AK4-1 (1141)

Chemical composition:

Fe 0.8 — 1.3
Si up to 0.35
Mn up to 0.2
Ni 0.8 — 1.3
Ti 0.02 — 0.1
Al 92.05 — 96.08
Cu 1.9 — 2.5
Mg 1.4 — 1.8
Zn up to 0.3

For the manufacture of jet engine parts Technical requirements: GOST 4784−97 Deformable aluminum and alloys. GOST R 51834−01 grades. Extruded aluminum alloy bars of high strength and increased ductility. Technical conditions OST 1 92014−90 Wrought aluminum alloys. Stamps

Classification

Country Section Category
CIS, Russia, Ukraine Aluminum, aluminum alloys Wrought Aluminum Alloys

Chemical composition

Standard Fe, % Si, % Mg, % Mn, % Cr, % Ti, % Cu, % Zn, % Ni, % Al, %
GOST 4784-97 0.8–1.4 < 0.35 1.2–1.8 < 0.2 < 0.1 0.02–0.1 1.9–2.7 < 0.3 0.8–1.4 93.05–95.28

Information on suppliers

Physical characteristics

Temperature, °C E\cdot 10^{9}, MPa \alpha\cdot 10^{6}, K^{-1} \varkappa, \frac{W}{m\cdot K} \rho, \frac{kg}{m^3} c\cdot 10^{-3}, \frac{J}{kg\cdot K} R\cdot 10^{-6}, \Omega\cdot m
20 72 2800 0.055
100 20.8 146 0.797

Mechanical properties at 20 °C

Rolling Standard Size, mm Tension Classifiers \sigma _{U}, MPa \sigma_{P}, MPa \epsilon_L, % KCU\cdot 10^{3}, \frac{J}{m^2} Treatment
Sheet 380 310 6 200
Round GOST 21488-97 365–390 275–315 6 Hardening and artificial aging
Round GOST 51834-2001 increased plasticity 390 335 6 Hardening and artificial aging
Profile 400 330 8
Sheet GOST 17232-99 385–390 295–325 6 Hardening and artificial aging

Brinell hardness number

Rolling Standard Classifiers Value, HBW
Alloy 109–117

Analogues

USA
AA2018

Standards

Standard Description
GOST 4784-97

Description of chemical elements

Element Units of measurement Description
Fe % Iron
Si % Silicon
Mg % Magnesium
Mn % Manganese
Cr % Chrome
Ti % Titan
Cu % Copper
Zn % Zinc
Ni % Nickel
Al % Aluminium

Description of physical characteristics

Parameter Units of measurement Description
E\cdot 10^{9} MPa Elastic modulus
\alpha\cdot 10^{6} K^{-1} Coefficient of thermal (linear) expansion (range 20°C–T)
\varkappa \frac{W}{m\cdot K} Coefficient of thermal conductivity (the heat capacity of the material)
\rho \frac{kg}{m^3} The density of the material
c\cdot 10^{-3} \frac{J}{kg\cdot K} The specific heat of the material (range 20°C–T)
R\cdot 10^{-6} \Omega\cdot m Electrical resistivity

Description of mechanical properties

Parameter Units of measurement Description
\sigma _{U} MPa Ultimate tensile strength
\sigma_{P} MPa Proportionality limit
\epsilon_L % Elongation at break (longitudinal)
KCU\cdot 10^{3} \frac{J}{m^2} Impact toughness