SU1785286A1 - Aluminium-base alloy - Google Patents

Aluminium-base alloy

Info

Publication number
SU1785286A1
SU1785286A1 SU4903732/02A SU4903732A SU1785286A1 SU 1785286 A1 SU1785286 A1 SU 1785286A1 SU 4903732/02 A SU4903732/02 A SU 4903732/02A SU 4903732 A SU4903732 A SU 4903732A SU 1785286 A1 SU1785286 A1 SU 1785286A1
Authority
SU
USSR - Soviet Union
Prior art keywords
alloy
aluminium
kgf
indium
magnesium
Prior art date
Application number
SU4903732/02A
Other languages
Russian (ru)
Inventor
А.М. Дриц
И.Н. Фридляндер
Т.В. Крымова
С.М. Можаровский
С.Б. Комаров
К.Н. Сергеев
А.Г. Вовнянко
А.М. Зиндер
П.Л. Даин
Original Assignee
Научно-производственное объединение "Всесоюзный институт авиационных материалов"
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Научно-производственное объединение "Всесоюзный институт авиационных материалов" filed Critical Научно-производственное объединение "Всесоюзный институт авиационных материалов"
Priority to SU4903732/02A priority Critical patent/SU1785286A1/en
Application granted granted Critical
Publication of SU1785286A1 publication Critical patent/SU1785286A1/en

Links

Landscapes

  • Powder Metallurgy (AREA)

Abstract

FIELD: metallurgy. SUBSTANCE: alloy has, wt.-%: copper 2-6; lithium 1.0-3.5; zirconium 0.02-0.25; cerium 0.005-0.2; magnesium 0.01-0.55; indium 0.01-0.35, at least one metal taken from the group containing scandium 0.01-0.35; manganese 0.05-0.6; titanium 0.01- 0.15; iron 0.005-0.25, and aluminium - the rest. Total content of indium and magnesium is 0.05-0.6. Alloy properties: sensitivity of material to tension concentrators at -196 C is 0.85-0.93, strength limit at -196 C is 70-74 kgf/mm, fluidity limit is 59.5-63.0 kgf/mm, relative elongation is 13-16. Alloy is used as structural material. EFFECT: enhanced quality of alloy. 3 tbl
SU4903732/02A 1991-01-18 1991-01-18 Aluminium-base alloy SU1785286A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4903732/02A SU1785286A1 (en) 1991-01-18 1991-01-18 Aluminium-base alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4903732/02A SU1785286A1 (en) 1991-01-18 1991-01-18 Aluminium-base alloy

Publications (1)

Publication Number Publication Date
SU1785286A1 true SU1785286A1 (en) 1994-08-15

Family

ID=60521787

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4903732/02A SU1785286A1 (en) 1991-01-18 1991-01-18 Aluminium-base alloy

Country Status (1)

Country Link
SU (1) SU1785286A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2001282045B2 (en) * 2000-08-01 2005-04-28 All Russian Institute Of Aviation Materials Viam Aluminium-based alloy and method of fabrication of semiproducts thereof
RU2639177C2 (en) * 2007-12-04 2017-12-20 Арконик Инк. Improved aluminium-copper-lithium alloys
EP3388540A1 (en) * 2017-04-11 2018-10-17 The Boeing Company Aluminum alloy with additions of copper, lithium and at least one of sr or a rare earth metal, and method of manufacturing the same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2001282045B2 (en) * 2000-08-01 2005-04-28 All Russian Institute Of Aviation Materials Viam Aluminium-based alloy and method of fabrication of semiproducts thereof
US7597770B2 (en) 2000-08-01 2009-10-06 Eads Deutschland Gmbh Aluminum-based alloy and method of fabrication of semiproducts thereof
RU2639177C2 (en) * 2007-12-04 2017-12-20 Арконик Инк. Improved aluminium-copper-lithium alloys
EP3388540A1 (en) * 2017-04-11 2018-10-17 The Boeing Company Aluminum alloy with additions of copper, lithium and at least one of sr or a rare earth metal, and method of manufacturing the same
CN108690926A (en) * 2017-04-11 2018-10-23 波音公司 Aluminium alloy and its method of manufacture
RU2761567C2 (en) * 2017-04-11 2021-12-10 Зе Боинг Компани Aluminum alloy with additives of copper, lithium and at least one alkaline earth or rear earth metal and its production method

Similar Documents

Publication Publication Date Title
TW367509B (en) Soft magnetic alloy powder for electromagnetic and magnetic shield, and shielding members containing the same
JPS55134160A (en) Fe alloy with superior molten zinc erosion resistance
SU1785286A1 (en) Aluminium-base alloy
AU621998B2 (en) Hot workable,ferritic steel alloy
YU2383A (en) Process for casting bands of amorphous metals
CA2054109A1 (en) Welding material for low coefficient of thermal expansion alloys
ES8304209A1 (en) Method for the preparation of vermicular graphite cast iron and device allowing to implement such method.
EP0231864A3 (en) Non-ageing steel strip
US5209901A (en) Agent for the treatment of cast iron melts
Sheng et al. Effects of rare earth alloys on structures and properties of grey cast iron
CA1198912A (en) Non-magnetic alloy having high hardness
JPS558486A (en) Forged steel material for heavy gauge excellent in strength and toughness
GB944124A (en) Iron-chromium-aluminium alloy
US2221784A (en) Method and agent for treating molten iron and steel
RU2116371C1 (en) Cast iron
SU734307A1 (en) Steel killing alloy
Chernyshov Reducing the Consumption of Alloying Elements When Melting Corrosion-Resisting Steel in 100 Ton Electric Furnaces
SU451778A1 (en) Alloy for deoxidizing, alloying and modifying steel
RU2012688C1 (en) Steel
RU95119740A (en) METHOD OF OBTAINING LOW-CARBON STEELS
Lott Reducing the Iron Content of Aluminum or Its Alloys
Abratis et al. Application of the Injection Technique in Steel Alloying
RU94016967A (en) Process for preparing ferroalloy
GEP19980577B (en) Burden for Obtaining Ferrosilicoaluminium
Hill et al. The effects of hydrogen on the ductility, toughness, and yield strength of an Al-Mg-Li alloy