This application claims priority to European Patent Application No. 22461532.8 filed Mar. 31, 2022, the entire contents of which is incorporated herein by reference.
The methods and systems described herein relate to rotary vane pumps and in particular, methods and systems for assessing wear of a vane of such pumps.
Sliding rotary vane pumps may be used in a plurality of different mechanical and industrial applications (e.g. they may be used in both liquid and gas pumping applications) and can be invariable exposed to a wide range of environmental conditions. One type of rotary vane pump is a dry air pumps, which are dry vacuum pumps constructed of carbon vanes and rotors which are self-lubricating. Such dry air pumps may comprise mechanical carbon rots and vanes that operate in a hardened metal cavity. Such pumps may provide a power source in a multitude of applications such as to provide power to pneumatically operated flight instruments, for example.
Although such dry air pumps do not use a liquid lubricant, they do use other lubricating methods such as self-lubricating coatings, amongst other methods. Although such lubricating methods may work well to some extent, the nature of the vane lubrication technique is still destructive to the parts of the pump. Due to this, parts of the pump, such as the vanes, can wear down over time. This results in the lengths of the vanes eventually being too short to fit into the slot in which it is positioned in use and this can result in failure of the pump. If the pump is used in an aircraft, such failure can result in one or more of the aircraft systems becoming inoperative and, since this would most often occur during use, i.e. in flight, this can be quite dangerous. It is therefore important to ensure that any wearing, or the extent of wearing of the vane can be clearly and accurately detected so that such failures do not occur.
Some known techniques, such as those discussed in U.S. Pat. No. 6,769,886 B2 assess the length of a vane using an external tool which is inserted into the pump via a designated channel. The tool is then used to measure the height of the vane. This measurement is only possible after the pump has been disassembled from the airplane and the measurement of the length vane is not precise.
A vane for use in a rotary vane pump is described herein, said vane having a length L extending between a first edge of the vane 16 and a second edge of the vane and a width W extending perpendicular to said length, said width extending between a third edge of said vane and a fourth edge of the vane, and further comprising a channel extending through said vane (16) and provided at a position along said length L of said vane.
In any of the examples described herein, the channel may be positioned away from said first and second edges such that said vane has a constant length L along its width.
In any of the examples described herein, said channel may extend between a first point along said length and a second point along said length and wherein a width of said channel varies in shape between said first and second points.
In any of the examples described herein, the width of said channel may taper from a first channel width to a second channel width, wherein said first channel width is smaller than said second channel width. The first point may be closer to said first edge and said second point is closer to said second edge, or vice versa.
In any of the examples described herein, said channel may have a triangular shape, a rectangular shape or a circular shape.
In any of the examples described herein, the vane may comprise a plurality of said channels.
In any of the examples described herein, a first of one of said plurality of channels may be offset from a second one of said plurality of channels along said length of said vane. That is, the first one of said plurality of channels may be provided at a first position along the length of the vane and a second of said plurality of channels may be provided at a second position along the length of said vane, and wherein said first position and said section are not the same as each other, such that said first channel is closer to said first edge than said second channel.
In any of the examples described herein, said plurality of channels may be offset from each other in along said width of said vane.
A rotary vane pump is also described that comprises the vanes described herein. The pump may comprise a rotor “R” configured to rotate about a central axis; said rotor comprising a plurality of circumferentially spaced vane slots, wherein at least one of said vane slots is configured to receive one of the vanes described herein.
The vane may be inserted into the slot of the rotor R such that the second edge of the vane is positioned closer to the central axis of the rotor R than the first edge of the vane 16.
A method for detecting a decrease in the length of a vane (i.e. wear of the vane 16) provided in a rotary vane pump is also described herein. The method comprises providing a rotor “R” configured to rotate about a central axis; said rotor comprising a plurality of circumferentially spaced vane slots, wherein at least one of said vane slots is configured to receive a vane, inserting said vane into said at least one vane slot, said vane having a length L extending between a first edge of the vane and a second edge of the vane and a width W extending perpendicular to said length, said width extending between a third edge of said vane and a fourth edge of the vane, and said vane further comprising a channel extending through said vane and provided at a position along said length L of said vane, said method comprising measuring a pressure in said rotary vane pump, and detecting a decrease in said pressure of said rotary vane pump, said decrease in pressure indicating that said vane has decreased to a length corresponding to said channel.
The method may be used in combination with any of the vanes described herein.
A rotary vane pump comprises a central annular body of stator, S, a cross-section of which is shown in
Each vane 16 is made from a material that during use, wears and produces a form of dry lubrication for the pump when in use. For example, vanes 16 can be made from carbon material, graphite, and various organic binders. In some examples, a self-lubricating coating may be applied to the pump parts to inhibit wear between the slidable vanes 16 and pump rotor R.
A stator S is provided that surrounds the rotor R. The stator S has two symmetrically opposite lobes 18 and 19, the surfaces of which act as cams that regulate the two extension and retraction cycles for the vanes 16 during each rotation of the rotor R. As is known in the art, the longitudinal spaces defined by the adjacent vanes 16 and the external surface of the rotor R, as well as the surface of a stator lobe, and end plates of the pump serve as pumping pockets which are moved from an intake zone to an exhaust zone to accomplish the pumping action of the pump R.
As can be seen in
In known rotary pumps, the vane is solid, and as the vane wears down, the length L of the vane gets shorter and shorter until the lengths of the vanes eventually become too short to fit into the slots of the rotor. As mentioned in the background section above, this results in failure of the pump.
In the examples described herein, however, the vane 16 comprises a channel 17 which extends through the vane 16. This channel 17 may be any number of shapes, including circular, square, rectangular, triangular, to name a few. The channel 17 may also be tapered.
The channel 17 may be provided so as to extend through the vane 16 and also between a first point P1 and a second point P2 along a portion of the length L of the vane as shown in
Whilst the channel remains in communication with the longitudinal space of the pump, this drop in pressure will remain as the vane continues to wear down. Once the vane 16 is worn down to such an extent that the channel 17 has been passed, the pressure in the longitudinal space will again increase and this provides a second warning signal that the vane 16 has worn down significantly to a length wherein the vane should be replaced.
In the example described and shown with reference to
Although the channel 17 shown in
The channel 17 may be positioned along the length L of the vane such that it is away from, i.e. not at, or cut into, the first or second edge. The length of the vane 16 therefore remains constant along the width of the vane and the channel 17 does not shorten the length of the vane at any point along its width. For example, the channel 17 may be positioned at a point approximately midway along the length L of the vane 16. In other examples, the channel may be positioned closer to one of the first or second edges rather than the other. In other words, the channel may not be in contact with the first edge 16c prior to use, or in contact with the second edge 16d prior to use but is positioned at a point between the first and second edges 16c, 16d, such that the drop in pressure can be detected due to wear.
In other examples, wherein the channel 17 is not triangular shaped, other shapes may be used wherein the channel 17 has a varying and/or tapered with along its length and between the end 16c which is being worn during use and the opposite end 16d which is closest to the central axis of the stator S during use. Although in the examples shown in
Another example of a new type of vane 16 is shown in
In the example shown in
Another example of this is shown in
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
Number | Date | Country | Kind |
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22461532 | Mar 2022 | EP | regional |
Number | Name | Date | Kind |
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3463384 | Kilbane | Aug 1969 | A |
3469500 | Lutz | Sep 1969 | A |
3869231 | Adams | Mar 1975 | A |
3904327 | Edwards et al. | Sep 1975 | A |
4705465 | Su | Nov 1987 | A |
6752604 | Althouse | Jun 2004 | B2 |
6769886 | Henderson | Aug 2004 | B2 |
6913451 | Hedrick et al. | Jul 2005 | B2 |
9828992 | Stambaugh, Sr. | Nov 2017 | B2 |
20020110467 | Henderson | Aug 2002 | A1 |
Number | Date | Country |
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3303906 | Aug 1984 | DE |
2596107 | Sep 1987 | FR |
2014010677 | Jan 2014 | WO |
Entry |
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Abstract for FR2596107 (A1), Published: Sep. 25, 1987, 1 page. |
Abstract: DE3303906 (A1), Published: Aug. 6, 1984, 1 page. |
European Search Report for Application No. 22461532.8, mailed Sep. 29, 2022, 8 pages. |
Number | Date | Country | |
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20230313683 A1 | Oct 2023 | US |