SU486699A1 - Aluminum based alloy - Google Patents
Aluminum based alloyInfo
- Publication number
- SU486699A1 SU486699A1 SU1706088A SU1706088A SU486699A1 SU 486699 A1 SU486699 A1 SU 486699A1 SU 1706088 A SU1706088 A SU 1706088A SU 1706088 A SU1706088 A SU 1706088A SU 486699 A1 SU486699 A1 SU 486699A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- based alloy
- aluminum based
- aluminum
- zirconium
- magnesium
- Prior art date
Links
Description
1one
Изобретение относитс к разработке сплавов , предназначенных дл изготовлени деталей летательных аппаратов и других жестких конструкций.The invention relates to the development of alloys for the manufacture of aircraft parts and other rigid structures.
Известен сплав на основе алюмини , содержащий , /о:Known alloy based on aluminum, containing / o:
20--4020--40
1-8 Остальное1-8 Else
Цель изобретени - повысить механические свойства и модуль упругости.The purpose of the invention is to improve the mechanical properties and modulus of elasticity.
Это достигаетс тем, что предложенный сплав дополнительно содержит титан и цирконий при следу1О ием This is achieved by the fact that the proposed alloy additionally contains titanium and zirconium at the following level.
соотношении компонентов ,о/,;:the ratio of components, o /,;:
Бериллий10 -30Beryllium10-30
ЛЛагнийО) )0LagniO)) 0
Титан0,05-1,0Titanium0.05-1.0
Цирконий 0,05 - 0,8Zirconium 0.05 - 0.8
Алюминий ОстальноеAluminum Rest
Свойства предложенного сгипава следующие:The properties of the proposed sgipava following:
Модуль упругости, кг/мм-11,500The modulus of elasticity, kg / mm-11,500
Предел прочности, кг/мм 42-48Strength, kg / mm 42-48
Относительное удлинение, о/ 20-34Relative lengthening, o / 20-34
Относительное сужение, о,-;,40-50Relative narrowing, oh, -; 40-50
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1706088A SU486699A1 (en) | 1971-10-14 | 1971-10-14 | Aluminum based alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1706088A SU486699A1 (en) | 1971-10-14 | 1971-10-14 | Aluminum based alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
SU486699A1 true SU486699A1 (en) | 1975-09-30 |
Family
ID=48227793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1706088A SU486699A1 (en) | 1971-10-14 | 1971-10-14 | Aluminum based alloy |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU486699A1 (en) |
-
1971
- 1971-10-14 SU SU1706088A patent/SU486699A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SU486699A1 (en) | Aluminum based alloy | |
SU446978A1 (en) | Aluminum based foundry alloy | |
SU415326A1 (en) | ||
SU346369A1 (en) | ALLOY BASED ON ALUMINUM | |
SU509656A1 (en) | Aluminum based alloy | |
SU403757A1 (en) | Flux | |
SU331110A1 (en) | ALLOY BASED ON ALUMINUM | |
SU362879A1 (en) | COPPER BASED ALLOY | |
SU473759A1 (en) | Aluminum based alloy | |
SU406930A1 (en) | ALUMINUM BRAIN | |
SU518528A1 (en) | Aluminum based alloy | |
SU159038A1 (en) | ||
SU461962A1 (en) | Aluminum based alloy | |
SU435296A1 (en) | SILVER-BASED ALLOY | |
SU283590A1 (en) | DEFORMABLE ALLOY BASED ON MAGNESIUM | |
SU443931A1 (en) | Aluminum based alloy | |
SU572512A1 (en) | Flux for treatment of aluminium alloys | |
SU118287A1 (en) | Aluminum based alloy | |
SU404882A1 (en) | ||
SU443094A1 (en) | Aluminum based alloy | |
SU548648A1 (en) | Modifier for cast aluminum alloys | |
SU539088A1 (en) | Titanium based alloy | |
SU436879A1 (en) | Aluminum based alloy | |
SU346368A1 (en) | ALLOY BASED ON ALUMINUM | |
SU429119A1 (en) | CASTING ALLOY BASED ON ALUMINUM |