EP0362086B1 - Procédé de fabrication de pièces en alliage d'aluminium gardant une bonne résistance à la fatigue après un maintien prolongé à chaud - Google Patents
Procédé de fabrication de pièces en alliage d'aluminium gardant une bonne résistance à la fatigue après un maintien prolongé à chaud 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
- 238000000034 method Methods 0.000 title claims abstract description 23
- 230000008569 process Effects 0.000 title claims abstract description 11
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 8
- 230000002035 prolonged effect Effects 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 30
- 239000000956 alloy Substances 0.000 claims abstract description 30
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 24
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 22
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 17
- 239000010949 copper Substances 0.000 claims abstract description 9
- 229910052742 iron Inorganic materials 0.000 claims abstract description 9
- 239000011777 magnesium Substances 0.000 claims abstract description 9
- 229910052802 copper Inorganic materials 0.000 claims abstract description 8
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 8
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 7
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000010703 silicon Substances 0.000 claims abstract description 7
- 238000004519 manufacturing process Methods 0.000 claims abstract description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 4
- 238000007711 solidification Methods 0.000 claims abstract 5
- 230000008023 solidification Effects 0.000 claims abstract 5
- 238000000137 annealing Methods 0.000 claims abstract 2
- 238000010438 heat treatment Methods 0.000 claims abstract 2
- 239000011572 manganese Substances 0.000 claims description 21
- 229910052748 manganese Inorganic materials 0.000 claims description 20
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 17
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 8
- 238000007792 addition Methods 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 claims description 2
- 239000000758 substrate Substances 0.000 claims description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract description 5
- 238000000889 atomisation Methods 0.000 description 6
- 238000004663 powder metallurgy Methods 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 238000005259 measurement Methods 0.000 description 5
- 238000009987 spinning Methods 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 238000007712 rapid solidification Methods 0.000 description 4
- 238000009718 spray deposition Methods 0.000 description 4
- 230000015556 catabolic process Effects 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 240000008042 Zea mays Species 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 229940082150 encore Drugs 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000002074 melt spinning Methods 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 235000009508 confectionery Nutrition 0.000 description 1
- -1 copper and magnesium Chemical class 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- DSGIMNDXYTYOBX-UHFFFAOYSA-N manganese zirconium Chemical compound [Mn].[Zr] DSGIMNDXYTYOBX-UHFFFAOYSA-N 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
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)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (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)
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 |
|---|---|---|---|
| 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 |
| FR8812982 | 1988-09-26 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0362086A1 EP0362086A1 (fr) | 1990-04-04 |
| EP0362086B1 true EP0362086B1 (fr) | 1993-06-09 |
Family
ID=9370672
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP89420361A Expired - Lifetime EP0362086B1 (fr) | 1988-09-26 | 1989-09-21 | Procédé de fabrication de pièces en alliage d'aluminium gardant une bonne résistance à la fatigue après un maintien prolongé à chaud |
Country Status (16)
| Country | Link |
|---|---|
| US (2) | US4963322A (ko) |
| EP (1) | EP0362086B1 (ko) |
| JP (1) | JPH0819496B2 (ko) |
| KR (1) | KR930003602B1 (ko) |
| CN (1) | CN1041399A (ko) |
| AT (1) | ATE90397T1 (ko) |
| BR (1) | BR8904844A (ko) |
| DD (1) | DD284904A5 (ko) |
| DE (1) | DE68906999T2 (ko) |
| DK (1) | DK468489A (ko) |
| ES (1) | ES2042048T3 (ko) |
| FI (1) | FI894499A (ko) |
| FR (1) | FR2636974B1 (ko) |
| HU (1) | HUT53680A (ko) |
| IL (1) | IL91738A0 (ko) |
| YU (1) | YU185389A (ko) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5368629A (en) * | 1991-04-03 | 1994-11-29 | Sumitomo Electric Industries, Ltd. | Rotor for oil pump made of aluminum alloy and method of manufacturing the same |
| US5372775A (en) * | 1991-08-22 | 1994-12-13 | Sumitomo Electric Industries, Ltd. | Method of preparing particle composite alloy having an aluminum matrix |
| DE69326290T2 (de) * | 1992-06-29 | 2000-01-27 | Sumitomo Electric Industries | Ölpumpe aus Aluminiumlegierungen |
| EP0657553A1 (en) * | 1993-11-10 | 1995-06-14 | Sumitomo Electric Industries, Ltd. | Nitrogenous aluminum-silicon powder metallurgical alloy |
| 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)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| DE3481322D1 (de) * | 1983-12-02 | 1990-03-15 | Sumitomo Electric Industries | 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 (ko) * | 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 US US07/409,694 patent/US4963322A/en not_active Expired - Fee Related
- 1989-09-20 KR KR1019890013512A patent/KR930003602B1/ko not_active IP Right Cessation
- 1989-09-21 ES ES198989420361T patent/ES2042048T3/es not_active Expired - Lifetime
- 1989-09-21 DD DD89332869A patent/DD284904A5/de not_active IP Right Cessation
- 1989-09-21 AT AT89420361T patent/ATE90397T1/de active
- 1989-09-21 EP EP89420361A patent/EP0362086B1/fr not_active Expired - Lifetime
- 1989-09-21 JP JP1246233A patent/JPH0819496B2/ja not_active Expired - Lifetime
- 1989-09-21 DE DE8989420361T patent/DE68906999T2/de not_active Expired - Fee Related
- 1989-09-22 FI FI894499A patent/FI894499A/fi not_active Application Discontinuation
- 1989-09-22 IL IL91738A patent/IL91738A0/xx unknown
- 1989-09-22 HU HU894979A patent/HUT53680A/hu unknown
- 1989-09-22 DK DK468489A patent/DK468489A/da not_active Application Discontinuation
- 1989-09-25 CN CN89107481A patent/CN1041399A/zh active Pending
- 1989-09-25 BR BR898904844A patent/BR8904844A/pt not_active IP Right Cessation
- 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 |
|---|---|
| DK468489A (da) | 1990-03-27 |
| DE68906999D1 (de) | 1993-07-15 |
| FI894499A (fi) | 1990-03-27 |
| FI894499A0 (fi) | 1989-09-22 |
| JPH0819496B2 (ja) | 1996-02-28 |
| DE68906999T2 (de) | 1993-09-16 |
| FR2636974A1 (fr) | 1990-03-30 |
| JPH02232324A (ja) | 1990-09-14 |
| IL91738A0 (en) | 1990-06-10 |
| EP0362086A1 (fr) | 1990-04-04 |
| DK468489D0 (da) | 1989-09-22 |
| ES2042048T3 (es) | 1993-12-01 |
| FR2636974B1 (fr) | 1992-07-24 |
| HUT53680A (en) | 1990-11-28 |
| BR8904844A (pt) | 1990-05-08 |
| CN1041399A (zh) | 1990-04-18 |
| KR930003602B1 (ko) | 1993-05-08 |
| KR900004951A (ko) | 1990-04-13 |
| YU185389A (sh) | 1992-12-21 |
| US4963322A (en) | 1990-10-16 |
| DD284904A5 (de) | 1990-11-28 |
| US4992242A (en) | 1991-02-12 |
| ATE90397T1 (de) | 1993-06-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0362086B1 (fr) | Procédé de fabrication de pièces en alliage d'aluminium gardant une bonne résistance à la fatigue après un maintien prolongé à chaud | |
| EP2475794B1 (en) | Aluminum alloy casting and production method thereof | |
| JP4923498B2 (ja) | 高強度・低比重アルミニウム合金 | |
| FR2573777A1 (fr) | Alliage d'aluminium resistant a la chaleur, a haute resistance, et procede pour fabriquer un element porteur constitue de cet alliage | |
| EP0265307B1 (fr) | Procédé de fabrication de pièces en alliage d'aluminium hypersilicié obtenu à partir de poudres refroidies à très grande vitesse de refroidissement | |
| RU2695852C2 (ru) | α-β ТИТАНОВЫЙ СПЛАВ | |
| JP4764094B2 (ja) | 耐熱性Ａｌ基合金 | |
| FR2633942A1 (fr) | Superalliage a base de nickel resistant aux pendillements par fatigue et son procede de fabrication | |
| EP0320417B1 (fr) | Pièces en alliage d'aluminium, telles que bielles notamment, ayant une résistance à la fatigue améliorée et procédé de fabrication | |
| JPH03104832A (ja) | クロムとケイ素で改変されたγ‐チタン‐アルミニウム合金 | |
| JP3173452B2 (ja) | 耐摩耗性被覆部材及びその製造方法 | |
| CN115233030A (zh) | 一种焊接性能优异的铜合金及其制备方法 | |
| EP0430754B1 (fr) | Alliage inoxydable à mémoire de forme et procédé d'élaboration d'un tel alliage | |
| JPH07197165A (ja) | 高耐磨耗性快削アルミニウム合金とその製造方法 | |
| CA2444175C (fr) | Acier a outils a tenacite renforcee, procede de fabrication de pieces dans cet acier et pieces obtenues | |
| JPH0457738B2 (ko) | ||
| JPH02247348A (ja) | 引張強度、延性および疲労強度にすぐれた耐熱性アルミニウム合金 | |
| JP4704720B2 (ja) | 高温疲労特性に優れた耐熱性Ａｌ基合金 | |
| JPH11269592A (ja) | 焼入れ感受性の低いＡｌ−過共晶Ｓｉ合金およびその製造方法 | |
| JP3245652B2 (ja) | 高温用アルミニウム合金及びその製造方法 | |
| JPH02147195A (ja) | コバルト・クロム基合金溶接材料の製造方法 | |
| JP2746390B2 (ja) | 引張および疲労強度にすぐれたアルミニウム合金の製造方法 | |
| Reddy et al. | Effect of cold rolling on the porosity, hardness properties of the spray deposited Al-18% Pb And Al-22% Pb Alloys | |
| EP0092629A1 (fr) | Procédé de fabrication de barres et de tubes en aciers à hautes caractéristiques mécaniques | |
| JP2572832B2 (ja) | 焼結用Ａｌ基合金粉末 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH DE ES FR GB GR IT LI LU NL SE |
|
| 17P | Request for examination filed |
Effective date: 19900420 |
|
| 17Q | First examination report despatched |
Effective date: 19920513 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH DE ES FR GB GR IT LI LU NL SE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 19930609 Ref country code: AT Effective date: 19930609 |
|
| REF | Corresponds to: |
Ref document number: 90397 Country of ref document: AT Date of ref document: 19930615 Kind code of ref document: T |
|
| ITF | It: translation for a ep patent filed | ||
| GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19930609 |
|
| REF | Corresponds to: |
Ref document number: 68906999 Country of ref document: DE Date of ref document: 19930715 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19930930 Ref country code: LI Effective date: 19930930 Ref country code: CH Effective date: 19930930 Ref country code: BE Effective date: 19930930 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2042048 Country of ref document: ES Kind code of ref document: T3 |
|
| BERE | Be: lapsed |
Owner name: PECHINEY RECHERCHE Effective date: 19930930 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| 26N | No opposition filed | ||
| EAL | Se: european patent in force in sweden |
Ref document number: 89420361.1 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19970718 Year of fee payment: 9 Ref country code: GB Payment date: 19970718 Year of fee payment: 9 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19970719 Year of fee payment: 9 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19970911 Year of fee payment: 9 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19970930 Year of fee payment: 9 Ref country code: ES Payment date: 19970930 Year of fee payment: 9 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19980921 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19980922 Ref country code: ES Free format text: LAPSE BECAUSE OF THE APPLICANT RENOUNCES Effective date: 19980922 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990401 |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19980921 |
|
| EUG | Se: european patent has lapsed |
Ref document number: 89420361.1 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990531 |
|
| NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee |
Effective date: 19990401 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19990701 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20001102 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050921 |