CN1056549C - Technological process of laser repairing damage area in high-temperature and high-speed wheel disc - Google Patents

Technological process of laser repairing damage area in high-temperature and high-speed wheel disc Download PDF

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Publication number
CN1056549C
CN1056549C CN97111021A CN97111021A CN1056549C CN 1056549 C CN1056549 C CN 1056549C CN 97111021 A CN97111021 A CN 97111021A CN 97111021 A CN97111021 A CN 97111021A CN 1056549 C CN1056549 C CN 1056549C
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China
Prior art keywords
wheel disc
powder
laser
laser irradiation
erosion
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Expired - Fee Related
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CN97111021A
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Chinese (zh)
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CN1199663A (en
Inventor
王茂才
陈江
吴维
白林祥
龙康
王烈炯
华伟刚
窦明伦
庄波
王维岩
邵丕仁
王赋春
王行义
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METAL CORROSION AND PROTECTION
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METAL CORROSION AND PROTECTION
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Priority to CN97111021A priority Critical patent/CN1056549C/en
Publication of CN1199663A publication Critical patent/CN1199663A/en
Application granted granted Critical
Publication of CN1056549C publication Critical patent/CN1056549C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Laser Beam Processing (AREA)

Abstract

The technological method is used for restoring lasers of wheel discs which bear particle erosion, mechanical wear or hot corrosion in rotation at high speed. The technological method is characterized in that a focusing laser beam with high energy is utilized to fuse special metal powder into the erosion area of a wheel disc to form a gradient clad, so the geometric size of the wheel disc in the original design is restored with higher erosion resistance than that of materials of the wheel disc. The present invention has the advantages that the strength in wheel discs is not lowered, and the restored gradient clad has certain carrying capacity at the same time. The present invention also has the advantages of simplicity and convenient implementation. The present invention is an ideal technological method for restoring wheel discs.

Description

The high-temperature and high-speed wheel disc technological process of laser repairing damage area
The present invention relates to a kind of high-temperature and high-speed wheel disc technological process of laser repairing damage area, be applicable to that mainly import or homemade cigarette machine I and II wheel disc suffer the impact injury of catalyst particle, the heat erosion damage of gas turbine wheel disk and steam turbine turbine disk cavitation damage etc. also are applicable to the reparation of all high temperature alloy wheel discs that are operated under other state.
Military service is at high temperature and high speed and wheel disc under the environmental attack situation is arranged, tend to take place the damage of surface local zone, such as the flue-gas expander in oil plant, the catalytic cracking unit energy-recovering machine group (being called for short a cigarette machine) secondary wheel disc, operating temperature is about 720 ℃, rotating speed is 6363 rev/mins, be subjected to the impact of high speed catalyst granules, the dark erosion damage district of 10-12mm takes place at wheel disc tenon tooth place, thereby reduced the intensity of wheel disc, because this wheel disc is the WaspaloyNi base superalloy, common melting welding is repaired and is subject to fire damage, produces fire check.Concentrate for dynamic balancing and elimination erosion ditch wedge angle stress, all adopt turning processing to remove gulley at present.Calculation of finite element strength, wheel disc are through a turning 10mm, and the life-span dropped to 16700 hours by 100000 hours, if once more the turning 10mm life-span will reduce to 1300 hours, wheel disc is in the state of scrapping substantially.Yet high-temperature and high-speed wheel disc like this and so on all is very expensive, makes also very difficultly, is the key issue of using and keeping in repair of restriction cigarette machine always.
For being subjected to work condition environment to corrode institute, the high-temperature and high-speed wheel disc that solves cigarette wheel dish and so on causes the geometry reparation of regional area damage and such industrial requirement of overhaul phase of prolongation wheel disc, the process that purpose of the present invention provides a kind of laser repairing to rebuild the high-temperature and high-speed wheel disc damage zone, the geometry of utilizing this process can recover the wheel disc damage zone also improves the anti-environment of damage zone erosion performance more simultaneously.
The present invention's process is achieved in that the present invention's process key step is to utilize the bombardment with laser beams can accurately modulate high-energy-density apace Co base or Ni base self-fluxing alloy or their mixed powder to be fused on the wheel disc damage zone matrix layer by layer, make it to realize each other the excellent metallurgical combination and form hardness distribution gradient layer, concrete steps are as follows:
1) laser irradiation parameter is:
Laser irradiation density 〉=10w/cm
Laser irradiation speed is second 2.0mm/ second-15mm/
2) laser emission mode: the laser beam focus form is garden shape or rectangle; The collimated excitation beam scan mode is linear scanning, rotation sweep or both is compound; Successively put powder irradiation, layer by layer growth;
3) metal powder material: Ni base self-fluxing powder, the composite powder that Co powder self-fluxing alloy or both mix in proportion;
4) powder preset mode: the plane is put deposited, feeds automatically or both compound, adopts mold copper or graphite or other high-temperature ceramic materials to assist presetting of powder and control the laser cladding moulding of wheel disc erosion district;
5) the reconstruction technical process is applied in the laser in-situ casting:
(1) repairs preparation
(2) implement by above-mentioned 1-4 process
(3) shape reparation
(4) defect repair
(5) machine glazed finish
(6) spraying hardened layer
(7) rotor dynamic balancing.
This process also comprises: need repair preparation in this laser irradiation first being processed, promptly carry out the Non-Destructive Testing and the intensity of common wheel disc and calculate, with the value of distinguishing whether this wheel disc uses in addition and repair; With suitable machined finishing and cleaning surfaces processing being carried out in surface, wheel disc erosion district to also needing.This process also is included in layer quality rebuild in this laser irradiation processing afterwards to laser repairing detection and repairing.
Detect qualified after, adopt large-scale Vertical Mill lathe and hand sand instrument that laser repairing is rebuild layer mill again and repair wheel disc by the geometric shape before dashing, carry out X-ray more thereupon, fluorescence and painted control triage are surveyed, and adopt CO2 laser and YAG laser to repair to detecting open defect, at last, the laser repairing reconstructed surface is polished with the cloth wheel comprehensively.If necessary can be at this surperficial spraying plating erosion resistance coating such as WC, SiC can further improve wheel disc anti-impact erosion ability.Need carry out common rotor dynamic balancing adjustment after the wheel disc assembling after laser repairing is rebuild.After the action of above-mentioned series of steps, whole disk rotors reparation is cleaned one newly, just can put into operation again.For the damage again in the reconstruction district of wheel disc, this process can be reused once more.
The present invention's advantage: restorative procedure is simple, operation easily, the wheel disc matrix is not subjected to big heat effect, indeformable, intensity improves behind the wheel disc reconstruction, has anti-bad environmental attack performance, wheel disc can be repaired repeatedly, repeatedly using, is the effective ways that high-temperature and high-speed wheel disc is repaired, and has very big economic worth.
The present invention's embodiment:
Embodiment 1
1,200,000 tons of/year catalysis of oil plant are split in the catalytic cracking unit energy-recovering machine group, the standby diameter ψ 800 of E-232 type cigarette wheel of U.S.'s import, material Waspaloy, operate in wheel disc tenon tooth zone through one section the dark groove mark that washes away for 10-12mm has taken place, adopt to repair and prepare laser irradiation, the shape mill is repaiied, defect repair, the reconstruction technical process is applied in a whole set of such laser in-situ casting of polishing and rotor dynamic balancing, and this wheel disc has been carried out reconstruction.
Machined parameters is applied in the laser in-situ casting:
Power density 10W/cm
Sweep speed 2.0-3.5mm/ second
Straight line and the scanning of rotation complex light, powder is put in the constituency, and constituency irradiation is successively put powder, and successively irradiation is fed powder automatically, and Cu matter mold, dusty material are Co base and Ni base mixed-powder, reconstruction layer maximum height 15mm is applied in the laser casting.Facts have proved that certain oil plant cigarette machine secondary wheel disc running after first laser repairing rebuild 569 days produces a desired effect fully.

Claims (1)

1. one kind is adopted the casting of laser irradiation original position to apply the process that reconstruction high temperature and high speed rotation roulette is subjected to the damage zone of work condition environment erosion, it is characterized in that this process is by laser irradiation parameter and mode, preset metal powder material and pre-setting method and technical process composition etc., it thes contents are as follows:
1) laser irradiation parameter is:
Laser irradiation density 〉=10 4W/cm 2
Laser irradiation speed is second 2.0mm/ second~15mm/
2) laser irradiation mode: the laser beam focus form is garden shape or rectangle; The collimated excitation beam scan mode is linear scanning, rotation sweep or both is compound; Successively put powder irradiation, layer by layer growth.
3) metal powder material: Ni base self-fluxing powder, Co base self-fluxing powder or the composite powder that both mix in proportion.
4) powder pre-setting method: the plane is put deposited, feeds automatically or both compound, adopts mold copper or graphite or other high-temperature ceramic materials to assist presetting of powder and control the laser cladding moulding of wheel disc erosion district.
5) the reconstruction technical process is applied in the laser in-situ casting:
(1) repairs preparation
(2) implement by above-mentioned 1~4 process
(3) shape reparation
(4) defect repair
(5) machine glazed finish
(6) spraying hardened layer
(7) rotor dynamic balancing
CN97111021A 1997-05-17 1997-05-17 Technological process of laser repairing damage area in high-temperature and high-speed wheel disc Expired - Fee Related CN1056549C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN97111021A CN1056549C (en) 1997-05-17 1997-05-17 Technological process of laser repairing damage area in high-temperature and high-speed wheel disc

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN97111021A CN1056549C (en) 1997-05-17 1997-05-17 Technological process of laser repairing damage area in high-temperature and high-speed wheel disc

Publications (2)

Publication Number Publication Date
CN1199663A CN1199663A (en) 1998-11-25
CN1056549C true CN1056549C (en) 2000-09-20

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CN97111021A Expired - Fee Related CN1056549C (en) 1997-05-17 1997-05-17 Technological process of laser repairing damage area in high-temperature and high-speed wheel disc

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1298880C (en) * 2004-06-30 2007-02-07 中国科学院金属研究所 Magnesium alloy laser surface reinforced repairing method
CN100431773C (en) * 2005-11-17 2008-11-12 沈阳黎明航空发动机(集团)有限责任公司 Laser melting rehabilitation method for titanium alloy thin-wall case

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100463766C (en) * 2005-06-30 2009-02-25 沈阳大陆激光技术有限公司 Screw rotor repairing process
CN100423883C (en) * 2005-12-26 2008-10-08 沈阳大陆激光技术有限公司 Renovation technique of combustion turbine first order jet nozzle
CN100423884C (en) * 2005-12-26 2008-10-08 沈阳大陆激光技术有限公司 Detecting tools for combustion turbine first order jet nozzle renovation technique and renovation technique thereof
CN100400219C (en) * 2006-01-11 2008-07-09 桂林航天工业高等专科学校 Build-up welding repair process of disc shear blade and repaired disc shear blade thereby
CN113718247B (en) * 2021-09-09 2024-02-02 中国人民解放军陆军装甲兵学院 Plasma cladding repair method for copper alloy damaged part

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0176942A1 (en) * 1984-10-01 1986-04-09 General Electric Company Method for repairing metal in an article
EP0504095A2 (en) * 1991-03-13 1992-09-16 United Technologies Corporation Gas turbine engine component repair

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0176942A1 (en) * 1984-10-01 1986-04-09 General Electric Company Method for repairing metal in an article
EP0504095A2 (en) * 1991-03-13 1992-09-16 United Technologies Corporation Gas turbine engine component repair

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1298880C (en) * 2004-06-30 2007-02-07 中国科学院金属研究所 Magnesium alloy laser surface reinforced repairing method
CN100431773C (en) * 2005-11-17 2008-11-12 沈阳黎明航空发动机(集团)有限责任公司 Laser melting rehabilitation method for titanium alloy thin-wall case

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Publication number Publication date
CN1199663A (en) 1998-11-25

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