DRAG PUMP
20220299036 · 2022-09-22
Inventors
Cpc classification
F04D29/281
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A drag pump for pumping fluid from an inlet to an outlet includes a stator and a rotor. One of the stator or rotor includes a disc having a plurality of channels each of the channels extending from an inlet portion of the disc at or close to an inlet edge towards an outlet portion at or close to an outlet edge. The plurality of channels each has walls for guiding fluid flow from the inlet edge to the outlet edge in response to relative motion between the stator and the rotor. The disc further includes a plurality of protrusions extending from the channels, each of the protrusions being arranged to divide a channel at the inlet or the outlet end of the channel, into sub-channels that extend for a portion of a length of the channel and do not extend for a whole length of the channel.
Claims
1. A drag pump for pumping fluid from an inlet to an outlet said drag pump, comprising: a stator and a rotor; one of said stator or rotor comprising a disc comprising a plurality of channels, each of said channels extending from an inlet portion of said disc at or close to an inlet edge towards an outlet portion at or close to an outlet edge, said plurality of channels each comprising walls for guiding fluid flow from said inlet edge to said outlet edge of said disc in response to relative motion between said stator and said rotor; said disc further comprising a plurality of protrusions extending from said channels towards said other of said rotor or said stator, each of said protrusions being arranged to divide a channel at said inlet or said outlet end of said channel, into sub-channels that extend for a portion of a length of said channel and do not extend for a whole length of said channel.
2. The drag pump according to claim 1, wherein said protrusions do not extend along a mid portion of said channel.
3. The drag pump according to claim 1, wherein said protrusions have a length that is less than 60% of a length of one of said walls which said protrusion is adjacent to,
4. The drag pump according to claim 1, wherein said plurality of protrusions are arranged in each channel at an inlet end of said channels.
5. The drag pump according to claim 1, wherein said plurality of protrusions are arranged in each channel at an outlet end of said channels.
6. The drag pump according to claim 1, wherein said plurality of protrusions arranged at said inlet end of said channels extend from an inlet edge of said channel to a point beyond a line extending perpendicularly from a trailing wall of said channel.
7. The drag pump according to claim 6, wherein 50% or less of said protrusion extends beyond a line perpendicular to said trailing wall of said channel.
8. The drag pump according to claim 1, wherein said plurality of protrusions are arranged such that said sub-channels have substantially the same cross section.
9. The drag pump according to claim 1, wherein said plurality of protrusions are arranged such that said sub-channels each have a different cross sectional area.
10. The drag pump according to claim 1, said drag pump comprising a plurality of protrusions arranged between each of said channel walls such that said plurality of protrusions divides said channel into a plurality of three or more sub-channels.
11. The drag pump according to claim 1, wherein said protrusions have a thickness that varies along a length of said protrusions.
12. The drag pump according to claim 11, wherein said protrusions are configured to be thicker at an end adjacent to an edge of said disc and thinner towards a middle of said disc.
13. The drag pump according to claim 1, said inlet portion of said disc comprising an outer circumference of said disc.
14. The drag pump according to claim 1, wherein said drag pump comprises a Siegbahn drag pump, said channels being formed on a surface of a disc shaped stator.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0044] Embodiments of the present invention will now be described further, with reference to the accompanying drawings, in which:
[0045]
[0046]
[0047]
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[0050]
[0051]
DETAILED DESCRIPTION
[0052] Before discussing the embodiments in any more detail, first an overview will be provided.
[0053] Embodiments provide the addition of short vanes or sealing lands at the outlet and/or or inlet of a drag pump either on the stator or the rotor between the walls forming the channels to provide reduced cross sectional sub-channels and impede recirculation and provide more pumping surface.
[0054] For a drag pump such as a Holweck stage the compression ratio increases as a function of channel length L and velocity v.Math.cos α, where α is the angle between the channel and the direction of rotation, v.Math.cos α being the component of drag velocity along the channel.
[0055] Increasing rotational velocity for a drag pump has negative impacts on durability and balance, while increasing L, which is done in a Holweck pump by increasing the Holweck rotor & stator heights is in many applications undesirable as a pump's space claim is all too often limited.
[0056] The physical length of a channel can alternatively be increased by using a shallower channel angle, but as the angle reduces, the problems of recirculation of gases at the input and output, where there is a region of the channel that is in effect single sided, increases. This recirculation means that the flow back towards the inlet increases and we “lose” a considerable proportion of the extra length gained.
[0057] The mechanism by which a drag pumps works, and specifically a Holweck stage, is to influence the rate of relative flow of molecules (M12 from inlet to outlet, M21 from outlet to inlet) by adding a degree of momentum in the M12 direction. The geometry of the channels in conjunction with the direction of rotation of the rotor tend to bias the molecules towards the downstream or trailing wall as molecules pass through the stage, see
[0058] Further at the inlet and particularly for shallow angle Holwecks, the opportunity for reverse transmission of molecules (to re-exit the inlet) remains until they are shrouded by the “upper” channel wall & thus have no direct path back out of the stage.
[0059] With a steep angled channel design the length of the channel is severely limited by the Holweck's height or in a Siegbahn disc by the Siegbahn's diameter, thus a shallower angle is preferred to increase the channel length. However, on a shallower angled channel (of the same channel width) though the channel length can be greatly increased, a significant length of the channel at both the inlet & exhaust has only one side wall, see
[0060]
[0061]
[0062] In effect this protrusion or splitter vane creates an extension to the upper or leading channel wall 13 and provides positive blockage extending the effective channel length and thus reducing back leakage.
[0063]
[0064] In the embodiment of
[0065] The protrusions of
[0066] This design not only extends the effective Holweck channel length, but also adds a positive block to aid reverse transmission of molecules that have left the Holweck stage.
[0067]
[0068]
[0071] In summary a relatively short blade or splitter land will help address the recirculation and area ratio problems encountered by Siegbahn stages.
[0072] Although in
[0073] In summary advantages of embodiments include [0074] Maintaining capacity at the inlet & compression at the outlet; [0075] Enhanced pump performance within a pump particular space envelope.
[0076] Although illustrative embodiments of the invention have been disclosed in detail herein, with reference to the accompanying drawings, it is understood that the invention is not limited to the precise embodiment and that various changes and modifications can be effected therein by one skilled in the art without departing from the scope of the invention as defined by the appended claims and their equivalents.
[0077] Although elements have been shown or described as separate embodiments above, portions of each embodiment may be combined with all or part of other embodiments described above.
[0078] Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are described as example forms of implementing the claims.