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
Standards
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 |