JPS6346311B2 - - Google Patents
Info
- Publication number
- JPS6346311B2 JPS6346311B2 JP3505784A JP3505784A JPS6346311B2 JP S6346311 B2 JPS6346311 B2 JP S6346311B2 JP 3505784 A JP3505784 A JP 3505784A JP 3505784 A JP3505784 A JP 3505784A JP S6346311 B2 JPS6346311 B2 JP S6346311B2
- Authority
- JP
- Japan
- Prior art keywords
- pilot
- oil
- oil passage
- spool
- switching valve
- 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
Links
- 230000007935 neutral effect Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000006386 neutralization reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
- F15B13/042—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
- F15B13/0422—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with manually-operated pilot valves, e.g. joysticks
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluid-Driven Valves (AREA)
- Multiple-Way Valves (AREA)
- Fluid-Pressure Circuits (AREA)
Description
【発明の詳細な説明】
この発明はリモートコントロール弁で制御され
るパイロツト切換弁のパイロツト部の構造に関す
る。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the structure of a pilot section of a pilot switching valve controlled by a remote control valve.
パイロツト切換弁で、リモートコントロール弁
によつて制御されるものでは、両者の間をパイロ
ツト油路で連結し、リモートコントロール弁から
のパイロツト油がパイロツト切換弁の左右のパイ
ロツト室に作用し、スプールを作動してこれを切
換える如くしている。リモートコントロール弁は
通常パイロツト切換弁を遠い位置から制御すると
いう状態にあるため、そのパイロツト油路も長く
なり、また、単にスプールを作動するだけでそれ
程油量を必要としないため、パイロツト油路の配
管の径はそれ程大きくしてない。このようにパイ
ロツト油路の配管が長く、かつ、径が小さいた
め、スプールの作動がそれ程早くないとはいえ、
厳密に言へばスプールの作動時にかなりの油の流
動抵抗があり、それによつてタイムラグが生じて
いる。特に寒冷時は油の粘度が上昇し、流動抵抗
が増加するので、細くて長いパイロツト油路の抵
抗によるタイムラグが生じやすくなるばかりでな
く、このパイロツト油路に封じ込められたエアの
除去の機会も少ないのでなおさらタイムラグが生
ずるという悪い条件がおきやすい。 For pilot switching valves that are controlled by a remote control valve, the two are connected by a pilot oil passage, and the pilot oil from the remote control valve acts on the left and right pilot chambers of the pilot switching valve, causing the spool to flow. It operates to switch this. Since a remote control valve normally controls a pilot switching valve from a remote location, its pilot oil path is also long, and since it does not require a large amount of oil just to operate the spool, the pilot oil path is shortened. The diameter of the pipe is not that large. Because the pilot oil passage piping is long and small in diameter, the spool does not operate as quickly, but
Strictly speaking, there is considerable oil flow resistance when the spool is activated, which causes a time lag. Particularly in cold weather, the viscosity of the oil increases and the flow resistance increases, which not only tends to cause time lags due to the resistance of the long and thin pilot oil passage, but also creates an opportunity to remove the air trapped in this pilot oil passage. Since it is small, it is easy to create a bad condition where a time lag occurs.
この発明は上記の問題を解決し、パイロツト操
作時にタイムラグが生じない装置を提供すること
を目的とするものである。 The object of the present invention is to solve the above problems and provide an apparatus that does not cause time lag during pilot operations.
この発明の構成は、リモートコントロール弁か
らパイロツト油路を通じたパイロツト切換弁にお
いて、該パイロツト切換弁のスプールに、一方の
パイロツト油室にパイロツト圧が作用して該スプ
ールが移動すると他方のパイロツト油室と弁本体
内の戻り油路とを連通せしめる如き流通路を設け
たことにある。 The structure of the present invention is such that in a pilot switching valve through which a pilot oil passage passes from a remote control valve, when pilot pressure acts on the spool of the pilot switching valve in one pilot oil chamber and the spool moves, the other pilot oil chamber A flow path is provided that communicates the return oil path in the valve body with the return oil path in the valve body.
パイロツト油室がパイロツト油路を通じてタン
ク側に通じたとき、同時に弁本体内の戻り側油路
に通じるから、パイロツト油路を通る戻り油の抵
抗を軽減することができ、タイムラグの発生を予
防できる。また、油の流通が可能であるからパイ
ロツト油路内のエアが外部へ抜けやすくなる。 When the pilot oil chamber communicates with the tank side through the pilot oil passage, it also communicates with the return side oil passage inside the valve body, so the resistance of the return oil passing through the pilot oil passage can be reduced and the occurrence of time lag can be prevented. . Furthermore, since oil can flow, air in the pilot oil passage can easily escape to the outside.
以下、本発明の実施例を図面によりて詳細に説
明する。 Embodiments of the present invention will be described in detail below with reference to the drawings.
1,2,3はいずれもパイロツト切換弁で、こ
れらのパイロツト切換弁1,2,3には油圧ポン
プ4から油路5,6,7がそれぞれ並列に通じて
おり、これらの切換弁1,2,3はそれぞれ戻り
油路8,9,10でタンク11に通じている。な
お、12は中立時の戻り油路であり、13はアク
チユエータであるが、該アクチユエータ13には
パイロツト切換弁1から油路14,15が通じて
いる。16はリモートコントロール弁で、左右の
弁体17,18と、これを操作するレバー装置1
9からなり、弁体17,18には補助油圧ポンプ
20から油路21が通じている。また、左方の弁
体17からパイロツト切換弁1の右方のパイロツ
ト油室22にはパイロツト油路23が通じてお
り、右方の弁体18からパイロツト切換弁1の左
方のパイロツト油室24にはパイロツト油路25
が通じている。なお、26はリリーフ弁である。 Reference numerals 1, 2, and 3 are all pilot switching valves, and oil passages 5, 6, and 7 from a hydraulic pump 4 are connected in parallel to these pilot switching valves 1, 2, and 3, respectively. 2 and 3 communicate with the tank 11 through return oil passages 8, 9, and 10, respectively. In addition, 12 is a return oil passage at the time of neutrality, and 13 is an actuator, and oil passages 14 and 15 communicate with the pilot switching valve 1 to the actuator 13. Reference numeral 16 denotes a remote control valve, which includes left and right valve bodies 17 and 18, and a lever device 1 for operating the same.
9, and an oil passage 21 from an auxiliary hydraulic pump 20 communicates with the valve bodies 17 and 18. Further, a pilot oil passage 23 communicates from the left valve element 17 to the right pilot oil chamber 22 of the pilot switching valve 1, and from the right valve element 18 to the left pilot oil chamber of the pilot switching valve 1. 24 has a pilot oil passage 25
is understood. Note that 26 is a relief valve.
第2図はパイロツト切換弁1,2,3の内部を
示し、第3図、第4図、第5図、第6図、第7図
は第2図におけるA矢視部の作動、実施例を示す
拡大図であるが、27はスプールで、その両側端
は左右のパイロツト油室24,22に臨んでお
り、右端部はバネ受28を介してバネ29で、左
端部はバネ受30を介してバネ31で支持されて
いる。スプール27には中央部に該スプール27
が中立位置にあるときのみその戻り油路12を開
通する2個の切込み32,33が左右対象にあ
り、その外方にはポンプ4に通じた油路5をアク
チユエータ13に通じた油路14、あるいは、油
路15に、また、同時にタンク11に通じた油路
8に通ぜしむる切込み34,35が左右対象にあ
る。更にその外方には戻り油路8と他の切換弁2
の戻り油路9を開通する切込み36,37を左右
対象に設けているが、該切込み36,37は単に
戻り油路8,9を開通するのみならず、スプール
27が中立以外にあるときは油路8をパイロツト
油室22、あるいは、24に通ぜしめる如く形成
しており、スプール27が右行したときはパイロ
ツト油室22が切込み36を介して油路8に通
じ、左行したときはパイロツト油室24が切込み
37を介して油路8に通ずる。 Fig. 2 shows the inside of the pilot switching valves 1, 2, and 3, and Figs. 3, 4, 5, 6, and 7 show the operation and embodiments of the part shown by arrow A in Fig. 2. In this enlarged view, 27 is a spool, whose both ends face the left and right pilot oil chambers 24, 22, the right end is connected to the spring 29 via the spring receiver 28, and the left end is connected to the spring receiver 30. It is supported by a spring 31 via. The spool 27 has a central part of the spool 27.
There are two symmetrical notches 32 and 33 that open the return oil passage 12 only when the is in the neutral position, and an oil passage 14 that connects the oil passage 5 that communicates with the pump 4 to the actuator 13 is located on the outside thereof. Alternatively, there are symmetrical cuts 34 and 35 in the oil passage 15 and at the same time, the oil passage 8 communicating with the tank 11. Furthermore, a return oil passage 8 and another switching valve 2 are arranged outwardly.
Notches 36 and 37 are provided symmetrically on the left and right to open the return oil passages 9, but the notches 36 and 37 not only open the return oil passages 8 and 9, but also open the return oil passages 8 and 9 when the spool 27 is in a position other than neutral. The oil passage 8 is formed so as to communicate with the pilot oil chamber 22 or 24, and when the spool 27 moves to the right, the pilot oil chamber 22 communicates with the oil passage 8 through the notch 36, and when the spool 27 moves to the left, it communicates with the oil passage 8. The pilot oil chamber 24 communicates with the oil passage 8 via the notch 37.
本発明は上記の如く構成しており、アクチユエ
ータ13を作動せず、レバー装置19を中立にし
ている場合は、補助油圧ポンプ20の油はリリー
フ弁26からタンク11に帰り、パイロツト油路
23,25を通つてパイロツト油室22,24は
タンク11に通じているから、スプール27はバ
ネ29,31で中立位置に保持され、中立時の戻
り油路12のみ切込み32,33によつて開通さ
れており、油圧ポンプ4からの圧油は中立時の戻
り油路12を通つてタンク11に帰る。 The present invention is constructed as described above, and when the actuator 13 is not operated and the lever device 19 is in the neutral position, the oil in the auxiliary hydraulic pump 20 returns to the tank 11 from the relief valve 26, and the oil in the pilot oil path 23, Since the pilot oil chambers 22 and 24 communicate with the tank 11 through 25, the spool 27 is held in the neutral position by the springs 29 and 31, and only the return oil passage 12 in the neutral state is opened by the notches 32 and 33. The pressure oil from the hydraulic pump 4 returns to the tank 11 through the return oil path 12 at the time of neutralization.
次にアクチユエータ13を作動する場合はレバ
ー装置19を操作する。例えば右側(矢印方向)
に倒した場合は、補助油圧ポンプ20からの油が
弁体18、パイロツト油路25を通つてパイロツ
ト油室24に流入し、スプール27をバネ29に
抗して右方に押す。切込み36によつてパイロツ
ト油室22が戻り油路8に通ずる。スプール27
の突入によつて押されたパイロツト油室22の油
はパイロツト油路23から弁体17を通つてタン
ク11に流れるのみならず、一部は切込み36か
ら油路8を通つてタンク11に流れる。パイロツ
ト油路23も、切換弁1の戻り油路8も共にタン
ク11に通じておりパイロツト油室22の油圧は
殆んどなくなり、スプール27はバネ29に抗し
て移動することになるが、その過程において一方
は細くて長いパイロツト油路23から、更に弁体
17を通つてタンク11に通じ、その内部抵抗が
大きいが、他方は切換弁1の戻り油路8を通つて
タンク11に通じその流路が大きく、かつ、短い
のでその内部抵抗が少なく、切込み36を設けて
パイロツト室22の油を油路8を通つてタンク1
1に流す効果は大きい。特に、スプール27が圧
油によつて動く場合の作動速度が早いことと、ス
プール27の断面積がパイロツト油路23の断面
積に比較して大きいことから、パイロツト油室2
2からパイロツト油路23へ押出されるときの抵
抗も大きくなるが、スプール27に切込み36を
設けてパイロツト油室22の油の一部を油路8に
逃がすことは、単に戻り油路を別個に設けたとい
うばかりでなく、パイロツト油路23より効果の
ある戻り油路を増設したことになるのでその意義
は大きい。 Next, when actuating the actuator 13, the lever device 19 is operated. For example, the right side (arrow direction)
When it is tilted down, oil from the auxiliary hydraulic pump 20 flows into the pilot oil chamber 24 through the valve body 18 and the pilot oil passage 25, pushing the spool 27 to the right against the spring 29. The pilot oil chamber 22 communicates with the return oil passage 8 through the notch 36 . Spool 27
The oil in the pilot oil chamber 22 pushed by the entry of the oil not only flows from the pilot oil passage 23 through the valve body 17 to the tank 11, but also partially flows from the notch 36 through the oil passage 8 to the tank 11. . Both the pilot oil passage 23 and the return oil passage 8 of the switching valve 1 communicate with the tank 11, so the oil pressure in the pilot oil chamber 22 is almost gone, and the spool 27 moves against the spring 29. In this process, one side is connected to the tank 11 through the thin and long pilot oil passage 23 and further through the valve body 17, which has a large internal resistance, and the other side is connected to the tank 11 through the return oil passage 8 of the switching valve 1. Since the flow path is large and short, its internal resistance is small, and a notch 36 is provided to allow oil in the pilot chamber 22 to flow through the oil path 8 into the tank 1.
1 has a great effect. In particular, when the spool 27 is moved by pressure oil, the operating speed is fast and the cross-sectional area of the spool 27 is larger than the cross-sectional area of the pilot oil passage 23.
However, providing a notch 36 in the spool 27 to release some of the oil in the pilot oil chamber 22 to the oil path 8 simply creates a separate return oil path. This is significant because it not only provides a return oil passage that is more effective than the pilot oil passage 23.
スプール27に設けた切込み36は、スプール
がパイロツト油室22側に押されたときのみ該油
室22を油路8に通ぜしめればよいから、第3図
のような切込み36であるばかりでなく、第6図
に示すようなスプール27がパイロツト油室22
側に押されたときのみ該油室22と油路8を通ぜ
しめる如き油路38、あるいは、第7図に示すよ
うな軸方向の油溝39を設けることによつても本
発明の目的は達成することができる。 The notch 36 provided in the spool 27 is the same as the notch 36 shown in FIG. 3 because it is only necessary to allow the oil chamber 22 to pass through the oil passage 8 when the spool is pushed toward the pilot oil chamber 22. Instead, the spool 27 as shown in Fig. 6 is connected to the pilot oil chamber 22.
The object of the present invention can also be achieved by providing an oil passage 38 that allows the oil chamber 22 and oil passage 8 to communicate only when pushed to the side, or an axial oil groove 39 as shown in FIG. can be achieved.
以上述べたように、本発明はリモートコントロ
ール弁とパイロツト油路で結ばれているパイロツ
ト切換弁のスプールに、該スプールがパイロツト
圧で押されたとき、反対側のパイロツト油室と切
換弁のタンクポートとを連通する流通路を設けた
から、パイロツト油室からの油の流出が早くな
り、寒冷時にパイロツト油路内の油の抵抗が増加
する場合でもタイムラグが生じない。また、パイ
ロツト油室が2個所で外部に通じるので、油の流
通がよくなり、パイロツト油路内にエアが外部に
抜けやすくなり、エアの内在することによるタイ
ムラグが生ずることも防止できる。 As described above, the present invention provides a system in which when the spool of a pilot switching valve connected to a remote control valve by a pilot oil passage is pushed by pilot pressure, the pilot oil chamber on the opposite side and the tank of the switching valve Since the flow passage communicating with the port is provided, the oil flows out from the pilot oil chamber quickly, and there is no time lag even when the oil resistance in the pilot oil passage increases in cold weather. In addition, since the pilot oil chamber communicates with the outside at two locations, oil circulation is improved, air is easily released from the pilot oil passage to the outside, and time lags due to the presence of air can be prevented.
図面はいずれも本発明の実施例であるが、第1
図は油圧回路図、第2図は横断面図、第3図は第
2図のA部の拡大図、第4図、第5図はいずれも
第3図の作動時の状況を示す図、第6図、第7図
は本発明の他の実施例を示す図である。
1……パイロツト切換弁、8……油路、16…
…リモートコントロール弁、22……パイロツト
油室、23……パイロツト油路、24……パイロ
ツト油室、25……パイロツト油路、27……ス
プール、36……切込み、37……切込み。
The drawings are all embodiments of the present invention, but the first
The figure is a hydraulic circuit diagram, Figure 2 is a cross-sectional view, Figure 3 is an enlarged view of section A in Figure 2, Figures 4 and 5 are diagrams showing the operating situation in Figure 3, FIGS. 6 and 7 are diagrams showing other embodiments of the present invention. 1...Pilot switching valve, 8...Oil passage, 16...
...remote control valve, 22...pilot oil chamber, 23...pilot oil passage, 24...pilot oil chamber, 25...pilot oil passage, 27...spool, 36...notch, 37...notch.
Claims (1)
連結されたパイロツト切換弁において、該パイロ
ツト切換弁のスプールの両側端より若干内方によ
つた位置に、上記パイロツト切換弁の一方のパイ
ロツト油室にパイロツト圧が作用して該スプール
が若干移動すると他方のパイロツト油室がパイロ
ツト切換弁の戻り油路と連通する如き流通路を設
けたことを特徴とする切換弁。1. In a pilot switching valve connected to a remote control valve by a pilot oil passage, pilot pressure is applied to one pilot oil chamber of the pilot switching valve at a position slightly inward from both ends of the spool of the pilot switching valve. A switching valve characterized in that a flow passage is provided such that when the spool is moved slightly by operation, the other pilot oil chamber communicates with a return oil passage of the pilot switching valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3505784A JPS60179578A (en) | 1984-02-24 | 1984-02-24 | Selector valve |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3505784A JPS60179578A (en) | 1984-02-24 | 1984-02-24 | Selector valve |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60179578A JPS60179578A (en) | 1985-09-13 |
| JPS6346311B2 true JPS6346311B2 (en) | 1988-09-14 |
Family
ID=12431404
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3505784A Granted JPS60179578A (en) | 1984-02-24 | 1984-02-24 | Selector valve |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60179578A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4900671B2 (en) * | 2006-03-14 | 2012-03-21 | キャタピラー エス エー アール エル | Electronic control valve calibration device |
| JP2010127373A (en) * | 2008-11-27 | 2010-06-10 | Mitsubishi Heavy Ind Ltd | Hydraulic pilot type proportional solenoid control valve |
| JP5916450B2 (en) | 2012-03-15 | 2016-05-11 | Kyb株式会社 | Switching valve |
-
1984
- 1984-02-24 JP JP3505784A patent/JPS60179578A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60179578A (en) | 1985-09-13 |
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