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GB2535601A - Method of manufacturing structual member - Google Patents

Method of manufacturing structual member Download PDF

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Publication number
GB2535601A
GB2535601A GB1522078.3A GB201522078A GB2535601A GB 2535601 A GB2535601 A GB 2535601A GB 201522078 A GB201522078 A GB 201522078A GB 2535601 A GB2535601 A GB 2535601A
Authority
GB
United Kingdom
Prior art keywords
load
bearing element
insulating core
lintel
bearing
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
GB1522078.3A
Other versions
GB201522078D0 (en
GB2535601B (en
Inventor
Price Richard
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.)
Tata Steel UK Ltd
Original Assignee
Tata Steel UK 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 Tata Steel UK Ltd filed Critical Tata Steel UK Ltd
Priority to IE20160009A priority Critical patent/IE87277B1/en
Publication of GB201522078D0 publication Critical patent/GB201522078D0/en
Publication of GB2535601A publication Critical patent/GB2535601A/en
Application granted granted Critical
Publication of GB2535601B publication Critical patent/GB2535601B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/29Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • C09J5/06Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers involving heating of the applied adhesive
    • 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
    • B32B2419/00Buildings or parts thereof
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C2003/023Lintels

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Rolls And Other Rotary Bodies (AREA)

Abstract

The method comprises providing a first load-bearing element 30 in a first orientation, providing an insulating core 40, applying an adhesive to the first load-bearing element or insulating core and bringing them into contact, providing a second load-bearing element 44, applying an adhesive to the second load-bearing element or insulating core and bringing them into contact, changing the orientation of the lintel, and applying heat and pressure to at least one of the load-bearing elements to cure the adhesive. The load-bearing elements may be metal, and there may be no direct contact between them. The load-bearing elements and insulating core may be moved into contact vertically downwards. The insulating core and second load-bearing element may have corresponding angled surfaces, and a heat press applied to the angled surface of the second load-bearing element to apply the heat and pressure. The heat press may comprise rollers. Also claimed is a thermally broken lintel manufactured according to the method.

Description

Method of manufacturing structural member
Field of the Invention
The present invention concerns a method of manufacturing a structural member. More particularly, but not exclusively, this invention concerns a method of manufacturing a lintel. The invention also concerns a method of manufacturing a thermally broken lintel.
Background of the Invention
Lintels are load bearing components used in the construction industry. They are often made of a metal "box" structure 10 and an insulating core material 12 located within the box, as shown in figure 1. As modern buildings are required to become ever more thermally efficient, it has been recognised that the metal box structure of a traditional lintel may reduce thermal efficiency by providing a thermally conductive path from inside a building to outside a building. In order to avoid this problem, "thermally broken" lintels may be provided, where instead of a continuous box structure 10, a first metal load bearing element 18 and a second metal load bearing element 16 are joined to an insulating core material 12, but not directly connected to each other, as shown in figure 2. Therefore, the thermal path from one side of the lintel to the other side of the lintel is removed. However, existing designs for thermally broken lintels are difficult to manufacture, leading to poor quality control and/or increased expense.
The present invention seeks to mitigate the above-mentioned problems. Alternatively or additionally, the -2 -present invention seeks to provide an improved method of manufacture.
Summary of the Invention
The present invention provides, according to a first aspect, a method of manufacturing a structural member, the method comprising the steps of: providing a first load-bearing element in a first orientation, providing an insulating core, applying an adhesive to the first load-bearing element or insulating core, bringing the first load-bearing element and insulating core into contact, providing a second load-bearing element, applying an adhesive to the second load-bearing element or insulating core, bringing the second load-bearing element and insulating core into contact, changing the orientation of the structural member, and applying heat and pressure to at least one of the first load-bearing element and second load-bearing element to cure the adhesive.
The step of applying heat and pressure to at least one of the first load-bearing element and second load-bearing element may comprise passing the structural member through a heat press, and applying pressure and heat to at least one of the first load-bearing element and second load-bearing element to cure the adhesive.
The step of applying heat and pressure to at least one of the first load-bearing element and second load-bearing element may comprise applying a clamp to one or -3 -both of the first load-bearing element and second load-bearing element. The heat may then be applied by heating the clamp or heating the area around the clamp.
The structural member may be a lintel. The structural member may be a thermally-broken lintel. The first load-bearing element and/or second load-bearing element may be metal. The metal may be steel, stainless steel, or aluminium. The first load-bearing element and second load-bearing element may be joined to the insulating core such that there is no direct contact between the first load-bearing element and second load-bearing element.
The step of applying adhesive to the first load-bearing element or insulating core may comprise applying adhesive to the first load-bearing element. The adhesive may be applied via an adhesive spray or a bead applicator. Applying the adhesive via an adhesive spray or bead applicator may ensure an even coverage of adhesive. The insulating core may then be placed in contact with the adhesive. The first load-bearing element may be oriented such that the insulating core is moved into contact with the first load-bearing element in an approximately downwards, for example approximately vertically downwards, direction.
The step of applying adhesive to the second load-bearing element or insulating core may comprise applying adhesive to the insulating core. The adhesive may be applied via an adhesive spray or bead applicator. The insulating core may be oriented such that the second load-bearing element is moved into contact with the insulating core in an approximately vertical downwards direction.
Constructing the structural member in this way may ensure the accuracy of the placement of the first load- -4 -bearing element, second load-bearing element, and insulating core. Preferably, the application of adhesive is to an approximately horizontal surface, which reduces or prevents adhesive run off. This may reduce the amount of wasted adhesive and/or keep the production line cleaner and reduce maintenance required. Applying adhesive to a horizontal surface may also ensure an even coverage of adhesive, resulting in a secure bonding of the load-bearing elements and the insulating core.
The structural member may comprise a longitudinal axis. The change of orientation of the structural member may comprise rotating the structural member approximately 90 degrees about the longitudinal axis.
The heat press or clamp may apply pressure to the first load-bearing element or second load-bearing element by applying pressure in an approximately horizontal direction. Due to the rotation of the structural member, the heat press or clamp may apply pressure to a side of the structural member which was previously the top or bottom of the structural member before the change of orientation. Applying the heat press or clamp in this orientation may reduce the possibility of the curing process causing the misalignment of the two load-bearing elements and the insulating core.
The heat applied, for example via one or more rollers within a heated enclosure, accelerates the adhesive curing process, and the pressure applied to the load-bearing elements ensures a good bond with the insulating core.
The insulating core may comprise an angled surface, corresponding to the shape of the second load-bearing element. The method may comprise applying pressure in a heat press to the corresponding angled surface of the second load-bearing element. The method may comprise the -5 -movement of the structural member along a processing line. The processing line may comprise a plurality of alignment rollers to ensure the correct alignment of the first load-bearing member, the insulating core, and the second load-bearing member.
The orientation of the structural member when it is removed from the processing line may be such that the structural member is correctly oriented for stacking and/or labelling.
According to a second aspect of the invention there is also provided a lintel, the lintel manufactured according to the method of the first aspect of the invention. The lintel may be a thermally-broken lintel.
It will of course be appreciated that features 15 described in relation to one aspect of the present invention may be incorporated into other aspects of the present invention. For example, the method of the invention may incorporate any of the features described with reference to the apparatus of the invention and vice 20 versa.
Description of the Drawings
Embodiments of the present invention will now be 25 described by way of example only with reference to the accompanying schematic drawings of which: Figure 1 shows a cross sectional view of a lintel according to the prior art; Figure 2 shows a cross sectional view of a thermally broken lintel according to the prior art; Figure 3 shows a number of steps of a method according to a first embodiment of the invention; -6 -Figure 4 shows a number of steps following the steps shown in figure 3; Figure 5 shows a number of steps following the steps shown in figure 4; Figure 6 shows a cross-section taken from figure taken through the section marked A-A. 3, Figure 7 shows a cross-section taken from figure taken through the section marked B-B; 3, Figure 8 shows a cross-section taken from figure 3, taken through the section marked C-C; Figure 9 shows a cross-section taken from figure taken through the section marked D-D; 4, Figure 10 shows a cross-section taken from figure taken through the section marked E-E; 5, Figure 11 shows a cross-section taken from figure 5, taken through the section marked F-F; and Figures 12 to 16 show a second embodiment of the invention.
Detailed Description
Figure 3, moving from left to right, shows a number of steps in a method of manufacturing a thermally-broken lintel according to a first aspect of the invention. A first load-bearing element 30 is loaded onto a processing line 32 at a loading station 33, the processing line 32 including a plurality of alignment rollers 34. The processing line 32 includes a number of rollers on which the first load-bearing element 30 is placed which are rotated to move the first load-bearing element along the processing line. The first load-bearing element 30 comprises an elongate square C-shaped metal beam, with a cross section as shown in figure 6. In an alternative embodiment, the first load-bearing element may be an -7 -elongate L-shaped metal beam. The processing line 32 moves the first load-bearing element 30 in the direction X (left to right in figure 3), passing through a first processing station 36. The processing station 36 comprises a traversing adhesive bead applicator and a water mist spray, operated such that as the first load-bearing element 30 moves through the processing station 36, adhesive beads and a water mist are applied to the top surface of the first load-bearing element 30. In an alternative embodiment, the processing station 36 may comprise a traversing adhesive spray. In further alternative embodiments, it may not be necessary that the processing station 36 includes a water mist spray, depending on the particular adhesive being used, and the humidity in the processing area.
The first load-bearing element 30 is moved into an insulation load station 38, where an insulating core 40 is placed on the adhesive covered top surface of the first load-bearing member 30. The insulating core 40 is made of an insulating foam and is approximately cuboid, though with an angled face at the top of the insulating core, as can be seen in figure 7. The insulating foam may be replaced by any suitable insulating material. Preferably, the insulating material has a low thermal conductivity, typically less than 0.1 W/mK. The bottom of the insulating core 40 is the same length and width as the first load-bearing member 30, as can be seen in figure 7. In alternative embodiments, the insulating core may be made up of a plurality of sections, the sections when combined having the same length and width as the first load-bearing member 30. The insulating core 40 is aligned with the first load-bearing member 30 by the alignment rollers 34. As can be seen in figure 7, the top of the insulating core 40 includes an angled -8 -surface, which corresponds with the shape of a second load-bearing element.
The first load-bearing element 30 and insulating core 40 are moved through a second processing station 42, which again comprises a traversing adhesive bead applicator and a water mist spray operated such that as the insulating core 40 moves through the processing station 42, adhesive beads and a water mist are applied to the top surface of the insulating core 42.
The first load-bearing element 30 and insulating core 40 is moved to a top load station, where a second load-bearing element 44 is placed on the top surface of the insulating core 40. The second load-bearing element 44 is an elongate approximately L-shaped metal beam, with a cross section that corresponds to the shape of the top surface of the insulating core 40, as shown in figure 8. Again, the alignment rollers 34 ensure the correct alignment of the first load-bearing element 30, the insulating core 40, and the second load-bearing element 44.
The lintel 45 is then rotated 90 degrees about the longitudinal axis of the lintel 45, as shown in figure 9. The lintel 45 is then moved to a curing line 46, as is shown in figure 5, where the adhesive applied to the first load-bearing element 30, the insulating core 40, and the second load-bearing element 44 is cured. In particular, the lintel is moved through a heat press 48, where rollers in a heated environment press the first load-bearing element 30 and second load-bearing element 44 into the insulating core 40. As can be seen in figure 10 the positioning of the rollers ensures the alignment of the lintel does not change as the lintel is pressed. A second section of rollers may also be used to cure the adhesive applied to the angled section of the insulating -9 -core 40 and second load-bearing element 44, as can be seen in figure 11. Once the curing process is complete, the manufacture of the lintel is substantially complete. Some post processing steps may occur, for example, cutting the lintel to various sizes as required by the end user.
Figures 12 to 16 show a second embodiment of the invention. Like elements, for example the lintel 45' have the same numbers as those given with reference to the first embodiment of the invention. The method step of applying a heat press to the lintel 45, as described with reference to the first embodiment of the invention, is replaced by the step of applying a clamp 50 to the lintel 45', and heating the lintel 45' whilst the clamp 50 is applied. Figure 12 shows the lintel 45' prior to application of the clamp, when the load-bearing elements have been adhesively fastened to the insulating core, and the resultant lintel rotated 90 degrees in orientation, as described for the initial stages of figure 9. The clamp 50 is brought close to the lintel 45' as shown in figure 13, and then lowered and engaged with the first load-bearing element and second load-bearing element as shown in figure 14. Once clamped, heat is applied to the lintel 45' either by direct heating of the clamp 50, or heating the local environment of the lintel 45'. Once the adhesive has been cured, the clamp 50 is removed as shown in figure 15, and then the lintel 45' may be labelled and stacked as required. The clamp 50 may be adjustable for engagement with different sized lintels.
In some embodiments of the invention, the clamp 50 may automatically sense the size of the lintel and adjust for engagement with the lintel accordingly.
Whilst the present invention has been described and illustrated with reference to particular embodiments, it -10 -will be appreciated by those of ordinary skill in the art that the invention lends itself to many different variations not specifically illustrated herein. By way of example only, certain possible variations will now be described. Whilst the heat press has been described as comprising a number of rollers and a heated enclosure, and the structural member is passed through the rollers and heated enclosure, an alternative heat press may comprise heated plates that are pressed into the structural member, for example when the structural member is stationary.
Where in the foregoing description, integers or elements are mentioned which have known, obvious or foreseeable equivalents, then such equivalents are herein incorporated as if individually set forth. Reference should be made to the claims for determining the true scope of the present invention, which should be construed so as to encompass any such equivalents. It will also be appreciated by the reader that integers or features of the invention that are described as preferable, advantageous, convenient or the like are optional and do not limit the scope of the independent claims. Moreover, it is to be understood that such optional integers or features, whilst of possible benefit in some embodiments of the invention, may not be desirable, and may therefore be absent, in other embodiments.

Claims (23)

  1. Claims 1. A method of manufacturing a structural member, the method comprising the steps of: providing a first load-bearing element in a first orientation, providing an insulating core, applying an adhesive to the first load-bearing element or insulating core, bringing the first load-bearing element and insulating core into contact, providing a second load-bearing element, applying an adhesive to the second load-bearing element or insulating core, bringing the second load-bearing element and insulating core into contact, changing the orientation of the structural member, and applying heat and pressureto at least one of the 20 first load-bearing element and second load-bearing element to cure the adhesive.
  2. 2. A method as claimed in claim 1, wherein the structural member is a lintel.
  3. 3. A method as claimed in claim 1 or claim 2, wherein the structural member is a thermally-broken lintel.
  4. 4. A method as claimed in any preceding claim, wherein 30 the first load-bearing element and/or second load-bearing element is metal.
  5. 5. A method as claimed in any preceding claim, wherein the first load-bearing element and second load-bearing -12 -element are joined to the insulating core such that there is no direct contact between the first load-bearing element and second load-bearing element.
  6. 6. A method as claimed in any preceding claim, wherein the step of applying adhesive to the first load-bearing element or insulating core comprises applying adhesive to the first load-bearing element.
  7. 7. A method as claimed in claim 6, wherein the first load-bearing element is oriented such that the insulating core is moved into contact with the first load-bearing element in an approximately downwards direction.
  8. 8. A method as claimed in any preceding claim, wherein the step of applying adhesive to the second load-bearing element or insulating core comprises applying adhesive to the insulating core.
  9. 9. A method as claimed in any preceding claim, wherein the insulating core is oriented such that the second load-bearing element is moved into contact with the insulating core in an approximately vertical downwards direction.
  10. 10. A method as claimed in any preceding claim, wherein the structural member comprises a longitudinal axis, and the change of orientation of the structural member may comprise rotating the structural member approximately 90 degrees about the longitudinal axis.
  11. 11. A method as claimed in any preceding claim, wherein the step of applying heat and pressure to at least one of the first load-bearing element and second load-bearing -13 -element comprises applying a heat press to at least one of the first load-bearing element and second load-bearing element.
  12. 12. A method as claimed in claim 11, wherein the heat press applies pressure to the first load-bearing element or second load-bearing element in an approximately horizontal direction.
  13. 13. A method as claimed in claim 11 or claim 12, wherein the insulating core comprises an angled surface, corresponding to the shape of the second load-bearing element, and the method comprises the step of applying pressure with a heat press to the corresponding angled surface of the second load-bearing element.
  14. 14. A method as claimed in any of claims 11 to 13, wherein the heat press comprises one or more rollers.
  15. 15. A method as claimed in any of claims 1 to 10, comprising the step of clamping at least one of the first load-bearing element and second load-bearing element prior to applying heat to at least one of the first load-bearing element and second load-bearing element.
  16. 16. A method as claimed in claim 15, wherein the step of applying heat to at least one of the first load-bearing element and second load-bearing element comprises applying heat via the clamp.
  17. 17. A method as claimed in claim 15, wherein the step of applying heat to at least one of the first load-bearing element and second load-bearing element comprises applying heat in the vicinity of the clamp.
    -14 -
  18. 18. A method as claimed in any preceding claim, comprising the movement of the structural member along a processing line.
  19. 19. A method as claimed in claim 18, wherein the processing line comprises a plurality of alignment rollers to ensure the correct alignment of the first load-bearing member, the insulating core, and the second load-bearing member.
  20. 20. A lintel, the lintel manufactured according to the method of any of claims 1 to 19.
  21. 21. A lintel as claimed in claim 20, wherein the lintel 15 is a thermally-broken lintel.
  22. 22. A method of manufacturing a lintel substantially as herein described with reference to any of Figs. 3 to 16 of the accompanying drawings.
  23. 23. A lintel manufactured substantially as herein described with reference to any of Figs. 3 to 16 of the accompanying drawings.
GB1522078.3A 2015-01-13 2015-12-15 Method of manufacturing structual member Active GB2535601B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IE20160009A IE87277B1 (en) 2015-01-13 2016-01-12 Method of manufacturing structural member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1500507.7A GB201500507D0 (en) 2015-01-13 2015-01-13 Method of manufacturing structural member

Publications (3)

Publication Number Publication Date
GB201522078D0 GB201522078D0 (en) 2016-01-27
GB2535601A true GB2535601A (en) 2016-08-24
GB2535601B GB2535601B (en) 2021-04-07

Family

ID=52597528

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB1500507.7A Ceased GB201500507D0 (en) 2015-01-13 2015-01-13 Method of manufacturing structural member
GB1522078.3A Active GB2535601B (en) 2015-01-13 2015-12-15 Method of manufacturing structual member

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB1500507.7A Ceased GB201500507D0 (en) 2015-01-13 2015-01-13 Method of manufacturing structural member

Country Status (2)

Country Link
GB (2) GB201500507D0 (en)
IE (1) IE87277B1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5678381A (en) * 1994-11-25 1997-10-21 Denadel; Duane G. Insulated beam
WO2001071119A1 (en) * 2000-03-22 2001-09-27 International Concept Technologies Nv Composite building components
WO2011141402A1 (en) * 2010-05-12 2011-11-17 Akzo Nobel Coatings International B.V. Method of manufacturing a composite product
US20140007543A1 (en) * 2011-06-24 2014-01-09 Ronald T. Den Adel Blast resistant structural building element

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5678381A (en) * 1994-11-25 1997-10-21 Denadel; Duane G. Insulated beam
WO2001071119A1 (en) * 2000-03-22 2001-09-27 International Concept Technologies Nv Composite building components
WO2011141402A1 (en) * 2010-05-12 2011-11-17 Akzo Nobel Coatings International B.V. Method of manufacturing a composite product
US20140007543A1 (en) * 2011-06-24 2014-01-09 Ronald T. Den Adel Blast resistant structural building element

Also Published As

Publication number Publication date
IE87277B1 (en) 2021-11-24
IE20160009A1 (en) 2016-08-24
GB201522078D0 (en) 2016-01-27
GB201500507D0 (en) 2015-02-25
GB2535601B (en) 2021-04-07

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