JPH0224638B2 - - Google Patents
Info
- Publication number
- JPH0224638B2 JPH0224638B2 JP57192062A JP19206282A JPH0224638B2 JP H0224638 B2 JPH0224638 B2 JP H0224638B2 JP 57192062 A JP57192062 A JP 57192062A JP 19206282 A JP19206282 A JP 19206282A JP H0224638 B2 JPH0224638 B2 JP H0224638B2
- Authority
- JP
- Japan
- Prior art keywords
- welding
- arc
- welded
- irradiation
- weld metal
- 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by any single one of main groups B23K1/00 - B23K28/00
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Heat Treatment Of Articles (AREA)
Description
本発明は溶接継手や溶造管等の溶着金属の強化
法に関する。
2000m深海潜水調査船、あるいは6000m深海潜
水調査船の超高圧で使用される耐圧殼造の際、こ
れら耐圧殼を構成する超高張力鋼に対し貫通金物
はめ込み溶接を行なう必要がある場合がある。こ
れらの溶接継手は増厚、溶接後の切削許容されな
いうえに、外観品質も厳しく、通常のパス数によ
る溶接のままで、所定の強度(0.2%耐力≧90Kg
f/mm2)を得る事が要求される。
これらの溶接法としては一般に被覆アーク溶接
或にはTIG溶接法等が用いられ、板厚によつて第
1図に示すような多層盛り溶接を行う事が多い。
第1図において、0は母材、1〜10は溶着金
属をさすが、それぞれの番号は溶接パスに対応し
ている。
材料が焼入れ後、焼戻し或は時効を施して用い
られるものである場合、第1図のように10パス
の溶接であれば、1〜9パスに相等する中間パス
は、それぞれ2〜10パスの溶接熱により焼戻し
或いは時効の効果が得られ、焼入れ焼戻し或いは
焼入れ時効を施した鋼と同程度の強度レベルが得
られる。ところが最終パスである10パス目で
は、この効果が得られないため、強度レベルは焼
入れのみの鋼程度におちてしまう。たとえば、
NS80、NS90、10Ni−80Co鋼等0.2%耐力が80〜
140Kgf/mm2級の高張力鋼では、10パスめの溶着
金属の0.2%耐力がそれ以外の溶着金属の0.2%耐
力と比較して10〜20Kgf/mm2程度低下する。
このため、従来実際の溶接継手では、
最終パス部の強化低下を考慮して、あらかじ
め継手部の板厚を厚くする
正規の余盛形状になるパス数に加えて更に余
分に積層して、強度レベルの高い部分を増やす
等の処置を施して対応せざるを得ないが、これら
の対策も、溶接後の継手形状が著るしく不均一に
なり溶接後、増厚部或いは余盛部を切削すること
が必要なケースも生じる不具合がある。
本発明は、上記従来技術の欠点を解消し、余分
な板厚増と余盛り積層増にない、最終パス部の溶
着金属の強化法を提供する事を目的とする。
このため本発明は、溶接または溶造工程を伴う
海中船用耐圧殼の製造法において溶接または溶造
の最終パスに相当する溶着金属表面にアーク、電
子ビーム、レーザー光若しくはプラズマ等の高密
度エネルギーを照射しながら高密度エネルギーを
溶接線方向に移動して、当該溶着金属表面に対し
複数回の照射を行い該照射回数を重ねる毎に照射
熱量を減少させることを特徴とする海中船用耐圧
殼の製造法とした。
尚、レーザー光は大気中で、電子ビームは真空
中で、プラズマ及びアークは不活性ガス雰囲気中
で行われる事が多い。また溶着金属へのアーク等
の照射とは少なくとも最終パスに相当する溶着金
属へ照射する事を必要とするという意味であり、
それ以外の溶着金属に照射しても良い。
アーク、電子ビーム、レーザー光及びプラズマ
はいずれもエネルギー密度の高いものであるが、
たとえば、エネルギー密度の低いガス炎等では熱
の拡散が大きく昇温が不十分となり、0.2%耐力
の向上が望めなかつたので上記のとおり限定し
た。
また、本発明で対象とする合金は本実施例で示
された超高張力鋼に限られるものなく、Al合金、
銅合金、Ti合金等、熱処理を施して用いられる
金属材料全てが含まれるが、高強度材料ほどその
効果は著るしい。
以下、実施例を用いて本発明の溶着金属の強化
法について説明する。
実施例として2000m深海潜水調査船耐圧殼を想
定した溶接材の試験結果を説明する。
第2図に本実施例で溶接を行つた継手の開先形
状の断面模式図を示す。第2図において、aの貫
通金物はめ込み継手(H開先)は板厚t30mm、b
の赤道継手(U開先)は板厚t40mmであり、両継
手とも、開先角φ12゜、開先半径R6mmである。
母材とては第1表の組成の0.2%耐力90Kgf/
mm2レベル焼入焼戻鋼NS90を用い、また溶接金属
に相当するワイヤは第2表の組成の共金系の
TN8を用い、下向きに自動TIG溶接を行つた。
溶接条件は第3表に示すとおりである。
すなわち、最終パスである6パス目終了後、溶
接ワイヤの送給を停止し、アーク電流を若干低下
させながら、溶着金属上に2度アークを照射す
る。尚、ここで、照射1パス目の電流値は200〜
300A、照射2パス目の電流値は150〜250A、そ
れ以下の照射パスは200A以下であるほうが熱処
理効果及び作業性の点で好ましい。
溶接及び本発明を施した試験材について第3図
a,bに示す個所より、直径6mmにJISZ3111A−
2号引張試験片を採取し、引張試験を行つた。そ
の結果を第4表に示す。尚、第3図a,bにおい
て表面層Aの試験片採取位置t1、板厚中央部Bの
試験片採取位置t2はそれぞれ母材表面から4mm、
7.5mmであり、また、表面層Cの試験片採取位置
t3、板厚中応部Dの試験片採取位置t4はそれぞれ
5mm、20mmである。
第4表の結果に示されるように、表層部に対し
アークによる加熱を施さない従来法の継手では、
板厚中央部B及びDの0.2%耐力が98〜100Kgf/
mm2の十分高い値となるものの、表層部A及びCで
は90Kgf/mm2の目標値をも下回る80〜85Kgf/mm2
程度の低い0.2%耐力しか得られない。板厚中央
部では、それぞれのパスの溶着金属が次のパスの
溶着金属より熱影響を受けて、焼戻しされるので
高い耐力となるが、最終パスの溶着金属は焼戻し
されないので、低い耐力のままとなつているので
ある。
これに対して表層部にアークを照射した本発明
法の継手では表層部A及びCあつても98〜100Kg
f/mm2と板厚中部B及びDと同等な高い耐力とな
る。尚、本実施例では、溶接後に同じ溶接装置を
そのまま利用し、単にワイヤの送給を停止してア
ーク電流を下げるだけで加熱できるので特別な装
置及び準備作業が不要であり、しかも簡単迅速に
作業が行えるメリツトがある。また、熱処理のた
めにわざわざワイヤを送給する必要がないので、
ビード形状が不自然にもりあがることもなく、ま
た余盛り部を切削する必要もなくなつた。
以上、詳述したように本発明の強化法によれ
ば、エネルギー密度の高い加熱体により時効若し
くは焼もどしを必要とする材料の溶着金属を強化
する事ができ、しかも溶接後の継手形状を均一と
し、余盛部を切削する事も不要である。従つて本
発明法は焼入れ後、焼戻し或いは時効等を行なう
材料の溶接部全てに適用可能であるが、特に加工
精度の要求のきびしい深海潜水調査船、潜水艦等
の耐圧殼、橋梁水圧鉄管の溶接継手の強化法とし
て好適である。
The present invention relates to a method for strengthening welded metal such as welded joints and molten pipes. When constructing pressure-resistant shells for use at ultra-high pressures for 2,000m deep-sea diving research vessels or 6,000m deep-sea diving research vessels, it may be necessary to perform inset welding of penetrating metal fittings to the ultra-high tensile strength steel that composes these pressure shells. These welded joints are not allowed to be thickened or cut after welding, and the appearance quality is also strict.They are still welded by the normal number of passes, and the specified strength (0.2% yield strength ≥ 90 kg) is not allowed.
f/mm 2 ). These welding methods generally include shielded arc welding or TIG welding, and depending on the plate thickness, multilayer build-up welding as shown in FIG. 1 is often performed. In FIG. 1, 0 indicates the base material and 1 to 10 indicate the weld metal, and each number corresponds to a welding pass. If the material is to be used after being quenched and then tempered or aged, if welding requires 10 passes as shown in Figure 1, the intermediate passes equivalent to passes 1 to 9 will consist of passes 2 to 10, respectively. The welding heat produces a tempering or aging effect, resulting in a strength level comparable to that of steel that has been quenched and tempered or quenched and aged. However, in the 10th and final pass, this effect cannot be obtained, and the strength level falls to the same level as steel that has only been quenched. for example,
0.2% yield strength of NS80, NS90, 10Ni−80Co steel, etc. is 80~
140Kgf/mm In class 2 high tensile strength steel, the 0.2% yield strength of the weld metal in the 10th pass is lower by about 10 to 20Kgf/mm2 compared to the 0.2% yield strength of other welded metals. For this reason, conventionally in actual welded joints, the thickness of the joint part is increased in advance to take into account the reduction in reinforcement at the final pass part. In addition to the number of passes required to form the regular reinforcement shape, an additional layer is laminated to increase the strength. We have no choice but to take measures such as increasing the number of high-level parts, but even with these measures, the shape of the joint after welding becomes significantly uneven, resulting in cutting off the thickened part or excess part after welding. There are also cases where it is necessary to do so. It is an object of the present invention to eliminate the drawbacks of the above-mentioned prior art and to provide a method for strengthening the weld metal in the final pass portion without increasing the plate thickness or adding additional layers. For this reason, the present invention applies high-density energy such as arc, electron beam, laser light, or plasma to the surface of the deposited metal corresponding to the final pass of welding or melting in a method for manufacturing a pressure hull for an underwater ship that involves a welding or melting process. Manufacture of a pressure-resistant shell for an underwater ship characterized by moving high-density energy in the direction of the weld line while irradiating, irradiating the surface of the welded metal multiple times, and reducing the amount of irradiation heat each time the irradiation is repeated. It became law. Note that laser beams are often used in the atmosphere, electron beams are used in a vacuum, and plasma and arc are often used in an inert gas atmosphere. Furthermore, irradiation of weld metal with arc, etc. means that it is necessary to irradiate at least the weld metal corresponding to the final pass.
Other weld metals may also be irradiated. Arc, electron beam, laser light and plasma all have high energy density,
For example, with a gas flame or the like with low energy density, the heat diffusion is large and the temperature rise is insufficient, and an improvement in 0.2% proof stress could not be expected, so the above limitations were made. Furthermore, the alloys targeted by the present invention are not limited to the ultra-high tensile strength steel shown in this example, but include Al alloys,
This includes all metal materials that undergo heat treatment, such as copper alloys and Ti alloys, but the higher the strength of the material, the more remarkable the effect. Hereinafter, the method for strengthening weld metal of the present invention will be explained using Examples. As an example, we will explain the test results of a welding material assuming a pressure hull of a 2000m deep-sea submersible research vessel. FIG. 2 shows a schematic cross-sectional view of the groove shape of the joint welded in this example. In Figure 2, the plate thickness of the through-fitting joint (H groove) in a is 30 mm, and b
The equatorial joint (U groove) has a plate thickness of 40 mm, and both joints have a groove angle of φ12° and a groove radius of R6 mm. The base material has a 0.2% yield strength of 90Kgf/with the composition shown in Table 1.
mm 2 Level quenched and tempered steel NS90 was used, and the wire corresponding to the weld metal was a co-metallic wire with the composition shown in Table 2.
Automatic TIG welding was performed downward using TN 8 . The welding conditions are shown in Table 3. That is, after the sixth pass, which is the final pass, the feeding of the welding wire is stopped, and the weld metal is irradiated with arc twice while the arc current is slightly lowered. In addition, here, the current value of the first pass of irradiation is 200~
300 A, the current value of the second irradiation pass is 150 to 250 A, and the current value of the lower irradiation passes is preferably 200 A or less in terms of heat treatment effect and workability. JISZ3111A-
A No. 2 tensile test piece was taken and subjected to a tensile test. The results are shown in Table 4. In addition, in Fig. 3a and b, the test piece sampling position t 1 of the surface layer A and the test piece sampling position t 2 of the plate thickness center part B are respectively 4 mm from the base material surface.
7.5mm, and the specimen sampling position of surface layer C
t 3 and the test piece sampling position t 4 of the mid-thickness section D are 5 mm and 20 mm, respectively. As shown in the results in Table 4, in conventional joints that do not apply arc heating to the surface layer,
0.2% yield strength of plate thickness center part B and D is 98~100Kgf/
mm 2 is a sufficiently high value, but in surface areas A and C it is 80 to 85 Kgf/mm 2 which is lower than the target value of 90 Kgf/mm 2
Only a low yield strength of 0.2% can be obtained. At the center of the plate thickness, the weld metal of each pass is affected by heat and tempered compared to the weld metal of the next pass, resulting in a high yield strength, but the weld metal of the final pass is not tempered, so the yield strength remains low. It has become. On the other hand, in the joint of the present invention in which the surface layer is irradiated with an arc, the weight of the surface layer A and C is 98 to 100 kg.
f/mm 2 and a high yield strength equivalent to those in the middle of the plate thickness B and D. In this example, after welding, the same welding equipment can be used as is, and heating can be done by simply stopping the wire feed and lowering the arc current, so no special equipment or preparation work is required, and it is simple and quick. It has the advantage of being able to work. In addition, there is no need to take the trouble to feed the wire for heat treatment.
The bead shape does not rise unnaturally, and there is no need to cut the excess portion. As detailed above, according to the strengthening method of the present invention, it is possible to strengthen the weld metal of materials that require aging or tempering using a heating element with high energy density, and the shape of the joint after welding is uniform. Therefore, there is no need to cut the excess portion. Therefore, the method of the present invention can be applied to all welded parts of materials that undergo quenching, tempering, or aging, but is particularly applicable to welding of pressure shells of deep-sea research vessels, submarines, etc., and bridge penstocks, which require severe processing accuracy. This method is suitable for strengthening joints.
【表】【table】
【表】【table】
【表】【table】
第1図は溶接継手断面模式図、第2図は開先形
状説明用の溶接継手断面模式図、第3図は試験片
採取位置説明用の溶接継手断面模式図であり、a
はH形開発、bはU形開先のものを指す。
0……母材、1〜10……溶着金属。
Fig. 1 is a schematic cross-sectional view of a welded joint, Fig. 2 is a schematic cross-sectional view of a welded joint for explaining the groove shape, and Fig. 3 is a schematic cross-sectional view of a welded joint for explaining the test piece sampling position.
indicates H-shaped development, and b indicates U-shaped groove. 0... Base material, 1-10... Weld metal.
Claims (1)
製造法において、溶接または溶造の最終パスに相
当する溶着金属表面に、アーク、電子ビーム、レ
ーザー光若しくはプラズマ等の高密度エネルギー
を照射しながら高密度エネルギーを溶接線方向に
移動して、当該溶着金属表面に対し複数回の照射
を行い該照射回数を重ねる毎に照射熱量を減少さ
せることを特徴とする海中船用耐圧殼の製造法。1. In a manufacturing method for pressure hulls for underwater ships that involves welding or melting processes, the surface of the deposited metal corresponding to the final pass of welding or melting is irradiated with high-density energy such as arc, electron beam, laser light, or plasma. A method for manufacturing a pressure shell for an underwater ship, characterized by moving high-density energy in the direction of the welding line, irradiating the surface of the welded metal multiple times, and reducing the amount of irradiation heat each time the irradiation is repeated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19206282A JPS5982187A (en) | 1982-11-01 | 1982-11-01 | Strengthening method of deposited metal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19206282A JPS5982187A (en) | 1982-11-01 | 1982-11-01 | Strengthening method of deposited metal |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5982187A JPS5982187A (en) | 1984-05-12 |
| JPH0224638B2 true JPH0224638B2 (en) | 1990-05-30 |
Family
ID=16284983
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19206282A Granted JPS5982187A (en) | 1982-11-01 | 1982-11-01 | Strengthening method of deposited metal |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5982187A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5343015A (en) * | 1992-11-06 | 1994-08-30 | Fintube Limited Partnership | Laser assisted high frequency welding |
| RU2496618C2 (en) * | 2011-09-14 | 2013-10-27 | Открытое акционерное общество "Ордена Трудового Красного Знамени и ордена труда ЧССР опытное конструкторское бюро "Гидропресс" | Method of automatic pipe welding |
| CN104259666B (en) * | 2014-08-06 | 2016-02-24 | 沈阳富创精密设备有限公司 | A kind of aluminium alloy laser-TIG hybrid welding with filler wire method |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS50133943A (en) * | 1974-04-15 | 1975-10-23 | ||
| JPS6035410B2 (en) * | 1977-07-29 | 1985-08-14 | 株式会社日立製作所 | How to improve the toughness of welded joints |
| JPS5450446A (en) * | 1977-09-30 | 1979-04-20 | Nippon Kokan Kk <Nkk> | Improving method for low-temperature toughness of 9%ni steel weld zone obtained by similar-metal-welding |
-
1982
- 1982-11-01 JP JP19206282A patent/JPS5982187A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5982187A (en) | 1984-05-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6230957B1 (en) | Method of using friction stir welding to repair weld defects and to help avoid weld defects in intersecting welds | |
| EP1169177B9 (en) | Weldable aluminium alloy structural component | |
| EP0005945B1 (en) | Method of welding metal parts | |
| EP0645465A1 (en) | Aluminium alloy casting having high laser weldability, joint of aluminium alloy casting and method for improving aluminium alloy cast structural member | |
| US4817859A (en) | Method of joining nodular cast iron to steel by means of fusion welding | |
| Dwivedi | Fundamentals of metal joining | |
| US5227609A (en) | Method and apparatus for welding | |
| CA1055736A (en) | Welding of age hardenable stainless steel | |
| Kim et al. | Experimental investigation on the laser welding characteristics of 6061-T6 aluminum alloy sheets | |
| JPH0224638B2 (en) | ||
| WO2020148191A1 (en) | Improvements in the welding of pipes | |
| Uchino et al. | A study on adopting λ-shape groove for laser-arc hybrid welding to construct thick plate butt welded joints | |
| Holovko et al. | The influence of introducing refractory compounds into the weld pool on the weld metal dendritic structure | |
| WO2022008750A1 (en) | Welding together of work-pieces | |
| US3679858A (en) | Method forming clad plates from curved surfaces | |
| JPH0616943B2 (en) | Welding repair method for carbon steel, etc. | |
| US5324914A (en) | Method and apparatus for welding precipitation hardenable materials | |
| Bowyer et al. | Design basis for the copper/steel canister | |
| Maydanchuk et al. | restOratIOn Of bells anD art PrODucts maDe Of cOPPer allOys | |
| US20050252901A1 (en) | Low cost titanium welding method | |
| Langford | Plasma arc welding for large titanium aerospace structures | |
| Arivarasu et al. | Investigations on mechanical and metallurgical properties of pulsed GTA welded maraging steel C300 | |
| Batch et al. | Properties of Additively Manufactured Deposits of Alloy 718 | |
| SU841852A1 (en) | Method of argon arc welding | |
| Churiaque Bermejo et al. | Laser Hybrid Butt Welding of Large Thickness Naval Steel |