Patent Grant
7980118
The present invention generally relates to a system, apparatus and a method for estimating the apparent viscosity of a non-Newtonian fluid, such as lubrication greases, inks and adhesives. This information is useful in designing fluid flow systems, such as (but not limited to) fluid dispensing systems and lubrication systems.
Apparent viscosity has been accepted increasingly by design engineers in sizing pumps and other components of fluid flow systems, such as grease lubrication systems. In general, the apparent viscosity of a fluid is defined as shear stress over shear rate. For non-Newtonian fluids, such as grease, the apparent viscosity changes at different shear rates. The standard method for measuring grease apparent viscosity is defined by ASTM D-1092. Using this method, the apparent viscosity of a non-Newtonian fluid can be measured at different shear rates. However, this method has several drawbacks. The test involves expensive equipment and takes time and effort to run. Further, a separate test must be run for each selected shear rate. Also, the test is not useful at shear rates less than 10 sec−1.
This invention is directed to a method of estimating an apparent viscosity of a non-Newtonian fluid by using test apparatus. The test apparatus comprises a conduit for receiving a non-Newtonian fluid under pressure, the conduit having an inside diameter D, a length L and a L/D ratio greater than 40, a valve system operable in a first mode to block fluid flow in the conduit to allow fluid to accumulate under pressure in a pressure zone of the conduit and in a second mode to vent the pressure zone of the conduit, and a pressure measuring device for measuring the pressure inside the pressure zone of the conduit. The method comprises
a) with the valve system operating in its first mode, supplying fluid under pressure to the conduit until the fluid in said pressure zone reaches a predetermined pressure;
b) operating the valve system in its second mode to vent the pressure zone of the conduit for a predetermined time interval during which there is a transition between non-Newtonian flow and Newtonian flow;
c) using the pressure measuring device, measuring the pressure P in the pressure zone during the transition;
d) calculating a wall shear stress τ of the fluid based on conduit length L, conduit diameter D, and the measured pressure P during the transition; and
e) determining an estimated apparent viscosity ηest of the fluid at a selected shear rate using a first formula ηest=τ/γs, where τ is the calculated wall shear stress and γs is the selected shear rate not based on any measurement of fluid output from the conduit.
In another aspect, a method of this invention further comprises the step of selecting equipment for a pumping system based at least in part on the estimated apparent viscosity ηest.
In another aspect, this invention is directed to a system for estimating an apparent viscosity of a non-Newtonian fluid. The system comprises a conduit for receiving fluid under pressure, the conduit having an inside diameter D, a length L and a L/D ratio greater than 40. A valve system is operable in a first mode to block fluid flow in the conduit to allow fluid to accumulate under pressure in a pressure zone of the conduit and in a second mode to vent the pressure zone of the conduit. A pressure measuring device is provided for measuring the pressure inside the pressure zone of the conduit. The pressure measuring device provides a pressure signal indicative of the pressure inside the pressure zone. A controller selectively operates the valve system in the first and second modes and receives the pressure signal. The controller also provides output information indicative of the viscosity of the fluid based on the conduit length L, conduit diameter D, and a measured pressure P when the valve mechanism is open and the fluid transitions from non-Newtonian flow to Newtonian flow. The viscosity is not based on any measurement of fluid output from the conduit.
Other objects and features will be in part apparent and in part pointed out hereinafter.
Corresponding reference characters indicate corresponding parts throughout the drawings.
In general, this invention is useful in the design of non-Newtonian fluid flow systems by providing a method of determining apparent viscosity. The design of a fluid flow system involves the determination of pressure drop in the system. To determine pressure drop, it is necessary to know the apparent viscosity of the fluid because the amount of pressure drop will vary depending on the apparent viscosity of the fluid used in the system. As apparent viscosity increases, the pressure drop inside supply and feed lines will also increase, and greater pump power is required for a given flow rate. The converse is also true. As apparent viscosity decreases, the pressure drop will decrease and less pump power will be needed. The method and apparatus of this invention for estimating apparent viscosity of a non-Newtonian fluid can be applied to many fluid flow systems, especially to those with flow generating shear rates in the range of 1-150 sec−1.
Similar calculations are necessary to properly size the fluid power capacity of the pump and tubing in a progressive lubrication system, such as the progressive system 31 shown in
One useful tool that has been used by design engineers is the “Ventmeter” tester, developed years ago by Lincoln Industries of St. Louis, Mo. This tester simulates the conditions and operation of a centralized lubrication system. As shown in
In one embodiment, the coiled metal tube 61 of the “Ventmeter” has a length of about 25 feet and an inside (flow) diameter of about 0.25 in. The tube may have other lengths and diameters. Desirably, the tube has a length (L) to diameter (D) ratio greater than 40 and even more desirably greater than 500. The vent line 71 has a flow diameter about the same as the flow diameter of the coiled tube 61, and desirably not substantially smaller than that of the coiled tube 61 so that it does not restrict flow from the tube during venting, as will be described.
In one embodiment, the two valves 75, 81 are needle valves movable manually between open and closed positions. In another embodiment, one or both valves are solenoid-operated valves. The first (venting) valve has a flow orifice not substantially smaller in diameter than the flow diameter of the coiled tube, and desirably about the same size or larger than the flow diameter of coiled tube so that the valve does not restrict the venting process, as will be described. Other valve systems are possible, including systems which have only one valve or systems which have more than two valves.
In the embodiment of
Prior to the present invention, the “Ventmeter” tester 51, 101 described above was used to estimate apparent viscosity by using the following test procedure. The pump 55 was operated with the first valve 71 closed and the second valve 81 open to prime the system with the lubricating fluid (e.g., grease) to be tested. After the coiled tube 61 was filled with fluid, the second valve 81 was closed to block further flow through the tube, and the pump 55 was operated to supply fluid under pressure to the coiled tube until the fluid in the conduit (i.e., tube 61) reached a predetermined pressure generally in the range of 1500-2200 psig and desirably about 1800 psig as measured by the pressure measuring device 85. The venting valve 75 was then operated (opened) to vent the coiled tube 61 via the vent line 71. During this venting process, the pressure in the tube 61 decreased, at first rapidly and then more slowly. The venting process was allowed to continue for a “venting” interval of time until the rate of pressure decrease was relatively small (e.g., less than about 5 psi/second over a period of 5 seconds). The pressure in the pressure zone 91 was then measured (using the pressure measuring device 85) and recorded manually. Desirably, the “venting” interval was equal to or greater than 30 seconds for tests conducted at lower temperatures. The weight of fluid vented from the vent line 71 during the “venting” interval was also measured and recorded.
The above information was then used to estimate the apparent viscosity of the lubricating fluid by using a series of calculations, as described below.
First, the wall shear stress of the fluid was calculated using the following formula 1:
τ=PD/4L (formula 1),
where L is the length of the conduit 61, D is the inside diameter (flow area) of the conduit 61, and P is the pressure in the pressure zone 91 as measured by the pressure measuring device 85 at the end of the “venting” interval.
Second, the approximate shear rate of the fluid was calculated using the following formula 2:
γ=(32Q)/(πD3) (formula 2),
where D is the inside diameter (flow area) of the conduit 61, and Q is the flow rate of the fluid vented during the “venting” interval determined by measuring fluid output (weight) over the time of the venting interval.
Third, the apparent viscosity of the fluid was calculated using the following formula 3:
ηa=τ/γ (formula 3).
The present invention represents an improvement over the previous testing methodology because it allows the apparent viscosity of the lubricating fluid to be determined without the need to measure fluid output during the venting process, thereby saving substantial time and effort. The new method can be conducted using the “Ventmeter” tester 51, 101 described above or other test apparatus comprising a conduit (e.g., coiled tube 61) for receiving a non-Newtonian fluid (e.g., grease) under pressure, where the conduit 61 has an inside diameter D, a length L and a L/D ratio greater than 40, a valve system (e.g., valves 75 and 81) operable in a first mode to block fluid flow in the conduit 61 to allow fluid to accumulate under pressure in a pressure zone of the conduit (e.g., pressure zone 91) and in a second mode to vent the pressure zone of the conduit, and a pressure measuring device (e.g., device 85) for measuring the pressure inside the pressure zone of the conduit.
The new method comprises the following steps:
Step (a) with the valve system (e.g., valves 75 and 81) operating in its first mode, supplying fluid under pressure to the conduit (e.g., 61) until the fluid in the pressure zone (e.g., 91) reaches a predetermined pressure;
Step (b) operating the valve system in its second mode to vent the pressure zone of the conduit for a “venting” time interval during which there is a transition between non-Newtonian flow and Newtonian flow;
Step (c) using the pressure measuring device (e.g., 85), measuring the pressure P in the pressure zone (e.g., 91) during the transition;
Step (d) calculating a wall shear stress τ of the fluid based on conduit length L, conduit diameter D, and the measured pressure P during the transition; and
Step (e) calculating an estimated apparent viscosity ηest of the fluid at a selected shear rate using a formula 4:
ηest=τ/γs (formula 4),
where τ is the calculated wall shear stress and γs is the selected shear rate not based on any measurement of fluid output from the conduit.
Using the “Ventmeter” tester (e.g., 51, 101), steps (a) and (b) are carried out in the same manner described above using the previous (“old”) test procedure. That is, after the system has been primed and the valves (e.g., 75, 81) moved to their closed positions, lubricating fluid is pumped into the coiled tube (e.g., 61) until the pressure reaches the desired predetermined pressure (e.g., in the range of 1500-2200 psig, and desirably about 1800 psig). The venting valve (e.g., 75) is then opened to vent the coiled tube for a venting time interval (e.g., 30 seconds) during which there is a transition from non-Newtonian flow and Newtonian flow. This transition is best illustrated in the graph of
In step (c) of the test method of the present invention, the pressure in the conduit pressure zone (e.g., 91) is measured at some time during the transition from non-Newtonian to Newtonian fluid flow. In the example of
In step (d) the wall shear stress τ of the fluid is calculated based on conduit length L, conduit diameter D, and the measured pressure P during the transition. In particular, the following formula may be used: τ=PD/4L (formula 1).
In step (e), an estimated (extrapolated) apparent viscosity ηest of the fluid can be calculated at a selected shear rate by using formula 4:
ηest=τ/γs (formula 4),
where τ is the wall shear stress calculated using formula 1 and γs is the selected shear rate. The selected shear rate is desirably in the range of 1 to 150 sec−1. Many fluids (greases, inks, adhesives, etc.) have shear rates in this range under typical dispensing and delivering conditions.
As a result, the estimated apparent viscosity at a selected shear rate can be calculated using just one pressure reading and avoiding the need to determine shear rate which would require measuring the fluid output (weight) over the time of the venting interval. As noted below with regard to
The following non-limiting example is provided to further illustrate steps (a) to (e) above. In this example, three tests were conducted, each involving steps (a) to (e). In each test, the “venting” interval was initiated when the pressure in the pressure zone, as measured by the pressure measuring device 85, reached about 1800 psi. During the venting interval, a pressure reading P was taken during the transition S2 (e.g., at about t=2 seconds). The tests results are tabulated below in Table 1.
Using the information in Table 1, the shear stress was calculated using formula (1) τ=P*D/(4L), where D=0.19 in. (corresponding to the inside (flow) diameter of the coiled tube 19) and L=300 in. (corresponding to the length of the tube). This calculation resulted in the information in Table 2 below.
Using the information in Table 2, the estimated apparent viscosity was calculated using formula (4) ηest=τ/γs (formula 4) at a selected shear rate of 67 sec−1, yielding the results in Table 3 below.
Optionally, the method of the present invention may also include a step (f) which calculates an “adjusted” estimated apparent viscosity having a value which correlates (compares to) the results of the ASTM D-1092 test method. In this step (f), the adjusted estimated apparent viscosity is calculated using the following formula 5:
ηadj=ηest(γs/γref)n (formula 5),
where ηest is the estimated apparent viscosity calculated using formula 4, γs is the selected shear rate (e.g., in the range of 1-150 sec−1), γref is a reference shear rate (to be explained later), and “n” is relatively stable number for a type of fluid at certain temperature in the selected shear rate range of 1-150 sec−1 (to be explained later).
Table 4 below represents the adjusted estimated apparent viscosities calculated using formula 5 and the information in Table 3. Three iterations of the test were run (i.e., Tests 1, 2, and 3) and two calculations were made, the first based on the results of Test 1 and the second on the results of Test 2. The results of Test 3 were not used. In the first calculation, the following numbers were used: ηest=8096.3 cP; γref=20 sec−1; “n”=0.36; and a selected shear rate of 67 (cP). In the second calculation, the following numbers were used: ηest=8731.7 cP; γref=30 sec−1; “n”=0.36; and a selected shear rate γs of 67 sec−1.
It will be observed from Table 4 that the adjusted estimated apparent viscosity at a shear rate of 67 sec−1 for Test 1 and Test 2 are 12511.3 cP and 11660.7 cP, respectively or, in other words, within a range of 11660.7-12511.3 cP. Table 5 below shows the apparent viscosities determined using the ASTM D-1092 test procedure.
Thus, at a shear rate of 67.0 sec−1, it will be observed that the adjusted estimated apparent viscosity determined by the test method of the present invention (i.e., 11660.7-12511.3 cP) compares favorably to the value obtained using the ASTM D-1092 test procedure.
In the above tests, steps (a)-(e) were repeated three times to determine three estimated apparent viscosities, and the largest and smallest of the three estimated apparent viscosities were used to calculate the corresponding adjusted estimated apparent viscosities. However, it will be understood that the number of tests conducted can vary from one to two or more. In one example, at least two tests are conducted to determine at least two estimated apparent viscosities ηesthigh and ηestlow, where ηesthigh is the greater of the two values. These values are then used to calculate an adjusted estimated apparent viscosity ηadj using formula 5, and the results are recorded.
Explanation of Adjustment Step (F)
As noted above, the formula used to calculate the adjusted estimated apparent viscosity of a non-Newtonian fluid is ηadj=ηest (γs/γref)n (formula 5). The manner by which this formula was derived is explained below.
τ=K*γn (formula 6),
where K is an unknown constant. Thus, the shear stress at two different times t1 and t2 (e.g., at a first time during the transition segment S2 of the “venting” interval and at a second time during the Newtonian segment S2 of the “venting” interval) would be:
τ1=K*(γ1)n
τ2=K*(γ2)n
or
τ1/τ2=(γ1/γ2)n (formula 7).
As noted below with regard to
τ1/τref=(γ1/γref)n
or
τ1=τref(γs/γref)n (formula 8),
at a selected shear rate γs. From formula 4, we have η=τ/γs, so that substituting formula 8 into formula 4 yields
ηadj=τ1/γ1=(τref/γ1)(γ1/γref)n (formula 9),
at a selected shear rate γs. But (τref/γs)=ηa=ηest in the approximate range of 20 to 30 sec−1, so formula 9 becomes
ηadj=ηest(γs/γref)n (formula 5),
for a selected shear rate γa.
Explanation of the Value of “n”
The value of “n” can be approximated because it is substantially the same for shear rates in the range of 1 to 150 sec−1. The reason for this is that, as noted above in regard to
It will be observed from formula 1 that the shear stresses τ1 and τ2 are directly proportional to pressure readings P1 and P2 taken at times t1 and t2, respectively, or:
τ1/τ2=P1/P2
or from formula 7
P1/P2=(γ1/γ2)n (formula 10)
If we consider pressure P1 to be a pressure PS2 measured during the transition segment S2 of the “venting” interval (e.g., at t=2 seconds), and if we consider pressure P2 to be a pressure PS3 as measured during the Newtonian flow segment S3 of the “venting” interval (e.g., at t=30 seconds), then, formula 10 becomes
PS2/PS3=(γS2/γS3)n (formula 11)
(The pressure PS3 measured during the non-Newtonian flow segment S3 of
Therefore, taking the natural log of formula 11 yields the following:
ln(PS2/PS3)=n*ln(γS2/γS3)
In tests conducted on common lubricating fluids (e.g., greases) using the previous “Ventmeter” test procedure and the ASTM test method, it has been determined that (γS2/γS3)is about 3, so that
n=ln(PS2/PS3)/ln3 (formula 12).
Using the “Ventmeter” tester 101, three tests were conducted on a lubricating fluid under the same ambient conditions. The initial pressures at the start of the intervals were measured (using device 85) to be 1801 psig, 1787.9 psig, and 1821.1 psig. Pressure readings PS2 and PS3 were taken at times t=about 2 seconds and t=about 30 seconds, respectively, yielding the results in Table 6 below.
Thus, based on this series of tests, “n” is about 0.36, which closely corresponds to the 0.3 value if “n” calculated using the ASTM data.
In using formula 5 to determine adjusted estimated apparent viscosity, the value of “n” can be determined in different ways. A first way is to assume that it is a particular number which has been determined to be reasonably accurate for the type of non-Newtonian fluid being tested within a specific shear range, such as 0.3 and 0.4 for grease at 72° F. and 32° F., respectively, for shear rates in the range of 1-150 sec−1. Alternatively, the value may be calculated as outlined above using pressure measurements PS2 and PS3, where PS2 is a measured pressure in the transition segment S2 of the “venting” interval and PS3 is a measured pressure in the third segment S2 of the “venting” interval. Further, this calculated value may be based on one test or multiple tests using an average of pressure readings PS2 and an average of pressure readings PS3.
Explanation of Correspondence between Adjusted and Apparent Viscosity for Shear Rates in the Approximate Range of 20 to 30 sec−1
Table 8 shows the estimated apparent viscosities (ηest) of fluids tested using the test method of this invention, the “Ventmeter” tester 101, and formula 4. The tests were conducted on shear thinning non-Newtonian fluids at shear rates ranging from 1 to 67 sec−1. Table 8 also shows the corresponding apparent viscosities determined using the ASTM D-1092 test method at shear rates of 17, 23, 33, 50 and 67 sec−1.
Table 9 shows “adjusted” estimated apparent viscosities (ηadj) based on the information in Table 8 and using the power-law relationship incorporated in formula 5, where “n”=0.3, the reference shear rate γref=20 (sec−1) for Test 4 and γref=30 (sec−1) for Tests 1-3 and 5. Table 9 also shows the corresponding apparent viscosities determined using the ASTM D-1092 test method at shear rates of 17, 23, 33, 50 and 67 sec−1.
Table 10 shows the percentage differences between the “adjusted” estimated apparent viscosities in Table 9 and the corresponding viscosities determined by the ASTM D-1092 test. The largest percentage difference is less than 15%.
Results in a Wider Shear Rate Range
The above analysis focuses on shear rates in the range of 17-67 sec−1.
Thus, using the “Ventmeter” testers 51, 101 and test procedures of this invention, the apparent viscosities of non-Newtonian fluids at selected shear rates can be quickly calculated. Once the apparent viscosity of a particular fluid is calculated, an engineer can use this information to select the appropriate equipment to be used in a pumping system, such as systems for delivering non-Newtonian fluids to a desired location. By way of example but not limitation, the information derived by using the testing apparatus and procedures of this invention may be used to determine the size of the pump, the size of the supply line(s) for delivering fluid from the pump, the maximum length of the supply line(s), and the type of fluid to be used under given ambient conditions. Further, this information can be determined without using the ASTM D-1092 test procedure.
In operation, a user provides user input to the controller 205 via the input device 213. The input includes the following information:
After the tube 61 is primed with the venting valve 75 closed, the controller 205 begins the process by closing the second valve 81. The controller 205 operates the pump 55 to pump fluid into the tube 61 to increase the pressure in the pressure zone 91 to about a predetermined pressure (e.g., about 1800 psig) as measured by the pressure measuring device 85. The controller then opens the second valve 81 to begin the “venting” interval. At some time t1 during the transition segment S2 of this interval (e.g., at t1=about 2 seconds), a pressure reading P is taken, as described previously. After the “venting” interval is over, the venting valve 75 is closed and the controller repeats the process N times. Desirably, the test results are recorded by a suitable recording device. The number of test runs (or iterations) “n” can be 1, 2, 3, 4 or more, and is desirably at least one. The controller then uses the collected information to calculate the adjusted estimated apparent viscosity, using formula 5 as described above, where γref is desirably in the range of about 20-30 sec−1 and using n=0.3. (If only one test is run, it is recommended to use γref=20 sec−1.)
Alternatively, the value of “n” can be calculated by taking two pressure readings PS2 and PS3 (using the pressure measuring device 85) and using these readings in formula (12), as explained above. These pressure readings PS2 and PS3 can be based on one test or an average of multiple tests.
If more than one test is run, that is, if N is greater than 1, it is desirable (but not essential) that the pressure reading(s) (PS2 and PS3) be taken at approximately the same times during the tests. For example, if two pressure reading PS2 and PS3 are taken during each test, it is desirable that the PS2 reading be taken at the same time during all of the tests, and that the PS3 reading be taken at the same time during the tests.
The apparatus and method of this invention can be used to estimate apparent viscosity in the range of 1-150 sec−1. The method is practical and efficient, and the method can be carried out using only the “Ventmeter” tester 55, 101 or similar apparatus which is relatively inexpensive. Unlike the previous procedure, there is no need to weigh the output of fluid from the conduit 61 during the “venting” interval. Further, using formula 5, the apparent viscosity can be easily determined at different selected shear rates. Another advantage of this method is that it allows the estimation of apparent viscosity at any shear rate value within the range of 1-150 sec−1. Conventional test methods provide apparent viscosity values only at certain shear rates within a more limited range.
When introducing elements of the present invention or the preferred embodiments(s) thereof, the articles “a”, “an”, “the” and “said” are intended to mean that there are one or more of the elements. The terms “comprising”, “including” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements.
In view of the above, it will be seen that the several objects of the invention are achieved and other advantageous results attained.
The order of execution or performance of the operations in embodiments of the invention illustrated and described herein is not essential, unless otherwise specified. That is, the operations may be performed in any order, unless otherwise specified, and embodiments of the invention may include additional or fewer operations than those disclosed herein. For example, it is contemplated that executing or performing a particular operation before, contemporaneously with, or after another operation is within the scope of aspects of the invention.
Embodiments of the invention may be implemented with computer-executable instructions. The computer-executable instructions may be organized into one or more computer-executable components or modules on a tangible computer readable storage medium. Aspects of the invention may be implemented with any number and organization of such components or modules. For example, aspects of the invention are not limited to the specific computer-executable instructions or the specific components or modules illustrated in the figures and described herein. Other embodiments of the invention may include different computer-executable instructions or components having more or less functionality than illustrated and described herein.
Having described aspects of the invention in detail, it will be apparent that modifications and variations are possible without departing from the scope of aspects of the invention as defined in the appended claims.
As various changes could be made in the above constructions and methods without departing from the scope of the invention, it is intended that all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
| Number | Date | Country | |
|---|---|---|---|
| 20090293594 A1 | Dec 2009 | US |
