GEOGRIDS
20200283985 ยท 2020-09-10
Assignee
Inventors
Cpc classification
E02D29/0241
FIXED CONSTRUCTIONS
B29D28/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
There is disclosed a geogrid in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure formed of interconnecting mesh defining elements including elongate tensile elements wherein the molecular orientation of the mesh structure is uniform throughout the extent thereof. A method of making the geogrid is also described and its use in stabilizing, reinforcing or strengthening a mass of particulate material.
Claims
1. A geogrid in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure formed of interconnecting mesh defining elements including elongate tensile elements wherein the molecular orientation of the mesh structure is uniform throughout the extent thereof.
2. A geogrid in the form of an integral, mesh structure comprising polymeric material, the mesh structure comprising elongate tensile elements interconnected by junctions in the mesh structure wherein the junctions and the elongate tensile elements have the same mean thickness.
3. A geogrid as claimed in claim 2 wherein the polymeric material of the geogrid is uniformly molecularly oriented throughout the extent thereof.
4. A geogrid in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure comprising elongate tensile elements interconnected by junctions in the mesh structure wherein there is no thickening of the junctions caused by stretching of the polymeric material.
5. A geogrid as claimed in claim 1 wherein the cross-section of the tensile elements is uniform along their length.
6. A geogrid as claimed in claim 5 wherein the cross-section of the elongate tensile elements is rectangular.
7. A geogrid as claimed in claim 1 in which the polymeric material is uniaxially oriented.
8. A uniax geogrid as claimed in claim 7 having a Creep Reduction Factor (RF.sub.CR) determined in accordance with PD ISO/TR 20432:2007 on the basis of a Static Creep Tests in accordance with BE EN ISO 13431:1999 and Stepped Isothermal Method creep testing in accordance with ASTM D6992-03 of at least 55%, more preferably at least 60%, even more preferably at least 65%, and most preferably at least 70%.
9. A uniax geogrid in the form of an integral, mesh structure comprising polymeric material which is uniaxially oriented and where the geogrid has a Creep Reduction Factor (RF.sub.CR) determined in accordance with PD ISO/TR 20432:2007 on the basis of a Static Creep Tests in accordance with BE EN ISO 13431:1999 and Stepped Isothermal Method creep testing in accordance with ASTM D6992-03 of at least 55%, more preferably at least 60%, even more preferably at least 65%, and most preferably at least 70%.
10. A uniax geogrid as claimed in claim 7 having a thickness of 0.1 to 3 mm.
11. A uniax geogrid as claimed in claim 7 having a stretch ratio of at least 4:1.
12. A uniax geogrid as claimed in claim 7 having a tensile strength of at least 30 kN/m.
13. A uniax geogrid as claimed in claim 7 comprising: (i) a plurality of the elongate tensile elements extending parallel to each other in the direction of orientation, and (ii) a plurality of connector elements integral with the tensile elements and each serving to connect adjacent rib structures together, the connector elements connecting any two tensile elements together being spaced from each other in the direction of orientation thereby defining, with the tensile elements, elongate apertures extending parallel to the tensile elements.
14. A uniax geogrid as claimed in claim 13 wherein the tensile elements have a width of 2 to 50 mm, the apertures have a length of 40 to 400 mm and a width of 5 to 100 mm and the connector elements have a width (as measured in the longitudinal direction of the tensile elements of 2 to 20 mm.
15. A uniax geogrid as claimed in claim 14 wherein the tensile elements have a width of 5 to 40 mm, the apertures have a length of 40 to 250 mm and a width of 10 to 80 mm and the connector elements have a width of 6 to 18 mm.
16. A uniax geogrid as claimed in claim 11 wherein the connector elements are arranged as a plurality of sets in which the connectors of any one set are aligned with each other in a direction transverse to the rib structures and the sets are spaced from each other in the longitudinal direction of the rib structures.
17. A uniax geogrid as claimed in claim 7 comprising: (a) a plurality of generally parallel rib structures extending in the direction of uniaxial orientation, and (b) a plurality of spaced, generally parallel bar structures extending transversely (preferably perpendicularly) to the rib structures, said rib structures and said bar structures being interconnected by junctions at spaced locations along their respective lengths whereby the rib structures are sub-divided along their lengths into alternating junctions and rib segments and the bar structures are sub-divided along their lengths into alternating bar segments and junctions.
18. A uniax geogrid as claimed in claim 17 wherein the rib structures have a width of 2 to 50 mm the apertures have a length of 40 to 400 mm and a width of 5 to 100 mm and the bar structures have a width of 2 to 20 mm (as measured in the longitudinal direction of the rib structures).
19. A uniax geogrid as claimed in claim 18 wherein the rib structures have a width of 5 to 40 mm, the apertures have a length of 40 to 250 mm and a width of 10 to 80 mm and the bar structures have a width of 6 to 18 mm.
20. A uniax geogrid as claimed in claim 7 wherein the geogrid has integral beads of the polymeric material on a face of the geogrid at least partly around peripheral edges of the apertures.
21. A uniax geogrid as claimed in claim 20 wherein the beads are formed along the ends of the apertures and reduce to zero height along the elongate edges thereof.
22. A geogrid as claimed in claim 1 in which the polymeric material is biaxially orientated, optionally the biax geogrid having a stretch ratio of at least 1.5:1 and/or further optionally the biax geogrid having a tensile strength of at least 10 kN/m.
23. A method of producing a geogrid comprising the steps of: (a) stretching an elongate polymeric starting sheet to form a geogrid precursor comprising molecularly orientated polymer, the geogrid precursor being of essentially uniform thickness, and (b) converting the geogrid precursor into a geogrid by forming apertures in the geogrid precursor to define an integral mesh structure formed of interconnecting mesh defining elements including elongate tensile elements.
24. A method as claimed in claim 23 wherein the polymeric starting sheet has a mean thickness of 2 to 12 mm.
25. A method as claimed in claim 24 wherein the polymeric starting sheet has a mean thickness of 4 to 10 mm.
26. A method as claimed in claim 23 wherein the apertures are formed such that the elongate tensile elements are generally rectangular as seen in cross-section at right angles to the longitudinal extent of the elongate tensile elements, the length sides of the rectangular cross-section being along the faces of the geogrid.
27. A method as claimed in claim 26 wherein the apertures are formed such that the tensile elements have a width on opposite sides of the geogrid of 2 to 20 mm.
28. A method as claimed in claim 27 wherein the tensile elements width is from 6 to 18 mm.
29. A method as claimed in claim 27 wherein the apertures are formed to have a length of 40 to 250 mm and a width of 5 to 80 mm.
30. A method as claimed in claim 29 wherein the apertures have a length of 50 to 200 mm and a width of 5 to 50 mm.
31. A method as claimed in claim 23 wherein the stretching in step (a) is effected in a single direction to provide a geogrid precursor where the polymeric material is uniaxially orientated.
32. A method as claimed in claim 31 wherein, in step (a), polymeric starting sheet is stretched to a stretch ratio of at least 4:1.
33. A method as claimed in claim 32 wherein said stretch ratio is at least 7:1.
34. A method as claimed in claim 33 wherein said stretch ratio is from 7:1 to 12:1.
35. A method as claimed in claim 31 wherein the apertures are formed such that the tensile elements extend parallel to the stretching direction and the apertures are elongate and also extend parallel to that direction.
36. A method as claimed in claim 35 wherein the apertures are formed such that the mesh structure produced in step (b) comprises: (i) a plurality of the elongate tensile elements extending parallel to each other, and (ii) a plurality of connector elements integral with the tensile elements and each serving to connect adjacent rib structures together, the connector elements connecting any two tensile elements being spaced from each other in the stretching direction thereby defining, with the tensile element, the elongate apertures.
37. A method as claimed in claim 36 wherein the apertures are formed such that the connector elements are arranged as a plurality of sets in which the connector elements of any one set are aligned with each other in a direction traverse to the elongate tensile elements, and wherein the sets are spaced from each other in the longitudinal direction of the tensile elements.
38. A method as claimed in claim 36 or 37 wherein the apertures are formed such that the tensile elements have a width of 2 to 50 mm, the apertures have a length 40 to 400 mm and a width of 5 to 100 mm and the connector elements have a width (as measured in the longitudinal direction of the tensile elements) of 2 to 20 mm.
39. A method as claimed in claim 38 wherein the tensile elements have a width of 5 to 40 mm, the apertures have a length of 40 to 250 mm and a width of 10 to 80 mm and the connector elements have a width of 6 to 18 mm.
40. A method as claimed in claim 35 wherein the apertures are formed such that the mesh structure produced in step (b) comprises: (i) a plurality of generally parallel rib structures extending in the direction of uniaxial orientation, and a plurality of spaced, generally parallel bar structures extending transversely (preferably perpendicularly) to the rib structures, said rib structures and said bar structures being interconnected by junctions at spaced locations along their respective lengths whereby the rib structures are sub-divided along their lengths into alternating junctions and rib segments and the bar structures are sub-divided along their lengths into alternating bar segments and junctions.
41. A method as claimed in claim 40 wherein the apertures are formed such that the rib structures have a width of 2 to 50 mm, the apertures have a length of 40 to 400 mm and a width to 5 to 100 mm, and the bar structures have a width (as measured in the longitudinal direction of the rib structures) of 2 to 20 mm.
42. A method as claimed in claim 41 wherein the rib structures have a width of 5 to 40 mm, the apertures have a length of 40 to 250 mm and a width of 10 to 80 mm and the bar structures have a width of 6 to 18 mm.
43. A method as claimed in claim 35 wherein the apertures are provided by a punching operation.
44. A method as claimed in claim 43 wherein the punching operation forms integral beads of the polymeric material on a face of the geogrid and at least partly around peripheral edges of the apertures.
45. A method as claimed n claim 44 herein the beads are formed along the ends of the apertures and reduce to zero height along the elongate edges thereof.
46. A method as claimed in claim 23 wherein the sheet starting material is stretched in two mutually perpendicular directions to produce a geogrid precursor where the polymeric material is biaxially orientated.
47. A method of producing a geogrid comprising the steps of: (a) providing a geogrid precursor in the form of a polymeric starting sheet comprising polymeric material uniformly molecularly orientated throughout the extent of the sheet, and (b) converting the geogrid precursor into a geogrid by forming apertures in the geogrid precursor to define an integral mesh structure formed of interconnecting mesh defining elements including elongate tensile elements.
48. A method as claimed in claim 47 wherein the geogrid formed in step (b) is in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure formed of interconnecting mesh defining elements including elongate tensile elements wherein the molecular orientation of the mesh structure is uniform throughout the extent thereof.
49. A geogrid obtained and/or obtainable by a method as claimed in claim 23.
50. A method of strengthening a particulate material, comprising embedding in the particulate material a geogrid as claimed in claim 1.
51. A particulate material strengthened by the method of claim 50.
52. A geoengineering construction comprising a mass of particulate material having embedded therein a geogrid as claimed in claim 1.
53. A geoengineering construction as claimed in claim 52 selected from the group consisting of: embankment foundation, railway track ballast and/or sub ballast; road bed foundation, bridge abutment, retaining wall, steep (20 degrees) slope, slip repair, steel mesh face, wraparound face, terraced wall, wall and slope, vegetated face, non-vegetated face, modular blocks, concrete panel, marine unit and/or gabion face.
54. A geoengineering construction as claimed in claim 52 where the geogrid imparts to the geoengineering construction an improvement (compared to the construction absent said geogrid) in at least one property selected from: strength; stabilization, reduced layer thickness; increased life; increased bearing capacity; control of differential settlement; ability to cap weak deposits, and/or ability to span voids of and/or beneath the particulate material and/or geoengineering construction.
55. A geoengineering construction as claimed in claim 52 comprising a mass of particulate material improved in at least one property selected from: strength; stabilization: reduced layer thickness; increased life; increased bearing capacity; control of differential settlement; ability to cap weak deposits; and/or ability to span voids of and/or beneath the particulate material and/or geoengineering construction by embedding therein a geogrid in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure formed of interconnecting mesh defining elements including elongate tensile elements wherein the molecular orientation of the mesh structure is uniform throughout the extent thereof.
56. Use of a geogrid as claimed in claim 1 with a particulate material to form a geoengineering construction for at least one purpose selected from the group consisting of: strengthening; stabilizing, reducing layer thickness; increasing the life of; increasing bearing capacity; controlling differential settlement; capping weak deposits, and/or spanning voids of and/or beneath the particulate material and/or geoengineering construction.
57. Use of a geogrid in the form of an integral, mesh structure comprising molecularly orientated polymeric material, the mesh structure formed of interconnecting mesh defining elements including elongate tensile elements wherein the molecular orientation of the mesh structure is uniform throughout the extent thereof with a particulate material to form an improved geoengineering construction as claimed in claim 55.
Description
[0103] In the figures referred to herein some of the reference numbers refer to the following elements: 1 denotes a geogrid generally; 2 denotes rib structures; 3 denotes bar structures; 4 denotes elongate apertures; 5 denotes junctions; 6 denotes a rib segment or strand; 7 denotes a bar segment; and 10 denotes a pressure mark.
[0104]
[0105]
[0106]
[0107]
[0108]
[0109]
[0110]
[0111]
[0112]
[0113]
[0114] Expressed alternatively, the geogrid 1 shown in
[0115] There are a number of points to note about the geogrid 1. Firstly, the geogrid is of generally uniform thickness. Any deviation from non-uniformity is likely to result for the case where the web material (from which the geogrid is produced) is unrestrained in the width direction during the stretch in the length direction, in which case the marginal edge regions of the stretched web may be slightly thicker than the central region (these marginal edges may be removed from the commercial product). There may also be some localised non-uniformity in thickness around parts of the apertures. Secondly, the degree of orientation in the MD direction is the same throughout the geogrid.
[0116] It will therefore be appreciated that the uniax geogrid 1 of
[0117] Reference is now made to
[0118] The pressure mark 10 provides reinforcement at the ends of the apertures and as such inhibits tearing of the connector 7 (bar segment) from one edge to the other. Although not illustrated in
Example 1 (FIGS. 1, 2, 3a, 3b & 4)
[0119] In this Example, the method of the invention was used for producing a geogrid from an extruded, initially unoriented sheet of High Density Polyethylene (HDPE) having an indefinite length, a width of 1515 mm and a nominal thickness of 6.35 mm (giving a cross-sectional area of approximately 9620 mm.sup.2).
First Step
[0120] In a first step of the process, the sheet of unoriented HDPE was heated to a temperature of about 105 C. and then drawn (in the length direction, LD or MD) at a nominal draw ratio of about 10:1 prior to cooling. No restraint on width was applied to the web during the drawing step. Samples of the oriented web were then cut for further processing in the second step of the process (see below).
[0121] The width of the oriented web was 1249 mm (the reduction as compared to the starting width of 1515 mm being due to lack of width restraint during the draw process) and it was noted that the oriented web was somewhat thicker at the outer marginal regions (about 50 mm inbound of each edge) than at the centre.
[0122] The average thickness of the oriented web was determined to be 0.76 mm, giving a cross-sectional area of about 949 mm.sup.2. This compares with a cross-sectional area of about 9620 mm.sup.2 for the starting material, thus confirming the anticipated draw ratio of about 10:1.
[0123] Second Step
[0124] In the second step of the process, samples of the sheet of oriented HDPE obtained from the first step were perforated to produce a geogrid 1 as shown in
[0125] Perforating was effected by feeding the samples (in the length direction, LD or MD) through a perforating station provided with side-by-side matched punches and dies having a length of 25.4 mm. The punches had radiused ends and formed waists where the width at their mid-points was less than at their ends. To produce the geogrid the punching station was programmed to make a single stroke followed by 13 consecutive 14.6 mm index strokes followed by a larger single index of 41.28 mm to form the transverse bar. The punch tool formed an aperture that formed slight waists of narrower widths intermediate to the width at its ends (the punch has a corresponding waist shape).
[0126]
Example 2 (FIG. 5)
[0127] For a uniax geogrid intended for soil reinforcement applications such as in walls or slopes, two properties of the material of the geogrid are especially useful. The first is the short-term tensile strength and the second is the percentage of the short-term tensile strength available for the long-term creep performance of the product.
[0128] This Example demonstrates short term tensile testing of rib segments cut from the geogrid produced in accordance with Example 1 and compares the results with those obtained for a conventional uniax geogrid commercially available from Tensar International Ltd under the designation RE560. Tensile test specimens in accordance with ISO10319 were cut from the geogrid produced in accordance with Example 1. Tensile testing was carried out according to ISO10319 on a testing machine available from Instron, with the jaws drawn relatively apart at a rate of 20% of the specimen gauge length in accordance with the ISO10319 Standard. The results are shown in the following Table.
TABLE-US-00001 Strain at Strength at Strength at Strength At Max Load 2% Strain 5% Strain Max Load Ex (%) (kN/m) (kN/m) (kN/m) 1 5.9 43.66 75.65 85.51 2 6.33 41.64 73.4 88.06 3 5.63 43.22 76.3 83.22 4 5.96 40.7 72.7 83.12 5 6.03 42.94 75.6 86.95 Mean 5.97 42.44 74.7 85.37
[0129] For the purposes of comparison
[0130]
[0131] The data in
Invention=(85.4/0.50)=171(kN/m)/(kg/m.sup.2)
RE560=(94.0)/0.62=152(kN/m)/(kg/m.sup.2)
[0132] Thus the gain in short-term tensile efficiency of the geogrid of the invention over an equivalent strength conventional uniax product is about 12.5% on the basis of weight of polymer.
[0133] Furthermore,
Example 3 (FIG. 6)
[0134] This Example demonstrates the creep properties of a geogrid produced according to Example 1 in comparison with those of a conventional equivalent strength uniax product.
[0135] A sample of geogrid produced in accordance with Example 1 was subjected to a static creep test according to BS EN ISO 13431:1999 at 20 C. using a load corresponding to 60% of short term tensile strength. For comparison an example of a conventional equivalent strength uniax geogrid (RE560) was subjected to the same 20 C. temperature and load corresponding to 60% of its short-term tensile strength. The results are shown in
[0136] A comparison of the two data plots (15, 17) in
Example 4 (FIG. 7)
[0137] Conventional static creep loading carried out in accordance with BS EN ISO 13431:1999 formed part of a Time Temperature Superposition (TTS) creep program to establish a creep reduction factor RFcr in accordance with PD ISO/TR 20432:2007. As part of the process of establishing RFcr, in addition to the aforementioned TTS creep program, a Stepped Isothermal Method (SIM) program of creep testing was also carried out in accordance with ASTM D6992-03.
[0138]
[0139] The data in
Invention=(85.4*72%)/0.50)=123(kN/m)/(kg/m.sup.2)
RE560=(94.0*47.5%)/0.62)=72(kN/m)/(kg/m.sup.2)
[0140] Thus the gain in long-term creep limited tensile efficiency of the geogrid of the invention over an equivalent strength conventional uniax product is about 60% on the basis of weight of polymer.
Example 5 (FIGS. 8, 8A & 8B)
[0141] Shrinkage Reversion test for molecular orientation.
[0142]