Designation
Name |
The value |
Designation GOST Cyrillic |
В95 |
Designation GOST Latin |
B95 |
Transliteration |
V95 |
By chemical elements |
В95 |
Name |
The value |
Designation GOST Cyrillic |
1950 |
Designation GOST Latin |
1950 |
Transliteration |
1950 |
By chemical elements |
1950 |
Description
Alloy B95 is used: for the manufacture of rolled and extruded lengthy (30 m) semi-finished panels for the top wing (plates, sheets), stringers (bent and pressed sheet), beams, columns and other elements of the fuselage and wings of modern aircraft (TU-204, Il-96, be-200) and other highly loaded structures, working primarily in compression; profiles with cross-sectional area of 200 cm2 and a diameter of circumcircle up to 350mm, designed for use in the aviation industry and special machine building industries; extruded large pipes.
Note
High strength alloy system Al-Zn-Mg.
Standards
Name |
Code |
Standards |
Tape |
В54 |
GOST 13726-97 |
Sheets and strips |
В53 |
GOST 17232-99, GOST 21631-76, OST 1 90246-77, OST 4.021.047-92, OST 4.021.061-92, TU 1-2-298-80, TU 1-2-87-77, TU 1-804-473-2009 |
Tubes of non-ferrous metals and alloys |
В64 |
GOST 18482-79, OST 1 92048-90, OST 1 92048-76, TU 1-8-243-2000, TU 1-804-095-89 |
Bars |
В55 |
GOST 21488-97, GOST Р 51834-2001, OST 4.021.017-92, OST 4.021.036-92, TU 1-2-307-79, TU 1-2-459-84 |
Non-ferrous metals, including rare, and their alloys |
В51 |
GOST 4784-97, OST 4.021.009-92 |
Bars and shapes |
В52 |
GOST 8617-81, GOST 13616-97, GOST 13617-97, GOST 13618-97, GOST 13619-97, GOST 13620-90, GOST 13621-90, GOST 13622-91, GOST 13623-90, GOST 13624-90, GOST 13737-90, GOST 13738-91, GOST 17575-90, GOST 17576-97, GOST 29296-92, GOST 29303-92, GOST Р 50066-92, GOST Р 50067-92, GOST Р 50077-92, OST 1 92093-83, OST 1 92066-91, OST 1 92067-92, OST 1 92069-77, OST 1 90113-86, OST 1 90040-71, OST 4.021.134-92, OST 4.021.136-92, TU 1-2-370-77, TU 1-2-401-80 |
Processing of metals by pressure. Forgings |
В03 |
OST 1 90073-85 |
Chemical composition
Standard |
Mn |
Cr |
Si |
Ni |
Fe |
Cu |
Al |
Ti |
Zn |
Mg |
TU 1-804-473-2009 |
0.2-0.6 |
0.1-0.25 |
≤0.5 |
≤0.1 |
≤0.5 |
1.4-2 |
Rest |
≤0.05 |
5-7 |
1.8-2.8 |
Al is the base.
According to GOST 4784-97, the mass fraction of each other impurity (not regulated) ≤ 0.05%, the total mass fraction of other impurities ≤ 0.10%.
Mechanical properties
Section, mm |
sT|s0,2, MPa |
σU, MPa |
d5, % |
d |
HB, MPa |
Sheet metal in delivery condition of alloy В95А (normal plating) according to GOST 21631-76, OST 4.021.047-92 tape according to GOST 13726-97 (samples transverse) |
0.5-10.5 |
- |
≤245 |
- |
≥10 |
- |
0.5-1.9 |
≥400 |
≥480 |
- |
≥7 |
- |
1.9-6 |
≥410 |
≥490 |
- |
≥7 |
- |
6-10.5 |
≥410 |
≥490 |
- |
≥6 |
- |
Plate in the delivery condition on the other 1-804-473-2009 |
11-25 |
≥275 |
≥490 |
- |
≥7 |
- |
25-40 |
≥410 |
≥490 |
- |
≥3 |
- |
40-50 |
≥390 |
≥470 |
- |
≥2 |
- |
Plate alloy В95А (normal plating) according to GOST 17232-99 in the delivery condition (transverse specimens) |
11-25 |
≥410 |
≥490 |
- |
≥4 |
- |
25-40 |
≥410 |
≥490 |
- |
≥3 |
- |
40-50 |
≥390 |
≥470 |
- |
≥3 |
- |
Plate alloy В95А (normal plating) according to GOST 17232-99 in the state of delivery (samples perpendicular to the plane of the plate) |
40-50 |
- |
≥390 |
- |
≥2 |
- |
Slabs of В95Б alloy (with plating technology) OST 4.021.061-92 in the state of delivery (samples perpendicular to the plane of the plate) |
40-50 |
- |
≥392 |
- |
≥2 |
- |
Slabs of В95Б alloy (with plating technology) OST 4.021.061-92 in the state of delivery (samples transverse to the direction of rolling) |
12-25 |
≥411.6 |
≥490 |
- |
≥4 |
- |
25-40 |
≥411.6 |
≥490 |
- |
≥3 |
- |
40-50 |
≥382 |
≥470 |
- |
≥2 |
- |
Forgings section up to 150 mm OST 1 90073-85. Mode T1 (indicated by the direction of samples) |
|
- |
≥440 |
≥3 |
- |
≥125 |
|
≥410 |
≥490 |
5-6 |
- |
≥125 |
|
- |
≥450 |
≥4 |
- |
≥125 |
|
≥430 |
≥510 |
≥6 |
- |
≥125 |
Profiles extruded from alloy В95А (normal plating) OST 1 90113-86 normal strength with the cross-sectional area 200 cm2 and a diameter of circumcircle up to 350mm (sample transverse cross-sections show the direction of sample) |
|
- |
≥470 |
≥3 |
- |
- |
|
≥450 |
≥490 |
≥4 |
- |
- |
Profiles extruded from alloy В95А (normal plating) OST 1 90113-86 normal strength with the cross-sectional area 200 cm2 and a diameter of circumcircle up to 350mm (sample a longitudinal, in cross-section shows the thickness of the shelf) |
≤5 |
≥460 |
≥510 |
≥6 |
- |
- |
10-75 |
≥490 |
≥550 |
≥6 |
- |
- |
112-125 |
≥460 |
≥530 |
≥6 |
- |
- |
5-10 |
≥480 |
≥530 |
≥6 |
- |
- |
75-112 |
≥480 |
≥550 |
≥6 |
- |
- |
Extruded normal strength of the alloy В95А (normal plating) according to GOST 8617-81 in the delivery condition (longitudinal samples) |
|
- |
≤275 |
≤10 |
- |
- |
≤10 |
≥461 |
≥510 |
≥6 |
- |
- |
10-125 |
≥451 |
≥520 |
≥6 |
- |
- |
Bars extruded square alloy В95А (normal plating) on the EAST 4.021.036-92 (samples longitudinal cross-sections of the specified diameter of the inscribed circle) |
23-65 |
≥420 |
≥530 |
≥6 |
- |
- |
8-22 |
≥390 |
≥490 |
≥6 |
- |
- |
The pressed bars normal strength of the alloy В95А (normal plating) in the delivery state according to GOST 21488-97. 4.021.017-92 (longitudinal samples) |
131-300 |
≥420 |
≥510 |
≥6 |
- |
- |
23-130 |
≥420 |
≥530 |
≥6 |
- |
- |
300-400 |
≥390 |
≥490 |
≥4 |
- |
- |
8-22 |
≥390 |
≥490 |
≥6 |
- |
- |
The pressed bars of high strength alloy В95А (normal plating) in the delivery state according to GOST 21488-97 (longitudinal samples) |
130-300 |
≥430 |
≥530 |
≥6 |
- |
- |
22-130 |
≥430 |
≥550 |
≥6 |
- |
- |
8-22 |
≥400 |
≥510 |
≥7 |
- |
- |
Tubes extruded in the state of delivery according to GOST 18482-79 (samples, in cross-section shows the thickness of the wall) |
20-40 |
≥400 |
≥510 |
≥5 |
- |
- |
5-20 |
≥375 |
≥490 |
≥7 |
- |
- |
Pipe large-size extruded from alloy В95А (normal plating) OST 1 92048-76 in the state of delivery (samples longitudinal cross-section shows the thickness of the wall) |
10-20 |
≥373 |
≥490 |
≥7 |
- |
- |
20 |
≥402 |
≥510 |
≥5 |
- |
- |
Description mechanical marks
Name |
Description |
sT|s0,2 |
Yield strength or limit of proportionality with a tolerance for residual deformation of 0.2% |
σU |
Limit short-term strength |
d5 |
Elongation after rupture |
d |
Elongation after rupture |
HB |
Brinell hardness number |
Physical characteristics
Temperature |
Е, HPa |
r, kg/m3 |
20 |
74 |
2850 |
A description of the physical symbols
Name |
Description |
Е |
The normal elasticity modulus |
r |
Density |
l |
Coefficient of thermal conductivity |
R |
UD. the resistivity |
С |
Specific heat |