GB2047435A - Hydraulic control valve system - Google Patents
Hydraulic control valve system Download PDFInfo
- Publication number
- GB2047435A GB2047435A GB8009962A GB8009962A GB2047435A GB 2047435 A GB2047435 A GB 2047435A GB 8009962 A GB8009962 A GB 8009962A GB 8009962 A GB8009962 A GB 8009962A GB 2047435 A GB2047435 A GB 2047435A
- Authority
- GB
- United Kingdom
- Prior art keywords
- servo
- valve
- passage
- bore
- bleed
- 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
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
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/04—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
- F15B11/044—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the return line, i.e. "meter out"
-
- 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
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/04—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
- F15B11/042—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the feed line, i.e. "meter in"
-
- 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
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Safety Valves (AREA)
- Servomotors (AREA)
- Fluid-Pressure Circuits (AREA)
- Details Of Valves (AREA)
Abstract
A multifunction hydraulic flow metering valve arrangement circuit comprises a main valve (14), a bleed flow orifice (18), and a servo valve (64) acting with the main valve provides for proportional speed control for lowering loads and as an anti-cavitation check valve. Control pressure applied to a control chamber (44) acts on a piston (66) to compress spring (68) and whereby lift servo valve (64) from its seat (62), whereby the bleed chamber (42) is communicated with return chamber (38) and load pressure in the chamber (40) lifts the main valve (14) from its seat (54) to an extend determined by the control pressure. A pilot valve (20) in the circuit acting with the main valve provides the circuit with a pressure limiting relief valve facility. <IMAGE>
Description
SPECIFICATION
Hydraulic control valve system
This invention relates to a hydraulic control valve system.
In the control of return fluid flow from loads applied to hydraulic actuators, such as cylinders on earth-moving and construction vehicles, it is customary to provide spool-type valve elements with each valve element serving various individual functions such as speed control of lowering loads, limiting excessive
pressure, preventing or minimizing cavitation
in the hydraulic cylinders, and holding a load stationary in a preselected position.
However, use of spool-type valve elements having a movable spool member leads to certain disadvantages, such as instability of the spool member while throttling fluid flow to decelerate a lowering load, resulting in erratic or jerky movements of the load, and drifting of a stationary load from a preselected position due to leakage of fluid past clearances necessary for proper operation of the spool member.
An object of the present invention is to provide a single hydraulic flow-metering valve which may function as a proportional speedcontrol valve for lowering loads, a pressurelimiting relief valve, and possibly as an anticavitation check valve.
In accordance with the present invention, a hydraulic control valve comprises main valve means operable to shut off fluid flow between a source of load pressure and a return flow passage; a bleed flow orifice connected between said source of load pressure and a bleed pressure chamber associated with said main valve means for restricting fluid flow to said bleed chamber; and servo means associated with said main valve means for metering said restricted fluid flow from said bleed chamber to said return flow passage.
The main valve may be of the poppet type and preferably meters return fluid flow from loaded cylinders in response to a variable orifice formed in the main valve, which is controlled by an integral servo valve, and to fluid flow through the bleed flow orifice which is controlled by a pilot valve. The metering valve is advantageously designed so that the following three different valve functions can be accomplished::
when the main valve is controlled by fluid flow through the variable orifice, the servo valve provides a machine operator with a proportional speed control for lowering loads;
if cylinder fluid pressure drops below return fluid pressure in the system, the main valve will open allowing fluid from the return to flow to the cylinder thereby operating as an anti-cavitation check valve;
the pilot valve controls bleed flow from the bleed flow orifice through the main valve to provide operation as a pressure-limiting relief valve.
The invention is further described, by way of example, with reference to the accompany
ing drawings, in which:
Figure 1 is a schematic diagram of a hydraulic circuit embodying a hydraulic control valve according to the invention;
Figure 2 is a diagrammatic sectional view of a preferred embodiment of the invention; and
Figure 3 is another embodiment of the hydraulic circuit of Fig. 1.
Referring to Fig. 1, a hydraulic control valve circuit includes a load pressure line 10 adapted to be connected to a source of load pressure and a return flow line 1 2 adapted to be connected to the return flow of a pump or other source of fluid. A main valve 1 4 is spring-loaded to yieldingly shut off fluid flow between lines 10 and 12. Main valve 14 is controlled by a bleed flow through a bleed flow orifice 1 8 positioned between pressure line 10 and bleed flow end 1 6 of valve 14, and a variable orifice, more fully described below, formed between bleed flow orifice 1 8 and return flow line 1 2.
A pilot valve 20 controls the bleed flow and thereby the opening of main valve 1 4. Pilot valve 20 includes a pilot piston 22 mounted for movement in a pilot bore 24. Pilot bore 24 includes a pressure end 26 connected to load pressure through line 10, a bleed flow chamber 28 connected to bleed flow end 1 6 of valve 14, a drain chamber 30 connected to return flow, and a spring end 32 also connected to return flow. Pilot piston 22 is yieldingly urged toward pressure end 26 to shut off flow between bleed flow chamber 28 and drain chamber 30 by a spring member 34 positioned in spring end 32 of pilot bore 24.
Main valve 14 is mounted for movement in a main bore 36. Main bore 36 includes a return chamber 38 formed in one end thereof, a load pressure chamber 40 adjacent return chamber 38, a bleed chamber 42 spaced from return chamber 38 by pressure chamber 40, and a control pressure chamber 44 formed at the opposite end of main bore 36.
Return chamber 38 is connected to the return flow through line 1 2 with pressure chamber 40 connected to the load pressure source through line 10, bleed chamber 42 is connected to bleed flow chamber 28 of pilot bore 24 and through bleed flow orifice 1 8 through bleed flow line 46, and control pressure chamber 44 is connected to a source of control pressure through a control line 48.
Main valve 14 includes a main piston 50 mounted for movement in main bore 36.
Main piston 50 is formed with a head end 51 having a tapered portion 52 extending into return chamber 38. Tapered portion 52 is adapted for engagement with a main valve seat 54 formed at the juncture of load pressure chamber 40 and main bore 36. A spring
member 56 yieldingly urges main piston 50
in the direction of return chamber 38 to seat tapered portion 52 in engagement with main
valve seat 54 to shut off fluid flow between
load pressure chamber 40 and return cham
ber 38.
Main piston 50 includes a large area of rear
end 58 and head end 51 contacts valve seat
54 at a diameter less than that of rear end 58
thereby forming a first differential area which
is acted on by fluid pressure in load pressure
chamber 40. The portion of head end 51
extending into return chamber 38 forms a
second differential area which is acted on by fluid pressure in return chamber 38.
Main piston 50 further includes a counter
bore 60 formed in rear end 58 and which together with the walls of main bore 36
define bleed chamber 42. A metering passage
62 formed through head end 51 provides a
path for fluid flow between bleed chamber 42 and return chamber 38.
A poppet type servo valve 64 having a cone shaped end 65 extends from control chamber 44 in the direction of main piston 50 and is yieldingly urged by spring member 56 into seated engagement with metering passage 62 to shut off fluid flow therethrough. Movement of cone shaped end 65 into or out of engagement with metering passage 62 generates a variable orifice therebetween for metering fluid flow between bleed chamber 42 and return chamber 38.
A servo piston 66 associated with servo valve 64 is slidably mounted for movement relative thereto in control chamber 44. Servo piston 66 is yieldingly urged by a spring member 68 to resist movement thereof by control pressure in control chamber 44. Under the urging of control pressure in chamber 44 servo piston 66 acts on servo valve 64 against the force of spring members 56 and 68 to unseat the engagement of the servo valve 64 with metering passage 62.
METERING OPERATION AS A FLOW CON
TROL VALVE
Metered flow, from load pressure to return, will be proportional to the applied control pressure, with this proportionality achieved in the following manner. Control pressure, acting on the exposed area of the servo piston 66, generates a force that moves the servo piston 66 and poppet valve 64 in a direction away from main piston 50 against the force of springs 56 and 68. Motion stops when the spring force becomes equal to the control pressure-generated force. Because the springs have a linear rate, displacement of the servo valve 64 will be proportional to the applied control pressure.
As servo valve 64 moves, it separates from main piston 50 allowing fluid flow through the variable orifice so formed and through metering passage 62 into return chamber 38.
The resulting drop in pressure across metering passage 62 due to the variable orifice reduces the closing force on large area end 58 of
main piston 50 to a lesser value than the opening force developed on the first differential area of piston 50 by the load pressure.
The main piston 50, therefore, will move following the motion of the servo valve 64. As a steady-state condition, the flow area between the servo valve 64 and the variable orifice must result in a bleed flow rate through the variable orifice that develops a closing pressure on large area end 58 of main piston 50 that exactly balances the opening force on the first differential area of main piston 50.
Since the gain ratio between the servo valve motion and bleed chamber 42 pressure is very high, the positional difference between the servo valve 64 and main piston 50 is negligible, and main piston 50 displacement may be considered as being directly proportional to applied control pressure. If the variable metering orifice in the main piston 50 is of constant width, metered flow will be pro portion to piston displacement and to applied control pressure, assuming a cosntant pressure differential between load and return.
OPERATION AS A RELIEF VALVE
If the load pressure exceeds a predetermined "cracking" pressure, the pilot valve 20 will be displaced to open a flow path from the load pressure through bleed flow orifice 18, to return. This bleed flow reduces the pressure and closing force on large area end 58 of the main piston 50, and in the same manner as described above for flow control, the main piston will open, allowing flow from load to return. If load pressure tends to drop below the cracking pressure, pilot valve 20 will close, causing an increase in the pressure and closing force on the main piston 50.
OPERATION AS AN ANTI-CAVITATION
VALVE
in the type of system for which this valve is intended, load pressure may drop below return line pressure as the result of an overrunning load. To prevent cavitation, the valve is designed to open in response to such a pressure differential, allowing fluid flow from the return line into the load pressure line.
If return line pressure in return chamber 38, acting on the second differential area of main piston 50, generates a force exceeding the sum of the forces developed by load pressure acting on an equal area and spring 56, main piston 50 will move away from valve seat 54, opening a flow path from return to load. A free sliding fit between servo piston 66, and servo valve 64 and the use of two springs 56 and 68 allows the closing force exerted by servo valve 64 on main piston 50 to be held to a minimum and, therefore, requiring a relatively small pressure differential to open the main valve 14.Note that if servo valve 64 and servo piston 66 were one piece and only one spring having a force equal to the sum of forces of springs 56 and 68 were used, the other two functions of the valve, as described above, would not be significantly affected, but the higher spring force of the single spring would require a high pressure differential to overcome it and open the valve, such high pressure differential generally being unacceptable.
Fig. 2 shows a preferred embodiment of the hydraulic control circuit of the present invention as a unitary multiple function control valve wherein coresponding elements shown in Fig. 1 are provided with a suffix a.
The control valve circuit of Fig. 1 is shown housed in a body 70 which includes a load pressure passage 1 0a spaced from a return passage 12a. A main bore 36a formed in body 70 extends from return chamber or passage 1 2a through pressure passage 1 0a and terminates at a bearing member 72 held in position in main bore 36a by an end cap 74 portion of body 70. End cap portion 74 of body 70 includes a servo bore 76 spaced from main bore 36a by bearing member 72 and terminates at a distal end 78. A pilot bore 24a is formed in body 70 spaced from main bore 36a and includes a pressure end 26a in communication with and extending transverse of pressure passage 10a, a drain chamber 30a, and a spring end 32a spaced from pressure end 26a by drain flow chamber 30a.
Body 70 further includes a bleed flow passage 46a extending between main bore 36a adjacent bearing member 72 and in communication with pressure end 26a of pilot bore 24a through bleed flow orifice 1 8a adjacent drain chamber 30a, a drain passage 80 interconnecting distal end 78 of servo bore 76 and drain chamber 30a of pilot bore 24a with return passage 12a, and a control passage 48a in communication with servo bore 76 adjacent bearing member 72.
A pilot valve 20a is mounted for movement in pilot bore 24a and is yieldingly urged to shut off fluid flow between bleed flow passage 46a and metered flow passage 80. Pilot valve 20a includes a pilot piston 22a extending through pilot bore 24a between spring end 32a and pressure end 26a. Pilot piston 22a is of two-piece construction and includes a metering section 82 and spring end section 83.
Section 82 is formed with a tapered portion 84 positioned in drain chamber 30a and seats in bore 24a to form a leak-proof seal when system pressure is below the cracking pressure level of the pilot valve. Metering section 82 also includes a shoulder portion 86 extending into pressure end 26a of bore 24a in which one or more metering slots 87 are formed. A reduced diameter portion 88 of metering section 82 spaces shoulder portion 86 from a head portion 90 of metering section 82 defining therebetween a bleed flow chamber 28a and having slots 87 in communication therewith and in which one end of bleed flow passage 46a terminates. Bleed flow chamber 28a is in communication with pressure passage 1 0a through a bleed flow orifice 1 8a formed in head portion 90.
Spring end section 83 is held in abutting relationship with metering section 82 by a spring member 34a and is slightly smaller in diameter than shoulder portion 86 and head portion 90 of metering section 82. The differential area formed by the slight differences in diameters is acted on by load pressure in pressure end 22a generating a force tending to open the pilot valve against the force exerted by spring member 34a.
Spring member 34a is positioned in pilot bore 24a between spring end section 83 and an adjustment member 94 in threaded engagement with body 70. Adjustment member 94 provides a means for varying the amount of compression of spring 34a thereby providing for adjusting the cracking pressure level of the pilot valve.
A main piston 50a is movably mounted in main bore 36a to yieldingly shut off fluid flow between pressure passage 1 0a and return passage 12a. Main piston 50a includes a large area or rear end 58a and a spool section 96 extending from a tapered portion of piston 50a into return passage 1 2a and terminates at a head end 51a. Tapered portion 52a is adapted for seated engagement with a valve seat 54a formed on body 70 at the juncture of pressure passage 1 0a and main bore 36a.
Spool section 96 is formed with a plurality of radial notches 98 terminating adjacent tapered portion 52a. Tapered portion 52a is proportioned for low leakage when in seated enagement with valve seat 54a. When fully closed, poppet action at tapered portion 52a on the valve seat 54a provides a virtually leak proof seal. As tapered portion 52a moves away from valve seat 54a, main piston 50a behaves as a sliding or spool type valve and fluid flow is metered through radial notches 98. By selective dimensioning of the width of radial notches 98, it is possible to control flow gain through the valve as contrasted to a very high flow gain that would result if the main piston was a pure poppet type valve with only poppet action between the main piston and the valve seat.
Fluid pressure in pressure passage 1 0a acts.
on main piston 50a on a first differential area formed by tapered portion 52a contacting valve seat 54a at a diameter less than that of rear end 58a. Fluid pressure in return passage 1 2a acts on a second differential area of main piston 50a formed by the radial surfaces of spool section 96 exposed to the fluid in the return passage.
Main piston 50a further includes a counterbore 60a formed in rear end 58a and a metering passage 62a extending from the bottom of counterbore 60a through spool section 96 into return passage 12a. Counterbore 60a, main bore 36a, and bearing member 72 define therebetween a bleed chamber 42a in main bore 36a which is connected to return passage 1 2a through metering passage 62a and to bleed flow chamber 28a in pilot bore 24a through bleed flow passage 46a.
A servo valve 46a having a stem portion 100 supported for sliding movement in bearing member 72 extends from servo bore 76 through bearing member 72 and terminates in cone shaped end 65a. Cone shaped end 65a is yieldingly urged into engagement with metering passage 62a to shut off fluid flow therethrough by a spring member 77 arranged in bleed chamber 42a between bearing member 72 and a spring seat 104 positioned on stem 100 adjacent cone end 65a.
Movement of cone end 65a into or out of engagement with metering passage 1 2a generates a variable orifice therebetween for metering fluid flow between bleed chamber 42a and return passage 12a.
A servo piston 66a associated with poppet valve 64a is mounted for movement relative thereto in servo bore 76. Servo piston 66a includes a counterbore 106 which together with bearing member 72 and the walls of servo bore 76 define a control pressure chamber 44a in communication with control pressure passage 48a. A relatively light spring member 107 positioned between bearing member 72 and the bottom of counterbore
106 keeps servo piston 66a in contact with a shoulder portion 108 of servo valve 64a and prevents servo piston 66a from blocking passage 48a. Under the urging of control pressure in chamber 44a, servo piston 66a acts to unseat cone end 65a through shoulder portion 108 for controlling the variable orifice metering action of the servo valve 64a.
Note that in this embodiment, spring member 77 combines the functions of springs 56 and 68 shown and described above in relation to Fig. 1. As previously mentioned, the resulting higher spring force limits the use of this embodiment as an anti-cavitation check valve.
One of the features of the control valve is low leakage in the shut off position. The seats between main piston 50a and body 70 and poppet valve 64a and metering orifice 62a can be considered as positive seals with zero leakage. With reasonable tolerances very low leakage rates can be maintained.
Many changes may be made to the above described control valve without departing from the invention.
One such change, by way of example, is shown in Fig. 3 wherein like elements have the same reference numerals as in Fig. 1 with the suffix b added.
Fig. 3 shows a spool type servo valve 108 in place of the servo piston 66 and poppet type servo valve 64 of Fig. 1. Servo valve 108 includes a piston end 110 positioned in control chamber 44b, a spool member 11 2 extending from piston end 110 into and through a bore 114 formed in main piston 50b, and having a metering passage 62b formed therein in communication with return chamber 38b through the end of spool member 11 2 positioned in bore 114. Servo valve 108 is mounted for movement in bore 114 and is yieldingly urged by spring member 68b to shut off fluid flow between bleed chamber 42b and return chamber 38b through metering passage 62b. Servo valve 108 is operable by control pressure applied to piston end 110 for generating a variable orifice as passage 62b is exposed to bleed chamber 42b thereby metering fluid flow through metering passage 62b between bleed chamber 42b and return chamber 38b.
Servo valve 108 has the advantages that system pressure forces have less effect on the spool type valve force balance than on the poppet type valve force balance and movement of servo valve 108 is not required when the circuit is functioning as a relief valve. A disadvantage of the spool type valve, as previously mentioned, is that it is susceptible to leakage through the clearances between bore 114 and spool member 112.
The above-described hydraulic pressure relief circuit is useful in the hydraulic system described in co-pending application No.
(agent's reference A4991 /B).
Claims (11)
1. A hydraulic control valve arrangement comprising: main valve means operable to shut off fluid flow between a source of load pressure and a return flow passage; a bleed flow orifice connected between said source of load pressure and a bleed pressure chamber associated with said main valve means for restricting fluid flow to said bleed chamber; and servo means associated with said main valve means for metering said restricted fluid flow from said bleed chamber, to said return flow passage.
2. A valve arrangement as claimed in claim 1, wherein said main valve means includes a main piston and said servo means comprises a metering passage located in said main piston between said bleed chamber and said return flow line, and a servo element yieldingly urged to shut off fluid flow through said metering passage.
3. A valve arrangement as claimed in claim 2, wherein said servo means includes a servo piston operable from a source of control pressure for controlling said metering action of the servo means.
4. A valve arrangement as claimed in claim 2 or 3, wherein said servo element comprises a servo valve adapted for engagement with said metering passage and wherein movement of said servo valve into or out of engagement with said metering passage in response to said control pressure generates a variable orifice therebetwen.
5. A valve arrangement as claimed in any of claims 2 to 4, wherein said servo valve is a poppet type valve having a cone-shaped end yieldingly urged into seated engagement with said metering passage and wherein movement of said cone-shaped end into or out of engagement with said metering passage generates said variable orifice.
6. A valve arrangement as claimed in claims 3 and 5, wherein said servo piston is slidably mounted for movement relative to said poppet type valve and under the urging of said control pressure acts on said poppet type valve to unseat said cone-shaped end from engagement with said metering passage to generate said variable orifice.
7. A valve arragement as claimed in claim 4, wherein a bore is formed in said main piston between said bleed chamber and said return flow line, and wherein said servo valve is a spool-type valve having said metering passage formed therein in communication with said return flow line and movably mounted in said bore.
8. A valve arrangement as claimed in claim 7, wherein said spool-type valve is operable by said control pressure for generating said variable orifice as said metering passage is exposed to said bleed chamber.
9. A valve arrangement as claimed in claim 1, which also comprises a body having therein said return flow passage and a pressure passage forming said source of load pressure, said body also having therein a main bore extending between said pressure and return passages, a servo bore in aligned relationship to said main bore, a pilot bore spaced from said main bore and in communication with said pressure passage, a bleed flow passage extending from said main bore into said pilot bore, a drain passage extending from said servo bore and said pilot bore to said return passage and a control pressure passage in communication with said servo bore, said bleed flow orifice being positioned in said body between said pressure passage and said bleed flow passage to restrict fluid flow from said pressure passage to said bleed flow passage, and a pilot valve mounted for movement in said pilot bore and yieldingly urged to shut off fluid flow between said bleed flow passage and said drain passage, a metering slot being formed in said pilot valve and being adapted, upon movement of said pilot valve, to meter fluid flow from said bleed flow passage to said drain passage, said main valve means comprising a valve member mounted for movement in said main bore and yieldingly urged to shut off fluid flow between said pressure passage and said return passage and said servo means comprising a metering passage located in said main valve between said bleed flow passage and said return passage, and a servo element movably mounted in said servo bore and extending into said metering passage for generating a variable orifice to meter fluid flow through said metering passage.
1 0. A valve arrangement as claimed in claim 9, wherein said servo element comprises a servo valve and said servo means includes a servo piston mounted in said servo bore in communication with said control pressure passage, said servo piston being operatively associated with said servo valve for controlling said generation of said variable orifice, and said main valve includes a main piston and a bleed chamber, said main piston having said metering passage formed therethrough and said bleed flow chamber being connected to said return passage through said metering passage and to said bleed flow passage through said main bore, and wherein said servo valve is yieldingly urged into seated engagement with said metering passage to shut off fluid flow between said bleed chamber and said return passage, and wherein said servo piston is mounted for movement relative to said servo valve in said servo bore, and wherein under the urging of control pressure applied to said servo piston said servo piston acts on said servo valve to unseat engagement of the servo valve with said metering passage, said servo valve including a stem member having a cone-shaped end adapted for seated engagement with said metering passage, and wherein a first spring member urges said cone-shaped end into engagement with said metering passage, said stem member including a shoulder portion spaced from said cone-shaped end and positioned in said servo bore in abutting relationship with said servo piston and said servo piston acts on said shoulder portion to unseat said cone-shaped end from engagement with said metering passage, and said servo valve further includes a spring seat member adjacent said coneshaped end in said bleed chamber, a first spring member arranged within said bleed chamber in engagement with said first spring member to yieldingly urge said cone-shaped end in seated engagement with said metering passage, and a second spring member arranged in said servo bore in engagement with said servo piston to maintain said servo piston in said abutting relationship with said shoulder portion and prevents said servo piston from blocking communication of said control passage with said servo bore, a first counterbore being formed in said main piston to form part of said bleed chamber, and said spring seat and said first spring member being arranged in said first counterbore, a control pressure chamber being formed in said servo bore adjacent said control pressure passage and a second counterbore being formed in said servo piston to form part of said control pressure chamber, said second spring being arranged in said second counterbore.
11. A hydraulic control arrangement constructed and adapted to operate substantially as herein described with reference to and as illustrated in the accompanying drawings.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/024,058 US4201052A (en) | 1979-03-26 | 1979-03-26 | Power transmission |
US06/117,934 US4365647A (en) | 1980-02-04 | 1980-02-04 | Power transmission |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2047435A true GB2047435A (en) | 1980-11-26 |
GB2047435B GB2047435B (en) | 1983-04-20 |
Family
ID=26697983
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8009962A Expired GB2047435B (en) | 1979-03-26 | 1980-03-25 | Hydraulic control valve system |
Country Status (6)
Country | Link |
---|---|
AU (1) | AU534584B2 (en) |
CA (1) | CA1138740A (en) |
DE (1) | DE3011196A1 (en) |
GB (1) | GB2047435B (en) |
IN (1) | IN154912B (en) |
SE (1) | SE443431B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2123987A (en) * | 1982-07-22 | 1984-02-08 | Petroles Cie Francaise | A safety connection connecting a vessel containing a gas under pressure to a discharge system |
EP0160265A2 (en) * | 1984-04-30 | 1985-11-06 | Vickers Incorporated | Hydraulic control system |
EP1239201A1 (en) * | 2001-03-08 | 2002-09-11 | Bestobell Valves | Valve System |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2706483B2 (en) * | 1988-09-28 | 1998-01-28 | 日立建機株式会社 | Pressure control valve |
FR2668761B1 (en) * | 1990-11-02 | 1996-06-21 | Schlumberger Ind Sa | HYDROCARBON DISPENSING LANCE. |
DE10023583B4 (en) * | 2000-05-13 | 2012-05-24 | Robert Bosch Gmbh | Electrohydraulic lowering module |
CN103791129B (en) * | 2014-02-28 | 2016-05-11 | 昆明中铁大型养路机械集团有限公司 | The traveling control load valve that a kind of closed type hydraulic system drives |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH309289A (en) * | 1951-12-07 | 1955-08-31 | Limited Electraulic Presses | Control valve for hydraulic fluids. |
DE1045755B (en) * | 1956-09-20 | 1958-12-04 | Schloemann Ag | Shut-off and control valve actuated by the pressure medium flowing through and control by an auxiliary slide |
US3411536A (en) * | 1966-07-06 | 1968-11-19 | Koehring Co | Pilot operated control valve mechanism |
DE2424973C3 (en) * | 1974-05-22 | 1980-01-31 | Montan-Hydraulik Gmbh & Co Kg, 4755 Holzwickede | Device for controlling hydraulic drives |
-
1980
- 1980-03-22 DE DE19803011196 patent/DE3011196A1/en active Granted
- 1980-03-25 GB GB8009962A patent/GB2047435B/en not_active Expired
- 1980-03-25 AU AU56826/80A patent/AU534584B2/en not_active Ceased
- 1980-03-25 SE SE8002301A patent/SE443431B/en not_active IP Right Cessation
- 1980-03-25 CA CA000348365A patent/CA1138740A/en not_active Expired
- 1980-09-02 IN IN1003/CAL/80A patent/IN154912B/en unknown
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2123987A (en) * | 1982-07-22 | 1984-02-08 | Petroles Cie Francaise | A safety connection connecting a vessel containing a gas under pressure to a discharge system |
EP0160265A2 (en) * | 1984-04-30 | 1985-11-06 | Vickers Incorporated | Hydraulic control system |
EP0160265A3 (en) * | 1984-04-30 | 1986-02-12 | Vickers, Incorporated | Hydraulic control system |
EP1239201A1 (en) * | 2001-03-08 | 2002-09-11 | Bestobell Valves | Valve System |
Also Published As
Publication number | Publication date |
---|---|
AU534584B2 (en) | 1984-02-09 |
SE8002301L (en) | 1980-09-27 |
DE3011196A1 (en) | 1980-10-09 |
CA1138740A (en) | 1983-01-04 |
GB2047435B (en) | 1983-04-20 |
IN154912B (en) | 1984-12-22 |
AU5682680A (en) | 1980-10-02 |
SE443431B (en) | 1986-02-24 |
DE3011196C2 (en) | 1993-04-29 |
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Date | Code | Title | Description |
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PE20 | Patent expired after termination of 20 years |
Effective date: 20000324 |