The present invention relates to the field of rotary devices, such as pumps and motors.
Vane pumps are well-known positive-displacement pumps. A simple vane pump consists of a rotor positioned inside a larger circular cavity. The rotation axis is offset from the axis of the cavity and vanes are allowed to slide into and out of the rotor and seal on all edges. This creates, on one side of the pump, vane chambers that increase in volume. These increasing volume vane chambers are filled with fluid forced in by the inlet pressure. Often this inlet pressure is nothing more than pressure from the atmosphere. On the discharge side of the pump, there are created vane chambers which decrease in volume. This forces fluid out of the pump. Typically, these pumps run at relatively high speeds, and the centrifugal force associated with the rotation is used to hold the vanes against the surface of the interior cavity for sealing. While vane pumps are known to have utility, many suffer from a disadvantageous combination of relatively high cost and relatively low longevity.
A rotary device forms one aspect of the invention and comprises a barrier ring, a rotor, a plurality of vanes, a sealing structure and an arrangement. The barrier ring has a central longitudinal axis and a tubular interior surface through which the longitudinal axis extends centrally, in spaced relation. The interior surface includes one or more portions which each define a longitudinally extending, inwardly-projecting ridge. Defined through the interior surface, on opposite circumferential sides of each of said one or more ridges, is a first port and a second port. The rotor is mounted for rotation in the barrier ring about the longitudinal axis and includes a rotor body. The vanes are mounted to the rotor body for rotation with the rotor body about the longitudinal axis and for radial extension and retraction relative to the rotor body such that at least portions of the interior surface of the barrier ring can be swept by the vanes. The sealing structure provides a seal between the rotor and the barrier ring to permit fluid communication into and out of the rotary device substantially only via the first and second ports. The arrangement, which is for causing the vanes to retract and extend as the rotor body rotates such that chambers are created which decrease in volume when in communication with the first ports and such that chambers are created which increase in volume when in communication with the second ports, includes a fluid pressure mechanism for causing the vanes to retract.
According to another aspect of the invention, the rotor can further comprise a pair of axially spaced supports which support the axially-spaced edges of the vanes when extended from the rotor body.
According to another aspect of the invention, the fluid pressure mechanism can be for causing retraction and, at least in part, extension of the vanes.
According to another aspect of the invention, the rotor can define a slot for each vane, and each vane can be mounted in the slot provided for it in the manner of a piston in a cylinder. As well, the fluid pressure mechanism can comprise a fluid circuit which couples the base of each slot to a point in the rotor which, in rotation, immediately precedes the slot immediately preceding the slot from which said fluid path extends.
According to another aspect of the invention, the rotor can define a slot for each vane, each vane being mounted in the slot provided for it in the manner of a piston in a cylinder, and the fluid pressure mechanism can comprise a fluid circuit which, in rotation, selectively couples the base of each slot approaching a ridge to the base of the slot immediately preceding said each slot.
According to another aspect of the invention: the rotor can define a slot for each vane, each vane being mounted in the slot provided for it in the manner of a piston in a cylinder; the fluid pressure mechanism can provide for fluid communication between slots occupied by vanes which need to retract to breach the ridges and slots occupied by vanes which need to extend to sweep the barrier ring; and in use, the pressure of the fluid passing between the first and second ports can provide the motive force for the extension and retraction of the vanes.
According to another aspect of the invention, the fluid pressure mechanism can cause the vanes to retract as they approach the ridges and to extend after they pass the ridges.
According to another aspect of the invention, in each slot, a spring can bias the vane mounted within said each slot for extension.
According to another aspect of the invention, the spring compression can vary over its length, such that, in use, relatively high force is required to bottom out the spring and such that, as the vane reaches full extension, the spring provides relatively low force to the vane.
According to another aspect of the invention, the one or more portions can comprise a plurality of portions, each defining a longitudinally extending, inwardly-projecting ridge.
According to another aspect of the invention, the first ports can be outlets and the second ports can be inlets.
The rotary device can, according to another aspect of the invention, form part of a pump for a fluid. In this pump, a shaft is coupled to the rotor body for receiving power and converting received power into rotation of the rotor such that, if the inlets are placed in communication with a supply of said fluid at a relatively low pressure, the outlets create a supply of fluid at a relatively higher pressure.
In this pump, the vanes can have neutral buoyancy in said fluid.
The pump itself can, according to another aspect of the invention, form part of a fluid pumping system. This system includes a windmill which, in use, can rotate at less than 20 rpm and which can drive the pump at less than 20 rpm.
The invention permits the construction of pumps that operate at relatively low rotational speed, that are relatively robust, that have relatively high flow capacity and that are of relatively high-efficiency.
Other advantages, features and characteristics of the present invention, as well as methods of operation and functions of the related elements of the structure, and the combination of parts and economies of manufacture, will become more apparent upon consideration of the following detailed description and the appended claims with reference to the accompanying drawings, the latter being briefly described hereinafter.
A rotary device 20 according to an exemplary embodiment of the invention is shown in perspective view in
The supporting bosses 30 form part of the end caps 40 and the separator ring 43.
The barrier ring 36 is circumferentially supported by the supporting bosses 30 inside the housing 24 and, as best seen in
The barrier ring 36 has a central longitudinal axis X-X and a tubular, undulating interior surface 46 through which the longitudinal axis X-X extends centrally, in spaced relation. The interior surface 46 includes a plurality of, specifically five, portions 48, each defining a longitudinally extending, inwardly-projecting ridge 50.
On opposite circumferential sides of each of said one or more ridges 50 is defined an inlet 54 in the form of a second port and an outlet 56 in the form of a first port, the inlets 54 collectively communicating with the inlet manifold 32 and the outlets 56 collectively communicating with the outlet manifold 34.
The separator ring 43 separates the housing parts 24A,24B from one another, and avoids comingling of the flows leading into and out of the rotary device.
With reference to
The rotor 60 includes a rotor body member 66, a pair of end rings 68 and shaft discs 65 from which stubs forming the shaft 24 protrude. Although not shown, it will be understood that threaded shafts extend through communicating bores provided in the main body 66, shaft discs and end rings 60, to hold the rotor 60 together. The main body 66 is fluted, and the end rings 68 are notched, such that the rotor 60 has defined therein a plurality of longitudinally-extending radial slots 74, as best seen in
An exemplary vane is shown in
In the device shown, sixteen vanes 62 are provided, and each vane 62 is mounted in the slot 74 provided for it in the manner of a piston in a cylinder. The vanes have substantially neutral buoyancy in the fluid to be pumped, ie they neither float nor sink.
The manner in which the vanes 62 are mounted allows for the vanes 62 to move with the rotor 60 about the longitudinal axis X-X, and also allows for radial extension and retraction thereof relative to the rotor body 66 such that the interior surface 46 of the barrier ring 36 can be swept by the vanes. Notably, as the vanes extend, they do not extend in a cantilevered manner, but are supported throughout such extension by the end rings 68.
The end caps 40 collectively define a sealing structure which seals the gaps between the rotor 60 and barrier ring 36 thereby to permit fluid communication into and out of the rotary device substantially only via the inlets 54 and the outlets 56. As shown, the end caps 40 are secured to one another by threaded rods, and drawn tightly against the barrier ring, to arrest flow around the periphery of the barrier ring, and a pair of gasket rings 53 are provided, which are relatively tightly held against one another in the interstice between the rotor assembly and the end cap, to arrest flow through the hole in the end cap provided for the shaft 24. The end caps 40 also support the bearings 59 which, in turn, support the rotor for rotation, via the shaft 24.
The illustrated, exemplary rotary device also includes a vane actuation arrangement, for causing the vanes 62 to retract and extend as the rotor 60 is rotated, to sweep the interior surface 46 of the barrier ring 36 such that chambers are created which decrease in volume when in communication with the outlets 56 and such that chambers are created which increase in volume when in communication with the inlets 54.
In the exemplary embodiment shown, the vane actuation arrangement includes a plurality of springs 80 and a fluid pressure mechanism.
The springs 80 are provided for each slot 74, at the base of each vane 62, as shown in
The fluid pressure mechanism includes a fluid circuit which, in this example, couples the base of each slot to a point in the rotor which, in rotation, immediately precedes the slot immediately preceding the slot from which said fluid path extends. In
A snapshot of the rotary device in operation is shown schematically in
Whereas a single embodiment of the rotary device is shown in
For example, whereas five ridges are shown, it should be understood that greater or number of ridges may be employed, as desired. For greater clarity in this regard, it should also be “understood” that “ridge” in this description and in the appended claims should be understood to mean a structure for dividing the annular space in which the vanes traverse into subspaces. The “ridge” need not be sinusoidal as shown; it could be, for example, triangular, or even be defined by an upstanding plate 105, as shown in
Similarly, whereas a sixteen vane/five ridge apparatus is shown, it is contemplated that the invention can be carried out with greater and lesser numbers of vanes.
Persons of ordinary skill will readily appreciate that, adjustments to the number of ridges and vanes will require corresponding adjustments to the fluid circuit, so as to ensure that the vanes continue to automatically retract and extend as desired, i.e. if greater numbers of vanes per ridge are employed, the fluid circuit might, for example, couple the base of each slot to a point in the rotor which, in rotation, immediately precedes the slot twice preceding the slot from which said fluid path extends. Further, whereas in the structure illustrated in
Further, it should also be understood that persons of ordinary skill might well wish to tune the fluid circuit, i.e. restrict or extend the flow paths, depending, for example, on the pressure head to be generated and the expected RPM of the rotor, so as to avoid hammering of the vanes as they extend and retract. In the context of the embodiment of
As well, whereas it is contemplated that the vanes retract under fluid pressure, it should be appreciated that it is not critical that only fluid pressure be employed. The use of fluid pressure retraction generally allows steeper slopes on the ridges, and thus, complete avoidance of fluid pressure retraction would negate certain advantages of the present invention, but it is contemplated that the invention could be employed in combination with conventional cam-style retraction.
As well, routine changes in sizes and shapes of the parts, and their manner of assembly and connection, are also contemplated.
For example, only,
Yet further, whereas the previous descriptions contemplated the use of the rotary device as a pump, this structure could be used as a motor with suitable modifications to the fluid circuit.
Further, whereas the structure of
As well, whereas in
Additionally, whereas no filters or the like are shown in the structure of
Further, whereas a specific vane is shown in
Accordingly the invention should be understood as limited only by the accompanying claims, purposively construed.
This application claims priority to U.S. Provisional Application No. 61/220,319 filed Jun. 25, 2009, which is herein incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
23764 | Freeman, Jr. | Apr 1859 | A |
68186 | Hall | Aug 1867 | A |
232559 | Smith | Sep 1880 | A |
390044 | Voorhies | Sep 1888 | A |
520810 | Thomson | Jun 1894 | A |
643432 | Washington et al. | Feb 1900 | A |
949431 | Hokanson | Feb 1910 | A |
1014495 | Lincoln | Jan 1912 | A |
1023872 | Pearson | Apr 1912 | A |
1042595 | Pearson | Oct 1912 | A |
1066506 | Krogel | Jul 1913 | A |
1339723 | Smith | May 1920 | A |
1349353 | Wilber, Jr. | Aug 1920 | A |
1393698 | Piatt | Oct 1921 | A |
1515961 | Meyer | Nov 1924 | A |
1745800 | Kramer | Sep 1930 | A |
1972744 | Lister | Sep 1934 | A |
2098244 | Hopfensberger | Nov 1937 | A |
2310816 | Taylor | Feb 1943 | A |
2476397 | Bary | Jul 1949 | A |
2536938 | Hunter | Jan 1951 | A |
2728300 | Petersen | Dec 1955 | A |
2819677 | Leath | Jan 1958 | A |
2853978 | Smyser | Sep 1958 | A |
3057157 | Close | Oct 1962 | A |
3057304 | Rohde | Oct 1962 | A |
3305209 | Bender et al. | Feb 1967 | A |
3312387 | Cassidy et al. | Apr 1967 | A |
3401641 | Adams et al. | Sep 1968 | A |
3431861 | Martin | Mar 1969 | A |
3464395 | Kelly | Sep 1969 | A |
3478728 | Kelly | Nov 1969 | A |
3514237 | Spyridakis | May 1970 | A |
3525963 | Burdett | Aug 1970 | A |
3640648 | Odawara | Feb 1972 | A |
3694114 | Eickmann | Sep 1972 | A |
3727589 | Scott | Apr 1973 | A |
3797975 | Keller | Mar 1974 | A |
3863611 | Bakos | Feb 1975 | A |
3873253 | Eickmann | Mar 1975 | A |
4086645 | Gorman et al. | Apr 1978 | A |
4154208 | Kunieda et al. | May 1979 | A |
4203062 | Bathen | May 1980 | A |
4408964 | Mochizuki et al. | Oct 1983 | A |
4410305 | Shank et al. | Oct 1983 | A |
4415322 | Baudin | Nov 1983 | A |
4416598 | Merz | Nov 1983 | A |
4418663 | Bentley | Dec 1983 | A |
4432711 | Tsuchiya et al. | Feb 1984 | A |
4468964 | Groeneweg | Sep 1984 | A |
4484863 | Pagel | Nov 1984 | A |
4551896 | Sakamaki et al. | Nov 1985 | A |
4561834 | Poss | Dec 1985 | A |
4646568 | Lew | Mar 1987 | A |
4772187 | Thompson | Sep 1988 | A |
4917584 | Sakamaki et al. | Apr 1990 | A |
4958995 | Sakamaki et al. | Sep 1990 | A |
5002473 | Sakamaki et al. | Mar 1991 | A |
5092752 | Hansen | Mar 1992 | A |
5160252 | Edwards | Nov 1992 | A |
5163825 | Oetting | Nov 1992 | A |
6030195 | Pingston | Feb 2000 | A |
6439868 | Tomoiu | Aug 2002 | B1 |
6527525 | Kasmer | Mar 2003 | B2 |
6554596 | Patterson et al. | Apr 2003 | B1 |
6776136 | Kazempour | Aug 2004 | B1 |
6799549 | Patterson et al. | Oct 2004 | B1 |
6896502 | Patterson | May 2005 | B1 |
6899528 | Youngpeter et al. | May 2005 | B2 |
6945218 | Patterson | Sep 2005 | B2 |
7048526 | Patterson | May 2006 | B2 |
7229262 | Patterson | Jun 2007 | B2 |
8011909 | Dong | Sep 2011 | B2 |
20050196299 | Patterson | Sep 2005 | A1 |
Number | Date | Country |
---|---|---|
32552 | Oct 1889 | CA |
115442 | Dec 1908 | CA |
202671 | Aug 1920 | CA |
203163 | Aug 1920 | CA |
2628539 | Jan 1977 | DE |
29720052 | Feb 1998 | DE |
166871 | Jan 1922 | GB |
468390 | Jul 1937 | GB |
2078303 | Jan 1982 | GB |
2401402 | Nov 2004 | GB |
57032095 | Feb 1982 | JP |
61152987 | Jul 1986 | JP |
61241482 | Oct 1986 | JP |
3206381 | Sep 1991 | JP |
6307252 | Nov 1994 | JP |
Number | Date | Country | |
---|---|---|---|
20110171054 A1 | Jul 2011 | US |
Number | Date | Country | |
---|---|---|---|
61220319 | Jun 2009 | US |