JPH02149682A - Production of aluminum alloy material having superior wear resistance - Google Patents

Production of aluminum alloy material having superior wear resistance

Info

Publication number
JPH02149682A
JPH02149682A JP63304519A JP30451988A JPH02149682A JP H02149682 A JPH02149682 A JP H02149682A JP 63304519 A JP63304519 A JP 63304519A JP 30451988 A JP30451988 A JP 30451988A JP H02149682 A JPH02149682 A JP H02149682A
Authority
JP
Japan
Prior art keywords
base material
wear resistance
alloyed layer
powder
aluminum alloy
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
JP63304519A
Other languages
Japanese (ja)
Other versions
JP2769339B2 (en
Inventor
Fukuhisa Matsuda
松田 福久
Kazuhiro Nakada
一博 中田
Tamotsu Ueno
保 上野
Ichizo Tsukuda
市三 佃
Shigetoshi Jogan
茂利 成願
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.)
Altemira Co Ltd
Original Assignee
Showa Aluminum Corp
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 Showa Aluminum Corp filed Critical Showa Aluminum Corp
Priority to JP63304519A priority Critical patent/JP2769339B2/en
Publication of JPH02149682A publication Critical patent/JPH02149682A/en
Application granted granted Critical
Publication of JP2769339B2 publication Critical patent/JP2769339B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Laser Beam Processing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

PURPOSE:To produce an Al alloy material having superior wear resistance and durability by locally melting the surface of an Al or Al alloy base material together with a boride or silicide to form a hard alloyed layer in the surface of the base material. CONSTITUTION:A shallow groove 2 is cut in the surface of an Al or Al alloy base material 1 and powder 3 of one or more kinds of borides such as TiB2 or one or more kinds of silicides such as Mg2Si is fed from the outside of the base material 1 and embedded in the groove 2. The surface of the base material 1 is locally melted together with the powder 3 by irradiation with laser beams 4. The molten part solidities in a short time, a hard alloyed layer 5 contg. the borides or silicides dispersed uniformly and densely in the Al matrix is formed and an Al alloy material having superior wear resistance is obtd. The alloyed layer 5 bonds to the base material 1 in one body, does not cause exfoliation at all and ensures satisfactory durability.

Description

【発明の詳細な説明】 産業上の利用分野 この発明は、自動車、事務機、一般機械等において、耐
摩耗性の要求される部品材料として使用される耐摩耗性
に優れたアルミニウム合金材の製造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application This invention relates to the production of aluminum alloy materials with excellent wear resistance, which are used as parts materials that require wear resistance in automobiles, office machines, general machinery, etc. Regarding the method.

従来の技術 周知のように、アルミニウムあるいはアルミニウム合金
は汎用されている鉄系材料等と比較して格段に軽量であ
るのに加え、熱伝導特性に優れ、また耐食性も優れると
ころから、最近では自動車等の各種機械部品として広く
使用されるようになっている。しかしながら、一般にア
ルミニウムあるいはアルミニウム合金は鉄系材料と比較
して耐摩耗性が劣り、このことが自動車等における軽量
化等を目的として鉄系部材をAρ合金部材に代える際の
大きな障害となっていた。
As is well known in the art, aluminum or aluminum alloys are much lighter than commonly used iron-based materials, have excellent thermal conductivity, and have excellent corrosion resistance, so they have recently been used in automobiles. It has come to be widely used as various machine parts such as. However, aluminum or aluminum alloys generally have inferior wear resistance compared to iron-based materials, and this has been a major obstacle when replacing iron-based parts with Aρ alloy parts for the purpose of reducing weight in automobiles, etc. .

そこで従来から、耐摩耗性が要求される部位に適用され
るアルミニウム合金材の耐摩耗性向上策として、メツキ
や陽極酸化処理、あるいは溶射等の表面処理を施して耐
摩耗性の高い表面処理層を形成する試みがなされている
が、いずれも耐摩耗性の要求に対しいまだ充分な満足を
与え得るものではなかった。しかも、いずれの場合も表
面処理層の基材に対する密着性が充分でないところから
、高面圧下で使用した場合に充分な耐久性を確保できな
いという欠点があった。
Therefore, as a measure to improve the wear resistance of aluminum alloy materials used in areas where wear resistance is required, surface treatments such as plating, anodizing, or thermal spraying have been applied to create a highly wear-resistant surface treatment layer. Attempts have been made to form a steel sheet, but none of them have yet been able to fully satisfy the requirements for wear resistance. Moreover, in both cases, the adhesion of the surface treatment layer to the base material is insufficient, resulting in the drawback that sufficient durability cannot be ensured when used under high surface pressure.

この発明は、このような技術的背景のもとでなされたも
のであって、優れた耐摩耗性を仔するとともに、高面圧
下で使用した場合にも充分な耐久性を有するアルミニウ
ム合金材料の製作提供を目的とするものである。
This invention was made against this technical background, and it is an aluminum alloy material that has excellent wear resistance and sufficient durability even when used under high surface pressure. The purpose is to produce and provide.

課題を解決するための手段 上記目的において、この発明は、アルミニウムまたはア
ルミニウム合金基材の表面を、基材外部から供給した1
種または2種以上の硼化物ないしは珪化物とともに局部
的に溶融することにより、Alマトリックスと前記硼化
物ないしは珪化物粒子を合金化せしめた硬質合金化層を
前記基材の表面に形成し、もって耐摩耗性の向上を図ら
んとするものである。
Means for Solving the Problems In order to achieve the above object, the present invention provides a surface of an aluminum or aluminum alloy base material that is supplied from the outside of the base material.
By locally melting the seed or two or more borides or silicides, a hard alloyed layer in which the Al matrix and the boride or silicide particles are alloyed is formed on the surface of the base material. The purpose is to improve wear resistance.

基材として用いるアルミニウムまたはアルミニウム合金
の組成は特に限定されるものではなく、JIS1000
番台の純アルミニウムの他、用途に応じて必要とされる
機械的性質、加工特性を有する各種のアルミニウム合金
を用いうる。
The composition of aluminum or aluminum alloy used as the base material is not particularly limited, and is based on JIS1000.
In addition to standard pure aluminum, various aluminum alloys can be used that have the required mechanical properties and processing characteristics depending on the application.

また基材の形状も、適用される部品の形状に応じて任意
に設計すれば良い。
Further, the shape of the base material may be arbitrarily designed depending on the shape of the part to which it is applied.

かかるアルミニウムまたはアルミニウム合金基材の表面
の溶融はレーザビーム、電子ビーム、TIGアーク等の
照射による高密度エネルギー源を用いた溶融手段によれ
ば良い。このような手段を用いることにより、基材表面
層のみを溶融しえて基材への熱影響を少なくでき、基材
の一部のみを局部的に合金化することができる。
The surface of the aluminum or aluminum alloy base material may be melted by a melting means using a high-density energy source such as laser beam, electron beam, TIG arc, or the like. By using such means, only the surface layer of the base material can be melted to reduce the thermal influence on the base material, and only a part of the base material can be locally alloyed.

−膜内にはレーザビームを用いる場合が多く、具体的に
はYAGレーザ(波長1.06μm。
- A laser beam is often used inside the film, specifically a YAG laser (wavelength: 1.06 μm).

パルス発振)とかCO2レーザ(波長10.6μm5連
続発振)を主に用いる。また、溶融は耐摩耗性の要求さ
れる部位について行えば良いが、その部位が広範囲にわ
たるときはレーザビーム等のオシレーション幅の調整や
、順次的照射により対処すれば良い。
Pulse oscillation) or CO2 laser (wavelength: 10.6 μm, 5 continuous oscillations) are mainly used. Further, melting may be carried out on a region where wear resistance is required, but when the region is spread over a wide range, it may be necessary to adjust the oscillation width of a laser beam or the like or sequentially irradiate the material.

基材表面の溶融は、基材外部から供給した硼化物ないし
は珪化物、即ち金属元素と硼素ないしは珪素との化合物
の溶融を伴いつつ行う。硼化物、珪化物の供給態様の1
つとしては、これを粉末にしてレーザビーム等の照射前
に予め所期する部位にコーティング層を形成しておく場
合を挙げうる。コーティング層の形成は湿式メツキ、C
VD、PVD、溶射法等により、あるいは粉末をエチル
アルコールなど各種バインダーを用いて塗布することに
より行いうる。また、他の供給態様として、粉末をレー
ザビーム等の照射中に溶融部に直接投入する場合を挙げ
うる。
The surface of the base material is melted while accompanying the melting of boride or silicide, that is, a compound of a metal element and boron or silicon, supplied from outside the base material. 1 of supply modes of boride and silicide
One example is the case where the powder is made into powder and a coating layer is formed in advance at a desired location before irradiation with a laser beam or the like. The coating layer is formed by wet plating, C
This can be done by VD, PVD, thermal spraying, etc., or by applying powder using various binders such as ethyl alcohol. In addition, as another supply mode, the powder may be directly introduced into the melting zone during irradiation with a laser beam or the like.

いずれの方法を用いても良いが、直接投入方式の場合、
供給速度の調整等が面倒であるため、簡便性の点でコー
ティング方式、特にバインダーを用いた粉末塗布法が優
れている。
Either method may be used, but in the case of the direct injection method,
Since it is troublesome to adjust the supply rate, etc., a coating method, especially a powder coating method using a binder, is superior in terms of simplicity.

上記のように、レーザビーム等の照射により基材表面を
硼化物ないしは珪化物と共に溶融した後においては、溶
融部分は短詩に凝固しAlマトリックスに硼化物ないし
は珪化物粒子が均一緻密に分散しあるいは塊状化した合
金化層となる。而して、硼化物や珪化物はそれ自体極め
て硬度が高いため、合金化層が全体として高い硬度を示
し、優れた耐摩耗性を具有する。かかる効果を生じさせ
る点で硼化物と珪化物とは相互に均等物であり、少なく
ともそれら化合物の1種を溶融すれば足りる。好ましい
硼化物の例としてはTiB2、ZrB2、NbB2、C
rB2、TaB2、NiB等を挙げうる。一方、好まし
い珪化物の例としてはMg2 S 1STiSi2、M
oSi2、NbSi2、CrSi2等を挙げつる。この
ように、硼化物ないしは珪化物は合金化層の硬度向上を
図るための必須構成要素であるが、単に硬度向上のため
てあれば、同じく高い硬度を有するWC,Tic等の炭
化物やTiN、ZrN等の窒化物を用いることも考えら
れる。しかしこの発明において硼化物ないしは珪化物を
用いるのは次の理由による。即ち、上記WCやTiN等
の粉末を基材とともに溶融しても、基材との濡れ性が悪
く良好な合金化層を形成することができないが、硼化物
ないしは珪化物を用いた場合には基材との濡れ性が良く
、表面が滑らかで極めて良好な合金化層の形成が可能と
なるからである。これは、硼化物中のBや珪化物中のS
iが基材Alとの濡れ性向上作用を果しているからと考
えられる。なお合金化層の厚さはレーザビーム等の照射
条件、例えば出力、照射速度、焦点位置等を変化させる
ことで数十μmから数mm程度にまで容易に制御できる
。
As mentioned above, after the surface of the base material is melted together with boride or silicide by irradiation with a laser beam or the like, the melted portion solidifies briefly, and the boride or silicide particles are uniformly and densely dispersed in the Al matrix. It becomes a lumpy alloyed layer. Since borides and silicides themselves have extremely high hardness, the alloyed layer as a whole exhibits high hardness and has excellent wear resistance. Borides and silicides are equivalent to each other in terms of producing this effect, and it is sufficient to melt at least one of these compounds. Examples of preferred borides include TiB2, ZrB2, NbB2, C
Examples include rB2, TaB2, NiB, and the like. On the other hand, examples of preferable silicides include Mg2 S 1STiSi2, M
Examples include oSi2, NbSi2, CrSi2, etc. As described above, borides or silicides are essential components for improving the hardness of the alloyed layer, but if they are simply used to improve the hardness, carbides such as WC and Tic, which also have high hardness, TiN, It is also possible to use a nitride such as ZrN. However, the reason why borides or silicides are used in this invention is as follows. That is, even if powders such as WC or TiN are melted together with a base material, they have poor wettability with the base material and cannot form a good alloyed layer, but when borides or silicides are used, This is because it has good wettability with the base material, has a smooth surface, and can form an extremely good alloyed layer. This is B in boride and S in silicide.
This is thought to be because i has an effect of improving wettability with the base material Al. The thickness of the alloyed layer can be easily controlled from several tens of μm to several mm by changing the irradiation conditions of the laser beam, such as output, irradiation speed, focal position, etc.

表面に硬質合金化層を形成した基材は、その後必要に応
じて最終製品形状に機械加工し、耐摩耗性部品として実
用に供する。
The base material with the hard alloyed layer formed on its surface is then machined into the final product shape as required, and put into practical use as a wear-resistant part.

発明の詳細 な説明したように、この発明は、アルミニウムまたはア
ルミニウム合金基材の表面を、基材外部から供給した1
種または2種以上の硼化物あるいは珪化物とともに局部
的に溶融することにより、へΩマトリックスと前記硼化
物ないしは珪化物粒子が合金化した硬質合金化層を基材
の表面に形成するするものであるから、本発明によって
製造したアルミニウム合金材は格段に耐摩耗性に優れた
ものとなり、従って自動車等に要請される耐摩耗部品と
して好適なものとなしうる。また、合金化層は従来のよ
うなメツキ等による表面処理層と異なり、基材と一体的
に結合しているから、高面圧下で使用した場合にも抜屑
の剥離等を起こす危険はなく、充分な耐久性を確保しう
るちのとなる。
DETAILED DESCRIPTION OF THE INVENTION As described above, the present invention provides the surface of an aluminum or aluminum alloy base material with a single layer supplied from outside of the base material.
By locally melting a seed or two or more borides or silicides, a hard alloyed layer in which the hemium matrix and the boride or silicide particles are alloyed is formed on the surface of the base material. Therefore, the aluminum alloy material produced according to the present invention has extremely excellent wear resistance, and can therefore be suitable as wear-resistant parts required for automobiles and the like. In addition, unlike conventional surface treatment layers such as plating, the alloyed layer is integrally bonded to the base material, so there is no risk of peeling of chips even when used under high surface pressure. , ensuring sufficient durability.

実施例 (実施例1) 第1図に示すように、工業用純Al(A1070)から
なる厚さ7.5MX幅40mmX長さ100#の試験片
を基材(1)として用いた。
Examples (Example 1) As shown in FIG. 1, a test piece made of industrially pure Al (A1070) and having a thickness of 7.5 MX, a width of 40 mm, and a length of 100# was used as the base material (1).

そしてこの試験片の中央部長手方向に、深さ0゜5#、
幅6順の浅溝(2)を掘り、抜溝に1〜10、czm径
のTiSi2粉末(3)をエチルアルコールをバインダ
ーとして埋込み状態に塗布した。塗布厚さは約0.5#
ll!であった。
Then, in the longitudinal direction of the center of this test piece, a depth of 0°5#,
Shallow grooves (2) with widths in order of 6 were dug, and TiSi2 powder (3) having a diameter of 1 to 10 czm was applied to the grooves in an embedded state using ethyl alcohol as a binder. Coating thickness is approximately 0.5#
ll! Met.

次に10kw級CO2レーザ加工機を用いて、前記試験
片の粉末塗布部分にレーザビーム(4)を照射し、Ti
Si2粉末とその直下の基材Alとを共に溶融した。照
射条件は、出力51(w。
Next, using a 10kw class CO2 laser processing machine, the powder coated part of the test piece was irradiated with a laser beam (4), and the Ti
The Si2 powder and the substrate Al immediately below it were melted together. The irradiation conditions were an output of 51 (w).

試片移動速度100rrrm/m i n、焦点位置+
30、ビームオシレーション5Hz、5mとした。
Specimen moving speed 100rrrm/min, focal position +
30, beam oscillation was 5 Hz, and 5 m.

レーザビームの照射による溶融後、凝固した試験片の組
織状態を調べたところ、溝部分の全体にわたって表面が
滑らかで欠陥のない厚さ約1.3rrmの合金化層(5
)が形成されていた。
After melting by laser beam irradiation, the microstructure of the solidified test piece was examined, and it was found that the alloyed layer (5 rrm) with a thickness of about 1.3 rrm had a smooth surface and no defects throughout the groove.
) was formed.

かつこの合金化層は、TiSi2が比較的均一緻密に分
散した部分と塊状になった部分とを有し、合金化層全体
の硬さはHv81〜824(荷重100g)であった。
Moreover, this alloyed layer had a portion where TiSi2 was relatively uniformly and densely dispersed and a portion where TiSi2 was in the form of a lump, and the hardness of the entire alloyed layer was Hv 81 to 824 (load: 100 g).

しかも、合金化層内及び合金化層と基材Al界面では割
れ及び気孔の発生は全く認められなかった。
Furthermore, no cracks or pores were observed within the alloyed layer or at the interface between the alloyed layer and the Al base material.

(実施例2) TiSi2粉末の代わりに、1〜5μm径のTiB2粉
末を用いた以外は実施例1と同一の条件で試験を行った
ところ、同様に表面が滑らかで欠陥のない厚さ約0. 
5#III+の合金化層が形成された。また合金化層の
硬度はHv250〜3200 (荷重50(1)であっ
た。
(Example 2) A test was conducted under the same conditions as in Example 1 except that TiB2 powder with a diameter of 1 to 5 μm was used instead of TiSi2 powder, and the surface was similarly smooth with no defects and a thickness of about 0. ..
A 5#III+ alloyed layer was formed. Moreover, the hardness of the alloyed layer was Hv250-3200 (load 50(1)).

(実施例3) TiSi2粉末に代えて、1〜5μm径のZrB2粉末
と1〜2μm径のMoSi2粉末との混合粉末を用いた
以外は実施例1と同一の条件で試験を行ったところ、厚
さ約0.5mmの合金化層が形成された。また合金化層
の硬度はH■150〜2800 (荷重500g)であ
った。
(Example 3) A test was conducted under the same conditions as in Example 1, except that a mixed powder of ZrB2 powder with a diameter of 1 to 5 μm and MoSi2 powder with a diameter of 1 to 2 μm was used instead of TiSi2 powder. An alloyed layer with a thickness of about 0.5 mm was formed. The hardness of the alloyed layer was H150-2800 (load 500 g).

(比較例1) TiB2粉末の代わりに、5〜10μm径のTiC粉末
を用いた以外は実施例1と同一の条件で試験を行ったと
ころ、表面に亀甲状の割れが認められ、一部が剥離して
おり、しかも合金化層直下に基材Aρのみの溶融域が存
在し、Alとの濡れ性が悪いことが認められた。
(Comparative Example 1) When a test was conducted under the same conditions as in Example 1 except that TiC powder with a diameter of 5 to 10 μm was used instead of TiB2 powder, tortoiseshell-shaped cracks were observed on the surface, and some parts It was found that there was peeling, and there was a melted region of only the base material Aρ directly below the alloyed layer, indicating poor wettability with Al.

(比較例2) 上記各実施例において基材として用いた1070アルミ
ニウム合金単体の硬度を調べたところ、1(v30 (
荷重5Ng)であった。
(Comparative Example 2) When the hardness of the 1070 aluminum alloy used as the base material in each of the above examples was investigated, it was found to be 1 (v30 (
The load was 5 Ng).

以上の試験結果かられかるように、本発明によれば、極
めて硬度が高く従って当然に耐摩耗性にも優れた合金化
層を基材表面に有するアルミニウム材料を製造しうるこ
とを確認しえた。
As can be seen from the above test results, it has been confirmed that according to the present invention, it is possible to produce an aluminum material having an alloyed layer on the surface of the base material that has extremely high hardness and therefore naturally has excellent wear resistance. .

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はこの発明の実施例における合金化の工程を模式
的に示す斜視図である。 (1)・・・基材、(3)・・・TiSi2粉末、(4
)・・・レーザビーム、(5)・・・合金化層。 以上 第1図
FIG. 1 is a perspective view schematically showing the alloying process in an embodiment of the present invention. (1)...Base material, (3)...TiSi2 powder, (4
)...Laser beam, (5)...Alloyed layer. Figure 1 above

Claims (1)

【特許請求の範囲】[Claims] アルミニウムまたはアルミニウム合金基材の表面を、基
材外部から供給した1種または2種以上の硼化物ないし
は珪化物とともに局部的に溶融し、もってAlマトリッ
クスと前記硼化物ないしは珪化物粒子が合金化した硬質
合金化層を基材の表面に形成することを特徴とする耐摩
耗性に優れたアルミニウム合金材の製造方法。
The surface of the aluminum or aluminum alloy base material is locally melted together with one or more borides or silicides supplied from outside the base material, thereby alloying the Al matrix and the boride or silicide particles. A method for producing an aluminum alloy material with excellent wear resistance, which comprises forming a hard alloyed layer on the surface of a base material.
JP63304519A 1988-11-30 1988-11-30 Manufacturing method of aluminum alloy material with excellent wear resistance Expired - Fee Related JP2769339B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63304519A JP2769339B2 (en) 1988-11-30 1988-11-30 Manufacturing method of aluminum alloy material with excellent wear resistance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63304519A JP2769339B2 (en) 1988-11-30 1988-11-30 Manufacturing method of aluminum alloy material with excellent wear resistance

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007169753A (en) * 2005-12-26 2007-07-05 Muneharu Kutsuna Laser peening treatment method and laser absorbing powder layer sheet
JP2007169754A (en) * 2005-12-26 2007-07-05 Muneharu Kutsuna Surface treatment method, laser absorbing powder layer sheet, and powder spray for laser peening
JP2009191733A (en) * 2008-02-14 2009-08-27 Toshiba Corp Steam turbine blade and surface reforming method thereof
CN110052615A (en) * 2018-08-10 2019-07-26 南方科技大学 Method for preparing high-strength aluminum alloy by selective laser melting
WO2021157683A1 (en) * 2020-02-06 2021-08-12 株式会社Uacj Aluminum alloy ingot and method for manufacturing same
JP2021123789A (en) * 2020-02-06 2021-08-30 株式会社Uacj Aluminium alloy ingot and method for manufacturing the same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6070136A (en) * 1983-09-14 1985-04-20 Honda Motor Co Ltd Surface treatment of work
JPS6254588A (en) * 1985-08-30 1987-03-10 Toyota Motor Corp Formation of composite aluminum alloy layer dispersed with ceramic particles
JPS63235087A (en) * 1987-03-20 1988-09-30 Toyota Central Res & Dev Lab Inc Overlay welding method
JPS63247379A (en) * 1987-04-03 1988-10-14 Furukawa Alum Co Ltd Composite aluminum and aluminum alloy
JPH02101177A (en) * 1988-10-05 1990-04-12 Toyota Motor Corp Wear-resistant al alloy member and its production

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6070136A (en) * 1983-09-14 1985-04-20 Honda Motor Co Ltd Surface treatment of work
JPS6254588A (en) * 1985-08-30 1987-03-10 Toyota Motor Corp Formation of composite aluminum alloy layer dispersed with ceramic particles
JPS63235087A (en) * 1987-03-20 1988-09-30 Toyota Central Res & Dev Lab Inc Overlay welding method
JPS63247379A (en) * 1987-04-03 1988-10-14 Furukawa Alum Co Ltd Composite aluminum and aluminum alloy
JPH02101177A (en) * 1988-10-05 1990-04-12 Toyota Motor Corp Wear-resistant al alloy member and its production

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007169753A (en) * 2005-12-26 2007-07-05 Muneharu Kutsuna Laser peening treatment method and laser absorbing powder layer sheet
JP2007169754A (en) * 2005-12-26 2007-07-05 Muneharu Kutsuna Surface treatment method, laser absorbing powder layer sheet, and powder spray for laser peening
JP2009191733A (en) * 2008-02-14 2009-08-27 Toshiba Corp Steam turbine blade and surface reforming method thereof
CN110052615A (en) * 2018-08-10 2019-07-26 南方科技大学 Method for preparing high-strength aluminum alloy by selective laser melting
WO2021157683A1 (en) * 2020-02-06 2021-08-12 株式会社Uacj Aluminum alloy ingot and method for manufacturing same
JP2021123789A (en) * 2020-02-06 2021-08-30 株式会社Uacj Aluminium alloy ingot and method for manufacturing the same
CN114761152A (en) * 2020-02-06 2022-07-15 株式会社Uacj Aluminum alloy ingot and method for producing same

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