1. Technical Field of the Invention
The present invention relates to high capacity valves, and more particularly to a globe valve configured to reduce flow losses and increase fluid flows therethrough.
2. Description of Related Art
In a globe valve, flow between a first fluid passage and a second fluid passage is controlled by a plug movable within a tubular throttling cage. Fluid flowing from the first passage to the second passage flows into the throttling cage through an open end, and out of the throttling cage through a plurality of radially oriented flow ports. Alternately, fluid flowing from the second passage to the first flows into the throttling cage through the radial flow ports and out the open end to the first passage. In either case, the plug is movable to selectively cover the flow ports, thereby restricting flow through the throttling cage and the valve.
The flow path through a globe valve is convoluted. In an example where fluid is flowing from the first passage to the second, fluid passes through the open end and into the throttling cage about its axis. Thereafter, the flow must be diverted 90° to exit through the radially oriented flow ports. Flow out through the radially oriented flow ports exits in all directions (360°) and is collected and directed towards a single passage. Thus, a portion of the flow exiting the radially oriented flow ports is diverted as much as 180° to flow around the interior of the valve to the passage. The directional changes are exacerbated in an inline configuration where the valve inlet and outlet are on a common flow axis, because the throttling cage is positioned in perpendicular relation to the common flow axis. As a result, the flow must be diverted an additional 90° to flow through the open end of the throttling cage. Further, the radial flow ports may not be vertically aligned with the outlet, and thus the flow between the second passage and the flow ports must be diverted to a common axis.
The convoluted flow causes flow losses in areas of the valve that are not controlled by the throttling cage and plug. Not only do the losses limit the overall flow efficiency of the valve, but because they are independent of the flow throttling, the losses impact the characteristics of the throttling control. In other words, as the flow rate increases the total flow loss through the valve becomes more a function of flow rate and less a function of the amount of the flow port covered by the plug.
Prior attempts to reduce flow losses have included increasing the size of the valve body and the fluid ports through which the fluid flows. Unfortunately, larger components such as a larger valve body and a larger throttling cage and plug that would result from the larger fluid ports, also increase the weight and cost of the valve. Further, such larger components also require stronger and more expensive mechanisms, for example the mechanism on which the plug reciprocates. It is preferable that a valve conform to commercially standardized installation dimensions. These dimensions limit the extent to which the size of the valve body and other components can be increased.
Therefore, there is a need for a globe valve that has reduced flow losses, especially at high flow rates, that is comparable in size, weight, and cost to other globe valves.
The present invention is drawn to a globe valve with refinements that reduce flow losses and increase maximum fluid flows therethrough. The valve has a flow body defining an interior cavity in communication with a first fluid passage and a second fluid passage. The volume of the cavity is substantially equally distributed about a central axis. A tubular throttling cage resides in the cavity. The throttling cage has an open end in communication with the first passage and a plurality of flow ports arranged about a perimeter of the throttling cage. Fluid can flow between the first fluid passage and the second fluid passage through the throttling cage. The longitudinal axis of the throttling cage is positioned offset from the central axis of the cavity. A plug is closely received in the throttling cage and movable about the longitudinal axis to selectively cover the flow ports thereby restricting flow between the first fluid passage and the second fluid passage. At least one of the flow ports facing the second fluid passage can be larger than at least one or all of the other flow ports. The flow ports can be angled towards the second fluid passage. The flow ports can pass substantially straight through the throttling cage.
An advantage of the invention is that the offset throttling cage allows more annular volume between the throttling cage and the cavity walls in which to more gradually expand or contract flows through the throttling cage. This more gradual expansion or contraction reduces fluid separation from the cavity walls and turbulent flow mixing that causes fluid drag.
Another advantage of the invention is that the angled flow ports reduce inertial flow losses as the flow impinges on the cavity wall, because the flow directional changes within the valve are made more gradually.
Another advantage of the invention is that the flow ports can pass straight through the throttling cage and are thus less expensive to manufacture than curved flow ports and require a thinner throttling cage wall thickness to achieve the same directional change.
These and other advantages will be apparent from the following detailed description with reference to the following drawings.
Various objects and advantages of the invention will become apparent and more readily appreciated from the following description of the presently preferred exemplary embodiments, taken in conjunction with the accompanying drawings of which:
Referring first to
The interior cavity 14 contains a tubular throttling cage 20 with a longitudinal axis A2 that is substantially perpendicular to the axis A1. The throttling cage 20 concentrically receives and guides a throttling plug 22 for movement of the plug 22 along the longitudinal axis A2. Plug 22 depends from a reciprocating stem 24 extending downward through an upper housing 26 (or bonnet) over the cavity 14. Fluid flows through an open end 28 of the cage 20, and also through a plurality of radially or laterally oriented fluid ports 30 arranged about its perimeter (see FIG. 2). Thus, if fluid enters through the first fluid passage 16, it will flow up through the open end 28 into the cage 20, out through the fluid ports 30 into the cavity 14, and out through the second fluid passage 18. Alternately, fluid flowing from the second fluid passage 18 to the first fluid passage 16 will flow from the second fluid passage 18 through the fluid ports 30 and into the throttling cage 20, then through the open end 28 to the first fluid passage 16. In one exemplary embodiment, the throttling cage 20 has a substantially cylindrical cross-section, and the plug 22 has a circular profile that fits closely within the inner diameter of the cage 20.
The plug 22 throttles flow through the throttling cage 20 by selectively covering a portion of the ports 30 thereby reducing the available area through which fluid can flow. Thus, the maximum flow through the valve 10 is achieved when the plug 22 is fully retracted (see
Referring to
The fluid ports 30 are angled with respect to radii of the cavity 14 (or the throttling cage 20), such that fluid exiting the ports 30 impinges on the cavity 14 walls at an angle other than perpendicular to the wall surface. Further, the ports 30 are angled towards the second fluid passage 18 to direct flow from within the throttling cage 20 towards the second fluid passage 18, or flow from the second passage 16 into the throttling cage 20, thereby contributing to the directional change necessary to route the flow through the throttling cage 20. In an exemplary embodiment, the fluid ports 30 on one side of the throttling cage 20 are a mirror image of those on the other side. Also, the fluid ports 30 furthest from the second passage 16 are oriented to distribute fluid evenly to either side of the cavity 14. The angled fluid ports 30 reduce inertial fluid losses as the fluid impacts the cavity 14 wall, because the directional change is made gradually.
In an exemplary embodiment, the fluid ports 30 are straight passages without curvature. Thus, the ports 30 pass substantially straight through the wall of the throttling cage 20. Also, the walls 31 of the ports 30 do not have to be parallel, so for example as in
The fluid port 30a nearest the second fluid passage 18 is larger than other fluid ports 30 and oriented towards the second fluid passage 18 to maximize the amount of flow that can flow directly between the second fluid passage 18 and the interior of the throttling cage 20 without directional changes. Opposite the forward fluid port 30a is a flow splitter 34. The flow splitter 34 is a generally triangular portion of the throttling cage 20 wall defined by two adjacent fluid ports 30b and 30c. A corner of the triangular shape 36 helps to split the flow exiting the upstream side of the throttling cage 20 and begin the 180° directional change that is required for the flow exiting the rear of the throttling cage 20. This flow would otherwise impinge on the wall of the cavity 14, thus the flow splitter 34 helps to reduce flow momentum losses as the fluid changes direction and reduces turbulent flow mixing.
Although several exemplary embodiments of the methods and systems of the invention have been illustrated in the accompanying drawings and described in the foregoing description, it will be understood that the invention is not limited to the embodiments disclosed, but is capable of numerous rearrangements, modifications and substations without departing from the spirit and scope of the invention as defined in the following claims.
Number | Name | Date | Kind |
---|---|---|---|
223573 | Ainsworth et al. | Jan 1880 | A |
817153 | Barr | Apr 1906 | A |
871775 | Glanchard et al. | Nov 1907 | A |
1333048 | Webster | Mar 1920 | A |
1511302 | Schnetzer | Oct 1924 | A |
1648708 | Wilkinson | Nov 1927 | A |
2585290 | Walker | Feb 1952 | A |
2911009 | Parker | Nov 1959 | A |
2915087 | Kruschik | Dec 1959 | A |
3023783 | Vickery | Mar 1962 | A |
3443793 | Hulsey | May 1969 | A |
3700003 | Smith | Oct 1972 | A |
3707161 | Crawford | Dec 1972 | A |
3709245 | O'Connor, Jr. | Jan 1973 | A |
3746049 | O'Connor, Jr. | Jul 1973 | A |
3776278 | Allen | Dec 1973 | A |
3780767 | Borg et al. | Dec 1973 | A |
3813079 | Baumann et al. | May 1974 | A |
3826281 | Clark | Jul 1974 | A |
3860032 | Rogers | Jan 1975 | A |
3880191 | Faumann | Apr 1975 | A |
3941350 | Kluczynski | Mar 1976 | A |
3954124 | Self | May 1976 | A |
3960177 | Baumann | Jun 1976 | A |
3971411 | Baumann | Jul 1976 | A |
3974860 | Stead et al. | Aug 1976 | A |
3987809 | Baumann | Oct 1976 | A |
3990475 | Myers | Nov 1976 | A |
4022423 | O'Connor et al. | May 1977 | A |
4085774 | Baumann | Apr 1978 | A |
4111229 | Christian | Sep 1978 | A |
4149563 | Seger | Apr 1979 | A |
4212321 | Hulsey | Jul 1980 | A |
4226263 | Muchow | Oct 1980 | A |
4230154 | Kalbfleish | Oct 1980 | A |
4249574 | Schnall et al. | Feb 1981 | A |
4256284 | Balhouse | Mar 1981 | A |
4295632 | Engelke | Oct 1981 | A |
4364415 | Polon | Dec 1982 | A |
4367807 | Fink et al. | Jan 1983 | A |
4397331 | Medlar | Aug 1983 | A |
4402485 | Fagerlund | Sep 1983 | A |
4479510 | Bey | Oct 1984 | A |
4530375 | Bey | Jul 1985 | A |
4540025 | Ledeen et al. | Sep 1985 | A |
4610273 | Bey | Sep 1986 | A |
4617963 | Stares | Oct 1986 | A |
4619436 | Bonzer et al. | Oct 1986 | A |
4624442 | Duffy et al. | Nov 1986 | A |
4691894 | Pyötsiä et al. | Sep 1987 | A |
4774984 | Peters | Oct 1988 | A |
4784039 | Leinen | Nov 1988 | A |
4825906 | Hartman | May 1989 | A |
4881718 | Champagne | Nov 1989 | A |
4889163 | Engelbertsson | Dec 1989 | A |
4929088 | Smith | May 1990 | A |
4967998 | Donahue | Nov 1990 | A |
4973406 | Ponzielli | Nov 1990 | A |
5070909 | Davenport | Dec 1991 | A |
5116019 | Rohweder et al. | May 1992 | A |
5180139 | Gethmann et al. | Jan 1993 | A |
5193583 | Gethmann et al. | Mar 1993 | A |
5218984 | Allen | Jun 1993 | A |
5277404 | Andersson | Jan 1994 | A |
5287889 | Leinen | Feb 1994 | A |
5332004 | Gethmann et al. | Jul 1994 | A |
5400825 | Gethmann et al. | Mar 1995 | A |
5427147 | Henriksson | Jun 1995 | A |
5437305 | Leinen | Aug 1995 | A |
5482249 | Schafbuch et al. | Jan 1996 | A |
5492150 | Aquilino | Feb 1996 | A |
5509446 | Bey | Apr 1996 | A |
5511584 | Leinen | Apr 1996 | A |
5516079 | Baumann | May 1996 | A |
5630528 | Nanaji | May 1997 | A |
5680889 | Boger | Oct 1997 | A |
5730416 | Welker | Mar 1998 | A |
5758689 | Leinen | Jun 1998 | A |
5765814 | Dvorak et al. | Jun 1998 | A |
5769388 | Welker | Jun 1998 | A |
5771929 | Boger | Jun 1998 | A |
5890505 | Boger | Apr 1999 | A |
5924673 | Welker | Jul 1999 | A |
5931445 | Dvorak et al. | Aug 1999 | A |
5988586 | Boger | Nov 1999 | A |
6003551 | Wears | Dec 1999 | A |
6029702 | Leinen et al. | Feb 2000 | A |
6079451 | Hegler | Jun 2000 | A |
6105614 | Bohaychuk et al. | Aug 2000 | A |
6250330 | Welker | Jun 2001 | B1 |
6289934 | Welker | Sep 2001 | B1 |
Number | Date | Country |
---|---|---|
1128832 | Aug 1982 | CA |
1229024 | Nov 1987 | CA |
237 241 | Aug 1945 | CH |
858 178 | Dec 1952 | DE |
1 200 688 | Sep 1965 | DE |
23 52 370 | Apr 1975 | DE |
23 59 717 | Jun 1975 | DE |
24 35 561 | Feb 1976 | DE |
26 54 769 | Jun 1978 | DE |
26 54 769 | Jun 1978 | DE |
26 54 769 | Jun 1978 | DE |
30 17 857 | Nov 1981 | DE |
43 28 095 | Feb 1995 | DE |
0 325 846 | Jan 1991 | EP |
0 621 428 | Oct 1994 | EP |
0 831 262 | Mar 1998 | EP |
0 838 617 | Apr 1998 | EP |
0 746 708 | Dec 1998 | EP |
1050164 | Jan 1954 | FR |
1462437 | Nov 1966 | FR |
751 060 | Jun 1956 | GB |
114066 | Jul 1982 | JP |
2000-202027 | Jul 2000 | JP |
WO 9407063 | Mar 1994 | WO |
WO 9831957 | Jul 1998 | WO |
Number | Date | Country | |
---|---|---|---|
20030159737 A1 | Aug 2003 | US |