JPS62214151A - Aluminum alloy having superior strength at high temperature - Google Patents

Aluminum alloy having superior strength at high temperature

Info

Publication number
JPS62214151A
JPS62214151A JP5645286A JP5645286A JPS62214151A JP S62214151 A JPS62214151 A JP S62214151A JP 5645286 A JP5645286 A JP 5645286A JP 5645286 A JP5645286 A JP 5645286A JP S62214151 A JPS62214151 A JP S62214151A
Authority
JP
Japan
Prior art keywords
strength
aluminum alloy
temperature
alloy
high temperature
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
Application number
JP5645286A
Other languages
Japanese (ja)
Inventor
Kazuhiko Asano
浅野 和彦
Osamu Takezoe
竹添 修
Yoshinori Yasuda
安田 善則
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel 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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP5645286A priority Critical patent/JPS62214151A/en
Publication of JPS62214151A publication Critical patent/JPS62214151A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To improve the strength of an Al-Cu-Mg-Zr alloy at high temp. by adding a small amount of Mn or V to the alloy. CONSTITUTION:The composition of an Al alloy is composed of 4.0-7.0% C, 0.3-1.0% Mg, 0.05-0.2% Zr, 0.2-0.7% Mn and/or 0.05-0.2% V and the balance Al with inevitable impurities. The alloy has superior strength, e.g., tensile strength in the wide temp. range of room temp. - about 250 deg.C.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は高温強度に優れたアルミニウム合金に関する。[Detailed description of the invention] [Industrial application field] The present invention relates to an aluminum alloy with excellent high-temperature strength.

[従来技術] エンジン、コンプレッサーにおいては軽量性の点から、
真空機器においてはガス吸着が少ないという点から、ア
ルミニウム合金が使用される。これらの部材は100〜
250℃の温度環境下で使用されるため、室温のみなら
ず高温において強度の高いことが要求される。
[Prior art] For engines and compressors, from the viewpoint of lightweight,
Aluminum alloys are used in vacuum equipment because of their low gas adsorption. These parts are 100~
Since it is used in a temperature environment of 250°C, it is required to have high strength not only at room temperature but also at high temperatures.

アルミニウム合金の中で高温強度の高い合金としては2
618と2219があげられる。
2 as an alloy with high high temperature strength among aluminum alloys
618 and 2219 are listed.

[発明が解決しようとする問題点] しかし、上記アルミニウム合金には以下の欠点がある。[Problem that the invention attempts to solve] However, the above aluminum alloy has the following drawbacks.

2618の強度は150℃から200℃までの温度域で
は高いがそれ以上及び150℃以下の温度域では低い。
The strength of 2618 is high in the temperature range from 150°C to 200°C, but low in the temperature range above and below 150°C.

一方、2219の強度は、250℃以上の温度域では高
いがそれ以下の温度域では低い。
On the other hand, the strength of 2219 is high in the temperature range above 250°C, but low in the temperature range below.

従って、室温から250℃までの広範囲の温度領域で強
度の優れるアルミニウム合金はなかった。
Therefore, there has been no aluminum alloy that has excellent strength over a wide temperature range from room temperature to 250°C.

部材に対する薄肉化要求も高まる近年、従来材より高温
強度の高いアルミニウム合金が望まれている。
In recent years, as demands for thinner parts have increased, aluminum alloys with higher high-temperature strength than conventional materials are desired.

[問題点を解決するための手段] 本発明は従来の耐熱アルミニウム合金2618や221
9より高温強度に優れるアルミニウム合金を提供する。
[Means for Solving the Problems] The present invention is based on the conventional heat-resistant aluminum alloys 2618 and 221.
To provide an aluminum alloy having superior high-temperature strength than No. 9.

すなわち、室温から250℃の広に温度領域において従
来のアルミニウム合金より強度の高いアルミニウム合金
を提供するものである。
That is, the present invention provides an aluminum alloy that has higher strength than conventional aluminum alloys in a wide temperature range from room temperature to 250°C.

つまり1本発明は、Cu:4.0〜7.0%、Mg:0
.3〜1.0%、Zr:0.05〜0.2%を含有し、
かつ、M n : 0 、2〜0 、7%、V:0.0
5〜0.2%の1種又は2種以上を含有し、残部An及
び不可避的不純物からなることを特徴とする高温強度に
優れたアルミニウム合金である。
In other words, 1 the present invention has Cu: 4.0 to 7.0%, Mg: 0
.. Contains 3 to 1.0%, Zr: 0.05 to 0.2%,
And Mn: 0, 2-0, 7%, V: 0.0
It is an aluminum alloy with excellent high-temperature strength, characterized by containing 5 to 0.2% of one or more kinds, and the remainder being An and unavoidable impurities.

以下に成分を限定した理由を説明する。The reason for limiting the ingredients will be explained below.

Cu : Cuは高温強度を維持させるため必要不可欠な元素であ
る。そのためには4.0%以上を必要とする。Cuは固
溶強化、析出強化の両面から強度維持に寄与するが、同
様のはたらきをするMgに比べ高温強度の向上に対する
寄与率が高い。7%を超えるとCu A 、Q4  の
晶出物が発生するため、押出性、鍛造性等の加工性が低
下するとともに強度も低下する。
Cu: Cu is an essential element for maintaining high-temperature strength. For that purpose, 4.0% or more is required. Cu contributes to maintaining strength from both solid solution strengthening and precipitation strengthening, but has a higher contribution rate to improving high temperature strength than Mg, which has a similar function. When it exceeds 7%, crystallized products of Cu A and Q4 are generated, resulting in deterioration of workability such as extrudability and forgeability, as well as deterioration of strength.

よってCu量は4.0〜7.0%とする。なお、強度加
工性両面から最も望ましい範囲は5〜6%である。
Therefore, the amount of Cu is set to 4.0 to 7.0%. In addition, the most desirable range from both strength and workability is 5 to 6%.

Mgは強度、特に室温から200℃の温度範囲での強度
を向上させる添加元素である。0.2%未満ではその効
果はない、1.0%を超える添加はCuの固溶量を低下
させるために強度向上への効果がなくなる。又加工性を
低下させる。
Mg is an additive element that improves strength, particularly in the temperature range from room temperature to 200°C. If it is less than 0.2%, there is no effect, and if it is more than 1.0%, the effect on improving strength is lost because the amount of solid solution of Cu is reduced. It also reduces workability.

よって、Mgは0.2〜1.0%の範囲が適切である。Therefore, the appropriate range for Mg is 0.2 to 1.0%.

もっとも望ましい範囲は0.4〜0.7%である。The most desirable range is 0.4 to 0.7%.

Zrは押出、鍛造等の加工後の組織を繊維状組織にする
ことによって強度を向上させる。
Zr improves strength by making the structure after processing such as extrusion or forging into a fibrous structure.

0.05%未満ではその効果はなく、0.2%でその効
果は飽和する。よって0.05〜0.2%の範囲とする
There is no effect at less than 0.05%, and the effect is saturated at 0.2%. Therefore, it is set in the range of 0.05 to 0.2%.

Mnはその一部がアルミニウム合金中に固溶することに
よって他の一部はZrと同様繊維状組織を生み出す効果
によって強度を高める。0.2%未満では強度向上に寄
与しない、0.7%を超えると巨大晶出物を発生させ1
強度、・特に疲労強度に悪影響をもたらす、又、Mn量
が大き程押出性は低下する。したがって、Mn量は0.
2〜0.7%とする。
A part of Mn is solid-solved in the aluminum alloy, and the other part increases the strength by creating a fibrous structure similar to Zr. If it is less than 0.2%, it will not contribute to improving the strength, and if it exceeds 0.7%, it will generate giant crystallized substances.
It has an adverse effect on strength, especially fatigue strength, and the larger the Mn content, the lower the extrudability. Therefore, the amount of Mn is 0.
2 to 0.7%.

■は、Zrと同様、押出、鍛造性等の加工後の組織を繊
維状組織にすることによって強度を向上させる。0.0
5%未満ではその効果はなく、0.2%でその効果は飽
和する。よって0.05〜0.2%の範囲とする。
Similarly to Zr, (2) improves strength by making the structure after processing such as extrusion and forging into a fibrous structure. 0.0
There is no effect at less than 5%, and the effect is saturated at 0.2%. Therefore, it is set in the range of 0.05 to 0.2%.

M n 、 Vはその1種以上を含有する。なお、Vo
、08〜0.11%の場合、Mn量は0.2〜0.4%
が適切である。また、■を含有しない場合、Mn量を0
.5〜0.7%にすることによって、V:0.08〜o
、tt%、Mn:0.2〜0.4%の場合とほぼ同様な
強度が得られる。
M n and V contain one or more of them. In addition, Vo
, 08-0.11%, the Mn amount is 0.2-0.4%
is appropriate. In addition, if it does not contain ■, the amount of Mn is 0.
.. By setting it to 5 to 0.7%, V: 0.08 to o
, tt%, and Mn: almost the same strength as in the case of 0.2 to 0.4%.

なお、上記成分以外に鋳塊組織を微細化し、機械的性質
を安定化させるためにTiO,OO1〜0.05%を含
有させてもよい。
In addition to the above components, 1 to 0.05% of TiO and OO may be contained in order to refine the ingot structure and stabilize mechanical properties.

[発明の実施例] 表1に示すアルミニウム合金を従来法により溶製し15
5φの鋳塊とした。
[Example of the invention] The aluminum alloys shown in Table 1 were melted by the conventional method and 15
The ingot was made into a 5φ ingot.

これら鋳塊を均質化処理(525℃X8hr)を行ない
、20φの丸棒へ熱間押出した。押出温度は470℃で
ある。この押出材から引張試験片を作製し、焼入、焼戻
処理を行なった。
These ingots were subjected to homogenization treatment (525°C x 8 hours) and hot extruded into a 20φ round bar. The extrusion temperature is 470°C. A tensile test piece was prepared from this extruded material and subjected to quenching and tempering treatments.

次にこの引張試験片を150℃、200℃。Next, this tensile test piece was tested at 150°C and 200°C.

250℃の各温度下に100時間保持した後、各温度で
引張試験を行なった。0.2%耐力で各材喀 料の高温強度を比較した。
After holding at each temperature of 250° C. for 100 hours, a tensile test was conducted at each temperature. The high temperature strength of each material was compared using 0.2% proof stress.

その結果を表1に示す。The results are shown in Table 1.

表1において、Nol、No12.No13は比較例で
あり、そのうちNo1lは2219であり、No13は
2618である。No2〜N。
In Table 1, No.1, No.12. No. 13 is a comparative example, of which No. 11 is 2219 and No. 13 is 2618. No2~N.

11は本発明の実施例である。11 is an example of the present invention.

表1に示すように、実施例は、150〜250℃のいず
れの温度においても比較例である2219.2618よ
り高い強度を示している。
As shown in Table 1, the examples show higher strength than the comparative example 2219.2618 at any temperature from 150 to 250°C.

[発明の効果][Effect of the invention]

Claims (1)

【特許請求の範囲】 Cu:4.0〜7.0%、Mg:0.3〜 1.0%、Zr:0.05〜0.2%を含有し、かつ、
Mn:0.2〜0.7%、V:0.05〜0.2%の1
種又は2種以上を含有し、残部Al及び不可避的不純物
からなることを特徴とする高温強度に優れたアルミニウ
ム合金。 (但し%は重量%である。以下同じ)
[Claims] Contains Cu: 4.0 to 7.0%, Mg: 0.3 to 1.0%, Zr: 0.05 to 0.2%, and
Mn: 0.2-0.7%, V: 0.05-0.2% 1
An aluminum alloy having excellent high-temperature strength, characterized in that it contains one or more species, and the remainder consists of Al and unavoidable impurities. (However, % is weight %. The same applies below)
JP5645286A 1986-03-14 1986-03-14 Aluminum alloy having superior strength at high temperature Pending JPS62214151A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5645286A JPS62214151A (en) 1986-03-14 1986-03-14 Aluminum alloy having superior strength at high temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5645286A JPS62214151A (en) 1986-03-14 1986-03-14 Aluminum alloy having superior strength at high temperature

Publications (1)

Publication Number Publication Date
JPS62214151A true JPS62214151A (en) 1987-09-19

Family

ID=13027495

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5645286A Pending JPS62214151A (en) 1986-03-14 1986-03-14 Aluminum alloy having superior strength at high temperature

Country Status (1)

Country Link
JP (1) JPS62214151A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020012182A (en) * 2018-07-20 2020-01-23 日本軽金属株式会社 Cold forging material for impeller, and manufacturing method therefor
JP2020066785A (en) * 2018-10-26 2020-04-30 日本軽金属株式会社 Extrusion material for impeller and method for manufacturing the same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020012182A (en) * 2018-07-20 2020-01-23 日本軽金属株式会社 Cold forging material for impeller, and manufacturing method therefor
JP2020066785A (en) * 2018-10-26 2020-04-30 日本軽金属株式会社 Extrusion material for impeller and method for manufacturing the same

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