The disclosure generally relates to pressure relief valves, and, more particularly, to a resettable pressure relief valve.
In aerospace applications, pressure relief valves are critical devices used for many aspects of flight safety. The valves may be mounted to an airframe, for example, to provide pressure relief in fluid lines subject to freezing and/or overpressure, conditions that could potentially result in degraded performance or outright equipment failure. Conventional pressure relief valves, once activated, must be removed from the aircraft and rebuilt or replaced.
A need exists for a pressure relief valve that can be easily reset from the outside of an aircraft, avoiding the cost of downtime for rebuilds and/or replacement inventory.
The foregoing needs are met by the present disclosure, wherein according to certain embodiments, a resettable relief valve includes a valve body having a valve seat and forming a pressure chamber, a poppet valve coupled to a poppet shaft slidably received in the valve body, a main spring mounted on the poppet shaft and seated against the valve body for urging the poppet valve into a closed position against the valve seat; and at least one spring loaded ball detent mounted in the valve body to apply pressure against the poppet shaft.
In accordance with another embodiment of the present disclosure, a method of resetting a pressure relief valve without disassembly includes the steps of mounting a resettable relief valve so that a pressure chamber of the resettable valve is exposed to a pressurized fluid flow, wherein the resettable relief valve includes a valve body defining the pressure chamber, a poppet valve coupled to a poppet shaft and slidably received in the valve body, wherein the poppet shaft has at least two grooves, a first groove associated with a closed position of the poppet valve and a second groove associated with an open position of the poppet valve, a main spring mounted on the poppet shaft and seated against the valve body for urging the poppet valve into a closed position against the valve seat, and at least one spring loaded ball detent mounted in the valve body to apply pressure against the poppet shaft; and pushing the poppet valve toward the valve body when the poppet valve is in the open position so that the spring loaded ball detent disengages from the second groove on the poppet shaft and reengages with the first groove.
There has thus been outlined, rather broadly, certain aspects of the present disclosure in order that the detailed description herein may be better understood, and in order that the present contribution to the art may be better appreciated.
In this respect, before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of the construction and to the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of embodiments in addition to those described and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein, as well as the abstract, are for the purpose of description and should not be regarded as limiting.
As such, those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
The methods and systems disclosed herein enable a relief valve to be reset when an aircraft is on the ground, without having to remove the valve for a rebuild and/or replace the valve with inventory, generally reducing Aircraft On Ground (AOG) delays, maintenance costs and aircraft downtime. Additionally, the resettable relief valve will not change settings due to aircraft vibration, which minimizes false activations.
As shown in
In accordance with aspects of the disclosure, the end of the shaft 30 opposite of the distal end 32 may be coupled to the poppet valve 20 so the shaft 30 and poppet valve 20 move longitudinally in unison along an axis substantially centered with respect to the shaft 30. A knob 34 may be formed on the end of the shaft 30 to fit into a shaft retaining channel 28 formed in the poppet valve 20. The knob 34 may be press fit into the shaft retaining channel 28 and/or the channel 28 may be internally threaded to receive external threads on the knob 34. In accordance with yet other aspects of the present disclosure, the channel 28 may be formed to allow rotation of the knob 34 therein. To reduce friction and allow rotational movement of the shaft 30 with respect to the poppet valve 20, a ball 60 may be inserted into the channel 28 between the knob 34 of the shaft and a retainer mechanism 62, which may be a plug press fit into the channel 28 or a setscrew having external threads for mating with internal threads formed in the channel 28. An epoxy 64 may be applied for further stabilization of the assembly as well as to ensure an aerodynamic surface is provided external to the relief valve 10 when installed.
As shown in
As shown in
A mating groove 82 may be formed on the shaft 30 to seat the ball detent assembly 72 when the relief valve 10 is in a closed position. Accordingly, when a relief pressure in the pressure chamber 50 exceeds a certain predetermined threshold, the spring loaded ball detent and main spring forces are overcome, and the poppet valve 20 moves to an open position. In the open position, a gap is formed about the periphery of the poppet valve 20, allowing fluid to escape and releasing pressure from the fluid flow path. A second, hold-open groove 84 may be formed on the shaft 30 at a predetermined distance distal to the mating groove 82. When the relief valve 10 is exposed to a relief pressure exceeding the predetermined threshold, and the shaft 30 and poppet valve 20 release to an open position, the hold-open groove 84 may capture the ball detent assemblies 72 to hold open the relief valve 10 until reset. The relief valve 10 may be reset by simply pushing the poppet valve 20 back to the closed position.
In a preferred embodiment, four spring loaded ball detent assemblies 72 are arranged symmetrically around the poppet shaft 30 (e.g., every 90°). In other embodiments, even or odd numbers of spring loaded ball detent assemblies 72 may be arranged symmetrically or asymmetrically around the poppet shaft, such as, for example, three spring loaded ball detent assemblies 72 arranged symmetrically around the poppet shaft 30 (e.g., every 120°).
It is to be understood that any feature described in relation to any one aspect may be used alone, or in combination with other features described, and may also be used in combination with one or more features of any other of the disclosed aspects, or any combination of any other of the disclosed aspects.
The many features and advantages of the invention are apparent from the detailed specification, and, thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirit and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and, accordingly, all suitable modifications and equivalents may be resorted to that fall within the scope of the invention.
This application is a Continuation application of U.S. patent application Ser. No. 13/463,577 filed May 3, 2012, which claims priority to U.S. Patent Application Serial No. 61/482,190, filed on May 3, 2011, the disclosure of which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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61482190 | May 2011 | US |
Number | Date | Country | |
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Parent | 13463577 | May 2012 | US |
Child | 13675831 | US |