EP0362086B1 - Verfahren zur Herstellung von Werkstücken aus einer Aluminium-Legierung, welche bei einem längeren Verbleib auf höheren Temperaturen eine gute Ermüdungsbeständigkeit beibehält - Google Patents
Verfahren zur Herstellung von Werkstücken aus einer Aluminium-Legierung, welche bei einem längeren Verbleib auf höheren Temperaturen eine gute Ermüdungsbeständigkeit beibehält Download PDFInfo
- Publication number
- EP0362086B1 EP0362086B1 EP89420361A EP89420361A EP0362086B1 EP 0362086 B1 EP0362086 B1 EP 0362086B1 EP 89420361 A EP89420361 A EP 89420361A EP 89420361 A EP89420361 A EP 89420361A EP 0362086 B1 EP0362086 B1 EP 0362086B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- zirconium
- manganese
- process according
- mpa
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
Definitions
- the present invention relates to a process for manufacturing parts made of aluminum alloy retaining good resistance to fatigue after prolonged hot keeping.
- aluminum has the particular property of being three times lighter than steel and of having good corrosion resistance. By combining it with metals such as copper and magnesium, its mechanical resistance is greatly improved. Furthermore, the addition of silicon gives a product having good wear resistance. These alloys doped with other elements such as iron, nickel, cobalt, chromium and manganese, see their heat resistance improved. A compromise between these addition elements makes aluminum a material of choice for the manufacture of parts for automobiles such as engine block, piston, cylinder, etc.
- EP 144898 teaches an aluminum alloy containing by weight 10 to 36% of silicon, 1 to 12% of copper, 0.1 to 3% of magnesium and 2 to 10% of at least one element chosen from the group Fe, Ni, Co, Cr and Mn.
- This alloy is applicable to the manufacture of parts intended for both the aeronautical and automotive industries, said parts being obtained by the technique of powder metallurgy comprising, in addition to shaping by compacting and spinning, an intermediate processing step thermal between 250 and 550 ° C.
- Document JP-A-6342344 is also known, which teaches an aluminum alloy with excellent mechanical properties at high temperature by powder metallurgy, characterized in that it consists of Si, Fe, Cu, Mg and Mn in the weight proportions. 12 ⁇ If ⁇ 28%, 2.0 ⁇ Fe ⁇ 10%, 0.8 ⁇ Cu ⁇ 5.0%, 0.3 ⁇ Mg ⁇ 3.5% and 0.5 ⁇ Mn ⁇ 5%, of one or more elements chosen from Zr, Hf, Ni, Ti, V, Cr , Mo, Nb and Ta in a proportion by weight of 0.02 - 2.0% and, for the rest, of aluminum and inevitable impurities. But here, as in the previous document, no mention is made of the fatigue resistance properties after being kept for 1000 hours at 150 ° C. and the range of manganese content is relatively wide.
- the Applicant has noticed that if the zirconium brought a significant improvement from the point of view of the fatigue limit at 20 ° C, since it went from 150 to 185 MPa, on the other hand, after a maintenance of 1000 hours at 150 ° C (which roughly represents the working conditions of a connecting rod at mid-life of an engine), that limit dropped to 143 Mpa, a reduction of more than 22%.
- the present invention which consists of a process for manufacturing aluminum alloy parts obtained from the alloy in the state melted by a means of rapid solidification, retaining a suitable resistance to fatigue after prolonged keeping hot which contain by weight 11 to 26% of silicon, 2 to 5% of iron, 0.5 to 5% of copper, 0, 1% to 2% magnesium, zirconium, at least 0.5% manganese, optionally minor additions of nickel and / or cobalt and the aluminum balance, characterized in that an alloy containing 0.1 to 0.4% of zirconium and up to 1.5% of manganese is used.
- manganese has been substituted for part of the zirconium, which on the one hand allows savings on raw materials: manganese being cheaper than zirconium , on the other hand facilitates the melting conditions of the alloy since a binary alloy containing 1% of zirconium has a liquidus temperature of 875 ° C whereas if it is 1% of manganese this temperature remains close 660 ° C.
- the invention is also characterized in that the alloy is subjected in the molten state to a rapid solidification means before putting it in the form of parts.
- a rapid solidification means before putting it in the form of parts.
- elements such as iron, zirconium and manganese are very little soluble in the alloy, it is essential to obtain parts meeting the desired characteristics to avoid a rough and heterogeneous precipitation of these elements what we achieves by cooling them as quickly as possible.
- the alloy is preferably melted at a temperature above 700 ° C so as to avoid any phenomenon of premature precipitation.
- the parts after being possibly subjected to machining, are heat treated between 490 and 520 ° for 1 to 10 hours, then quenched in water before undergoing a tempering treatment between 170 to 210 ° C for 2 to 32 hours, which improves their mechanical characteristics.
- the combination of zirconium-manganese in limited quantities and the rapid solidification of the alloy obtained contribute to improving the resistance to fatigue, whether cold or hot, of parts liable to exhibit irregularities. surface like threads or connection curves and which find their application in the automobile industry, in particular in the confection of rods, axes of pistons and pistons.
Landscapes
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Powder Metallurgy (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
- Forging (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Coating By Spraying Or Casting (AREA)
- Conductive Materials (AREA)
Claims (5)
- Verfahren zur Herstellung von Werkstücken aus Aluminiumlegierung, die aus der Legierung im geschmolzenen Zustand durch ein Mittel zur raschen Erstarrung erhalten werden, eine geeignete Beständigkeit gegen die Ermüdung nach einem verlängerten Halten in der Wärme beibehalten und gewichtsmäßig 11 bis 26 % Silicium, 2 bis 5 % Eisen, 0,5 bis 5 % Kupfer, 0,1 bis 2 % Magnesium, Zirconium, wenigstens 0,5 % Mangan, gegebenenfalls geringere Zusätze von Nickel und/oder Kobalt und Rest Aluminium enthalten,
dadurch gekennzeichnet,
daß man eine Legierung einsetzt, die 0,1 bis 0,4 % Zirconium und bis zu 1,5 % Mangan enthält. - Verfahren nach dem Anspruch 1,
dadurch gekennzeichnet,
daß das Mittel zur raschen Erstarrung darin besteht, die geschmolzene Legierung in Form feiner Tröpfchen zu unterteilen. - Verfahren nach dem Anspruch 1,
dadurch gekennzeichnet,
daß das Mittel zur raschen Erstarrung aus einem Schleudern der geschmolzenen Legierung gegen eine gekühlte metallische Oberfläche besteht. - Verfahren nach dem Anspruch 1,
dadurch gekennzeichnet,
daß das Mittel zur raschen Erstarrung aus einem Schleudern der in einem Gasstrom zersprühten Legierung gegen ein Substrat besteht. - Verfahren nach dem Anspruch 1,
dadurch gekennzeichnet,
daß man die Werkstücke einer Wärmebehandlung bei einer Temperatur im Bereich von 490 bis 520 °C, einem Abschrecken in Wasser und einem Anlassen zwischen 170 und 210 °C unterwirft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT89420361T ATE90397T1 (de) | 1988-09-26 | 1989-09-21 | Verfahren zur herstellung von werkstuecken aus einer aluminium-legierung, welche bei einem laengeren verbleib auf hoeheren temperaturen eine gute ermuedungsbestaendigkeit beibehaelt. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8812982 | 1988-09-26 | ||
FR8812982A FR2636974B1 (fr) | 1988-09-26 | 1988-09-26 | Pieces en alliage d'aluminium gardant une bonne resistance a la fatigue apres un maintien prolonge a chaud et procede de fabrication desdites pieces |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0362086A1 EP0362086A1 (de) | 1990-04-04 |
EP0362086B1 true EP0362086B1 (de) | 1993-06-09 |
Family
ID=9370672
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89420361A Expired - Lifetime EP0362086B1 (de) | 1988-09-26 | 1989-09-21 | Verfahren zur Herstellung von Werkstücken aus einer Aluminium-Legierung, welche bei einem längeren Verbleib auf höheren Temperaturen eine gute Ermüdungsbeständigkeit beibehält |
Country Status (16)
Country | Link |
---|---|
US (2) | US4963322A (de) |
EP (1) | EP0362086B1 (de) |
JP (1) | JPH0819496B2 (de) |
KR (1) | KR930003602B1 (de) |
CN (1) | CN1041399A (de) |
AT (1) | ATE90397T1 (de) |
BR (1) | BR8904844A (de) |
DD (1) | DD284904A5 (de) |
DE (1) | DE68906999T2 (de) |
DK (1) | DK468489A (de) |
ES (1) | ES2042048T3 (de) |
FI (1) | FI894499A (de) |
FR (1) | FR2636974B1 (de) |
HU (1) | HUT53680A (de) |
IL (1) | IL91738A0 (de) |
YU (1) | YU185389A (de) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE69221690T2 (de) * | 1991-04-03 | 1998-04-02 | Sumitomo Electric Industries | Rotor für ölpumpe aus einer aluminiumlegierung und dessen herstellungsverfahren |
US5372775A (en) * | 1991-08-22 | 1994-12-13 | Sumitomo Electric Industries, Ltd. | Method of preparing particle composite alloy having an aluminum matrix |
EP0577062B1 (de) * | 1992-06-29 | 1999-09-08 | Sumitomo Electric Industries, Limited | Ölpumpe aus Aluminiumlegierungen |
EP0657553A1 (de) * | 1993-11-10 | 1995-06-14 | Sumitomo Electric Industries, Ltd. | Stickstoffhaltige Aluminium-Silizium pulvermetallurgische Legierung |
DE19523484C2 (de) * | 1995-06-28 | 2002-11-14 | Daimler Chrysler Ag | Verfahren zum Herstellen einer Zylinderlaufbüchse aus einer übereutektischen Aluminium/Silizium-Legierung zum Eingießen in ein Kurbelgehäuse einer Hubkolbenmaschine und danach hergestellte Zylinderlaufbüchse |
US6332906B1 (en) | 1998-03-24 | 2001-12-25 | California Consolidated Technology, Inc. | Aluminum-silicon alloy formed from a metal powder |
US5965829A (en) * | 1998-04-14 | 1999-10-12 | Reynolds Metals Company | Radiation absorbing refractory composition |
DE10053664A1 (de) * | 2000-10-28 | 2002-05-08 | Leybold Vakuum Gmbh | Mechanische kinetische Vakuumpumpe |
US6902699B2 (en) * | 2002-10-02 | 2005-06-07 | The Boeing Company | Method for preparing cryomilled aluminum alloys and components extruded and forged therefrom |
US7435306B2 (en) * | 2003-01-22 | 2008-10-14 | The Boeing Company | Method for preparing rivets from cryomilled aluminum alloys and rivets produced thereby |
JP4665413B2 (ja) * | 2004-03-23 | 2011-04-06 | 日本軽金属株式会社 | 高剛性・低線膨張率を有する鋳造用アルミニウム合金 |
US7922841B2 (en) * | 2005-03-03 | 2011-04-12 | The Boeing Company | Method for preparing high-temperature nanophase aluminum-alloy sheets and aluminum-alloy sheets prepared thereby |
CN1317410C (zh) * | 2005-03-09 | 2007-05-23 | 沈阳工业大学 | 一种耐磨、耐热高硅铝合金及其成型工艺 |
DE102008018850A1 (de) * | 2007-11-30 | 2009-06-04 | Andreas Borst | Kolben und Verfahren zu dessen Herstellung |
CN103031473B (zh) * | 2009-03-03 | 2015-01-21 | 中国科学院苏州纳米技术与纳米仿生研究所 | 高韧性Al-Si系压铸铝合金的加工方法 |
CN107377973A (zh) * | 2017-08-30 | 2017-11-24 | 广东美芝制冷设备有限公司 | 合金组件及其制备方法和应用 |
CN108265204A (zh) * | 2018-01-24 | 2018-07-10 | 安徽浩丰实业有限公司 | 一种含钴的活塞材料及其制备方法 |
CN109826900B (zh) * | 2019-02-13 | 2021-02-02 | 江苏汉苏机械股份有限公司 | 运行平稳的活塞杆组件 |
Family Cites Families (24)
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US2357450A (en) * | 1941-01-18 | 1944-09-05 | Nat Smelting Co | Aluminum alloy |
GB563994A (en) * | 1941-12-01 | 1944-09-08 | Nat Smelting Co | Improvements in or relating to aluminium base alloys |
GB1431895A (en) * | 1972-06-30 | 1976-04-14 | Alcan Res & Dev | Production of aluminium alloy products |
GB1583019A (en) * | 1978-05-31 | 1981-01-21 | Ass Eng Italia | Aluminium alloys and combination of a piston and cylinder |
AU536976B2 (en) * | 1980-09-10 | 1984-05-31 | Comalco Limited | Aluminium-silicon alloys |
US4347076A (en) * | 1980-10-03 | 1982-08-31 | Marko Materials, Inc. | Aluminum-transition metal alloys made using rapidly solidified powers and method |
US4647321A (en) * | 1980-11-24 | 1987-03-03 | United Technologies Corporation | Dispersion strengthened aluminum alloys |
US4419143A (en) * | 1981-11-16 | 1983-12-06 | Nippon Light Metal Company Limited | Method for manufacture of aluminum alloy casting |
JPS58204147A (ja) * | 1982-05-14 | 1983-11-28 | Nissan Motor Co Ltd | 耐熱アルミニウム合金 |
FR2529909B1 (fr) * | 1982-07-06 | 1986-12-12 | Centre Nat Rech Scient | Alliages amorphes ou microcristallins a base d'aluminium |
US4435213A (en) * | 1982-09-13 | 1984-03-06 | Aluminum Company Of America | Method for producing aluminum powder alloy products having improved strength properties |
US4592781A (en) * | 1983-01-24 | 1986-06-03 | Gte Products Corporation | Method for making ultrafine metal powder |
EP0144898B1 (de) * | 1983-12-02 | 1990-02-07 | Sumitomo Electric Industries Limited | Aluminiumlegierungen und Verfahren zu ihrer Herstellung |
JPS60131944A (ja) * | 1983-12-19 | 1985-07-13 | Sumitomo Electric Ind Ltd | 超耐熱耐摩耗アルミニウム合金およびその製造用複合粉末 |
US4734130A (en) * | 1984-08-10 | 1988-03-29 | Allied Corporation | Method of producing rapidly solidified aluminum-transition metal-silicon alloys |
JPS6148551A (ja) * | 1984-08-13 | 1986-03-10 | Sumitomo Light Metal Ind Ltd | 高温強度に優れたアルミニウム合金成形材 |
JPS61238947A (ja) * | 1985-04-16 | 1986-10-24 | Sumitomo Light Metal Ind Ltd | Al−Si系合金素材の製造方法 |
US4732610A (en) * | 1986-02-24 | 1988-03-22 | Aluminum Company Of America | Al-Zn-Mg-Cu powder metallurgy alloy |
JPS6311642A (ja) * | 1986-06-30 | 1988-01-19 | Showa Alum Corp | ヒ−トロ−ラ−用アルミニウム合金 |
US4847048A (en) * | 1986-07-21 | 1989-07-11 | Ryobi Limited | Aluminum die-casting alloys |
JPS6342344A (ja) * | 1986-08-06 | 1988-02-23 | Honda Motor Co Ltd | 高温強度特性に優れた粉末冶金用Al合金 |
CH673242A5 (de) * | 1986-08-12 | 1990-02-28 | Bbc Brown Boveri & Cie | |
US4729790A (en) * | 1987-03-30 | 1988-03-08 | Allied Corporation | Rapidly solidified aluminum based alloys containing silicon for elevated temperature applications |
FR2624137B1 (fr) * | 1987-12-07 | 1990-06-15 | Cegedur | Pieces en alliage d'aluminium, telles que bielles notamment, ayant une resistance a la fatigue amelioree et procede de fabrication |
-
1988
- 1988-09-26 FR FR8812982A patent/FR2636974B1/fr not_active Expired - Fee Related
-
1989
- 1989-09-20 KR KR1019890013512A patent/KR930003602B1/ko not_active IP Right Cessation
- 1989-09-20 US US07/409,694 patent/US4963322A/en not_active Expired - Fee Related
- 1989-09-21 JP JP1246233A patent/JPH0819496B2/ja not_active Expired - Lifetime
- 1989-09-21 DD DD89332869A patent/DD284904A5/de not_active IP Right Cessation
- 1989-09-21 EP EP89420361A patent/EP0362086B1/de not_active Expired - Lifetime
- 1989-09-21 ES ES198989420361T patent/ES2042048T3/es not_active Expired - Lifetime
- 1989-09-21 AT AT89420361T patent/ATE90397T1/de active
- 1989-09-21 DE DE8989420361T patent/DE68906999T2/de not_active Expired - Fee Related
- 1989-09-22 HU HU894979A patent/HUT53680A/hu unknown
- 1989-09-22 IL IL91738A patent/IL91738A0/xx unknown
- 1989-09-22 DK DK468489A patent/DK468489A/da not_active Application Discontinuation
- 1989-09-22 FI FI894499A patent/FI894499A/fi not_active Application Discontinuation
- 1989-09-25 BR BR898904844A patent/BR8904844A/pt not_active IP Right Cessation
- 1989-09-25 CN CN89107481A patent/CN1041399A/zh active Pending
- 1989-09-25 YU YU185389A patent/YU185389A/sh unknown
-
1990
- 1990-07-23 US US07/556,185 patent/US4992242A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FI894499A (fi) | 1990-03-27 |
JPH0819496B2 (ja) | 1996-02-28 |
DD284904A5 (de) | 1990-11-28 |
KR900004951A (ko) | 1990-04-13 |
FR2636974A1 (fr) | 1990-03-30 |
US4992242A (en) | 1991-02-12 |
DK468489A (da) | 1990-03-27 |
IL91738A0 (en) | 1990-06-10 |
FR2636974B1 (fr) | 1992-07-24 |
YU185389A (sh) | 1992-12-21 |
EP0362086A1 (de) | 1990-04-04 |
DE68906999T2 (de) | 1993-09-16 |
ES2042048T3 (es) | 1993-12-01 |
JPH02232324A (ja) | 1990-09-14 |
ATE90397T1 (de) | 1993-06-15 |
KR930003602B1 (ko) | 1993-05-08 |
DE68906999D1 (de) | 1993-07-15 |
FI894499A0 (fi) | 1989-09-22 |
DK468489D0 (da) | 1989-09-22 |
HUT53680A (en) | 1990-11-28 |
CN1041399A (zh) | 1990-04-18 |
BR8904844A (pt) | 1990-05-08 |
US4963322A (en) | 1990-10-16 |
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