JPS591781B2 - Porous aluminum sintered alloy sliding member - Google Patents
Porous aluminum sintered alloy sliding memberInfo
- Publication number
- JPS591781B2 JPS591781B2 JP7752578A JP7752578A JPS591781B2 JP S591781 B2 JPS591781 B2 JP S591781B2 JP 7752578 A JP7752578 A JP 7752578A JP 7752578 A JP7752578 A JP 7752578A JP S591781 B2 JPS591781 B2 JP S591781B2
- Authority
- JP
- Japan
- Prior art keywords
- weight
- sintered alloy
- sintered
- aluminum
- strength
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 title claims description 35
- 239000000956 alloy Substances 0.000 title claims description 35
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 23
- 229910052782 aluminium Inorganic materials 0.000 title claims description 18
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 claims description 24
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 14
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 14
- 229910052802 copper Inorganic materials 0.000 claims description 13
- 239000010949 copper Substances 0.000 claims description 13
- 229910052710 silicon Inorganic materials 0.000 claims description 13
- 239000010703 silicon Substances 0.000 claims description 13
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 11
- 150000001639 boron compounds Chemical class 0.000 claims description 11
- 229910052749 magnesium Inorganic materials 0.000 claims description 11
- 239000011777 magnesium Substances 0.000 claims description 11
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 9
- 229910021538 borax Inorganic materials 0.000 claims description 7
- 235000010339 sodium tetraborate Nutrition 0.000 claims description 7
- 239000004328 sodium tetraborate Substances 0.000 claims description 7
- 229910052787 antimony Inorganic materials 0.000 claims description 5
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 5
- 229910021540 colemanite Inorganic materials 0.000 claims description 4
- 238000005245 sintering Methods 0.000 description 17
- 230000000694 effects Effects 0.000 description 11
- 239000003921 oil Substances 0.000 description 11
- 239000000843 powder Substances 0.000 description 6
- 238000007792 addition Methods 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 5
- 230000007423 decrease Effects 0.000 description 5
- 239000000203 mixture Substances 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000011812 mixed powder Substances 0.000 description 3
- 230000007935 neutral effect Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 239000000654 additive Substances 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 125000004122 cyclic group Chemical group 0.000 description 2
- UQGFMSUEHSUPRD-UHFFFAOYSA-N disodium;3,7-dioxido-2,4,6,8,9-pentaoxa-1,3,5,7-tetraborabicyclo[3.3.1]nonane Chemical compound [Na+].[Na+].O1B([O-])OB2OB([O-])OB1O2 UQGFMSUEHSUPRD-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- BTBUEUYNUDRHOZ-UHFFFAOYSA-N Borate Chemical compound [O-]B([O-])[O-] BTBUEUYNUDRHOZ-UHFFFAOYSA-N 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910004835 Na2B4O7 Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- LQZZUXJYWNFBMV-UHFFFAOYSA-N dodecan-1-ol Chemical compound CCCCCCCCCCCCO LQZZUXJYWNFBMV-UHFFFAOYSA-N 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 1
Landscapes
- Sliding-Contact Bearings (AREA)
Description
【発明の詳細な説明】
この発明は、多孔質アルミニウム焼結合金摺動部材に関
するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a porous aluminum sintered alloy sliding member.
従来、アルミニウムを主成分とした焼結合金摺動部材は
、比較的速度特性が優れていること、耐蝕性を有し軽量
であることなどの利点がある反面、機械的強度、耐摩耗
性、耐荷重性が十分でなく、また焼結条件の設定が難し
いなどの問題があつて、必ずしも満足すべき結果が得ら
れていない。Conventionally, sintered alloy sliding members mainly made of aluminum have advantages such as relatively excellent speed characteristics, corrosion resistance, and light weight, but on the other hand, they have poor mechanical strength, wear resistance, There are problems such as insufficient load resistance and difficulty in setting sintering conditions, and satisfactory results are not always obtained.
この発明は従来のこのような問題点を大巾に改善するこ
とに成功したものであり、重量比で銅0.5〜6%、マ
グネシウム0.2〜2%、けい素5〜30%、三二酸化
ホウ素、ホウ砂、コレマナイト、ボロナトロカルサイト
から選択されたホウ素化合物0.5〜8%そして残部ア
ルミニウムからなる多孔質アルミニウム焼結合金摺動部
材を提供するものである。そして上記成分に錫およびア
ンチモンのいずれか一種または二種の合量が10%以下
、およびあるいは鉛20Cfl7以下を合金成分として
加えることによつてなじみ性、耐焼付き性を一層向上せ
しめた摺動部材として提供することもできる。This invention has succeeded in greatly improving these conventional problems, and the weight ratio is 0.5 to 6% copper, 0.2 to 2% magnesium, 5 to 30% silicon, The present invention provides a porous aluminum sintered alloy sliding member comprising 0.5 to 8% of a boron compound selected from boron sesquioxide, borax, colemanite, and boronatrocalcite, and the balance aluminum. A sliding member whose conformability and seizure resistance are further improved by adding 10% or less of one or both of tin and antimony to the above components, and/or 20Cfl7 or less of lead as an alloying component. It can also be provided as
上述した多孔質アルミニウム焼結合金摺動部材はいずれ
も大気中での焼結が可能であり、しかも機械的強度が優
れていることを特長とするものである。The porous aluminum sintered alloy sliding members described above are all characterized by being able to be sintered in the atmosphere and having excellent mechanical strength.
この発明で、とくにけい素を多く含む点については、本
発明者等がなした特公昭47−32163号、特公昭5
1−35364号に係わる発明ですでに詳細に開示した
ように、摺動部材として耐焼付き性、耐荷重性などの摺
動特性の向上のほか、成形性を向上せしめる点にある。Regarding this invention, especially regarding the fact that it contains a large amount of silicon, the inventors of the present invention et al.
As already disclosed in detail in the invention related to No. 1-35364, the present invention is capable of improving moldability as well as improving sliding properties such as seizure resistance and load resistance as a sliding member.
けい素が5重量%以下では、この発明においては耐荷重
・姓、耐焼付き性が改善されず、摺動部材としては使用
に供し難い。If the silicon content is less than 5% by weight, the present invention does not improve the load resistance, resistance, and seizure resistance, making it difficult to use as a sliding member.
そして10重量%前後の配合で、ロックウェル硬さ、圧
環強度常数ともに最大の値を示すが、それ以上に配合量
を増加せしめると、これらの値は徐々に減少する。けい
素の配合はまた焼結合金の多孔度(この発明では含油率
をもつて示した)を増大せしめる。When the content is around 10% by weight, both the Rockwell hardness and the radial crushing strength constant show maximum values, but when the content is increased beyond that, these values gradually decrease. The inclusion of silicon also increases the porosity (expressed in this invention by oil content) of the sintered alloy.
。とくに、けい素配合量が10重量%前後から含油率は
ほぼ直線的に増加するが、機械的強度の低下との兼ね合
いから30重量%をもつて上限とした。ホウ素化合物に
ついては、三二酸化ホウ素(B2O3)、ホウ砂(Na
2B407・10H20)、コレマナイト(Ca、B、
O、、・ 5H、O)、パンデルミツト(Ca,B6O
ll−3H20)、ボロナトロカルサイト(CaB4O
7・NaBO,・6H,0)などが使用されるが、とく
に三二酸化ホウ素ついでホウ砂が有効である。. In particular, the oil content increases almost linearly when the silicon content is around 10% by weight, but the upper limit was set at 30% by weight in view of the reduction in mechanical strength. Regarding boron compounds, boron sesquioxide (B2O3), borax (Na
2B407・10H20), Colemanite (Ca, B,
O,... 5H, O), pandermite (Ca, B6O
ll-3H20), boronatrocalcite (CaB4O
7.NaBO, .6H,0), etc. are used, but boron sesquioxide and borax are particularly effective.
結晶水を含むホウ酸塩を使用する場合は、結晶水を全部
飛ばしてから使用することが重要である。さもないと効
果が現れない。ホウ素化合物は、圧粉体の焼結性を向上
せしめ焼結合金の機械的強度を著しく向土せしめる効果
がある。本発明者の実験によれば、三二酸化ホウ素は0
.5重量%前後の添加ですでに効果が現われ、2重量%
前後で機械的強度向上にもつとも寄与し、無添加のもの
に比較して約2倍の強度上昇が確認された。2重量%を
超えてさらに多く添加すると強度は減少し始め、10重
量%前後の添加では三二酸化ホウ素無添加の合金と反程
度の強度となる。When using a borate containing water of crystallization, it is important to remove all the water of crystallization before use. Otherwise, the effect will not appear. The boron compound has the effect of improving the sinterability of the green compact and significantly increasing the mechanical strength of the sintered alloy. According to the inventor's experiments, boron sesquioxide has 0
.. Effects are already visible when around 5% by weight is added, and 2% by weight
It was confirmed that the before and after additions also contributed to the improvement of mechanical strength, and the strength increase was approximately twice that of the one without additives. If more than 2% by weight is added, the strength will begin to decrease, and if around 10% by weight is added, the strength will be the opposite of that of an alloy without boron sesquioxide.
上述したホウ素化合物は、金属酸化物を溶解せしめる作
用があり、また圧粉体焼結時において成分の酸化を防止
する効果があるから、アルミニウム粉末の焼結性を向上
せしめ、とくに大気中においても焼結を可能ならしめた
ものと考えられるが、さらに大きな効果は銅およびマグ
ネシウムおよびあるいはマグネシウムとけい素との化合
物(Mg2Si)のアルミニウム中への拡散を助長し、
均一な合金組織とすることで本発明者はX線マイクロア
ナライザーによる解析の結果この事実を確認した。The boron compound mentioned above has the effect of dissolving metal oxides and also has the effect of preventing the oxidation of components during compact sintering, so it improves the sinterability of aluminum powder, especially in the atmosphere. It is thought that this makes sintering possible, but an even greater effect is that it promotes the diffusion of copper and magnesium and/or a compound of magnesium and silicon (Mg2Si) into the aluminum.
By making the alloy structure uniform, the present inventor confirmed this fact as a result of analysis using an X-ray microanalyzer.
すなわちホウ素化合物を添加しない合金にあつては、た
とえば銅成分は焼結合金中の粒界もしくはボードの周辺
に多く存在するが、該化合物を添加すると銅の分布は著
しく均一となり、アルミニウム中への拡散が順調に進ん
でいることが確認された。In other words, in the case of alloys without the addition of boron compounds, for example, copper components are present in large quantities at the grain boundaries in the sintered alloy or around the board, but when such compounds are added, the distribution of copper becomes extremely uniform, and the copper component in the aluminum becomes more uniform. It was confirmed that the spread was progressing smoothly.
したがつて焼結体の合金化力塙度にはかられ、焼結体の
強度が著しく向上したものと考えることができる。この
ホウ素化合物の添加はまた焼結体の多孔度を大きくする
傾向がある。Therefore, it can be considered that the strength of the sintered body is significantly improved due to the degree of alloying strength of the sintered body. The addition of this boron compound also tends to increase the porosity of the sintered body.
機械的強度への影響と若干趣きを異にし、2重量%位ま
での添加に対しては著しい変化は無いが、さらに添加量
を増すと含油率は徐々に向上する。しかし前述したよう
にホウ素化合物は10重量%の添加でほぼ無添加のもの
と同程度もしくはそれ以下の強度にまで低下するから、
この強度との兼ね合いから0.5〜8重量%とくに1〜
6重量%とすることが望ましい。銅成分については、合
金の強度向上に寄与する。この発明の組成においては、
0.5重量%以下ではほとんど効果がなく、また6重量
%を超えて添加すると材質を脆くする傾向がでてくるか
ら、添加量は0.5〜6重量%とした。マグネシウム成
分については、銅と共存して合金の機械的強度向上に寄
与する。The effect on mechanical strength is slightly different, and there is no significant change when added up to about 2% by weight, but as the amount added is further increased, the oil content gradually increases. However, as mentioned above, when 10% by weight of boron compounds is added, the strength decreases to almost the same level as that without additives or even lower.
In consideration of this strength, 0.5 to 8% by weight, especially 1 to 8% by weight.
The content is preferably 6% by weight. The copper component contributes to improving the strength of the alloy. In the composition of this invention,
If it is less than 0.5% by weight, it has almost no effect, and if it exceeds 6% by weight, it tends to make the material brittle, so the amount added is set to 0.5 to 6% by weight. The magnesium component coexists with copper and contributes to improving the mechanical strength of the alloy.
またマグネシウムはけい素とMg2Siの形でアルミニ
ウム焼結合金の時効硬化性に寄与する。この発明の組成
においては、0.2重量%以下ではほとんど効果がなく
、また2重量%を超えると反つて強度低下をきたし焼結
性も悪くなる。錫、アンチモンおよび鉛成分は、摺動部
材としての合金のなじみ性および耐焼付き性の向上に寄
与する。Magnesium also contributes to the age hardenability of the aluminum sintered alloy in the form of silicon and Mg2Si. In the composition of the present invention, if it is less than 0.2% by weight, there is almost no effect, and if it exceeds 2% by weight, the strength will decrease and the sinterability will deteriorate. The tin, antimony, and lead components contribute to improving the conformability and seizure resistance of the alloy as a sliding member.
錫、アンチモンはそれぞれ単独または二者の合量が0.
3〜10重量%とすることが望ましい。0.3重量%以
下では添加の効果が明確でない。Tin and antimony are used individually or in a total amount of 0.
The content is preferably 3 to 10% by weight. The effect of addition is not clear below 0.3% by weight.
また10重量%を超えて添加すると合金の強度を低下せ
しめる。鉛は5〜20重量%添加すると、なじみ性の向
上に寄与するほか、耐焼付き性を向上せしめる。Moreover, if it is added in an amount exceeding 10% by weight, the strength of the alloy will be reduced. When lead is added in an amount of 5 to 20% by weight, it not only contributes to improving conformability but also improves seizure resistance.
5重量%以下では添加効果に再現性が乏しく、20重量
%を超えて添加すると合金の強度を損なつ。If it is less than 5% by weight, the effect of addition is poor in reproducibility, and if it is added in excess of 20% by weight, the strength of the alloy will be impaired.
これらなじみ性、耐焼付き性の向上に寄与する金属成分
は、使用目的に応じてそれぞれ単独もしくはいずれか二
種以上を混じて使用することができる。These metal components that contribute to improving conformability and seizure resistance can be used alone or in combination of two or more, depending on the purpose of use.
この発明の焼結合金を得るに際し、成形圧力は1〜5ト
ン/C77l、就中2〜4トン/〜が適当である。When obtaining the sintered alloy of the present invention, the compacting pressure is preferably 1 to 5 tons/C77l, particularly 2 to 4 tons/~.
成形圧力を高くすると圧環強度常数などの機械的強度は
向上するが多孔度(含油率)は減少する。焼結温度は5
50〜640℃とアルミニウムの融点以下の温度とし、
焼結時間は5〜60分である。When the molding pressure is increased, the mechanical strength such as the radial crushing strength constant improves, but the porosity (oil content) decreases. Sintering temperature is 5
The temperature is 50 to 640°C, which is below the melting point of aluminum,
Sintering time is 5-60 minutes.
中性もしくは環元性雰囲気中で焼結を進めても構わない
が、この発明の特徴は大気中における焼結が可能なこと
で、しかも得られた焼結体の機・械的強度は中性もしく
は環元性雰囲気中で焼結したものと比較して著しい差が
ないということである。さらに、ホウ素化合物を含まな
い同様の組成のアルミニウム焼結合金に比較しても、大
気中焼結であるにもかかわらず、その強度が著しく大き
いということである。Sintering may proceed in a neutral or cyclic atmosphere, but the feature of this invention is that sintering can be performed in the atmosphere, and the mechanical strength of the obtained sintered body is moderate. This means that there is no significant difference compared to those sintered in a neutral or cyclic atmosphere. Furthermore, even when compared to an aluminum sintered alloy of a similar composition that does not contain a boron compound, its strength is significantly greater despite being sintered in the air.
大気中焼結では焼結時間を過大にとることは何んら益が
ない。In air sintering, there is no benefit in taking too long a sintering time.
所定の温度に調整された炉内で迅速に焼結を進めること
が望ましい。焼結時間30分前後で焼結体の機械的強度
はほば最高強度に達する。そして得られた焼結体の外表
面も中性もしくは還元性雰囲気中で焼結したものと比較
してほとんど遜色がない。It is desirable to rapidly proceed with sintering in a furnace adjusted to a predetermined temperature. The mechanical strength of the sintered body almost reaches its maximum strength after about 30 minutes of sintering time. The outer surface of the obtained sintered body is also almost comparable to that of one sintered in a neutral or reducing atmosphere.
表は、銅4重量%、マグネシウム0.5重量%、けい素
10重量%とし、ホウ素化合物として三二酸化ホウ素の
配合量を変えた場合、圧環強度常数、含伸率が如何に影
響を受けるかについて示したものである。The table shows how the radial crushing strength constant and elongation content are affected when the content of boron sesquioxide as a boron compound is changed using 4% by weight of copper, 0.5% by weight of magnesium, and 10% by weight of silicon. This is what is shown.
成形圧力は3トン/o/l、焼結条件は大気中で580
℃±10℃の温度に保持した炉内で10分間焼結したも
のである。以上のように、本発明の多孔質アルミニウム
焼結合金摺動部材(上表の黒2〜黒8)は、機械的強度
が高く摺動特性にすぐれ、しかもその製造においては焼
結が容易であること、特別の雰囲気調整も不要で大気中
焼結が可能であることなどの特長を有するものである。The molding pressure was 3 tons/o/l, and the sintering conditions were 580°C in the air.
It was sintered for 10 minutes in a furnace maintained at a temperature of ±10°C. As described above, the porous aluminum sintered alloy sliding members of the present invention (black 2 to black 8 in the table above) have high mechanical strength and excellent sliding properties, and are easy to sinter in manufacturing. It has the advantages of being able to be sintered in the atmosphere without the need for special atmosphere adjustment.
以下実施例にもとずいて説明する。The following description will be made based on examples.
(実施例 1)
200メツシユを通過する電解銅粉末4重量%、同じく
200メツシユを通過するアグネシウム粉末0.5重量
%、250メツシユを通過するけい素粉末10重量%、
200メツシユを通過する三二酸化ホウ素粉末2重量%
、そして残部を250メツシユを通過するアトマイズア
ルミニウム粉末とし、これに少量のラウリルアルコール
、ステアリン酸亜鉛などの滑剤′全合金粉末に対して2
重量%)を均一に混合し、得られた混合粉末を金型中で
成形圧力3トン/dで圧粉したのち型から取り出し、こ
れを大気中で580℃±10℃の温度に保持した炉内で
10分間焼結した。(Example 1) 4% by weight of electrolytic copper powder passing through 200 meshes, 0.5% by weight of agnesium powder passing through 200 meshes, 10% by weight of silicon powder passing through 250 meshes,
2% by weight of boron sesquioxide powder passing through 200 meshes
, and the remainder is atomized aluminum powder that passes through 250 meshes, and a small amount of lubricant such as lauryl alcohol and zinc stearate '2 for all alloy powders.
% by weight), the resulting mixed powder was compacted in a mold at a compacting pressure of 3 tons/d, taken out from the mold, and placed in a furnace maintained at a temperature of 580°C ± 10°C in the atmosphere. sintered for 10 minutes.
かくして得た焼結合金の圧環強度常数は20.5k9/
Md、含油率3.2重量%、初期摩擦係数(μR)0.
120、定常状態における摩擦係数(μc)0.100
であった。The radial crushing strength constant of the sintered alloy thus obtained was 20.5k9/
Md, oil content 3.2% by weight, initial coefficient of friction (μR) 0.
120, coefficient of friction in steady state (μc) 0.100
Met.
(実施例 2)
ホウ素化合物として三二酸化ホウ素の代りにホウ砂を4
00℃で焼いて結晶水を飛ばして得た四ホウ酸ソーダ(
Na2B4O7)を200メツシユを通過する粉末に粉
砕し、この粉末を2重量%添加して以下実施例1と同様
にして焼結合金を得た。(Example 2) Borax was used instead of boron sesquioxide as a boron compound.
Sodium tetraborate obtained by baking at 00℃ and removing crystallization water (
A sintered alloy was obtained in the same manner as in Example 1 by pulverizing Na2B4O7) into a powder that passed through 200 meshes and adding 2% by weight of this powder.
このものの圧環強度常数は16.0kg/M77f、含
油率3.0重量%、μRO.l2O、μCO.lOOで
あつた。(実施例 3)
銅、マグネシウム、けい素、三二酸化ホウ素を実施例1
と同様の配合比にとり、これにさらに250メツシユを
通過する搗砕錫粉末を2重量%加えて残部をアルミニウ
ム粉末とし、以下実施例1と同様にして焼結合金を得た
。This material has a radial crushing strength constant of 16.0 kg/M77f, an oil content of 3.0% by weight, and a μRO. l2O, μCO. It was lOO. (Example 3) Copper, magnesium, silicon, boron sesquioxide in Example 1
A sintered alloy was obtained in the same manner as in Example 1, using the same blending ratio as above, adding 2% by weight of crushed tin powder that passed through 250 meshes and using the remainder as aluminum powder.
このものの圧環強度常一数19.0kg/Md、含油率
3.0重量%、μRO.llO、μCO,O95であつ
た。(実施例 4)
実施例3において、錫粉末の代りに250メツシユを通
過するアンチモン粉末を2重量%加えて残部をアルミニ
ウム粉末とし、以下同様にして焼結合金を得た。This product has a constant radial crushing strength of 19.0 kg/Md, an oil content of 3.0% by weight, and a μRO. They were llO, μCO, and O95. (Example 4) In Example 3, 2% by weight of antimony powder that passes through 250 meshes was added in place of the tin powder, and the remainder was made into aluminum powder, and a sintered alloy was obtained in the same manner.
このものの圧環強度常数18.5kV龍、含油率3.0
重量%、μRO.llO、μCO.O95であつた。(
実施例 5)
実施例3において、錫粉末の代りに250メ.ツシユを
通過する鉛粉末を10重量%加えて残部をアルミニウム
粉末とし、以下同様にして焼結合金を得た。This product has a radial crushing strength constant of 18.5 kV and an oil content of 3.0.
Weight %, μRO. llO,μCO. It was O95. (
Example 5) In Example 3, 250 ml of tin powder was used instead of tin powder. 10% by weight of the lead powder passing through the thread was added and the remainder was made into aluminum powder, and a sintered alloy was obtained in the same manner.
このものの圧環強度常数14.0kg/M7l、含油率
2.7重量%、μRO.O95、μCO.O9Oであつ
た。比較例として、前記表に示した崖1の焼結合金、す
なわち銅4重量%、マグネシウム0.5重量%、けい素
10重量%、残部アルミニウムからなる混合粉末を実施
例と同様の条件で成形・焼結して得た焼結合金の圧環強
度常数は9.5kg/7n7i、含油率3、1重量%、
μRO.l5,μCO.l2であつた。This product has a radial crushing strength constant of 14.0 kg/M7l, an oil content of 2.7% by weight, and a μRO. O95, μCO. It was O9O. As a comparative example, a mixed powder consisting of the sintered alloy of cliff 1 shown in the table above, ie, 4% by weight of copper, 0.5% by weight of magnesium, 10% by weight of silicon, and the balance aluminum was molded under the same conditions as in the example.・The radial crushing strength constant of the sintered alloy obtained by sintering is 9.5 kg/7n7i, oil content 3, 1% by weight,
μRO. l5,μCO. It was l2.
また、実施例3の比較例として、前述した従来技術の特
公昭47−32163号に開示された焼結合金を実施例
3と同様の成分組成に調整、すなわち、銅4重量%、マ
グネシウム0.5重量%、けい素10重量%、錫2重量
%、残部アルミニウムとし、これを実施例と同様の条件
で成形・焼結して得た焼結合金の圧環強度常数は18.
5k9/M7i、含油率1.5重量%、μRO.l3、
μCO.llであつた。そして、これら比較例の焼結合
金には、焼結時における酸化が認められた。Further, as a comparative example of Example 3, the sintered alloy disclosed in the prior art Japanese Patent Publication No. 47-32163 was adjusted to have the same composition as Example 3, that is, 4% by weight of copper and 0.0% by weight of magnesium. 5% by weight, 10% by weight of silicon, 2% by weight of tin, and the balance aluminum, and the sintered alloy obtained by molding and sintering this under the same conditions as in the example had a radial crushing strength constant of 18.
5k9/M7i, oil content 1.5% by weight, μRO. l3,
μCO. It was hot. Oxidation was observed in the sintered alloys of these comparative examples during sintering.
なお、各実施例および比較例で示したμR,μcは、モ
ービル油を含浸させたものを周速20m/朋、負荷10
0kg/C−FLで機械構造用炭素鋼を相手材としてス
ラスト摩擦摩耗試験機によつて試験した結果について示
した。In addition, μR and μc shown in each example and comparative example are measured at a circumferential speed of 20 m/day and a load of 10
The results of a test using a thrust friction and wear tester using carbon steel for machine structures as a mating material at 0 kg/C-FL are shown below.
以上述べた実施例の焼結合金は、比較例との比較におい
て、機械的強度が高く、かつ摺動特性にすぐれているこ
とがわかる。It can be seen that the sintered alloys of the examples described above have high mechanical strength and excellent sliding characteristics when compared with the comparative examples.
なお、実施例では混合粉末を成形後、焼結する方法につ
いて述べたが、焼結合金の使用目的によつては、加圧し
ながら焼結を進める方法を採用することにより、一層高
密度、高強度の焼結合金を得ることもできる。In addition, although the method of sintering the mixed powder after molding was described in the example, depending on the intended use of the sintered alloy, it is possible to achieve even higher density and higher density by adopting a method of proceeding with sintering while applying pressure. It is also possible to obtain a strong sintered alloy.
Claims (1)
%、けい素5〜30%、三二酸化ホウ素、ホウ砂、コレ
マナイト、ボロナトロカルサイトから選択されたホウ素
化合物0.5〜8%そして残部アルミニウムからなる多
孔質アルミニウム焼結合金摺動部材。 2 重量比で銅0.5〜6%、マグネシウム0.2〜2
%、けい素5〜30%、錫およびアンチモンのいずれか
一種または二種の合量が10%以下、およびあるいは鉛
20%以下、三二酸化ホウ素、ホウ砂、コレマナイト、
ボロナトロカルサイトから選択されたホウ素化合物0.
5〜8%そして残部アルミニウムからなる多孔質アルミ
ニウム焼結合金摺動部材。[Claims] 1. Copper 0.5-6%, magnesium 0.2-2% by weight
%, silicon 5-30%, boron sesquioxide, borax, colemanite, boronatrocalcite 0.5-8%, and the balance aluminum. 2 Copper 0.5-6%, magnesium 0.2-2% by weight
%, silicon 5-30%, the total amount of one or both of tin and antimony is 10% or less, and/or lead 20% or less, boron sesquioxide, borax, colemanite,
Boron compound selected from boronatrocalcite 0.
A porous aluminum sintered alloy sliding member consisting of 5 to 8% aluminum and the balance aluminum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7752578A JPS591781B2 (en) | 1978-06-28 | 1978-06-28 | Porous aluminum sintered alloy sliding member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7752578A JPS591781B2 (en) | 1978-06-28 | 1978-06-28 | Porous aluminum sintered alloy sliding member |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS556439A JPS556439A (en) | 1980-01-17 |
| JPS591781B2 true JPS591781B2 (en) | 1984-01-13 |
Family
ID=13636381
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7752578A Expired JPS591781B2 (en) | 1978-06-28 | 1978-06-28 | Porous aluminum sintered alloy sliding member |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS591781B2 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5794398A (en) * | 1980-12-04 | 1982-06-11 | Nippon Kayaku Co Ltd | Scale preventing agent |
| JPS5992097A (en) * | 1982-11-17 | 1984-05-28 | Katayama Chem Works Co Ltd | Additive for soft water in boiler |
| CN105154699A (en) * | 2015-08-31 | 2015-12-16 | 苏州莱特复合材料有限公司 | Preparation method of high temperature-resistant aluminium alloy material |
| CN111979440A (en) * | 2020-08-20 | 2020-11-24 | 安徽工业大学 | Aluminum alloy component for preparing foamed aluminum by powder metallurgy method and foaming method |
-
1978
- 1978-06-28 JP JP7752578A patent/JPS591781B2/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS556439A (en) | 1980-01-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4551395A (en) | Bearing materials | |
| US5292358A (en) | Sintered aluminum-alloy | |
| US3956568A (en) | Carbon-metal composite material | |
| US4177069A (en) | Process for manufacturing sintered compacts of aluminum-base alloys | |
| US3461069A (en) | Self-lubricating bearing compositions | |
| US4012230A (en) | Tungsten-nickel-cobalt alloy and method of producing same | |
| CA1045827A (en) | Grain refining of aluminum | |
| JPH0120215B2 (en) | ||
| EP0224619A1 (en) | Bearing materials | |
| JPS591781B2 (en) | Porous aluminum sintered alloy sliding member | |
| JPS5937339B2 (en) | Method for manufacturing high silicon aluminum alloy sintered body | |
| US6676894B2 (en) | Copper-infiltrated iron powder article and method of forming same | |
| JP4177534B2 (en) | Alloy powder for copper-based high strength sintered parts | |
| EP0171798A1 (en) | High strength material produced by consolidation of rapidly solidified aluminum alloy particulates | |
| US2945759A (en) | Method for measuring the strength of sintered ferrous articles | |
| EP0250414B1 (en) | Method in producing a molding of an iron alloy | |
| US4130422A (en) | Copper-base alloy for liquid phase sintering of ferrous powders | |
| JP2009007433A (en) | Copper-based oil-containing sintered sliding member and method for producing the same | |
| US3161948A (en) | Compositions containing iron, molybdenu, silicon and selected low-melting metals | |
| JPH045745B2 (en) | ||
| JPS6016511B2 (en) | Sintered oil-impregnated bearing with high strength and high oil content | |
| JPS5843459B2 (en) | Aluminum sintered alloy member and its manufacturing method | |
| JPS6038442B2 (en) | Manufacturing method of aluminum alloy low density sintered parts | |
| JPS5641348A (en) | Metal-graphite-ceramic composite | |
| JPS6346138B2 (en) |