JPS62250149A - Aluminum alloy for bicycle - Google Patents
Aluminum alloy for bicycleInfo
- Publication number
- JPS62250149A JPS62250149A JP9562786A JP9562786A JPS62250149A JP S62250149 A JPS62250149 A JP S62250149A JP 9562786 A JP9562786 A JP 9562786A JP 9562786 A JP9562786 A JP 9562786A JP S62250149 A JPS62250149 A JP S62250149A
- Authority
- JP
- Japan
- Prior art keywords
- aluminum alloy
- grain size
- strength
- stress corrosion
- corrosion cracking
- 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
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 19
- 239000012535 impurity Substances 0.000 claims abstract description 3
- 229910052782 aluminium Inorganic materials 0.000 claims abstract 2
- 239000013078 crystal Substances 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 238000005336 cracking Methods 0.000 abstract description 17
- 230000007797 corrosion Effects 0.000 abstract description 15
- 238000005260 corrosion Methods 0.000 abstract description 15
- 229910052796 boron Inorganic materials 0.000 abstract description 5
- 239000000463 material Substances 0.000 abstract description 5
- 229910052759 nickel Inorganic materials 0.000 abstract description 5
- 229910045601 alloy Inorganic materials 0.000 abstract description 4
- 239000000956 alloy Substances 0.000 abstract description 4
- 229910052804 chromium Inorganic materials 0.000 abstract description 4
- 229910052749 magnesium Inorganic materials 0.000 abstract description 4
- 238000003466 welding Methods 0.000 abstract description 4
- 229910052802 copper Inorganic materials 0.000 abstract description 3
- 229910052748 manganese Inorganic materials 0.000 abstract description 3
- 229910052710 silicon Inorganic materials 0.000 abstract description 3
- 229910052709 silver Inorganic materials 0.000 abstract description 3
- 229910052719 titanium Inorganic materials 0.000 abstract description 3
- 229910052725 zinc Inorganic materials 0.000 abstract description 3
- 229910052726 zirconium Inorganic materials 0.000 abstract description 3
- 239000000203 mixture Substances 0.000 abstract 2
- 230000001105 regulatory effect Effects 0.000 abstract 1
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 4
- 229910018571 Al—Zn—Mg Inorganic materials 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000007864 aqueous solution Substances 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 210000000078 claw Anatomy 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 239000011780 sodium chloride Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
- 238000010273 cold forging Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 229910001651 emery Inorganic materials 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
Landscapes
- Nonmetallic Welding Materials (AREA)
Abstract
Description
【発明の詳細な説明】
ｒ 産’Ｂ ｌ−ノミｆ口１１ ／、＞ ’Ｌ！） １
本発明は自転車用アルミニウム合金に関し、さらに詳し
くは、耐応力腐蝕割れ性が良好で、かつ、強度の優れた
自転車用アルミニウム合金に関する。[Detailed description of the invention] r production'B l-flea f mouth 11 /, >'L! ) 1
The present invention relates to an aluminum alloy for bicycles, and more particularly to an aluminum alloy for bicycles that has good stress corrosion cracking resistance and excellent strength.
［従来技術］
近年における自転車は軽量化が要求されてきており、そ
のためアルミニウム合金製のフレームが製作されている
。[Prior Art] Bicycles in recent years have been required to be lightweight, and therefore frames made of aluminum alloy have been manufactured.
このフレームには高荷重が負荷されるので、高強度であ
って、かつ、溶接構造であるため溶接性の良いアルミニ
ウム合金が要求されている。そのため、アルミニウム合
金を使用ずろ場合には、Ａｌ−７，ｎ−Ｍｇ系合金が使
用されるが、この種の高力アルミニウム合金は、高強度
になるに従って応力腐蝕割れが発生し易くなるので、上
記Ａｌ−Ｚｎ−Ｍｇ系合金をフレームとして使用する際
に、ｔ、？酷な使用条件では応力腐蝕割れが生じるとい
う問題がある。Since this frame is subjected to a high load, it is required to be made of an aluminum alloy that has high strength and has good weldability because it has a welded structure. Therefore, if an aluminum alloy is not used, an Al-7, n-Mg alloy is used, but as this type of high-strength aluminum alloy becomes higher in strength, stress corrosion cracking becomes more likely to occur. When using the above Al-Zn-Mg alloy as a frame, t,? There is a problem that stress corrosion cracking occurs under severe usage conditions.
また、フレームには耐久性か要求されるので疲労強度の
高いアルミニウム合金が必要であり、Ａｌ−Ｚｎ−Ｍｇ
系合金は比較的高い疲労強度を有するが、溶接を行なっ
た場合に溶接部の疲労強度が低くなるという問題がある
。In addition, since durability is required for the frame, an aluminum alloy with high fatigue strength is required, and Al-Zn-Mg
Although these alloys have relatively high fatigue strength, there is a problem in that when welding is performed, the fatigue strength of the welded part becomes low.
［発明が解決しようとずろ問題点］
本発明は上記に説明したように、従来における自転車用
アルミニウム合金の種々の問題点に鑑みなされた乙ので
あり、本発明者が鋭意研究を行ない、検討を重ねた結果
、結晶粒径が微細であり、溶接部の耐応力腐蝕割れ性が
良好であり、さらに、疲労強度の高い自転車用アルミニ
ウム合金を開発 。[Problems to be Solved by the Invention] As explained above, the present invention was made in view of the various problems of conventional aluminum alloys for bicycles, and the present inventor has conducted extensive research and studies. As a result of repeated efforts, we developed an aluminum alloy for bicycles that has fine grain size, good resistance to stress corrosion cracking in welded parts, and high fatigue strength.
したのである。That's what I did.
［問題点を解決するための手段］
本発明に係る自転車用アルミニウム合金の特徴とすると
ころは、
Ｚｎ ３．０〜８．０ｗｔ％、Ｍｇ ０．３〜３．ｈｔ
％、’ｒ ｉ ０．００５〜０．２０ｗｔ％、Ｂ ０．
００５〜０．０５ｗｔ％、Ｃｕ ０．０３〜０．５ｗｔ
％、Ｍｎ ０．０５〜０．４０ｗｔ％を含有し、および
、
Ａｇ ０．０３〜０．５ｗｔ％、Ｎ ｉ ０．０３〜０
．５ｗｔ％、Ｓ ｉ Ｑ、２〜０．７ｗｔ％
のうちから選んだ１種
を含イｆし、さらに、
Ｃｒ ０．０５〜０．４０ｗＬ％、Ｚ ｒ ０．０５〜
０．２５ｗＬ％の２種
を含有し、残部Ａ１および不可避不純物からなり、かつ
、鋳造組織における結晶粒径を１５００μｍ以下とした
ことことにある。[Means for Solving the Problems] The aluminum alloy for bicycles according to the present invention is characterized by: Zn: 3.0 to 8.0 wt%, Mg: 0.3 to 3.0 wt%. ht
%, 'r i 0.005-0.20wt%, B 0.
005-0.05wt%, Cu 0.03-0.5wt
%, Mn 0.05-0.40 wt%, and Ag 0.03-0.5 wt%, Ni 0.03-0
．． 5 wt%, S i Q, 2 to 0.7 wt%, and further contains Cr 0.05 to 0.40 wL%, Z r 0.05 to
It contains 0.25wL% of two types, the remainder consists of A1 and unavoidable impurities, and the crystal grain size in the cast structure is 1500 μm or less.
本発明に係る自転車用アルミニウム合金について、以下
詳細に説明する。The aluminum alloy for bicycles according to the present invention will be explained in detail below.
先ず、本発明に係る自転車用アルミニウム合金の含有成
分および成分割合について説明する。First, the components and component ratios of the aluminum alloy for bicycles according to the present invention will be explained.
Ｚｎは強度を向上させるために最も重要な元素であり、
含有量が３．Ｏｖｔ％未満では充分な強度を得ることが
できず、また、８．０ｗ１％を越えて含有されると応力
腐蝕割れが発生し易くなる。よって、Ｚｎ含有量は３．
０〜８．０ｗｔ％とする。Zn is the most important element for improving strength,
The content is 3. If the content is less than Ovt%, sufficient strength cannot be obtained, and if the content exceeds 8.0w1%, stress corrosion cracking is likely to occur. Therefore, the Zn content is 3.
0 to 8.0 wt%.
ＭｇはＺｎと同様に強度向上に対して重要な元素であり
、含有量が０．３ｗｔ％未満では充分な強度が得られず
、また、３．０ｗｔ％を越えて含有されろと応力腐蝕割
れが発生し易くなる。Like Zn, Mg is an important element for improving strength; if the content is less than 0.3 wt%, sufficient strength cannot be obtained, and if the content exceeds 3.0 wt%, stress corrosion cracking may occur. is more likely to occur.
ＴｉおよびＢは鋳塊の組織微細化のために重要な元素で
あり、Ｔｉ含有量が０．００５ｗｔ％未満およびＢ含有
量が０．００５ｗｔ％未満では結晶粒微細化に効果が少
なく、また、Ｔｉ ０．２０ｗｔ％、Ｂ ０．０５ｗＬ
％を夫々越えて含有されると巨大化合物が生成する可能
性がある。よって、Ｔｉ含有量は０．００５〜０．２（
ｍ％、Ｂ Ｑ、ＱＱ５〜０．０５ｗｔ％とする。Ti and B are important elements for refining the structure of an ingot, and if the Ti content is less than 0.005 wt% and the B content is less than 0.005 wt%, there is little effect on grain refining. Ti 0.20wt%, B 0.05wL
If the content exceeds 5% of each, there is a possibility that a giant compound will be formed. Therefore, the Ti content is 0.005 to 0.2 (
m%, BQ, QQ5 to 0.05wt%.
Ｃｕは耐応力腐蝕割れ性を著しく向上させる元素であり
、含有量が０．０３ｗｔ％未満ではこの効果は少な（、
また、０．５ｗｔ％を越えて含有されると溶接性が劣化
する。よって、Ｃｕ含有量は０．０３〜０．５ｗｔ％と
する。Cu is an element that significantly improves stress corrosion cracking resistance, and if the content is less than 0.03 wt%, this effect is small (,
Moreover, if the content exceeds 0.5 wt%, weldability deteriorates. Therefore, the Cu content is set to 0.03 to 0.5 wt%.
Ｍｎは組織改善のために必要な元素であり、含有量が０
．０５ｗｔ％未満ではこの効果は少なく、また、０．０
４０ｗ１％を越えて含有されると巨大化合物が生成する
ようになる。よって、Ｍｎ含有量は０．０５〜０．４ｈ
ｔ％とする。Mn is an element necessary for improving the structure, and the content is 0.
．． If it is less than 0.05 wt%, this effect is small, and if it is less than 0.0
If the content exceeds 40w1%, giant compounds will be generated. Therefore, the Mn content is 0.05-0.4h
It is assumed to be t%.
八ｇ１Ｎｔｓ Ｓｓはこのうちから選んだ１種を含有さ
せること（こより耐応力腐蝕割れ性を向上させることが
でき、含有ａｈ＜Ａｇ ０．０３ｗｔ％未満、Ｎ１Ｏ−
０３ｖｔ％−ｒ週−Ｓｉ ０−２ｗｔ％央溝では耐応力
腐蝕割れ性を向上させる効果は少なく、また、Ａｇ０９
５ｗｔ％、Ｎｉ ０．５ｗＬ％、Ｓｉ０．７ｗｔ％を夫
々越えて含有されると溶接性が劣化する。よって、Ａｇ
０．０３〜０．５ｗｔ％、Ｎ ｉ ０．０３〜０．５ｗ
ｔ％、Ｓｉ０．３〜０．７ｗｔ％とする。8g1Nts Ss should contain one selected from these (this can improve stress corrosion cracking resistance, content ah<Ag less than 0.03wt%, N1O-
03vt%-r week-Si 0-2wt% center groove has little effect on improving stress corrosion cracking resistance, and Ag09
If the content exceeds 5 wt%, Ni 0.5 wL%, and Si 0.7 wt%, weldability deteriorates. Therefore, Ag
0.03-0.5wt%, Ni 0.03-0.5w
t% and Si0.3 to 0.7wt%.
Ｃｒ５Ｚｒは組織を改善するために必要な元素で、均質
化、熱間加工の組合せによって結晶粒を微細にするもの
であり、含有量がＣｒ Ｑ、０５ｗｔ５未満、Ｚｒ ０
．０５ｗｔ％未満ではこの効果は少なく、また、Ｃｒ
０．４０ｗｔ％、Ｚｒ ０．２５ｗｔ％を夫々越えて含
有されると巨大化合物が生成する可能性がある。よって
、Ｃ「含有量は０．０５〜０．４ｈＬ％、Ｚｒ含￥Ｔｆ
ｆｉは０．０５〜０．２５ｗｔ％とする。Cr5Zr is an element necessary to improve the structure, and is used to make crystal grains fine by a combination of homogenization and hot working.
．． This effect is small at less than 0.05 wt%, and Cr
If the content exceeds 0.40 wt% and 0.25 wt% of Zr, a giant compound may be formed. Therefore, the C content is 0.05 to 0.4 hL%, Zr-containing \Tf
fi is 0.05 to 0.25 wt%.
また、鋳造組織における結晶粒径が１５００μｍを越え
る大きさでは製品の粒径が肥大化して溶接性を劣化させ
る。よって、鋳造組織における結晶粒径は１５００μｍ
以下とする。Furthermore, if the crystal grain size in the cast structure exceeds 1500 μm, the grain size of the product becomes enlarged and weldability deteriorates. Therefore, the crystal grain size in the cast structure is 1500 μm.
The following shall apply.
［実 施 例］
次に、本発明に係る自転車用アルミニウム合金について
実施例を説明する。[Example] Next, an example of the aluminum alloy for bicycles according to the present invention will be described.
実施例
第１表に示す食台成分、成分割合のＡｌ−Ｚｎ−Ｍｇ系
合金を通常の方法により溶製し鋳造した鋳塊を、４００
〜４５０℃の温度で押出し、直径３５ｍｍ肉厚４ｍｍの
管および直径１５ｍｍの棒を製作した。EXAMPLE An ingot produced by melting and casting an Al-Zn-Mg alloy having the table components and component ratios shown in Table 1 in a conventional manner was
Extrusion was carried out at a temperature of ~450°C to produce tubes with a diameter of 35 mm and a wall thickness of 4 mm and rods with a diameter of 15 mm.
これらの押出し管を、冷間抽伸、およびテーパー加工を
行なって、ホークステムおよびホーク足等のフレーム部
品を製作した。These extruded tubes were subjected to cold drawing and taper processing to produce frame parts such as a hawk stem and hawk legs.
また、これらの押出し棒を、冷間鍛造によりホーク爪を
製作した。Furthermore, hawk claws were produced from these extruded rods by cold forging.
このようにして製作されたホークスヂム、ホーク足、ホ
ーク爪を、４５０℃の温度で３０分間の溶体化処理を行
なった後、水冷し、１２０℃の温度において２４時間の
時効を行なった。The thus produced hawk limbs, hawk feet, and hawk claws were subjected to solution treatment at a temperature of 450°C for 30 minutes, then cooled with water, and aged at a temperature of 120°C for 24 hours.
これらの部品を溶接により前ホークを製作した。The front hawk was made by welding these parts together.
第２表に前ホークの性能を示しである。Table 2 shows the performance of the previous Hawk.
・結晶粒径は管材の長手方向に平行な断面を金属顕微鏡
により観察した。・Crystal grain size was determined by observing a cross section parallel to the longitudinal direction of the tube material using a metallurgical microscope.
・耐応力腐蝕割れ性はＣ−Ｒｉｎｇ試験片を用いて長さ
方向に応力を負荷し、１００℃の３ｇ／ｌＮａＣｌ
３０ｆ’！／ｌ Ｋ、Ｃｒ：＋Ｏｔ ３ （３ｇ／Ｉ
Ｃｒｙｓ混合水溶液に浸漬した。記号○ｔはｔ分浸漬
ににって乙割れか発生しないことを示す。・Stress corrosion cracking resistance was measured by applying stress in the longitudinal direction using a C-Ring test piece and applying 3 g/l NaCl at 100°C.
30f'! /l K, Cr: +Ot 3 (3g/I
It was immersed in a Crys mixed aqueous solution. The symbol ○t indicates that no cracking occurs after immersion for t minutes.
・溶接部の耐応力腐蝕割れ性は第１図に示すように、ビ
ン５を有ずろ支持金具３に溶接ビード２がある板材ｌを
支持する３点指示法で、１５Ｋｇ／ｍｍ２の応力を加え
た試験を１００°Ｃの、３ｇ／ｌＮａＣｌ ３６ｇ／
ｌＣｒＯ３ａｏｇ／１Ｋ２ｃｒ３０□の混合水溶液に浸
漬して割れを観察した。試料の厚さは２ｍｍとし、溶加
材は５３５６を使用し、電流は１２０Ａとした。４は割
れを示す。・As shown in Figure 1, the stress corrosion cracking resistance of the welded part is determined by applying a stress of 15 kg/mm2 using the 3-point pointing method in which a plate 1 with a weld bead 2 is supported on a pin 5 with a dowel support 3. The test was carried out at 100°C with 3g/l NaCl 36g/l
It was immersed in a mixed aqueous solution of lCrO3aog/1K2cr30□ and cracks were observed. The thickness of the sample was 2 mm, 5356 was used as the filler metal, and the current was 120 A. 4 indicates cracking.
・溶接材の疲労強度は通常のシェンク式平面曲げ疲労試
験で１０７回の疲労強度を求めた。試験片の１！１さは
２ｍｍとし、溶接部の余盛りは除去し、表面は＃！００
耐水エメリーペーパーにより仕上げを行なった。・The fatigue strength of the welded material was determined using a normal Schenk plane bending fatigue test 107 times. The 1:1 height of the test piece was 2 mm, the excess of the weld was removed, and the surface was #! 00
Finishing was done with water-resistant emery paper.
・振動強度は第２図に示すように、フロントフォーク１
１と鉄製フレーム体１５とを組合せた自転車車体を固定
台１７と振動台１６とに取り付け、第３表に示す試験条
件により垂直な上下振動を与えた時の、アルミニウム合
金製フロントフォークの各部に破損、著しい変形、また
は、ゆがみの発生を目視により調査した。１２．１３．
１４は荷重点、１８は振幅、１９は中点である。・Vibration strength is as shown in Figure 2, front fork 1
1 and a steel frame body 15 was attached to a fixed table 17 and a vibration table 16, and vertical vibration was applied to each part of the aluminum alloy front fork under the test conditions shown in Table 3. The occurrence of damage, significant deformation, or distortion was visually inspected. 12.13.
14 is a load point, 18 is an amplitude, and 19 is a midpoint.
第２表に振動強度を示すが、ＯはｌＯ万万態以上振動回
数でも破損、著しい変形または、ゆがみの発生がないこ
とを表わす。なお、フレームには鉄製ダイヤモンド形を
採用した。Table 2 shows the vibration strength, and O indicates that no damage, significant deformation, or distortion occurs even when the number of vibrations is 10 or more. The frame is made of iron and has a diamond shape.
［発明の効果］
以上説明したように、本発明に係る自転車用アルミニウ
ム合金は上記の構成であるから、結晶粒径は微細であり
、溶接部の耐応力腐蝕割れ性に優れ、溶接材の疲労強度
が高く、さらに、振動強度に潰れているという効果を有
するものである。[Effects of the Invention] As explained above, since the aluminum alloy for bicycles according to the present invention has the above-mentioned structure, the crystal grain size is fine, the stress corrosion cracking resistance of the welded part is excellent, and the fatigue of the welded material is reduced. It has the effect of being high in strength and being crushed by vibration strength.
第１図は溶接部の応力腐蝕割れ性の試験機の断面図、第
２図は振動強度の試験方法の説明図である。
■・・板材、２・・溶接ビード、３・・支持金具、４・
・割れ、５・・ピン、ＩＩフロントフォーク（供試材）
、１２．１３．１４・・荷重点、１５・・鉄製フレーム
、１６・・振動台、Ｉ７・・固定台、１８・・振幅、Ｉ
９・・中点。
１ｍ
第２閲FIG. 1 is a sectional view of a tester for stress corrosion cracking of welded parts, and FIG. 2 is an explanatory diagram of a vibration strength test method. ■... Plate material, 2... Welding bead, 3... Support metal fittings, 4...
・Crack, 5...Pin, II front fork (sample material)
, 12.13.14... Load point, 15... Steel frame, 16... Vibration table, I7... Fixed table, 18... Amplitude, I
9...Middle point. 1m 2nd inspection
Claims (1)
、Ｔｉ０．００５〜０．２０ｗｔ％、Ｂ０．００５〜０
．０５ｗｔ％、Ｃｕ０．０３〜０．５ｗｔ％、Ｍｎ０．
０５〜０．４０ｗｔ％を含有し、および、 Ａｇ０．０３〜０．５ｗｔ％、Ｎｉ０．０３〜０．５ｗ
ｔ％、Ｓｉ０．２〜０．７ｗｔ％ のうちから選んだ１種 を含有し、さらに、 Ｃｒ０．０５〜０．４０ｗｔ％、Ｚｒ０．０５〜０．２
５ｗｔ％の２種 を含有し、残部Ａｌおよび不可避不純物からなり、かつ
、鋳造組織における結晶粒径を１５００μｍ以下とした
ことを特徴とする自転車用アルミニウム合金。[Claims] Zn3.0-8.0wt%, Mg0.3-3.0wt%
, Ti0.005~0.20wt%, B0.005~0
．． 05wt%, Cu0.03-0.5wt%, Mn0.
0.05 to 0.40 wt%, and 0.03 to 0.5 wt% of Ag, 0.03 to 0.5 w of Ni.
t%, Si0.2-0.7wt%, and further contains Cr0.05-0.40wt%, Zr0.05-0.2
1. An aluminum alloy for bicycles, characterized in that it contains 5 wt% of two kinds of aluminum, the remainder being Al and unavoidable impurities, and having a crystal grain size of 1500 μm or less in a cast structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9562786A JPS62250149A (en) | 1986-04-24 | 1986-04-24 | Aluminum alloy for bicycle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9562786A JPS62250149A (en) | 1986-04-24 | 1986-04-24 | Aluminum alloy for bicycle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62250149A true JPS62250149A (en) | 1987-10-31 |
Family
ID=14142759
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9562786A Pending JPS62250149A (en) | 1986-04-24 | 1986-04-24 | Aluminum alloy for bicycle |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62250149A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03122247A (en) * | 1989-10-06 | 1991-05-24 | Furukawa Alum Co Ltd | High strength aluminum alloy for welding excellent in stress corrosion cracking resistance |
| WO2005106057A3 (en) * | 2004-04-22 | 2006-01-26 | Alcoa Inc | Heat treatable al-zn-mg alloy for aerospace and automotive castings |
| WO2005106058A3 (en) * | 2004-04-22 | 2006-09-14 | Alcoa Inc | Heat treatable al-zn-mg-cu alloy for aerospace and automotive castings |
| WO2006127811A3 (en) * | 2005-05-25 | 2007-03-01 | Howmet Corp | An al-zn-mg-ag high-strength alloy for aerospace and automotive castings |
| CN102319884A (en) * | 2011-10-10 | 2012-01-18 | 东北轻合金有限责任公司 | Method for preparing solderable flat aluminum alloy ingots |
| US8157932B2 (en) | 2005-05-25 | 2012-04-17 | Alcoa Inc. | Al-Zn-Mg-Cu-Sc high strength alloy for aerospace and automotive castings |
| US9353430B2 (en) | 2005-10-28 | 2016-05-31 | Shipston Aluminum Technologies (Michigan), Inc. | Lightweight, crash-sensitive automotive component |
| CN109355538A (en) * | 2018-12-05 | 2019-02-19 | 辽宁忠旺集团有限公司 | A kind of high-strength 7 line aluminium alloy tubing production technology |
| EP3239313A3 (en) * | 2016-04-04 | 2019-08-14 | Korea Automotive Technology Institute | Wrought aluminum alloy |
-
1986
- 1986-04-24 JP JP9562786A patent/JPS62250149A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03122247A (en) * | 1989-10-06 | 1991-05-24 | Furukawa Alum Co Ltd | High strength aluminum alloy for welding excellent in stress corrosion cracking resistance |
| WO2005106057A3 (en) * | 2004-04-22 | 2006-01-26 | Alcoa Inc | Heat treatable al-zn-mg alloy for aerospace and automotive castings |
| WO2005106058A3 (en) * | 2004-04-22 | 2006-09-14 | Alcoa Inc | Heat treatable al-zn-mg-cu alloy for aerospace and automotive castings |
| WO2006127811A3 (en) * | 2005-05-25 | 2007-03-01 | Howmet Corp | An al-zn-mg-ag high-strength alloy for aerospace and automotive castings |
| US8157932B2 (en) | 2005-05-25 | 2012-04-17 | Alcoa Inc. | Al-Zn-Mg-Cu-Sc high strength alloy for aerospace and automotive castings |
| US9353430B2 (en) | 2005-10-28 | 2016-05-31 | Shipston Aluminum Technologies (Michigan), Inc. | Lightweight, crash-sensitive automotive component |
| CN102319884A (en) * | 2011-10-10 | 2012-01-18 | 东北轻合金有限责任公司 | Method for preparing solderable flat aluminum alloy ingots |
| EP3239313A3 (en) * | 2016-04-04 | 2019-08-14 | Korea Automotive Technology Institute | Wrought aluminum alloy |
| EP3680356A1 (en) * | 2016-04-04 | 2020-07-15 | Korea Automotive Technology Institute | Wrought aluminum alloy |
| CN109355538A (en) * | 2018-12-05 | 2019-02-19 | 辽宁忠旺集团有限公司 | A kind of high-strength 7 line aluminium alloy tubing production technology |
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