CN105817832B - Pressure vessel field repair is with remanufacturing technique - Google Patents

Pressure vessel field repair is with remanufacturing technique Download PDF

Info

Publication number
CN105817832B
CN105817832B CN201610206171.9A CN201610206171A CN105817832B CN 105817832 B CN105817832 B CN 105817832B CN 201610206171 A CN201610206171 A CN 201610206171A CN 105817832 B CN105817832 B CN 105817832B
Authority
CN
China
Prior art keywords
powder
msub
mrow
pressure vessel
powder feeder
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.)
Expired - Fee Related
Application number
CN201610206171.9A
Other languages
Chinese (zh)
Other versions
CN105817832A (en
Inventor
苗西魁
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201610206171.9A priority Critical patent/CN105817832B/en
Publication of CN105817832A publication Critical patent/CN105817832A/en
Application granted granted Critical
Publication of CN105817832B publication Critical patent/CN105817832B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/04Repairing fractures or cracked metal parts or products, e.g. castings
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/082Coating starting from inorganic powder by application of heat or pressure and heat without intermediate formation of a liquid in the layer
    • C23C24/085Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • C23C24/087Coating with metal alloys or metal elements only

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

The invention discloses pressure vessel field repair and technique is remanufactured, is comprised the following steps:Step 1, grinding process and cleaning treatment are carried out to container position to be repaired;Step 2, cold welding repairing is carried out to position to be repaired, wlding specification is 1.6~2.0mm of Φ, and electric current is 0~300A, and shield gas flow rate is 3 6L/min;Step 3, finishing is carried out to postwelding surface reinforcement and edge until nondestructive inspection detection surface is qualified;Step 4, face progress blasting treatment of repairing watch is treated, make its surface coarsening, one layer of enhancement layer is sprayed to vessel surface using supersonic spray coating technology, spray pressure is 1.5~3.5MPa, and vessel surface temperature is no more than 150 DEG C, and spray distance is 60~120mm.The present invention has the advantage that as follows:Mechanical damage, corrosion, wear defect to vessel surface etc. are repaired, and form enhancement layer of a layer thickness more than 0.1mm in vessel surface, protective container is being resisted the corrosion for disliking summary and abrasion environment, increased the service life for a long time.

Description

Pressure vessel field repair is with remanufacturing technique
Technical field
The present invention relates to pressure vessel to repair field, and particularly a kind of pressure vessel field repair is with remanufacturing technique.
Background technology
Pressure vessel is widely used, and it is that the industries such as petro chemical industry, energy industry, scientific research and military project are indispensable Visual plant.Pressure vessel is typically formed by cylinder, end socket, flange, potted component, perforate and adapter, bearing etc. six are most of Vessel, apply mostly under high temperature, high pressure, the complicated severe rugged environment of high corrosion, often there is various weld defects, knot Structure defect, fault in material, using caused crackle, corrosion, wear etc., along with material caused by long-term extended active duty damages Wound, easily causes the forms such as brittle failure, fatigue, burn into erosion, stress corrosion, intercrystalline corrosion and corrosion fatigue, once thing occurs Therefore extremely serious consequence can be brought.
Because Surface Pressure Vessel degree of impairment is complicated, and many pressure vessel scales are big, and volume is big, tonnage causes greatly It is difficult to field repair is carried out, therefore single renovation technique is indeterminable, many pressure vessels need to use kinds of processes Joint reparation can be only achieved working condition requirement.
The content of the invention
It is an object of the invention to solve at least the above and defect, and provide the advantages of at least will be described later.
A further object of the invention be cold welding is repaired, mechanical reconditioning, overall sandblasting, the process integration such as supersonic spray coating Pressure vessel is repaired, not only vessel surface is repaired, also one layer of enhancement layer is formed in vessel surface, increases the service life.
It is a still further object of the present invention to provide a kind of supersonic spray coating technology, with a kind of two-way powder feeding supersonic cold gas spray Powder and compressed air are formed gas-solid two-phase flow by device, hit matrix under complete solid-state after accelerated, larger modeling occurs Property deformation and be deposited on matrix surface and form enhancement layer.
In order to realize according to object of the present invention and further advantage, there is provided pressure vessel field repair is with remanufacturing Technique, comprise the following steps:
Step 1, grinding process and cleaning treatment are carried out to container position to be repaired;
Step 2, cold welding repairing is carried out to position to be repaired, wlding specification is 1.6~2.0mm of Φ, and electric current is 0~300A, is protected Shield gas flow is 3-6L/min;
Step 3, finishing is carried out to postwelding surface reinforcement and edge until nondestructive inspection detection surface is qualified;
Step 4, face progress blasting treatment of repairing watch is treated, make its surface coarsening, using supersonic spray coating technology to container table Face sprays one layer of enhancement layer, and spray pressure be 1.5~3.5MPa, and vessel surface temperature is no more than 150 DEG C, spray distance for 60~ 120mm。
Preferably, position to be repaired carries out radius of curvature >=20mm after grinding process in the step 1.
Preferably, cold welding electric current is 160~300A in the step 2.
Preferably, cold welding amendment uses the instruments such as angle grinder or hand grinding tool in the step 3.
Preferably, blasting treatment is in the step 4:Sprayed using pressure type sand-blasting machine with 24 mesh white fused alumina sand Sand.
Preferably, sprayed in the step 4 using supersonic spray coating device.
Preferably, the enhancement layer is sprayed by iron(-)base powder forms.
Preferably, in addition to the surface after spraying hole sealing agent is brushed, carries out sealing pores.
Preferably, enhancement layer is formed by a kind of spraying of two-way powder feeding supersonic cold-spraying apparatus in the step 4, is sprayed Device includes:Air accumulator, the first powder feeder, the second powder feeder, air heater and spray gun, the air accumulator separate three air Branch road is connected with the first powder feeder, the second powder feeder, air heater respectively, first powder feeder, the second powder feeder difference The first powder and the second powder transfer to spray gun, compressed air are heated in the air heater under air effect, Air after heating forms supersonic airstream in the spray gun, drives the first powder and the second powder to spray shape from the spray gun Into enhancement layer, wherein, the first valve and the second valve are provided with the branch road where first powder feeder and the second powder feeder, First valve and the second Valve controlling flow are so as to controlling the emitted dose of the first powder and the second powder.
Preferably, the thickness D of the enhancement layer is:
Wherein,For the enhancement layer standard thickness sprayed in the unit time;η is the flow effect factor, zero dimension;Q1For The gas flow of one powder feeder, L/min;Q2For the gas flow of the second powder feeder, L/min;Q3For the gas stream of air heater Amount, L/min;κ1What the powder quality and the first powder feeder that are conveyed for the first powder feeder in the unit time and the second powder feeder conveyed The ratio of powder quality summation;κ2The powder quality conveyed for the second powder feeder in the unit time is sent with the first powder feeder and second The ratio of the powder quality summation of powder device conveying.
The present invention comprises at least following beneficial effect:1st, by selecting rational technological parameter and material, to pressure vessel Surface carries out cold-patch reparation and spraying coating process.Not only the mechanical damage of vessel surface, corrosion default, wear-out defect etc. are repaiied Mend, also form antiseptic wearable coat of a layer thickness more than 0.1mm in vessel surface.Protective container is resisting what evil was omited for a long time Corrosion and abrasion environment, make pressure vessel fundamentally be protected, extend the service life of pressure vessel.2nd, pressure is held The field repair of device is with remanufacturing technique, including Surface Pressure Vessel pretreatment, shaping, cold welding repairing, mechanical reconditioning, lossless spy The process procedures such as wound, overall sandblasting, supersonic spray coating, surface is carried out to pressure vessel by Solvent degreasing, derusting and located in advance Reason, is repaired to the hole of Surface Pressure Vessel, cold welding repairing is made it easier to, using class laser high energy pulse precision cold repair weld pair Defect carries out cold welding repairing, carries out mechanical reconditioning to postwelding surface, makes it concordant with inner surface of container, to carrying out table at cold repair weld Face is detected a flaw, and ensures weld flawless defect etc., is carried out overall blasting treatment to the vessel surface after repair welding, is sprayed using supersonic speed Painting sprays to the surface after sandblasting, forms one layer of antiseptic wearable coat.
Further advantage, target and the feature of the present invention embodies part by following explanation, and part will also be by this The research and practice of invention and be understood by the person skilled in the art.
Brief description of the drawings
Fig. 1 is the two-way powder feeding supersonic cold-spraying apparatus structural representation of the present invention
Fig. 2 is the spray gun structure schematic diagram of the two-way powder feeding supersonic cold-spraying apparatus of the present invention.
Embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings, to make those skilled in the art with reference to specification text Word can be implemented according to this.
It should be appreciated that such as " having ", "comprising" and " comprising " term used herein do not allot one or more The presence or addition of individual other elements or its combination.
Embodiment 1
Chilling tower reparation
Brief introduction:Major function is rapidly to be cooled down the high-temperature tail gas of hydrogenating reduction, and in April, 2010 goes into operation, and equipment is high About 28m, cylinder are rolled by composite plate and are welded, and both ends spherical shell cover is cold stamping shaped making.Parameter such as table 1:
The chilling tower material of table 1 and parameter
Title Material Diameter Thickness (mm) Long/high (m)
Cylinder 20R+304L Φ3600±18 16±3 20.7
End socket 20R+304L Φ3600±18 16±3 0.9
Skirt Q235-B Φ3614 22 6
Find main corrosion feature within 2014:
(1) spot corrosion pit, penetration corrosion pit, diffusion corrosion pit, machinery scratch.
(2) corrosion:Spot corrosion and homogeneous corrosion, spot corrosion Producing reason, be because produced in container higher chlorine from Son;Homogeneous corrosion Producing reason, it is due to have carbon dioxide and hydrogen sulfide gas in solution, makes solution slant acidity.
(3) corrosive medium:Chlorion and hydrogen ion
(4) damage location:Inner tank wall
(5) damage characteristic:There is a thicker yellowish-brown corrosion product on homogeneous corrosion, pitting corrosion, surface, spot corrosion pit, through corruption Lose pit, diffusion corrosion pit and in flakes, machinery scratch etc..
Handled with field repair of the present invention with remanufacturing technique, step is as follows:
Step 1, cold welding pre-treatment
Using method (such as angle grinder, abrasive machine, gauze sander, small-sized polishing machine, fine oil stone, the smooth file of mechanical grinding Knife or fine sandpaper) corrosion layer, fatigue layer and the oxide layer at position to be repaired are removed, until arriving fresh matrix material.To portion to be repaired Position and edge are repaired, and position to be repaired is seamlessly transitted from deep to shallow, are ensured that radius of curvature cannot be less than 20mm.Then use " high-effect detergent for removing grease dirt " thoroughly cleans surface to be repaired, wipes degreasing.Point corrosion pit is polished, detected, depth is less than 1.5mm uses grinding process, and depth uses cold welding method for repairing and mending more than 1.5mm.
Step 2, cold welding repairing
Cold welding repairing uses class laser high energy pulse precision cold repair weld equipment, using 1.6~2.0mm of Φ ER308L wldings Soldering is carried out, operating voltage 30V, operating current is 160~200A, and argon flow amount 5L/min, the cold welding time is 0.07s
Repaired after step 3, cold welding
Postwelding surface reinforcement and edge are repaired with instruments such as angle grinder, hand grinding tools, by polishing, grinding or even throw The methods of light processing soldering position, makes the surface curvature after soldering and surface smoothness are consistent with other positions.
Step 4, acceptance test
Ensure that soldering layer surface is smooth, layer even compact is simultaneously smooth with base material junction;Using lossless spy Triage surveys surface and whether there is weld defect, to unqualified position, should implement repair welding, until reaching requirement.
Step 5, blasting treatment
Using pressure type sand-blasting machine, the surface entirety sandblasting after being repaired from granularity for the white fused alumina sand of 24 mesh to cold welding, Surface coarsening processing is carried out, changes the roughness on surface, makes the mechanical performance on surface be improved, by increasing capacitance it is possible to increase surface and coating Between adhesive force, extend the durability of enhancement layer.
Step 6, spraying enhancement layer, are remanufactured to the surface of repairing, protection repairing surface and enhancing repairing surface Intensity.
Enhancement layer is formed by a kind of spraying of two-way powder feeding supersonic cold-spraying apparatus, as shown in figure 1, spray equipment includes: Compressor 110, air accumulator 120, the first powder feeder 130, the second powder feeder 140, air heater 150, lance tube 160, spray gun 170 and seal bootr 180.Compressor 110 is connected with air accumulator 120, and air forms compressed air after the compression of compressor 110, Store in air accumulator 120;The compressed air flowed out from air accumulator 120 is divided into three tunnels, is supplied to the first powder feeder all the way 130, the second powder feeder 140 is supplied to all the way, and another way is supplied to air heater 150.It is supplied to the He of the first powder feeder 130 The compressed air of second powder feeder 140 is as the driving gas for driving flow of powder in the first powder feeder 130 and the second powder feeder 140 Body, the second powder for making to be stored in the first powder and the second powder feeder 140 of the first powder feeder 130 are transported to lance tube In 160.Wherein, there is provided the compressed air to air heater 150 is heated to form hot-air in air heater 150, Hot-air is delivered in lance tube 160.Air after heating forms supersonic airstream in the spray gun 170, drives the first powder End and the second powder spray from the spray gun 170, realize spraying.It is further that first powder feeder 130 and second is sent The first valve and the second valve, first valve and the second Valve control gas stream are provided with branch road where powder device 140 Measure so as to control the emitted dose of the first powder and the second powder.It is further, as shown in Fig. 2 spray gun 170 includes convergence portion 171st, throat 172, diffusion part 173 and export department 174, the front end of spray gun 170 connect lance tube 160, the lance tube 160 The diameter parallel of axis and spray gun 170.The end of spray gun 170 connects conical seal bootr 180, and the seal bootr 180 is remote One end of spray gun 170 is uncovered structure, and seal bootr 180 covers on sprayed surface and forms closed bin to ensure that supersonic airstream smoothly sprays Apply.The powder of air driven first, the second powder after being heated flow through convergence portion 171, throat 172, diffusion part in spray gun 170 Supersonic airstream is formed after 173, outflow forms gas-solid two-phase flow from export department 174, hits base under complete solid-state after accelerated Body, larger plastic deformation occurs and is deposited on the matrix surface through blasting treatment and forms enhancement layer.
Supersonic spray coating equipment choosing granularity is 15-40 μm of 316L powder of stainless steel, the composition of 316L powder of stainless steel As shown in Table 1, wherein, the first powder is made up of carbon, chromium, nickel, molybdenum, silicon, manganese and sulphur, and the second powder is made up of iron powder.
The 316L powder of stainless steel composition tables of table one
Composition C Cr Ni Mo Si Mn S Fe
Content (%) 0.06 17~19 11~13 1.5~2.5 < 1.0 < 0.6 < 0.5 Surplus
Standard thicknessIt is defined as:Under conditions of reservoir outlet pressure is 2.9MPa, the gas of the first powder feeder is set Body flow Q1For 10L/min, the gas flow Q of the second powder feeder2For 10L/min, the gas flow Q of air heater3For 10L/ The powder quality m of conveying in min, the minutes of the first powder feeder one1Conveyed for 19.5g, the minutes of the second powder feeder one Powder quality m2Under conditions of 19.5g, two-way powder feeding supersonic cold-spraying apparatus is sprayed caused by 1 second on sprayed surface Coating thickness.Through measuring standard thicknessFor 0.35mm.
Spraying parameter is in the present embodiment:The outlet pressure of air accumulator 120 is 2.9MPa, Q1=20L/min;Q2= 60L/min;Q3=50L/min;m1=39g, m2=117g, κ1=m1/(m1+m2)=0.25, κ2=m2/(m1+m2)=0.75;Through The temperature of gas is 120 DEG C after air heater heating, spray distance 60mm.Calculated using formula (1) and (2) and strengthen thickness Spend D:
Wherein,For the enhancement layer thickness sprayed in the unit time;η is the flow effect factor, zero dimension;Q1Sent for first The gas flow of powder device, L/min;Q2For the gas flow of the second powder feeder, L/min;Q3For the gas flow of air heater, L/min;κ1The powder quality and the first powder feeder that are conveyed for the first powder feeder in the unit time and the powder of the second powder feeder conveying The ratio of last quality summation, κ1=m1/(m1+m2);κ2The powder quality conveyed for the second powder feeder in the unit time is sent with first The ratio of powder device and the powder quality summation of the second powder feeder conveying, κ2=m2/(m1+m2)。
η=3.5 calculated according to (2), are strengthened thickness degree D=1.22mm according to formula (1), and porosity is 2.79%.The influence of heat gas temperatures and spray distance is ignored in formula (1) and (2), main to consider flow and powder conveying capacity Influence to coating layer thickness, during actual repair, when the powder proportions of spraying are fixed, i.e. the first powder and the second powder Ratio kappa1κ2It is fixed, it is desirable to the gas flow Q of the first powder feeder1With the gas flow Q of the second powder feeder2Also fix, adjust The gas flow Q of air heater3, the thickness that can obtain coating is calculated by formula, calculates the thickness of enhancement layer It is less than 0.1% with the error actually sprayed.
Step 7, sealing pores
From more than 150 DEG C of heatproof, anti-H 2 S, chlorion and the multifunctional macromolecule of oxide etch base compound hole sealing material Expect to carry out sealing pores to the surface after spraying.
Embodiment 2
Torch liquid separation tank major function is used to come out the drop separation discharged in gas, and in April, 2010 goes into operation, specification of equipment For:1800 × 3600 × 14mm, gross weight are 5.2 tons, and cylinder material is SA516GR.70N, and working media is containing H2S acid Property liquid.
Find that there is the different etch pit of depth, wherein hot spot for torch liquid separation pot bottom large area in maintenance in 2014 Most deep 6.0mm, the corrosion gross area is about 0.6m2
Handled with field repair of the present invention with remanufacturing technique, step is as follows:
Step 1, cold welding pre-treatment
Using method (such as angle grinder, abrasive machine, gauze sander, small-sized polishing machine, fine oil stone, the smooth file of mechanical grinding Knife or fine sandpaper) corrosion layer, fatigue layer and the oxide layer at position to be repaired are removed, until arriving fresh matrix material.To portion to be repaired Position and edge are repaired, and position to be repaired is seamlessly transitted from deep to shallow, are ensured that radius of curvature cannot be less than 20mm.Then use " high-effect detergent for removing grease dirt " thoroughly cleans surface to be repaired, wipes degreasing.Point corrosion pit is polished, detected, depth is less than 3mm, using built-up welding cold-patch restorative procedure, depth is more than 3mm, using the method for digging cold welding pattching.To cold welding rear region immediately 300 DEG C of dehydrogenations are carried out, after dehydrogenation, 100% Magnetic testing and 100% Liquid penetrant testing are carried out to soldering position, until It is qualified.
Step 2, cold welding repairing
Cold welding repairing uses class laser high energy pulse precision cold repair weld equipment, using 1.6~2.0mm of Φ H08Mn (HIC) Wlding carries out soldering, and operating voltage 30V, operating current is 160~200A, argon flow amount 5L/min, and the cold welding time is 0.07s
Repaired after step 3, cold welding
Postwelding surface reinforcement and edge are repaired with instruments such as angle grinder, hand grinding tools, by polishing, grinding or even throw The methods of light processing soldering position, makes the surface curvature after soldering and surface smoothness are consistent with other positions.
Step 4, acceptance test
Ensure that soldering layer surface is smooth, layer even compact is simultaneously smooth with base material junction;Using lossless spy Triage surveys surface and whether there is weld defect, to unqualified position, should implement repair welding, until reaching requirement.
Step 5, blasting treatment
Using pressure type sand-blasting machine, from the white fused alumina sand that granularity is 24 mesh to the inside and outside table of torch liquid separation tank after repairing Face carries out Sa2.5 level blasting treatments.
Step 6, spray-on coating
Organic silicic acid yellow zinc chromate primer paint is done 2 times to torch liquid separation tank inner and outer surfaces, thickness of dry film is 75 μm;Organic silicic acid is heat-resisting Finish paint 2 times, thickness of dry film are 25~40 μm.
As described above, the present invention has the advantages that:1st, by selecting rational technological parameter and material, to pressure Vessel surface carries out cold-patch reparation and spraying coating process.Not only the mechanical damage of vessel surface, corrosion default, wear-out defect etc. are entered Row repairing, also form enhancement layer of a layer thickness more than 0.1mm in vessel surface.Protective container dislikes the corruption of summary resisting for a long time Erosion and abrasion environment, make pressure vessel fundamentally be protected, extend the service life of pressure vessel.2nd, pressure vessel Field repair and remanufacture technique, including Surface Pressure Vessel pretreatment, shaping, cold welding repairing, mechanical reconditioning, lossless spy The process procedures such as wound, overall sandblasting, supersonic cold gas spray, it is pre- that surface is carried out to pressure vessel by Solvent degreasing, derusting Processing, is repaired to the hole of Surface Pressure Vessel, cold welding repairing is made it easier to, using class laser high energy pulse precision cold repair weld Cold welding repairing is carried out to defect, mechanical reconditioning is carried out to postwelding surface, makes it concordant with inner surface of container, to being carried out at cold repair weld Surface inspection, ensure weld flawless defect etc., overall blasting treatment is carried out to the vessel surface after repair welding, using supersonic speed Cold spraying sprays to the surface after sandblasting, forms one layer of enhancement layer.
Although embodiment of the present invention is disclosed as above, it is not restricted in specification and embodiment listed With.It can be applied to various suitable the field of the invention completely., can be easily for those skilled in the art Realize other modification.Therefore it is of the invention and unlimited under the universal limited without departing substantially from claim and equivalency range In specific details and shown here as the legend with description.

Claims (8)

1. pressure vessel field repair is with remanufacturing technique, it is characterised in that comprises the following steps:
Step 1, grinding process and cleaning treatment are carried out to container position to be repaired;
Step 2, cold welding repairing is carried out to position to be repaired, wlding specification is 1.6~2.0mm of Φ, and electric current is 0~300A, protects gas Body flow is 3-6L/min;
Step 3, finishing is carried out to postwelding surface reinforcement and edge until nondestructive inspection detection surface is qualified;
Step 4, face progress blasting treatment of repairing watch is treated, make its surface coarsening, vessel surface is sprayed using supersonic spray coating technology Apply one layer of enhancement layer, spray pressure be 1.5~3.5MPa, and vessel surface temperature is no more than 150 DEG C, spray distance for 60~ 120mm;
Enhancement layer is formed by the spraying of two-way powder feeding supersonic cold-spraying apparatus in the step 4, and spray equipment includes:Air accumulator, First powder feeder, the second powder feeder, air heater and spray gun, the air accumulator separate three air passages and sent respectively with first Powder device, the second powder feeder, air heater connection, first powder feeder, the second powder feeder are respectively by the under air effect One powder and the second powder transfer to spray gun, compressed air are heated in the air heater, and the air after heating is in institute State and supersonic airstream is formed in spray gun, drive the first powder and the second powder to spray to form enhancement layer from the spray gun, wherein, institute State and be provided with the first valve and the second valve, first valve and on the branch road where the first powder feeder and the second powder feeder Two Valve controlling flows are so as to controlling the emitted dose of the first powder and the second powder;
The thickness D of the enhancement layer is:
<mrow> <mi>D</mi> <mo>=</mo> <mover> <mi>D</mi> <mo>&amp;OverBar;</mo> </mover> <mo>&amp;times;</mo> <mi>&amp;eta;</mi> </mrow>
<mrow> <mi>&amp;eta;</mi> <mo>=</mo> <msup> <mrow> <mo>&amp;lsqb;</mo> <msup> <mrow> <mo>(</mo> <mfrac> <msub> <mi>Q</mi> <mn>1</mn> </msub> <msub> <mi>Q</mi> <mn>3</mn> </msub> </mfrac> <mo>)</mo> </mrow> <msub> <mi>&amp;kappa;</mi> <mn>1</mn> </msub> </msup> <mo>+</mo> <msup> <mrow> <mo>(</mo> <mfrac> <msub> <mi>Q</mi> <mn>2</mn> </msub> <msub> <mi>Q</mi> <mn>3</mn> </msub> </mfrac> <mo>)</mo> </mrow> <msub> <mi>&amp;kappa;</mi> <mn>2</mn> </msub> </msup> <mo>&amp;rsqb;</mo> </mrow> <mrow> <mn>3.0179</mn> <mo>&amp;times;</mo> <mfrac> <msub> <mi>Q</mi> <mn>3</mn> </msub> <mrow> <msub> <mi>Q</mi> <mn>1</mn> </msub> <mo>+</mo> <msub> <mi>Q</mi> <mn>2</mn> </msub> </mrow> </mfrac> </mrow> </msup> </mrow>
Wherein,For the enhancement layer standard thickness sprayed in the unit time;η is the flow effect factor, zero dimension;Q1Sent for first The gas flow of powder device, L/min;Q2For the gas flow of the second powder feeder, L/min;Q3For the gas flow of air heater, L/min;κ1The powder quality and the first powder feeder that are conveyed for the first powder feeder in the unit time and the powder of the second powder feeder conveying The ratio of last quality summation;κ2The powder quality conveyed for the second powder feeder in the unit time and the first powder feeder and the second powder feeding The ratio of the powder quality summation of device conveying.
2. pressure vessel field repair according to claim 1 is with remanufacturing technique, it is characterised in that in the step 1 Position to be repaired carries out radius of curvature >=20mm after grinding process.
3. pressure vessel field repair according to claim 2 is with remanufacturing technique, it is characterised in that in the step 2 Cold welding electric current is 160~300A.
4. pressure vessel field repair according to claim 3 is with remanufacturing technique, it is characterised in that in the step 3 Cold welding finishing uses angle grinder or hand grinding tool instrument.
5. pressure vessel field repair according to claim 4 is with remanufacturing technique, it is characterised in that in the step 4 Blasting treatment is:Sandblasting is carried out with 24 mesh white fused alumina sand using pressure type sand-blasting machine.
6. pressure vessel field repair according to claim 5 is with remanufacturing technique, it is characterised in that in the step 4 Sprayed using two-way powder feeding supersonic cold-spraying apparatus.
7. pressure vessel field repair according to claim 6 and remanufacture technique, it is characterised in that the enhancement layer by Iron(-)base powder sprays to be formed.
8. pressure vessel field repair according to claim 7 is with remanufacturing technique, it is characterised in that also includes to spraying Hole sealing agent is brushed on surface afterwards, carries out sealing pores.
CN201610206171.9A 2016-04-05 2016-04-05 Pressure vessel field repair is with remanufacturing technique Expired - Fee Related CN105817832B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610206171.9A CN105817832B (en) 2016-04-05 2016-04-05 Pressure vessel field repair is with remanufacturing technique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610206171.9A CN105817832B (en) 2016-04-05 2016-04-05 Pressure vessel field repair is with remanufacturing technique

Publications (2)

Publication Number Publication Date
CN105817832A CN105817832A (en) 2016-08-03
CN105817832B true CN105817832B (en) 2018-02-09

Family

ID=56525734

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610206171.9A Expired - Fee Related CN105817832B (en) 2016-04-05 2016-04-05 Pressure vessel field repair is with remanufacturing technique

Country Status (1)

Country Link
CN (1) CN105817832B (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106737212A (en) * 2016-12-02 2017-05-31 江苏毅合捷汽车科技股份有限公司 A kind of automobile turbocharger of high-efficiency environment friendly remanufactures blasting craft
CN108968637A (en) * 2017-06-02 2018-12-11 九阳股份有限公司 Cast the manufacturing method of cookware
CN108890214A (en) 2018-07-03 2018-11-27 中信戴卡股份有限公司 A kind of die surface renovation technique
CN109352261B (en) * 2018-11-14 2019-11-15 西安必盛激光科技有限公司 A kind of cold-welding recovery method of cladding laser surfaces hydraulic vertical prop
CN109836027A (en) * 2019-04-11 2019-06-04 苏州工业园区中法环境技术有限公司 The restorative procedure of sludge drying device
CN111872629B (en) * 2020-06-11 2022-04-08 南通鑫拓封头制造有限公司 End socket preparation process for nondifferential repair of micro gap
CN112247339B (en) * 2020-10-12 2022-05-13 菲斯达精密工业部件(苏州)有限公司 Welding process of 5G large-scale die casting
CN112643033A (en) * 2020-11-23 2021-04-13 合肥通用机械研究院有限公司 Additive manufacturing and repairing method for build-up welding cracks of hydrogenation reactor
CN112893055A (en) * 2021-02-08 2021-06-04 新疆八一钢铁股份有限公司 COREX gas chamber bottom plate anticorrosion treatment method
CN113210844A (en) * 2021-04-09 2021-08-06 浙江工业大学 Process method for enhancing sealing performance of welded shell of lithium ion battery based on supersonic laser deposition technology
FR3125733A1 (en) * 2021-07-30 2023-02-03 L'Air Liquide Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude Process for reinforcing and/or repairing mechanically welded equipment under pressure
CN114799722B (en) * 2022-04-14 2023-07-21 江苏海川石化工程技术有限公司 Quick repairing method for local stress corrosion defect of pressure vessel

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5071054A (en) * 1990-12-18 1991-12-10 General Electric Company Fabrication of cast articles from high melting temperature superalloy compositions
CN102061436A (en) * 2010-12-22 2011-05-18 天津大学 Re-manufacturing method of engineering machinery axle and coating of engineering machinery axle
CN102889195A (en) * 2012-07-24 2013-01-23 虞岩贵 Technology for remanufacturing compressor
CN103710660A (en) * 2013-12-24 2014-04-09 中国人民解放军装甲兵工程学院 Method for size restoring and reinforcing of outer wall and inner wall of water-cooling cylinder sleeve of engine
CN104043941A (en) * 2014-06-23 2014-09-17 河南伟彤科技股份有限公司 Re-manufacturing machining process of surface of inner hole of hydraulic cylinder scrap guide sleeve
CN204817040U (en) * 2015-07-31 2015-12-02 北京天诚宇新材料技术有限公司 Double - circuit send whitewashed supersonic speed cold spraying device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5071054A (en) * 1990-12-18 1991-12-10 General Electric Company Fabrication of cast articles from high melting temperature superalloy compositions
CN102061436A (en) * 2010-12-22 2011-05-18 天津大学 Re-manufacturing method of engineering machinery axle and coating of engineering machinery axle
CN102889195A (en) * 2012-07-24 2013-01-23 虞岩贵 Technology for remanufacturing compressor
CN103710660A (en) * 2013-12-24 2014-04-09 中国人民解放军装甲兵工程学院 Method for size restoring and reinforcing of outer wall and inner wall of water-cooling cylinder sleeve of engine
CN104043941A (en) * 2014-06-23 2014-09-17 河南伟彤科技股份有限公司 Re-manufacturing machining process of surface of inner hole of hydraulic cylinder scrap guide sleeve
CN204817040U (en) * 2015-07-31 2015-12-02 北京天诚宇新材料技术有限公司 Double - circuit send whitewashed supersonic speed cold spraying device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
冷喷涂锌镍合金工艺及性能研究;吕保民;《中国优秀硕士学位论文全文数据库》;20130115(第01期);绪论第14,16-17页,正文第51-56页 *

Also Published As

Publication number Publication date
CN105817832A (en) 2016-08-03

Similar Documents

Publication Publication Date Title
CN105817832B (en) Pressure vessel field repair is with remanufacturing technique
CN108559996B (en) A kind of hydraulic support movable post outer surface laser melting coating restorative procedure
CN101767261B (en) Process for repairing water erosion damage of flow passage component of steam turbine and protecting flow passage component of steam turbine
CN104532233B (en) Rotor axle position laser melting coating restorative procedure
CN101797676B (en) Repair and surface protection process of desulfuration recycle pump
CN107520526A (en) A kind of anti-sulphur well head valve body welding repair method
CN105397241B (en) A kind of welding method for 610U2L material spherical tanks
CN110257826A (en) Grain roll bearing position laser cladding method and laser melting coating alloy powder
CN101397663A (en) Novel repair and reconstruction technique for defect treatment of strip coiler hollow axle
CN103100826B (en) A kind of manufacture method of anti-corrosion type hydraulic rod and equipment
CN107723699A (en) A kind of method for repairing heat-resisting alloy
CN105177489A (en) Method for enhancing corrosion and wear resistance of metal member surface
CN109112465A (en) A kind of novel undercarriage Shaft of Titanium Alloy remanufactures repair method
CN101113508A (en) Method for metal parts surface defects restoring and antiseptic treatment
CN105171330B (en) Chilling ring of gasifying furnace restorative procedure
CN111139465A (en) Manufacturing method for manufacturing composite steel pipe by laser
CN107761095A (en) A kind of band chromium coating Axle Parts coating abrasion laser melting coating restorative procedure
CN110241411A (en) Repair the ultrahigh speed laser cladding powder and restorative procedure of impaired water filling combination valve
WO2021073628A1 (en) Cladding welding method applied to hydraulic support column
CN106078525A (en) Large-scale galvanizing surface of the work Pretreatment Technology Before Finishing
CN103817320A (en) Cobalt-based composite powder used for restoring rack of rolling mill and method for restoring rack of rolling mill
JP6046954B2 (en) Solid phase system and method for repairing forged parts
CN111020563A (en) Remanufacturing method for direct laser cladding of failure carburized and quenched part
CN106835119A (en) A kind of oil-field flooding reciprocating type plunger pump plunger restorative procedure
CN112159947A (en) Electric arc spraying method

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180209

Termination date: 20210405