CN106863856B - A kind of method for repairing and mending of PE armour - Google Patents

A kind of method for repairing and mending of PE armour Download PDF

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Publication number
CN106863856B
CN106863856B CN201710068493.6A CN201710068493A CN106863856B CN 106863856 B CN106863856 B CN 106863856B CN 201710068493 A CN201710068493 A CN 201710068493A CN 106863856 B CN106863856 B CN 106863856B
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China
Prior art keywords
armour
block
panel
aluminium sheet
filled
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CN201710068493.6A
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CN106863856A (en
Inventor
黄小忠
陈幸开
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HUNAN BOOM NEW MATERIALS CO Ltd
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HUNAN BOOM NEW MATERIALS CO Ltd
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    • 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
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • 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
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/24Apparatus or accessories not otherwise provided for
    • B29C73/26Apparatus or accessories not otherwise provided for for mechanical pretreatment
    • 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
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/24Apparatus or accessories not otherwise provided for
    • B29C73/26Apparatus or accessories not otherwise provided for for mechanical pretreatment
    • B29C2073/266Apparatus or accessories not otherwise provided for for mechanical pretreatment for cutting out an undercut for anchoring the repairing 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
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/06PE, i.e. polyethylene

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention discloses a kind of method for repairing and mending of PE armour, after the panel of original destruction and the removal of PE armour, it polishes aluminium sheet face, the PE armour that repairing is used block is filled up as PE armour by the way of viscous riveting to be mounted on aluminium sheet, and it is bonded panel in the outer surface that PE armour fills up block, finally gap is filled and led up using repair sheets.The present invention is a kind of monolith replacement for being avoided that PE armour, and the PE armour after repairing keeps original performance, and repairing is at low cost, easy to operate feasible, greatly reduces the method for repairing and mending of the PE armour of the use cost of PE armour.

Description

A kind of method for repairing and mending of PE armour
Technical field
The present invention relates to a kind of shellproof method for repairing and mending, more particularly to a kind of method for repairing and mending of PE armour.
Background technique
For military vehicle commonly using steel plate, ceramic wafer as bullet resistant material, steel plate, ceramic density are big, seriously affect vehicle Mobility.With the development of high molecular material, there is novel high performance material, wherein ultra-high molecular weight polyethylene (PE) fiber has the characteristic of high-strength light, and density is only 1g/cm3, intensity reached 3.3GPa, suppressed using the fiber PE armour have good ballistic performance.
PE armour can be used as the use such as bulletproof armour, bulletproof flashboards, and after by gunslinging, PE armour can be layered And bulge phenomenon, as the PE armour of 20mm thickness designs outside by 100 meters of 7.62 ball, 53 formula rifle, it may appear that diameter is about For the round bulge of 150mm.PE armour after there is layering bulge loses ballistic performance, for traditional PE armour, by It is poor in the cementability of PE, it is necessary to monolith replacement, higher cost.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of monolith replacements for being avoided that PE armour, the PE after repairing Armour keeps original performance, and repairing is at low cost, and easy to operate feasible, the PE for greatly reducing the use cost of PE armour is shellproof The method for repairing and mending of plate.
In order to solve the above technical problem, the present invention provides PE armour method for repairing and mending, the PE armour from It is inward outside the panel 1, PE armour and the aluminium sheet that are bonded together by way of gluing, the panel of original destruction and PE is prevented After diving board removal, the surface of the PE armour to aluminium sheet in face of destroying is polished, by the PE of repairing by the way of viscous riveting Armour is filled up block as PE armour and is mounted on aluminium sheet, and is bonded panel in the outer surface that PE armour fills up block, finally Gap is filled and led up using repair sheets.
It comprises the following steps that
(1), the cutting of PE armour: using hand-held cutting machine or hole making drill from panel side to the PE armour area of bulge The panel and PE armour in domain are cut, the panel 1 and PE armour after removal destruction;
(2), PE armour encapsulates: filling up block as PE armour using PE armour, first fills up block in PE armour Then surrounding aperture fills up block using the glass fabric package PE armour for being soaked with epoxy resin, solidifies for 24 hours~28h;
(3), the aluminium sheet of rear region the viscous riveting of PE armour: will be cut in face of the surface of the PE armour destroyed using sand paper Grinding process is carried out, then bonded adhesives is scratched in face of the surface of the PE armour destroyed in aluminium sheet, by the PE armour after encapsulation Block filling is filled up, then PE armour is filled up by block using rivet and is riveted on aluminium sheet;
(4), gap is filled up: panel being bonded in surface that PE armour fills up block using repair sheets, and by junction Gap tamped, struck off, it is ambient temperature curing for 24 hours~28h.
The cutting of PE armour in above-mentioned steps (1): using limiter when cutting, in order to avoid damage aluminium sheet.
(1), the cutting of PE armour: using hand-held cutting machine from panel side to the panel in the PE armour region of bulge It is cut with PE armour, when cutting, uses limiter, in order to avoid damage aluminium sheet;Limitation depth of cut is 19mm, with bulge area Centered on domain, the square hole of 300mm × 300mm, panel and PE armour after removal destruction are cut out;
(2), PE armour encapsulates: block is filled up as PE armour using the PE armour of 20mm thickness 298mm × 298mm, The surrounding of block first is filled up with 100mm or so aperture in PE armour, then aperture 5mm is soaked with asphalt mixtures modified by epoxy resin using 0.1mm thickness The glass fabric package PE armour of rouge fills up block, and solidification is for 24 hours;
(3), the aluminium sheet of rear region the viscous riveting of PE armour: will be cut in face of the surface of the PE armour destroyed using sand paper Grinding process is carried out, then bonded adhesives is scratched in face of the surface of the PE armour destroyed in aluminium sheet, by the PE armour after encapsulation Block filling is filled up, then uses the rivet of 5mm diameter that PE armour is filled up block and is riveted on aluminium sheet;
(4), gap is filled up: the panel of 300mm × 300mm being bonded in the table that PE armour fills up block using repair sheets Face, and the gap of junction tamped, is struck off, it is ambient temperature curing for 24 hours.
Specific step is as follows:
(1), the cutting of PE armour: PE armour of the diameter for the hole making drill of 300mm from panel side to bulge is used The panel and PE armour in region are cut, and limitation depth of cut is 23mm, and centered on bulge region, cutting out diameter is The circular hole of 300mm, panel and PE armour after removal destruction;Limiter is used when cutting, in order to avoid damage aluminium sheet;
(2), PE armour encapsulates: using 24mm thickness diameter to fill up block as PE armour for the PE armour of 298mm, first In PE armour fill up block surrounding with 100mm or so aperture, aperture 5mm, then using 0.1mm it is thick be soaked with epoxy resin Glass fabric package PE armour fills up block, solidifies 28h;
(3), the aluminium sheet of rear region the viscous riveting of PE armour: will be cut in face of the surface of the PE armour destroyed using sand paper Grinding process is carried out, then bonded adhesives is scratched in face of the surface of the PE armour destroyed in aluminium sheet, by the PE armour after encapsulation Block filling is filled up, then uses the rivet of 5mm diameter that PE armour is filled up block and is riveted on aluminium sheet;
(4), gap is filled up: using the repair sheets diameter is bonded in the table that PE armour fills up block for the panel of 300mm Face, and the gap of junction tamped, is struck off, ambient temperature curing 28h.
The method for repairing and mending of PE armour by adopting the above technical scheme, the beneficial effect is that:
The present invention repairs shellproof PE armour using the method for viscous riveting, need to only cut bulge region, then uses same model PE armour filled up, can avoid the monolith replacement of PE armour, PE armour after repairing keeps original performance, and energy Guarantee the original ballistic performance of PE armour, repair it is at low cost, it is easy to operate feasible, greatly reduce the use of PE armour at This.
In conclusion the present invention is a kind of monolith replacement for being avoided that PE armour, the PE armour after repairing keeps former There is performance, repairing is at low cost, and it is easy to operate feasible, greatly reduce the repairing side of the PE armour of the use cost of PE armour Method.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of PE armour described in the invention.
Specific embodiment
Following embodiment is intended to further illustrate the content of present invention, rather than limits the scope of the invention.
Embodiment 1:
The installation of PE armour: bullet resistant material is used as using the PE armour 4 of 20mm thickness, is pressed in the surrounding of PE armour 4 Distance 200mm drilling, aperture 5mm, then in the back side of PE armour 4 bonding with the aluminium sheet 6 of size 0.5mm thickness, surface is viscous Connect the panel 1 of same size 0.3mm thickness;2h is suppressed, temperature is 60 DEG C, after natural cooling 4h, directlys adopt rivet in equipment On.
Referring to Fig. 1, the method for repairing and mending of PE armour, steps are as follows:
(1), the cutting of PE armour 4: using hand-held cutting machine from 1 side of panel to the face in the PE armour region of bulge Plate 1 and PE armour 4 are cut, and when cutting uses limiter, in order to avoid damage aluminium sheet 6;Limitation depth of cut is 19mm, with drum Centered on wrapping region, the square hole of 300mm × 300mm, panel 1 and PE armour 4 after removal destruction are cut out;
(2), PE armour encapsulates: block 3 is filled up as PE armour using the PE armour of 20mm thickness 298mm × 298mm, The surrounding of block 3 first is filled up with 100mm or so aperture in PE armour, then aperture 5mm is soaked with epoxy using 0.1mm thickness The glass fabric 2 of resin wraps up PE armour and fills up block 3, and solidification is for 24 hours;
(3), the aluminium sheet 6 of rear region the viscous riveting of PE armour: will be cut in face of the table of the PE armour 4 destroyed using sand paper Face carries out grinding process, then scratches bonded adhesives in face of the surface of the PE armour 4 destroyed in aluminium sheet 6, the PE after encapsulation is prevented Diving board fills up the filling of block 3, then uses the rivet 5 of 5mm diameter that PE armour is filled up block 3 and be riveted on aluminium sheet 6;
(4), gap is filled up: the panel 1 of 300mm × 300mm being bonded in PE armour using repair sheets and fills up block 3 Surface, and the gap of junction tamped, is struck off, it is ambient temperature curing for 24 hours.
Armour after the present embodiment repairing can defend 53 formula rifles, and the common steel core bullet of 7.62mm is vertical in 100m distance Do not puncture under shooting, impairment scale is not more than 4 grades.
Embodiment 2:
The installation of PE armour: bullet resistant material is used as using the PE armour 4 of 24mm thickness, is pressed in the surrounding of PE armour 4 Distance 200mm drilling, aperture 5mm, then in the back side of PE armour 4 bonding with the aluminium sheet 6 of size 0.7mm thickness, surface is viscous Connect the panel 1 of same size 0.5mm thickness;2h is suppressed, temperature is 60 DEG C, after natural cooling 4h, directlys adopt rivet in equipment On.
The method for repairing and mending of PE armour, steps are as follows:
(1), the cutting of PE armour: PE armour of the diameter for the hole making drill of 300mm from 1 side of panel to bulge is used The panel 1 and PE armour 4 in region are cut, and limitation depth of cut is 23mm, and centered on bulge region, cutting out diameter is The circular hole of 300mm, panel 1 and PE armour 4 after removal destruction;Limiter is used when cutting, in order to avoid damage aluminium sheet 6;
(2), PE armour encapsulates: use 24mm thickness diameter to fill up block 3 as PE armour for the PE armour of 298mm, 3 surrounding of block first is filled up with 100mm or so aperture in PE armour, then aperture 5mm is soaked with asphalt mixtures modified by epoxy resin using 0.1mm thickness The glass fabric 2 of rouge wraps up PE armour and fills up block 3, solidifies 28h;
(3), the aluminium sheet 6 of rear region the viscous riveting of PE armour: will be cut in face of the table of the PE armour 4 destroyed using sand paper Face carries out grinding process, then scratches bonded adhesives in face of the surface of the PE armour 4 destroyed in aluminium sheet 6, the PE after encapsulation is prevented Diving board fills up the filling of block 3, then uses the rivet 5 of 5mm diameter that PE armour is filled up block 3 and be riveted on aluminium sheet 6;
(4), gap is filled up: being used repair sheets that diameter is bonded in PE armour for the panel 1 of 300mm and is filled up block 3 Surface, and the gap of junction tamped, is struck off, ambient temperature curing 28h.
Armour after the present embodiment repairing can defend 79 formula rifles, and the common steel core bullet of 7.62mm is vertical in 100m distance Do not puncture under shooting, impairment scale is not more than 4 grades.

Claims (4)

1. a kind of method for repairing and mending of PE armour, the PE armour by way of gluing from outside inward to be bonded together Panel, PE armour and aluminium sheet, it is characterized in that: by the panel of original destruction and PE armour removal after, to aluminium sheet face carry out Polishing, fills up block as PE armour for the PE armour that repairing is used by the way of viscous riveting and is mounted on aluminium sheet, and anti-in PE Diving board fills up the outer surface bonding panel of block, is finally filled and led up gap using repair sheets;
It comprises the following steps that
(1), the cutting of PE armour: using hand-held cutting machine or hole making drill from panel side to the PE armour region of bulge Panel and PE armour are cut, the panel and PE armour after removal destruction;
(2), PE armour encapsulates: filling up block as PE armour using PE armour, first fills up the surrounding of block in PE armour Then aperture fills up block using the glass fabric package PE armour for being soaked with epoxy resin, solidifies for 24 hours~28h;
(3), the viscous riveting of PE armour: the aluminium sheet face for cutting rear region is carried out by grinding process using sand paper, then in aluminium sheet face Bonded adhesives is scratched with the surface of the PE armour of destruction, the PE armour after encapsulation is filled up into block filling, then use rivet by PE Armour is filled up block and is riveted on aluminium sheet;
(4), gap is filled up: panel being bonded in the surface that PE armour fills up block using repair sheets, and by the seam of junction Gap is tamped, is struck off, it is ambient temperature curing for 24 hours~28h.
2. the method for repairing and mending of PE armour according to claim 1, it is characterized in that: PE armour in above-mentioned steps (1) Cutting: using limiter when cutting, in order to avoid damage aluminium sheet.
3. the method for repairing and mending of PE armour according to claim 1 or 2, it is characterized in that: specific step is as follows:
(1), the cutting of PE armour: using hand-held cutting machine from panel side to the panel and PE in the PE armour region of bulge Armour is cut;Limitation depth of cut is that 19mm cuts out the square hole of 300mm × 300mm centered on bulge region, Panel and PE armour after removal destruction;
(2), PE armour encapsulates: filling up block as PE armour using the PE armour of 20mm thickness 298mm × 298mm, first exists PE armour fills up the surrounding of block with 100mm or so aperture, aperture 5mm, then using 0.1mm it is thick be soaked with epoxy resin Glass fabric package PE armour fills up block, and solidification is for 24 hours;
(3), the viscous riveting of PE armour: the aluminium sheet for cutting rear region is carried out in face of the surface of the PE armour destroyed using sand paper Then grinding process scratches bonded adhesives in face of the surface of the PE armour destroyed in aluminium sheet, the PE armour after encapsulation is filled up Block filling, then use the rivet of 5mm diameter that PE armour is filled up block and be riveted on aluminium sheet;
(4), gap is filled up: the panel of 300mm × 300mm is bonded in the surface that PE armour fills up block using repair sheets, And the gap of junction is tamped, is struck off, it is ambient temperature curing for 24 hours.
4. the method for repairing and mending of PE armour according to claim 1 or 2, it is characterized in that: specific step is as follows:
(1), the cutting of PE armour: PE armour region of the diameter for the hole making drill of 300mm from panel side to bulge is used Panel and PE armour cut, limitation depth of cut be 23mm, centered on bulge region, cut out diameter be 300mm Circular hole, removal destroy after panel and PE armour;
(2), PE armour encapsulates: using 24mm thickness diameter to fill up block as PE armour for the PE armour of 298mm, first in PE Armour fills up block surrounding with 100mm or so aperture, then aperture 5mm uses the glass for being soaked with epoxy resin of 0.1mm thickness Fiber cloth package PE armour fills up block, solidifies 28h;
(3), the viscous riveting of PE armour: the aluminium sheet for cutting rear region is carried out in face of the surface of the PE armour destroyed using sand paper Then grinding process scratches bonded adhesives in face of the surface of the PE armour destroyed in aluminium sheet, the PE armour after encapsulation is filled up Block filling, then use the rivet of 5mm diameter that PE armour is filled up block and be riveted on aluminium sheet;
(4), gap is filled up: use the repair sheets diameter is bonded in the surface that PE armour fills up block for the panel of 300mm, and The gap of junction is tamped, is struck off, ambient temperature curing 28h.
CN201710068493.6A 2017-02-08 2017-02-08 A kind of method for repairing and mending of PE armour Active CN106863856B (en)

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107804004A (en) * 2017-10-22 2018-03-16 巩浩然 A kind of nylon pulley block excavation filling mend method and reparation clamping structure
CN108749011A (en) * 2018-05-24 2018-11-06 湖北三江航天万峰科技发展有限公司 The high seamless viscous rivetting method of thickness functional material

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2131741A (en) * 1982-12-10 1984-06-27 Ronald William Jenkins Panel repair method
CN103770346A (en) * 2014-01-07 2014-05-07 杭州华聚复合材料有限公司 Repairing method of thermoplastic cellular board
CN105173109A (en) * 2014-06-06 2015-12-23 哈尔滨飞机工业集团有限责任公司 Repairing method for honeycomb sandwich structure
CN105750815A (en) * 2016-02-25 2016-07-13 陕西飞机工业(集团)有限公司 Skin damage repair method for aluminum alloy skin foam sandwich part
CN205808250U (en) * 2016-06-14 2016-12-14 湖南博翔新材料有限公司 A kind of composite construction of PE armour

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2131741A (en) * 1982-12-10 1984-06-27 Ronald William Jenkins Panel repair method
CN103770346A (en) * 2014-01-07 2014-05-07 杭州华聚复合材料有限公司 Repairing method of thermoplastic cellular board
CN105173109A (en) * 2014-06-06 2015-12-23 哈尔滨飞机工业集团有限责任公司 Repairing method for honeycomb sandwich structure
CN105750815A (en) * 2016-02-25 2016-07-13 陕西飞机工业(集团)有限公司 Skin damage repair method for aluminum alloy skin foam sandwich part
CN205808250U (en) * 2016-06-14 2016-12-14 湖南博翔新材料有限公司 A kind of composite construction of PE armour

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