The present invention generally relates to valves, and more particularly relates to butterfly valves with an improved seal arrangement for straight shaft configurations.
Valves are used in myriad systems to control the flow of a fluid. One particular system in which valves are used is an aircraft bleed air system. As is generally known, a portion of the compressed air generated by an aircraft gas turbine engine, which may be either a main propulsion engine or an auxiliary power unit, may be selectively routed to one or more pneumatic loads. Typically, this selective routing of bleed air to one or more pneumatic loads is controlled via one or more bleed air valves.
Bleed air valves may be variously configured. One exemplary type of valve that is used is a butterfly valve. A butterfly valve typically includes a valve body and a butterfly plate. The valve body includes an inner surface that defines a flow channel. The butterfly plate is mounted on a shaft and disposed within the flow channel. An actuation mechanism is coupled to the shaft and, upon supplying a torque to the shaft, causes the butterfly to rotate between a closed position and a plurality of open positions. The configuration of the butterfly plate and shaft are such that, at least for low-leakage and relatively high-pressure applications such as bleed air systems, the shaft is arranged to extend through the butterfly plate and across the flow channel at an angle relative to the direction of flow. This allows a suitable seal arrangement to be disposed and maintained between the butterfly plate and the valve body inner surfaces.
Although the above-described angled sealing butterfly valve is quite reliable and robust, it can exhibit certain drawbacks. For example, the angled configuration may not allow the valve to be installed in some space envelopes, unless certain other features are increased in size and/or weight. A zero-angled (or straight-shaft) butterfly valve may be configured to meet numerous space envelopes, but presently known straight-shaft butterfly valves either exhibit undesirably high internal leakage characteristics and/or insufficient pressure capabilities and/or insufficient structural stiffness and/or increased manufacturing costs and weight.
Hence, there is a need for a straight-shaft butterfly valve that exhibits sufficiently low internal leakage characteristics and/or sufficient pressure capabilities and/or sufficient structural stiffness and/or adequate manufacturing costs and weight. The present invention meets one or more of these needs.
In one embodiment, and by way of example only, a valve assembly includes a valve body, a shaft, a valve element, and a seal element. The valve body has an inner surface that defines a flow channel. The shaft is rotationally mounted on the valve body and extends across the flow channel. The shaft includes a first seal opening and a second seal opening. The first and second seal openings are spaced apart from each other and extend through the shaft. The valve element is coupled to the shaft and is rotatable therewith, and has an outer periphery. The seal element is coupled to the valve element, extends from the outer periphery, and extends through the first and second seal openings.
In another embodiment, an assembly includes a shaft, a valve element, and a seal element. The shaft is configured to be rotationally mounted on a valve body and to extend across a flow channel formed through the valve body. The shaft includes a first seal opening and a second seal opening. The first and second seal openings are spaced apart from each other and extend through the shaft. The valve element is coupled to the shaft, and has an outer periphery. The seal element is coupled to the valve element, extends from the outer periphery, and extends through the first and second seal openings.
In yet another embodiment, a valve assembly includes a valve body, a shaft, a butter fly plate, and a seal element. The valve body has an inner surface that defines a flow channel. At least a portion of the flow channel is disposed symmetrically about a central axis. The shaft is rotationally mounted on the valve body and extends across the flow channel at least substantially perpendicular to the central axis. The shaft includes a first seal opening and a second seal opening. The first and second seal openings are spaced apart from each other and extend through the shaft. The butterfly plate is coupled to the shaft and is rotatable therewith, and has an outer periphery. The seal element is coupled to the butterfly plate, extends from the outer periphery, and extends through the first and second seal openings.
Furthermore, other desirable features and characteristics of the valve assembly and its constituent parts will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the preceding background.
The present invention will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and wherein:
The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background or the following detailed description. In this regard, although the valve described and claimed herein is preferably configured for implementation into an aircraft bleed air system, it will be appreciated that it may be implemented in any one of numerous other systems, not just bleed air systems, and in numerous other environments, not just aircraft.
Turning now to
The valve element 104 is disposed within the flow channel 116 and, as is depicted most clearly in
The valve element 104, as was noted above, is coupled to the shaft 118. The valve element 104 is thus rotated with the shaft 118 between a closed position and any one of a plurality of open positions. In the closed position, which is the position depicted in
The valve actuator 106 is coupled to the shaft 118. The valve actuator 106 is configured to supply a drive torque to the shaft 118, which rotates and in turn causes the valve element 104 to rotate to the closed or open position. It will be appreciated that the valve actuator 106 may be variously configured to implement this functionality. In the depicted embodiment, however, the valve actuator 106 is implemented as an electrically-actuated, fluid-operated device. The valve actuator 106 is additionally configured, via a suitable spring mechanism, to bias the valve element 104 toward the closed position. A discussion of the specific configuration and implementation of the valve actuator 104 is not needed to fully describe or enable the claimed invention, and will thus not be provided.
Turning now to
It is additionally seen that a seal element 412, an embodiment of which is depicted in
In order for the seal element 412 to extend around the entire outer periphery 408 of the valve element 104, the seal element 412 also extends through the shaft 118. To facilitate this, as shown most clearly in
With the configuration disclosed herein the structural rigidity and stiffness of the valve element 104 is not compromised and any internal leakage that may occur is commensurate with that of an angled butterfly shaft valve. The valve assembly 100 simultaneously provides the weight and envelope benefits of a non-sealing straight shaft butterfly valve. The valve assembly 100 may also be assembled relatively easily, as will now be described.
The valve assembly 100 is preferably assembled by first installing the valve element 104 into the valve body 102. The shaft 118 is then inserted into the valve body 102, and down through the valve element shaft opening 602. When the fastener opening 802 in the shaft 118 lines up with the fastener opening 603 in the valve element 104, the set screw 308 is inserted and tightened onto the shaft 118L, and then the locking nut 312 is tightened onto the set screw 308. The valve element 104 is then centered via appropriate shimming
Once the valve element 104 is centered, the piston ring 412 is fed into the groove 604 around the periphery 408 of the valve element 104, through the first seal opening 804 in the shaft 118, and then continuing around the periphery 408 through the second seal opening 806, and then around until the seal element 412 is fully disposed within the valve element groove 604. The retaining clip 202 is then inserted to hold the seal element in place. Although not depicted in any of the drawings, it will be appreciated that a cut away may be optionally provided on the valve element 104 to ease installation and removal of the seal element.
While at least one exemplary embodiment has been presented in the foregoing detailed description of the invention, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment of the invention. It being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the invention as set forth in the appended claims.