JPH0350146B2 - - Google Patents

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Publication number
JPH0350146B2
JPH0350146B2 JP13861588A JP13861588A JPH0350146B2 JP H0350146 B2 JPH0350146 B2 JP H0350146B2 JP 13861588 A JP13861588 A JP 13861588A JP 13861588 A JP13861588 A JP 13861588A JP H0350146 B2 JPH0350146 B2 JP H0350146B2
Authority
JP
Japan
Prior art keywords
pilot valve
hydraulic
valve
servo
oil passage
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
JP13861588A
Other languages
Japanese (ja)
Other versions
JPS6487962A (en
Inventor
Torao Hatsutori
Noryuki Takahashi
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor 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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP13861588A priority Critical patent/JPS6487962A/en
Publication of JPS6487962A publication Critical patent/JPS6487962A/en
Publication of JPH0350146B2 publication Critical patent/JPH0350146B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】 本発明は油圧式無段変速機における直結制御弁
駆動用油圧サーボモータ、特に油圧式無段変速機
の油圧モータと油圧ポンプ間の直結制御を行うた
めの直結制御弁を前端に連設したサーボピストン
をサーボシリンダのシリンダ孔に摺動自在に嵌合
し、そのサーボシリンダの後端壁を摺動自在に貫
通し外周には油路切換溝が形成されるパイロツト
弁を、前記サーボピストンの、環状油路とランド
を内周に有する盲孔状の弁孔に摺動自在に嵌合し
た形式の油圧サーボモータに関する。
Detailed Description of the Invention The present invention relates to a hydraulic servo motor for driving a directly coupled control valve in a hydraulic continuously variable transmission, and particularly to a directly coupled control valve for directly controlling a hydraulic motor and a hydraulic pump in a hydraulic continuously variable transmission. A pilot valve in which a servo piston with a front end connected to the piston is slidably fitted into a cylinder hole of a servo cylinder, the rear end wall of the servo cylinder is slidably penetrated, and an oil passage switching groove is formed on the outer periphery. The present invention relates to a hydraulic servo motor which is slidably fitted into a blind valve hole of the servo piston having an annular oil passage and a land on the inner periphery.

かかるサーボモータにおいて、パイロツト弁が
サーボピストンに対して過度に後退すなわちオー
バシフトすると、油路切換溝による的確な油路切
換作用が行われなくなるという問題がある。
In such a servo motor, if the pilot valve moves backward or overshifts excessively with respect to the servo piston, there is a problem in that the oil passage switching groove does not accurately switch the oil passage.

またサーボモータにおいて、パイロツト弁の油
路切換溝を環状溝とすると、パイロツト弁の操作
時に、該弁の僅かな傾きにより上記環状溝の端縁
が弁孔の環状油路の端縁に引掛けてパイロツト弁
の円滑な摺動が妨げられ、サーボピストンの油圧
駆動に故障を生じる原因となる。
Furthermore, in a servo motor, if the pilot valve's oil passage switching groove is an annular groove, when the pilot valve is operated, the edge of the annular groove will catch on the edge of the annular oil passage of the valve hole due to a slight inclination of the valve. This prevents smooth sliding of the pilot valve and causes a failure in the hydraulic drive of the servo piston.

本発明は、上記に鑑み提案されたもので、直結
制御弁に邪魔されずにサーボピストン内に無理な
く配置可能であると共に組付容易な共通のストツ
パ機構を、パイロツト弁のサーボピストンに対す
る後退限規制手段と、サーボシリンダからの抜け
止め手段とに兼用できるようにし、しかもパイロ
ツト弁の弁孔に対する倒れや、油路切換溝及び環
状油路の端縁相互の引掛かりを効果的に防止しパ
イロツト弁を常に円滑に摺動させ得るようにして
前記問題を解決した構造簡単な、油圧式無段変速
機における直結制御弁駆動用油圧サーボモータを
提供することを目的とする。
The present invention has been proposed in view of the above, and uses a common stopper mechanism that can be easily disposed within the servo piston without being obstructed by the direct control valve, and is easy to assemble. It can be used both as a regulating means and as a means for preventing the pilot valve from coming off from the servo cylinder, and also effectively prevents the pilot valve from falling against the valve hole and from getting caught between the edges of the oil passage switching groove and the annular oil passage. It is an object of the present invention to provide a hydraulic servo motor for driving a directly coupled control valve in a hydraulic continuously variable transmission, which has a simple structure and solves the above problem by allowing the valve to always slide smoothly.

そしてこの目的を達成するために本発明は、油
圧式無段変速機の油圧モータと油圧ポンプ間の直
結制御を行うための直結制御弁を前端に連設した
サーボピストンをサーボシリンダのシリンダ孔に
摺動自在に嵌合し、そのサーボシリンダの後端壁
を摺動自在に貫通し外周には油路切換溝が形成さ
れるパイロツト弁を、前記サーボピストンの、環
状油路とランドを内周に有する盲孔状の弁孔に摺
動自在に嵌合した、油圧式無段変速機における直
結制御弁駆動用油圧サーボモータにおいて、前記
サーボピストンの後端面には、内端面に前記弁孔
を開口させ且つ内周面にストツパリングを係止し
た凹部を形成し、前記パイロツト弁のサーボピス
トンに対する後退限を規制すべく前記凹部内で前
記ストツパリングに係合し得るストツパピンを前
記パイロツト弁の外周に一体的に突設し、さらに
前記油路切換溝を、パイロツト弁外周面に設けた
円周方向に並ぶ複数の面取り部より構成すると共
に、それら面取り部の間に、前記ランドに接触し
て該パイロツト弁の傾きを防止する複数の案内ラ
ンドを該パイロツト弁の円周方向に略等間隔をお
いて設けたことを特徴とする。
In order to achieve this object, the present invention provides a servo piston with a direct connection control valve connected to the front end for direct connection control between the hydraulic motor and the hydraulic pump of a hydraulic continuously variable transmission, in the cylinder hole of a servo cylinder. A pilot valve that is slidably fitted and slidably passes through the rear end wall of the servo cylinder and has an oil passage switching groove formed on the outer periphery is connected to the annular oil passage and land of the servo piston on the inner periphery. In a hydraulic servo motor for driving a directly coupled control valve in a hydraulic continuously variable transmission, the servo piston is slidably fitted into a blind valve hole in the servo piston, and the rear end surface of the servo piston has the valve hole in the inner end surface. A recess is formed that is open and locks a stopper ring on the inner circumferential surface, and a stopper pin that can engage with the stopper ring within the recess is integrated on the outer periphery of the pilot valve in order to limit the retraction limit of the pilot valve with respect to the servo piston. Further, the oil passage switching groove is formed of a plurality of chamfered portions arranged in the circumferential direction provided on the outer peripheral surface of the pilot valve, and between the chamfered portions, the oil passage switching groove is provided in contact with the land and the pilot valve is The pilot valve is characterized in that a plurality of guide lands for preventing the valve from tilting are provided at approximately equal intervals in the circumferential direction of the pilot valve.

以下、図面により本発明の一実施例について説
明すると、第1図において油圧サーボモータS
は、機枠1に固定されたサーボシリンダ2と、そ
のサーボシリンダ2のシリンダ孔3に摺動自在に
嵌合したサーボピストン4と、サーボシリンダ2
の後端壁2aの貫通孔hに中間部が摺動自在に嵌
合され且つサーボピストン4の弁孔5に先部外周
が摺動自在に嵌合されたパイロツト弁6とより構
成される。サーボシリンダ2の前部には油圧源に
連なる高圧油室8が形成され、該室8にはサーボ
ピストン4前端のピストンロツド7がその前端を
常に臨ませている。
Hereinafter, one embodiment of the present invention will be explained with reference to the drawings. In Fig. 1, a hydraulic servo motor S
, a servo cylinder 2 fixed to a machine frame 1, a servo piston 4 slidably fitted into a cylinder hole 3 of the servo cylinder 2, and a servo cylinder 2.
The pilot valve 6 is comprised of a pilot valve 6 whose intermediate portion is slidably fitted into the through hole h of the rear end wall 2a and whose tip outer periphery is slidably fitted into the valve hole 5 of the servo piston 4. A high-pressure oil chamber 8 connected to a hydraulic pressure source is formed at the front of the servo cylinder 2, and a piston rod 7 at the front end of the servo piston 4 always faces the front end of the piston rod 7 into the chamber 8.

シリンダ孔3には、サーボピストン4によりピ
ストンロツド7を囲繞する前部油室9と、パイロ
ツト弁6を囲繞する後部油室10とが画成され、
その後部油室10はサーボピストン4を軸方向に
貫通する油孔11を介して高圧油室8と常時連通
する。
The cylinder hole 3 is defined by a front oil chamber 9 surrounding the piston rod 7 by the servo piston 4, and a rear oil chamber 10 surrounding the pilot valve 6.
The rear oil chamber 10 is always in communication with the high pressure oil chamber 8 via an oil hole 11 passing through the servo piston 4 in the axial direction.

サーボピストン4の弁孔は前端が閉じられて盲
孔状に形成されており、その前端から後端に向つ
て環状油路12、ランド13、環状油路14およ
びランド15がその内周に順次形成され、環状油
路12はパイロツト弁6を軸方向に貫通する油孔
16を介して図示しない油溜と常時連通し、また
環状油路14は半径方向の油孔17を介して前部
油室9と常時連通する。
The valve hole of the servo piston 4 is formed into a blind hole with the front end closed, and an annular oil passage 12, a land 13, an annular oil passage 14, and a land 15 are sequentially arranged on the inner circumference from the front end to the rear end. The annular oil passage 12 is in continuous communication with an oil reservoir (not shown) through an oil hole 16 passing through the pilot valve 6 in the axial direction, and the annular oil passage 14 is connected to a front oil reservoir through an oil hole 17 extending in the radial direction. Constant communication with room 9.

一方、パイロツト弁6は、その前後摺動により
環状油路14を他方の環状油路12と後部油室1
0とに選択的に連通させる油路切換溝18の先部
外周に有し、その油路切換溝18は、第2および
第3図に明示するようにパイロツト弁6の外周円
筒面の部分的切除により形成した円周方向に並ぶ
複数個、図示例では3個の面取り部19,19,
19より構成され、そしてこれら面取り部19,
19,19の各間には、それらの前後部の外周円
筒面と同一面の複数の案内ランド20,20,2
0をパイロツト弁6円周方向に略等間隔をおいて
残存させる。尚、各案内ランド20には、第2図
に鎖線で示すように相隣る面取り部19,19間
を連通する細溝21を形成することがある。
On the other hand, the pilot valve 6 moves the annular oil passage 14 between the other annular oil passage 12 and the rear oil chamber 1 by sliding back and forth.
The oil passage switching groove 18 is provided on the outer periphery of the tip of the oil passage switching groove 18 that selectively communicates with the pilot valve 6, and as shown in FIGS. A plurality of chamfered portions 19, 19, arranged in the circumferential direction, three in the illustrated example, formed by cutting.
19, and these chamfered portions 19,
19, 19, a plurality of guide lands 20, 20, 2 are provided on the same plane as the outer peripheral cylindrical surface of the front and rear parts.
0 remain at approximately equal intervals in the circumferential direction of the pilot valve 6. In addition, each guide land 20 may be formed with a narrow groove 21 that communicates between the adjacent chamfered portions 19, as shown by chain lines in FIG.

サーボピストン4の後端面には、内端面に前記
弁孔5を開口させ且つ内周面にサークリツプより
なるストツパリング22を係止した凹部4aが形
成されており、前記パイロツト弁6のサーボピス
トン4に対する後退限を規制すべく前記凹部4a
内で前記ストツパリング22に係合し得るストツ
パピン23が、その両端部を前記パイロツト弁6
の外周面よりそれぞれ突出させてパイロツト弁6
に固着される。
A recess 4a is formed in the rear end surface of the servo piston 4, and the valve hole 5 is opened in the inner end surface, and a stop ring 22 made of a circlip is engaged in the inner peripheral surface of the recess 4a. The recess 4a to restrict the backward limit
A stopper pin 23 that can engage the stopper ring 22 within the pilot valve 6 has both ends thereof connected to the pilot valve 6.
The pilot valves 6 each protrude from the outer peripheral surface of the pilot valve 6.
is fixed to.

以上において各部の寸法は次式が成立するよう
に設計される。
In the above, the dimensions of each part are designed so that the following formula holds.

B<A−C 但し、A…サーボピストン4の断面積 B…ピストンロツド7の断面積 C…パイロツト弁6の断面積 次に前記サーボモータSの作動を説明すると、
先ずパイロツト弁6を前進(第1図では左動)さ
せて、その外周面により環状油路14と後部油室
10間を遮断すると共に、油路切換溝18即ち面
取り部19,19,19を介して弁孔5の両環状
油路12,14間を連通すれば、高圧油室8の圧
油は油圧11を経て後部油室10にのみ流入し、
サーボピストン4の後端面に油圧を作用させる。
而してサーボピストン4の後端受圧面積はA−C
であり、また高圧油室8に臨ませたピストンロツ
ド7の前端受圧面積はBであるから、前述の不等
式B<A−Cによりサーボピストン4はパイロツ
ト弁6と追従するように前方へ油圧駆動される。
B<A-C However, A... Cross-sectional area of the servo piston 4 B... Cross-sectional area of the piston rod 7 C... Cross-sectional area of the pilot valve 6 Next, the operation of the servo motor S will be explained.
First, the pilot valve 6 is moved forward (moved to the left in FIG. 1) to block the annular oil passage 14 and the rear oil chamber 10 with its outer peripheral surface, and to open the oil passage switching groove 18, that is, the chamfered portions 19, 19, 19. If the two annular oil passages 12 and 14 of the valve hole 5 are communicated through the valve hole 5, the pressure oil in the high pressure oil chamber 8 will flow only into the rear oil chamber 10 via the oil pressure 11.
Hydraulic pressure is applied to the rear end surface of the servo piston 4.
Therefore, the rear end pressure receiving area of the servo piston 4 is A-C
Since the front end pressure receiving area of the piston rod 7 facing the high pressure oil chamber 8 is B, the servo piston 4 is hydraulically driven forward to follow the pilot valve 6 due to the above-mentioned inequality B<A−C. Ru.

次にパイロツト弁6を後退(第1図では右動)
させて、その外周面により両環状油路12,14
間を遮断すると共に油路切換溝18を介して環状
油路14と後部油路10を連通すれば、高圧油室
8の圧油は後端油室10のみならず前部油室9に
も流入し、サーボピストン4の前後の両端面に油
圧を作用させる、そして、このときにもピストン
ロツド7の前端面は高圧油室8の油圧を受けてい
るので、結局サーボピストン4が後退方向の油圧
を受ける受圧面積はAであるのに対し、前進方向
の油圧を受ける受圧面積はA−Cとなり、当然に
A>A−Cによりサーボピストン4はパイロツト
弁6に追従するように後方へ油圧駆動される。
Next, move the pilot valve 6 back (rightward movement in Figure 1)
and both annular oil passages 12, 14 are connected by the outer peripheral surface thereof.
If the annular oil passage 14 and the rear oil passage 10 are communicated with each other via the oil passage switching groove 18, the pressure oil in the high-pressure oil chamber 8 can flow not only to the rear end oil chamber 10 but also to the front oil chamber 9. The oil flows in and applies hydraulic pressure to both the front and rear end faces of the servo piston 4. At this time, too, the front end face of the piston rod 7 receives the hydraulic pressure from the high pressure oil chamber 8, so the servo piston 4 eventually receives the hydraulic pressure in the backward direction. The pressure-receiving area that receives the hydraulic pressure in the forward direction is A, while the pressure-receiving area that receives the hydraulic pressure in the forward direction is A-C. Naturally, since A>A-C, the servo piston 4 is hydraulically driven rearward to follow the pilot valve 6. be done.

ここで注目すべきことは、パイロツト弁6の前
後操作に伴い、油路切換溝18即ち面取り部1
9,19,1が弁孔5のランド13または15を
通過するときでも、通過するランドに対しパイロ
ツト弁6の案内ランド20,20,20が接触し
ていることであり、これによつてパイロツト弁6
の何れの方向の傾きも防止することができる。
What should be noted here is that as the pilot valve 6 is operated back and forth, the oil passage switching groove 18, that is, the chamfered portion 1
Even when the guide lands 9, 19, 1 pass through the lands 13 or 15 of the valve hole 5, the guide lands 20, 20, 20 of the pilot valve 6 are in contact with the lands passing through, and thereby the pilot valve Valve 6
Tilt in either direction can be prevented.

次に前記サーボモータSと、それが組込まれる
油圧式無段変速機との関係構造について説明す
る。図示例では、サーボピストン4により、油圧
ポンプと油圧モータよりなる公知の油圧式無段変
速機のクラツチ制御と前記ポンプおよびモータの
直結制御とを行うようにしている。即ち、Dは油
圧ポンプと油圧モータ(いずれも図示せず)間に
介装される作動油分配機構であつて、分配盤24
と、前記サーボシリンダ2の前端部に支持されて
分配盤24に密着する分配環25とより構成さ
れ、分配環25の内側に形成した前記高圧油室8
において油圧ポンプの吐出行程にあるシリンダ孔
に連なる吐出ポート26と油圧モータの膨脹行程
にあるシリンダ孔に連なる高圧連絡ポート27と
が連通され、分配環25の外側に形成した低圧油
室8′において油圧ポンプの吸入行程にあるシリ
ンダ孔に連なる吸入ポート26′と油圧モータの
収縮行程にあるシリンダ孔に連なる低圧連絡ポー
ト27′とが連通され、これらの連通により油圧
ポンプおよびモータ間で作動油が循環して油圧伝
動が行われる。
Next, the relationship between the servo motor S and the hydraulic continuously variable transmission in which it is incorporated will be explained. In the illustrated example, the servo piston 4 performs clutch control of a known hydraulic continuously variable transmission comprising a hydraulic pump and a hydraulic motor, and direct control of the pump and motor. That is, D is a hydraulic oil distribution mechanism interposed between a hydraulic pump and a hydraulic motor (both not shown), and is connected to the distribution panel 24.
and a distribution ring 25 supported by the front end of the servo cylinder 2 and in close contact with the distribution plate 24, and the high pressure oil chamber 8 formed inside the distribution ring 25.
A discharge port 26 connected to a cylinder hole in the discharge stroke of the hydraulic pump and a high pressure communication port 27 connected to a cylinder hole in the expansion stroke of the hydraulic motor are communicated in a low pressure oil chamber 8' formed on the outside of the distribution ring 25. The suction port 26' connected to the cylinder hole in the suction stroke of the hydraulic pump and the low pressure communication port 27' connected to the cylinder hole in the contraction stroke of the hydraulic motor are communicated, and due to these communication, hydraulic oil is transferred between the hydraulic pump and the motor. Hydraulic power transmission is carried out in circulation.

サーボシリンダ2の側壁には、高圧油室8と低
圧油室8′間を連通する短絡ポート28,28が
ピストンロツド7の前後動に応じて開閉されるよ
うに穿設され、またピストンロツド7の先端に
は、それが短絡ポート28,28の閉塞位置を越
えて前進したとき吐出ポート26を閉塞するポペ
ツト弁よりなる直結制御弁29が付設される。
尚、吐出ポート26には図示しないフイードポン
プに連なる補給ポート30が開口し、そこに逆止
弁31が設けられている。
Short-circuit ports 28, 28 that communicate between the high-pressure oil chamber 8 and the low-pressure oil chamber 8' are bored in the side wall of the servo cylinder 2 so as to be opened and closed according to the forward and backward movement of the piston rod 7. is provided with a direct control valve 29, which is a poppet valve, which closes the discharge port 26 when it advances beyond the closed position of the short-circuit ports 28, 28.
A replenishment port 30 connected to a feed pump (not shown) opens in the discharge port 26, and a check valve 31 is provided there.

而して、ピストンロツド7が図示の後退位置に
あるときに短絡ポート28,28は開放され、し
たがつてそれらのポート28,28を通して高圧
油室8の圧油が低圧油室8′へ短絡して流れるの
で油圧モータは作動せず、これが所謂クラツチオ
フ状態である。またピストンロツド7が前進して
短絡ポート28,28を完全に閉塞すれば、高圧
油室8の圧油は高圧連絡ポート27を通して油圧
モータへ供給されそれを作動するので、これが所
謂クラツチオン状態であり、それに至るまでの短
絡ポート28,28の半開のときが半クラツチ状
態である。そしてピストンロツド7が短絡ポート
28,28の閉鎖位置を越えて更に前進すれば、
直結制御弁29が分配盤24に密着して吐出ポー
ト26を閉塞し、これにより油圧ポンプを油圧的
にロツクするので、油圧ポンプから油圧モータを
機械的に直接駆動し、即ち油圧ポンプおよびモー
タの直結状態が得られる。以上の制御がすべてパ
イロツト弁6の前後操作により行われることは言
うまでもない。
Thus, when the piston rod 7 is in the retracted position shown, the shorting ports 28, 28 are opened, and therefore, the pressure oil in the high pressure oil chamber 8 is short-circuited to the low pressure oil chamber 8' through these ports 28, 28. The hydraulic motor does not operate, and this is the so-called clutch-off state. Furthermore, when the piston rod 7 moves forward and completely closes the short-circuit ports 28, 28, the pressure oil in the high-pressure oil chamber 8 is supplied to the hydraulic motor through the high-pressure communication port 27 and operates it, so this is a so-called clutch-on state. When the short-circuit ports 28, 28 are half-opened up to this point, the clutch is in a half-clutch state. If the piston rod 7 moves further beyond the closed position of the short-circuit ports 28, 28,
The direct control valve 29 closes the distribution panel 24 and closes the discharge port 26, thereby hydraulically locking the hydraulic pump, so that the hydraulic motor can be mechanically driven directly from the hydraulic pump, that is, the hydraulic pump and motor can be driven directly. A direct connection state is obtained. It goes without saying that all of the above controls are performed by operating the pilot valve 6 back and forth.

以上のように本発明によれば、油圧式無段変速
機の油圧モータと油圧ポンプ間の直結制御を行う
ための直結制御弁を前端に連設したサーボピスト
ンをサーボシリンダのシリンダ孔に摺動自在に嵌
合し、そのサーボシリンダの後端壁を摺動自在に
貫通し外周には油路切換溝が形成されるパイロツ
ト弁を、前記サーボピストンの、環状油路とラン
ドを内周に有する盲孔状の弁孔に摺動自在に嵌合
した、油圧式無段変速機における直結制御弁駆動
用油圧サーボモータにおいて、前記サーボピスト
ンの後端面には、内端面に前記弁孔を開口させ且
つ内周面にストツパリングを係止した凹部を形成
し、前記パイロツト弁のサーボピストンに対する
後退限を規制すべく前記凹部内で前記ストツパリ
ングに係合し得るストツパピンを前記パイロツト
弁の外周に一体的に突設したので、前記ストツパ
リング及びストツパピンは、それらの協働によ
り、パイロツト弁のサーボピストンに対する後退
限を確実に規制してパイロツト弁のオーバシフト
防止に効果的である上、パイロツト弁のサーボシ
リンダからの抜け出しをも確実に防止することが
できる。その上、かかるストツパリング及びスト
ツパピンはサーボピストン後端面の前記凹部内に
設けられるから、サーボピストン前端側の前記直
結制御弁の存在とは無関係に無理なく配置するこ
とができる。しかもサーボモータの組立時には、
パイロツト弁の先部をサーボピストンの弁孔内に
嵌挿させてからストッパリングを凹部内周にセツ
トするだけでよく、従つて該ストツパリング及び
ストツパピンを前記凹部内に特設するもサーボモ
ータの組立性が低下するようなことはない。
As described above, according to the present invention, a servo piston having a direct connection control valve connected to its front end for performing direct connection control between a hydraulic motor and a hydraulic pump of a hydraulic continuously variable transmission is slid into a cylinder hole of a servo cylinder. The servo piston has an annular oil passage and a land on its inner periphery, and includes a pilot valve that is freely fitted, slidably penetrates the rear end wall of the servo cylinder, and has an oil passage switching groove formed on its outer periphery. In a hydraulic servomotor for driving a directly coupled control valve in a hydraulic continuously variable transmission, which is slidably fitted into a blind valve hole, the valve hole is opened on an inner end surface of the rear end surface of the servo piston. A recessed portion in which a stopper ring is engaged is formed on the inner peripheral surface, and a stopper pin that can engage with the stopper ring within the recessed portion is integrally formed on the outer periphery of the pilot valve in order to limit the retraction limit of the pilot valve with respect to the servo piston. Since the stopper ring and stopper pin are provided in a protruding manner, the stopper ring and the stopper pin work together to reliably restrict the retraction limit of the pilot valve with respect to the servo piston and are effective in preventing overshifting of the pilot valve. It is also possible to reliably prevent the material from slipping out. Moreover, since the stopper ring and the stopper pin are provided in the recess on the rear end surface of the servo piston, they can be easily arranged regardless of the presence of the direct-coupled control valve on the front end side of the servo piston. Moreover, when assembling the servo motor,
It is only necessary to fit the tip of the pilot valve into the valve hole of the servo piston and then set the stopper ring on the inner periphery of the recess. Therefore, although the stopper ring and stopper pin are specially installed in the recess, the ease of assembling the servo motor is improved. There is no decline in

さらに前記油路切換溝を、パイロツト弁外周面
に設けた円周方向に並ぶ複数の面取り部より構成
すると共に、それら面取り部の間に、前記ランド
に接触して該パイロツト弁の傾きを防止する複数
の案内ランドを該パイロツト弁の円周方向に略等
間隔をおいて設けたので、それら複数の案内ラン
ド部は、パイロツト弁の円周方向に分散配置され
るも、パイロツト弁の操作時には弁孔のランドと
絶えず摺接してパイロツト弁の摺動を常に的確に
案内することができ、従つてパイロツト弁の先部
及び中間部がそれぞれ摺合する弁孔及びサーボシ
リンダ後端壁の貫通孔の中心軸線相互の多少ずれ
ているような場合でも、パイロツト弁の弁凹中心
軸線に対する倒れや、油路切換溝及び環状油路の
端縁相互の引掛かりが各案内ランド部によつて効
果的に阻止されてパイロツト弁を常に円滑に摺動
させることができ、以上の結果、前述の如くパイ
ロツト弁のサーボピストンに対する後退限が確実
に規制される効果と相俟つて、サーボピストン前
端の直結制御を常に的確に油圧駆動することがで
きる。しかも前記油路切換溝は、パイロツト弁の
外周面に単純な面取り加工を施すだけて形成でき
るから、加工が容易でコストの低減及び加工精度
の向上に寄与し得る。
Furthermore, the oil passage switching groove is constituted by a plurality of chamfered portions arranged in the circumferential direction provided on the outer circumferential surface of the pilot valve, and a chamfered portion is provided between the chamfered portions and contacts the land to prevent the pilot valve from tilting. Since a plurality of guide lands are provided at approximately equal intervals in the circumferential direction of the pilot valve, the plurality of guide lands are distributed in the circumferential direction of the pilot valve, but when the pilot valve is operated, the valve does not move. The center of the through hole in the valve hole and the rear end wall of the servo cylinder is in constant sliding contact with the land of the hole and can always accurately guide the sliding movement of the pilot valve, so that the tip and middle portions of the pilot valve slide together, respectively. Even if the axes are slightly misaligned, each guide land effectively prevents the pilot valve from falling with respect to the center axis of the valve recess, and from getting caught between the edges of the oil passage switching groove and the annular oil passage. As a result, the pilot valve can always slide smoothly, and as a result, the retraction limit of the pilot valve with respect to the servo piston is reliably regulated as described above, and the direct control of the front end of the servo piston is always controlled. It can be accurately hydraulically driven. Moreover, since the oil passage switching groove can be formed by simply chamfering the outer circumferential surface of the pilot valve, machining is easy and can contribute to cost reduction and improvement of machining accuracy.

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

第1図は本発明の一実施例を示す縦断面図、第
2図はそれにおけるパイロツト弁の要部側面図、
第3図は第2図の−線断面図である。 S……油圧サーボモータ、2……サーボシリン
ダ、2a……後端壁、3……シリンダ孔、4……
サーボピストン、4a……凹部、5……弁孔、6
……パイロツト弁、12,14……環状油路、1
3,15……ランド、18……油路切換溝、19
……面取り部、20……案内ランド、22……ス
トツパリング、23……ストツパピン、29……
直結制御弁。
FIG. 1 is a longitudinal sectional view showing one embodiment of the present invention, FIG. 2 is a side view of the main part of the pilot valve therein,
FIG. 3 is a sectional view taken along the line -- in FIG. 2. S... Hydraulic servo motor, 2... Servo cylinder, 2a... Rear end wall, 3... Cylinder hole, 4...
Servo piston, 4a... recess, 5... valve hole, 6
... Pilot valve, 12, 14 ... Annular oil passage, 1
3, 15...Land, 18...Oil passage switching groove, 19
... Chamfered portion, 20 ... Guide land, 22 ... Stopper ring, 23 ... Stopper pin, 29 ...
Direct control valve.

Claims (1)

【特許請求の範囲】[Claims] 1 油圧式無段変速機の油圧モータと油圧ポンプ
間の直結制御を行うための直結制御弁29を前端
に連設したサーボピストン4をサーボシリンダ2
のシリンダ孔3に摺動自在に嵌合し、そのサーボ
シリンダ2の後端壁2aを摺動自在に貫通し外周
には油路切換溝18が形成されるパイロツト弁6
を、前記サーボピストン4の、環状油路12,1
4とランド13,15を内周に有する盲孔状の弁
孔5に摺動自在に嵌合した、油圧式無段変速機に
おける直結制御弁駆動用油圧サーボモータにおい
て、前記サーボピストン4の後端面には、内端面
に前記弁孔5を開口させ且つ内周面にストツパリ
ング22を係止した凹部4aを形成し、前記パイ
ロツト弁6のサーボピストン4に対する後退限を
規制すべく前記凹部4a内で前記ストツパリング
22に係合し得るストツパピン23を前記パイロ
ツト弁6の外周に一体的に突設し、さらに前記油
路切換溝18を、パイロツト弁6外周面に設けた
円周方向に並ぶ複数の面取り部19より構成する
と共に、それら面取り部19の間に、前記ランド
13,15に接触して該パイロツト弁6の傾きを
防止する複数の案内ランド20を該パイロツト弁
6の円周方向に略等間隔をおいて設けたことを特
徴とする、油圧式無段変速機における直結制御弁
駆動用油圧サーボモータ。
1 A servo cylinder 2 is equipped with a servo piston 4 connected to a front end thereof with a direct connection control valve 29 for direct connection control between a hydraulic motor and a hydraulic pump of a hydraulic continuously variable transmission.
A pilot valve 6 is slidably fitted into the cylinder hole 3 of the servo cylinder 2, slidably penetrates the rear end wall 2a of the servo cylinder 2, and has an oil passage switching groove 18 formed on its outer periphery.
is the annular oil passage 12, 1 of the servo piston 4.
4 and lands 13 and 15 on the inner periphery of the hydraulic servo motor for driving a control valve in a hydraulic continuously variable transmission, which is slidably fitted into a blind hole-shaped valve hole 5 having lands 13 and 15 on the inner periphery. The end face is formed with a recess 4a in which the valve hole 5 is opened on the inner end face and a stopper ring 22 is locked on the inner circumferential face. A stopper pin 23 that can be engaged with the stopper ring 22 is integrally provided on the outer periphery of the pilot valve 6, and the oil passage switching groove 18 is formed on the outer periphery of the pilot valve 6 through a plurality of circumferentially arranged stopper pins 23. A plurality of guide lands 20 are provided between the chamfered portions 19 in the circumferential direction of the pilot valve 6 to prevent the pilot valve 6 from tilting by contacting the lands 13 and 15. A hydraulic servo motor for driving a directly coupled control valve in a hydraulic continuously variable transmission, characterized in that the motors are provided at equal intervals.
JP13861588A 1988-06-06 1988-06-06 Hydraulic servomotor for directly-coupled control valve driving in hydraulic continuously variable transmission Granted JPS6487962A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13861588A JPS6487962A (en) 1988-06-06 1988-06-06 Hydraulic servomotor for directly-coupled control valve driving in hydraulic continuously variable transmission

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13861588A JPS6487962A (en) 1988-06-06 1988-06-06 Hydraulic servomotor for directly-coupled control valve driving in hydraulic continuously variable transmission

Publications (2)

Publication Number Publication Date
JPS6487962A JPS6487962A (en) 1989-04-03
JPH0350146B2 true JPH0350146B2 (en) 1991-07-31

Family

ID=15226225

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13861588A Granted JPS6487962A (en) 1988-06-06 1988-06-06 Hydraulic servomotor for directly-coupled control valve driving in hydraulic continuously variable transmission

Country Status (1)

Country Link
JP (1) JPS6487962A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9334934B2 (en) 2010-11-08 2016-05-10 Yanmar Co., Ltd. Belt type continuously variable transmission
JP5732328B2 (en) * 2011-06-23 2015-06-10 ヤンマー株式会社 Belt type continuously variable transmission
US9309952B2 (en) 2011-06-15 2016-04-12 Yanmar Co., Ltd. Belt-type continuously variable transmission

Also Published As

Publication number Publication date
JPS6487962A (en) 1989-04-03

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