Wear Prognosis Method And Maintenance Method

Abstract

A wear prognosis method and a maintenance method for an earth working machine are disclosed, along with an apparatus for performing the method. Provision is made that the current wear state of one or more earth working tools is sensed. The residual wear capacity until the wear limit is reached is then ascertained from the current wear state.

Claims

1- 23. (cancelled)

24. A method of determining wear for an earth working machine having at least one earth working tool with a first wear state, the method comprising during an earth working operation of the earth working machine: continuously determining an actual work output of the earth working machine from one or more machine parameters; determining a second wear state of the at least one earth working tool, based on a calculated change in wear from the first wear state corresponding to the continuously determined actual work output and a material property of a corresponding substrate worked since beginning the earth working operation; and predicting a remaining work output until a third wear state of the at least one earth working tool, based on an expected change in wear from the second wear state corresponding to a material property of a substrate yet to be worked during the earth working operation.

25. The method of claim 24, further comprising selectively storing the determined second wear state as the first wear state.

26. The method of claim 25, wherein the determined second wear state is stored as the first wear state for a new earth working operation.

27. The method of claim 25, wherein the determined second wear state is stored as the first wear state upon determining a change in substrate to be worked during the earth working operation.

28. The method of claim 24, wherein the at least one earth working tool includes a bit and/or a bit holder.

29. The method of claim 24, during the earth working operation further comprising: continuously determining the material property of the substrate being worked by the earth working machine, and reading out at least one characteristic value from a database, wherein the at least one characteristic value is derived from the determined material property and corresponding to a change in the wear state which is expected for a given work output in the substrate to be worked.

30. The method of claim 29, further comprising: identifying a working area within which two or more earth working machines are being used, wherein a characteristic value for the first one of the earth working machines is derived from a previously produced work output of the first one of the earth working machines and a change in wear state of the at least one earth working tool of the first one of the earth working machines corresponding to the previously produced work output; and wherein the characteristic value for the first one of the earth working machines in the working area is used to determine a remaining work output for a second one of the earth working machines in the working area.

31. The method of claim 24, further comprising: determining a second wear state for each of a plurality of earth working tools of the earth working machine; and determining a remaining work output for the earth working machine based upon each one of the plurality of earth working tools having at least a threshold residual wear capacity.

32. The method of claim 24, further comprising: planning a working process; and determining maintenance intervals for the earth working machine as a function of predicted remaining work output for each of a plurality of earth working tools as a function of the planned working process.

33. The method of claim 24, further comprising: ascertaining a planned route of travel during the earth working operation, and material properties associated with sub-areas to be traversed along the planned route of travel; and predicting a remaining work output until the third wear state of the at least one earth working tool, based on an expected change in wear from the second wear state corresponding to the material properties associated with the sub-areas.

34. A system for determining wear for an earth working machine having at least one earth working tool with a first wear state, the system comprising: a controller configured to continuously ascertain one or more machine parameters of the earth working machine during an earth working operation; and wherein the controller is configured during the earth working operation of the earth working machine to determine an actual work output of the earth working machine from the one or more machine parameters; determine a second wear state of the at least one earth working tool, based on a calculated change in wear from the first wear state corresponding to the continuously determined actual work output and a material property of a corresponding substrate worked since beginning the earth working operation; and predict a remaining work output until a third wear state of the at least one earth working tool, based on an expected change in wear from the second wear state corresponding to a material property of a substrate yet to be worked during the earth working operation.

35. The system of claim 34, wherein the controller is further configured to selectively store in a memory the determined second wear state as the first wear state.

36. The system of claim 35, wherein the determined second wear state is stored as the first wear state for a new earth working operation.

37. The system of claim 35, wherein the determined second wear state is stored as the first wear state upon determining a change in substrate to be worked during the earth working operation.

38. The system of claim 34, wherein the controller is in mutual communication with the earth working machine via a wireless remote data transfer link.

39. The system of claim 34, wherein the controller is further configured during the earth working operation to: continuously determine the material property of the substrate being worked by the earth working machine, and read out at least one characteristic value from a database, said characteristic value derived from the determined material property and corresponding to a change in the wear state which is expected for a given work output in the substrate to be worked.

40. The system of claim 39, wherein the controller is further configured during the earth working operation to: identify a working area within which two or more earth working machines are being used, wherein a characteristic value for the first one of the earth working machines is derived from a previously produced work output of the first one of the earth working machines and a change in wear state of the at least one earth working tool of the first one of the earth working machines corresponding to the previously produced work output, and wherein the characteristic value for the first one of the earth working machines in the working area is used to determine a remaining work output for a second one of the earth working machines in the working area.

41. The system of claim 34, wherein the controller is further configured to: determine a second wear state for each of a plurality of earth working tools of the earth working machine; and determine a remaining work output for the earth working machine based upon each one of the plurality of earth working tools having at least a threshold residual wear capacity.

42. The system of claim 34, wherein the controller is further configured to: plan a working process; and determine maintenance intervals for the earth working machine as a function of predicted remaining work output for each of a plurality of earth working tools as a function of the planned working process.

43. The system of claim 34, wherein the controller is further configured to: ascertain a planned route of travel during the earth working operation, and material properties associated with sub-areas to be traversed along the planned route of travel; and predict a remaining work output until the third wear state of the at least one earth working tool, based on an expected change in wear from the second wear state corresponding to the material properties associated with the sub-areas.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0032] The invention will be explained in further detail below with reference to an exemplifying embodiment depicted in the drawings, in which:

[0033] FIG. 1 is a side view of a bit, namely a round shank bit for a road milling machine, a mining machine, a surface miner, or the like, which is inserted into the holder of a quick-change holder tool for such machines;

[0034] FIG. 2 is a diagram showing the bit head of the bit according to FIG. 1;

[0035] FIGS. 3 to 7 are diagrams showing various wear states of the bit head;

[0036] FIG. 8 is a schematic depiction and side view of a milling machine;

[0037] FIG. 9 shows a milling drum of the milling machine in accordance with FIG. 8, having an example of a surveying device based on the triangulation principle;

[0038] FIG. 10 shows the milling drum in accordance with FIG. 8, having an alternative embodiment of the surveying device based on a shadow-casting method; and

[0039] FIG. 11 schematically depicts a working situation with two milling machines.

DETAILED DESCRIPTION

[0040] FIG. 1 shows, as an example of an earth working tool, a bit 10 as known from the existing art and described by way of example in DE 38 18 213 A1. Bit 10 comprises a bit head 12 and a bit shank 15 shaped integrally thereonto. Bit head 12 carries a bit tip 11 made of a hard material, for example of carbide metal.

[0041] This bit tip 11 is usually soldered onto bit head 12 along a contact surface. A circumferential pull-out groove 13 is recessed into bit head 12. This groove serves as a tool receptacle, such that a removal tool can be set in place and bit 10 can be removed from a bit holder 70.

[0042] Bit shank 15 carries a longitudinally slotted cylindrical clamping sleeve 21. This is held on bit shank 15 in lossproof fashion in the direction of the longitudinal dimension of bit 10, but freely rotatably in the circumferential direction. A wear protection washer 20 is arranged in the region between clamping sleeve 21 and bit head 12. In the installed state, wear protection washer 20 is braced against a countersurface of a bit holder 70 and against bit holder 70, facing away from the underside of bit head 12.

[0043] Bit holder 70 is equipped with a projection 71 into which a bit receptacle 72 in the form of a cylindrical bore is recessed. In this bit receptacle 72, clamping sleeve 21 is held with its external periphery clamped against the inner wall of the bore. Bit receptacle 72 opens into a drift opening 73. Through this, a drift punch (not shown) can be introduced for the purpose of removing bit 10. Said punch acts on the end of bit shank 15 in such a way that bit 10 is pushed out of bit receptacle 72 as the clamping force of clamping sleeve 21 is overcome.

[0044] As is evident from FIG. 1, extension 71 is equipped in a cylindrical region below wear protection washer 20 with two circumferential grooves. These grooves serve as wear markings 74. During operational use, wear protection washer 20 rotates and, in that context, can create wear (bit holder wear) on the support surface of projection 71. When the support surface has been worn away to the extent that the second wear marking has been reached, bit holder 70 is considered to be worn in such a way that it must be replaced.

[0045] Bit holder 70 comprises an insertion projection 75 that is introducible into an insertion receptacle 82 of a base part 80 and can be clamped there by means of a clamping screw 83.

[0046] Clamping screw 83 presses an abutment surface 76 of bit holder 70 onto a support surface 84 of base part 80. Although this is not depicted in further detail in FIG. 1, base part 80 itself is welded via its underside 81 onto the milling drum tube of a milling drum.

[0047] Noncontact surveying of bit head 12 is performed in order to ascertain the current wear state of bit 10 installed on the bit holder, a defined point or multiple points of bit head 12 being measured/ascertained as a position value. FIG. 2 is a side view of the contour of an unworn bit head 12. This contour is illustrated in a diagram, the dimension of bit head 12 in the direction of the longitudinal bit axis of bit 10 (X axis) being plotted against the dimension in the width direction (perpendicular to the longitudinal center axis, i.e. Y axis). The contour of bit head 12 (including bit tip 11) is assembled from a plurality of measured points, and the linear boundary (contour line) represents an interpolation of these position values.

[0048] Surveying of a milling drum 35 (see FIGS. 9 and 10) can be performed when bit 10 is in the unworn, worn-out, or partly worn state. These points, the calculated bit head contour, or even only a single measurement point can then be acquired and stored as a reference value in a memory unit.

[0049] FIG. 3 shows a variety of measured images of a bit 10, bit head 12 being depicted in the unworn state and in three measured wear states V1 to V3. Wear state V3 represents the state in which bit 10 is no longer suitable for further processing and must be replaced. The wear can be ascertained by comparing the reference value (contour in the unworn state) with the respectively measured current bit head contour (wear states V1, V2, or V3) that reproduce the position value.

[0050] The contours must be aligned with one another. Because of holder wear or other error sources, unworn contour regions are not necessarily located at the same absolute positions (or relative positions with respect to the drum rotation axis). In order to correlate the contours there is a further need for reference features that are uniquely identifiable, occur in the unworn and worn state, and thus permit alignment and conclusive evaluation. Pull-out groove 13, wear markings 74, wear protection washer 20, or other salient regions that are subject to little or no wear can serve as reference features.

[0051] As illustrated by FIG. 3, the length of bit head 12 decreases during operational use. By differentiating the contour lines in a circuit unit it is possible to generate a statement regarding the wear state, which can be made visible to the user, for example, in a display unit. Instead of surveying the entire contour of bit head 12, it is also possible to sense only a portion of the contour or a single point, in particular the front end of bit tip 11, as a position value. Further detail in the wear statement can be achieved if the wear on bit tip 11 and on bit head 12 (without bit tip 11) is sensed separately.

[0052] This can easily be done using the position (attachment point TP/attachment line 18), known a priori, at which bit tip 11 attaches to bit head 12 in the unworn state.

[0053] When the measured wear states V1 to V3 are overlaid on the unworn contour of bit head 12, as shown in FIG. 2, it is then possible to ascertain the total wear volume by integrating the measured contours along the X axis. In FIG. 4 the wear volume is shown as hatched areas.

[0054] The wear volume that constitutes a position value can thus be compared with a reference value. The reference value can be constituted by a functional relationship or a characteristics diagram, different wear volumes being correlated with associated wear states (for example, A mm.sup.3 of wear volume corresponds to B% wear). From the position, known a priori, of attachment point TP/attachment line 18, the tip wear 16 and head wear 17 can then also be separately ascertained by differentiation. This wear detection process provides the user, for example, with a qualitative statement as to whether bit 10 is still suitable for specific milling tasks. For example, a bit that has not yet reached its wear limit but exhibits some tip wear can no longer be used, for example, for precision milling work.

[0055] In the method according to FIGS. 3 and 4, the measured position values are overlaid on the reference values. During the working process, not only bit head 12 but also the bit holder becomes worn. The latter wears away in the direction of the longitudinal center axis of bit 10. Isolated identification of the longitudinal wear on the bit holder in this direction can now easily be achieved by the fact that the magnitude of the displacement of the position value toward the reference value in order obtain the overlays indicated in FIGS. 3 and 4 (shifting bit head 12 in the direction of the X axis, for example until the pull-out grooves of the individual wear states are superimposed) yields an absolute value for the wear on the bit holder. The total displacement of bit tip 11, minus said wear value, then separately indicates the bit wear.

[0056] FIG. 5 shows a variant method in which a wear statement is arrived at based on surveying one uniquely identifiable feature on the bit. The feature, or the surroundings of said feature, should be subject to little or no wear. According to FIG. 5, pull-out groove 13, a portion of pull-out groove 13, or a point (for example the groove base) on pull-out groove 13 is used as a unique feature and reference criterion.

[0057] The distance from this feature to the position of the free end of bit tip 11 (position value) is then further ascertained. It is then easy to ascertain the longitudinal wear in this manner. If the position of bit tip 11 is known, then once again, as described above, the bit holder wear can also be identified. Alternatively or additionally, as defined in FIG. 4, the wear volume and the associated wear lengths—X.sub.1 (currently measured length of partly worn bit), X.sub.2 (worn-out length), and Xges (total length of unworn bit)—can also be ascertained.

[0058] Relative measurement using a uniquely identifiable feature as reference point has the advantage that wear detection can be performed even when a reference measurement is not available, for example because the length of the replaced bit 10, or the wear state of bit 10 or of the bit holder, is not known.

[0059] FIG. 3 shows the change in the bit head contour as wear proceeds. The decreasing length of bit head 12 is evident. If the measured bit head contours are respectively shifted to the point of the maximum length of bit 10 (FIG. 6), the increasing wear state of bit 10 is evident on the one hand from the change in head angle (the angle becomes flatter as bit wear increases) and on the other hand from the increasing volume of bit head 12 when the area under the contour curve is integrated from the respective tip over a specific length. A functional relationship can thus be created between the head volume/area and the absolute bit length for a specific bit type, for example by means of experiments carried out a priori in order to ascertain the reference values.

[0060] Once this relationship is known, the length of bit 10 can be ascertained by measurement/integration of the respectively current head volume. This method requires, however, that bit tip 11 have a cross section that increases in the longitudinal direction of the bit. The integration path is preferably defined so that integration does not occur into the head region even for completely worn-out bits 10, since head erosion distorts the result.

[0061] This method has the advantage of not requiring a reference point that is subject to little wear. Such a reference point sometimes is not present or is very difficult to identify.

[0062] The average between the upper and lower contour line can, for example, be calculated in order to identify the degree of wear asymmetry. FIG. 7 shows the contour lines, and their averages, for a new bit tip 11 and for one that is worn rotationally symmetrically (R1) and rotationally asymmetrically (R2). It is evident that with the asymmetrically worn bit 10, the center line M2 of the two contour lines exhibits a certain slope with respect to the longitudinal bit axis. The angular position could easily be evaluated in order to determine the degree of wear asymmetry. The location/deviations of several contour lines could, however, also be identified/ascertained directly.

[0063] Asymmetrical wear on bit head 12 can be identified using the same method. Usually, however, an asymmetrically worn bit tip 11 will be accompanied by an asymmetrically worn bit head 12. An analysis of bit tip 11 is thus sufficient.

[0064] FIG. 8 symbolically depicts a milling machine 30, for example a surface miner, a road milling machine, or the like, in which a machine body 32 is carried by four columnar drive units 31. Road milling machine 30 can be operated from a control station 33. A milling drum 35 is arranged in a milling drum box 34.

[0065] In order to measure the wear state according to one of the methods described above, a light source 50 and a camera 40 are associated with milling drum 35. Milling drum 35 is shown more clearly in FIG. 9. A plurality of bit holder quick-change systems, each having a bit holder 70, are mounted on the surface of a milling tube 35.1 of milling drum 35. A bit 10 is held in each bit holder 70. In the present example, bit holders 70 are welded directly onto milling drum 35.

[0066] It is also conceivable, however, to use the quick-change bit holder system according to FIG. 1, in which case base part 80 is then welded onto milling drum 35.

[0067] An optical system, in which an elevation line of the drum surface is respectively surveyed in a kind of “scanning” operation, is used as an apparatus for surveying the bit contours. The measurement principle that can be used here is, for example, a triangulation method in which the drum surface is illuminated, for example, by a light source 50, for example a laser line. When the laser line thereby generated is observed by a camera 40 at a different angle, elevation differences on the drum surface (caused, for example, by bits 10) are evident as shifts of these projection lines. If the angular difference between camera 40 and light source 50 is known, the elevation coordinates can be calculated. By rotating milling drum 35 it is thus possible to create an elevation profile of the drum's enveloping surface, from which profile the contour line of the individual bits 10 can then be read out. A further optical measurement principle for surveying the elevation and/or geometry of bits 10 is the shadow-casting method according to FIG. 10. This method makes use of the fact that bits 10 moving through a light curtain generated by a light source 50 generate a shadow contour that can be observed and evaluated by a camera 40. The great advantage of this method lies in the fact that it is possible to work with a single camera row, in principle like a document scanner. This means that, in particular, even milling drums 35 having a large diameter and high rotation speeds can be surveyed with sufficient resolution.

[0068] The method described with reference to FIG. 10 can be modified in accordance with an alternative variant embodiment of the invention. Here once again a light curtain in the form of a light plane is generated using a light source 50. This light plane extends parallel to the longitudinal center axis of milling drum 35 and tangentially to the drum surface. The light plane is configured so that in the case of a rotating milling drum 35, the tips of bits 10 are the first to penetrate through the light plane.

[0069] They then cast a shadow that can be sensed by camera 40. Bits 10 are guided through the light plane over a specific drum rotation angle until they then sink again below the light plane.

[0070] A reference measurement can be performed with unworn bits 10/bit holders 70. Here the time at which bit 10 passes through the light plane (entry or exit) is sensed, and the associated rotation angle of milling drum 35 is sensed. After operational use, a corresponding measurement is then performed on the partially worn (worn out) bit 10. Because of the reduced length as compared with an unworn system, bit 10 passes through the light plane at a later time, and sinks below it sooner. The corresponding rotation angle of milling drum 35 can then be ascertained as a position value. These rotation angles are then compared with the rotation angles for the unworn system (reference value). A calculation of the wear state can then be made from the angle difference by differentiation, or the rotation angle difference is employed directly as a wear criterion.

[0071] During the milling process, for example in phases during which measurement does not occur, the measurement system is usefully stowed in a corresponding protective apparatus. If a second camera 40 is used, for example, direct surveying of the elevation geometry can be performed without an additional illumination source.

[0072] Alternatively, by correspondingly placing a second camera, additional measurements of the contours can be carried out so that the overall information density is increased and the detection probability for asymmetrical wear states is raised.

[0073] Alternatively, the position of bit tip 11 or the location of the bit head contour can also be sensed in at least one step using other sensor equipment that measures distance (e.g. ultrasonic sensors, proximity switches).

[0074] As already explained in detail above, the following can be ascertained using the measurement methods described above: [0075] 1. The current wear state V.sub.1, V.sub.2, V.sub.3 of an earth working tool (bit 10), [0076] 2. The wear resulting from comparison of a reference value (bit 10 in the unworn or partially worn state) with the current wear state V.sub.1, V.sub.2, V.sub.3.

[0077] In order for the wear according to item 2. above to occur, the earth working machine must have produced a certain milling output. This milling output can be measured, for example as a number of tons milled (milled mass), as a milled volume, and/or as a milled distance, etc. The milling output can in particular be ascertained directly on an earth working machine. If the earth working machine is equipped with a measurement system described above, the wear (see 2.) can also be sensed directly and the characteristic value or values can be derived in conjunction with the ascertained milling output.

[0078] Based on the measured current wear state V1, V2, and with a knowledge of the wear limit V3 of bit 10, the residual wear capacity of bit 10 can now be ascertained. For example, if the measured free end of bit tip 11 according to FIG. 5 represents the current wear state constituting a position value, the distance to the reference contour R reproducing the wear state, and thus the residual wear length (Xges-X1), can thus be ascertained as the residual wear capacity by differentiating in the X axis direction. Additionally or alternatively, the residual wear capacity can be ascertained as the residual wear volume of bit tip 11 remaining until the wear limit V3 is reached. This is done, for example (see discussion above of FIG. 4), by overlaying the measured wear state V1, V2 of the bit contour on the reference contour R in the worn state V3. The residual wear volume can then be ascertained by integration along the X axis.

[0079] The change in wear state is influenced by material properties, for example by the hardness and/or abrasiveness of the milled material. The material properties can be sensed indirectly. For example, samples can be taken (e.g. sample boring operations) in the area to be milled, and can be evaluated.

[0080] It is also conceivable to use existing mining category systems. General hardness and abrasiveness categories are defined for mines (e.g. “hard, non-abrasive,” “moderate, non-abrasive,” “soft, abrasive,” etc.). From these categories, the category matching the planned route of travel can be selected.

[0081] The material properties can also be ascertained by evaluating machine data (e.g. rotation speed of the milling drum, torque, advance, and milling depth), since the material properties correlate directly with these machine data.

[0082] Characteristic values can be ascertained as a function of the milling output and/or the material properties. These characteristic values indicate the change in the wear state which is to be expected for a specific milling output and/or for predefined material properties.

[0083] Based on the residual wear capacity and in consideration of one or more characteristic values, the remaining working output can then be signaled to the machine operator. He can be informed, for example, as to the milling output that can still be produced (e.g. mass or volume of material that can still be milled, number of truckloads that can still be milled, travel distance that can be milled, or milling time).

[0084] If the milling output per unit time for an earth working machine is known, it is also possible in particular to indicate the time remaining until the next tool change. The milling output per unit time can be continuously ascertained on the basis of current machine parameters (advance, milling depth). It can also be previously known based on milling work already carried out at the same location.

[0085] FIG. 11 illustrates a milling area F, for example a mine, in which multiple milling machines 30 are working. Milling area F contains a raw material deposit, and the material properties change in sub-areas F.sub.1, F.sub.2, F.sub.3.

[0086] These sub-areas F.sub.1, F.sub.2, F.sub.3 are associated in mine maps with hardness and abrasion categories (see above). Before work begins, the measurement system (for example, camera 40) ascertains the current wear state V.sub.1, V.sub.2 and conveys this, as well as the current position of the machine, via a transmission and reception apparatus 61 to an external system unit 60. There, in consideration of the calculated residual wear capacity and of one or more characteristic values, the remaining milling output until the wear limit V3 is reached is ascertained. The characteristic value ideally takes into account the planned route of travel and the various hardness and abrasion categories, associated therewith, in sub-areas F.sub.1, F.sub.2, F.sub.3, as well as the expected wear related to the hardness and abrasion categories. The ascertained working output until the wear limit V3 is reached is signaled back to milling machine 30.

[0087] Milling machine 30 depicted on the right in FIG. 11 has already traveled over sub-areas F.sub.1 and F.sub.2 and has acquired measured values in that context. These measured values can be evaluated. For example, it is possible to sense what kind of wear occurs with what milling output. This result, or the characteristic values resulting therefrom, can then be respectively made available to the second milling machine in FIG. 11 in order to improve the quality of the wear prognosis.