JPS61165275A - Edge welding method - Google Patents
Edge welding methodInfo
- Publication number
- JPS61165275A JPS61165275A JP660585A JP660585A JPS61165275A JP S61165275 A JPS61165275 A JP S61165275A JP 660585 A JP660585 A JP 660585A JP 660585 A JP660585 A JP 660585A JP S61165275 A JPS61165275 A JP S61165275A
- Authority
- JP
- Japan
- Prior art keywords
- build
- projecting line
- blocks
- space
- welding
- 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.)
- Pending
Links
Landscapes
- Butt Welding And Welding Of Specific Article (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は、タービンブレード等突条部上喘に肉盛溶接を
行う場合のへり溶接方法に関するもである。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to an edge welding method for performing overlay welding on the upper part of a protruding part of a turbine blade or the like.
[従来の技術]
タービンブレード等では、ブレードの耐摩耗性を考慮し
て上端に耐摩耗性の高い金属を肉盛溶接し或はブレード
が摩耗した場合の補修作業どして摩耗分を肉盛溶接する
等している。[Prior art] In turbine blades, etc., a highly wear-resistant metal is overlaid on the upper end of the blade in consideration of its wear resistance, or when the blade is worn out, the wear is replaced by repair work. I do things like weld.
従来のへり溶接方法としては、第5図〜第8図に示づb
のがある。The conventional edge welding method is shown in Figures 5 to 8.
There is.
図中1は母体2に形成したタービンブレード等の突条で
あり、該突条1の上端に溶着金属をそのまま肉盛するも
のである。In the figure, reference numeral 1 denotes a protrusion of a turbine blade or the like formed on the base body 2, and the upper end of the protrusion 1 is directly overlaid with weld metal.
[発明が解決しようどする問題点]
然し乍ら、該突条の肉厚は0.3n++nと薄いものも
あり、従来のへり溶接を施工すると突条自体が溶接時の
熱によって変形し、肉盛金属(ビード)も蛇行や上下に
波打って不安定である。[Problems to be solved by the invention] However, the wall thickness of the protrusions is sometimes as thin as 0.3n++n, and when conventional edge welding is performed, the protrusions themselves are deformed by the heat during welding, and the overlay metal (Beads) are also unstable, meandering and waving up and down.
E問題点を解決するための手段1
本発明は上記実情に鑑みてなしたものであり、対峙する
1対の冷却ブロックにより突条上部に肉盛溶接空間を形
成せしめ、該空間に溶着金属を充填する様にしたもので
ある。Means for Solving Problem E 1 The present invention has been made in view of the above-mentioned circumstances, and a build-up welding space is formed on the upper part of the protrusion by a pair of opposing cooling blocks, and the weld metal is deposited in the space. It is designed to be filled.
[作 用]
1度の溶接作業で所要の肉盛りが行え、冷却ブロックで
溶着金属の形状が規制されると共に突条は冷却されるの
で変形が防止される。[Function] Required build-up can be performed in one welding operation, the cooling block regulates the shape of the weld metal, and the protrusions are cooled to prevent deformation.
[実 施 例] 以下図面を参照しつつ本発明の詳細な説明する。[Example] The present invention will be described in detail below with reference to the drawings.
突条1の」二部に肉盛空間3を形成する1対の冷却ブロ
ック4.5を、突条1を挾込む様に配設し、両冷却ブロ
ック4,5を所要の固定具6によって固定する。前記し
た肉盛空間3にフライワイヤ7をアーク8によって溶融
させて充填してゆく。A pair of cooling blocks 4.5 forming a built-up space 3 in the second part of the protrusion 1 are arranged so as to sandwich the protrusion 1, and both cooling blocks 4 and 5 are secured by a required fixture 6. Fix it. The fly wire 7 is melted by the arc 8 and filled into the build-up space 3 described above.
前記溶接の過程C突条1及び溶着金属9は冷却ブロック
4.5で冷却されるので、突条1の変形が防止されると
共に溶着金属9の形状も安定する。During the welding process C, the protrusions 1 and the weld metal 9 are cooled by the cooling block 4.5, so that deformation of the protrusions 1 is prevented and the shape of the weld metal 9 is stabilized.
尚、肉盛量の多い場合は第2図に示す様に多層盛とすれ
ばよい。In addition, if the amount of overlay is large, multi-layer overlay may be used as shown in FIG.
又、突条1と溶着金属9との融合不良等を解消するには
肉盛空間3の底部を第4図に示す如くするどJ、い。Furthermore, in order to eliminate poor fusion between the protrusion 1 and the weld metal 9, the bottom of the build-up space 3 should be shaped as shown in FIG. 4.
即ら、肉盛空間3の溝幅Wを突条1の肉厚tより若干大
ぎくし、且突条1の上端が肉盛空間3に突出し■肉盛空
間3下端がR又はテーパ形状ににつて漸次溝幅をt迄減
少させる。That is, the groove width W of the build-up space 3 is made slightly larger than the wall thickness t of the protrusion 1, and the upper end of the protrusion 1 protrudes into the build-up space 3, and the lower end of the build-up space 3 is rounded or tapered. The groove width is gradually decreased to t.
ここで、肉盛空間3の溝幅Wを突条1の肉厚tJ:り大
きくしたのは後加工の切削代である。Here, the reason why the groove width W of the build-up space 3 is made larger than the wall thickness tJ of the protrusion 1 is due to the cutting allowance in post-processing.
尚、−ト記冷却ブロックは水冷却してもよく、溶接入熱
の小さい場合は熱伝導性のよい金属塊であってもよい。Note that the cooling block described in (g) may be water-cooled, or may be a metal block with good thermal conductivity when the welding heat input is small.
又、冷却ブロックに充分な′重量があれば特に固定具は
必要ない。Further, if the cooling block has sufficient weight, no special fixtures are required.
「発明の効果」
以上述べた如く本発明によれば、仕」:精度のよく0能
率のよいへり溶接が可能となる。"Effects of the Invention" As described above, according to the present invention, it is possible to perform edge welding with high accuracy and efficiency.
第1図は本発明の実施例を示す斜視図、第2図は本発明
を実施したへり溶接部の側面図、第3図は正断面図、第
4図は肉盛空間底部の拡大図、第5図はへり溶接施工箇
所の斜視図、第6図は従来の方法を実施した場合のへり
溶接部側面図、第7図は平面図、第8図は正断面図であ
る。
1は突条、2は母体、3は肉盛空間、4,5は冷却ブロ
ック、6は固定具、7はフイラワイヤ、8はアーク、9
は溶着金属を示す。FIG. 1 is a perspective view showing an embodiment of the present invention, FIG. 2 is a side view of an edge weld in which the present invention is implemented, FIG. 3 is a front sectional view, and FIG. 4 is an enlarged view of the bottom of the overlay space. FIG. 5 is a perspective view of the edge welding area, FIG. 6 is a side view of the edge weld when the conventional method is carried out, FIG. 7 is a plan view, and FIG. 8 is a front sectional view. 1 is a protrusion, 2 is a base body, 3 is a build-up space, 4 and 5 are cooling blocks, 6 is a fixture, 7 is a filler wire, 8 is an arc, 9
indicates weld metal.
Claims (1)
空間を形成せしめ、該空間に溶着金属を充填することを
特徴とするヘリ溶接方法。1) An edge welding method characterized in that a build-up space is formed on the upper part of the protrusion by a pair of opposing cooling blocks, and the space is filled with weld metal.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP660585A JPS61165275A (en) | 1985-01-17 | 1985-01-17 | Edge welding method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP660585A JPS61165275A (en) | 1985-01-17 | 1985-01-17 | Edge welding method |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS61165275A true JPS61165275A (en) | 1986-07-25 |
Family
ID=11642972
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP660585A Pending JPS61165275A (en) | 1985-01-17 | 1985-01-17 | Edge welding method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61165275A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1466695A1 (en) | 2003-04-12 | 2004-10-13 | Rolls-Royce Deutschland Ltd & Co KG | Method or rebuilding damaged planar articles |
-
1985
- 1985-01-17 JP JP660585A patent/JPS61165275A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1466695A1 (en) | 2003-04-12 | 2004-10-13 | Rolls-Royce Deutschland Ltd & Co KG | Method or rebuilding damaged planar articles |
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