SU387018A1 - ALLOY BASED ON ALUMINUM - Google Patents
ALLOY BASED ON ALUMINUMInfo
- Publication number
- SU387018A1 SU387018A1 SU1600540A SU1600540A SU387018A1 SU 387018 A1 SU387018 A1 SU 387018A1 SU 1600540 A SU1600540 A SU 1600540A SU 1600540 A SU1600540 A SU 1600540A SU 387018 A1 SU387018 A1 SU 387018A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- aluminum
- alloy based
- alloy
- zirconium
- manganese
- Prior art date
Links
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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
Description
Изобретение относитс к разработке сплавов на основе алюмини , предназначенных дл изготовлени сварных конструкций, работающих при низкой температуре.The invention relates to the development of aluminum based alloys for the manufacture of welded structures operating at low temperature.
Известен сплав на основе алюмини , содержащий медь, марганец, титан, кадмий, цирконий .Known alloy based on aluminum, containing copper, manganese, titanium, cadmium, zirconium.
Предлагаемый сплав отличаетс от известного тем, что он дополнительно содержит церий, бериллий и олово при следующем соотношении компонентов, вес. %:The proposed alloy differs from the known one in that it additionally contains cerium, beryllium and tin in the following ratio of components, weight. %:
Медь5,5-7,5Copper 5,5-7,5
Марганец0,2-1Manganese 0.2-1
Церий-0,2-1Cerium-0.2-1
Титан0,05-0,3 Цирконий0,05-0,3Titanium 0.05-0.3 Zirconium 0.05-0.3
Кадмий0,05-0,5Cadmium0.05-0.5
Бериллий0,001-0,005 Олово0,03-0,6Beryllium0.001-0.005 Tin0.03-0.6
Алюминийостальное.Aluminum total.
Это способствует повышению предела ползучести.This contributes to an increase in creep strength.
Механические свойства сплава представлены в таблице.The mechanical properties of the alloy are presented in the table.
Предел ползучести сплава при 200° С за 100 час- 18-20 кг/мм.The creep limit of the alloy at 200 ° С in 100 hours is 18–20 kg / mm.
Температура испытани , в °СTest temperature, ° C
10ten
Предмет изобретени Subject invention
Сплав на основе алюмини , включающий медь, марганец, титан, кадмий, цирконий, отличающийс тем, что, с целью повышени предела ползучести, он дополнительно содержит церий, бериллий и олово лри следующем соотношении компонентов, вес. % :An aluminum based alloy including copper, manganese, titanium, cadmium, zirconium, characterized in that, in order to increase the creep strength, it additionally contains cerium, beryllium and tin, with the following ratio of components, weight. %:
Медь.5,5-7,5Copper 5,5-7,5
Марганец0,2-1Manganese 0.2-1
Церий0,2-1Cerium0,2-1
Титан0,05-0,3Titanium0.05-0.3
Цирконий0,05-0,3Zirconium 0.05-0.3
Кадмий0,05-0,5Cadmium0.05-0.5
Бериллий 0,001-0,005Beryllium 0.001-0.005
Олово0,03-0,6Tin0,03-0,6
Алюминийостальное.Aluminum total.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1600540A SU387018A1 (en) | 1970-12-18 | 1970-12-18 | ALLOY BASED ON ALUMINUM |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1600540A SU387018A1 (en) | 1970-12-18 | 1970-12-18 | ALLOY BASED ON ALUMINUM |
Publications (1)
Publication Number | Publication Date |
---|---|
SU387018A1 true SU387018A1 (en) | 1973-06-21 |
Family
ID=20461559
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1600540A SU387018A1 (en) | 1970-12-18 | 1970-12-18 | ALLOY BASED ON ALUMINUM |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU387018A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109797326A (en) * | 2019-03-14 | 2019-05-24 | 南京玖铸新材料研究院有限公司 | A kind of high strength heat resistant alloy and preparation method thereof |
-
1970
- 1970-12-18 SU SU1600540A patent/SU387018A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109797326A (en) * | 2019-03-14 | 2019-05-24 | 南京玖铸新材料研究院有限公司 | A kind of high strength heat resistant alloy and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SU446978A1 (en) | Aluminum based foundry alloy | |
SU387018A1 (en) | ALLOY BASED ON ALUMINUM | |
SU331110A1 (en) | ALLOY BASED ON ALUMINUM | |
SU346369A1 (en) | ALLOY BASED ON ALUMINUM | |
SU336361A1 (en) | ALLOY BASED ON ALUMINUM ALL-UNION FILES? NTNO-T [HNN'1ESS | |
SU406930A1 (en) | ALUMINUM BRAIN | |
SU447452A1 (en) | Magnesium based alloy | |
SU456030A1 (en) | Manganese Based Alloy | |
SU420189A3 (en) | ZINC BASED ALLOY | |
SU346368A1 (en) | ALLOY BASED ON ALUMINUM | |
SU283590A1 (en) | DEFORMABLE ALLOY BASED ON MAGNESIUM | |
SU451773A1 (en) | Aluminum based foundry alloy | |
SU378480A1 (en) | ALLOY BASED ON MEDIRP, "^. =" - • "- •> &I;"!O;..; d KJ ^ .jt'l'S ^ "-,.": - .. h - ^ i 1 .S L12 ' | |
SU486065A1 (en) | Titanium based alloy | |
SU572355A1 (en) | Welding wire composition | |
SU362879A1 (en) | COPPER BASED ALLOY | |
SU417513A1 (en) | ||
SU348633A1 (en) | ||
SU172050A1 (en) | HIGH-STRENGTH MAGNETIC ALLOY | |
SU219368A1 (en) | ||
SU404879A1 (en) | ALLOY BASED ON ALUMINUM | |
SU464641A1 (en) | Aluminum based alloy | |
SU146493A1 (en) | Deformable heat resistant magnesium alloy | |
SU456843A1 (en) | Titanium based alloy | |
SU231836A1 (en) | METAL CERAMIC MAGNESIUM ALLOY |