DK141373B - Aluminum-zinc alloy, preferably for use as a bearing material, and process for making it. - Google Patents
Aluminum-zinc alloy, preferably for use as a bearing material, and process for making it. Download PDFInfo
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- DK141373B DK141373B DK597570AA DK597570A DK141373B DK 141373 B DK141373 B DK 141373B DK 597570A A DK597570A A DK 597570AA DK 597570 A DK597570 A DK 597570A DK 141373 B DK141373 B DK 141373B
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- DK
- Denmark
- Prior art keywords
- aluminum
- content
- nickel
- alloy
- zinc
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/04—Alloys based on zinc with aluminium as the next major constituent
-
- 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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
(11) FREMLÆGGELSESSKRIFT 141373 DANMARK om Intet.’C 22 C 21/00 • (21) Ansøgning nr. 5975/70 (22) Indleverat den 24. nOV. 1970 (23) Løbedsg 24. nov. 1970 (44) Ansøgningen fremlagt og(11) PRESENTATION 141373 DENMARK on Nothing.'C 22 C 21/00 • (21) Application No 5975/70 (22) Filed on 24 Nov. 1970 (23) Løbedsg Nov 24 1970 (44) The application presented and
fremlæggeteeeekriftet offentliggjort den 5· tnar . I98Othe presentation paper published on 5 January. I98O
DIREKTORATET FORDIRECTORATE OF
PATENT-OG VAREMÆRKEVÆSENET (3°> Prioritet begæret fra denPATENT AND TRADEMARKET (3 °> Priority requested from it
5. feb. 1970, 1045/70, ATFeb 5 1970, 1045/70, AT
(71) VEREINIGTE OESTERREICHISCHE EISEN- UND STAHLWERKE AKTIENGESELLSGHAFT, Muldenetrasee 5> Linz, AT.(71) UNITED AUSTRALIAN REQUIREMENTS AND STAHLWERKE AKTIENGESELLSGHAFT, Muldenetrasee 5> Linz, AT.
(72) Opfinder: Erich _Pelzel, Wettersteinstrasse D-8031 Puchheim* (ved Muenchen), DE.(72) Inventor: Erich _Pelzel, Wettersteinstrasse D-8031 Puchheim * (near Munich), DE.
(74) Fuldmægtig under sagens behandling:(74) Plenipotentiary in the proceedings:
Firmaet Chas. Hude.The company Chas. Hude.
(54) Legering på aluminium-zinkbasis, fortrinsvis til brug som lejemateriale, og fremgangsmåde til fremstilling deraf.(54) Aluminum-zinc alloy, preferably for use as a bearing material, and process for making it.
Den foreliggende opfindelse angår en legering på aluminium-zinkbasis med et aluminiumindhold på 38-75%, fortrinsvis 50-65%, et indhold af nikkel og eventuelt et indhold af magnesium og kobber og resten zink, og en fremgangsmåde til fremstilling deraf.The present invention relates to an aluminum-zinc alloy having an aluminum content of 38-75%, preferably 50-65%, a content of nickel and optionally a content of magnesium and copper and the residual zinc, and a process for their preparation.
Sådanne legeringer anvendes først og fremmest som lejematerialer til lejeskåle eller lignende lejedele, hvorhos disse fremstilles ved hjælp af støbning eller ved hjælp af passende formgivning ud fra valsede plader. I hvert tilfælde fremstilles først et stykke støbegods, hvis struktur i vid udstrækning bestemmer lejets egenskaber.Such alloys are primarily used as bearing materials for bearing bowls or similar bearing parts, whereby they are manufactured by casting or by suitable shaping from rolled sheets. In each case, a piece of castings is first manufactured, the structure of which largely determines the properties of the bed.
2 1413732 141373
De indledningsvis nævnte legeringer på aluminium-zinkbasis har på grund af deres store størkningsinterval tilbøjelighed til omvendt bloksejgring, og som følge deraf indtræder interkrystallinsk porøsitet. Sådanne porer er ikke, som man tidligere antog, gunstige for lejeslidforholdene. Porøse lejer, der er gennemvædet med olie, er kun selvsmørende, når porer med en bestemt størrelse er regelmæssigt fordelt over lejeslidfladen. Er dette ikke tilfældet, fjerner en glideflades porøse steder oliefilmen på de tætte steder, hvilket kan føre til rivning af lejet.The aluminum-zinc-based alloys initially mentioned, due to their high solidification range, are prone to reverse block annealing and, as a result, intercrystalline porosity occurs. Such pores are not, as was previously assumed, favorable for the bearing wear conditions. Porous bearings that are soaked with oil are only self-lubricating when pores of a certain size are regularly distributed over the bearing wear surface. If this is not the case, the porous locations of a sliding surface remove the oil film in the dense locations, which may lead to tearing of the bearing.
Dét er kendt, at man i tilfælde af simpelt formede stykker støbegods af aluminiumzinklegeringer ved hjælp af meget hurtig afkøling af disse ved støbningen opnår gode mekaniske egenskaber. Det har imidlertid hidtil ikke været muligt at udnytte de ved hjælp af hurtig afkøling af støbegodset opnåelige fordele, da også den omvendte bloksejgring tager til med tiltagende størkningshastighed.og porer derfor også optræder i forøget antal i støbegodsstykkerne. Tilbøjeligheden til poredannelse kan ganske vist formindskes ved hjælp af støbetekniske foranstaltninger, såsom ved forøget anbringelse af stigrør og støbetappe og ved at holde disse flydende. Metallet, der stivner i stigrørene og støbetappene, skal imidlertid skilles fra det egentlige støbte produkt, f. eks. ved hjælp af en skærebrænder, og ender som skrot. Da metalmængden, der størkner i stigrørene og støbetappene, udgør en betydelig del af den samlede metalmængde, som skal udstøbes til fremstilling af et støbt produkt, har de af skrotmængden forårsagede ulemper og større omkostninger ved støbning stor betydning. Bortset fra sådanne økonomiske overvejelser fører de støbetekniske foranstaltninger desuden ikke sikkert nok til et vellykket resultat.It is known that in case of simply shaped pieces of aluminum zinc alloy castings, by virtue of very rapid cooling of these during casting, good mechanical properties are obtained. However, it has not hitherto been possible to exploit the advantages obtained by the rapid cooling of the castings, as the reverse block rise also increases with increasing solidification speed and therefore pores also appear in increased numbers in the castings. Admittedly, the propensity for pore formation can be diminished by casting techniques, such as by increased placement of riser and casting pins and by keeping them fluid. However, the metal that solidifies in the risers and molding pins must be separated from the actual molded product, for example by means of a cutting burner, and ends up as scrap. Since the amount of metal that solidifies in the riser pipes and casting pins constitutes a significant portion of the total amount of metal to be cast to produce a molded product, the disadvantages caused by the scrap quantity and greater cost of casting are of great importance. Apart from such financial considerations, the casting technical measures also do not lead to a successful outcome.
Opfindelsen har til formål at afhjælpe disse ulemper, og legeringen ifølge opfindelsen af den i indledningen angivne art er med henblik herpå ejendommelig ved, at nikkelindholdet andrager mindst 0,05% og højst svarer til forløbet af den eutektiske rende i systemet aluminium-zink-nikkel, hvorhos det maksimale indhold af nikkel ved 38% aluminium andrager 0,6%, ved 50% aluminium 1,1%, ved 60% aluminium 1,7%, ved 70% aluminium 2,4%, ved 75% aluminium 2,8% og bestandig forløber mellem de angivne værdier.The invention aims to overcome these disadvantages, and the alloy according to the invention of the kind mentioned in the preamble is characterized in that the nickel content is at least 0.05% and at most corresponds to the course of the eutectic gutter in the aluminum-zinc-nickel system. , where the maximum content of nickel at 38% aluminum is 0.6%, at 50% aluminum 1.1%, at 60% aluminum 1.7%, at 70% aluminum 2.4%, at 75% aluminum 2, 8% and constant runs between the values stated.
3 U13733 U1373
Herved opnås en porefri og finkornet struktur af det støbte produkt og en forøgelse af dets hårdhed.This results in a pore-free and fine-grained structure of the molded product and an increase in its hardness.
Legeringen kan fordelagtigt yderligere indholde 0,005-0,05% magnesium, hvorved der opnås en yderligere kornformindskelse. Endvidere kan kobber være indeholdt i en mængde på højst 6,5% af aluminiumindholdet. Denne yderligere bestanddel bevirker ligeledes en hårdhedsforøgelse.Advantageously, the alloy may further contain 0.005-0.05% magnesium, thereby obtaining a further grain reduction. Furthermore, copper may be contained in an amount not exceeding 6.5% of the aluminum content. This additional component also causes a hardness increase.
Fremgangsmåden til fremstilling af legeringen ifølge opfindelsen er ejendommelig ved, at udgangsmaterialerne har en renhed på mindst 99,5% og er fri for grundstoffer, der danner uopløselige forbindelser med nikkel, såsom silicium eller bor, samt er fri for grundstoffer, der udkrystalliserer primært og som nåle, såsom jern, mangan, titan, vanadin, molybdæn, wolfram og carbon.The process for preparing the alloy of the invention is characterized in that the starting materials have a purity of at least 99.5% and are free of elements which form insoluble compounds with nickel, such as silicon or boron, and are free of elements which crystallize primarily and such as needles such as iron, manganese, titanium, vanadium, molybdenum, tungsten and carbon.
Magnesium indføres eventuelt hensigtsmæssigt i form af en specifikt tung forlegering, fortrinsvis i form af en legering med 5% aluminium, 3% magnesium og 92% zink..Optionally, magnesium is suitably introduced in the form of a specific heavy alloy, preferably in the form of an alloy with 5% aluminum, 3% magnesium and 92% zinc.
Ved fremstilling af formstykker ud fra legeringen ifølge opfindelsen er det fordelagtigt, at varmebortledningen ved størkningen deraf holdes under 0,2 kal/sek/g, fortrinsvis mellem 0,05-0,1 kal/sek/g.In the manufacture of moldings from the alloy of the invention, it is advantageous that the heat dissipation during solidification thereof be kept below 0.2 cal / sec / g, preferably between 0.05-0.1 cal / sec / g.
Formstykker, der er fremstillet ud fra legeringen ifølge opfindelsen, kan hurtigt afkøles fra temperaturer over 350°C til stuetemperatur og derefter varmebehandles i et tidsrum mellem 0,25 og 8 timer ved temperaturer mellem 90°C og 275°C. Ved hjælp af denne varmebehandling frembringes en udskillelse af rene zinkkrystaller fra legeringen i findélt form, hvorved notslidegenskaberne for lejematerialer, der er fremstillet ud fra legeringen ifølge opfindelsen, kan forbedres væsentligt.Moldings made from the alloy of the invention can be rapidly cooled from temperatures above 350 ° C to room temperature and then heat-treated for a period between 0.25 and 8 hours at temperatures between 90 ° C and 275 ° C. By means of this heat treatment, a separation of pure zinc crystals from the alloy is produced in finely divided form, whereby the slip resistance properties of bearing materials made from the alloy according to the invention can be substantially improved.
Legeringen ifølge opfindelsen kan varmdeformeres ved temperaturer mellem 200°C og 400°C, men kan også formes koldt. Det er altså muligt at fremstille tyndvæggede lejeskåle ved formgivning af kold-valsede plader bestående af legeringen ifølge opfindelsen.The alloy of the invention can be thermoformed at temperatures between 200 ° C and 400 ° C, but can also be cold formed. Thus, it is possible to make thin-walled bearing bowls by forming cold-rolled sheets consisting of the alloy according to the invention.
. 141373 4 I de følgende eksempler angives mekaniske egenskaber for en række legeringer ifølge opfindelsen.. In the following examples, mechanical properties of a variety of alloys according to the invention are given.
Eksempel 1Example 1
Lejelegering til middel belastning, udglødet i 1 time ved 150°C.Medium load bearing alloy, annealed for 1 hour at 150 ° C.
Sammensætning: Al 50%, Zn 49,3%, Ni 0,7%.Composition: Al 50%, Zn 49.3%, Ni 0.7%.
Støbehårdhed: IL, - 90 kp/mm2 " 2 Hårdhed efter udglødning: Ηβ - 65 kp/mm ·Cast Hardness: IL, - 90 kp / mm2 "2 Hardness after annealing: Ηβ - 65 kp / mm ·
Eksempel 2Example 2
Lejemateriale til højere belastning, udglødet i 1 time ved 150°C. Sammensætning: Al 58%, Zn 40%, Ni 1%, Cu 1%.Higher load bearing material, annealed for 1 hour at 150 ° C. Composition: Al 58%, Zn 40%, Ni 1%, Cu 1%.
Støbehårdhed: H_ - 110 kp/mm2 “ 2 Hårdhed efter udglødning: H_, - 90 kp/mm B 2 Efter tilsætning af 0,03% Mg stiger hårdheden med 10 kp/mm .Cast Hardness: H_ - 110 kp / mm2 “2 Hardness after annealing: H_, - 90 kp / mm B 2 After the addition of 0.03% Mg the hardness increases by 10 kp / mm.
Eksempel 3Example 3
Lejelegering, varmvalset ved 280°C fra 30 mm til 6 mm, udglødet i 3 timer ved 150°C.Bearing alloy, hot rolled at 280 ° C from 30 mm to 6 mm, annealed for 3 hours at 150 ° C.
a) Sammensætning: Al 60%, Zn 38,3% , Ni 1,7% 2a) Composition: Al 60%, Zn 38.3%, Ni 1.7% 2
Støbehårdhed: Ηβ - 115 kp/mrr^ Hårdhed efter udglødning: Ηβ ^ kp/mm b) Sammensætning: Al 60%, Zn 38%, Ni 1,7%, Cu 0,3%Cast Hardness: Ηβ - 115 kp / mrr ^ Hardness after annealing: Ηβ ^ kp / mm b) Composition: Al 60%, Zn 38%, Ni 1.7%, Cu 0.3%
Støbehårdhed: Hn - 130 kp/mm2 ** 2 Hårdhed efter udglødning: Ηβ - 85 kp/mmCast Hardness: Hn - 130 kp / mm2 ** 2 Hardness after annealing: Ηβ - 85 kp / mm
Legeringerne a) og· b) blev koldvalset og varmebehandlet i 3 timer ved 150°C. Hvor der er angivet to værdier efter hinanden, angiver den første værdi resultatet af målingen parallelt med valseretningen, og den anden værdi angiver resultatet af målingen vinkelret på valseretningen .Alloys a) and · b) were cold rolled and heat treated for 3 hours at 150 ° C. Where two values are given in succession, the first value indicates the result of the measurement parallel to the rolling direction, and the second value indicates the result of the measurement perpendicular to the rolling direction.
Claims (4)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT104570A AT294440B (en) | 1970-02-05 | 1970-02-05 | Aluminum-zinc-based alloy and process for its manufacture and heat treatment |
AT104570 | 1970-02-05 |
Publications (2)
Publication Number | Publication Date |
---|---|
DK141373B true DK141373B (en) | 1980-03-03 |
DK141373C DK141373C (en) | 1980-08-18 |
Family
ID=3505383
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK597570AA DK141373B (en) | 1970-02-05 | 1970-11-24 | Aluminum-zinc alloy, preferably for use as a bearing material, and process for making it. |
Country Status (17)
Country | Link |
---|---|
US (1) | US3790373A (en) |
JP (1) | JPS518089B1 (en) |
AT (1) | AT294440B (en) |
BE (1) | BE759747A (en) |
BR (1) | BR7024871D0 (en) |
CH (2) | CH560251A5 (en) |
DE (1) | DE2055307C3 (en) |
DK (1) | DK141373B (en) |
ES (1) | ES386489A1 (en) |
FR (1) | FR2080495A5 (en) |
GB (1) | GB1326777A (en) |
IL (1) | IL35699A (en) |
LU (1) | LU62034A1 (en) |
NL (1) | NL154274B (en) |
NO (1) | NO127202B (en) |
SE (1) | SE358903B (en) |
YU (1) | YU34147B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4599279A (en) * | 1984-10-01 | 1986-07-08 | Ball Corporation | Zinc alloy for reducing copper-zinc diffusion |
JP4578631B2 (en) * | 2000-07-03 | 2010-11-10 | 有限会社ヤブサキ自動車工業 | Bracket for vehicle sheet metal work |
US6383657B1 (en) | 2000-12-18 | 2002-05-07 | Alltrista Zinc Products | Aluminum clad zinc bimetallic coin planchet |
CN101985709B (en) * | 2010-11-08 | 2012-08-08 | 西安晟金新材料科技有限公司 | Wear-resistant high zinc-aluminum-based bronze substitute material |
CN117026029B (en) * | 2023-08-09 | 2024-03-01 | 仲恺农业工程学院 | High-strength high-damping aluminum-zinc bimetallic alloy and preparation method thereof |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1788751A (en) * | 1926-02-27 | 1931-01-13 | Max Dietiker | Aluminum alloy |
US2280170A (en) * | 1939-10-27 | 1942-04-21 | Aluminum Co Of America | Aluminum alloy |
US2870008A (en) * | 1954-11-18 | 1959-01-20 | Main Alloy Company Establishme | Zinc-aluminium alloys and the method for producing same |
-
1970
- 1970-02-05 AT AT104570A patent/AT294440B/en not_active IP Right Cessation
- 1970-11-04 SE SE14911/70A patent/SE358903B/xx unknown
- 1970-11-10 DE DE2055307A patent/DE2055307C3/en not_active Expired
- 1970-11-10 LU LU62034D patent/LU62034A1/xx unknown
- 1970-11-13 NO NO04331/70A patent/NO127202B/no unknown
- 1970-11-16 NL NL707016759A patent/NL154274B/en unknown
- 1970-11-17 YU YU2815/70A patent/YU34147B/en unknown
- 1970-11-18 CH CH1320473A patent/CH560251A5/xx not_active IP Right Cessation
- 1970-11-18 CH CH1701770A patent/CH556914A/en not_active IP Right Cessation
- 1970-11-19 IL IL35699A patent/IL35699A/en unknown
- 1970-11-24 DK DK597570AA patent/DK141373B/en unknown
- 1970-12-02 BE BE759747D patent/BE759747A/en unknown
- 1970-12-03 GB GB5753070A patent/GB1326777A/en not_active Expired
- 1970-12-03 US US00094938A patent/US3790373A/en not_active Expired - Lifetime
- 1970-12-15 ES ES386489A patent/ES386489A1/en not_active Expired
- 1970-12-15 JP JP45111324A patent/JPS518089B1/ja active Pending
- 1970-12-22 BR BR224871/70A patent/BR7024871D0/en unknown
-
1971
- 1971-01-29 FR FR7103122A patent/FR2080495A5/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
BE759747A (en) | 1971-05-17 |
NL7016759A (en) | 1971-08-09 |
IL35699A0 (en) | 1971-01-28 |
DE2055307A1 (en) | 1971-08-19 |
CH556914A (en) | 1974-12-13 |
AT294440B (en) | 1971-11-25 |
YU281570A (en) | 1978-06-30 |
FR2080495A5 (en) | 1971-11-12 |
BR7024871D0 (en) | 1973-04-05 |
US3790373A (en) | 1974-02-05 |
GB1326777A (en) | 1973-08-15 |
CH560251A5 (en) | 1975-03-27 |
NO127202B (en) | 1973-05-21 |
DE2055307C3 (en) | 1979-11-08 |
IL35699A (en) | 1974-01-14 |
ES386489A1 (en) | 1973-11-16 |
YU34147B (en) | 1978-12-31 |
SE358903B (en) | 1973-08-13 |
LU62034A1 (en) | 1971-05-10 |
JPS518089B1 (en) | 1976-03-13 |
DK141373C (en) | 1980-08-18 |
NL154274B (en) | 1977-08-15 |
DE2055307B2 (en) | 1979-03-22 |
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