Method and system for measuring a property of a non-newtonian fluid

Abstract

A system and method for measuring the deformation over time of the surface of a non-Newtonian fluid in a sampling container in response to an airjet that is applied for a specified time are disclosed. The change is the sample surface displacement is measured quantitatively by means of optical triangulation or other similar optical or electronic distance measuring device. After cessation of the airjet, gravitational forces cause the sample material to flow back to its original surface profile. Both the amplitude of the deformation displacement due to the force of the airjet and the recovered displacement, within specific time periods are characteristic of asphalt binder material with varying amounts of polymer or other additives used to control the ultimate properties and performance of the material. As a result, comparison of the quantitative measurements of control samples can allow discrimination from samples with different properties and hence different formulations.

Claims

1. A method for measuring a property of a non-Newtonian fluid, comprising steps of: providing the non-Newtonian fluid held within a container and having an initial height; applying at least one fluid jet to a location on the surface of the non-Newtonian fluid held within the container for a first period of time to form a basin in the non-Newtonian fluid, the surface of the non-Newtonian fluid within the basin being displaced from the initial height by a first displacement distance amount, the container being different from an application surface to which the non-Newtonian fluid is finally applied; measuring the first displacement distance amount; measuring a second displacement distance amount relative to the initial height of the surface within the basin after a second period of time; and calculating a property of the non-Newtonian fluid based on a comparison of the first and second displacement distance amounts.

2. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the step of applying at least one fluid jet to a location on a surface of a non-Newtonian fluid comprises applying a single fluid jet.

3. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the step of applying at least one fluid jet to a location on a surface of a non-Newtonian fluid comprises applying a plurality of fluid jets.

4. A method for measuring a property of a non-Newtonian fluid according to claim 3, wherein the plurality of fluid jets are directed to a single location on the surface of the non-Newtonian fluid.

5. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the non-Newtonian fluid comprises asphalt.

6. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the step calculating is performed by a computer.

7. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the second period of time includes at least part of the first period of time in which the fluid jet is being applied.

8. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the second period of time includes a period after cessation of the application of the fluid jet.

9. A method for measuring a property of a non-Newtonian fluid according to claim 8, wherein the step of calculating a property of the non-Newtonian fluid comprises calculating the viscosity of the non-Newtonian fluid.

10. A method for measuring a property of a non-Newtonian fluid according to claim 9, wherein the step of calculating the viscosity of the non-Newtonian fluid is performed using the formula: =cln(1/kD)/D.sup.2, where D=airjet displacement of sample surface and c and k are numerical constants for the system.

11. A method for measuring a property of a non-Newtonian fluid according to claim 8, wherein the step of calculating the viscosity of the non-Newtonian fluid further comprises determining a temperature of the of the non-Newtonian fluid.

12. A method for measuring a property of a non-Newtonian fluid according to claim 11, wherein the step of determining the temperature of the non-Newtonian fluid is performed using a non-contact temperature sensor.

13. A method for measuring a property of a non-Newtonian fluid according to claim 1, wherein the step of applying at least one fluid jet to a location on a surface of a non-Newtonian fluid comprises applying an air jet.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a schematic diagram of the device for measuring characteristics of non-Newtonian fluids showing the key components in accordance with an embodiment of the invention.

(2) FIG. 2 shows the graphed displacement measurements over time for two samples of non-Newtonian fluids, in these cases asphalt binder.

(3) FIG. 3 shows a manifold with a plurality of tubes for directing air to a single convergent point in space to create a single linear jet of air with a uniform pressure over a variable working distance that is substantially coaxial with the laser beam or other sensing medium used to measure sample surface displacements.

(4) FIG. 4 shows another device configuration using a convergent conical cavity to generate a single linear jet of air with a uniform pressure over a variable working distance that is substantially coaxial with the laser beam or other sensing medium used to measure sample surface displacements.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S)

(5) The embodiments of the present invention comprise components and method for making quantitative measurements of the deformation of the surface of a non-Newtonian fluid over time in order to discriminate samples with varying properties. Various air jet tube configurations yield similar results, the objective being to create a flow of air emanating from a tube or nozzle that retains its cross sectional velocity profile for a working distance from the tube or nozzle end point to the surface of the sample being tested. Further, best results are obtained when the center of the air jet is coincident with the center of the measuring laser beam from the laser based displacement sensor.

(6) If the angle between the airjet and the laser beam is substantially greater than zero degrees, the airjet and the laser will be coincident at substantially only one point in space, the coincident point, requiring the sample container to be adjusted in height until the plane of the sample surface contains the coincident point.

(7) Using a plurality of tubes or nozzles as shown in FIG. 3, or a conical nozzle as shown in FIG. 4 air can be directed to combine into a substantially single jet of air with an approximately constant pressure cross section over a working distance of up to several inches. This allows for a simplified sample holder and reduces the need for precise adjustments to the sample container height. The system operates by applying an airjet to the sample surface, creating a force of that deforms the sample surface. Samples that have a low viscosity may be tested with a lower jet pressure to keep the deformation within the range of the displacement measuring device. A load cell may be included to measure the force of the airjet on the sample during test. The system can then use the force measurement to control the airflow so repeatable applications of force are applied to samples regardless of the air temperature, altitude and air pressure at the location where the tests are conducted.

(8) FIG. 1 shows a schematic diagram for a system for screening asphalt binder material to determine the presence of the expected constituent ingredients prior to the construction or maintenance of road surfaces. This device specifically measures the sample surface deformation in response to an applied force and the changes in surface displacement during a recovery period after the air jet is turned off.

(9) The system consisting of the following components and features. The force of gravity g 1 causes the surface 4 of asphalt binder sample 3 with mass (m) held in container 2 to become level over time. Once level, the container 2 is placed in a position such that both the laser beam 13 from the laser distance measuring device 10 and the off axis air jet 8 from tube 6 meet on the surface 4 of the asphalt binder material 3. The air jet may be formed by a single tube and impinge on the surface 4 at an angle. If a greater working distance range is desired, the use of multiple tubes as shown in FIG. 3 or a series of orifices in a ring manifold or a conical annular nozzle as shown in FIG. 4, causes the air flow to converge and form a single directed airjet 58 that may be both co-axial with the displacement measuring laser beam 13 from the displacement sensor 10 and retain a substantially constant pressure cross section over a working distance range of several inches. The used of an airjet 58 that is coaxial with laser beam 13 generally allows for more consistent results than the use of a single off axis airjet 8.

(10) Referring to FIG. 1, the test is performed during a time sequence controlled by the control computer 30 starting the acquisition of voltage data from the non-contact, pyroelectric temperature sensor 32 which is positioned to receive thermal radiation from sample 3 correlating use to determine the temperature of the sample. The control computer directs a jet of fluid, preferably air, against a location on a surface of the asphalt binder material for a first period of time. In the preferred embodiment, this is accomplished by the computer 30 opening the electrically activated solenoid valve 26, enabling the control line 24 to allow air from the constant pressure source 22 to flow through pipe 6 creating an air jet 8 that impinges on the surface 4 of the binder sample 3, causing the formation of basin 5 with a maximum displacement distance amount 7, which increases over time during the duration of the airjet, against the binder mass restoring force mg. A load cell located underneath and supporting the sample 3 in container 2 is used to measure the force applied to the sample surface 4.

(11) The computer will open or close the solenoid valve 26 to ensure a constant force is exerted by the airjet onto the sample surface. Note that the laser position sensor 10 produces a continuous electronic output signal 11 of the height of the binder surface 4 with respect to a set datum distance within the sensor 10 working distance range. At the beginning of the test, the sensor measured height from the sensor datum is subtracted from the displacement 7 measurements, in effect setting the output height of the surface 4 to zero creating a new datum based on the starting height of the surface 4 of the sample held in container 2. The actual height of the sample 3 surface 4 in container 2 can vary from sample to sample.

(12) When the test begins, the airjet acting on surface 4 of the sample surface starts the downward deformation 5 and the sensor 10 starts to output distance values 7 showing the displacement values from the start position. The distance values in inches or millimeters, may be presented either as positive or negative, however, as the restoring force acting on the sample is gravity and surface is actually deforming downward, we shall use negative distance values and by convention herein, an increasing displacement refers to a negative distance value that is increasingly further from the starting datum. Measurements of the binder surface height from the start datum are made continuously starting at a time just prior to opening the air jet valve, continuing thru the cessation of the air jet until the end of the measuring period time for the recovery.

(13) Commercially available laser based displacement sensors are generally comprised of a laser light source 12 that produces a substantially collimated laser beam 13 that reflects from the surface 4 and is scattered as a diffuse reflection. Some of this light 14 enters lens 16 and is focused onto a linear area of photosensors 18. The position of the focused laser beam spot 17 moves across the photosensor array 18 as the of the surface 4 of the sample 3 deforms 7 causing changes in the signal output 11 of the displacement sensor 10. The output of computer 30 is sent to a computer monitor 34 and displayed either numerically, graphically or both in a manner useful to the operator. Further, the computer program can be designed to provide data useful for evaluating material samples 4. For example, when the solenoid air valve 26 is opened for a programmed period of time 41 as shown on the graph in FIG. 2, the displacement is increasing. With the same air pressure and force from the constant pressure source 22, is applied for the same time period 41, the maximum displacement 7 of the sample 4 is shown as 46 for sample 50. At the end of time period 41, the air jet is turned off by deactivating solenoid valve 26.

(14) Samples can be compared by the total maximum displacement measured. Additional comparison data can be used to evaluate samples such as the determination of the percentage of recover over a set period of time 42, such as 120 seconds after cessation of the air flow (8 and 58). For sample test run 50, the percentage of recovery can be calculated as the Maximum deformation (D) 46 minus the Final Displacement, R, after recovery for a set period of time, 120 seconds, 48, divided by the maximum deformation 46.
Recovery %=DR/D

(15) The two sample tests graphed in FIGS. 2, 50 and 52, for sample 1 and sample 2 respectively, show very different responses. Sample 1, 50, has a larger deformation 46, due to the airjet than does Sample 2, 52 and better recovery 48 compared to 49. Sample 1 has additives in the asphalt binder, Sample 2 does not. For QC applications, base-line tests would be run on material samples. Then production tests would be run on new material to ensure the same results are obtained. The tolerance for variations can be set by testing material samples 4 with known variations in additive quantity. Algorithms change have tolerance factors requiring sample test results to be within a specified percentage of results for a know sample standard. Properties that can be measured include shear viscosity, viscoelasticity, yield stress and squeeze flow.

(16) Another test includes the determination of viscosity, , for a sample where the equation takes the form:
=cln(1/kD)/D.sup.2, where D=airjet displacement of sample surface c and k are numerical constants for the system.
The calculation could be formed mathematically, or by using a lookup table that is stored in memory.

(17) Another method for determining viscosity for asphalt binder viscosity measurements uses established equations with a factor k, which compensates for the lack of friction when using the airjet technology disclosed here in as a penetrometer. The k factor can be determined as the ratio of the penetration measurement made a penetrometer meeting ASTM D 5 and the penetration measured using the air jet technology described herein.

(18) In this method, the following equation should be used for penetrations less than 5.4 mm:

(19) $\begin{array}{cc}=\frac{1.559719{10}^9.Math.\ln \left(\frac{0.0275}{3.94{10}^{-6}.Math.P+0.000075}\right)}{P^2}& \left(k\right)\end{array}$
Where: p=viscosity in poise P=penetration in penetration mm k=machine constant determined experimentally

(20) This second equation should be used for penetrations greater than 5.4 mm

(21) $\begin{array}{cc}=\frac{1.559719{10}^9.Math.\ln \left(\frac{0.0275}{0.0005-\frac{0.0114488}{P}}\right)}{P^2}& \left(k\right)\end{array}$
Where: p=viscosity in poise P=penetration in penetration units. k=machine constant

(22) The data in Table 1 is based on the equations above and can be used as an alternative to hand calculations, multiplying the Viscosity in Poise by k.

(23) TABLE-US-00001 TABLE 1 Viscosity from Penetration Penetration Viscosity (Poise) 20 2.02 10.sup.7 21 1.83 10.sup.7 22 1.66 10.sup.7 23 1.51 10.sup.7 24 1.38 10.sup.7 25 1.26 10.sup.7 26 1.16 10.sup.7 27 1.07 10.sup.7 28 9.95 10.sup.6 29 9.24 10.sup.6 30 8.59 10.sup.6 31 8.02 10.sup.6 32 7.49 10.sup.6 33 7.02 10.sup.6 34 6.59 10.sup.6 35 6.19 10.sup.6 36 5.83 10.sup.6 37 5.50 10.sup.6 38 5.19 10.sup.6 39 4.91 10.sup.6 40 4.65 10.sup.6 41 4.41 10.sup.6 42 4.19 10.sup.6 43 3.98 10.sup.6 44 3.79 10.sup.6 45 3.61 10.sup.6 46 3.45 10.sup.6 47 3.29 10.sup.6 48 3.15 10.sup.6 49 3.01 10.sup.6 50 2.88 10.sup.6 51 2.76 10.sup.6 52 2.65 10.sup.6 53 2.54 10.sup.6 54 2.44 10.sup.6 55 2.35 10.sup.6 56 2.26 10.sup.6 57 2.17 10.sup.6 58 2.09 10.sup.6 59 .sup.2.02 106 60 1.95 10.sup.6 61 1.88 10.sup.6 62 1.81 10.sup.6 63 1.75 10.sup.6 64 1.70 10.sup.6 65 1.64 10.sup.6 66 1.59 10.sup.6 67 1.54 10.sup.6 68 1.49 10.sup.6 69 1.45 10.sup.6 70 1.40 10.sup.6 71 1.36 10.sup.6 72 1.32 10.sup.6 73 1.28 10.sup.6 74 1.25 10.sup.6 75 .sup.1.21 106

(24) FIG. 3 shows how a plurality of air jets 56 can be used to converge and form a single airjet 58 that is substantially coaxial with laser beam 13. Air 51 is supplied at pressure through tube 50 into a ring manifold 52. A plurality of tubes 54, are directed towards the sample surface 4, but converging at a spot located above the sample surface. Flow testing demonstrates the vector forces in the air jets combine to create a single jet, in space, directed towards the sample surface, but in a vector direction that is not aligned with any of the tubes used to create the jet 58. Two tubes 54 can be used, but the airjet formed tends to have an elliptical cross section. Three or four tubes 54 tend to produce a well formed air jet with a good working range of several inches.

(25) FIG. 4 shows an alternative arrangement that advantageously eliminates the tubes 54, by creating a hollow convergent cone of air 57 by applying air flow 51 through tube 50 into a circular manifold 55 machined in a cylindrical body 53 made of a material such as aluminum or plastic. A conical tapering hole 54 is machined through the body 53 to provide air flow 57 through an open orifice 60. A top plate 51 having hole 56 for the transmission of laser beam 13 and an inner cone 59 that channels air 57 into a single convergent air jet 58. Alternatively, these parts may be manufactured by precision castings or 3D printing technology.

(26) Preferably, the system is mounted on a mobile platform so as to permit testing of asphalt in situ in a location where it is being prepared for deployment. The mobile system also preferably includes its own electrical generator or storage capacity so that the system can operate in locations that do not have a readily available power source.

(27) It is to be understood, however, that even though numerous characteristics and advantages of the present invention have been set forth in the foregoing description, together with details of the structure and function of the invention, the disclosure is illustrative only, and changes may be made in detail, especially in matters of shape, size and arrangement of parts within the principles of the invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed.