ATE455874T1 - ALUMINUM-BASED ALLOY - Google Patents

ALUMINUM-BASED ALLOY

Info

Publication number
ATE455874T1
ATE455874T1 AT07747842T AT07747842T ATE455874T1 AT E455874 T1 ATE455874 T1 AT E455874T1 AT 07747842 T AT07747842 T AT 07747842T AT 07747842 T AT07747842 T AT 07747842T AT E455874 T1 ATE455874 T1 AT E455874T1
Authority
AT
Austria
Prior art keywords
aluminum
magnesium
copper
lithium
finished products
Prior art date
Application number
AT07747842T
Other languages
German (de)
Inventor
Valeriy Ivanovich Popov
Boris Vladimirovich Ovsyannikov
Viktor Mikhailovich Zamyatin
Original Assignee
Otkrytoe Akcionernoe Obschestv
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 Otkrytoe Akcionernoe Obschestv filed Critical Otkrytoe Akcionernoe Obschestv
Application granted granted Critical
Publication of ATE455874T1 publication Critical patent/ATE455874T1/en

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
    • 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
    • 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
    • C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Forging (AREA)
  • Materials For Medical Uses (AREA)
  • Battery Electrode And Active Subsutance (AREA)
  • Laminated Bodies (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Secondary Cells (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

The invention covers a field of metallurgy of alloys based on aluminum, in particular, to the alloy of aluminum-copper-magnesium-lithium system applied for manufacturing semi-finished products and parts thereof used as structural materials for aerospace engineering. The invention is directed to enhancement of ductility and processibility of aluminum-copper-magnesium-lithium system alloys, increase of yields by manufacturing semi-finished products and parts thereof, assurance of possibility to produce thin sheets, thin-walled sections and die-forgings by reducing production labor intensiveness, by preservation required strength and operation characteristics demanded to structural materials for aerospace engineering. The indicated technical result is achieved by the fact, that the alloy contains the following component ratio, wt %: lithium- 1.6 - 1.9; copper- 1.3 - 1.5; magnesium- 0.7 - 1.1; zirconium- 0.04 - 0.2; beryllium- 0.02 - 0.2; titanium- 0.01 - 0.1; nickel-0.01-0.15; manganese- 0.01 - 0.2; gallium- O 0.001; - 0.01 - 0.3; sodium- up to 0.0005; calcium- 0.005 - 0.02; and, at least, one element selected from the group including vanadium- 0.005 - 0.01 and scandium-0.005 - 0.01; aluminum- remainder.
AT07747842T 2006-03-27 2007-03-07 ALUMINUM-BASED ALLOY ATE455874T1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2006109658/02A RU2310005C1 (en) 2006-03-27 2006-03-27 Aluminum base alloy and product of such alloy
PCT/RU2007/000109 WO2007111529A1 (en) 2006-03-27 2007-03-07 Aluminium-based alloy

Publications (1)

Publication Number Publication Date
ATE455874T1 true ATE455874T1 (en) 2010-02-15

Family

ID=38541383

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07747842T ATE455874T1 (en) 2006-03-27 2007-03-07 ALUMINUM-BASED ALLOY

Country Status (8)

Country Link
US (1) US20090068056A1 (en)
EP (1) EP2006403B1 (en)
AT (1) ATE455874T1 (en)
DE (2) DE07747842T1 (en)
ES (1) ES2319718T3 (en)
PT (1) PT2006403E (en)
RU (1) RU2310005C1 (en)
WO (1) WO2007111529A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8437332B2 (en) 2009-06-22 2013-05-07 Qualcomm Incorporated Low complexity unified control channel processing
WO2015181210A1 (en) * 2014-05-30 2015-12-03 Basf Se Polymer for use as protective layers and other components in electrochemical cells

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1412280A (en) * 1920-03-29 1922-04-11 Aluminum Co Of America Aluinum alloy
US1767916A (en) 1926-06-23 1930-06-24 Coleman Automatic Transmission Transmission
US4232910A (en) * 1976-04-12 1980-11-11 Motor Wheel Corporation Systems and methods for controlling trailer brakes as a function of trailer wheel rotation
FR2646172B1 (en) * 1989-04-21 1993-09-24 Cegedur AL-LI-CU-MG ALLOY WITH GOOD COLD DEFORMABILITY AND GOOD DAMAGE RESISTANCE
AT407404B (en) * 1998-07-29 2001-03-26 Miba Gleitlager Ag INTERMEDIATE LAYER, IN PARTICULAR BOND LAYER, FROM AN ALUMINUM-BASED ALLOY
RU2163940C1 (en) * 1999-08-09 2001-03-10 Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Aluminum-base alloy and article made of it
RU2180928C1 (en) 2000-09-14 2002-03-27 Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Aluminum-based alloy and a piece made from this alloy

Also Published As

Publication number Publication date
DE602007004465D1 (en) 2010-03-11
US20090068056A1 (en) 2009-03-12
EP2006403B1 (en) 2010-01-20
PT2006403E (en) 2010-04-26
ES2319718T1 (en) 2009-05-12
RU2310005C1 (en) 2007-11-10
WO2007111529A1 (en) 2007-10-04
DE07747842T1 (en) 2009-04-30
EP2006403A1 (en) 2008-12-24
EP2006403A4 (en) 2009-03-18
ES2319718T3 (en) 2010-05-28

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