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CN104339077B - A kind of electron beam welding guard method - Google Patents

A kind of electron beam welding guard method Download PDF

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Publication number
CN104339077B
CN104339077B CN201410629630.5A CN201410629630A CN104339077B CN 104339077 B CN104339077 B CN 104339077B CN 201410629630 A CN201410629630 A CN 201410629630A CN 104339077 B CN104339077 B CN 104339077B
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CN
China
Prior art keywords
protective material
coating
beam welding
hour
electron beam
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
CN201410629630.5A
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Chinese (zh)
Other versions
CN104339077A (en
Inventor
王艳丽
陈桂荣
魏晓丽
田野
张斌
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.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group Co Ltd
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Filing date
Publication date
Application filed by Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201410629630.5A priority Critical patent/CN104339077B/en
Publication of CN104339077A publication Critical patent/CN104339077A/en
Application granted granted Critical
Publication of CN104339077B publication Critical patent/CN104339077B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00Electron-beam welding or cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00Electron-beam welding or cutting
    • B23K15/0033Preliminary treatment

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

A kind of electron beam welding guard method, belongs to electron beam welding technology field.Comprise following processing step: parts processed surface; Prepare protective material, ensure that the viscosity of protective material is in 15 ± 5 scopes, is stirred to not a half hour; The coating of protective material is carried out in non-solder region before weld parts, and the distance of coating zone distance weld seam is 3-5 millimeter, and coverage rate is 100%, and dry 5-10 carries out second time coating after dividing in atmosphere, until uniform fold protective material; The solidification of protective material: after completing the coating needing protection zone, by part dry 1-1.5 hour in atmosphere, right fed to boiler solidifies 1-2 hour in drying baker, and solidification temperature is 80 ± 5 DEG C, then carries out the welding of part; Electron beam welding pipe fitting; The protective material of part has been welded in manual removal.Adopt electro-beam welding method of the present invention, greatly improve quality and the operating efficiency of part, reduce cost.

Description

A kind of electron beam welding guard method
Technical field
The invention belongs to electron beam welding technology field, particularly relate to a kind of electron beam welding guard method.
Background technology
Aviation part CF-34 combustion box is by rear housing by electro-beam welding method, combustion chamber front housing, export orientation vane diffuser is together with inner outlet guide vane flange welding, it is the weld seam of full penetration type, minimum weld width requires at 2.1-2.9mm, need higher power could meet minimum weld width requirement, there is larger splashing at the postwelding weld parts back side, pincers are repaiied workman and are repeatedly polished and could remove, remove splash later surface still remaining have non-ly see vestige, the non-constant of surface quality.The assembly particularly formed after export orientation vane diffuser and inner outlet guide vane flange welding, due to structure, polishing region is narrow, is difficult to splashing to clean out.
Summary of the invention
In order to solve the technical problem of above-mentioned existence; the invention provides a kind of electron beam welding guard method; it can be applied in the coating protective material of piece surface; piece surface is protected when electron beam welding; namely meet initial workpiece development and batch need of production of on-the-spot part, greatly improve quality and the operating efficiency of part.
The technical solution used in the present invention is as follows:
A kind of electron beam welding guard method of the present invention, comprises following processing step:
(1) parts processed surface: clear up protection surface, the surface after cleaning is without greasy dirt, exotic;
(2) prepare protective material: before use, ensure that the viscosity of protective material is within the scope of 15 ± 5S; Or in process and after using a period of time, add toluene, the mixture of dimethylbenzene or toluene or dimethylbenzene dilutes protective material as diluent, ensure that the viscosity of protective material is within the scope of 15 ± 5S, and then carry out the stirring of-1 hour half an hour;
(3) protective material is applied: coating weld seam to be welded lock basal surface non-solder region being carried out to protective material before weld parts, the distance of coating zone distance weld seam is 3-5 millimeter, uniformity is wanted in the coating of weld root locality protection material, coverage rate is 100%, then dry 5-10 carries out second time coating again after dividing in atmosphere, until need protect surface all uniform fold protective materials;
(4) solidification of protective material: after completing the coating needing protection zone, by part dry 1-1.5 hour in atmosphere, right fed to boiler solidifies 1-2 hour in drying baker, and solidification temperature is 80 ± 5 DEG C, then carries out the welding of part;
(5) welding of part: weld by electro-beam welding process code;
(6) removal of protective material: the removal part welded being carried out protective material, the part after solidification can remove coating material by hand, ensures that coating material is removed complete, thorough.
Further, described protective material is anti-splash coating protection agent TURCOFORMMASK522, and adopt the mode of leaching or brushing to be coated in piece surface, its solids content is 34.5%, and viscosity is 15 ± 5S, and after solidification, the bond strength of rete reaches more than 900psi.
Beneficial effect of the present invention:
The present invention, by the research of electron beam welding splatter guard material and progress, makes part finally meet the technical requirement of design drawing and associated documents, and can greatly improve quality and the operating efficiency of part, reduce cost.
Accompanying drawing explanation
Fig. 1 is electron beam welding of the present invention protection part schematic diagram.
In figure: 1. rectified diffusion device assembly, protection zone I of splashing 2., 3. casing leading portion, 4. casing back segment, protection zone II of splashing 5., protection zone III of splashing 6., arrow is designated as electronic beam current direction.
Detailed description of the invention
Describe the present invention below in conjunction with drawings and Examples:
Embodiment: as shown in Figure 1, as shown in Figure 1, for the present invention needs the part of welding, specific embodiments is as follows:
(1) parts processed surface: in order to ensure the adhesion that protective film is good, clear up protection surface, the surface after cleaning is without greasy dirt, exotic;
(2) protective material is prepared: the use viscosity of coating protection agent TURCOFORMMASK522, within the scope of 15 ± 5S, when initially using, need not be added any diluent, can directly use; In use with use a period of time after, due to the volatilization of the solvent in protective agent, need to add toluene, the mixture of dimethylbenzene or toluene and dimethylbenzene dilutes protective material as diluent, ensure that viscosity is within the scope of 15 ± 5S, and then carry out the stirring of 1-1.5 hour; The detection of viscosity is that use No. 5 Zahn cup viscosity meters detect.
(3) protective material is applied: the coating first rectified diffusion device assembly 1 weld seam lock basal surface non-solder region being carried out to protective material before weld parts, the distance of coating zone distance weld seam is 3-5 millimeter, uniformity is wanted in the coating of weld root locality protection material, coverage rate is 100%, then dry 5-10 carries out second time coating again after dividing in atmosphere, until need protect surface all uniform fold protective materials;
(4) solidification of protective material: after completing the coating needing protection zone, by part dry 1-1.5 hour in atmosphere, right fed to boiler solidifies 1-2 hour in drying baker, and solidification temperature is 80 ± 5 DEG C, then carries out the welding of part;
(5) welding of part: weld by electro-beam welding process code;
(6) removal of protective material: the removal part welded being carried out protective material, the part after solidification can remove coating material by hand, ensures that coating material is removed complete, thorough.
(7) according to (1)-(6), two other weld seam casing is comprised to the weld seam of back segment 4 and casing leading portion 3, the weld seam of casing leading portion 3 and rectified diffusion device assembly 1 carries out the removal of the coating of weld seam lock basal surface non-solder locality protection material, solidification, welding and protective material.
Described protective material is anti-splash coating protection agent TURCOFORMMASK522; TURCOFORMMASK522 is a kind of brown; liquid, the peelable type protective material of one-component; the mode of leaching or brushing is adopted to be coated in piece surface; its solids content is 34.5%; viscosity is 15 ± 5S, and after solidification, the bond strength of rete reaches more than 900psi.

Claims (2)

1. an electron beam welding guard method, is characterized in that: comprise following processing step:
(1) parts processed surface: clear up protection surface, the surface after cleaning is without greasy dirt, exotic;
(2) prepare protective material: before use, ensure that the viscosity of protective material is within the scope of 15 ± 5S; Or in process and after using a period of time, the mixture adding toluene, dimethylbenzene or toluene and dimethylbenzene dilutes protective material as diluent, ensure that the viscosity of protective material is within the scope of 15 ± 5S, and then carry out the stirring of-1 hour half an hour;
(3) protective material is applied: coating weld seam to be welded lock basal surface non-solder region being carried out to protective material before weld parts, the distance of coating zone distance weld seam is 3-5 millimeter, uniformity is wanted in the coating of weld root locality protection material, coverage rate is 100%, then second time coating is carried out in atmosphere after dry 5-10 minute again, until surface all uniform fold protective materials need be protected;
(4) solidification of protective material: after completing the coating needing protection zone, by part dry 1-1.5 hour in atmosphere, right fed to boiler solidifies 1-2 hour in drying baker, and solidification temperature is 80 ± 5 DEG C, then carries out the welding of part;
(5) welding of part: weld by electro-beam welding process code;
(6) removal of protective material: the removal part welded being carried out protective material, the part after solidification can remove coating material by hand, ensures that coating material is removed complete, thorough.
2. electron beam welding guard method as claimed in claim 1; it is characterized in that: described protective material is anti-splash coating protection agent TURCOFORMMASK522; the mode of leaching or brushing is adopted to be coated in piece surface; its solids content is 34.5%; viscosity is 15 ± 5S, and after solidification, the bond strength of rete reaches more than 900psi.
CN201410629630.5A 2014-11-11 2014-11-11 A kind of electron beam welding guard method Expired - Fee Related CN104339077B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410629630.5A CN104339077B (en) 2014-11-11 2014-11-11 A kind of electron beam welding guard method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410629630.5A CN104339077B (en) 2014-11-11 2014-11-11 A kind of electron beam welding guard method

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CN104339077A CN104339077A (en) 2015-02-11
CN104339077B true CN104339077B (en) 2016-04-13

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106244968A (en) * 2016-08-30 2016-12-21 广东通宇通讯股份有限公司 A method of arc spraying on the surface of an antenna phase shifter aluminum profile cavity and the aluminum profile cavity
CN112719554A (en) * 2020-12-22 2021-04-30 宁波江丰电子材料股份有限公司 Electron beam welding method adopting welding blocking piece

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN88101238A (en) * 1987-03-09 1988-11-02 阿尔斯汤姆大西洋有限公司 The method of coating protective layer reaches the blade that obtains by this method on titanium alloy blade
CN1223191A (en) * 1998-01-06 1999-07-21 阿尔斯通有限公司 Method for protecting metal work-pieces by welding
CN1902338A (en) * 2003-10-09 2007-01-24 凯克控股公司 Surface reactive preservative for use with solder preforms
CN101168222A (en) * 2007-11-27 2008-04-30 西安理工大学 Stainless steel welding protectant
CN103056510A (en) * 2012-12-19 2013-04-24 江西洪都航空工业集团有限责任公司 Technique for controlling indentation depth of friction stir welding

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN88101238A (en) * 1987-03-09 1988-11-02 阿尔斯汤姆大西洋有限公司 The method of coating protective layer reaches the blade that obtains by this method on titanium alloy blade
CN1223191A (en) * 1998-01-06 1999-07-21 阿尔斯通有限公司 Method for protecting metal work-pieces by welding
CN1902338A (en) * 2003-10-09 2007-01-24 凯克控股公司 Surface reactive preservative for use with solder preforms
CN101168222A (en) * 2007-11-27 2008-04-30 西安理工大学 Stainless steel welding protectant
CN103056510A (en) * 2012-12-19 2013-04-24 江西洪都航空工业集团有限责任公司 Technique for controlling indentation depth of friction stir welding

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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City

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: 20160413

Termination date: 20201111