CN110026733A - A kind of corrosion of metal structure damaged composite material bonding repair method - Google Patents
A kind of corrosion of metal structure damaged composite material bonding repair method Download PDFInfo
- Publication number
- CN110026733A CN110026733A CN201910226073.5A CN201910226073A CN110026733A CN 110026733 A CN110026733 A CN 110026733A CN 201910226073 A CN201910226073 A CN 201910226073A CN 110026733 A CN110026733 A CN 110026733A
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- CN
- China
- Prior art keywords
- corrosion
- composite material
- metal structure
- repair method
- sticking patch
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B19/00—Single-purpose machines or devices for particular grinding operations not covered by any other main group
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B27/00—Other grinding machines or devices
- B24B27/033—Other grinding machines or devices for grinding a surface for cleaning purposes, e.g. for descaling or for grinding off flaws in the surface
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D201/00—Coating compositions based on unspecified macromolecular compounds
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D5/00—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes
- C09D5/08—Anti-corrosive paints
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D7/00—Features of coating compositions, not provided for in group C09D5/00; Processes for incorporating ingredients in coating compositions
- C09D7/40—Additives
- C09D7/60—Additives non-macromolecular
- C09D7/61—Additives non-macromolecular inorganic
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D7/00—Features of coating compositions, not provided for in group C09D5/00; Processes for incorporating ingredients in coating compositions
- C09D7/40—Additives
- C09D7/70—Additives characterised by shape, e.g. fibres, flakes or microspheres
Abstract
The present invention provides a kind of corrosion of metal structure damaged composite material bonding repair method, belongs to Metal Structure Damage and repairs field.This repair method is suitable for corrosion of metal structure damage repair, fills etch pit using the resin material that deployed resin material or the glass fibre added with chopping or metal powder are reinforced, then bonding composites laminate sticking patch.The composite material laminated board sticking patch selected from the composite material laminated board being cured, or uses wet-laid process, is successively laid with, after solidification, finally obtains composite material laminated board sticking patch.The present invention is directed to structure erosion injury region potting resin material, in conjunction with adhesive composite materials laminate sticking patch, it carries out emergency repair and usually repairs, not only having can be avoided secondary damage, slows down stress concentration, improve corrosion-resistant and fatigue performance, weight increases few, outstanding advantages of designability is strong, for the bigger damage of corrosion size, additionally it is possible to meet the rigidity requirement at corrosion damage.
Description
Technical field
The invention belongs to Metal Structure Damages to repair field, and specifically a kind of corrosion of metal structure damaged composite material is viscous
Connect repair method.
Background technique
Metal structure by surrounding medium chemical action or electrochemical action and corrode, the generation of corrosion not only can
Direct economic damage is brought, and ecological environment can be destroyed.After metal structure is corroded, corrosion product and ontology are detached from
It will lead to structural section thickness to become smaller, structural-load-carrying capacity decline.If handled not in time, corrosion can further develop, finally
Lead to structural failure.Although having put into the corrosion protection of metal structure very much, it is difficult to avoid corruption completely
The generation of erosion.It after corrosion occurs, places under repair in time to structure, restores structural-load-carrying capacity, and corresponding anticorrosion is taken to arrange
It applies most important for the service life of extending structure.
After corroding at present for metal structure, if corrosion damage size is more than damage tolerance, machine is generallyd use
The mode that tool is repaired reinforces structure, and carries out corrosion protection.If mainly taking corruption without departing from damage tolerance
Lose safeguard procedures.Metal reinforcing plates are connected to corrosion damage knot by repair of machine, the form mainly taking riveting or being spirally connected
Structure, to restore the bearing capacity of structure.Rivet, be spirally connected repairing need drill on original structure, be bound to cause structure in this way
Secondary damage, and repair construction and need certain space.It just needs detaching structure in order to obtain construction space or opens fabrication hole,
The time for repairing construction in this way will extend.Although after repairing, safeguard procedures can be taken to prevent the generation of corrosion, one
In a little rather harsh environments, for example, high temperature and humidity marine environment with high salt or the direct structure used in the seawater, corrosion
Usually also occur that.At this point, main measure is exactly to reinforce checking and constantly be protected.It is undoubtedly will increase in this way using dimension
The cost of shield.Therefore, the repair method that can restore structural strength and excellent Corrosion Protection well is taken, it is right
It is very significant in corrosion of metal structure damage repair.
It is that composite material laminated board sticking patch is adhered in damaged metal structure that composite material bonding, which is repaired, plays recovery knot
The effect of structure intensity.It is secondary with avoiding relative to traditional mechanical connection repairing that composite material bonding repairs damaged metal structure
It damages, slow down stress concentration, improve corrosion-resistant and fatigue performance, weight increases few, outstanding advantages of designability is strong.More
It is important that composite material itself has very excellent corrosion resistance, moreover, composite panels are adhered to metal structure
After upper, damaged structure and external environs also can be avoided corroding again by bonding region.This patent is just to provide one
The composite material of kind metal erosion damaged structure is bonded repair method.
Summary of the invention
Technical assignment of the invention is in view of the deficiencies of the prior art, to provide a kind of corrosion of metal structure damaged composite material
It is bonded repair method.
To reach above-mentioned target, the present invention proposes a kind of corrosion of metal structure damaged composite material bonding repair method, this
Repair method is suitable for corrosion of metal structure damage repair, using deployed resin material or added with the glass fibers of chopping
The resin material that dimension or metal powder are reinforced fills etch pit, then bonding composites laminate sticking patch.
Optionally, the composite material laminated board sticking patch selected from the composite material laminated board being cured, or uses wet-laying
Method is successively laid with, after solidification, finally obtains composite material laminated board sticking patch.
Optionally, for the composite material laminated board having had been cured, each sideband has appropriate chamfering eight are trimmed to
Side shape, and need to polish to gluing of surfaces, it cleans, dry, be then adhered at Metal Structure Damage, complete solidification.
Optionally, for wet-laid process, the fiber cloth cut is impregnated with deployed resin, is then successively laid with,
And solidify according to selected technique；Fiber cloth herein is glass fabric or carbon cloth；The shape of fiber cloth is eight sides
Shape, round rectangle or circle, ellipse；Size between every adjacent two layers differs 5mm-15mm, the layer of laying in surrounding
Number is determined according to damaged metal concrete condition.
Optionally, for wet-laid process, when selecting carbon cloth, it is necessary to which laying layer of glass cloth first makes metal knot
Structure and carbon cloth are kept apart.
Optionally, the sequence of the laying be according to sticking patch laying size from big to small, or from small to large.
Optionally, the solidification of the composite panels uses and vulcanizes instrument in-situ solidifying, or damaged structure is dismantled down
Come, solidification is completed using autoclave or Electric heat oven and vacuum pump.
Optionally, specific steps include the following:
1) corrosion damage is handled, it is thoroughly clear using mechanical grinding or the method for mechanical grinding combination chemical reagent
Except corrosion product；
2) corrosion area after removing corrosion product is surface-treated；
3) etch pit is filled: by the tree of deployed resin or glass fibre or metal powder reinforcement added with chopping
Rouge material is filled into etch pit, is smeared smooth；
4) after resin filling solidification, at polishing finishing filling, keep it concordant with metal structure face, repaired in order to implement bonding
Reason；After finishing, start bonding composites laminate sticking patch；
5) after the solidification for completing composite panels, polishing finishing is carried out, and restore metal structure surface protective layer.
Optionally, in step 2), specific steps include sandblasting, apply coupling agent.
A kind of corrosion of metal structure damaged composite material of the invention is bonded repair method, produced compared with prior art
Beneficial effect be:
The present invention is directed to structure erosion injury region potting resin material, in conjunction with adhesive composite materials laminate sticking patch, carries out
It emergency repair and usually repairs, not only having can be avoided secondary damage, slows down stress concentration, improve corrosion-resistant and fatigue durability
Outstanding advantages of energy, weight increase less, and designability is strong, for the bigger damage of corrosion size, additionally it is possible to meet and corrode damage
The rigidity requirement of injury.
Detailed description of the invention
Attached drawing 1 is the structure chart of resin filling etch pit of the present invention；
Attached drawing 2 is the shape and structure figure after the composite material laminated board sticking patch finishing that the present invention is cured；
Attached drawing 3 is the shape and structure figure that fiber cloth of the present invention is cut；
Attached drawing 4 is the structure chart that composite panels laying of the present invention is laid with from big to small；
Attached drawing 5 is the structure chart that composite panels laying of the present invention is laid with from small to large.
Respectively label indicates in attached drawing:
1, corrosion damage, 2, resin material, 3, composite material laminated board sticking patch.
Specific embodiment
1-5 with reference to the accompanying drawing makees a kind of corrosion of metal structure damaged composite material bonding repair method of the invention
It is described further below.
The present invention provides a kind of corrosion of metal structure damaged composite material bonding repair method, this repair method is suitable for gold
Belong to structure erosion damage 1 to repair, using deployed resin material 2, (or the glass fibre or metal powder of addition chopping add
Strong resin material 2) filling etch pit, then bonding composites laminate sticking patch 3.Composite material laminated board sticking patch 3, can be with
It is the composite material laminated board being cured, wet-laid process can also be used, be successively laid with, after solidification, finally obtain composite layer
Pressing plate sticking patch 3.
Specific step is as follows:
1) corrosion damage 1 is handled, it is thoroughly clear using mechanical grinding or the method for mechanical grinding combination chemical reagent
Except corrosion product.
2) corrosion area after removing corrosion product is surface-treated, key step includes sandblasting, applies coupling agent.
3) etch pit is filled.It by deployed resin, or is added to the resin of filler and is filled into etch pit, apply and smooth out
It is whole, as shown in Figure 1.
4) after resin filling solidification, at polishing finishing filling, keep it concordant with metal structure face, repaired in order to implement bonding
Reason.After finishing, start bonding composites laminate sticking patch 3.Composite material laminated board sticking patch 3 can be using the lamination being cured
Plate can also use wet-laid process, successively be laid with.For the laminate having had been cured, generally it is trimmed to as shown in Figure 2
Each sideband has the octagon of appropriate chamfering, and needs to polish to gluing of surfaces, cleans, dries, and is then adhered to metal knot
Structure injury region completes solidification.For wet-laid process, then the fiber cloth cut is impregnated with deployed resin, then successively
It is laid with, and solidifies according to selected technique.Fiber cloth herein can be glass fabric, be also possible to carbon cloth, select
When carbon cloth, it is necessary to which laying layer of glass cloth first keeps apart metal structure and carbon cloth.The shape of fiber cloth
Shape can be octagon, be also possible to round rectangle or circle, ellipse, as shown in Figure 3.Size between every adjacent two layers
5mm-15mm should be differed in surrounding, the number of plies of laying is determined according to damaged metal concrete condition.The sequence of laying can be
According to sticking patch laying size from big to small, as shown in figure 4, be also possible to from small to large as shown in Figure 5.
5) after the solidification for completing composite panels, polishing finishing is carried out, and restore metal structure surface protective layer.It is compound
The solidification of material can also be disassembled damaged structure using instrument in-situ solidifying is vulcanized, and be dried using autoclave or electric heating
Case and vacuum pump complete solidification.
Claims (9)
1. a kind of corrosion of metal structure damaged composite material is bonded repair method, which is characterized in that this repair method is suitable for gold
Belong to structure erosion damage repair, is reinforced using deployed resin material or the glass fibre added with chopping or metal powder
Resin material fill etch pit, then bonding composites laminate sticking patch.
2. a kind of corrosion of metal structure damaged composite material according to claim 1 is bonded repair method, which is characterized in that
The composite material laminated board sticking patch selected from the composite material laminated board being cured, or uses wet-laid process, is successively laid with, solidification
Afterwards, composite material laminated board sticking patch is finally obtained.
3. a kind of corrosion of metal structure damaged composite material according to claim 2 is bonded repair method, which is characterized in that
For the composite material laminated board having had been cured, it is trimmed to the octagon that each sideband has appropriate chamfering, and is needed to viscous
It connects surface to polish, cleans, dries, be then adhered at Metal Structure Damage, complete solidification.
4. a kind of corrosion of metal structure damaged composite material according to claim 2 is bonded repair method, which is characterized in that
For wet-laid process, the fiber cloth cut is impregnated with deployed resin, is then successively laid with, and according to selected technique
Solidification；Fiber cloth herein is glass fabric or carbon cloth；The shape of fiber cloth is octagon, round rectangle or circle
Shape, ellipse；Size between every adjacent two layers differs 5mm-15mm in surrounding, and the number of plies of laying is specific according to damaged metal
Situation determines.
5. a kind of corrosion of metal structure damaged composite material according to claim 4 is bonded repair method, which is characterized in that
For wet-laid process, when selecting carbon cloth, it is necessary to which metal structure and carbon cloth is isolated in laying layer of glass cloth first
It comes.
6. a kind of corrosion of metal structure damaged composite material bonding repair method according to any one of claim 2-5,
It is characterized in that, the sequence of the laying be according to sticking patch laying size from big to small, or from small to large.
7. a kind of corrosion of metal structure damaged composite material bonding repair method, feature described in -5 exist according to claim 1
In the solidification of the composite panels, which uses, vulcanizes instrument in-situ solidifying, or damaged structure is disassembled, using autoclave
Or Electric heat oven and vacuum pump complete solidification.
8. a kind of corrosion of metal structure damaged composite material according to any one of claims 1-5 is bonded repair method,
It is characterized in that, specific steps include the following:
1) corrosion damage is handled, using mechanical grinding or the method for mechanical grinding combination chemical reagent, thoroughly removes corruption
Lose product；
2) corrosion area after removing corrosion product is surface-treated；
3) etch pit is filled: by deployed resin or the resinous wood of glass fibre or metal powder reinforcement added with chopping
Material is filled into etch pit, is smeared smooth；
4) after resin filling solidification, at polishing finishing filling, keep it concordant with metal structure face, repaired in order to implement bonding；
After finishing, start bonding composites laminate sticking patch；
5) after the solidification for completing composite panels, polishing finishing is carried out, and restore metal structure surface protective layer.
9. a kind of corrosion of metal structure damaged composite material according to claim 8 is bonded repair method, which is characterized in that
In step 2), specific steps include sandblasting, apply coupling agent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910226073.5A CN110026733A (en) | 2019-03-22 | 2019-03-22 | A kind of corrosion of metal structure damaged composite material bonding repair method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910226073.5A CN110026733A (en) | 2019-03-22 | 2019-03-22 | A kind of corrosion of metal structure damaged composite material bonding repair method |
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| Publication Number | Publication Date |
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| CN110026733A true CN110026733A (en) | 2019-07-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910226073.5A Pending CN110026733A (en) | 2019-03-22 | 2019-03-22 | A kind of corrosion of metal structure damaged composite material bonding repair method |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111958331A (en) * | 2020-08-06 | 2020-11-20 | 国营芜湖机械厂 | Method for repairing damage of large-size hole of complex metal structure |
| CN112507454A (en) * | 2020-12-04 | 2021-03-16 | 中国航空工业集团公司成都飞机设计研究所 | Fiber layering and layer losing method for reinforcing large-area metal structure composite material |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5771557A (en) * | 1996-11-21 | 1998-06-30 | Contrasto; Sam | Concrete internal metal stitching |
| JP2009096900A (en) * | 2007-10-17 | 2009-05-07 | Car Conveni Club Kk | Reactor composition for curing two-liquid type clear main agent and method for forming clear layer using the same |
| EP2253460B1 (en) * | 2000-03-03 | 2015-12-02 | Quickstep Technologies Pty, Ltd. | Method of joining composite components |
| 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 |
| CN109058648A (en) * | 2018-06-29 | 2018-12-21 | 中国石油天然气集团有限公司 | A method of with composite material to the continuous pipe reinforcement recovery of surface damage |
-
2019
- 2019-03-22 CN CN201910226073.5A patent/CN110026733A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5771557A (en) * | 1996-11-21 | 1998-06-30 | Contrasto; Sam | Concrete internal metal stitching |
| EP2253460B1 (en) * | 2000-03-03 | 2015-12-02 | Quickstep Technologies Pty, Ltd. | Method of joining composite components |
| JP2009096900A (en) * | 2007-10-17 | 2009-05-07 | Car Conveni Club Kk | Reactor composition for curing two-liquid type clear main agent and method for forming clear layer using the same |
| 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 |
| CN109058648A (en) * | 2018-06-29 | 2018-12-21 | 中国石油天然气集团有限公司 | A method of with composite material to the continuous pipe reinforcement recovery of surface damage |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111958331A (en) * | 2020-08-06 | 2020-11-20 | 国营芜湖机械厂 | Method for repairing damage of large-size hole of complex metal structure |
| CN112507454A (en) * | 2020-12-04 | 2021-03-16 | 中国航空工业集团公司成都飞机设计研究所 | Fiber layering and layer losing method for reinforcing large-area metal structure composite material |
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Application publication date: 20190719 |