1. Field of the technology
The present disclosure relates generally to peristaltic pumps and, more specifically, to a rotor assembly for a peristaltic pump.
2. Related Art
Current peristaltic pumping systems that are used in endoscopic surgeries, such as arthroscopy and hysteroscopy, create fluctuations in pressure and flow. These fluctuations are the result of rollers that rotate around an axis while applying force on a flexible tube that is typically wrapped around the rollers. In essence, this rotational motion of the rollers creates fluid pockets, within the tube, that continually get pushed through the tube, thereby creating flow. Due to the nature of these fluid pockets, the resultant flow and pressure of the rollers have a tendency to fluctuate. In surgery, this problem manifests itself as an unstable surgical environment that includes, without limitation, having a poor view for the surgical staff, movement of tissue or organ within the surgical cavity, varying cavity volume, and slow pump response to varying flow demands.
One method of addressing the above-stated problem has been to use an in-line chamber. The chamber is part of the tube, is located downstream of the rollers, and, in addition to containing liquid, is also partially filled with air so that it can act as a cushion to soften the fluctuations. The user is responsible for filling the chamber with the correct amount of liquid in order to ensure that a sufficient amount of air is left in the chamber. Often, users do not do this properly, which in turn substantially reduces the effect of the chamber. In addition to user error, this chamber is an added cost in the price of the tubing.
A peristaltic apparatus and method of application, that substantially reduces pressure and flow output fluctuations, is needed.
In one aspect, the present disclosure relates to a rotor assembly for a peristaltic pump. The rotor assembly includes a first rotor having a plurality of rollers and a second rotor, coupled to the first rotor, having a plurality of rollers. The rollers of the first and second rotors are located at an angle of about 45° relative to each other. In an embodiment, the first rotor and the second rotor are circular. In another embodiment, the rollers of the first rotor are located at an angle, about 90°, relative to each other. In yet another embodiment, the rollers of the second rotor are located at an angle, about 90°, relative to each other. In a further embodiment, the second rotor has a smaller diameter than the first rotor.
In another aspect, the present disclosure relates to a pump. The pump includes a first tubing and a second tubing, wherein the second tubing has a first end coupled to the first tubing and a second end coupled to the first tubing; an arcuate support surface arranged to support the first tubing, the first tubing being arranged to extend around the arcuate support surface; and a rotor assembly arranged to rotate about an axis, the first rotor including a plurality of rollers and a second rotor including a plurality of rollers, the second rotor coupled to the first rotor, the rollers of the first and second rotors located at an angle relative to each other. The rollers of the first rotor squeeze the first tubing against the support surface as the rotor assembly rotates and the rollers of the second rotor compress the second tubing as the rotor assembly rotates. In an embodiment, the first tubing has a larger diameter than the second tubing.
In yet another aspect, the present disclosure relates to a method of supplying fluid to a surgical area. The method includes providing a pump including a first tubing and a second tubing, the second tubing having a first end coupled to the first tubing and a second end coupled to the first tubing, an arcuate support surface arranged to support the first tubing, the first tubing being arranged to extend around the arcuate support surface, and a rotor assembly arranged to rotate about an axis, the rotor assembly including a first rotor having a plurality of rollers and a second rotor having a plurality of rollers, the second rotor coupled to the first rotor, the rollers of the first and second rotors located at an angle relative to each other; providing a fluid from a fluid source into the first and second tubings; operating the pump such that rotation of the rotor assembly causes the rollers of the first rotor to squeeze the first tubing against the support surface and create fluid pockets within the first tubing and causes the rollers of the second rotor to compress the second tubing and create fluid pockets within the second tubing. The fluid pockets of the first and second tubing are delivered to the surgical area by the first tubing.
Further areas of applicability of the present disclosure will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the disclosure, are intended for purposes of illustration only and are not intended to limit the scope of the disclosure.
The accompanying drawings, which are incorporated in and form a part of the specification, illustrate the embodiments of the present disclosure and together with the written description serve to explain the principles, characteristics, and features of the disclosure. In the drawings:
The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the disclosure, its application, or uses.
For the purposes of this disclosure, the rollers 24 of the second rotor 23 are located at an angle Θ of about 45° relative to the rollers of the first rotor 21. However, angle Θ may be more or less than 45°. The first rotor 21 has a larger diameter than the second rotor 23, with the first rotor 21 being between about 5 cm to about 10 cm and the second rotor 23 being between about 2 cm and about 4 cm. The part of the rotor shaft 50 that is extending out of the housing 10 is by means of a coupling 51 coupled to a motor 60 for rotating the rotor assembly 20 during operation.
First tube 30 is located between arcuate support surface 11 and the first rotor 21. Second tube 40 has a first end 41 and a second end 42, wherein each end 41, 42 is coupled to the first tube 30. The second tube 40 extends around the second rotor 23.
During operation, fluid flows from a fluid source (not shown) into the first tube 30 with some of the fluid entering the second tube 40 as the fluid approaches the rollers 22 of the first rotor 21. For the purposes of this disclosure, the fluid is saline, but may be another type of biocompatible fluid. The rotor assembly 20 rotates in a counter-clockwise manner, as indicated by arrow 70. The rollers 22,24 of the first and second rotors 21,23 apply pressure to the first and second tubes 30,40, which creates fluid pockets, within the tubes 30,40, that continually get pushed through the tubes 30,40, thereby creating flow. The fluid pockets of the second tube 40 are deposited into the first tube 30 at the second end 42. The fluid pockets of the first and second tubes 30,40 are then delivered to the surgical area.
Since the first and second rotors 21,23 are located on the same shaft, the velocity, or revolutions per minute (RPM) of the rotors 21,23 are the same. However, due to the rollers 24 of the second rotor 23 being located at an angle relative to the rollers 22 of the first rotor 21, there is a delay between when the first rotor 21 starts to push a pocket of fluid through the first tube 30 and when the second rotor 23 starts to push a pocket of fluid through the second tube 40. Additionally, as mentioned above, the second tube 40 has a smaller diameter than the first tube 30 and thus is capable of pushing smaller fluid pockets than the first tube 30. Consequently, the fluid flow rate of the first and second tubes 30,40 are different with the fluid flow rate of the first tube 30 having periods of high and low flow that are opposite the periods of high and low flow of the second tube 40, i.e. when the first tube 30 has a period of high flow, the second tube 40 will have a period of low flow and vice-versa. Therefore, it is believed that a flow and pressure output will result that has smaller fluctuations in pressure and flow as compared to rotor assemblies having one rotor delivering the fluid, via a tube, to a surgical site.
As various modifications could be made to the exemplary embodiments, as described above with reference to the corresponding illustrations, without departing from the scope of the disclosure, it is intended that all matter contained in the foregoing description and shown in the accompanying drawings shall be interpreted as illustrative rather than limiting. Thus, the breadth and scope of the present disclosure should not be limited by any of the above-described exemplary embodiments, but should be defined only in accordance with the following claims appended hereto and their equivalents.
This application claims the benefit of U.S. Provisional Application No. 61/031,799, filed Feb. 27, 2008, the disclosure of which is incorporated by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
3737251 | Berman et al. | Jun 1973 | A |
3787148 | Kopf et al. | Jan 1974 | A |
4537561 | Xanthopoulos | Aug 1985 | A |
4549860 | Yakich | Oct 1985 | A |
4564342 | Weber et al. | Jan 1986 | A |
4902277 | Mathies et al. | Feb 1990 | A |
4952372 | Huber | Aug 1990 | A |
5000733 | Mathies et al. | Mar 1991 | A |
5131823 | Guignard | Jul 1992 | A |
5257917 | Minarik | Nov 1993 | A |
5571389 | Kerampran | Nov 1996 | A |
5927956 | Lim et al. | Jul 1999 | A |
6527745 | Kanda et al. | Mar 2003 | B1 |
Number | Date | Country |
---|---|---|
1 498 376 | Jan 1978 | GB |
2 102 503 | Feb 1983 | GB |
WO0070225 | Nov 2000 | WO |
WO2006013316 | Feb 2006 | WO |
Number | Date | Country | |
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20090214366 A1 | Aug 2009 | US |
Number | Date | Country | |
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61031799 | Feb 2008 | US |