US3790373A - Alloy on aluminum-zinc-basis - Google Patents
Alloy on aluminum-zinc-basis Download PDFInfo
- Publication number
- US3790373A US3790373A US00094938A US3790373DA US3790373A US 3790373 A US3790373 A US 3790373A US 00094938 A US00094938 A US 00094938A US 3790373D A US3790373D A US 3790373DA US 3790373 A US3790373 A US 3790373A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- present
- alloy
- zinc
- nickel
- 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
- 239000000956 alloy Substances 0.000 title claims abstract description 26
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 26
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 29
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 29
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 28
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 15
- 239000011777 magnesium Substances 0.000 claims abstract description 9
- 239000011701 zinc Substances 0.000 claims abstract description 9
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052802 copper Inorganic materials 0.000 claims abstract description 8
- 239000010949 copper Substances 0.000 claims abstract description 8
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 7
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 6
- 230000005496 eutectics Effects 0.000 claims abstract description 6
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 2
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 claims description 2
- -1 aluminum-zinc-nickel Chemical compound 0.000 claims description 2
- 230000002250 progressing effect Effects 0.000 claims description 2
- 229910000897 Babbitt (metal) Inorganic materials 0.000 abstract description 2
- 238000005266 casting Methods 0.000 description 8
- 239000011148 porous material Substances 0.000 description 5
- 238000000137 annealing Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000001996 bearing alloy Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 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 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
Definitions
- This alloy is an excellent bearing metal by which the running characteristics are essentially improved.
- the invention relates to an alloy on aluminum-zincbasis consisting of 38 to 75 preferably of 50 to 65 aluminum, nickel and, if desired, magnesium and copper, remainder zinc, and to a process for the production of such alloy and process for the production of shaped bodies from such alloy.
- Such alloys are used primarily as bearing material for bearing bushings or the like, which parts are produced by casting or by appropriate shaping from rolled plates and sheets. In any case at first a casting is made whose structure is responsible to a great degree for the properties of the bearing.
- the invention is aimed at avoiding these disadvantages and, in an alloy of the kind defined in the introductory part, resides in that the nickel content amounts to at least 0.05 and maximally corresponds to the course of the eutectic groove in the aluminum-zincnickel system, this maximum content of nickel amounting to 0.6 when 38 aluminum are present, to 1.1 when 50 aluminum are present, to 1.7 when 60 aluminum are present, to 2.4 when 70 aluminum are present, and to 2.8 when 75 aluminum are present, and progresses continuously between the given values.
- the nickel content suggested by the invention causes in the cast product a structure without pores and of fine grain and an increase in hardness.
- the alloy may, with advantage, contain also from 0.005 to 0.05 of magnesium, by which addition the grain is rendered even finer. Furthermore, copper may be contained in an amount of maximally 6.5 of the aluminum content. This additional'ingredient also effects an increase in hardness.
- starting materials with a purity of at least 99.5 are used which are free from elements which form insoluble compounds with nickel, such as silicium or boron,'and from elements which crystallize primarily and in the form of needles, such as iron, manganese, titanium, vanadium, molybdenum, tungsten and carbon.
- the magnesium may be added, suitably in the form of a pre-alloy of high specific gravity, advantageously in the form of an alloy with 5 aluminum, 3 magnesium and 92 zinc.
- Shaped bodies produced from an alloy according to the invention may be cooled rapidly from temperatures of more than 350 C to room temperature and then be heat treated for a period of from 0.25 to 8 hours at temperatures between and 275 C. During this heat treatment pure zinc crystals will separate from the alloy in most finely distributed form so that the emergency running characteristics (running without oil) of the bearing parts produced from the alloy according to the invention are materially improved.
- the alloy according to the invention may be hot shaped at temperatures of from 200 to 400 C but may also be cold shaped. Thus it becomes possible to produce bearing bushings with thin walls by shaping cold rolled sheets made of the alloys according to the invention.
- Hardness as cast hardness after annealing EXAMPLE 2 Hardness as cast hardness after annealing H kp/mm H 90 lip/mm .By adding 0.03 Mg the hardness values are increased by 10 kplmm EXAMPLE 3 Bearing alloy, hot rolled at 280 C from 30 mm to 6 mm, annealed for 3 hours at C.
- HARDNESS AS CAST H 115 kplmm hardness after annealing b.
- the first value refers to the result when the measurement was taken parallel to the rolling direction
- the second value refers to the result when the measurement was taken perpendicularly to the rolling direction.
- An aluminum-zinc alloy consisting essentially of 38 to 75% aluminum
- nickel 0.05 to 2.8% nickel, the maximum nickel content being determined by the eutectic groove in the aluminum-zincmickel system and amounting to 0.6% when 38% aluminum are present, 1.1% when 50% aluminum are present, 1.7% when 60% aluminum are present, 2.4% when, aluminum are present and 2.8% when aluminum are present, the eutectic groove progressing continuously between the given values;
Landscapes
- 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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT104570A AT294440B (de) | 1970-02-05 | 1970-02-05 | Legierung auf Aluminium-Zink-Basis sowie Verfahren zu ihrer Herstellung und Wärmebehandlung |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3790373A true US3790373A (en) | 1974-02-05 |
Family
ID=3505383
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00094938A Expired - Lifetime US3790373A (en) | 1970-02-05 | 1970-12-03 | Alloy on aluminum-zinc-basis |
Country Status (17)
| Country | Link |
|---|---|
| US (1) | US3790373A (en:Method) |
| JP (1) | JPS518089B1 (en:Method) |
| AT (1) | AT294440B (en:Method) |
| BE (1) | BE759747A (en:Method) |
| BR (1) | BR7024871D0 (en:Method) |
| CH (2) | CH556914A (en:Method) |
| DE (1) | DE2055307C3 (en:Method) |
| DK (1) | DK141373B (en:Method) |
| ES (1) | ES386489A1 (en:Method) |
| FR (1) | FR2080495A5 (en:Method) |
| GB (1) | GB1326777A (en:Method) |
| IL (1) | IL35699A (en:Method) |
| LU (1) | LU62034A1 (en:Method) |
| NL (1) | NL154274B (en:Method) |
| NO (1) | NO127202B (en:Method) |
| SE (1) | SE358903B (en:Method) |
| YU (1) | YU34147B (en:Method) |
Cited By (3)
| 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 |
| US6383657B1 (en) | 2000-12-18 | 2002-05-07 | Alltrista Zinc Products | Aluminum clad zinc bimetallic coin planchet |
| CN101985709A (zh) * | 2010-11-08 | 2011-03-16 | 西安晟金新材料科技有限公司 | 一种耐磨高锌铝基代青铜材料 |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4578631B2 (ja) * | 2000-07-03 | 2010-11-10 | 有限会社ヤブサキ自動車工業 | 車両の板金作業用当て金 |
| CN117026029B (zh) * | 2023-08-09 | 2024-03-01 | 仲恺农业工程学院 | 一种高强高阻尼铝锌双金属合金及其制备方法 |
Citations (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/de not_active IP Right Cessation
- 1970-11-04 SE SE14911/70A patent/SE358903B/xx unknown
- 1970-11-10 DE DE2055307A patent/DE2055307C3/de 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/xx unknown
- 1970-11-17 YU YU2815/70A patent/YU34147B/xx unknown
- 1970-11-18 CH CH1701770A patent/CH556914A/xx not_active IP Right Cessation
- 1970-11-18 CH CH1320473A patent/CH560251A5/xx not_active IP Right Cessation
- 1970-11-19 IL IL35699A patent/IL35699A/xx unknown
- 1970-11-24 DK DK597570AA patent/DK141373B/da unknown
- 1970-12-02 BE BE759747D patent/BE759747A/xx unknown
- 1970-12-03 US US00094938A patent/US3790373A/en not_active Expired - Lifetime
- 1970-12-03 GB GB5753070A patent/GB1326777A/en not_active Expired
- 1970-12-15 JP JP45111324A patent/JPS518089B1/ja active Pending
- 1970-12-15 ES ES386489A patent/ES386489A1/es not_active Expired
- 1970-12-22 BR BR224871/70A patent/BR7024871D0/pt unknown
-
1971
- 1971-01-29 FR FR7103122A patent/FR2080495A5/fr not_active Expired
Patent Citations (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 |
Cited By (4)
| 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 |
| US6383657B1 (en) | 2000-12-18 | 2002-05-07 | Alltrista Zinc Products | Aluminum clad zinc bimetallic coin planchet |
| CN101985709A (zh) * | 2010-11-08 | 2011-03-16 | 西安晟金新材料科技有限公司 | 一种耐磨高锌铝基代青铜材料 |
| CN101985709B (zh) * | 2010-11-08 | 2012-08-08 | 西安晟金新材料科技有限公司 | 一种耐磨高锌铝基代青铜材料 |
Also Published As
| Publication number | Publication date |
|---|---|
| NL7016759A (en:Method) | 1971-08-09 |
| GB1326777A (en) | 1973-08-15 |
| BR7024871D0 (pt) | 1973-04-05 |
| YU34147B (en) | 1978-12-31 |
| FR2080495A5 (en:Method) | 1971-11-12 |
| YU281570A (en) | 1978-06-30 |
| LU62034A1 (en:Method) | 1971-05-10 |
| NO127202B (en:Method) | 1973-05-21 |
| ES386489A1 (es) | 1973-11-16 |
| DK141373C (en:Method) | 1980-08-18 |
| IL35699A0 (en) | 1971-01-28 |
| BE759747A (fr) | 1971-05-17 |
| DE2055307A1 (de) | 1971-08-19 |
| CH560251A5 (en:Method) | 1975-03-27 |
| AT294440B (de) | 1971-11-25 |
| DE2055307C3 (de) | 1979-11-08 |
| SE358903B (en:Method) | 1973-08-13 |
| NL154274B (nl) | 1977-08-15 |
| IL35699A (en) | 1974-01-14 |
| JPS518089B1 (en:Method) | 1976-03-13 |
| DE2055307B2 (de) | 1979-03-22 |
| CH556914A (de) | 1974-12-13 |
| DK141373B (da) | 1980-03-03 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR101066536B1 (ko) | 기계적 특성이 우수한 난연성 마그네슘 합금 및 그 제조방법 | |
| US4636357A (en) | Aluminum alloys | |
| US4772342A (en) | Wrought Al/Cu/Mg-type aluminum alloy of high strength in the temperature range between 0 and 250 degrees C. | |
| US4373970A (en) | Copper base spinodal alloy strip and process for its preparation | |
| US4126487A (en) | Producing improved metal alloy products (Al-Fe alloy and Al-Fe-Si alloy) | |
| US4126486A (en) | Producing improved metal alloy products | |
| US20110116966A1 (en) | Aluminum alloy, method of casting aluminum alloy, and method of producing aluminum alloy product | |
| JPH0328500B2 (en:Method) | ||
| JPS6283446A (ja) | 急速固化した高力、耐食性マグネシウムベ−スメタル合金、その製法およびこれから圧縮された金属物品 | |
| US20210140474A1 (en) | Monotectic aluminum plain bearing alloy, method for producing same, and plain bearing produced therewith | |
| US20240263279A1 (en) | High strength microalloyed magnesium alloy | |
| US5296057A (en) | High abrasion resistant aluminum bronze alloy, and sliding members using same | |
| GB2127039A (en) | Fine-grained copper-nickel-tin alloys | |
| US3790373A (en) | Alloy on aluminum-zinc-basis | |
| EP1477577B1 (en) | Aluminum alloy, cast article of aluminum alloy, and method for producing cast article of aluminum alloy | |
| US4002502A (en) | Aluminum base alloys | |
| JP3110512B2 (ja) | 高強度高靭性マグネシウム合金材料 | |
| JPH0756067B2 (ja) | アルミニウム箔地の製造方法 | |
| KR20210121541A (ko) | 고물성 마그네슘 합금 가공재 및 그 제조방법 | |
| US3827882A (en) | High lead aluminium alloy | |
| US3469974A (en) | Magnesium base alloys | |
| JP3387548B2 (ja) | マグネシウム合金成形物の製造方法 | |
| JP2020509196A (ja) | 難燃性に優れた高強度マグネシウム合金及びその製造方法 | |
| US3969160A (en) | High-strength ductile uranium alloy | |
| US2774664A (en) | Magnesium-base alloy |