The present invention relates to a rotary diaphragm positive displacement pump. Such a pump is disclosed in our own earlier EP0819853.
Such a rotary pump comprises a housing defining an annular chamber with inlet and outlet ports spaced apart around the chamber, a flexible annular diaphragm forming one side of the chamber spaced opposite an annular wall of the housing, the diaphragm being sealed at its edge to the housing, a partition extending across the chamber from a location between the inlet and outlet ports to the diaphragm; wherein the diaphragm is configured to be pressed progressively against the opposite wall of the housing to force fluid drawn in at the inlet port on one side of the partition around the chamber and to expel it at the outlet port at the other side of the partition.
In EP0819853, we added a reinforcement ring to the diaphragm in order to add rigidity to a central portion of the diaphragm so that it can cope with higher loads and to prolong the lifetime of the pump.
The pump has been commercially successful for application such as medical analysis and water dispensing. All of these applications are at a relatively low pressure (typically below 200 kPa but more normally below 100 kPa). However, at higher pressures, the current design of pump has a more limited life span.
The present invention is directed to modified version of the pump to allow it to operate more reliable at higher pressures over a longer period of time.
According to the present invention there is provided a rotary pump as defined in claim 1.
The presence of a trough at the part of the diaphragm which faces the inlet port and/or outlet port substantially reduces or eliminates the possibility of the diaphragm material being forced up into the inlet port and/or outlet port which could, over time, result in a failure of the diaphragm. As a result the pump can be operated at a higher pressure.
Preferably the trough is confined to the part of the outer face of the annular diaphragm which faces the inlet port and/or the part of the diaphragm which faces the outlet port. Confining the trough only to these regions provides full contact of the outer surface of the diaphragm with the annular wall of the housing thereby ensuring that the fluid is reliably circulated around the pump.
This modification can be applied with or without a reinforcement ring but preferably there is a reinforcement ring surrounding the rotating means and connected to the central region of the diaphragm.
The configuration of the rotary pump is preferably such that the diaphragm does not rotate relative to the housing.
An example of a pump in accordance with the present invention will now be described with reference to the accompanying drawings, in which:
As shown in
As the drive shaft 7 rotates, the bearing 5, reinforcing ring 4 and central portion of the diaphragm 3 all orbit together inside the housing. The two ends of the diaphragm 3 are clamped to the housing 1 by end caps 9, providing an effective and static seal to atmosphere. As the central portion of the diaphragm 3 orbits round inside the groove 2, line contact 10 exists between the diaphragm and the groove providing an abutment which pushes the fluid along towards the outlet port 11 and simultaneously draws fluid in through the inlet port 12. The pump thus provides pressure and suction cycles at the output and intake respectively which are symmetrical and which vary sinusoidally. Since the diaphragm does not rotate relative to the housing, there is minimal sliding action between them and therefore almost no wear.
From
The above description applies equally to the prior art pump of EP0189853. The modifications to the present pump will now be described.
The end caps 9 are best shown in
The end cap 9 has a tapered outer face 24 tapering inwardly away from the first end 20. This outer face 24 supports the diaphragm 3 when the diaphragm is in its radially innermost position as shown on the right hand side of
At the radially innermost portion of the second end 21 is an annular projection 25. The presence of this projection 25 forms a recess 26 which provides a step reduction in the outer diameter of the end cap 9 in the region adjacent to the second end 21. As can be seen from
As will be apparent from
The small nature of the second gap 28 also ensures that there is only a very small region of the compressible diaphragm 3 which remains unsupported as the diaphragm 3 is pressed against the end cap 9 (as shown in the right hand side of
The reinforcement ring 4 has a modified shape as best shown in
This comprises an embedded portion 30 forming the radially outermost portion of ring 4 and a support portion 31 forming the radially innermost portion of the ring 4. The embedded portion 30 has a crenulated configuration in this case consisting of four annular ridges which, in cross section, have a curved configuration which is devoid of sharp corners. This is to avoid any stress concentrations in the ring 4. These crenulations are designed to provide a large surface area within a relatively limited axial region. The diaphragm 3 is formed as an over mould on the ring 4 and the presence of the crenulations maximises the surface area for bonding between the two. The relatively large number of rings 32 combined with their generally curved cross sections effectively spreads the load transmission between the two components thereby avoiding delamination of the two components even under relatively high loads.
The support portion 31 of the ring 4 extends axially beyond the crenulations 32 forming diaphragm support portions 34. These have a radially outwardly facing surface 35 which directly faces an inner face of the diaphragm 3. The diaphragm 3 is not bonded to the face 35. However, in the position in which the diaphragm 3 is furthest from the housing 1, the diaphragm is supported in this region by the face 35.
This feature provides support for the diaphragm at a time when it is under a relatively high inward pressure from the pressure within the pump chamber. As with the gap 28 mentioned above, this support prevents extrusion of the diaphragm material in this stressed position.
As shown in
In the absence of these troughs 40, 41 when the diaphragm 3 is in the uppermost position, it is possible that while under high pressure, the diaphragm material will extrude into the port to a limited extent thereby causing damage to the diaphragm over time. The presence of the troughs 40, 41 reduces or eliminates this effect. However, trough terminates at edge 43 which is adjacent to the edge of duct 44 so that the full thickness of the diaphragm is available immediately downstream of the edge 43. This means that the diaphragm is able to fully engage with the housing 1 as the diaphragm reaches the top of its travel thereby ensuring that the point contact 10 is maintained up until the outlet duct 44 in order to expel the liquid. A similar geometry is provided for the inlet duct 45.
Reinforcing members 50 are best shown in
The reinforcing member 50 comprises a frame of material which is harder than the material of the partition and therefore more resistant to deflection under pressure. This is shaped to fit in a shallow recess 51 in the side of the partition. It is preferably a press fit but may be, more securely attached if the application requires it. As shown best in
With reference to
As can be seen from
Number | Date | Country | Kind |
---|---|---|---|
1711604 | Jul 2017 | GB | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/GB2018/051967 | 7/11/2018 | WO |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2019/016518 | 1/24/2019 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2246488 | Fraser | Jun 1941 | A |
2428619 | Douglas | Oct 1947 | A |
2460617 | Balogh | Feb 1949 | A |
2544628 | Copping | Mar 1951 | A |
2946291 | Roebig | Jul 1960 | A |
3507585 | Mercer | Apr 1970 | A |
5988998 | Glover | Nov 1999 | A |
20170016444 | Hodgson | Jan 2017 | A1 |
Number | Date | Country |
---|---|---|
0053868 | Jun 1982 | EP |
0819853 | Mar 2003 | EP |
1114877 | Aug 1954 | FR |
583578 | Dec 1946 | GB |
2256462 | Dec 1992 | GB |
S56143385 | Nov 1981 | JP |
Entry |
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GB Search Report for GB Application No. GB1711604.7 dated Dec. 15, 2017, 3 pages. |
International Search Report and the Written Opinion for International Application No. PCT/GB2018/051967 dated Sep. 26, 2018, 10 pages. |
Number | Date | Country | |
---|---|---|---|
20200166028 A1 | May 2020 | US |