JPH05223169A - Transmission mechanism for hydraulic continuously variable-transmission - Google Patents
Transmission mechanism for hydraulic continuously variable-transmissionInfo
- Publication number
- JPH05223169A JPH05223169A JP2788892A JP2788892A JPH05223169A JP H05223169 A JPH05223169 A JP H05223169A JP 2788892 A JP2788892 A JP 2788892A JP 2788892 A JP2788892 A JP 2788892A JP H05223169 A JPH05223169 A JP H05223169A
- Authority
- JP
- Japan
- Prior art keywords
- continuously variable
- pilot
- hydraulic
- variable transmission
- hydraulic continuously
- 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.)
- Granted
Links
Landscapes
- Control Of Fluid Gearings (AREA)
- Control Of Transmission Device (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、走行車輌の車軸駆動装
置等として使用される油圧式無段変速装置における、変
速操作レバーの操作機構に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an operation mechanism of a gear shift operation lever in a hydraulic continuously variable transmission used as an axle drive device of a traveling vehicle.
【0002】[0002]
【従来の技術】従来から、油圧式無段変速装置の変速操
作系統中に流体ダンパーを介在した技術は公知とされて
いるのである。例えば特開昭61−27730号公報に
記載の技術の如くである。2. Description of the Related Art Conventionally, a technique in which a fluid damper is interposed in a shift operation system of a hydraulic continuously variable transmission has been known. For example, it is like the technique described in JP-A-61-27730.
【0003】[0003]
【発明が解決しようとする課題】しかし、上記従来技術
においては、油圧式無段変速装置の変速操作系統中に流
体ダンパーを介在した技術は公知とされているが、該流
体ダンパーの減衰力定数は常時不変であり、車輌の加速
度変化まで減衰させることは出来なかったのである。However, in the above-mentioned prior art, it is known that the fluid damper is interposed in the gear shift operation system of the hydraulic continuously variable transmission, but the damping force constant of the fluid damper is known. Was always constant and could not be dampened to changes in vehicle acceleration.
【0004】[0004]
【課題を解決するための手段】本発明の解決すべき課題
は以上の如くであり、次に該課題を解決する為の手段を
説明する。即ち、油圧式無段変速装置の変速操作系統中
に流体ダンパーを介在した構成において、該流体ダンパ
ーの流路中にパイロット差圧感知式可変オリフィス弁を
介装し、該パイロット差圧感知式可変オリフィス弁のパ
イロット室a・bに、前記油圧式無段変速装置の作動油
を導入しパイロット室a・bの油圧差が大きくなるにつ
れてその絞り穴径を小さくするように構成したものであ
る。The problems to be solved by the present invention are as described above, and the means for solving the problems will be described below. That is, in a configuration in which a fluid damper is interposed in a gear shift operation system of a hydraulic type continuously variable transmission, a pilot differential pressure sensing type variable orifice valve is provided in a flow path of the fluid damper, and the pilot differential pressure sensing type variable valve is installed. The hydraulic fluid of the hydraulic continuously variable transmission is introduced into the pilot chambers a and b of the orifice valve, and the throttle hole diameter is reduced as the hydraulic pressure difference between the pilot chambers a and b increases.
【0005】[0005]
【作用】次に作用を説明する。即ち、油圧式無段変速装
置を車軸駆動装置とする走行車輌において、油圧式無段
変速装置の作動油圧の変化に追従して、流体ダンパーの
減衰力定数が変化し、走行車輌の加速度変化減衰、急発
進や急停車等の衝撃を和らぐことになる。[Operation] Next, the operation will be described. That is, in a traveling vehicle in which the hydraulic continuously variable transmission is used as the axle drive device, the damping force constant of the fluid damper changes in accordance with the change in the operating oil pressure of the hydraulic continuously variable transmission, and the acceleration change damping of the traveling vehicle is attenuated. , The impact of sudden start or sudden stop will be softened.
【0006】[0006]
【実施例】次に実施例を説明する。図1は、油圧式無段
変速装置の変速操作機構において、2個のパイロット差
圧感知式可変オリフィス弁Aを配置した実施例の油圧回
路図、図2は本発明の油圧式無段変速装置の変速操作機
構において、油圧ポンプPと油圧モーターMにより構成
する閉回路の高圧回路と、低圧回路の間にシャトル弁1
4を介装し、1個のパイロット差圧感知式可変オリフィ
ス弁Aのみを配置した構成の油圧回路図、図3はパイロ
ット差圧感知式可変オリフィス弁の作動態様を示す図
面、図4は油圧式無段変速装置の変速操作機構の模式図
である。EXAMPLES Next, examples will be described. FIG. 1 is a hydraulic circuit diagram of an embodiment in which two pilot differential pressure sensing type variable orifice valves A are arranged in a shift operation mechanism of a hydraulic continuously variable transmission, and FIG. 2 is a hydraulic continuously variable transmission of the present invention. In the speed change operation mechanism of the shuttle valve 1, a shuttle valve
4 is a hydraulic circuit diagram of a configuration in which only one pilot differential pressure sensing type variable orifice valve A is arranged, FIG. 3 is a drawing showing an operating mode of the pilot differential pressure sensing type variable orifice valve, and FIG. FIG. 3 is a schematic view of a gear shift operation mechanism of a continuously variable transmission.
【0007】図1において説明する。走行車輌に油圧式
無段変速装置が搭載されており、該走行車輌のエンジン
Eにより、可動斜板6を具備した油圧ポンプPを駆動し
ている。該油圧ポンプPは可動斜板6の角度を変更する
ことにより、圧油の吐出方向を逆にすることができ、油
圧モーターMの回転を前進回転と後進回転と、その間に
非回転状態の中立状態に変速することができる。前進回
転と後進回転は、可動斜板6の回動角の変更により無段
変速を可能としている。This will be described with reference to FIG. The traveling vehicle is equipped with a hydraulic continuously variable transmission, and an engine E of the traveling vehicle drives a hydraulic pump P having a movable swash plate 6. The hydraulic pump P can reverse the discharge direction of the pressure oil by changing the angle of the movable swash plate 6, and the rotation of the hydraulic motor M can be forward rotation and reverse rotation, and a neutral state in a non-rotation state between them. It is possible to shift to the state. The forward rotation and the reverse rotation enable stepless speed change by changing the rotation angle of the movable swash plate 6.
【0008】そして油圧ポンプPと油圧モーターMの間
に閉回路を構成する一対の油路4・5により連結してい
る。油路4・5は一方が高圧となる場合には、他方が低
圧となり、どちらが高圧となるかは可動斜板6の回動方
向により決定する。そして4・5の間にチャージチェッ
ク弁11・12を介して、チャージポンプCPからの圧
油が供給されるべく構成されている。The hydraulic pump P and the hydraulic motor M are connected by a pair of oil passages 4 and 5 forming a closed circuit. When one of the oil passages 4 and 5 has a high pressure, the other has a low pressure, and which one has a high pressure is determined by the rotating direction of the movable swash plate 6. The pressure oil is supplied from the charge pump CP via the charge check valves 11 and 12 between 4 and 5.
【0009】該作動油補給チェック弁11・12は、閉
回路内の作動油が減少して、内部に負圧が発生した場合
に、低圧側のチャージチェック弁11・12が開いて、
該開いたチャージチェック弁11・12から、作動油が
補給されるのである。該チャージポンプCPはエンジン
Eにより油圧ポンプPの軸と同じ軸により駆動されてお
り、閉回路に作動油の補給の必要の無い場合には、チャ
ージポンプCPからの圧油はチャージリリーフ弁13に
より、作動油タンクであるミッションケース内に噴出さ
れている。The hydraulic oil replenishment check valves 11 and 12 open the low-pressure side charge check valves 11 and 12 when the hydraulic oil in the closed circuit decreases and a negative pressure is generated inside.
The hydraulic oil is replenished from the open charge check valves 11 and 12. The charge pump CP is driven by the engine E by the same shaft as that of the hydraulic pump P, and when there is no need to replenish the operating oil to the closed circuit, the pressure oil from the charge pump CP is supplied by the charge relief valve 13. , Is ejected into the mission case, which is a hydraulic oil tank.
【0010】以上のような構成において、走行車輌に乗
車したオペレーターは、変速レバー1を前後に回動する
ことにより可動斜板6を回動し、圧油の吐出方向と吐出
量を変更し、油圧モーターMの回転方向と回転数を操作
するのである。しかし、変速レバー1の回動操作によ
り、可動斜板6を一気に大きく傾斜させると、油圧ポン
プPからの吐出圧油の量と方向が一気に変化してしま
い、油圧モーターMの回転数や回転方向が一気に変更さ
れてしまうのである。このように、油圧モーターMの回
転数が一気に変更されることは、増速の加速度や、減速
の加速度が一気に変化することとなり、オペレーターに
とっては、機体の急発進や急停止状態を感じるのであ
る。In the above configuration, the operator who gets on the traveling vehicle rotates the movable swash plate 6 by rotating the speed change lever 1 back and forth to change the discharge direction and discharge amount of the pressure oil, The rotation direction and the rotation speed of the hydraulic motor M are operated. However, when the movable swash plate 6 is greatly tilted at a stroke by the rotation operation of the speed change lever 1, the amount and direction of the pressure oil discharged from the hydraulic pump P change at once, and the rotation speed and rotation direction of the hydraulic motor M are changed. Is changed all at once. In this way, if the rotational speed of the hydraulic motor M is changed at once, the acceleration for acceleration and the acceleration for deceleration change at once, and the operator feels a sudden start or sudden stop of the machine. .
【0011】以上のような急発進や急停車等の加速度の
急な変化を回避する為に、変速レバー1の回動速度を規
制する流体ダンパーDが設けられている。該流体ダンパ
ーDはピストン3とシリンダ2により、往復動シリンダ
に構成され、内部に油が充填されている。図1におい
て、ピストン3がシリンダ2の内部で左右に摺動する
と、ピストン3によりシリンダ2が完全に2室に分割さ
れているので、ピストン3が圧縮する方向のシリンダ2
の油室eあるいは油室fの油は、流路Cを経て、移動自
在である。In order to avoid a sudden change in acceleration such as a sudden start or a sudden stop as described above, a fluid damper D for regulating the rotational speed of the speed change lever 1 is provided. The fluid damper D is composed of a piston 3 and a cylinder 2 into a reciprocating cylinder, and the inside thereof is filled with oil. In FIG. 1, when the piston 3 slides left and right inside the cylinder 2, the piston 3 completely divides the cylinder 2 into two chambers.
The oil in the oil chamber e or the oil chamber f is movable via the flow path C.
【0012】本発明は、この流路Cに、パイロット差圧
感知式可変オリフィス弁Aを配置したのである。パイロ
ット差圧感知式可変オリフィス弁Aは閉回路4・5から
の圧油を、パイロット室a・bに案内している。In the present invention, the pilot differential pressure sensing type variable orifice valve A is arranged in the flow path C. The pilot differential pressure sensing type variable orifice valve A guides the pressure oil from the closed circuits 4 and 5 to the pilot chambers a and b.
【0013】そして該パイロット差圧感知式可変オリフ
ィス弁Aのパイロット室a・bへ導入する圧油とオリフ
ィス弁の開度は、図3に示す如く構成されている。即ち
パイロット室aへは、油路4・5の圧油が直接に導入さ
れているが、パイロット室bへは絞りmを介して、圧油
が導入されているので、この絞りmの分だけパイロット
室a・bの圧力に差が出て、オリフィス弁が開閉される
のである。The pressure oil introduced into the pilot chambers a and b of the pilot differential pressure sensing type variable orifice valve A and the opening of the orifice valve are constructed as shown in FIG. That is, the pressure oil in the oil passages 4 and 5 is directly introduced into the pilot chamber a, but the pressure oil is introduced into the pilot chamber b through the throttle m, so that only the portion corresponding to this throttle m. The difference between the pressures in the pilot chambers a and b causes the orifice valve to open and close.
【0014】即ち、絞りmを介して導入されるパイロッ
ト室bの油圧Pbは、絞りmにより均一化された定常圧
となっており、それ程、加速度変化の影響を受けないの
である。これに対して、絞りmを通過しないで、油路4
・5から直接にパイロット室aに導入される油圧Pa
は、変動圧そのままを受け入れるものであり、変動圧の
大小がそのまま入力されるのである。このパイロット室
aに入力される変動圧と、パイロット室bに入力される
定常圧の差を、パイロット差圧感知式可変オリフィス弁
Aが感知するのである。That is, the oil pressure Pb of the pilot chamber b introduced through the throttle m is a steady pressure which is uniformized by the throttle m, and is not so affected by the acceleration change. On the other hand, the oil passage 4 does not pass through the throttle m.
・ Hydraulic pressure Pa introduced directly into the pilot chamber a from 5
Accepts the fluctuating pressure as it is, and the magnitude of the fluctuating pressure is input as it is. The pilot differential pressure sensing type variable orifice valve A senses the difference between the fluctuating pressure input to the pilot chamber a and the steady pressure input to the pilot chamber b.
【0015】その結果、図3に示す如く、変動圧の方が
定常圧よりも大きい場合「Pa>Pb」においては、パ
イロット差圧感知式可変オリフィス弁Aの絞り穴径も小
径に絞る。変動圧が定常圧と等しい場合「Pa=Pb」
においては、絞り穴径を中径に絞る。変動圧の方が定常
圧よりも小さい場合「Pa<Pb」においては、絞り穴
径を大径とする。即ち、変動圧と定常圧の大小により、
パイロット差圧感知式可変オリフィス弁Aの絞り穴径を
変化させて、流路Cで油が通過するのに抵抗を与え変速
レバー1に与える抵抗力を変化させるのである。As a result, as shown in FIG. 3, when the fluctuation pressure is larger than the steady pressure, "Pa>Pb", the throttle hole diameter of the pilot differential pressure sensing type variable orifice valve A is also reduced to a small diameter. When the fluctuating pressure is equal to the steady pressure "Pa = Pb"
In, the aperture diameter is reduced to a medium diameter. When the fluctuating pressure is smaller than the steady pressure, the diameter of the throttle hole is set to a large diameter in the case of "Pa <Pb". That is, depending on the magnitude of the fluctuating pressure and the steady pressure,
By changing the throttle hole diameter of the pilot differential pressure sensing type variable orifice valve A, resistance is given to the passage of oil in the flow path C and the resistance force given to the speed change lever 1 is changed.
【0016】図1の実施例では油路4・5において、高
圧側の圧力によりどちらか一方のパイロット差圧感知式
可変オリフィス弁Aが作動するのであり、低圧側の圧力
では、他方のオリフィス弁Aは作動しない。油路4・5
のどちらか高圧側の圧油によりパイロット差圧感知式可
変オリフィス弁Aを作動させる必要があるので、パイロ
ット差圧感知式可変オリフィス弁A2組が配置されてい
るのである。In the embodiment of FIG. 1, in the oil passages 4 and 5, either one of the pilot differential pressure sensing type variable orifice valves A is operated by the high pressure side pressure, and the other orifice valve is operated by the low pressure side pressure. A does not work. Oil passage 4.5
Since it is necessary to operate the pilot differential pressure sensing type variable orifice valve A by the pressure oil on either side of the high pressure side, two pilot differential pressure sensing type variable orifice valves A are arranged.
【0017】また、図2の実施例に示す如く、ボールバ
ルブ9が低圧側の回路を閉鎖する構造の、シャトル弁1
4を油路4・5の間に介装した場合には、該シャトル弁
14から、常時高圧側の圧油をパイロット差圧感知式可
変オリフィス弁Aに案内すべく構成することにより、1
個のパイロット差圧感知式可変オリフィス弁Aのみで、
構成することが出来るのである。As shown in the embodiment of FIG. 2, the shuttle valve 1 having a structure in which the ball valve 9 closes the circuit on the low pressure side.
When 4 is provided between the oil passages 4 and 5, the shuttle valve 14 is configured to constantly guide the high pressure side pressure oil to the pilot differential pressure sensing type variable orifice valve A.
With only one pilot differential pressure sensing type variable orifice valve A,
It can be configured.
【0018】[0018]
【発明の効果】本発明は以上の如く構成したので、次の
ような効果を奏するのである。即ち、油圧式無段変速装
置を車軸駆動装置に用いた走行車輌において、油圧式無
段変速装置の高圧側油路の油圧差により、パイロット差
圧感知式可変オリフィス弁の絞り穴径を変化させて、こ
れにより流体ダンパーDの減衰力定数を変化することが
出来るのである。故に、走行車輌の加速度変化を減衰さ
せることが可能となり、急発進や急停車等の衝撃を和ら
げることが可能となったのである。Since the present invention is configured as described above, it has the following effects. That is, in a traveling vehicle using a hydraulic continuously variable transmission as an axle drive device, the throttle hole diameter of the pilot differential pressure sensing type variable orifice valve is changed by the hydraulic pressure difference of the high pressure side oil passage of the hydraulic continuously variable transmission. As a result, the damping force constant of the fluid damper D can be changed. Therefore, it becomes possible to damp the acceleration change of the traveling vehicle and soften the shock such as sudden start or sudden stop.
【図1】油圧式無段変速装置の変速操作機構において、
パイロット差圧感知式可変オリフィス弁をAを2個配置
した実施例の油圧回路図。FIG. 1 shows a shift operation mechanism of a hydraulic continuously variable transmission,
FIG. 3 is a hydraulic circuit diagram of an embodiment in which two pilot differential pressure sensing type variable orifice valves A are arranged.
【図2】本発明の油圧式無段変速装置の変速操作機構に
おいて、油圧ポンプPと油圧モーターMにより構成する
閉回路の高圧回路と、低圧回路の間にシャトル弁14を
介装し、1個のパイロット差圧感知式可変オリフィス弁
Aを配置した構成の油圧回路図。FIG. 2 is a diagram showing a shift operation mechanism of a hydraulic continuously variable transmission according to the present invention, in which a shuttle valve 14 is interposed between a closed high-pressure circuit composed of a hydraulic pump P and a hydraulic motor M, and a low-pressure circuit; FIG. 3 is a hydraulic circuit diagram of a configuration in which one pilot differential pressure sensing type variable orifice valve A is arranged.
【図3】パイロット差圧感知式可変オリフィス弁の作動
態様を示す図面である。FIG. 3 is a view showing an operation mode of a pilot differential pressure sensing type variable orifice valve.
【図4】油圧式無段変速装置の変速操作機構の模式図で
ある。FIG. 4 is a schematic view of a shift operation mechanism of a hydraulic continuously variable transmission.
A パイロット差圧感知式可変オリフィス弁 C 流路 D 流体ダンパー a・b パイロット室 1 変速レバー 2 流体ダンパーDのシリンダ 3 流体ダンパーDのピストン 4・5 油路 6 可動斜板 14 シャトル弁 A Pilot differential pressure sensing type variable orifice valve C Flow path D Fluid damper a / b Pilot chamber 1 Shift lever 2 Fluid damper D cylinder 3 Fluid damper D piston 4.5 Oil passage 6 Movable swash plate 14 Shuttle valve
Claims (1)
流体ダンパーを介在した構成において、該流体ダンパー
の流路中にパイロット差圧感知式可変オリフィス弁を介
装し、該パイロット差圧感知式可変オリフィス弁のパイ
ロット室a・bに、前記油圧式無段変速装置の作動油を
導入しパイロット室a・bの油圧差が大きくなるにつれ
てその絞り穴径を小さくするように構成したことを特徴
とする油圧式無段変速装置の変速操作機構。1. A hydraulic differential continuously variable transmission having a structure in which a fluid damper is interposed in a speed change operation system, wherein a pilot differential pressure sensing type variable orifice valve is provided in a flow path of the fluid damper, and the pilot differential pressure is provided. The hydraulic fluid of the hydraulic continuously variable transmission is introduced into the pilot chambers a and b of the sensing type variable orifice valve, and the throttle hole diameter is reduced as the hydraulic pressure difference between the pilot chambers a and b increases. A gear shifting operation mechanism of a hydraulic continuously variable transmission characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP4027888A JP2986278B2 (en) | 1992-02-14 | 1992-02-14 | Shift operation mechanism of hydraulic continuously variable transmission |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP4027888A JP2986278B2 (en) | 1992-02-14 | 1992-02-14 | Shift operation mechanism of hydraulic continuously variable transmission |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH05223169A true JPH05223169A (en) | 1993-08-31 |
JP2986278B2 JP2986278B2 (en) | 1999-12-06 |
Family
ID=12233433
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4027888A Expired - Fee Related JP2986278B2 (en) | 1992-02-14 | 1992-02-14 | Shift operation mechanism of hydraulic continuously variable transmission |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2986278B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008018563A1 (en) * | 2006-08-09 | 2008-02-14 | Hitachi Construction Machinery Co., Ltd. | Travel control device for hydraulically driven vehicle |
WO2009128172A1 (en) * | 2008-04-14 | 2009-10-22 | ヤンマー株式会社 | Work vehicle |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102482348B1 (en) * | 2016-12-20 | 2022-12-29 | 키네틱스 드라이브 솔루션스 아이엔씨. | Hydrostatic drive system with variable vibration damper |
-
1992
- 1992-02-14 JP JP4027888A patent/JP2986278B2/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008018563A1 (en) * | 2006-08-09 | 2008-02-14 | Hitachi Construction Machinery Co., Ltd. | Travel control device for hydraulically driven vehicle |
WO2009128172A1 (en) * | 2008-04-14 | 2009-10-22 | ヤンマー株式会社 | Work vehicle |
JP2009257391A (en) * | 2008-04-14 | 2009-11-05 | Yanmar Co Ltd | Work vehicle |
US8418797B2 (en) | 2008-04-14 | 2013-04-16 | Yanmar Co., Ltd. | Work vehicle |
Also Published As
Publication number | Publication date |
---|---|
JP2986278B2 (en) | 1999-12-06 |
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