SU91998A1 - The method of heat treatment of the bearing alloy based on zinc - Google Patents
The method of heat treatment of the bearing alloy based on zincInfo
- Publication number
- SU91998A1 SU91998A1 SU432508A SU432508A SU91998A1 SU 91998 A1 SU91998 A1 SU 91998A1 SU 432508 A SU432508 A SU 432508A SU 432508 A SU432508 A SU 432508A SU 91998 A1 SU91998 A1 SU 91998A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- zinc
- heat treatment
- bearing alloy
- alloy based
- alloy
- Prior art date
Links
Description
Изобретение относитс к области термической обработки антифрикционнгэкх сплавов на цинковой основе.This invention relates to the field of heat treatment of anti-friction zinc-based alloys.
Термообработка подшипникового сплава на цинковой основе с добавками алюмини 10% и,меди 5°о (ЦАМ-10-5) проводитс путем нагрева до 70-80°, выдержки при этой температуре 8-10 час. и последующего медленного охлаждени в печи. Предлагаетс нагрев зтого сплава осуществл ть до 270-300°, производить выдержку при зтой температуре в 3 часа и з тем медленно охлаждать до 70-80° в печи и далее на воздухе. Предлагаема термообработка понижает твердость этого сплава на цинковси оепове и улучшает его антифрикционные характеристики .Heat treatment of the zinc-based bearing alloy with the addition of aluminum 10% and copper 5 ° C (CAM-10-5) is carried out by heating to 70-80 °, holding at this temperature for 8-10 hours. and subsequent slow cooling in the oven. It is proposed to heat this alloy to 270-300 °, hold at this temperature for 3 hours and then slowly cool to 70-80 ° in an oven and then in air. The proposed heat treatment lowers the hardness of this alloy on zinc oxide and improves its antifriction characteristics.
Пред м е т изо б р е т е н и Prevention isotopes
Способ термической обработки подщипникового сплава на цинковой основе с добавками Ю алюмини и 5% меди, о т .ч и ч а ю щи liс тем, что, в 1дел х понижени твердости силава и улучшени его антифрикционных характеристик, нагревают сплав до температуры 270-300°, дают при зтой температуре выдержку в 3 часа и зате.м медленно охлаждают до 70-80° в иечи и далее на воздухе.The method of heat treatment of a zinc-based sub-base alloy with the addition of U aluminum and 5% copper, therefore, in that it reduces the hardness of the force and improves its antifriction characteristics, heating the alloy to a temperature of 270-300 °, give at this temperature an exposure of 3 hours and then slowly cool to 70-80 ° in the lake and then on the air.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU432508A SU91998A1 (en) | 1950-08-03 | 1950-08-03 | The method of heat treatment of the bearing alloy based on zinc |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU432508A SU91998A1 (en) | 1950-08-03 | 1950-08-03 | The method of heat treatment of the bearing alloy based on zinc |
Publications (1)
Publication Number | Publication Date |
---|---|
SU91998A1 true SU91998A1 (en) | 1950-11-30 |
Family
ID=48367822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU432508A SU91998A1 (en) | 1950-08-03 | 1950-08-03 | The method of heat treatment of the bearing alloy based on zinc |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU91998A1 (en) |
-
1950
- 1950-08-03 SU SU432508A patent/SU91998A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB961635A (en) | Stainless steel alloy | |
SU91998A1 (en) | The method of heat treatment of the bearing alloy based on zinc | |
GB1095034A (en) | A method of heat treating continuously cast aluminium alloy billets | |
GB1013778A (en) | Alloy steel | |
GB597308A (en) | New aluminium base alloys | |
GB1087491A (en) | Improvements in or relating to the heat treatment of tungsten-base compositions or alloys | |
DE375244C (en) | Zinc alloys | |
GB621224A (en) | Working and heat-treating beryllium-copper alloys | |
GB575316A (en) | Improvements in brass | |
GB672263A (en) | Aluminium bronze alloy | |
RU2652926C1 (en) | Heat-resistant alloy | |
GB1343635A (en) | Annealing | |
SU89343A1 (en) | Iron based magnetic alloy and heat treatment method | |
GB706502A (en) | Improvements in and relating to copperbase alloys | |
GB474812A (en) | Improvements in and relating to hardening processes for magnesium base alloys | |
SU359972A1 (en) | Method of vacuum heat treatment of niobium-base alloys | |
GB1033425A (en) | Improvements relating to the heat-treatment of copper free aluminum base alloys | |
GB1186161A (en) | Improvements in or relating to the Heat Treatment of Aluminium Alloys | |
SU377341A1 (en) | ||
GB972532A (en) | Improvements in or relating to titanium base alloys | |
GB681906A (en) | Improvements relating to aluminium base alloys | |
GB386972A (en) | Improvements in or relating to alloys containing tin and copper | |
GB948216A (en) | Improvements in the heat treatment of zinc alloys containing magnesium and aluminium | |
GB1144304A (en) | Method of heat-treating beta titanium-base alloy | |
Godecke et al. | Constitution of the Fe-Ga System Between 10 and 50 At. per cent Ga and Its Dependence on Heat Treatment. Pt. 3. Supercooling Diagram and Process Diagrams for Ga Annealing of Furnace Cooled or Quenched Alloys |