1. Field of Invention
The present invention relates to safety valves for use in full operational hydraulic systems and sub-systems.
2. Discussion of Relevant Prior Art
Hydraulic hose and line failures in the field create an extreme hazard for operators, work crews and the environment. Injuries resulting from hydraulic lines breaks happen almost daily. Although various shut off fuses exist, none of the current designs provide a reliable and cost effective method of shutting off fluid flow when a line break occurs.
Velocity fuses are currently used for emergency shut off of fluid flow within cylinder systems. They work by sensing flow across a control orifice. When the pressure differential within the system exceeds a predetermined range, a spring biased poppet or spool closes, shutting flow to the damaged hydraulic circuit. This provides for limited protection, as the load may be protected from free falling, but the system pump is still running. Under this condition the pump continues to push high pressure fluid into atmosphere until either the machine is turned off, or pump destroys itself from lack of lubrication. A significant amount of fluid may already be lost and damage done to the operators and/or equipment. Because of this and other limitation, conventional velocity fuses are not practical as safety valves on the supply pressure side of hydraulic circuit that delivers flow to the whole operational system. Accordingly, a great need exists for a safety valve that can shut off the supply of pressurized fluid, air, water, or steam to the sub systems that has a catastrophic event where a ruptured component is venting to atmosphere.
The present invention is directed to a safety valve for use either immediately downstream from a hydraulic power pump and safety relief valve on the pressure supply line before the operational control valves or in working subsystems. This invention eliminates the need for expensive electronic feedback, flow, and pressure devices, by using the natural physics of fluid pressure and flow characteristics. Unlike velocity fuses currently known in the art, the valve of the present invention is not affected by flow rates or by hydraulic control valves with tandem or open center positions. Furthermore, the present invention will continue to allow flow even if the system is in a neutral position.
More specifically, the present invention is directed to a safety shut off valve comprising a velocity fuse coupled with a surge chamber, return line or a surge chamber wherein a constant back pressure is maintain with a return line. When used within a system, fluid flows through the fuse and into the adjacent surge chamber before exiting into the rest of the system. The chamber acts as an accumulator of fluid. This accumulation controls and changes the orientation of flow thus increasing differential pressure on surface of the velocity fuse which is enough to keep the fuse from prematurely shutting off during normal fluctuations in system flow. As a result, the fuse within the valve will not close until a catastrophic line rupture causes an increase in differential pressure through the drop in the chamber volume.
Furthermore, maintaining a back pressure in a return line flow downstream of subsystem, ensures that the accumulate volume and pressure within the chamber or directly against the velocity fuse will maintain the differential pressure on the surface of the spool thereby keeping the velocity fuse in an open position
The return line flow throttle can be changed in shape and size to facilitate the desired differential pressure in system. This differential load or resistance can be adjustable in shape and size through manufacturing or controlled by air, mechanical, electrical, pilot operation, by design or manually but not limited to these alone shown.
Referring now to
The velocity fuse chamber 20 is defined by chamber inlet 22 and chamber outlet 24. The chamber diameter is predetermined by the system requirements. A spool 26 having a positioning end 28 and a valve end 30 is aligned within the fuse chamber 20 so that the valve end 30 will close off the fuse chamber outlet 24 when the velocity fuse 12 is in a closed position. The spool 26 is of a diameter and length that will allow the spool 26 to slide within the fuse chamber 20 in accordance with the requirements of the system. A compression spring 32 is positioned between the valve end 30 of the spool 26 and the fuse chamber outlet 24. As fluid exits the velocity fuse chamber 20 through fuse chamber outlet 24, it enters a surge accumulator 34 via connecting port 36.
Fluid flowing through the connecting port 36 enters the accumulator 34 through a surge chamber inlet 38, and exits the accumulator 34 through a surge chamber outlet 40 which empties back into the system through valve outlet port 42. The accumulator 34 acts to disrupt and slow the flow of the fluid through the system, thereby providing a backpressure against the velocity fuse 12. As a result, normal pressure surges created during the normal operation if the hydraulic system which would typically result in a closure of a conventional velocity valve, will be damped by the backpressure created by the accumulator 34. The size and shape of the accumulator 34 will vary and will be determined by the pressure differential requirements for each system. Furthermore this differential back pressure is aided by resistance created in return line flow line, see
Referring now to
Nomenclature
Δ PGeneral Pressure differences
ΔPDV Pressure drop across the directional valve
ρw (Fluid) Water density
A General area
A1 Projected area at the upstream side of the spool
A12 Fixed restricted area between upstream side of the spool and the spring chamber
Λ2 Projected area at the downstream side of the spool
Λ23 Variable restricted area at the entrance of the surge chamber
Λ3 Spool face projected area when the spool advancing in the entrance hole of the surge chamber
A34 Fixed restricted area at the outlet of the surge chamber
Ath Throttling area of the tank line throttle
B Fluid bulk Modulus
Cd Discharge coefficient
DSL1 Sleeve geometrical diameter
DSL2 Sleeve geometrical diameter
DsL3 Sleeve geometrical diameter
DSP1 Spool geometrical diameter
DSP2 Spool geometrical diameter
DSP3 Spool geometrical diameter
DSP4 Spool geometrical diameter
P5 (PPump) Back pressure before tank line throttle
Pco Relief valve dead head pressure
PCR Relief valve cracking pressure
PRL Pressure equivalent to the external load
Q General Flow rate
Q34 Flow from surge chamber to the system
QP Flow source (from the pump)
QRV Flow through the relief valve
QSV Flow into surge chamber from the spring chamber
Qth Flow through tank line throttle valve
S (Smax) Instantaneous (maximum) spool displacement
S′ Spool velocity
S″ Spool acceleration
SG Fluid specific gravity
Vs Volume of the surge chamber
Xmax Spring maximum (Free) length
If the spool face 27 is blocking the entrance of connecting port 36 the variable orifice is considered closed. If the spool face 27 is completely out of contact with the entrance connecting port 36 the variable orifice is considered open.
The following very well know equation will be used to describe the nonlinear relation between the differential pressure across any sharp-edged short orifice and the flow rate passing through it.
Q=C
d
A(2ΔP/SG*ρw)1/2
This equation can be mathematically manipulated and rewritten to get one constant using as follows.
Q[gpm]=22.85×A[in2] (ΔP [psi]/SG)1/2
This can be used to find the differential pressure in terms of the flow rate.
Δ P [psi]=SG×Q2[gpm]2/22.85×A2[in2]2
By applying this equation on the return tank line throttle and neglecting the flow resistance in the hydraulic line between the throttle and the tank, pressure P5 is found as follows.
P
5
=SG×Q
th
2/22.852×Ath2
Fluid flow through the tank line throttle equals the safety valve 10 flow QSV in this case and if a hydraulic motor is used. If a differential cylinder is used, ratio must be considered in calculating the return flow.
The tank line throttling area is a simple variable circular area function of the throttle diameter as follows.
A
th
=πD
2
th/4
Pressure in the fuse chamber 20 is calculated by the following equation, P2=P3+(SG×QSV2)/(22.852×A232) wherein A23 is the throttling area between the fuse chamber and surge volume.
The return line throttle 41 is considered to be any controlled, uncontrolled, or design feature that creates for the purpose of operation control of any type which valve operates on such needed restriction or back pressure. This is by no means the only way to create back pressure and can be created for reasons of control. Mechanical, electrical, air, pilot pressure, may be used as may other methods internal or external.
During a line rupture, load pressure suddenly is released to the atmospheric pressure and the pressure in the return line becomes zero. Consequentially, the safety valve 10 immediately shuts off supply pressure upstream wherever it is located in system, as discussed above. In this condition, a surge flow is developed at the upstream side of the valve spool 10 and drives it to reach its saturation limit and shuts off the pump flow supply line. Accordingly, pump pressure increases to the relief valve setting. This protects pump, personal, equipment, and environment. In some circumstances it may not be necessary for a return line throttle, as the internal resistance of return line can be designed for optimized operation. In such a case, safety valve 10 is then kept open as in normal pump unloading conditions using the surge chamber and the tank line pressure optimized to achieve this situation.
Once operating pressure is removed from valve 10, the spring 32 returns spool 26 back to its beginning position normal operation by such spring 32. Once a line break is repaired the safety valve 10 has already reset itself to normal operating position without any need of adjustment.
In use, the safety valve 10 is able to remain open in steady state loading conditions and unloading conditions. When the load pressure suddenly drops to atmospheric pressure (a state simulating a line rupture), a surge flow is developed at the upstream side of the spool that drives it to reach its saturation limit and shutoff the pump flow.
Any velocity fuse can be used if the differential pressure is maintained by either the accumulator chamber 34 or the restrictor line. Preferably, the accumulator chamber 34 is used in combination with the restrictor line.
While we have shown and described the preferred embodiments of my invention, it will be understood that the invention may be embodied otherwise than as herein specifically illustrated or described, and that certain changes in form and arrangement of parts and the specific manner of practicing the invention may be made within the underlying idea or principles of the invention.
This application is a continuation in part of U.S. patent application Ser. No. 11/836,302 which claims priority of U.S. Provisional Patent Application No. 60/837,600, filed Aug. 9, 2006, the contents of which is hereby incorporated by references.
Number | Date | Country | |
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60837600 | Aug 2006 | US |
Number | Date | Country | |
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Parent | 11836302 | Aug 2007 | US |
Child | 11933266 | US |