Classifications

• • E—FIXED CONSTRUCTIONS
  • E21—EARTH OR ROCK DRILLING; MINING
  • E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
  • E21D5/00—Lining shafts; Linings therefor
  • E21D5/06—Lining shafts; Linings therefor with iron or steel
  • E21D5/10—Lining shafts; Linings therefor with iron or steel in the form of tubbing or of rings composed of profile elements
• • E—FIXED CONSTRUCTIONS
  • E21—EARTH OR ROCK DRILLING; MINING
  • E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
  • E21D11/00—Lining tunnels, galleries or other underground cavities, e.g. large underground chambers; Linings therefor; Making such linings in situ, e.g. by assembling
  • E21D11/14—Lining predominantly with metal
  • E21D11/15—Plate linings; Laggings, i.e. linings designed for holding back formation material or for transmitting the load to main supporting members
  • E21D11/155—Laggings made of strips, slats, slabs or sheet piles
• • E—FIXED CONSTRUCTIONS
  • E21—EARTH OR ROCK DRILLING; MINING
  • E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
  • E21D11/00—Lining tunnels, galleries or other underground cavities, e.g. large underground chambers; Linings therefor; Making such linings in situ, e.g. by assembling
  • E21D11/38—Waterproofing; Heat insulating; Soundproofing; Electric insulating
  • E21D11/385—Sealing means positioned between adjacent lining members

Definitions

• This application relates generally to liner systems for vertical mine shafts and underground tunnels and, more particularly, to liner plate system and method for providing a waterproof shaft or tunnel.
• a liner plate structure for use in lining shafts and tunnels includes a primary plate portion and at least one flange disposed at a side edge of the primary plate portion.
• a thermoplastic fusion element extends along an exterior surface of the flange.
• thermoplastic fusion element of the flange is disposed within a recess of the exterior surface of the flange.
• the thermoplastic fusion element of the flange includes a multi-layer assembly including at least one thermoplastic fusion layer at the outer side of the recess and at least one elastic polymer layer below the thermoplastic fusion layer for permitting compression of the thermoplastic fusion element within the recess.
• the thermoplastic fusion layer protrudes slightly above the exterior surface of the flange.
• At least one electrofusion chord element is embedded within the thermoplastic fusion layer.
• thermoplastic fusion element has a width that is less than a width of the recess.
• a sub-recess is located to one side of the recess.
• the sub-recess has a depth that is less than the depth of the recess, and the sub-recess has one side edge in communication with the recess.
• the sub-recess includes at least two spaced apart extensions, each of which extends to an inward facing edge of the flange.
• thermoplastic fusion element in the liner plate structure of one of the preceding aspects, includes at least one electrofusion chord element with end portions extending inward through an opening or openings in the flange and terminating at an interior side of the liner plate structure.
• first, second, third and fourth flanges circumscribe the primary plate portion, each flange has a corresponding recess and electrofusion element, the recesses align to form a circumscribing recess and the electrofusion elements are joined to form a circumscribing electrofusion element.
• the primary plate portion has a height and length, the length larger than the height, the primary plate portion is curved in the lengthwise direction.
• a structural member protrudes from an inner side face of the primary plate portion, the structural member extends in the lengthwise direction and is also curved.
• the primary plate portion and flange are both formed of metal plate material, the flange metallurgically welded to the primary plate portion.
• the primary plate portion has a height and length, the length larger than the height, the primary plate portion is curved in the lengthwise direction.
• First, second, third and fourth flanges circumscribe the primary plate portion, each flange has a first portion extending outwardly beyond an outer side face of the primary plate portion and a second portion extending inwardly beyond an inner side face of the primary plate portion.
• the flanges are welded to the primary plate portion, the first portion of each flange is substantially smaller than the second portion.
• the primary plate portion includes at least two holes extending from an inner side face to an outer side face of the primary plate portion, each of the holes including threads.
• a liner structure within a shaft or tunnel includes at least first and second liner plate members assembled together, the liner plate members formed of metal plate material having respective metal surfaces in contact with each other along a plate joint.
• a thermoplastic fusion seal arrangement is located along the plate joint.
• each metal surface includes a respective recess, the thermoplastic fusion seal arrangement formed by respective thermoplastic fusion elements within each recess, the thermoplastic fusion elements fused to each other.
• a coating seal material is located at an exterior surface of the assembled liner plate members.
• a grout material located within a spaced between the coating seal material and a wall of the shaft or tunnel.
• each liner plate member includes a structural member protruding from an inner side face of the liner plate member.
• An inner liner system is connected to the structural members of the liner plate members.
• a method of lining a mine shaft bore includes the steps of: providing a plurality of liner plate members, each liner plate member having a curved shape; assembling a first set of liner plate members into a first ring structure;
• the forming step involves energizing electrofusion chord members located on both the first ring structure and the second ring structure.
• the forming step includes applying a coating along an exterior surface of the joined first and second ring structures.
• a further step includes applying a grout material into a space between the exterior of the joined ring structures and the mine shaft bore.
• a liner plate structure for use in lining shafts and tunnels includes a primary plate portion having a length and height, the length greater than the height, the primary plate portion further including first, second, third and fourth side edges. First, second, third and fourth flanges respectively disposed at the first, second, third and fourth side edges, each flange having a plurality openings therein for facilitating connection to another liner plat structure.
• a structural member is connected to and protrudes from an inner side face of the primary plate portion, the structural member extending in the lengthwise direction and located in a central region along the height of the primary plate portion.
• the primary plate portion includes at least one hole extending from the inner side face to an outer side face of the primary plate portion, the hole including threads for receiving a threaded plug.
• each flange in the liner plate structure of one of the two immediately preceding aspects, includes a first flange portion overhanging the interior side face of the primary plate portion and a second flange portion overhanging and exterior side face of the primary plate portion, the overhang of the first flange portion larger than the overhang of the second flange portion.
• Fig .1 illustrated one embodiment of a liner plate structure
• Fig. 2A shows one embodiment of a cross section of the liner plate of Fig. 1 along line 2-2;
• FIG. 2B shows another embodiment of a cross-section of the liner plate of Fig. 1 along line 2-2;
• FIG. 3 shows a cross-section of the liner plate of Fig. 1 along line 3-3;
• Fig. 4 shows an enlarged partial view of the corner of the cross-section of
• Figs. 5A-5C show alternative fusion chord configurations in cross-section
• FIGs. 6A and 6B show partial cross-sections of one embodiment of fusion joints at adjacent liner plate flanges
• FIGs. 7A and 7B show partial cross-sections of another embodiment of fusion joints at adjacent liner plate flanges
• Figs. 8A and 8B show exemplary liner plate assembly configurations
• Fig. 9 show another embodiment of a liner plate structure including openings to facilitate assembly
• Fig. 10 shows a cross-section of the liner plate of Fig. 9 taken along line 10-
• Fig ⁇ . 1 1 shows another embodiment of a liner plate structure
• Fig 5. 12 shows another embodiment of a liner plate structure
• Fig 5. 13 shows an assembly of liner plates in a vertical mine shaft bore installation
• Fig 5. 14 shows another embodiment of a liner plate structure in partial section view
• Fig 5. 15 shows a side elevation view of the liner plate of Fig. 14;
• Fig 5. 16 shows the liner plate of Fig. 16 with anchor structure added
• Fig 5s 17A and 17B show assembled liner plate structures during
• Fig. 18 shows a partial cross-section of assembled liner plates according to
• Fig. 19 shows another embodiment of a liner plate structure in partial cross- section view
• Fig. 20 shows a side elevation view of the liner plate of Fig. 19;
• Fig. 21 shows multiple liner plates according to Fig. 19 with an interior liner assembly added
• Figs. 22-24 show a partial cross-section of a flange recess and electrofusion chord and extrusion assembly
• Fig. 25 shows a partial cross-section of a corner section of an extrusion
• Fig. 26 shows a schematic cross-section of an extrusion ring structure
• Fig. 27 shows a schematic layout of one arrangement of electrofusion chord
• Fig. 28 shows a schematic partial cross section of the electrofusion chord arrangement of Fig. 27;
• Fig. 29 shows another embodiment of a liner plate structure including a secondary sealing recess
• Fig. 30 shows a partial cross-section of the liner plate of Fig. 29.
• Fig. 31 shows a cross-section view of an arrangement of liner plates including an exterior polyurea coating.
• an exemplary liner plate 10 is shown and includes a primary plate portion 12 of arcuate (or other curvature) configuration with peripheral top, bottom, left and right side flanges 14, 16, 18 and 20 located at respective side edges of the plate portion.
• the plate and flanges are preferably formed primarily of a strong material such structural carbon steel or aluminum.
• To form the liner plate a generally flat piece of plate material may be curved into an arcuate shape and generally flat pieces of flange material may be formed or cut into corresponding arcuate shapes. It is recognized that corrugations could be incorporated into plate portion 12 for increased strength and/or inwardly facing vertical or lateral ribs could be formed in or applied to the plate portion 12 for increased strength.
• the top and bottom arcuate flange portions may then be welded to the arcuate plate portion. Left and right side flange portions may then be welded to plate ends as well. Any suitable metal welding technology may be used.
• Any suitable metal welding technology may be used.
• the flat plate could be cut to include the flange portion (e.g., by removing corner sections), the flange portions folded relative to the base plate portion, the structure formed into an arcuate shape and then the flange portions welded to each other at the corners.
• a stamping operation, forging operation or metal casting operation may be used to form the liner plate.
• a material other than steel or other alloy is used, such as concrete, in which case the liner plates may be formed by casting.
• the dimensions of the liner plate may vary depending upon the size of the mine shaft or tunnel into which the liner plates will be assembled, as well as other factors. However, it is contemplated that the thickness of the plate portion 12 may generally be in the range of about 1/4" to 1" or more (e.g., such as in the range of about 2" to 5"). In applications where the liner plate is installed to provide structural support for the shaft or tunnel wall, the plate thickness may be higher.
• the arcuate length or extent of a typical liner plate may be in the range of about 36" to 72" or more, such as up to about 216" and the arc encompassed by that length may typically be in the range of about 18 to 36 degrees or more (e.g., such as about 40 to 180 degrees).
• each liner plate may typically be in the range of about 24" to 36" or more (e.g., such as between about 42" to 96").
• the radial depth of the liner plates may be in the range of about 5" to 10" or more (e.g., such as in the range of about 10" to 18"). Variations on these dimensions are possible.
• the thickness of the flanges 14, 16, 18 and 20 will match that of the arcuate plate 12. In other embodiments the thickness of the flanges may be more or less than that of the arcuate plate.
• Fig. 2A shows a cross-section in which the outer surface of each of the arcuate plate 12 and top and bottom flange 14 and 16 has a polypropylene layer 22, 24 and 26 bonded thereto.
• Other suitable thermoplastics that can be thermally bonded could be used to form the layers, such as polyethylene.
• polypropylene layer it may be applied after the plate and flanges are formed and welded.
• embodiments in which the polypropylene layer is coated onto the plate and flanges prior to the components being welded together may be possible.
• FIG. 2B shows an embodiment in which only the top and bottom flanges 14 and 16 include a polypropylene layer.
• both the left and right flanges 18 and 20 would include corresponding polypropylene layers 28 and 30 as well, as shown in Fig. 3.
• the polypropylene layers may typically have a thickness in the range of about 1/8" to 1/2", but variations are possible.
• the primary purpose of the polypropylene layers is to provide a sealing function when liner plates are abutted against each other and assembled into a cylindrical liner for a mine shaft or tunnel.
• the flange portions of the liner plate may include one or more thermoplastic fusion elements (e.g., such as electro-fusion joining elements) extending therealong.
• the illustrated electro-fusion joining elements 32 include a generally planar resistive element 34 coated in polypropylene and the elements are applied directly to the outer surface of the polypropylene layer (e.g., per Fig. 5A).
• the shape of the elements 32 could vary, such as the oval or round-shaped elements shown in Figs. 5B and 5C.
• electrofusion chord as described in U.S. Patent No. 5,407,514 could be used. Energization of the resistive elements of the chord heats the thermoplastic and causes the fusion to take place.
• the electro-fusion elements are incorporated into the liner plates prior to installation of the liner plates in the field, but in field of application of the electro-fusion elements may be possible.
• the electro-fusion elements 32 are sandwiched between the polypropylene layers 24 and 26 of the two liner plates.
• the electro-fusion element may be formed of a lattice-type resistive element that extends along substantially the entire flange depth, to produce a relatively continuous bond and seal along the depth of adjoining flanges per Fig. 7B.
• Other variations are possible. Although not shown, similar electro- fusion bonds would be formed between abutting left and right side flanges of side-by-side liner plates.
• a plurality of like liner plates are assembled together to form, for example, a cylindrical mine shaft liner that is sealed against penetration by groundwater.
• Other mine shaft liner geometries are possible as well, such as oval, elliptical or rectangular of other polygonal shapes.
• the liner plates are assembled in aligned columns and rows per Fig. 8A, but a preferred assembly configuration offsets the liner plates from row to row as shown in Fig. 8B.
• a sealed cylindrical structure can be formed (i.e., sealed along its entire height for a full 360 degrees).
• openings 40 are provided in the flanges so that the openings of adjacent flanges align and nut and bolt assemblies can be used. At least one or more of the electro-fusion sealing elements, or portions thereof should, in such cases, extend along the external side of the opening (i.e., between the opening and the cylindrical outer surface of the arcuate plate 12).
• a typical liner plate may include electro-fusion elements along only two flanges (e.g., one of the top and bottom flanges and one of the left or right flanges).
• electro-fusion elements extend along the outer surfaces of polyethylene layers 28 and 26 of the left and bottom flanges, but not along the other surfaces of the polypropylene layers 24 and 30 of the top and right flanges.
• a left flange with element 32 When properly assembled, a left flange with element 32 will always abut a right flange without element 32 so that the adjacent polypropylene layers can be sealed by electro-fusion, and a bottom flange with element 32 will always abut a top flange without element 32 so that the adjacent polypropylene layers can be sealed by electro-fusion.
• such a forced assembly arrangement could be achieved by non-symmetrical placement of the openings 40 on, for example the left and right flanges 18 and 20.
• upper side flange openings 40a are spaced a distance dl from the top edge of the liner plate and lower side flange openings 40b are spaced a distance d2 from the bottom edge of the liner plate, where d2 is greater than dl .
• the side flange openings will be centered on each other to facilitate receiving the nut and bolt assemblies.
• FIG. 13 an exemplary installation of assembled liner plates 12 to form a cylindrically extending liner 50 of a vertical mine shaft 51 is shown.
• Grout e.g., cementious grout
• other filler material 54 may be delivered into the gap or spacing 52 between the external surface of the cylindrical liner and the inward facing surface or wall of the mine shaft bore 51 itself.
• the arcuate plate portions of the liner plates may be formed with grout openings for purpose of feeding grout into the space, in which case suitable plug structures could be provided for such openings.
• each electro-fusion chord should terminate so they are accessible from the inward facing side of the liner plate (e.g., radially inward of the arcuate plate), making them accessible from the inside of the assembled ring of liner plates when installed.
• the chord ends can protrude through the gap between mating plastic sheets or extended through openings or holes in the flange or flanges and terminate at the radially inner side of the flanges of the liner plate.
• the electro-fusion process is performed after full rings of liner plates have been assembled (e.g., each time one ring is assembled or each time a specified number of rings are assembled), but could alternatively be performed as individual liner plates are assembled into place.
• electro-fusion chords may be eliminated and adjacent flanges of the assembled/installed liner plates could be field welded in place using, for example, a down-hole field extrusion gun that applies a thermoplastic material.
• the a true metallic weld may be applied to adjacent flanges (e.g., at the radially inner edges of the abutting flanges).
• the electro-fusion chords may also be placed within a perimeter recess 80 formed in the flanges 14, 16, 18 and 20.
• a perimeter recess 80 formed in the flanges 14, 16, 18 and 20.
• the electro-fusion chord installed in the recess may protrude slightly outward of the flange surfaces so as to assure contact with the chord of an adjacent liner plate.
• the electro-fusion chord may include a compressible rubberized thermoplastic or rubber core and a thermoplastic exterior, making the chord more readily compressible when adjacent plates are bolted together.
• the liner plates may also include a structural member 82 on the primary plate portion 12.
• the structural member is a T-shaped member, with the base 84 of the T-shaped member welded to the inner face of the arcuate plate portion 12 and the cross or head 86 of the T disposed radially inward of the arcuate plate portion.
• the T-shaped structural member has a curved configuration that matches the curve of the liner plate as best seen in Figs. 17A and 17B.
• the configuration of the structural member could vary. By way of example, other possibilities include wide flange beams, tubes, channels, standing ribs, etc. Referring again to Fig.
• anchor loops 88 may be connected to the external face of the arcuate plate portions 12 (e.g., by welding) to provided an integrated connection with the grout or other filler material that is delivered into any gap or spacing between the external surface of the cylindrical liner and the inward facing surface of the mine shaft bore itself.
• the anchor loops may, by way of example be formed of curved rebar structure, such as #5 rebar.
• the primary plate portion 12 includes one or more holes 90 and 92 (Fig. 17A) for delivering the grout into the space at the external surface of the liner.
• the holes 90 and 92 may be threaded to enable easy installation of a threaded plug to assure sealing of the holes (gaskets or thread dope may be used in connection with the plugs).
• the main plate structure 12 may be connected (e.g., welded) to the main plate structure 12 so as to extend radially outward beyond the outer side face of the plate portion 12 slightly (e.g., 1/8 inch to 1 inch or more) as shown at locations 94, 96 and 98.
• These overhanging portions act to assist in anchoring the plates to the fill grout to provide an integrated connection with the grout or other filler material, in which case the anchor loops may be eliminated in certain implementations.
• the overhanging arrangement facilitates use of a filet weld to secure the flanges 14, 16, 18 and 20 to the main plate portion 12.
• an inner liner system 100 may be connected to the plate structures upon installation and after thermoplastic fusion weld sealing.
• the aforementioned T-shaped structural member may include a series of bolt openings 102 for connecting a smooth inner liner plate 104 formed of metal, plastic or other suitable material.
• Bolt and nut assemblies 105 secure the liner to the structural member.
• the inner liner members may also have an inward and downward facing hook structure 106 that overlaps and rests atop the upper edge of the T portion 86 of the structural member 82.
• each inner liner structure may be formed with an inwardly (Fig. 18) or outwardly (Fig. 21) offset lower edge or flange 108 that receives the upper edge of an immediately adjacent lower liner structure.
• the upper edge could include the inwardly or outwardly offset flange to receive the lower edge of an immediately adjacent upper liner structure.
• the thickness of the steel plate making up the arcuate plate and flanges may, for example, be on the order of two to four inches, but other variations are possible. In one embodiment the thickness of the arcuate plate portion is between 25% and 75% thicker than the thickness of the flanges (e.g., 50% thicker).
• the arcuate length or extent of a typical structural liner plate may be in the range of about 72" to 190", such as about 1 10" to 150", such as about 125" to 135", but variations in the range of 36" to 216" are envisioned as well.
• the arc encompassed by each plate may be in the range of about 40 to 80 degrees, such as about 50 to 70 degrees, such as about 60 degrees, but variations are possible, including in the range of about 40 to 180 degrees.
• the radial depth of the flanges may be on the order of about 5" to 15" depending on the application, such as about 8" to 12" (e.g. about 10"), but variations in the range of 5" to 18" are envisioned as well.
• the width or radial depth of the recess to receive the electro fusion chord will typically vary according to the radial depth of the flanges.
• the width or radial depth of the recess may be on the order of about 10% to 30% of the radial depth of the liner plate flanges.
• the electro fusion chord 120 may be incorporated into an extrusion that is placed in the recess 80.
• a multi-layer gasket extrusion 122 of polypropylene top layer 124 (it is recognized that other materials may be used, particularly thermoplastic materials that are capable of heat fusion), an elastic polymer intermediate layer 126 (e.g., EPDM (ethylene propylene diene Monomer (M-class) material)) and a bottom layer of material 128 (e.g., such as sanoprene) that will bond to metal at the bottom of the recess in the presence of heat is created (e.g., via a co-extrusion process or via multiple layered extrusions).
• EPDM ethylene propylene diene Monomer
• the polyproylene layer 124 may be formed with spaced apart recesses 130 (e.g., generally semicircular in form) that will receive the electrofusion chord 120 (e.g., chord that is circular in cross-section).
• the extrusion 122 is then cut to lengths to facilitate formation of a rectangular ring structure that can circumscribe the continuous, circumscribing recess 80 formed by aligned recesses of all flanges on a liner plate.
• end portions of extrusion strips 122 may be cut with a fourty-five degree taper and then bonded together (e.g., via heating) to form the right angle turns needed to transition from one flange to the next.
• a rectangular ring structure 134 with three fused corners 136 and one unfused corner 138 is formed (e.g., per the schematic cross-section of Fig. 26), enabling the ring structure to be applied into the recess 80 of a liner plate. Once applied, the corner 138 can be fused to hold the ring structure in place. Heat may then be applied at the inner surfaces of the flanges in the vicinity of the recesses to cause layer 128 to bond to the metal. In an alternative embodiment an adhesive (e.g., one that does not require heat) could be used to bond the ring structure in the recess 80.
• an adhesive e.g., one that does not require heat
• all extrusions 122 making up the ring structure are straight and the upper and lower extrusions are flexible enough to take the shape of the curved recess portions of the top and bottom flanges 14 and 16 of the liner plate.
• the top and bottom extrusions may be cold rolled into the desired curvature prior to forming the ring structure 134.
• other techniques for placing the extrusion in the liner plate recess may be used, such as extrusion directly into the recess.
• the fusion chord 120 is then applied into extrusion recesses 130.
• numerous configurations for the placement pattern of the chord are possible.
• the recess 80 of each flange is fitted with two distinct fusion chord loops as outer and inner loops 140 and 142.
• Transverse recesses are cut into the extrusion ends to receive the lateral portions 144 and 148 of the chords. These lateral portions 144 and 148 may be curved portions rather than straight portions.
• Each fusion chord loop 140, 142 is terminated with loop ends 150 in proximity to each other and loop ends 152 in proximity to each other.
• the loop ends 150 are displaced relative to loop ends 152 by some distance. As best seen in the schematic view of Fig. 28, at the location of the loop ends 150 and 152 holes 160 and 162 are drilled through the flange and the fusion chord fed through the holes so that each fusion chord loop has end portions 164, 166 that are accessible at the internal side of the liner plate to facilitate connection of the power supply for the fusing operation.
• an overlay er 170 of polypropylene is applied (e.g., via extrusion) over the top to hold the chord in place.
• the end result is a thermoplastic fusion element in the form of a multi-layer fusion assembly 180 applied in the recess 180 with upper layer 170 extending slightly above the exterior surface or side face of the flange 182, and with one or both of the side edges of the assembly spaced from the side edges of the recess.
• the raised nature of layer 170 assures good contact with a similar raised layer of an adjacent liner plate flange when two plates are secured together with flanges surfaces 182 contacting each other.
• the side to side spacing provides sufficient room for the assembly 180 when it is compressed (e.g., downward compression of the multi-layer assembly results in some outward bowing of the sides of the assembly 180).
• the height HA of the assembly 180 before compression is between about 10% and 20% greater than the overall recess height HR (e.g., for a recess having a depth of about 1/4" to 3/4" the assembly may protrude by about 0.025" to 0. 15"), but variations are possible.
• the width (or radial depth) WA of the assembly 180 before compression may be between about 2% and 8% less than the width (or radial depth) WR of the recess (e.g., for a recess having a width or radial depth of about 1.75" to 2.25" the width or radial depth of the assembly may be between about 1.60" and 2.20"), but variations are possible.
• the height of the fusion assembly 180 above the surface 182 of the flange may be defined by implementing a post installation trimming operation. That is, the assembly 180 may be fully formed in the recess 80 such that layer 170 extends higher than desired. A planing type device may then be run along the surface 182 to trim the layer down to the desired height.
• a planing type device may then be run along the surface 182 to trim the layer down to the desired height.
• other techniques could also be used.
• the resistive elements in the fusion chords 120 of adjacent fusion assemblies 180 are energized and heating takes place, the polyproylene layers 170 and 174 are heated and fusion of abutting layers 170 takes place.
• the heating may also cause the exterior sides of the layers 170 and 174 to bond to the side walls of the recess 80.
• a secondary or back-up sealing system may also be enabled by providing a small recess or sub-recess 200 in the flanges at the radially internal side of the recess 80 and extrusion assembly 180 (e.g., in the illustrated embodiment immediately adjacent to the recess with one side of the sub-recess in communication with the recess 80).
• This sub-recess 200 (e.g., about 1/16 to 3/16 inch depth and 1/8" to 1/2" wide (or radial depth), such as, about 1/8" deep and 1/4" wide) on the flanges would align with a similar recess on adjacent flanges of adjacent liner plates to create a continuous recess (e.g., 1/4" by 1/4" in total) that could be filled with grout or other sealant (e.g., via a radially inward extending portion 202 or portions of the sub-recess that extend to the inward facing side edges of the flange).
• grout or other sealant e.g., via a radially inward extending portion 202 or portions of the sub-recess that extend to the inward facing side edges of the flange.
• the method of testing for a leak may involve plugging two spaced apart sub-recess extensions 202 (e.g., inserting a temporary plug the sealingly abuts against the thermoplastic fusion element) and then applying pressurized air to a sub-recess extension located between the two plugged extensions. If the sub-recess holds the pressure, then the thermoplastic fusion seal is deemed sound in the region between the two plugged sub-recess extensions. If the sub- recess does not hold the pressure, then the thermoplastic fusion seal is deemed imperfect or leaking in the region.
• the secondary recess 200 may be filled with grout only in situations where a leak is identified. Alternatively, the secondary recess 200 may always be filled with grout to provide the secondary or back-up seal for the installation.
• Fig. 31 an embodiment including a two or three stage sealing system is shown. Specifically, the electrofusion chord assembly seal 210 is provided between adjacent flanges of the liner plates. At the external surface of the assembled liner plate structure a polyurea coating 212 is also applied for sealing purposes.
• the polyurea coating may be applied by suitable spray process and may, by way of example, have a thickness of between about 1/10" and 1/2", but variations are possible.
• the third stage sealing could be by way of the grout seal mentioned above.
• the liner is assembled in a top down manner in the case of a vertical mine shaft installation.
• a series of liner plates are assembled together with nut and bolt assemblies within the shaft to form a ring. That ring is then raised upward and connected via nut an bolt assemblies to the lower side of a previously installed ring.
• the exterior of the joined rings is then sprayed with polyurea to provide the first sealant barrier. Suitable equipment capable of reaching the exterior side of the assembled liner plate rings may be used for this purpose. Additional ring layers may be added in a similar fashion (by repeating the foregoing steps) to achieve the desired depth of the liner plate structure.
• grout may be applied to the exterior of the polyurea layer in the space 52 between the bore or shaft 51 and the liner assembly by providing a temporary form structure at the bottom of the lowest ring layer and pumping grout 220 upward into the space 52 between the liner plate assemblies and the mine shaft bore wall 50.
• the electrofusion sealing may also be performed periodically by delivering power to the leads of the electrofusion chords.
• Figs. 17A and 17B where Fig. 17A contemplates energization of the chords on the vertical plate flanges and Fig. 17B contemplates energization of the chord on the horizontal plate flanges. The exact number of chords energized at any one time and the overall sequence of energization could vary.
• a mine or tunnel shaft liner system could be made up of a combination of liner plate structures with thermoplastic fusion seals and liner plate structures without thermoplastic fusion seals.
• certain sections of the liner system could utilize the thermoplastic fusion seals in those regions where groundwater is an issue and other sections could be installed without the thermoplastic fusion seals in regions where groundwater is not an issue.

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• Engineering & Computer Science (AREA)
• Mining & Mineral Resources (AREA)
• Structural Engineering (AREA)
• Life Sciences & Earth Sciences (AREA)
• General Life Sciences & Earth Sciences (AREA)
• Geochemistry & Mineralogy (AREA)
• Geology (AREA)
• Architecture (AREA)
• Civil Engineering (AREA)
• Mechanical Engineering (AREA)
• Lining And Supports For Tunnels (AREA)
• Bulkheads Adapted To Foundation Construction (AREA)
• Lining Or Joining Of Plastics Or The Like (AREA)
• Excavating Of Shafts Or Tunnels (AREA)

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• 2011
  • 2011-02-01 WO PCT/US2011/023290 patent/WO2011097201A2/en active Application Filing
  • 2011-02-01 EP EP11707944A patent/EP2531697A2/de not_active Withdrawn
  • 2011-02-01 AU AU2011213137A patent/AU2011213137A1/en not_active Abandoned
  • 2011-02-01 CA CA2788349A patent/CA2788349A1/en not_active Abandoned
  • 2011-02-02 US US13/019,372 patent/US20110188939A1/en not_active Abandoned
• 2012
  • 2012-07-30 ZA ZA2012/05738A patent/ZA201205738B/en unknown
  • 2012-08-03 CL CL2012002174A patent/CL2012002174A1/es unknown

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