CN101444870A - Method for hot-sizing welded integral vane disk by utilizing electron beam - Google Patents

Method for hot-sizing welded integral vane disk by utilizing electron beam Download PDF

Info

Publication number
CN101444870A
CN101444870A CNA2008102469225A CN200810246922A CN101444870A CN 101444870 A CN101444870 A CN 101444870A CN A2008102469225 A CNA2008102469225 A CN A2008102469225A CN 200810246922 A CN200810246922 A CN 200810246922A CN 101444870 A CN101444870 A CN 101444870A
Authority
CN
China
Prior art keywords
electron beam
blisk
school
shape
sizing
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.)
Granted
Application number
CNA2008102469225A
Other languages
Chinese (zh)
Other versions
CN101444870B (en
Inventor
刘成来
杨胜群
曲伸
刘艳
邵天巍
岳召启
程卫祥
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
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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN2008102469225A priority Critical patent/CN101444870B/en
Publication of CN101444870A publication Critical patent/CN101444870A/en
Application granted granted Critical
Publication of CN101444870B publication Critical patent/CN101444870B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Welding Or Cutting Using Electron Beams (AREA)

Abstract

The invention relates to a method for hot-sizing a welded integral vane disk by utilizing an electron beam, which belongs to the hot-sizing technical field. The method comprises the steps as follows: (1) in the preparation step before welding, the integral vane disk is processed through regional marking based on data variation characteristic according to a vane disk component deformation data table, then the vane disk is cleared, and combined technical equipment is adopted to enable the integral vane disk to achieve the sizing demand; (2) in the electron beam sizing step, the input of electron beam energy is controlled by electron beam sizing parameters according to the deflection range, so as to determine the range for depth of fusion; (3) in the position degree measurement step after sizing, position degree measurement is carried out on the integral vane disk which is processed through electron beam sizing, and the obtained result is recorded, compared and analyzed; and (4) in the heat treatment step for eliminating stress, the integral vane disk whose deformation satisfied the control limit is processed through heat treatment for eliminating stress. Through sizing process, various sizes and position accuracies of welded integral vane disk components fully satisfy the finish machining demands, various performance indexes accord with relevant demands, and the welded integral vane disk components are machined in good quality currently.

Description

A kind of method of utilizing electron beam to the hot school of welded type blisk shape
Technical field
The invention belongs to hot school shape technical field, particularly a kind of method of utilizing electron beam to the hot school of welded type blisk shape.
Background technology
The welded type blisk is complicated large welded structures, promptly utilize electron beam welding that the monomer forging blade is welded into a whole leaf joint, be welded into a blisk with dish again, be finish-machined to the blisk assembly at last, the weld seam length overall reaches 4000mm on this assembly.The manufacturing technology key point of welded type blisk should be the welding of whole leaf joint, but by technological preparation before the weldering, the welding tooling development, test such as layout of welding procedure route and welding condition optimization tackling key problem work, successfully realized the welding of whole leaf joint, but when carrying out electron beam welding with dish again after the processing of whole leaf joint, but because welding deformation and the influence of every accumulated error, cause the blisk assembly process area axial deformation to occur, blade angle is to overproof problems such as change in location, be difficult to satisfy finishing requirements, though successively take different process scheme and process system to heat-treat school shape twice, but all less than improving the circumstances that this assembly will face overproof payment even scrap.
Summary of the invention
In order to solve the blisk assembly process area axial deformation, blade angle appear to overproof problems such as change in location, the invention provides a kind of method of utilizing electron beam to the hot school of welded type blisk shape, the process area axial deformation (is compared with perfect condition, in the warpage that makes progress upward, maximum 2.8mm, minimum of a value 1.08mm, mean value 1.85mm), blade angle is to change in location (the azimuthal variation amount of false boss is in-0.6mm~0.6mm scope, and variable quantity is 1.2mm).
Technical scheme of the present invention is achieved in that a kind of method of utilizing electron beam to the hot school of welded type blisk shape, carries out according to the following steps:
(1) prepares before the weldering
According to the leaf dish assembly deformation data table of measuring, the position of need school shape is measured and indicated at the end at weld seam reverse side lock, surveying record according to deformable blade, by data variation characteristic, blisk is carried out regionality to indicate, clear up the leaf dish then, adopt assembled tool, the blisk assembling is reached school shape requirement;
(2) electron beam school shape
Carry out school shape selection of process parameters and determine that the formal welding parameter of blisk assembly is: high pressure is 150KV according to the blisk deformation data, speed of welding is 8.0~10mm/s, square wave, scan frequency is 50~80Hz, and scan amplitude is 0.8~1.2mm, and welding current is 40~43mA;
1. blisk assembly electron beam school shape parameter
According to the scope of deflection, the input of control beam energy, other parameter constant is only adjusted welding current, determines the scope of fusion penetration.
A) deflection is in (3.0~2.2) mm scope, formal welding line when adopting blisk combination in this zone, and fusion penetration is controlled at (28~33) mm;
B) deflection is in (2.2~1.7) mm scope, 2/3 times formal welding line when adopting blisk combination in this zone, and fusion penetration is controlled at (21~25) mm;
C) deflection is in (1.7~1.2) mm scope, 1/2 times formal welding line when adopting blisk combination in this zone, and fusion penetration is controlled at (15~20) mm;
D) deflection is in (1.2~0.5) mm scope, 1/4 times formal welding line when adopting blisk combination in this zone, and fusion penetration is controlled at (7~10) mm;
2. electron beam school shape program composition
Reach the deformed region that on assembly, identifies according to the blisk deformation data and carry out the shape program composition of electron beam school, realize of the correspondence control of electron beam school shape parameter deformed region;
(3) position measurement after the shape of school
Blisk after the shape of electron beam school is carried out position measurement, record in addition, and compare, analyze;
(4) heat treatment that eliminates stress
To the blisk of deflection in control range, heat treatment eliminates stress.
The specific embodiment
Example 1: is example with leaf joint with dish welding back process area axial deformation, and the electron beam thermal source has advantages such as concentration of energy, numerical control degree height, atmosphere cleaning, and the main technique step of the hot school of the electron beam of welded type blisk shape is as follows:
(1) prepares before the weldering
Adopt three coordinate machine to measure the distortion of 41 blades of welded type blisk, data see Table 1,
Table 1 leaf joint and dish welding front and back deformation data (mm)
Figure A200810246922D00041
Figure A200810246922D00051
Surveying record table according to deformable blade, adopt the oil pen on the shape locus circle internal diameter direction of electron beam school, to identify at the 15mm place, and make curvilinear path according to the data variation difference, with the diameter is that Φ 600mm electron beam trace circle is a theoretical center, deformation values adopts 10 times of amplification processing to carry out that sign, instrument is slide calliper rule, dial gauge and rotating torques, the blisk material is TC4, method for cleaning adopts clean silk to dip in to get acetone carefully to be cleared up, forbid adopting halide reagent cleaning part, bare-handed touch is forbidden at the shape position, school after the cleaning.Adopt assembled tool, the annular inner portion of the good blisk of clamping makes that 41 blades are in free state on the circumference.
(3) electron beam school shape
1. blisk assembly electron beam school shape parameter
Carry out school shape selection of process parameters and determine that the formal welding parameter of blisk assembly is: high pressure is 150KV according to the blisk deformation data, speed of welding is 8.0~10mm/s, square wave, and scan frequency is 50~80Hz, scan amplitude is 0.8~1.2mm; Welding current is 40~43mA;
The unit type that electron beam school shape is adopted is a KS120-G300KM-CNC high pressure vacuum electron-beam welder, and according to the blisk deformation data, school shape technological parameter sees Table 2.
Table 2 electron beam school shape parameter
The welding position Fusion penetration (mm) Welding line (mA) Speed of welding (mm/s) Vacuum pressure (mbar) Sweep waveform Scan frequency (Hz) Scan amplitude (mm)
The process area axial deflection is in (3.0~2.2) mm scope 28~33 40~43 8.0~10.0 ≤4.0×10 -4 Square wave 50~80 0.8~1.2
The process area axial deflection is in (2.2~1.7) mm scope 21~25 26~29 8.0~10.0 ≤4.0×10 -4 Square wave 50~80 0.8~1.2
The process area axial deflection is in (1.7~1.2) mm scope 15~20 20~22 8.0~10.0 ≤4.0×10 -4 Square wave 50~80 0.8~1.2
The process area axial deflection is in (1.5~0.5) mm scope 7~10 10~11 8.0~10.0 ≤4.0×10 -4 Square wave 50~80 0.8~1.2
2. school shape program composition
Reach the curvilinear path that on assembly, identifies according to the blisk deformation data and carry out school shape program composition, realize of the segmented linear gradient corresponding control of school shape technological parameter deformed region.
Adopt the definite school shape technological parameter and the program of establishment, blisk is carried out electron beam school shape.
(3) position measurement after the shape of school
Adopt three coordinate measuring machine to carry out position measurement to the blisk after the shape of electron beam school, write down, analyzed, data see Table 3, digital proof, after adopting electron beam school shape, realized the hot school shape of the blisk that size and positional precision are serious overproof, through measuring, the blisk assembly after the shape of school satisfies finishing requirements fully.
Record before and after the shape of table 3 blisk school
Sequence number Before the shape of school After the shape of school Correcting value Theoretical value Correction-theory
1 55.60 56.30 0.70 53.70 2.60
2 54.96 55.52 0.56 53.70 1.82
3 55.40 55.80 0.40 53.70 2.10
4 55.80 55.96 0.16 53.70 2.26
5 55.58 55.66 0.08 53.70 1.96
6 56.20 56.12 -0.08 53.70 2.42
7 55.80 55.66 -0.14 53.70 1.96
8 55.90 55.50 -0.40 53.70 1.80
9 55.80 55.34 -0.46 53.70 1.64
10 55.90 55.26 -0.64 53.70 1.56
11 55.90 55.26 -0.64 53.70 1.56
12 55.90 55.40 0.50 53.70 1.70
13 55.48 55.08 -0.40 53.70 1.38
14 55.46 55.20 -0.26 53.70 1.50
15 55.30 55.24 -0.06 53.70 1.54
16 55.50 55.50 0 53.70 1.80
17 54.94 55.10 0.16 53.70 1.40
18 55.20 55.6 0.40 53.70 1.90
19 55.46 55.92 0.46 53.70 2.22
20 55.48 55.94 0.46 53.70 2.24
21 55.70 56.10 0.40 53.70 2.40
22 55.48 56.00 0.52 53.70 2.30
23 56.02 56.36 0.34 53.70 2.66
24 56.24 56.34 0.10 53.70 2.64
25 56.26 56.32 0.06 53.70 2.62
26 56.46 56.44 -0.02 53.70 2.74
27 56.18 55.94 -0.24 53.70 2.24
28 57.04 56.76 -0.28 53.70 3.06
29 57.16 56.82 -0.34 53.70 3.12
30 56.48 56.12 -0.36 53.70 2.42
31 56.22 55.80 -0.42 53.70 2.10
32 56.26 55.90 -0.36 53.70 2.20
33 55.60 55.26 -0.34 53.70 1.56
34 55.90 55.56 -0.34 53.70 1.86
35 55.66 55.36 -0.30 53.70 1.66
36 55.86 55.68 -0.18 53.70 1.98
37 55.92 55.82 -0.10 53.70 2.12
38 55.58 55.80 0.22 53.70 2.10
39 55.70 56.12 0.42 53.70 2.42
40 55.70 56.40 0.70 53.70 2.70
41 55.68 56.54 0.86 53.70 2.84
(4) heat treatment that eliminates stress
To deflection blisk in control range, the heat treatment that eliminates stress, system is: 750 ℃, 2.0h, cools off with stove by 500 ℃.
After the serious overproof welded type blisk assembly of size and positional precision adopted electron beam to carry out hot school shape, every size and positional precision satisfied finishing requirements fully, and every performance indications meet related request, and it is qualified that this blisk assembly has now been processed.

Claims (1)

1, a kind of method of utilizing electron beam to the hot school of welded type blisk shape is characterized in that carrying out according to the following steps:
(1) prepares before the weldering
According to the leaf dish assembly deformation data table of measuring, the position of need school shape is measured and indicated at the end at weld seam reverse side lock, surveying record according to deformable blade, by data variation characteristic, blisk is carried out regionality to indicate, clear up the leaf dish then, adopt assembled tool, the blisk assembling is reached school shape requirement;
(2) electron beam school shape
Carry out school shape selection of process parameters and determine that the formal welding parameter of blisk assembly is: high pressure is 150KV according to the blisk deformation data, speed of welding is 8.0~10mm/s, square wave, scan frequency is 50~80Hz, and scan amplitude is 0.8~1.2mm, and welding current is 40~43mA;
1. blisk assembly electron beam school shape parameter
According to the scope of deflection, the input of control beam energy, other parameter constant is only adjusted welding current, determines the scope of fusion penetration, and deflection is at 0.5~3.0mm, and the energy of electron beam is 1/4~1 times a formal welding line, and fusion penetration is controlled at 7~33mm;
2. electron beam school shape program composition
Reach the deformed region that on assembly, identifies according to the blisk deformation data and carry out the shape program composition of electron beam school, realize of the correspondence control of electron beam school shape parameter deformed region;
(3) position measurement after the shape of school
Blisk after the shape of electron beam school is carried out position measurement, record in addition, and compare, analyze;
(4) heat treatment that eliminates stress
To deflection blisk in control range, heat treatment eliminates stress.
CN2008102469225A 2008-12-30 2008-12-30 Method for hot-sizing welded integral vane disk by utilizing electron beam Active CN101444870B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2008102469225A CN101444870B (en) 2008-12-30 2008-12-30 Method for hot-sizing welded integral vane disk by utilizing electron beam

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2008102469225A CN101444870B (en) 2008-12-30 2008-12-30 Method for hot-sizing welded integral vane disk by utilizing electron beam

Publications (2)

Publication Number Publication Date
CN101444870A true CN101444870A (en) 2009-06-03
CN101444870B CN101444870B (en) 2011-07-20

Family

ID=40740917

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2008102469225A Active CN101444870B (en) 2008-12-30 2008-12-30 Method for hot-sizing welded integral vane disk by utilizing electron beam

Country Status (1)

Country Link
CN (1) CN101444870B (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101706245B (en) * 2009-11-06 2011-06-22 无锡透平叶片有限公司 Method for detecting welding deformation amount of vane
CN102837160A (en) * 2012-08-23 2012-12-26 沈阳黎明航空发动机(集团)有限责任公司 Assembling precision control method of single-body blades in blisk of electron beam welding structure
CN103706938A (en) * 2013-12-11 2014-04-09 中国航空工业集团公司北京航空制造工程研究所 Electron beam welding method and system using multiple heat sources to control residual stress
CN103753099A (en) * 2014-01-03 2014-04-30 西安航天动力机械厂 Device for heat shaping of thin-walled titanium alloy parts
CN104475960A (en) * 2014-10-30 2015-04-01 中国科学院金属研究所 Ferronickel-based alloy welding joint heat-affected zone grain boundary liquation crack control method
CN105562919A (en) * 2014-10-13 2016-05-11 沈阳黎明航空发动机(集团)有限责任公司 Control method for electron beam welding splash of part with narrow lock bottom structure
CN105772908A (en) * 2016-04-20 2016-07-20 湖北三环离合器有限公司 Welding method of driven disc and disc welding part
CN109332425A (en) * 2018-09-17 2019-02-15 中车大连机车车辆有限公司 Distortion correcting method
CN110484709A (en) * 2019-08-06 2019-11-22 中国船舶重工集团公司第七二五研究所 A method of eliminating sealing drum welding stress in nuclear reactor heap
CN112496685A (en) * 2020-11-27 2021-03-16 中国航发四川燃气涡轮研究院 Manufacturing method of blisk
CN114888419A (en) * 2022-06-29 2022-08-12 中国航发动力股份有限公司 Electron beam welding shape correction method for short-ring parts

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6639173B1 (en) * 2003-04-30 2003-10-28 General Electric Company Electron beam welding method providing post-weld heat treatment
CN100369706C (en) * 2004-10-22 2008-02-20 沈阳黎明航空发动机(集团)有限责任公司 Vacuum electron beam welding method for thin-walled titanium alloy assembly
JP2006161100A (en) * 2004-12-07 2006-06-22 Fu Sheng Industrial Co Ltd Heat treatment method for golf club head
CN100395068C (en) * 2005-12-29 2008-06-18 东方电气集团东方汽轮机有限公司 High pressure vacuum electronic beam welding method for stator ring of air compressor of gas steam turine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101706245B (en) * 2009-11-06 2011-06-22 无锡透平叶片有限公司 Method for detecting welding deformation amount of vane
CN102837160A (en) * 2012-08-23 2012-12-26 沈阳黎明航空发动机(集团)有限责任公司 Assembling precision control method of single-body blades in blisk of electron beam welding structure
CN103706938B (en) * 2013-12-11 2015-10-21 中国航空工业集团公司北京航空制造工程研究所 A kind of method and system utilizing multi-heat source to control the electron beam welding of residual stress
CN103706938A (en) * 2013-12-11 2014-04-09 中国航空工业集团公司北京航空制造工程研究所 Electron beam welding method and system using multiple heat sources to control residual stress
CN103753099B (en) * 2014-01-03 2016-04-20 西安航天动力机械厂 A kind of device for thin-wall titanium alloy part hot school shape
CN103753099A (en) * 2014-01-03 2014-04-30 西安航天动力机械厂 Device for heat shaping of thin-walled titanium alloy parts
CN105562919A (en) * 2014-10-13 2016-05-11 沈阳黎明航空发动机(集团)有限责任公司 Control method for electron beam welding splash of part with narrow lock bottom structure
CN104475960A (en) * 2014-10-30 2015-04-01 中国科学院金属研究所 Ferronickel-based alloy welding joint heat-affected zone grain boundary liquation crack control method
CN104475960B (en) * 2014-10-30 2016-08-17 中国科学院金属研究所 A kind of iron nickel base alloy welding point heat affected area grain boundary liquation crack controlling means
CN105772908A (en) * 2016-04-20 2016-07-20 湖北三环离合器有限公司 Welding method of driven disc and disc welding part
CN105772908B (en) * 2016-04-20 2018-08-31 湖北三环离合器有限公司 A kind of welding method of driven disc and disk weldment
CN109332425A (en) * 2018-09-17 2019-02-15 中车大连机车车辆有限公司 Distortion correcting method
CN110484709A (en) * 2019-08-06 2019-11-22 中国船舶重工集团公司第七二五研究所 A method of eliminating sealing drum welding stress in nuclear reactor heap
CN112496685A (en) * 2020-11-27 2021-03-16 中国航发四川燃气涡轮研究院 Manufacturing method of blisk
CN114888419A (en) * 2022-06-29 2022-08-12 中国航发动力股份有限公司 Electron beam welding shape correction method for short-ring parts

Also Published As

Publication number Publication date
CN101444870B (en) 2011-07-20

Similar Documents

Publication Publication Date Title
CN101444870B (en) Method for hot-sizing welded integral vane disk by utilizing electron beam
CN102927952B (en) Method for detecting diameter of outer wall of tapered case of aviation engine on line
CN104139321B (en) Large-sized structural parts in site measurement automatic capturing system and aligning method thereof
US20040083024A1 (en) Systems and methods for automated sensing and machining for repairing airfoils of blades
CN105397549B (en) The small change point methods of machine tooling hole face workpiece
CN107717219B (en) RTCP precision error compensation method for five-axis three-dimensional laser cutting machine
CN104246635B (en) For the method processing turbine engine blade trailing edge
JP4855327B2 (en) Tool and tool compensation method
CN103182552B (en) Deep hole processing online detection and correction device
CN104316014B (en) Rapid measurement route planning method of sections of blades of aviation engine
CN103586513B (en) A kind of processing method of PRECISION HOLE of airplane turbine casing mounting edge
CN104625876B (en) Supercharger impeller blade machining process based on on-machine measurement
CN108296533B (en) Counterweight blade double-station Milling Process aligning method and fixture
CN103707132A (en) Method of presetting tools on numerical control machine tool on the basis of spherical-contact sensing part of tool-presetting measuring head
CN107243715A (en) The defect correcting method of one class precision castings blank
Wang et al. Novel on-machine measurement system and method for flatness of large annular plane
CN112629456B (en) System and method for automatically measuring complex curved surface of part of turboshaft engine
CN113917888A (en) Machining precision improving method based on fixed angular orientation calibration and compensation
CN115533287A (en) Method for checking and controlling electron beam welding deviation of nickel electroforming dissimilar metal
CN209605781U (en) A kind of detection device of machined part size
CN107999974B (en) A kind of annular spread group hole laser spot rapid survey and its group's hole forming method
US20240110481A1 (en) Methods of machining turbine components using a reference surface
CN108917691A (en) The measurement method of spiral bevel gear root angle
CN112405114B (en) Method and system for compensating machine tool errors
CN105479266A (en) Five-shaft turn-milling machining center dynamic accuracy testing 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
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

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