JPH0369379U - - Google Patents
Info
- Publication number
- JPH0369379U JPH0369379U JP1990111563U JP11156390U JPH0369379U JP H0369379 U JPH0369379 U JP H0369379U JP 1990111563 U JP1990111563 U JP 1990111563U JP 11156390 U JP11156390 U JP 11156390U JP H0369379 U JPH0369379 U JP H0369379U
- Authority
- JP
- Japan
- Prior art keywords
- duct
- hydraulic
- movable core
- chamber
- pilot
- 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
Links
- 238000004804 winding Methods 0.000 claims description 5
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims 5
- 230000004323 axial length Effects 0.000 claims 1
- 239000003302 ferromagnetic material Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
- F16K31/36—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor
- F16K31/40—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor with electrically-actuated member in the discharge of the motor
- F16K31/406—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor with electrically-actuated member in the discharge of the motor acting on a piston
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T15/00—Construction arrangement, or operation of valves incorporated in power brake systems and not covered by groups B60T11/00 or B60T13/00
- B60T15/02—Application and release valves
- B60T15/025—Electrically controlled valves
- B60T15/028—Electrically controlled valves in hydraulic systems
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D16/00—Control of fluid pressure
- G05D16/20—Control of fluid pressure characterised by the use of electric means
- G05D16/2093—Control of fluid pressure characterised by the use of electric means with combination of electric and non-electric auxiliary power
- G05D16/2097—Control of fluid pressure characterised by the use of electric means with combination of electric and non-electric auxiliary power using pistons within the main valve
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Transportation (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Magnetically Actuated Valves (AREA)
- Safety Valves (AREA)
Description
第1図は本考案の液圧装置の第1実施例の部分
的な断面図、第2図は本考案の液圧装置の第2実
施例の部分的な断面図、第3図は本考案の装置の
一部を形成するパイロツト弁の実際的な実施例の
圧力/電流特性の線図を示す。
1……サーボ弁の体部、2……体部の円筒形ボ
ア、3……パイロツト弁の体部、4……電磁石、
5……巻線、6……管状ボビン、7……アーマチ
ユア、11……スリーブ、12……可動コア、1
4……パイロツトチヤンバ、15……排出孔、1
8……ダクト、19……主チヤンバ、20……補
助ダクト、23……制限オリフイス、29……ボ
ールシヤツタ、30……プラグ、33……補助チ
ヤンバ、34……軸方向の周辺溝、35……環状
チヤンバ、36……ピン、38……螺旋形ばね、
39……制限板、42……小さい断面のオリフイ
ス。
FIG. 1 is a partial sectional view of a first embodiment of the hydraulic device of the present invention, FIG. 2 is a partial sectional view of a second embodiment of the hydraulic device of the present invention, and FIG. 3 is a partial sectional view of a second embodiment of the hydraulic device of the present invention. Figure 3 shows a diagram of the pressure/current characteristics of a practical example of a pilot valve forming part of a device; 1... body of servo valve, 2... cylindrical bore of body, 3... body of pilot valve, 4... electromagnet,
5... Winding wire, 6... Tubular bobbin, 7... Armature, 11... Sleeve, 12... Movable core, 1
4... Pilot chamber, 15... Discharge hole, 1
8... Duct, 19... Main chamber, 20... Auxiliary duct, 23... Limiting orifice, 29... Ball shutter, 30... Plug, 33... Auxiliary chamber, 34... Axial peripheral groove, 35... ... annular chamber, 36 ... pin, 38 ... helical spring,
39...Restriction plate, 42...Orifice with a small cross section.
Claims (1)
を調整する如くパイロツトチヤンバ14と、液圧
パイロツト弁とを有する液圧サーボ弁を具備し、
該パイロツト弁が、該パイロツトチヤンバ14に
連通し小さい断面のオリフイス23,42を介し
加圧流体源に結合されるダクト18と、排出タン
クに結合される孔15と、該排出孔15に該ダク
ト18を連通させる通路19,20とを有する体
部3と、該通路19,20に対応して該体部3に
形成される座と協働するシヤツタ29と、該パイ
ロツト弁体部3に取付けられるアーマチユア7と
、巻線5と、該巻線5に供給される電流の強さに
比例する力で該座に向い該シヤツタ29をその閉
鎖位置に付勢する可動コア12とを有する電磁石
4とを備え、電気的な比例制御を行う液圧装置に
おいて、前記シヤツタと協働する前記座が、前記
電磁石4のアーマチユア7内にある前記パイロツ
ト弁体部3の領域に位置し、該シヤツタ29が、
該電磁石4の前記可動コア12で直接に操作され
、前記電磁石4の可動コア12が、前記巻線15
の管状支持ボビン6に摺動可能に装着され、前記
パイロツト弁体部3が、ほぼ円筒形の要素の形態
であり、該電磁石4の巻線5の支持ボビン6の一
端内に挿入される一端を有し、該弁体部3の該一
端が、該支持ボビン6内の主チヤンバ19をそれ
に面する前記可動コア12の端部と共に限定し、
該パイロツト弁体部3に形成される前記ダクト1
8が、該主チヤンバに開口し、該ダクト18を排
出孔15に結合する前記通路が、該主チヤンバ1
9と、該主チヤンバ19を該排出孔15に結合す
る少くとも1つの補助ダクト20とで構成され、
前記シヤツタ29の座が、該主チヤンバ19に開
口する該ダクト18の端部で構成されることを特
徴とする、液圧装置。 (2) 前記ダクト18を加圧流体源に結合する小
さい断面のオリフイス23が、前記パイロツト弁
の体部3に形成されることを特徴とする実用新案
登録請求の範囲第1項記載の液圧装置。 (3) 前記ダクト18を加圧流体源に結合する小
さい断面のオリフイス42が、前記液圧サーボ弁
に形成され、前記パイロツトチヤンバ14が、該
ダクト18と、小さい断面の該オリフイス42と
の間に間挿されることを特徴とする実用新案登録
請求の範囲第1項記載の液圧装置。 (4) 小さい断面のオリフイス23,42が、比
較的短い軸方向長さを有することを特徴とする実
用新案登録請求の範囲第1項記載の液圧装置。 (5) 前記パイロツト弁体部3が、強磁性材料で
作られることを特徴とする実用新案登録請求の範
囲第1項記載の液圧装置。 (6) 前記可動コア12が、スリーブ11の間挿
により、前記巻線5の支持ボビン6内に摺動可能
に装着されることを特徴とする実用新案登録請求
の範囲第1項記載の液圧装置。 (7) 前記弁が、該弁の体部3に対向して前記ス
リーブ11の端部を閉じる閉鎖要素30を有し、
該閉鎖要素30が、それに面する前記可動コア1
2の端部と共に、該スリーブ11内に補助チヤン
バ33を限定し、該可動コア12が、前記主チヤ
ンバ19を該補助チヤンバ33に連通させる一連
の軸方向の周辺溝34を有することを特徴とする
実用新案登録請求の範囲第6項記載の液圧装置。 (8) 前記可動コア12が、環状周辺チヤンバ3
5を前記スリーブ11内に限定する小さい直径の
中間部分を有することを特徴とする実用新案登録
請求の範囲第7項記載の液圧装置。 (9) 弾性装置38が、前記閉鎖要素30と、該
要素に面する前記可動コア12の端部との間に間
挿されることを特徴とする実用新案登録請求の範
囲第7項記載の液圧装置。 (10) 前記閉鎖要素30の方向で前記可動コア1
2のストロークの限界を限定するストローク制限
装置36を備え、該可動コア12と、閉鎖要素3
0との対向する端部が、このストローク限界位置
で相互に離れることを特徴とする実用新案登録請
求の範囲第7項記載の液圧装置。 (11) 前記ストロークの制限装置が、前記可動コ
ア12内に圧力嵌めされる軸方向ピン36で構成
されることを特徴とする実用新案登録請求の範囲
第10項記載の液圧装置。 (12) 前記シヤツタ29の座が、前記ダクト18
の前記主チヤンバ19に開口する端部で前記弁体
部3に装着されるブツシユ28の内側端縁によつ
て限定されることを特徴とする実用新案登録請求
の範囲第1項記載の液圧装置。 (13) 前記電磁石の外方へ突出する前記弁体部3
の部分が、前記液圧サーボ弁と、パイロツト弁と
の結合を達成する如く該サーボ弁の体部1の座2
に挿入されることを特徴とする実用新案登録請求
の範囲第1項記載の液圧装置。 (14) 前記ダクト18が、前記体部3を軸方向に
貫通して延びるボアで構成されることを特徴とす
る実用新案登録請求の範囲第1項記載の液圧装置
。 (15) 前記パイロツトチヤンバ14に連通する前
記ダクト18の端部が、該ダクトと、パイロツト
チヤンバ14との間での圧力の揺動の伝達を防止
する如く孔付き制限板39を備えることを特徴と
する実用新案登録請求の範囲第1項記載の液圧装
置。[Claims for Utility Model Registration] (1) A hydraulic servo valve having a pilot chamber 14 and a hydraulic pilot valve for adjusting the pressure in the pilot chamber of the hydraulic servo valve;
The pilot valve has a duct 18 communicating with the pilot chamber 14 and connected to a source of pressurized fluid through small cross-section orifices 23, 42, a hole 15 connected to a discharge tank, and a hole 15 connected to the discharge hole 15. A body part 3 having passages 19, 20 communicating with the duct 18, a shutter 29 cooperating with a seat formed in the body part 3 corresponding to the passages 19, 20, and a shutter 29 provided in the pilot valve body part 3. an electromagnet having a mounted armature 7, a winding 5 and a movable core 12 which faces the seat and urges the shutter 29 into its closed position with a force proportional to the strength of the current supplied to the winding 5; 4, in which the seat cooperating with the shutter is located in the region of the pilot valve body 3 in the armature 7 of the electromagnet 4, and the shutter 29 is
Directly operated by the movable core 12 of the electromagnet 4, the movable core 12 of the electromagnet 4
The pilot valve body portion 3 is in the form of a generally cylindrical element, one end of which is inserted into one end of the support bobbin 6 of the winding 5 of the electromagnet 4. the one end of the valve body part 3 defines a main chamber 19 in the support bobbin 6 together with the end of the movable core 12 facing thereto;
The duct 1 formed in the pilot valve body portion 3
8 opens into the main chamber and the passage connecting the duct 18 to the discharge hole 15 is connected to the main chamber 1.
9 and at least one auxiliary duct 20 connecting the main chamber 19 to the discharge hole 15,
Hydraulic device, characterized in that the seat of the shutter 29 is constituted by the end of the duct 18 opening into the main chamber 19. (2) The hydraulic system according to claim 1, characterized in that an orifice 23 of small cross section connecting the duct 18 to a source of pressurized fluid is formed in the body 3 of the pilot valve. Device. (3) A small cross-section orifice 42 connecting the duct 18 to a source of pressurized fluid is formed in the hydraulic servo valve, and the pilot chamber 14 connects the duct 18 with the small cross-section orifice 42. The hydraulic device according to claim 1, characterized in that the hydraulic device is inserted in between. (4) The hydraulic device according to claim 1, wherein the orifices 23, 42 having a small cross section have a relatively short axial length. (5) The hydraulic device according to claim 1, wherein the pilot valve body portion 3 is made of a ferromagnetic material. (6) The fluid according to claim 1, wherein the movable core 12 is slidably mounted within the support bobbin 6 of the winding 5 by inserting the sleeve 11. Pressure device. (7) the valve has a closing element 30 closing the end of the sleeve 11 opposite the body 3 of the valve;
The closure element 30 faces the movable core 1
2 defines an auxiliary chamber 33 within said sleeve 11, characterized in that said movable core 12 has a series of axial peripheral grooves 34 which communicate said main chamber 19 with said auxiliary chamber 33. A hydraulic device according to claim 6 of the utility model registration claim. (8) The movable core 12 is connected to the annular peripheral chamber 3.
8. Hydraulic device according to claim 7, characterized in that it has an intermediate portion of small diameter which confines the hydraulic pressure device 5 within the sleeve 11. (9) The fluid according to claim 7, characterized in that an elastic device 38 is interposed between the closure element 30 and the end of the movable core 12 facing it. Pressure device. (10) the movable core 1 in the direction of the closure element 30;
a stroke limiting device 36 for limiting the stroke limit of the movable core 12 and the closing element 3;
8. The hydraulic device according to claim 7, wherein the ends opposite to each other are separated from each other at the stroke limit position. (11) The hydraulic device according to claim 10, wherein the stroke limiting device comprises an axial pin 36 press-fitted into the movable core 12. (12) The seat of the shutter 29 is located in the duct 18.
The hydraulic system according to claim 1, characterized in that it is limited by an inner edge of a bushing (28) which is attached to the valve body (3) at its end opening into the main chamber (19). Device. (13) The valve body portion 3 protruding outward from the electromagnet.
The seat 2 of the body part 1 of the servo valve is configured such that the portion 2 of the hydraulic servo valve achieves a connection between the hydraulic servo valve and the pilot valve.
The hydraulic device according to claim 1, which is inserted into a utility model. (14) The hydraulic device according to claim 1, wherein the duct 18 is constituted by a bore extending axially through the body portion 3. (15) The end of the duct 18 communicating with the pilot chamber 14 is provided with a restricting plate 39 with holes so as to prevent pressure fluctuations from being transmitted between the duct and the pilot chamber 14. A hydraulic device according to claim 1, characterized in that:
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67914/81A IT1144260B (en) | 1981-07-01 | 1981-07-01 | PROPORTIONAL ELECTRIC PILOT HYDRAULIC SYSTEM |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0369379U true JPH0369379U (en) | 1991-07-10 |
Family
ID=11306327
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57113801A Pending JPS5821074A (en) | 1981-07-01 | 1982-06-30 | Hydraulic device conducting electrical proportional control |
JP1990111563U Pending JPH0369379U (en) | 1981-07-01 | 1990-10-24 |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57113801A Pending JPS5821074A (en) | 1981-07-01 | 1982-06-30 | Hydraulic device conducting electrical proportional control |
Country Status (5)
Country | Link |
---|---|
JP (2) | JPS5821074A (en) |
DE (1) | DE3224189A1 (en) |
FR (1) | FR2509009B1 (en) |
GB (1) | GB2103390B (en) |
IT (1) | IT1144260B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009011253A (en) * | 2007-07-05 | 2009-01-22 | Tokyo Tobari Kk | Get over-preventing fence and return component |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60175884A (en) * | 1984-02-07 | 1985-09-10 | シ−ルド・パワ−・コ−ポレ−シヨン | Solenoid valve |
DE3443079A1 (en) * | 1984-07-21 | 1986-01-30 | Wabco Westinghouse Fahrzeugbremsen GmbH, 3000 Hannover | Valve device |
DE3427033A1 (en) * | 1984-07-21 | 1986-01-23 | Wabco Westinghouse Fahrzeugbremsen GmbH, 3000 Hannover | VALVE DEVICE |
JPS6166276U (en) * | 1984-10-08 | 1986-05-07 | ||
DE3442750A1 (en) * | 1984-11-23 | 1986-05-28 | Robert Bosch Gmbh, 7000 Stuttgart | SOLENOID VALVE FOR FLUID CONTROL |
DE3714337C2 (en) * | 1987-04-29 | 1997-03-20 | Rexroth Mannesmann Gmbh | Servo valve with piezo control and piezoelectric control motor |
JPS6457472U (en) * | 1987-10-05 | 1989-04-10 | ||
US5018431A (en) * | 1988-12-09 | 1991-05-28 | Quadrastat Corporation | Apparatus for positioning a work implement |
US5184644A (en) * | 1991-05-30 | 1993-02-09 | Coltec Industries Inc. | Solenoid operated pressure regulating valve |
DE4400115A1 (en) * | 1993-01-04 | 1994-07-07 | Aro Corp | Feed-through coil for a pneumatic valve |
JP2721117B2 (en) * | 1993-02-23 | 1998-03-04 | ステリス コーポレイション | Lock mechanism, system provided with the lock mechanism, and sterilization system provided with the lock mechanism |
US5421545A (en) * | 1993-09-03 | 1995-06-06 | Caterpillar Inc. | Poppet valve with force feedback control |
EP1054152A3 (en) * | 1999-05-19 | 2002-08-14 | HydraForce, Inc. | Electrically controlled valve having mechanism for controlling a nonlinear force |
US6769252B2 (en) | 2001-12-10 | 2004-08-03 | Caterpillar Inc | Fluid system having variable pressure relief |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5179024A (en) * | 1974-12-27 | 1976-07-09 | Rexroth Gmbh G L | JISHAKUCHOSETSUSHIKIATSURYOKUBEN |
US3983909A (en) * | 1973-12-14 | 1976-10-05 | Societe Anonyme D.B.A. | Three-way solenoid valve |
JPS551005B2 (en) * | 1974-03-21 | 1980-01-11 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB837899A (en) * | 1957-01-04 | 1960-06-15 | Concentric Mfg Company Ltd | Improvements in and relating to electrically controlled valves |
GB853974A (en) * | 1957-10-09 | 1960-11-16 | British Oxygen Co Ltd | Servo valve for pressure fluids |
GB992960A (en) * | 1961-08-02 | 1965-05-26 | Brakeshoe Internat S A | Improved electric and fluid pressure operated valve mechanism and control circuit therefor |
GB1072988A (en) * | 1963-10-05 | 1967-06-21 | Asea Ab | Fluid pressure regulator valve |
DE2023259A1 (en) * | 1969-05-20 | 1970-11-26 | Flight Refuelling Ltd., London | Solenoid operated flow medium valve, especially for hydraulic high pressure circuits of aircraft |
JPS4834246A (en) * | 1971-09-06 | 1973-05-17 | ||
US3861644A (en) * | 1973-10-09 | 1975-01-21 | Gen Motors Corp | Solenoid valve |
DE2439271A1 (en) * | 1974-08-16 | 1976-03-11 | Herion Werke Kg | Solenoid valve with main and auxiliary valve plug - opposing pole of latter slides in plug guide |
-
1981
- 1981-07-01 IT IT67914/81A patent/IT1144260B/en active
-
1982
- 1982-06-23 GB GB08218210A patent/GB2103390B/en not_active Expired
- 1982-06-29 DE DE19823224189 patent/DE3224189A1/en active Granted
- 1982-06-30 JP JP57113801A patent/JPS5821074A/en active Pending
- 1982-06-30 FR FR8211492A patent/FR2509009B1/en not_active Expired
-
1990
- 1990-10-24 JP JP1990111563U patent/JPH0369379U/ja active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3983909A (en) * | 1973-12-14 | 1976-10-05 | Societe Anonyme D.B.A. | Three-way solenoid valve |
JPS551005B2 (en) * | 1974-03-21 | 1980-01-11 | ||
JPS5179024A (en) * | 1974-12-27 | 1976-07-09 | Rexroth Gmbh G L | JISHAKUCHOSETSUSHIKIATSURYOKUBEN |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009011253A (en) * | 2007-07-05 | 2009-01-22 | Tokyo Tobari Kk | Get over-preventing fence and return component |
Also Published As
Publication number | Publication date |
---|---|
GB2103390B (en) | 1984-11-28 |
JPS5821074A (en) | 1983-02-07 |
GB2103390A (en) | 1983-02-16 |
DE3224189A1 (en) | 1983-01-20 |
FR2509009B1 (en) | 1986-08-22 |
FR2509009A1 (en) | 1983-01-07 |
IT8167914A0 (en) | 1981-07-01 |
IT1144260B (en) | 1986-10-29 |
DE3224189C2 (en) | 1988-06-16 |
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