JPS58133451A - Engine controller - Google Patents

Engine controller

Info

Publication number
JPS58133451A
JPS58133451A JP1439682A JP1439682A JPS58133451A JP S58133451 A JPS58133451 A JP S58133451A JP 1439682 A JP1439682 A JP 1439682A JP 1439682 A JP1439682 A JP 1439682A JP S58133451 A JPS58133451 A JP S58133451A
Authority
JP
Japan
Prior art keywords
engine
valve
lever
returned
piston
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.)
Pending
Application number
JP1439682A
Other languages
Japanese (ja)
Inventor
Toshihiro Ono
大野 俊弘
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.)
Hitachi Construction Machinery Co Ltd
Original Assignee
Hitachi Construction Machinery Co Ltd
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 Hitachi Construction Machinery Co Ltd filed Critical Hitachi Construction Machinery Co Ltd
Priority to JP1439682A priority Critical patent/JPS58133451A/en
Publication of JPS58133451A publication Critical patent/JPS58133451A/en
Pending legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02FDREDGING; SOIL-SHIFTING
    • E02F9/00Component parts of dredgers or soil-shifting machines, not restricted to one of the kinds covered by groups E02F3/00 - E02F7/00
    • E02F9/20Drives; Control devices
    • E02F9/22Hydraulic or pneumatic drives
    • E02F9/2246Control of prime movers, e.g. depending on the hydraulic load of work tools
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D29/00Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • F02D29/04Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/02Systems essentially incorporating special features for controlling the speed or actuating force of an output member
    • F15B11/04Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
    • F15B11/05Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed specially adapted to maintain constant speed, e.g. pressure-compensated, load-responsive
    • F15B11/055Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed specially adapted to maintain constant speed, e.g. pressure-compensated, load-responsive by adjusting the pump output or bypass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/20Fluid pressure source, e.g. accumulator or variable axial piston pump
    • F15B2211/275Control of the prime mover, e.g. hydraulic control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/60Circuit components or control therefor
    • F15B2211/635Circuits providing pilot pressure to pilot pressure-controlled fluid circuit elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/60Circuit components or control therefor
    • F15B2211/635Circuits providing pilot pressure to pilot pressure-controlled fluid circuit elements
    • F15B2211/6355Circuits providing pilot pressure to pilot pressure-controlled fluid circuit elements having valve means

Abstract

PURPOSE:To obtain the effect of energy saving or favorable workability corresponding to the working condition in such a way that resistance in the duct of a hydraulic device can be selected and changed over at the time of transferring the engine from its high speed revolution to its low speed revolution. CONSTITUTION:When a change-over valve 20 is manually changed over to a position 1, the pressurized oil in a pump 8 actuates a change-over valve 7 and arrives at the change-over valve 20 upon control of a lever 9. Since duct resistance for a throttle valve 23 is large, the pressurized oil is quickly fed to a cylinder 12, a piston 13 is moved to the right, and the engine 1 makes its high speed revolution. When the lever 9 is returned to its neutral position, the piston 13 is moved to the left, and the revolution speed of the engine 1 is lowered, or the pressurized oil can not be quickly returned to a tank 5, and the descent time is made longer. Besides, when the valve 20 is changed over to the position II, and a control lever 9 is returned to its neutral position, the pressurized oil on the rod side of the cylinder 12 is returned to the tank 5 the piston 13 is also quickly moved to the left, the injecting rate is reduced at once, and the descent time is made shorter.

Description

【発明の詳細な説明】 本発明はエンジンの制御装置に係り、特に作業機械の油
圧ホンダを駆動するタンク/の制御に好適なエンジン制
御装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an engine control device, and more particularly to an engine control device suitable for controlling a tank that drives a hydraulic engine of a working machine.

油圧シ讐ペル等の作業機械は、アクチュエータに圧油を
供給する油圧ポンプを備え、この油圧ポンプを作業機械
に塔載しているエンジンで駆動する。そして、このエン
ジンの回転速度は操作レバーで制御するようになってい
る。
A working machine such as a hydraulic pump is equipped with a hydraulic pump that supplies pressure oil to an actuator, and this hydraulic pump is driven by an engine mounted on the working machine. The rotational speed of this engine is controlled by a control lever.

このようなエンジンの制御装置の従来例を第1図に示す
A conventional example of such an engine control device is shown in FIG.

図で、lはエンジン、2はエンジンIK4Isえられて
いる燃料噴射機構、3は燃料噴射機構の燃料噴射量コン
トロールレバーである。コントロールレバー8は軸Cを
中心に回動自在に設けられ、時計方向の回動により燃料
噴射機構8がらの燃料噴射量を減少してエンジンlを低
迷回転とし、反時計方向の回動により燃料噴射量を増加
してエンジンlを高速回転とする。
In the figure, 1 is an engine, 2 is a fuel injection mechanism provided with the engine IK4Is, and 3 is a fuel injection amount control lever of the fuel injection mechanism. The control lever 8 is rotatably provided around an axis C. When the control lever 8 is rotated clockwise, the amount of fuel injected from the fuel injection mechanism 8 is reduced to make the engine 1 sluggish, and when the control lever 8 is rotated counterclockwise, the fuel injection The injection amount is increased to make the engine 1 rotate at a high speed.

4はエンジンllcJItAmされるl山王ポンプであ
り、タンク5に貯蔵されている油を圧油として油圧回路
に供給する。6は油圧ポンプ4かもの圧油により駆動さ
れるアクチェエータであり、図には(円圧シリンダが示
されている。7は油圧ホンダ4とアクチェエータ6を接
続する油圧回路に介在する方向切換弁であり、アクチェ
エータ6の作動方向およびアクチュエータ6への圧油の
量を制御する。
Reference numeral 4 designates a Sanno pump which is operated by an engine llcJItAm, and supplies oil stored in a tank 5 to the hydraulic circuit as pressure oil. 6 is an actuator driven by the pressure oil of the hydraulic pump 4, and in the figure (a circular pressure cylinder is shown). Controls the operating direction of the actuator 6 and the amount of pressure oil supplied to the actuator 6.

8は方向切換弁7を作動する圧油を供給するためのパイ
ロット用油圧ポンプ、9は運転席に設けられた操作レバ
ーで、操作レバー9の操作方向および操作量に応じてパ
イロット用油圧ポンプ8の圧油を方向切換弁7に供給し
てこれを作動する。
8 is a pilot hydraulic pump for supplying pressure oil to operate the directional control valve 7; 9 is an operating lever provided on the driver's seat; the pilot hydraulic pump 8 is activated depending on the operating direction and operating amount of the operating lever 9; Pressure oil is supplied to the directional control valve 7 to operate it.

10a、  lObは操作レバー9の操作量に応じて切
換えられるパイロット切換弁で、操作レバー9を図で左
側へ倒すとパイロット切換弁10aが、右側へ倒すとパ
イロット切換弁10bが切換えられ、操作レバー9が中
立位置にあるときはタンク5と連通する。11はパイロ
ット切換弁10a、  lObを経てきたパイロット用
油圧ポンプ8からの圧油を通過させるシャトル弁である
10a and lOb are pilot switching valves that are switched according to the amount of operation of the operating lever 9. When the operating lever 9 is pushed to the left in the figure, the pilot switching valve 10a is switched, and when it is pushed to the right, the pilot switching valve 10b is switched, and the operating lever is switched. When 9 is in the neutral position, it communicates with tank 5. 11 is a shuttle valve that allows the pressure oil from the pilot hydraulic pump 8 to pass through the pilot switching valves 10a and 1Ob.

12は制御シリンダである。制御シリンダ12はピスト
ン18、ピストンロッド14.  ピストン1Bをロッ
ド14側へ押すスプリング15より成る。制御シリンダ
12のロッド1411111は前記シャトル弁11と接
続されている。16は前記コントロールレバー8の端部
とロッド14の端部とを可回動に連結する連結杆である
12 is a control cylinder. The control cylinder 12 includes a piston 18, a piston rod 14. It consists of a spring 15 that pushes the piston 1B toward the rod 14 side. The rod 1411111 of the control cylinder 12 is connected to the shuttle valve 11. Reference numeral 16 is a connecting rod that rotatably connects the end of the control lever 8 and the end of the rod 14.

シャトル弁11.制御シリンダ12、連結杆16、コン
トロールレバー8、燃料噴射機構2によりエンジン制御
装置が構成されている。
Shuttle valve 11. The control cylinder 12, the connecting rod 16, the control lever 8, and the fuel injection mechanism 2 constitute an engine control device.

なお、17および18はそれぞれ油圧ポンプ4およびパ
イロット用油圧ポンプ8の最高圧力を設矩するリリーフ
弁である。
Note that 17 and 18 are relief valves that set the maximum pressure of the hydraulic pump 4 and the pilot hydraulic pump 8, respectively.

次に、このエンジン制御装置の動作を説明する。Next, the operation of this engine control device will be explained.

操作レバー9を図で左側又は右側へ倒すとパイロット用
油圧ポンプ8からの圧油はパイロット切換弁10a又は
lObを介しその圧力により方向切換弁7を操作レバー
9の操作量に応じて図の右方又は左方へ移行させ、油圧
ポンプ4の圧油をアクチュエータ6のヘッド側又はロッ
ド側へ供給すると共にロッド側又はヘッド側の油をタン
ク5へ戻す。
When the operating lever 9 is tilted to the left or right in the figure, the pressure oil from the pilot hydraulic pump 8 flows through the pilot switching valve 10a or lOb, and the pressure causes the directional switching valve 7 to shift to the right in the figure according to the amount of operation of the operating lever 9. The pressure oil from the hydraulic pump 4 is supplied to the head side or the rod side of the actuator 6, and the oil from the rod side or head side is returned to the tank 5.

これによりアクチェエータ6は操作レバー9の操作量に
応じて作動する。
Thereby, the actuator 6 operates according to the amount of operation of the operating lever 9.

同時に、パイロット切換弁10a又は10bを通った圧
油はシャトル弁11を介して制御シリンダ12のロッド
側へ供給される。なお、このとき、シャトル弁11はパ
イロット切換弁10b又は10aを通りタンク5へ通じ
る回路を遮断する。この結果、ピストン18はスプリン
グ15のばね力に抗して右方へ移行する。したがって、
ロッド14および連結杆16も右方へ移行しコントロー
ルレバー8は軸Cを中心に反時計方向へ回動し、燃料噴
射量を増加してエンジンlを高速回転させ、油圧ポンプ
令の吐出量を増大させる。
At the same time, the pressure oil that has passed through the pilot switching valve 10a or 10b is supplied to the rod side of the control cylinder 12 via the shuttle valve 11. Note that at this time, the shuttle valve 11 cuts off the circuit that passes through the pilot switching valve 10b or 10a and leads to the tank 5. As a result, the piston 18 moves to the right against the spring force of the spring 15. therefore,
The rod 14 and the connecting rod 16 also move to the right, and the control lever 8 rotates counterclockwise around the axis C to increase the fuel injection amount, rotate the engine at high speed, and increase the discharge amount of the hydraulic pump command. increase

操作レバー9を中立位置へ戻すとパイロット切換弁10
a又は1(Jbは元に戻り、パイロット甲油圧ポンプ8
からの圧油の通路を遮断するとともに制御シリンダ12
のロッド側の油をシャトル弁11を介してタンク5へ戻
す。このため、ピストン1B &!スプリング15のば
ね力により左方へ移行する。したがってロッド14、連
結杆16も左方へ移行してコントロールレバー8を軸C
を中心に時計方向へ回動し、燃料噴射量を減少してエン
ジンlの回転速度を低速とする。
When the operating lever 9 is returned to the neutral position, the pilot switching valve 10
a or 1 (Jb returns to its original position, pilot A hydraulic pump 8
While blocking the passage of pressure oil from the control cylinder 12
The oil on the rod side is returned to the tank 5 via the shuttle valve 11. For this reason, piston 1B &! It moves to the left by the spring force of the spring 15. Therefore, the rod 14 and the connecting rod 16 are also moved to the left to move the control lever 8 to the axis C.
It rotates clockwise around , decreases the fuel injection amount, and lowers the rotational speed of the engine l.

このようなエンジン制御装置においては、操作レバー9
を中立位置へ戻すことにより自動的に燃料噴射量を減少
してエンジンlを低速とするので不必要な燃料の消費を
抑えて省エネルギー効果を得ることができる。この省エ
ネルギー効果は、エンジンlの高速回転から低速回転へ
の移行時間(以下、降下時間という。)が早ければ早い
ほど太きい。
In such an engine control device, the operating lever 9
By returning the engine to the neutral position, the fuel injection amount is automatically reduced and the engine speed is reduced, so unnecessary fuel consumption can be suppressed and an energy saving effect can be obtained. This energy-saving effect is greater as the transition time from high-speed rotation to low-speed rotation (hereinafter referred to as descent time) of the engine 1 is faster.

一方、エンジン1が低速回転から高速回転へ移行する時
間(以下、復帰時間という。)は、負荷が大きい場合可
成り長い。即ち、操作レバー9を中立位置から操作した
場合、軽負荷であればエンジンは短時間で高速回転へ復
帰するが、負荷が大きいと長い復帰時間を要する。した
がって、この長い復帰時間の間は油圧ポンプ4の圧油の
吐出量も充分でなく、作業性に悪影響を及ぼす。時に、
操作レバー9の中立位置から操作位置への切保が頻繁な
作業においてその影響するところが太さい。
On the other hand, the time it takes for the engine 1 to shift from low speed rotation to high speed rotation (hereinafter referred to as return time) is quite long when the load is large. That is, when the operating lever 9 is operated from the neutral position, the engine returns to high speed rotation in a short time if the load is light, but it takes a long time to return to high speed if the load is large. Therefore, during this long return time, the amount of pressure oil discharged from the hydraulic pump 4 is not sufficient, which adversely affects work efficiency. Sometimes,
In operations where the operating lever 9 is frequently cut from the neutral position to the operating position, its influence is large.

この悪影響を除き作業性を艮くするためには、エンジン
lの降下時間を長くして、操作レバー9の中立位置から
操作位置への切換が降下時間の中途Kかかるようにすれ
ばよい。即ち、このようにすれば、操作レバー9の切換
が頻繁に行われる場合、操作レバー9を中立位置とした
後備かな間隔で操作位置に切換えると、エンジンlはま
だ低速回転にはなっていないので、高速回転へ復帰する
時間は極めて短時間となる。
In order to eliminate this negative effect and improve workability, the lowering time of the engine 1 may be lengthened so that switching of the operating lever 9 from the neutral position to the operating position takes K during the lowering time. That is, by doing this, if the operating lever 9 is frequently switched, if the operating lever 9 is placed in the neutral position and switched to the operating position at regular intervals, the engine l has not yet reached low speed rotation. , the time to return to high speed rotation is extremely short.

しかしながら、操作レバー9を中立位置へ戻した後、次
に操作位置へ切換えるまでの時間が長いような作業にお
いては、前述したように省エネルギー効果の見地から降
下時間を短かくするのが望ましい。
However, in operations where it takes a long time to switch the operating lever 9 to the next operating position after returning it to the neutral position, it is desirable to shorten the lowering time from the viewpoint of energy saving effect, as described above.

結局、省エネルギー効果を得るためには降下時間を短か
くする必要があるが、良好な作業性を得るためには降下
時間を長くしなけれはならないという相反する要望があ
り、いずれを採っても欠点が生じるのは免れない。
In the end, there are contradictory demands: it is necessary to shorten the descent time in order to obtain an energy-saving effect, but it is necessary to lengthen the descent time in order to obtain good workability, and there are drawbacks to either option. It is inevitable that this will occur.

本発明は、省エネルギー効果および良好な作業性のいず
れをも満すことができるエンジンの制御装置を提供する
にある。
An object of the present invention is to provide an engine control device that can satisfy both energy saving effects and good workability.

この目的を達成するため、本発明は、油圧ポンプを連結
したエンジンと、このエンジンの燃料噴と、前記油出ポ
ンプに接続されたアクチュエータを操作する操作装置と
、前記油圧装置に接続され前記操作装置の操作に応じて
圧油を導く管路とを備えたエンジン制御装置において、
前記エンジンを高速から低速へ移行させるときの前記管
路の管路抵抗を選択的に切換えることができるようにし
たことを%徴とする。
To achieve this object, the present invention provides an engine connected to a hydraulic pump, a fuel injection of the engine, an operating device for operating an actuator connected to the oil pump, and an operating device connected to the hydraulic device for operating the actuator. In an engine control device equipped with a conduit that guides pressure oil according to the operation of the device,
A feature of the present invention is that the resistance of the conduit can be selectively changed when the engine is moved from high speed to low speed.

以下、不発明を第2図に示す一実施例に基づいて説明す
る。
Hereinafter, the invention will be explained based on an embodiment shown in FIG.

この実施例において、第1図に示す従来例と同一部分に
は同一符号を付して説明を省略する。2゜は手動により
2位置へ切換える切換弁であり、第1の位置■と第2の
位置■へ選択して切換えることができる。21a 、 
21bs 21cは七の一方端を切換弁20に接続され
た管路な示す。22は管路21aに介在するチェック弁
で切換弁2oからの圧油は通し、制御シリンダ12から
の圧油は阻止する。28は管路21bに設けられた絞り
であり、ここを辿る圧油に対する管路抵抗は大きくなる
。なお、管路21Cには絞りは設けられておらず、管路
21Cを通る圧油に対する管路抵抗は極め【小さい。管
路21a。
In this embodiment, the same parts as those in the conventional example shown in FIG. 1 are given the same reference numerals, and their explanation will be omitted. 2° is a switching valve that can be manually switched between two positions, and can be selectively switched between the first position (■) and the second position (■). 21a,
21bs and 21c are pipe lines having one end connected to the switching valve 20. Reference numeral 22 denotes a check valve interposed in the pipe line 21a, which allows pressure oil from the switching valve 2o to pass therethrough and blocks pressure oil from the control cylinder 12. Reference numeral 28 denotes a throttle provided in the pipe line 21b, and the resistance of the pipe line against the pressure oil passing through this throttle increases. Note that the conduit 21C is not provided with a restriction, and the conduit resistance to the pressure oil passing through the conduit 21C is extremely small. Conduit 21a.

21b、 21Cの他端はいずれも制御シリンダ12の
ロッド側に接続されている。
The other ends of 21b and 21C are both connected to the rod side of the control cylinder 12.

次に、この実施例の動作を説明する。Next, the operation of this embodiment will be explained.

切換弁20は手動により位置Iへ切換えられているもの
とする。前述のように、操作レバー9を操作すると、パ
イロット用油圧ポンプ8の圧油は、パイロット切換弁1
0a又は10bを通り方向切換弁7を作動させるととも
にシャトル弁11を通って切換弁20に達する。切換弁
20にはチェック弁22と絞り28とがパラレルに接続
されている状態にあるが、絞り28の管路抵抗は大きい
ので、切換弁20に適した圧油は管路21Hのチェック
弁22を通って制御シリンダ12へ速かに供給され、ピ
ストン18を右行する。これKより燃料噴射機構2から
の燃料噴射蓋は増加してエンジンlは高速回転する。
It is assumed that the switching valve 20 has been manually switched to position I. As mentioned above, when the operating lever 9 is operated, the pressure oil of the pilot hydraulic pump 8 is transferred to the pilot switching valve 1.
0a or 10b to operate the directional switching valve 7 and pass through the shuttle valve 11 to reach the switching valve 20. A check valve 22 and a throttle 28 are connected in parallel to the switching valve 20, but since the pipe resistance of the throttle 28 is large, the pressure oil suitable for the switching valve 20 is the check valve 22 in the pipe 21H. is rapidly supplied to the control cylinder 12 through the piston 18, and moves the piston 18 to the right. From this K, the amount of fuel injected from the fuel injection mechanism 2 increases, and the engine 1 rotates at a high speed.

操作レバー9を中立位置に戻すと、パイロット切換弁1
0a、  lObともタンク5と連通した状態となる。
When the operating lever 9 is returned to the neutral position, the pilot switching valve 1
Both 0a and 1Ob are in communication with the tank 5.

制御シリンダ1zのピストン1Bはスプリング1zのば
ね力により左行しロッド側の圧油を排出するとともに燃
料噴射量を減少してエンジンlを低速回転とする。この
とき、制御シリンダ12のロッド側から排出された圧油
はチェック弁22を通ることはできないので、管路21
bの絞り28を遡り、シャトル弁11.パイロット切換
弁9を経由してタンク5へ戻る。この場合、絞り28に
よる管路抵抗が大きいので制御シリンダ12からの圧油
は急速にタンク5へ戻ることはできず、結局、制御シリ
ンダ12のビス)718の戻りは遅くなる。したがって
、燃料噴射機構2の燃料噴射量の減少に時間な債し、降
下時間を長くすることとなる。
The piston 1B of the control cylinder 1z moves to the left by the spring force of the spring 1z, discharging the pressure oil on the rod side, and reducing the fuel injection amount to make the engine 1 rotate at a low speed. At this time, the pressure oil discharged from the rod side of the control cylinder 12 cannot pass through the check valve 22, so the pipe line 21
Going back through the throttle 28 of b, the shuttle valve 11. It returns to the tank 5 via the pilot switching valve 9. In this case, the pressure oil from the control cylinder 12 cannot quickly return to the tank 5 because the pipe resistance due to the throttle 28 is large, and as a result, the return of the screw 718 of the control cylinder 12 becomes slow. Therefore, it takes time to reduce the amount of fuel injected by the fuel injection mechanism 2, and the descent time becomes longer.

切換弁20が手動で位置■へ切換えられていると、切換
弁20には管路ZICのみが接続された状態となる。し
たがって、この場合は第1図に示す従来例のものと同じ
状態となり、操作レバー18を中立位置に戻すと制御シ
リンダ12のロッド関の圧油は急速比タンク5へ戻され
、ピストン18も急速に左行して燃料噴射量を直ちに減
少させ、降下時間は短かくなる。
When the switching valve 20 is manually switched to position (2), only the pipe ZIC is connected to the switching valve 20. Therefore, in this case, the condition is the same as that of the conventional example shown in FIG. The fuel injection amount is immediately reduced by moving to the left, and the descent time is shortened.

このように、切換弁20を位置Iへ切換えることにより
長い降下時間を、又、切換弁20を位置■へ切換えるこ
とにより短い降下時間を得ることができる。
In this way, by switching the switching valve 20 to position I, a long descending time can be obtained, and by switching the switching valve 20 to position II, a short descending time can be obtained.

なお、この実施例においては、切換弁20を2位置に切
換えて2つの降下時間を選択できるようにしたが、絞り
の度合の異なる管路を用意し、又、それに応じた切換弁
を用いることにより、8つ又はそれ以上の降下時間を選
択して使用することができる。
Note that in this embodiment, the switching valve 20 is switched to two positions so that two falling times can be selected, but it is also possible to prepare pipes with different degrees of restriction and use switching valves accordingly. Accordingly, eight or more descent times can be selected and used.

以上述べたように、本発明では、エンジンを高速回転か
ら低速回転へ移行させるときの油圧装置の管路の管路抵
抗を選択して切換えることができるようにしたので、作
業状態に応じて省エネルギー効果又は良好な作業性を得
ることができる。
As described above, in the present invention, it is possible to select and switch the line resistance of the hydraulic system line when the engine shifts from high-speed rotation to low-speed rotation, so energy can be saved depending on the working condition. effect or good workability can be obtained.

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

g1図は従来のエンジン制御装置の油圧回路の系統図、
第2図は本発明に係る一実施・例のエンジン制御装置の
油圧回路の系統図である。 l・・・・・・エンジン、2・・・・・・燃料噴射機構
、8・・・・・・アクチェエータ、9・・・・・・操゛
作レバー、lOa、  10b・・・・・・パイロット
切換弁、11・・曲シャトル弁、1z・・・・・・制御
シリンダ、18・・朋ピストン、■4・・・・・・ロッ
ト、15・・・・・・スプリング、16・・・・・・連
結管、20・・・・・・切換弁、21a、21b121
c・・曲管路、22−ニーチェック弁、2B・・・・・
・絞り。 才1関 ′;i2図
Figure g1 is a system diagram of the hydraulic circuit of a conventional engine control device.
FIG. 2 is a system diagram of a hydraulic circuit of an engine control device according to an embodiment/example of the present invention. l...Engine, 2...Fuel injection mechanism, 8...Actuator, 9...Control lever, lOa, 10b... Pilot switching valve, 11... Curved shuttle valve, 1z... Control cylinder, 18... Piston, ■4... Lot, 15... Spring, 16... ...Connecting pipe, 20...Switching valve, 21a, 21b121
c...Curved pipe line, 22-knee check valve, 2B...
・Aperture. Sai1kan';i2 figure

Claims (1)

【特許請求の範囲】[Claims] 油出ポンプを連結したエンジンと、このエンジンの燃料
噴射機構と、この燃料噴射機構を制御する油圧装置と、
前記油圧ポンプに接続されたアクチュエータを操作する
操作装置と、前記油圧装置に接続され前記操作装置の操
作に応じて圧油を導<’を路とを備えたエンジン制御装
置において、前記エンジンを高速回転から低速回転へ移
行させるときの前記管路の管路抵抗を選択的に切換える
手段を設けたことを軸敵とするエンジン制御装置。
An engine connected to an oil pump, a fuel injection mechanism for this engine, and a hydraulic system that controls this fuel injection mechanism;
An engine control device comprising: an operating device for operating an actuator connected to the hydraulic pump; and a path connected to the hydraulic device to guide pressure oil in response to operation of the operating device, the engine control device operating the engine at high speed. An engine control device characterized by providing a means for selectively switching the resistance of the pipe when the rotation is shifted from rotation to low speed rotation.
JP1439682A 1982-02-02 1982-02-02 Engine controller Pending JPS58133451A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1439682A JPS58133451A (en) 1982-02-02 1982-02-02 Engine controller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1439682A JPS58133451A (en) 1982-02-02 1982-02-02 Engine controller

Publications (1)

Publication Number Publication Date
JPS58133451A true JPS58133451A (en) 1983-08-09

Family

ID=11859884

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1439682A Pending JPS58133451A (en) 1982-02-02 1982-02-02 Engine controller

Country Status (1)

Country Link
JP (1) JPS58133451A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61132733A (en) * 1984-11-30 1986-06-20 Hitachi Constr Mach Co Ltd Control equipment of motor for driving hydraulic system
JPS6354839U (en) * 1986-09-29 1988-04-13
US4776164A (en) * 1986-02-21 1988-10-11 Fiatallis Europe S.P.A. Hydraulic-electric control circuit for earth-moving machine main engine
US4989567A (en) * 1989-07-19 1991-02-05 Kabushiki Kaisha Kobe Seiko Sho Engine speed controlling system in construction machine
FR2743114A1 (en) * 1995-12-30 1997-07-04 Daewoo Heavy Ind Co Ltd Hydraulic drive and actuation circuit for dumper truck

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61132733A (en) * 1984-11-30 1986-06-20 Hitachi Constr Mach Co Ltd Control equipment of motor for driving hydraulic system
US4776164A (en) * 1986-02-21 1988-10-11 Fiatallis Europe S.P.A. Hydraulic-electric control circuit for earth-moving machine main engine
JPS6354839U (en) * 1986-09-29 1988-04-13
JPH0415962Y2 (en) * 1986-09-29 1992-04-09
US4989567A (en) * 1989-07-19 1991-02-05 Kabushiki Kaisha Kobe Seiko Sho Engine speed controlling system in construction machine
FR2743114A1 (en) * 1995-12-30 1997-07-04 Daewoo Heavy Ind Co Ltd Hydraulic drive and actuation circuit for dumper truck

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