) Valve timing control device for DOHC engine
DE3406100A1 (en) Speed-dependent adjustment of the valve timing in combustion engines
JP2809437B2 (en) Multi-valve 4-cycle engine
EP0343627B1 (en) Valve drive train for a v-type internal combustion engine
JPH0549804B2 (en)
JPH0354307A (en) Valve timing control device of dohc engine
JPH059610B2 (en)
JP3395350B2 (en) Valve timing control device for DOHC engine
JPS603924Y2 (en) valve timing control device
JP3049120B2 (en) Ignition system for multi-cylinder engine
GB2202002A (en) I.C. engine inlet valve timing control
JP2926366B2 (en) Engine output control device
JPS60164609A (en) Spark advance device for valve on-off timing of four-cycle engine
JPH042780B2 (en)
JPH0158324B2 (en)
JPH0151886B2 (en)
JP2745310B2 (en) Engine valve gear
JPS63230917A (en) Valve-timing changing device for double overhead cam engine
JPS5865919A (en) Adjusting system of optional valve timing