MEASURING THE ENERGY ABSORBING CAPACITY OF A SUBSTRATE
FIELD OF INVENTION
This invention relates to apparatus for, and a method of, measuring the energy absorbing capacity of a substrate and, particularly, the application of this to providing a measurement of the "going" of a racecourse.
BACKGROUND TO THE INVENTION
A large proportion of horse-racing takes place on turf courses.
The "going" of a course varies depending on, among other things, how it has been managed and how wet it is. It is well-known that race times vary depending on the state of the course and that hard ground brings an increased risk of injury to horse and rider. During the run up to race meetings, and at the events themselves, the state of the course is of interest to the racing authorities, trainers, owners, jockeys and punters.
The "going" of a racecourse is traditionally measured by a person pressing a walking stick into the ground and that person making an assessment of the "going", e.g. as "soft", "firm" or "hard" (and in some cases seven levels of assessment are given). This assessment is, however, highly subjective, especially on firm ground, and even though such assessments are carried out only by a small number of highly experienced people, it is common for their assessments to vary. Moreover, in many cases, the "going" will be different on different parts of the racecourse.
Previously, various methods of assessing soil or ground characteristics have been devised, but none are adapted to measure the energy absorbing capacity of such a substrate.
Further, various attempts have been made to provide a quantitative measurement of the "going" of a racecourse but the applicants are unaware of any successful and reliable solution to this problem.
The present invention aims to provide apparatus and a method for providing a quantitative measurement of the energy absorbing capacity of a substrate and, in particular, the "going" of a racecourse.
SUMMARY OF THE INVENTION
Thus, according to a first aspect of the invention, there is provided apparatus for measuring the energy absorption capacity of a substrate, comprising: a probe; drive means for driving the probe into the substrate so that the probe penetrates the substrate; measuring means arranged to take a plurality of measurements of the force applied to the probe and of the displacement of the probe as the probe penetrates the substrate; and processing means arranged to integrate instantaneous readings of both said measurements to give a measurement of the energy required to drive the probe into the substrate and hence provide a measurement of the energy absorbing capacity of the substrate.
According to a second aspect of the invention, there is provided a method of measuring the energy absorbing capacity of a substrate comprising the steps of: driving a probe into the substrate so the probe penetrates the substrate, taking a plurality of measurements of the force applied to the probe and the displacement of the probe as it penetrates the substrate, and integrating instantaneous readings of both said measurements to provide a measurement of the energy required to drive the probe into the substrate and hence provide a measurement of the energy absorbing capacity of the substrate.
The invention also relates to the use of a measurement of the energy absorbing capacity of the surface of a racecourse to provide a quantitative assessment of the "going" of a racecourse.
Other features of the invention will be apparent from the following description and from the subsidiary claims of the specification.
The invention will now be further described, merely by way of example, with reference to the accompanying drawings, in which:
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a side view of a preferred embodiment of apparatus according to the invention;
Figures 2 and 3 are enlarged, front and bottom views of a preferred form of probe used in the apparatus; and
Figure 4 is a flow diagram of a preferred procedure for carrying out measurements using the apparatus.
BEST MODE OF INVENTION
The invention will hereinafter be described in relation to its use in providing a measurement of the "going" of a racecourse, the surface of which comprises turf, which is a very non-homogeneous material, although the invention can also be applied to other types of surface, e.g. bare earth, sand, snow or a synthetic surface (e.g. comprising a mixture of sand and organic or synthetic fibres). However, it will be appreciated that the invention may also be used for measuring the energy absorbing capacity of other sports surfaces, substrates carrying any form of traffic (human, animal or mechanical) or substrates used for any other purpose. The term "racecourse" as used herein includes courses used for training.
A first important feature of the present invention is the use of a measurement of the energy absorbing capacity of a racecourse to provide an assessment of the
"going" of the racecourse. As the "going" has, until now, been a subjective assessment, it was first necessary to select a measurement which was capable of reflecting this assessment. A wide variety of parameters could be measured, e.g. the hardness of the ground, its compaction, its stiffness or resilience, its composition, its water content etc, but the measurement of the energy absorbing capacity was selected as this was considered to most closely reflect the work done by a horse's hoof as it moves over the racecourse, and experimental trials have shown that the results provide a good match to the current subjective assessment of the "going" of a racecourse.
The energy absorbing capacity of the substrate may be defined as the energy required to drive the probe into the ground and/or the energy required to subsequently extract the probe from the ground.
The apparatus shown in Figure 1 comprises a probe 1 in the form of a substantially conical spike with substantially flat wings 2 attached on opposite sides thereof.
The probe 1 is secured to a mounting 2. The mounting 2 is secured to steel guide rails 2A which are slidably mounted within a guide unit 7. The guide unit 7 is rigidly mounted to four steel support rails 3 which are preferably provided at the corners of a square (when the apparatus is viewed from above) although other arrangements would be possible. The mounting of the guide rails 2A within guide unit 7 ensures that the probe can only move axially and cannot be displaced at an angle to the axis thereof. The mounting 2 is also attached by a shaft 2B to drive means in the form of a pneumatic cylinder 5 so that movement of a piston (not shown) within the pneumatic cylinder 5 causes the probe 1 to be moved axially, i.e. up and down in the orientation shown in Figure 1. The probe 1 can thus be moved so it passes through an aperture in a steel base plate 6 and can be retracted again to the position shown in Figure 1.
A force transducer 4 is mounted in the connection between the shaft 2B and the pneumatic cylinder to measure the force applied to the probe 1.
A position transducer 8 in the form of a rotary potentiometer is mounted on the apparatus and, in the arrangement shown, measures the axial displacement of the probe 1 by means of a pulley 9, band 10 and linkage rod 13. The linkage rod 13 is rigidly attached to the shaft 2B and to the band 10 so that linear motion of the probe 1 is converted into rotary motion of the potentiometer.
Other types of force and position transducers may be used.
The pneumatic cylinder 5 is controlled by a pneumatic control valve 11, which, in turn, is controlled by an electronic control unit 12.
As shown in Figures 2 and 3, the probe 1 preferably has a generally conical shape with substantially flat wings 1B on opposite sides thereof. The probe may, for example, comprise a solid steel cone 1A with wings 1B welded to the sides thereof or, as shown in Figure 3, the wings 1B may comprise a single sheet of steel with two halves 1 D and 1 E of a cone attached on opposite sides thereof. The wings 1B are substantially co-planar with the axis of the cone. More than two such wings may be provided if required.
In use, the apparatus is positioned with the base plate 6 held in firm contact with the ground. The drive means is then activated so the probe 1 is driven into and penetrates the ground. When the probe 1 stops moving, the drive means is reversed to extract the probe 1 from the ground until it is retracted above to a position above the base plate 6, as shown in Figure 1. The extent to which the probe penetrates the ground will be determined by the maximum force permitted by the air pressure applied to the pneumatic cylinder and the hardness of the ground.
Whilst the probe 1 is being driven into the ground, and preferably also whilst it is being extracted from the ground, readings are taken either continuously or at frequent intervals from the force transducer 4 and the position transducer 8 by the electronic control unit. In a preferred arrangement readings are taken at the rate of at least 100 samples per second and preferably at least 500 samples per second. In a preferred arrangement, the time taken to drive the probe into the ground is less than one second.
It will be appreciated that by integrating the instantaneous readings from the force transducer 4 and position transducer 8 during the time the probe is penetrating the ground and, again, whilst it is being extracted from the ground, the apparatus is able to measure the energy required to drive the probe into the ground (and, optionally, to extract it again) and thus obtain a measurement of the energy absorbed by the ground during the measurement cycle. Further details of methods of processing the readings taken will be given below.
The apparatus may, optionally, also be provided with an accelerometer 14 to measure the acceleration and/or deceleration of the probe 1. The accelerometer may be mounted on the shaft 2A and readings taken therefrom at similar intervals to the readings from the force transducer 4 and position transducer 8.
The accelerometer is preferably used to determine the maximum deceleration of the probe 1 as it penetrates the ground as it is found that, on some surfaces, e.g. synthetic surfaces comprising a compaction of loose material, this measurement can be used to help differentiate between "firm" and "hard" surfaces. It may also be used to provide a measurement of the hardness (or stiffness) of a surface which can be used to assess whether the surface is safe to use.
The maximum deceleration can be determined by scanning the readings from the accelerometer during the penetration phase of a measurement cycle to
locate the maximum reading, or a high speed sample and hold circuit (e.g. 10KHz) can be used to capture the maximum deceleration.
If an accelerometer is used, the apparatus is preferably arranged so that the tip of the probe is at least 20 mm away from the ground before a measurement cycle is initiated so that the probe has time to accelerate before it engages the ground. The apparatus is thus arranged so that the probe can be retracted to a position at least 20 mm above the base plate 9.
The shape of the probe 1 is designed so that it is sufficiently sharp to penetrate the ground, e.g. to penetrate through thick turf, and it has a conical or tapered shape so that the sides of the probe continue to deform the ground as the probe penetrates the ground. This ensures that useful readings can continue to be taken throughout the vertical extent of the travel of the probe as it penetrates the ground.
The wings 1 B provide additional resistance as the probe penetrates the ground and, because they are substantially flat, their sides also remain in contact with ground as the probe is withdrawn so that useful readings can be taken whilst the probe is being extracted from the ground.
In a preferred example of the apparatus, the probe has a length of about 150 mm (from the tip of the case to the base thereof) and the base of the cone has a width of about 60 mm and it has been found that the maximum force required to drive such a probe into dense ground is about 600 N.
The shape of the probe should also be such that it provides useful measurements in a range of different types of ground and over the range of "goings" likely to be encountered.
As mentioned above, the probe is preferably driven through a circular aperture in the base plate 6. The circular aperture preferably has a diameter slightly larger than the combined width of the base of the cone and the wings at the base of the cone, e.g. of about 80 mm. The base plate 6 is in contact with the ground as the probe penetrates the ground and it serves to restrain material displaced by the probe and limits the extent to which this displaced material can rise above ground level. This helps ensure that the ground is deformed in a uniform, controlled manner by the probe 1 so the apparatus provides more consistent and reliable measurements. This arrangement is also beneficial in preventing clods of soil adhering to the probe 1 so reducing the need to clean the probe between measurements.
The force transducer 4 is preferably an electronic analogue force transducer which is arranged to measure both pulling and pushing forces and it is arranged so that it is only subject to axial forces and is not subject to any lateral thrusts.
The electronic control unit 12 is preferably arranged to scan operation of a start switch (not shown) and controls the air supply to the pneumatic cylinder 5. When measurements have been taken, the control unit 12 makes a stepwise integration of the force and position data for penetration and extraction of the probe 1. The upward velocity of the probe is measured at the point when the tip of the probe is passing the ground surface. This velocity is used to compute the kinetic energy which is subtracted from the extraction energy integral to leave only that which is due to the ground condition. These results, together with data on the penetration distance, the penetration and/or extraction time, maximum force and, optionally, the acceleration/deceleration of the probe, are used for further processing, storage and display either by the control unit 12 or by other means connected thereto, e.g. a personal computer (not shown).
The control unit runs a background task that takes the analogue measurements and stores them in a ring buffer. The foregound task manages the start switch, monitors the ring buffer results for the end of penetration and the end of
measurement and drives the pneumatic control valves. It also integrates the force and position data and transmits each test result to the attached computer.
The computer receives each test result, scales the measurements into engineering units and updates a user display. The data for each test result is saved in a file.
Once a set of test data has been scaled and its validity checked, it is used to compute a numerical "going" rating. A number of "going" ratings are combined and presented as a measured "going".
Tests with the apparatus have been compared with subjective tests carried out in the manner described above and calibrated in relation thereto. The test results have provided consistent, repeatable readings, which are well-matched to the results of the subjective assessments.
As indicated above, it is found that, in some circumstances, a combination of a measurement of the energy absorption with a measurement of the maximum deceleration of the probe enables the "going", particularly a "firm" to "hard" "going" to be assessed more reliably. Tests have shown that the maximum deceleration on "hard" ground may be around 25 to 30 g, on "good" ground it may be around 2 to 3 g, and on "soft" ground it would be very small, e.g. less than 1 g.
Figure 4 shows a flow chart describing the function of the control unit 12. With the description given above, this flow chart is self-explanatory so will not be described further.
The apparatus described above enables a quantitative measurement of the "going" of a racecourse, which is more repeatable and more reliable than the current subjective assessment. It also enables a finer assessment of the
"going" and may, for example, give "going" ratings from 15 (for "heavy") to 85 (for "hard").
Ratings of 15 to 85 may, for example, be given as an assessment of the "going" corresponding to the conventional assessments as follows:
15 to 25 represent a "heavy" going;
25 to 35 represent a "soft" going;
35 to 45 represent a "good to soft" going;
45 to 55 represent a "good" going;
55 to 65 represent a "good to firm" going;
65 to 75 represent a "firm" going; and
75 to 85 represent a "hard" going.
More accurate measurements can be given by numbers within the above ranges, e.g. to indicate that the "going" is towards the hard or soft end of a given rating. This system is thus capable of providing 70 levels of assessment (i.e. the numbers from 15 through 85) ranging from the softest to the hardest "going". Other ranges and forms of calibration may, of course, be used in place of that described above.