GB2109303A - Rubber element - Google Patents

Rubber element Download PDF

Info

Publication number
GB2109303A
GB2109303A GB08229784A GB8229784A GB2109303A GB 2109303 A GB2109303 A GB 2109303A GB 08229784 A GB08229784 A GB 08229784A GB 8229784 A GB8229784 A GB 8229784A GB 2109303 A GB2109303 A GB 2109303A
Authority
GB
United Kingdom
Prior art keywords
rubber
composite
resistant member
perforations
wear
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB08229784A
Other versions
GB2109303B (en
Inventor
Sven-Erik Dyrup
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Trelleborg Ltd
Trelleborg Ltd
Original Assignee
Trelleborg Ltd
Trelleborg Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Trelleborg Ltd, Trelleborg Ltd filed Critical Trelleborg Ltd
Priority to GB08229784A priority Critical patent/GB2109303B/en
Publication of GB2109303A publication Critical patent/GB2109303A/en
Application granted granted Critical
Publication of GB2109303B publication Critical patent/GB2109303B/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/06Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of natural rubber or synthetic rubber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B02CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
    • B02CCRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
    • B02C17/00Disintegrating by tumbling mills, i.e. mills having a container charged with the material to be disintegrated with or without special disintegrating members such as pebbles or balls
    • B02C17/18Details
    • B02C17/22Lining for containers
    • B02C17/225Lining for containers using rubber or elastomeric material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/70Completely encapsulating inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/18Layered products comprising a layer of metal comprising iron or steel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/20Layered products comprising a layer of metal comprising aluminium or copper
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/26Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/685Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates
    • B29C70/687Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates the inserts being oriented, e.g. nets or meshes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2021/00Use of unspecified rubbers as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/02Aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/08Transition metals
    • B29K2705/12Iron
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/554Wear resistance

Abstract

Wear-resistant rubber 1 has a perforate metal sheet 3 embedded therein (typically with an aperture ratio of 15-75% and circular perforations arranged in a hexagonal pattern) parallel to and adjacent one face 2 thereof so that rubber intercommunicates at perforations 4 with the thicker and thinner layers to either side. <IMAGE>

Description

SPECIFICATION Rubber element This invention relates to reinforced rubber cladding or structural elements.
It has been known for many years that there are advantages in constructing or lining materialshandling equipment with abrasion-resistant rubber.
Because the rubber, in addition to being wearresistant, resiliently resists sliding or crushing impact, it lasts longer than unprotected steel plates. It is also less noisy in use, lighter, and easy to fabricate.
Heavy-duty abrasion-resistant rubber layers have accordingly been proposed for a wide range of such equipment and used to line truck container bodies, mine car floors barges, hoppers for concrete or mineral working in mines and quarries, chutes, whether direct or cascade, excavator and bulldozer buckets, vibratory feeders, flotation launders, and other types of wet-or dry-handling equipment for granular, lump, boulder or mixed abrasive material.
Rubber materials used alone, even of heavy grade, i.e. of considerable thickness and high Shore hardness, are not always mechanically strong enough to be structural members per Se. Thus, they must usually be fixed to a steel frame.
One way of fixing such rubber layers is by securing them mechanically at a number of fixing points, e.g. holes extending partway or completely through the rubber to contain the heads of fixing bolts. If there are too any of such fixing points they weaken the layer. If there are too few, the layer takes up all the stresses at these relatively few points, and can start to tear. In practice, such fixing of unsupported rubber layers is not always successful.
Another way of fixing such layers is by adhesion, but this cannot be done in all constructions and typically needs an existing body panel or like extended area for attachment. Also, specialised operatives are necessary for such adhesion techniques.
It has become usual, therefore, to provide each rubber layer, prior to use, with its own steel backing sheet, typically of say 5 mm in thickness. This is glued to the rubber layer of e.g. 20.50 or 100 mm in thickness after careful cleaning and preparation of the contacting surfaces. This adhesion is carried out by the manufacturer as an additional manufacturing step. Typically the manufacturer then sells standard size composite steel/rubber sheets. These fequently need to be cut and bent to shape on site, in neither case behaving as conveniently as an unbacked rubber sheet. They are also heavier, and nosier in use. Moreover, although the adhesion layer itself is not often a source of problem ,the steel backing layer can corrode over long-term use, which is especially troublesome if it is in an inaccessible position.Therefore, although these steel/rubber composite layers present the great advantages of dimensional stability and secure fixing, they are not always suitable for every application.
The present invention sets out to provide a different form of composite metal/rubber having improved characteristics over these prior art layers.
In one aspect the invention provides a composite wear-resistant member comprising a layer of wearresistant rubber with a perforate metal sheet embedded therein parallel to and adjacent one face thereof with rubber on either face of the metal sheet and intercommunicating through the perforations.
Preferably, the perforate metal sheet is a steel or aluminium sheet having formed therein a multiplicity of regularly spaced perforations to a total aperture ratio of 15 to 75%. The perforations are each preferably circular and preferably arranged so that each circle is surrounded by six like circles equispaced at the vertices of a regular hexagon.
Other preferred features of the structure are described in more detail below.
In another aspect the invention provides a method of manufacturing a composite wear-resistant member as described above in which the perforate metal sheet is sandwiched between a thicker and thinner layer of unvulcanized rubber and subjected to vulcanization under temperature and pressure conditions such that the rubber layers flow into and join within the perforations.
In yet another aspect the invention provides self-sufforting materials-handling equipment having walls formed of wear-resistant composite members as described above with the perforate metal sheets nearer the outer surfaces.
While the invention extends generally to those various types of equipment listed above, particularly valuable examples of this type of equipment are constituted by lined hoppers and chutes for use in mines, or by rotary drum materials handling and treatment machinery. This latter category includes various types of milling equipment, and especially includes washer drums for the sand and gravel industry.
A particular advantage we have found in such equipment is that the rubber can abrade down to the perforate plate itself without becoming detached from the wall of the drum. Hitherto, especially with concave surfaces under abrasive impact, there has been a tendency for the layer to become detached well before total abrasion, with consequent inefficiency of utilisation.
The invention will be further described with reference to the accompanying drawings, in which: Figure 1 is a cross-section through a composite rubber-metal sheet according to one form of the invention, Figure 2 is a perspective view of one corner of the metal element of the composite sheet of Figure 1, Figure 3 shows how the sheet of Figure 1 can be secured to a support member, and Figure 4 shows a detail of fixing of the sheet inside a washer drum used in the sand and gravel industry.
In Figure 1 a rubber layer 1 has embedded therein, towards a back surface 2, a perforated steel sheet 3.
The rubber extends integrally to either side of the steel sheet and inter-communicates through the perforations 4. The surface 5 is operative wearresistant face of the rubber layer 1.
The distance between the steel sheet 3 and surface 2 is relatively small, being typically only sufficient to give a good grip on the steel sheet (by extending through its perforations) and to provide a smooth protective backing surface. The distance between the steel sheet 3 and the front surface 5 can be whatever is desired for the expected lifetime and environment in a given end use, as discussed below.
The thickness of the metallic sheet 3 is relatively low compared to that of the external unperforated sheet in the prior art, since its protected position guards against corrosion and consequent loss of material.
Figure 2 shows typical perforations in the sheet.
While these can adopt any individual shape or packing commensurate with the desired strength and flexibility of the layer they are circular in the embodiment shown and arranged so that their centres lie on the vertices of a multiplicity of equilateral triangles. Alternatively stated, each circular perforation is at the centre of a regularly hexagonal arrangnement of six identical circular perforations.
Specific dimensions in the example shown, and preferred ranges of dimension and relative proportion are as follows: (i) Length and width of composite layer This can be sheet-like e.g. of modular or standard widths from 400 to 2000 mm, and of standard lengths e.g. 2, 3, 5, 10 metres. It can also be presented as smaller bar-like elements or blocks provided these have a cross-section of the type shown above.
(ii) Thickness ofabrasion-resistantlayer This is for example the distance from metal sheet 3 to surface Sin Figure 1. It can vary widely, but is usually from 5 to 150 mm; more usually from 20 to 50 mm; and by way of specific example 25 mm.
(iii) Thickness of metal sheet This sheet which can be for example of steel or aluminium has a thickness suitable for the structural strength and flexibility desired. Usually this is between 0.5 to 3 mm and more usually from 0.5 to 1.5 mm, whereby it is appreciably easier to cut than the prior art (unperforated) steel backing sheets. By way of specific example it can be of 1 mm thickness.
(iv) Size ofperforations The size of perforations should be adequate to give good interconnection between the rubber on either side. A maximum dimension is usually about 10 mm, but more usually from 1.5 minimum to 6 mm maximum is used, e.g. as 1.5 to 6 mm diameter circular perforations. Specifically, 2 mm diameter circular perforations have been used.
(v) Spacing ofperforations The spacing of the perforations, in relation to their size, again affects strength and flexibility. Typically, it is such that the total aperture is from 15% to 75% of sheet area e.g. 25%. If "hexagonally-arranged" circles are used the spacing of centres can be from 1.2 to 2 times circle diameter; a specific example is circles of 2 mm diameter 3.6 mm apart for the 1 mm sheet described above, and used with the 25 mm backing layer.
(vi) Depth ofembedment This is the distance from the metal sheet 3 to surface 2 and is typically from 1 to 10 mm, more usually 1 to 3 mm e.g. 2 mm for the specific embodiment discussed above.
The rubber material is of a type known perse, being a vulcanized rubber product of hardness chosen for its particular environment (i.e. sliding, impacting or gouging particles or lumps) but typically 40, 50 or 60 Shore hardness.
Although the surface 5 is shown as a flat surface it is within the ambit of the invention to provide ribbed, grooves or otherwide configured surfaces, e.g. of a type to resist low-angle impact of material.
The composite sheet shown is manufactured without additional adhesive steps. A sheet of uncured rubber, corresponding to the eventual abrasion-resistant layer is covered with the perforated metal sheet and this is covered with a thin unvulcanized layer of the same rubber formulation. These three layers are pressed together and vulcanized so that the rubber intercommunicates through the perforations.
Figure 3 wherein like reference numerals are used as in Figures 1 and 2 shows how such a composite sheet can be secured to a frame member 6 by bolts 7 and washers 8. The head of the bolt lies within recess 9 in the layer 1. The floor 10 of this recess is spaced from the perforated steel sheet 3, although the extent or existence of this spacing is optional. It will be apparent that the essential dimensional stability and resistance to tearing imparted by the perforated steel sheet is still retained.
As shown, recess 9 is wide enough to receive a tightening or holding tool, but if desired the walls of this recess should contact the bolt head and thus prevent turning. Since the rubber is flexible, even an undersized recess, minimising the interruption in the abrasion-resistant surface 5, could be used. By constructional techniques of these types a dimensionally stable self-supporting structure e.g. a chute or hopper can be made, having not only the abrasion resistant interior but the low-noise corrosionresistant exterior of surface 2, as distinct from the metal backing, or existing constructional surfaces, normally encountered.
There are of course other ways in which the composite material can be fixed. Indeed, we have found that for some constructions, simple selftapping screws extending through the perforate plate and a support plate in either direction, can be used. Also, nails fixed from a nail gun are possible fixing means.
Cutting of the composite material is of course considerably easier than cutting of the rubberlsteel laminate of the prior art since the included sheet is both thinner and perforated. In case of cutting it resembles unreinforced sheet, and readily available hand or electric saws will suffice.
Thus, the novel composite as described in relation to Figure 1 is easier to manufacture, easier to cut and bend to shape, and lighter to assemble than the conventional steel-backed rubber material. It is also less prone to corrosion, and quieter in use, while preserving the strength and shape-retaining advantages of steel-clad rubber as compared to unclad rubber.
In Figure 4 there is shown the key constructional features of a horizontally mounted washing drum for sand and gravel. This is essentially composed of a concave steel shell 11 to which are fastened by normal screw fastenings 12 layers of the composite sheet material 13, 14. Each such layer is recessed at 15. Two such opposed recesses jointly accommodate a spacer or lifter bar 16, also made of wearresistant rubber and which may or may not possess internal reinforcement according to the invention.
The spacer bar 16 is bolted to the shell 11 at 17, thus further assisting in retention of the sheets 13, 14 especially at their longitudinal recessed edges.
In the construction shown, the lifter bar becomes worn by the abrasive material being washed. Wear arises disproportionately on the "upstream" corner 18 (with rotation as shown by arrow A) but the construction illustrated readily permits the bar to be removed and reversed for a further period of wear.
We have found that the sheets 13 and 14 in such a construction can in patches wear right down to their reinforcement 19 without becoming detached from the drum. Thus, a surprising improvement in operating life, over that of unreinforced rubber cladding, is achieved.

Claims (14)

1. A composite wear-resistant member comprising a layer of wear-resistant rubber which possesses a perforate metal sheet embedded therein parallel to and adjacent one face thereof with rubber on either face of the metal sheet and inter-communicating through the perforations.
2. A composite wear-resistant member as claimed in claim 1 in which the metal sheet is composed of steel or aluminium.
3. A composite wear-resistant member as claimed in claim 1 or 2 in which the aperture ratio, of total area of perforations to total metal sheet area, is from 15 to 75%.
4. A composite wear-resistant member as claimed in any one of the preceding claims in which the perforations are circular.
5. A composite wear-resistant member as claimed in claim 4 in which the circular perforations are arranged so that each circle is surrounded by six like circles equispaced at the vertices of a regular hexagon.
6. A composite wear-resistant member as claimed in any one of claims 1 to 5 in which the maximum dimension of the perforations is 10 mm.
7. A composite wear-resistant member as claimed in any one of claims 1 to 6 in which the thicker, abrasion resistant, layer of rubber is from 5 to 150 mm thick.
8. A composite wear-resistant member as claimed in any one of claims 1 to 7 in which the metal sheet is from 0.5 to 3 mm thick.
9. A composite wear-resistant member as claimed in any one of claims 1 to 8 which the thinner layer of rubber, embedding the metal sheet, is from 1 to 10 mm in thickness.
10. A method of manufacturing a composite wear-resistant member as claimed in any one preceding claim in which the perforate metal sheet is sandwiched between a thicker and a thinner layer of unvulcanized rubber and subjected to vulcanization under temperature and pressure conditions such that the rubber layers flow into and join within the perforations.
11. Materials-handling equipment having walls which comprise wear-resistant composite members as claimed in any of claims 1 to 8 with the perforate metal sheets nearerthe outer surfaces thereof.
12. Materials-handling equipment as claimed in claim 11 in which a self-supporting hopper or chute for abrasive materials is formed in the composite material.
13. Materials-handling equipment as claimed in claim 11 in which sheets of composite material are secured inside a rotary drum in a concave shape.
14. Materials-handling equipment as claimed in claim 13 formed as a washer for the sand and gravel industry, in which concave sheets of the composite material are secured inside the rotary drum with adjacent longitudinal edges each having a longitudinal recess therein over its whole length, each pair of recesses jointly accommodating a spacing bar extending above the sheet thickness along the drum.
GB08229784A 1981-10-20 1982-10-19 Rubber element Expired GB2109303B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08229784A GB2109303B (en) 1981-10-20 1982-10-19 Rubber element

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8131655 1981-10-20
GB08229784A GB2109303B (en) 1981-10-20 1982-10-19 Rubber element

Publications (2)

Publication Number Publication Date
GB2109303A true GB2109303A (en) 1983-06-02
GB2109303B GB2109303B (en) 1985-06-19

Family

ID=26281022

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08229784A Expired GB2109303B (en) 1981-10-20 1982-10-19 Rubber element

Country Status (1)

Country Link
GB (1) GB2109303B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4954387A (en) * 1987-06-04 1990-09-04 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Composite material of metal and plastic
DE3921302A1 (en) * 1989-06-29 1991-01-10 Manfred Straub Composite panel with heat insulating core and reinforced outer layers - has improved fatigue resistance and tensile strength by bonding perforated metal plate between at least one outer layer and core
EP3418114A1 (en) * 2017-06-22 2018-12-26 Metso Sweden Ab A lining element for a wear-resistant haul truck body lining, and a method for manufacturing a lining element
SE1751484A1 (en) * 2017-12-01 2019-06-02 Metso Sweden Ab Truck box
EP4260941A1 (en) * 2022-04-13 2023-10-18 Metso Outotec Finland Oy Wear protection component with local stress relief areas

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4954387A (en) * 1987-06-04 1990-09-04 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Composite material of metal and plastic
DE3921302A1 (en) * 1989-06-29 1991-01-10 Manfred Straub Composite panel with heat insulating core and reinforced outer layers - has improved fatigue resistance and tensile strength by bonding perforated metal plate between at least one outer layer and core
EP3418114A1 (en) * 2017-06-22 2018-12-26 Metso Sweden Ab A lining element for a wear-resistant haul truck body lining, and a method for manufacturing a lining element
WO2018234513A1 (en) * 2017-06-22 2018-12-27 Metso Sweden Ab Weight optimization
CN110770078A (en) * 2017-06-22 2020-02-07 美卓(瑞典)公司 Weight optimization
AU2018287166B2 (en) * 2017-06-22 2021-05-27 Metso Outotec Finland Oy Weight optimization
US11724654B2 (en) 2017-06-22 2023-08-15 Metso Sweden Ab Weight optimization
SE1751484A1 (en) * 2017-12-01 2019-06-02 Metso Sweden Ab Truck box
US11833980B2 (en) 2017-12-01 2023-12-05 Metso Outotec Finland Oy Truck box
EP4260941A1 (en) * 2022-04-13 2023-10-18 Metso Outotec Finland Oy Wear protection component with local stress relief areas
WO2023198740A1 (en) * 2022-04-13 2023-10-19 Metso Outotec Finland Oy Wear protection component with local stress relief areas

Also Published As

Publication number Publication date
GB2109303B (en) 1985-06-19

Similar Documents

Publication Publication Date Title
US5735377A (en) Modular impact or wear pads
US5842747A (en) Apparatus for roadway surface reclaiming drum
US3804346A (en) Liner for grinding mills
US5056924A (en) System for mixing and dispensing concrete
US20040026959A1 (en) Materials transport container
EP1909961B1 (en) Fastening spider and method of fastening
US4367255A (en) Lining sheet
US20050126056A1 (en) Bulk materials transport containers
US1921672A (en) Ball mill lining
KR20200056464A (en) Excavator bucket and manufacturing method
WO2016116837A1 (en) Interlocking wear-resistant panel system
GB2109303A (en) Rubber element
US5329864A (en) Door or wall reinforcing filler assembly
CN102548670B (en) Imrpoved screen panel
US4141511A (en) Mill lining elements
CA2216373C (en) Reversible scraper blade for cleaning conveyor belt
US4172560A (en) Replaceable liner for the discharge assembly of a rotary grinding mill or the like
US5378061A (en) Concrete mixing drum fin structure
CA2466209A1 (en) Squeegee blade
KR100931470B1 (en) Aggregate Shred Hammer Crusher
CA2428842A1 (en) A materials transport container
AU2008201356B2 (en) Rock box liners
JPH0996396A (en) Worn part repairing method of air transport pipe line of solid matter and complex for repairing
JP2007197049A (en) Rubber-coat material
AU652484B2 (en) Abrasion resistant means

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19991019