![]() Aluminum base alloy and method of manufacturing parts from aluminum alloys
专利摘要:
Aluminium alloy articles with an improved fatigue strength and process for their manufacture. …<??>These articles are made of an alloy containing, by weight, 11 to 22% of silicon, 2 to 5% of iron, 0.5 to 4% of copper, 0.2 to 1.5% of magnesium, having a characteristic of containing 0.4 to 1.5% of zirconium. …<??>The manufacturing process consists in subjecting the alloy in molten state to a means for fast solidification, in forming it, in subjecting it to a heat treatment between 480 and 530 DEG C followed by a water quenching and by annealing between 150 and 200 DEG C. …<??>These articles find their application especially in the form of connecting rods and gudgeon pins. 公开号:SU1722234A3 申请号:SU884356936 申请日:1988-12-05 公开日:1992-03-23 发明作者:Фор Жан-Франсуа 申请人:Сежедюр Сосьете Де Трансформасьон Де Лъалюминиум Пэшине (Фирма); IPC主号:
专利说明:
The invention relates to metallurgy, in particular, to details of aluminum alloy having increased fatigue strength, and to a method for manufacturing said parts. The purpose of the invention is to increase fatigue strength. Parts made of aluminum alloys containing wt.%: Silicon 11-22; iron 2-5; copper 0.5-4; Magnesium 0.2-1.5, characterized by that they also contain zirconium 0.4-1.5, aluminum - the rest .. After preparation of the alloy, it is melted at a temperature above 900 ° C to eliminate any phenomenon — premature precipitation followed by exposure to a means of rapid solidification. There are several ways to effect rapid curing: either by spraying the molten metal with gas or by mechanical spraying followed by cooling in a gas (air, helium, argon), which results in powders with a particle size of less than 400 / gm, which are then molded by cold or hot compaction in a uniaxial or an isostatic press followed by drawing and / or forging; or the ejection of the molten alloy onto the cooled metal surface, by the Anglo-Saxons, this technology is determined by the expression melt spinning or planar flow casting to produce strips less than 100 / W thick, which are then molded by the specified compaction; or else by ejecting the molten sprayed alloy in the gas stream onto the boundary layer, this technology is also called spray deposition, which leads to coherent deposition that is sufficiently malleable to be molded, for example, by forging, drawing or punching, In order to further enhance the deposition structure, the details, after with with possible mechanical treatment, heat treatment is carried out at 430-520 ° C for 1-10 hours, then quenching with water before being subjected to tempering at 155-195 ° C for 2-32 hours, which improves their mechanical characteristics. Example. Used six alloys are given in table. one. Alloys 1-3 were obtained by powder metallurgy, i.e. they are melted at 900 ° C, then sprayed under a nitrogen atmosphere in the form of particles with a grain size distribution of 300 / {m, then compacted under a pressure of 300 MPa in an isostatic press, and wire in the form of a rod 40 mm in diameter. For alloys 4-6, spray deposition technology is used, during which precipitation is obtained in the form of a cylindrical billet, which is then transformed by drawing into a rod with a diameter of 40 mm. The rods obtained in one way or another are then treated for 2 hours at 430-520 ° C, then quenched with water and subjected to temperature treatment at 155-195 ° C for 8 hours. The samples are measured on the Young's modulus, the conditional elastic limit at 0.2%, the load at break and elongation successively at 20 ° C and at 150 ° C after 100 hours of incubation, as well as the measurement of the fatigue strength limit at 20 ° C after 107 cycles and the fatigue strength coefficient determined by the ratio of the fatigue strength limit to the load at break. The results are given in Table. 2 There is a marked increase in fatigue strength from 150 to 192 MPa with the addition of zirconium. Similar results were obtained for parts manufactured using spray deposition and melt spining or planar flow casting. Before the heat treatment, the alloy AI + 18% Si + 3% Fe + 3% Cu + 1% Mg + 1% Zr has the following mechanical characteristics: Ro2 160 MPa; RM 250 MPa; And 8%; fatigue strength limit at 10 cycles at 20 ° С 110 MPa. 15
权利要求:
Claims (3) [1] 1. An aluminum-based alloy mainly for the manufacture of connecting rods containing silicon, iron, copper, magnesium, characterized in that, in order to increase fatigue strength, it additionally contains zirconium with the following component content, wt%: silicon 12-20; iron2,8-5; copper 1-3; magnesium 0.5-1.5; zirconium 0.45-1.4; aluminum - the rest. [2] 2. Method of manufacturing parts made of aluminum alloys, mainly connecting rods, including the impact of the means rapid solidification of the alloy and molding, characterized in that, in order to increase the fatigue strength, after molding, heat treatment is additionally carried out, including quenching from 430520 ° Set and tempering at 155-195 ° C, [3] 3. A method according to claim 2, characterized in that spraying is used as a means of rapid solidification. Table 1 table 2
类似技术:
公开号 | 公开日 | 专利标题 KR101223546B1|2013-01-18|An al-si-mg-zn-cu alloy for aerospace and automotive castings EP0572683B1|1999-12-08|Method for casting aluminum alloy casting and aluminum alloy casting SU1722234A3|1992-03-23|Aluminum base alloy and method of manufacturing parts from aluminum alloys US4853179A|1989-08-01|Method of manufacturing heat resistant, high-strength structural members of sintered aluminum alloy US3462248A|1969-08-19|Metallurgy JPH05179384A|1993-07-20|High strength and high toughness aluminum alloy manufactured by spray deposition method US4992242A|1991-02-12|Aluminum alloy with good fatigue strength US4732610A|1988-03-22|Al-Zn-Mg-Cu powder metallurgy alloy HUT53681A|1990-11-28|Process for producing high-strength al-zn-mg-cu alloys with good plastic properties JP4923498B2|2012-04-25|High strength and low specific gravity aluminum alloy US4104089A|1978-08-01|Die-cast aluminum alloy products JP5758402B2|2015-08-05|Cast parts made of copper aluminum alloy with high mechanical strength and high heat-resistant creep resistance JP4764094B2|2011-08-31|Heat-resistant Al-based alloy JP4704720B2|2011-06-22|Heat-resistant Al-based alloy with excellent high-temperature fatigue properties JPH05179383A|1993-07-20|Aluminum alloy having fine crystallized grain manufacture by spray deposition method JP3509163B2|2004-03-22|Manufacturing method of magnesium alloy member Webster et al.1981|Mechanical properties and microstructure of argon atomized aluminum-lithium powder metallurgy alloys JPH05179387A|1993-07-20|High strength and high toughness aluminum alloy manufactured by spray deposition method JP2856251B2|1999-02-10|High-strength wear-resistant Al-Si alloy forged member having low coefficient of thermal expansion and method for producing the same JP3245652B2|2002-01-15|High temperature aluminum alloy and method for producing the same JP2021070833A|2021-05-06|Manufacturing material of aluminum alloy forged material JPH05179385A|1993-07-20|High strength and high toughness aluminum alloy manufactured by spray deposition method EP0222002B1|1992-09-16|Alloy toughening method JP2020007596A|2020-01-16|Aluminum alloy material JP2020007595A|2020-01-16|Aluminum alloy material
同族专利:
公开号 | 公开日 IL88586D0|1989-07-31| CN1034585A|1989-08-09| AT66023T|1991-08-15| HUT50885A|1990-03-28| FI885657A|1989-06-08| FR2624137A1|1989-06-09| JPH01198444A|1989-08-10| JPH0617550B2|1994-03-09| KR890010260A|1989-08-07| PL276247A1|1989-06-12| ES2024044B3|1992-02-16| BR8806421A|1989-08-22| FR2624137B1|1990-06-15| YU220988A|1990-04-30| FI885657A0|1988-12-05| US4923676A|1990-05-08| EP0320417B1|1991-08-07| DD276109A5|1990-02-14| DK679288D0|1988-12-06| EP0320417A1|1989-06-14| DE3864128D1|1991-09-12| DK679288A|1989-06-08|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题 GB388109A|1930-10-03|1933-02-23|Skoda Works Plzen Ltd Company|Aluminium alloys for pistons| US1921195A|1931-07-14|1933-08-08|Aluminum Co Of America|Aluminum silicon alloy| GB563617A|1941-12-04|1944-08-23|Fairweather Harold G C|Improvements in or relating to aluminium base alloys| AU536976B2|1980-09-10|1984-05-31|Comalco Limited|Aluminium-silicon alloys| EP0144898B1|1983-12-02|1990-02-07|Sumitomo Electric Industries Limited|Aluminum alloy and method for producing same| US4734130A|1984-08-10|1988-03-29|Allied Corporation|Method of producing rapidly solidified aluminum-transition metal-silicon alloys| JPS63192838A|1987-02-04|1988-08-10|Showa Denko Kk|Aluminum-alloy powder compact excellent in creep resisting characteristic|FR2636974B1|1988-09-26|1992-07-24|Pechiney Rhenalu|ALUMINUM ALLOY PARTS RETAINING GOOD FATIGUE RESISTANCE AFTER EXTENDED HOT HOLDING AND METHOD FOR MANUFACTURING SUCH PARTS| EP0533950B1|1991-04-03|1997-08-20|Sumitomo Electric Industries, Ltd.|Rotor made of aluminum alloy for oil pump and method of manufacturing said rotor| JP3021487U|1995-08-08|1996-02-20|株式会社スリーリング|Car armrest cover| DE69814498T2|1997-02-12|2003-11-20|Yamaha Motor Co Ltd|Pistons for an internal combustion engine and process for its manufacture| US7699595B2|2004-07-19|2010-04-20|R + S Technik Gmbh|Method and apparatus for molding a laminated trim component without use of slip frame| CN101775530B|2010-03-04|2012-03-28|安徽省恒泰动力科技有限公司|Hypereutectic al-si alloy piston material| CN106756293B|2016-12-20|2019-03-01|江苏豪然喷射成形合金有限公司|A kind of preparation method of ferro-silicon-aluminium copper magnesium alloy| CN107377973A|2017-08-30|2017-11-24|广东美芝制冷设备有限公司|Alloy components and its preparation method and application| CN108715957A|2018-05-31|2018-10-30|益阳仪纬科技有限公司|A kind of automotive transmission shell high-strength aluminum alloy composite material and its preparation process| DE102018117418A1|2018-07-18|2020-01-23|Friedrich Deutsch Metallwerk Gesellschaft M.B.H.|Die-cast aluminum alloy|
法律状态:
优先权:
[返回顶部]
申请号 | 申请日 | 专利标题 FR8717674A|FR2624137B1|1987-12-07|1987-12-07|ALUMINUM ALLOY PARTS, SUCH AS CONNECTING RODS, WITH IMPROVED FATIGUE RESISTANCE AND METHOD OF MANUFACTURE| 相关专利
Sulfonates, polymers, resist compositions and patterning process
Washing machine
Washing machine
Device for fixture finishing and tension adjusting of membrane
Structure for Equipping Band in a Plane Cathode Ray Tube
Process for preparation of 7 alpha-carboxyl 9, 11-epoxy steroids and intermediates useful therein an
国家/地区
|