Transfer valve system

Information

  • Patent Grant
  • 6823669
  • Patent Number
    6,823,669
  • Date Filed
    Wednesday, April 2, 2003
    21 years ago
  • Date Issued
    Tuesday, November 30, 2004
    20 years ago
Abstract
A hydraulic transfer valve system has a main valve selectively placing one of a primary and secondary hydraulic system in communication with a hydraulic load. A pilot valve provides a toggling action between the primary and secondary systems with respect to pressure changes in such systems.
Description




BACKGROUND OF THE INVENTION




(1) Field of the Invention




This invention relates to hydraulics, and more particularly to transfer valve systems for aircraft hydraulics




(2) Description of the Related Art




In an aircraft, a transfer valve (also known as a switching valve) is used to direct pressure and flow from one of two available hydraulic supply systems to a downstream circuit. The valve switches between supply systems based on the relative magnitudes of the system pressures and a pressure bias built into the valve. The bias is often achieved by providing different pilot areas on each end of the valve, the larger of the pilot areas being on the end acted upon by the preferred, or primary, system. A spring is also sometimes used to provide a bias. With both supply pressures at normal operating pressure, the forces acting on the valve are such that the preferred (primary) system is connected to the circuit and the other (secondary/back-up) system is blocked. The purpose of a transfer valve is to allow the back-up system to take over for a failed or failing primary system. The transfer valve also isolates one hydraulic supply system from the other. As the primary system pressure decays, the force balance on the valve favors the primary system less and the back-up system more, until eventually the valve shuttles from the initial primary position to the back-up position. In the back-up position the valve connects the back-up system to the circuit and blocks the primary system.




Once pressures reach the switchover condition, the transfer valve advantageously shuttles with a snapping action, without interruption, hesitation, or instability. The snapping action is advantageous for two reasons. First, it minimizes transient pressure spikes as the valve closes off flow from one system and opens flow from the other. Second, it prevents the forces acting on the valve from achieving equilibrium when the valve is mid travel. If the valve stops mid travel it could block both supply systems and create a hydraulic lock in the downstream circuit. This snapping action can be enhanced through the use of a mechanical, hydraulic or electric detent mechanism.




Two well known styles of transfer valve are solenoid-operated and pressure-operated valves. Solenoid-operated transfer valves provide a high degree of control. The transfer valve can be switched from one system to the other by energizing and dc-energizing the solenoid. Because the solenoid controls when the valve shuttles, this design does not require a detent mechanism. This approach is generally relatively complicated and requires a suitable electronic computer or system to control the solenoid. In addition to the computer system, some means of sensing pressure is required. Because this approach is more complicated, it requires a higher level of redundancy and is generally more expensive.




Pressure-operated valves shuttle based on the relative pressures of the two supply systems and the pressure bias and detent action designed into the valve. This style or transfer valve may require no inputs from other devices. Pressure-operated transfer valves may make use of a hydraulic or mechanical detent to achieve the desired valve behavior. With a mechanical detent, a mechanism holds the valve in position until sufficient shuttling force is developed to overcome the detent. Once the detent is overcome, the valve moves away from the detent and the detent force no longer acts to hold the valve in position. With the detent force suddenly removed, the forces acting on the valve are no longer in equilibrium and the valve shuttles with a deliberate motion. Mechanical detents are typically spring-loaded devices. The mechanical detent may introduce friction and side loads on the valve spool, both of which have a negative effect on the valve's switching characteristic.




BRIEF SUMMARY OF THE INVENTION




Accordingly, one aspect of the invention involves a hydraulic transfer valve system for coupling one of primary and secondary hydraulic systems to a hydraulic load. The hydraulic systems each have a source and a return and the load has an input and a return. The system has first and second valves and a passageway coupling the first valve to the second valve and having first and second ports at the first and second valves, respectively. The first valve has a first condition in which it provides communication between the primary hydraulic system source and the hydraulic load input, provides communication between the primary hydraulic system return and the hydraulic load return, blocks communication between the secondary hydraulic system source and the hydraulic load input, provides communication between the secondary hydraulic system return and the hydraulic load return, and blocks the passageway first port. The first valve has a second condition in which it provides communication between the secondary hydraulic system source and the hydraulic load input, provides communication between the secondary hydraulic system return and the hydraulic load return, blocks communication between the primary hydraulic system source and the hydraulic load input, provides communication between the primary hydraulic system return and the hydraulic load return, and does not block the passageway first port. The second valve has a first condition in which it blocks the passageway second port and a second condition in which it does not block the passageway second port and herein, with the first valve in its second condition, the passageway permits a flow from the primary hydraulic system source to the primary hydraulic system return.




In various implementations the valves may be sliding spool valves. The valves may be spring-biased in a direction from their second conditions to their first conditions. Pressure from the primary hydraulic system source may bias the valves in the directions from their second conditions to their first conditions. Pressure from the secondary hydraulic system source may bias the valves in directions from their first conditions to their second conditions. With the valves in their first conditions, a recirculating flow from the secondary source to the secondary return may be permitted through the second valve. A pressure sensor may be coupled to the second valve and output a signal indicative of a pressure in the secondary hydraulic system.




Another aspect of the invention involves a hydraulic transfer valve system with means for piloting a first valve so that with primary and secondary hydraulic systems initially operating normally and the first valve in its first condition, a decrease in a pressure of the primary hydraulic system source relative to the secondary hydraulic system source causes the first valve to toggle to its second condition. With the secondary hydraulic system initially operating normally and the primary hydraulic system source initially operating with an insufficient pressure and the first valve in its second condition, a sufficient increase in the pressure of the primary hydraulic system source relative to the secondary hydraulic system source causes the first valve to toggle to the first condition.




The details of one or more embodiments of the invention are set forth in the accompanying drawings and the description below. Other features, objects, and advantages of the invention will be apparent from the description and drawings, and from the claims.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a partially schematic view of a transfer valve system in a normal operating condition.





FIG. 2

is a partially schematic view of the system of

FIG. 1

in an intermediate condition before switching to backup operation.





FIG. 3

is a partially schematic view of the system of

FIG. 1

in a backup condition.





FIG. 4

is a partially schematic view of the system of

FIG. 1

in an intermediate condition before returning to normal.











Like reference numbers and designations in the various drawings indicate like elements.




DETAILED DESCRIPTION





FIG. 1

shows a transfer valve system


20


coupling a hydraulic load or circuit


22


to primary and secondary hydraulic systems


24


and


26


. The circuit


22


has an input


30


for receiving hydraulic fluid from an engaged one of the systems and a return


31


for returning fluid to such engaged system. The primary system.


24


has a source


32


and a return


33


. The secondary system


26


has a source


34


and a return


35


. The system sources and returns may respectively be coupled to associated pumps and reservoirs (not shown). The transfer valve system


20


includes a main valve


40


and a pilot valve


42


. In the exemplary embodiment, both valves are spool-type valves having spools


44


and


46


and pistons


48


and


50


. The spools are mounted for reciprocal motion within sleeves or cylinders


52


and


54


. Likewise, the pistons are mounted for reciprocal movement in sleeves or cylinders


56


and


58


at proximal ends of the associated spool cylinders


52


and


54


. Springs


60


and


62


extend from the opposite ends of the piston cylinders and into the associated pistons to bias the pistons toward their associated spools.





FIG. 1

shows a normal operating condition of the system


20


. In this condition, the system input


30


and return


31


are respectively coupled to the primary source


32


and primary return


33


. Both valve pistons are in relatively distal positions. In this condition, a conduit branch or passageway


70


, communicating with the primary source


32


, has a port on the main spool cylinder


52


at the proximal end of an annular chamber or cavity


72


of the spool


44


. A conduit


74


leading to the circuit input


30


has a port on the cylinder


52


at the distal end of that chamber. Thus the circuit input


30


communicates with the primary source


32


via the annular chamber


72


. Additional conduits


76


and


78


communicating with the primary source


32


provide communication between the primary source


32


and proximal volumes


80


and


82


of the piston cylinders


56


and


58


. A restriction


83


(described below) is located in the conduit


76


at an inlet to the volume


80


. In the normal condition, pressure from the primary source


32


acting on the pistons


48


and


50


along with the compression force of the associated springs


60


and


62


biases each piston toward its distal position. A conduit


84


in communication with the circuit return


31


has a port on the cylinder


52


near a proximal end thereof and in communication with a distal headspace


86


of the cylinder


56


in the normal condition. A conduit


88


in communication with the primary return


33


has a port on the cylinder


56


also communicating with the headspace


86


. Thus normal condition communication between the circuit return


31


and primary return


33


is via the headspace


86


.




Adjacent the annular chamber


72


, the lands


100


and


102


of the spool have smaller annular chambers


104


and


106


communicating with a central proximal compartment


108


within the spool by associated ports or apertures. The compartment


108


is vented to the headspace


86


via an aperture


110


near the proximal end of the compartment


108


. In operation, high pressure leakage out of the chamber


72


will be vented into the compartment


108


via the chambers


104


and


106


and then passed to the headspace


86


via the aperture


110


. This helps isolate the flow within the primary system and prevents leakage and cross-communication between the primary and secondary systems. Similar features (discussed below) are provided for the secondary system. A conduit


120


communicating with the secondary source


34


has a port on the cylinder


52


at a proximal end of an annular chamber


122


located immediately distally of the land


102


. A conduit


124


communicating with the secondary return


35


has a port in the cylinder


52


at an annular chamber


126


located distally of the chamber


122


and separated therefrom by a land


128


. In the normal condition of

FIG. 1

, the chambers


122


and


126


are not in communication with any other ports on the cylinder


52


. A conduit


130


communicating with the circuit return


31


has a port on the cylinder


52


. This port and thus the conduit


130


is normally blocked by the land


128


. Annular channels


132


and


134


immediately distally and proximally of the chamber


122


respectively in the lands


102


and


128


communicate with a central distal compartment


136


of the spool


44


via associated apertures. The distal compartment


136


communicates with the chamber


126


and thus with the secondary return


35


. Accordingly, secondary source leakage from the chamber


122


passes through the chambers


132


and


134


and into the compartment


136


to return to the secondary return


35


via the chamber


126


so as to, thereby, isolate the secondary system.




Conduits


140


and


142


in communication with the secondary source


34


have ports at the respective distal headspaces of the spool cylinders


52


and


54


. The exemplary spool cylinders are of smaller diameter and cross-section than their associated piston cylinders. Pressure from the secondary source


34


acting on the headspaces


144


and


146


produces a smaller counterforce than the force from the primary source


32


on the volumes


80


and


82


(which primary source force is also augmented by the relatively small associated spring force). In the normal condition this pressure balance maintains the piston distal ends contacting the associated spool proximal ends and maintains the spools at distalmost positions determined by stop shoulders


148


and


150


separating a wall surrounding the normal condition headspaces


144


and


146


from main body portions of the cylinders


52


and


54


.




In the exemplary embodiment, the distal end


152


of the primary spool


44


is sealed. The pilot spool


46


has a passageway


160


extending through its distal end


161


and communicating with a distal annular chamber


162


between a distal end land


163


and an adjacent land


164


via a port in the spool. At a distal end of the chamber


162


, a conduit


165


in communication with the secondary return


35


has a port on the cylinder


54


. In the normal condition, the passageway


160


permits a recirculating flow of fluid from the secondary source


34


to the secondary return


35


. A constriction


166


is located within the passageway


160


to limit the rate of the recirculating flow. At a proximal end of the chamber


162


, a conduit


168


has a port on the cylinder


154


and provides communication with a pressure sensor


170


. In this normal operating condition, the pressure sensor


170


thus outputs a signal indicative of the operating pressure of the secondary system. If the secondary system were to fail or otherwise shutdown, the pressure sensor


170


would provide an indication of the associated pressure drop.




A number of additional conduits are inoperative or less relevant in the normal operating condition. A conduit


180


in communication with the secondary return


35


has a port on the cylinder


54


at an annular chamber


182


separated from the chamber


162


by the land


164


. The conduit


180


provides a return path for leakage over the land


164


from the chamber


162


. To minimize leakage/contamination it may be advantageous that source pressure from one system not be adjacent to a return of the other in any of the valves. A conduit


190


has a port at the main piston cylinder headspace


86


and a port on the pilot spool cylinder


54


at an annular chamber


192


located proximally of the chamber


182


and separated therefrom by a land


194


. A conduit


196


has a port on the cylinder


54


at the chamber


192


and a port at the headspace


198


of the pilot piston cylinder


58


. In the normal operating condition, the conduits


190


and


196


serve to expose the pilot piston cylinder headspace


198


to the pressure of the primary return


33


. A conduit


200


having a restriction


202


has a port on the main piston cylinder


56


. In the normal condition, this port is blocked (just barely overlapped) by a proximal land


204


separated by a chamber


206


from a distal land


208


. The piston


48


has apertures


210


providing communication between a volume


80


and the chamber


206


. The conduit


200


has a second port, at its opposite end, on the pilot spool cylinder


54


. In the normal condition, this port is blocked (just barely overlapped) by a proximal land


212


of the spool


46


adjacent the chamber


192


.




In a failure of the primary system, the pressure of the primary source will drop. The nature of the drop will depend upon the nature of the failure. For example, a normal operational pressure of the sources may be in the vicinity of 4000 psi. As the primary source pressure begins to drop, the distal biasing force from primary system fluid in the chambers


80


and


82


will drop. The valve geometries and spring forces are such that this has a greater initial impact in the pilot valve than in the main valve. At a moderate reduction in pressure (e.g., from 4000 psi down to 3500 psi) the proximally-directed forces on the piston


50


(including the force from the secondary source acting on the spool


46


in the headspace


146


) is sufficient to overcome the distally-directed forces (including those from the primary source and spring


62


). Over a very small further pressure drop, the pilot valve shuttles proximally to the condition of

FIG. 2

with the piston


50


and spool


46


in proximal positions. In these positions, the valve condition is such that the distal land


163


blocks the port of the conduit


164


and the proximal land


212


is clear of the pilot piston cylinder port of the conduit


200


so that the conduits


190


,


196


, and


200


all communicate with the chamber


192


. In this condition, the main piston cylinder port of the conduit


200


is still blocked by the proximal land


204


of the piston


48


. In this condition, the secondary recirculating flow through the conduit


164


is blocked. This interruption may initially cause a slight increase in the pressure from the secondary source


34


as measured by the sensor


170


. This pressure increase is also felt in the headspace


144


of the main spool cylinder. This pressure increase, along with any further decrease in primary source pressure (e.g., below 2,530 psi) will cause the primary spool and piston to be shifted slightly proximally so that the land


204


begins to underlap the main piston cylinder port of the conduit


200


. This port opening provides a venting of primary fluid from the chamber


80


through the apertures


210


and annular chamber


206


and into the conduit


200


. From the conduit


200


, this flow passes through the annular chamber


192


, through the conduit


190


and through the headspace


86


and conduit


88


to the primary return


33


. This flow contributes to a sharp drop in the pressure difference across the piston


48


. The resulting force imbalance from the pressure drop causes the primary piston to rapidly shuttle to a distalmost position of

FIG. 3

with the primary spool following. This final shuttling of the main spool


44


makes the switch between primary and secondary systems. During the shuttling, the land


100


blocks the main spool cylinder port of the conduit


84


to block communication between the primary return


33


and circuit return


31


. An initial substage of this shuttling also causes the land


102


to block the main spool cylinder port of the conduit


74


thus blocking communication between the circuit input


30


and the primary source


32


. In a final substage of this shuttling to the distalmost position, the land


102


again underlaps the main spool cylinder port of the conduit


74


establishing communication between that conduit and the annular chamber


122


which remains in communication with the conduit


120


. This establishes communication between the system input


30


and secondary source


34


via the chamber


122


. Similarly, in this final substage the land


44


will underlap the main spool cylinder port of the conduit


130


establishing communication between the conduit


130


and the annular chamber


126


which remains in communication with the conduit


124


. Thus this substage also establishes communication between the circuit return


31


and the secondary return


35


via the annular chamber


126


. With the secondary hydraulic system


26


thus active, flow from the secondary hydraulic system


26


to the circuit


22


will slightly decrease the pressure measured by the sensor


170


. In this condition, if there is residual pressure in the primary hydraulic system


24


there can be a recirculating flow through the main piston


48


, pilot spool cavity


192


, and main cylinder headspace


86


.




Should full functioning of the primary hydraulic system


24


be reestablished, the exemplary implementation provides for toggling back to use of the primary system. As primary system pressure increases, initially the flow through the piston apertures


210


prevents this pressure change from shuttling the primary valve distally. Thus, although the primary valve shuttled to its distal position after the pilot valve shuttled, it does not shuttle back before the pilot valve does. As the primary source pressure increases to a threshold value (e.g. an exemplary 2930 psi) the pressure balance on the pilot valve permits the pilot valve piston and spool to shuttle back to their initial distal positions (FIG.


4


). This shuttling, inter alia, causes the pilot spool proximal land


212


to overlap the associated port of the conduit


200


thereby terminating the recirculating flow of the primary system through the piston apertures


210


. This termination can further increase primary system pressure. Additionally, the shifting of the pilot spool reestablishes flow through the conduit


164


, slightly decreasing pressure in the secondary system. These pressure changes along with a further increase in primary source pressure and along with any associated drop in the pressure at the headspace


86


, cause the primary valve piston and spool to rapidly shuttle back to their distal positions of

FIG. 1

breaking communication between the secondary hydraulic system


26


and the circuit


22


and establishing communication between the primary hydraulic system


24


and the circuit


22


.




Accordingly, it is seen that the exemplary system provides a two-way toggling of the operation of the main valve: both in transferring from the primary system to the secondary system and in transferring back to the primary system.




The pressure sensor or switch


170


may advantageously be used to detect latent failures of the pilot valve. If the pilot valve were stuck, the transfer valve might continue to operate, although not at proper pressure thresholds and the aircrew or control system would be otherwise unaware of the failure. The state of the sensor may be periodically checked during a flight or mission to determine that the pilot valve is in the appropriate position. The sensor may be checked during preflight operations when the secondary system is pressurized and the primary system is not. Under these conditions, the pilot valve should be positioned that it blocks the connection to return, causing the sensor to be pressurized. In flight, the pilot valve should be positioned such that it opens the connection to return, causing the sensor to be unpressurized. The value at which the sensor trips may not be particularly critical as it may behave like a binary on-off switch. The size/geometry of the orifice


166


substantially determines the flow through the secondary system when the secondary system is inactive. This may be dictated or influenced by the performance characteristics of the secondary system. The relationship (e.g., size ratio) between the orifices


83


and


202


substantially determines the pressure at which the transfer valve shuttles in the event of a failed (e.g., jammed) pilot valve. The orifices


83


and


202


in series determine the inactive primary system flow, similar to the role of the orifice


166


for the secondary system. In operation, it is anticipated that the spool and piston of each valve will maintain their engagement to each other and thus may be further integrated. The geometry and spring bias will advantageously be such that under no anticipated conditions will return pressure transients be large enough to cause spool/piston separation. The two-piece construction aids maufacturability.




The relationship between: (a) the ratio of (i) the cross-sectional area of the pilot valve piston acted upon by the primary system pressure to (ii) the cross-sectional area of the pilot valve spool acted upon by the secondary pressure; and (b) the ratio of (i) the cross-sectional area of the main valve piston acted upon by the primary system pressure to (ii) the cross-sectional area of the main valve spool acted upon by the secondary system pressure will influence the shuttling action of the primary valve. The former should be smaller than the latter. This causes the pilot valve to shuttle first so as to give the transfer valve an advantageous snapping detent action characteristic when shuttling from primary to secondary systems. For example, at exemplary normal operating source pressures of 4000 psi (and return pressures essentially zero), the valves may be configured so that the initial shuttle of the pilot occurs when the primary source pressure drops to a first threshold in the range of 2200-3200 psi (55-80% of normal), more narrowly 2700-3000 (67.5-75%) psi. The main may then shuttle at a lower pressure in the range of 1700-2600 psi (42.5-65%), more narrowly 2300-2500 psi (57.5-62.5%). A resumption in primary source pressure may shuttle the valves back nearly simultaneously at one or more thresholds in the range of 2700-3400 psi (67.5-85%), more narrowly 2900-3100 psi (72.5-77.5%). If the pilot is jammed in its second position, the main may shuttle back as a somewhat higher pressure in the range of 2800-3500 psi (70-87.5%), more narrowly 3200-3500 psi (80-87.5%). With another normal pressure (e.g., 3000 psi), the shuttling pressures could be at similar percentages.




One or more embodiments of the present invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the invention. For example, if applied as a redesign or retrofit of an existing transfer valve system, various features of the existing system may influence the implementation. Accordingly, other embodiments are within the scope of the following claims.



Claims
  • 1. A hydraulic transfer valve system for coupling one of primary and secondary hydraulic systems, each having a source and a return, to a hydraulic load having an input and a return, the hydraulic transfer valve system comprising:a first valve; a second valve; and a passageway coupling the first valve to the second valve and having first and second ports at said first and second valves, respectively, the first valve having: a first condition in which the first valve: provides communication between the primary hydraulic system source and the hydraulic load input; provides communication between the primary hydraulic system return and the hydraulic load return; blocks communication between the secondary hydraulic system source and the hydraulic load input; provides communication between the secondary hydraulic system return and the hydraulic load return; and blocks the passageway first port; and a second condition in which the first valve: provides communication between the secondary hydraulic system source and the hydraulic load input; provides communication between the secondary hydraulic system return and the hydraulic load return; blocks communication between the primary hydraulic system source and the hydraulic load input; provides communication between the primary hydraulic system return and the hydraulic load return; and does not block the passageway first port; and the second valve having; a first condition in which the second valve blocks the passageway second port; and a second condition in which the second valve does not block the passageway second port and wherein with the first valve in its second condition, the passageway permits a flow from the primary hydraulic system source to the primary hydraulic system return.
  • 2. The hydraulic transfer valve system of claim 1 wherein:the first valve is a sliding spool valve; and the second valve is a sliding spool valve.
  • 3. The hydraulic transfer valve system of claim 1 wherein:the first valve is spring-biased in a direction from its second condition to its first condition; and the second valve is spring-biased in a direction from its second condition to its first condition.
  • 4. The hydraulic transfer valve system of claim 1 wherein:pressure from the primary hydraulic system source biases the first valve in a direction from its second condition to its first condition; pressure from the primary hydraulic system source biases the second valve in a direction from its second condition to its first condition; pressure from the secondary hydraulic system source biases the first valve in a direction from its first condition to its second condition; and pressure from the secondary hydraulic system source biases the second valve in a direction from its first condition to its second condition.
  • 5. The hydraulic transfer valve system of claim 1 wherein:with the first valve in its first condition and the second valve in its first condition, a recirculating flow from the secondary source to the secondary return is permitted through the second valve.
  • 6. The hydraulic transfer valve system of claim 1 further comprising a pressure sensor coupled to the second valve and outputting a signal indicative of a pressure in the secondary hydraulic system.
  • 7. A hydraulic transfer valve system for coupling one of primary and secondary hydraulic systems, each having a source and a return, to a hydraulic load having an input and a return, the hydraulic transfer valve system comprising:a first valve; a second valve; and a passageway coupling the first valve to the second valve and having first and second ports at said first and second valves, respectively, the first valve having: a first condition in which the first valve: provides communication between the primary hydraulic system source and the hydraulic load input; provides communication between the primary hydraulic system return and the hydraulic load return; blocks communication between the secondary hydraulic system source and the hydraulic load input; and provides communication between the secondary hydraulic system return and the hydraulic load return; and a second condition in which the first valve: provides communication between the secondary hydraulic system source and the hydraulic load input; provides communication between the secondary hydraulic system return and the hydraulic load return; blocks communication between the primary hydraulic system source and the hydraulic load input; and provides communication between the primary hydraulic system return and the hydraulic load return; and at least one of the first and second valves having means for piloting the first valve so that: with the primary and secondary hydraulic systems initially operating normally and the first valve in the first condition, a decrease in a pressure of the primary hydraulic system source relative to the secondary hydraulic system source causes the first valve to toggle to the second condition; and with the secondary hydraulic system initially operating normally and the primary hydraulic system source initially operating with an insufficient pressure and the first valve in the second condition, a sufficient increase in the pressure of the primary hydraulic system source relative to the secondary hydraulic system source causes the first valve to toggle to the first condition.
  • 8. The hydraulic transfer valve system of claim 7 wherein:the means are configured so that: said decrease causes said second valve to shift from a first condition to a second condition at a first threshold pressure between 2200 and 3200 psi; and said decrease causes said first valve to shift from its first condition to its second condition at a second threshold pressure, less than the first threshold pressure and between 1700 and 2600 psi.
  • 9. The hydraulic transfer valve system of claim 8 wherein:said first threshold pressure is between 2700 and 3000 psi; and said second threshold pressure is between 2300 and 2500 psi.
  • 10. The hydraulic transfer valve system of claim 8 wherein the means are configured so that:said increase causes both the first and second valves to shift to their first conditions at one or more third threshold pressures between 2700 and 3400 psi.
  • 11. The hydraulic transfer valve system of claim 10 wherein said one or more third threshold pressures between 2900 and 3100 psi.
  • 12. The hydraulic transfer valve system of claim 8 wherein the means are configured so that if the second valve is jammed in its second condition:said increase causes the first valve to shift to its first condition at a third threshold pressure, greater than the first threshold pressure, and between 2800 and 3500 psi.
  • 13. The hydraulic transfer valve system of claim 8 wherein said third threshold pressure is between 3200 and 3500 psi.
  • 14. The hydraulic transfer valve system of claim 7 wherein:the means are configured so that: said decrease causes said second valve to shift from a first condition to a second condition at a first threshold pressure between 55 and 80% of a normal operating pressure of at least one of the primary and secondary hydraulic systems; said decrease causes said first valve to shift from its first condition to its second condition at a second threshold pressure, less than the first threshold pressure and between 42.5 and 62.5% of said normal operating pressure; said increase normally causes both the first and second valves to shift to their first conditions at one or more third threshold pressures between 67.5 and 85% of said normal operating pressure; and if the second valve is jammed in its second condition said increase causes the first valve to shift to its first condition at a fourth threshold pressure, greater than the first threshold pressure, and between 70 and 87.5% of said normal operating pressure.
US Referenced Citations (4)
Number Name Date Kind
3791775 Bochnak et al. Feb 1974 A
3913324 Miller et al. Oct 1975 A
4164119 Parquet Aug 1979 A
6173728 Venable et al. Jan 2001 B1