Alloy V95och
Designation
Name |
The value |
Designation GOST Cyrillic |
В95оч |
Designation GOST Latin |
B95och |
Transliteration |
V95och |
The chemical elements |
В95оч |
Description
Alloy V95och 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; moulded panels of constant cross section with longitudinal fins in the aircraft industry, is made by a sweep of extruded finned tubes in the plane of the width of the fabric up to 2100 mm.
Note
High strength alloy system Al-Zn-Mg.
Standards
Name |
Code |
Standards |
Non-ferrous metals, including rare metals, and their alloys |
В51 |
GOST 4784-97, OST 1 90026-80 |
Metal forming. Forgings |
В03 |
OST 1 90073-85 |
Sheets and stripes |
В53 |
OST 1 90246-77, OST 1 90070-92, TU 1-5-072-78, TU 1-92-161-90 |
Bars |
В55 |
OST 1 90395-91 |
Sectional and shaped rolling |
В52 |
OST 1 92093-83, OST 1 92041-90, OST 1 90113-86, OST 1 90125-83 |
Chemical composition
Standard |
Mn |
Cr |
Si |
Ni |
Fe |
Cu |
Al |
Ti |
Zn |
Mg |
OST 1 90026-80 |
0.2-0.6 |
0.1-0.25 |
≤0.1 |
≤0.1 |
≤0.15 |
1.4-2 |
The rest |
≤0.05 |
5-6.5 |
1.8-2.8 |
GOST 4784-97 |
0.2-0.6 |
0.1-0.25 |
≤0.1 |
- |
≤0.15 |
1.4-2 |
The rest |
≤0.05 |
5-6.5 |
1.8-2.8 |
Al is the base.
According to GOST 4784-97 and OST 1 90026-80 the total content of other impurities is ≤ 0.10%. The content of each other impurity is ≤ 0.050%.
Mechanical characteristics
Section, mm |
sT|s0,2, MPa |
σB, MPa |
d5, % |
Brinell hardness number, MPa |
Sheet metal plated on OST 1 90246-77 heat treated in regime T2 (samples transverse to the direction of rolling) |
0.5-1.9 |
380-461 |
450-530 |
≥8 |
- |
1.9-4.5 |
380-461 |
460-540 |
≥8 |
- |
4.5-6 |
400-481 |
480-560 |
≥8 |
- |
6-10.5 |
390-471 |
470-550 |
≥8 |
- |
Sheet metal plated on OST 1 90246-77 with heat treatment regime T3 (samples transverse to the direction of rolling) |
0.5-1.9 |
345-420 |
430-500 |
≥8 |
- |
1.9-4.5 |
355-430 |
440-510 |
≥8 |
- |
4.5-10.5 |
375-450 |
450-520 |
≥8 |
- |
Flats for OST 1 90246-77 heat treated in regime T2 (samples transverse to the direction of rolling) |
1-3 |
420-500 |
490-570 |
≥8 |
- |
3-6 |
420-501 |
500-580 |
≥8 |
- |
6-10.5 |
420-501 |
490-570 |
≥8 |
- |
Flats for OST 1 90246-77 with heat treatment regime T3 (samples transverse to the direction of rolling) |
0.5-1 |
375-450 |
450-520 |
≥7 |
- |
1-6 |
380-460 |
460-530 |
≥8 |
- |
6-10.5 |
390-470 |
470-540 |
≥7 |
- |
Panels are extruded with fins on OST 1 92041-90 on delivery |
|
420-510 |
490-570 |
≥8 |
- |
Forgings for OST 1 90073-85. Mode T2: Quenching + artificial aging |
≤75 |
400-480 |
460-540 |
≥4 |
≥120 |
100-125 |
370-450 |
440-520 |
≥3 |
≥120 |
75-100 |
390-470 |
460-540 |
≥3 |
≥120 |
≤75 |
410-490 |
480-570 |
6-7 |
≥120 |
100-125 |
390-470 |
450-540 |
≥6 |
≥120 |
75-100 |
400-480 |
470-560 |
≥6 |
≥120 |
≤75 |
410-490 |
470-550 |
4-5 |
≥120 |
75-100 |
410-490 |
460-540 |
≥4 |
≥120 |
≤75 |
430-520 |
490-580 |
6-7 |
≥120 |
75-100 |
420-510 |
480-570 |
6-7 |
≥120 |
Forgings for OST 1 90073-85. Mode T3: Quenching + artificial aging |
≤75 |
370-450 |
440-520 |
4-5 |
≥110 |
100-125 |
340-430 |
410-490 |
3-4 |
- |
125-150 |
340-430 |
400-480 |
≥3 |
- |
75-100 |
360-450 |
430-510 |
3-4 |
- |
≤75 |
380-470 |
450-540 |
≥7 |
≥110 |
100-125 |
360-450 |
420-510 |
≥7 |
- |
125-150 |
360-450 |
410-500 |
≥7 |
- |
75-100 |
370-460 |
440-530 |
≥7 |
- |
≤75 |
370-450 |
440-520 |
≥5 |
≥110 |
75-100 |
360-450 |
430-510 |
3-4.5 |
- |
≤75 |
380-470 |
450-540 |
7-8 |
≥110 |
75-100 |
370-460 |
440-530 |
7-8 |
- |
Forgings section up to 150 mm OST 1 90073-85. Mode T1: Quenching + artificial aging (indicated by the direction of samples) |
|
- |
≥440 |
≥3 |
≥125 |
|
≥410 |
≥490 |
5-6 |
≥125 |
|
- |
≥450 |
≥4 |
≥125 |
|
≥430 |
≥510 |
≥6 |
≥125 |
Extruded at OST 1 90113-86 normal strength with the cross-sectional area 200 cm2 and a diameter of the circumscribed circle of up to 350 mm. (sample transverse cross-sections show the direction of the sample). Quenching + artificial aging |
|
- |
≥470 |
≥3 |
- |
|
≥450 |
≥490 |
≥4 |
- |
Extruded at OST 1 90113-86 normal strength with the cross-sectional area 200 cm2 and a diameter of the circumscribed circle of up to 350 mm. (sample longitudinal cross-section shows the thickness of the shelf). Quenching + artificial aging by softening regime T2 |
≤75 |
450-530 |
510-590 |
≥7 |
- |
75-125 |
420-530 |
490-590 |
≥7 |
- |
Extruded at OST 1 90113-86 normal strength with the cross-sectional area 200 cm2 and a diameter of the circumscribed circle of up to 350 mm. (sample longitudinal cross-section shows the thickness of the shelf). Quenching + artificial aging by softening mode T3 |
≤5 |
390-460 |
460-530 |
≥7 |
- |
40-75 |
400-470 |
470-540 |
≥8 |
- |
5-40 |
420-490 |
480-550 |
≥8 |
- |
75-125 |
390-460 |
460-530 |
≥7 |
- |
Profile hire for OST 1 90125-83 heat treated in regime T2 (samples longitudinal to direction of rolling) |
≤5 |
450-530 |
510-590 |
≥7 |
- |
5-80 |
450-530 |
510-590 |
≥7 |
- |
Profile hire for OST 1 90125-83 with heat treatment regime T3 (samples longitudinal to direction of rolling) |
≤5 |
390-460 |
460-530 |
≥7 |
- |
40-75 |
400-470 |
470-540 |
≥8 |
- |
5-40 |
420-490 |
480-550 |
≥8 |
- |
75-112 |
390-460 |
460-530 |
≥7 |
- |
Rolled plates (plates) OST 1 90125-83 alloys and clad V95och В95очА heat treated in regime T2 (samples transverse to the direction of rolling) |
11-50 |
420-500 |
490-560 |
≥7 |
- |
50-60 |
380-460 |
470-540 |
≥6 |
- |
60-85 |
365-440 |
460-530 |
≥6 |
- |
Rolled plates (plates) OST 1 90125-83 alloys and clad V95och В95очА with heat treatment regime T3 (samples transverse to the direction of rolling) |
11-50 |
400-480 |
470-540 |
≥7 |
- |
50-60 |
365-440 |
450-520 |
≥6 |
- |
60-85 |
345-420 |
440-510 |
≥6 |
- |
Description mechanical marks
Name |
Description |
Section |
Section |
sT|s0,2 |
Yield strength or limit of proportionality with a tolerance for residual deformation of 0.2% |
σB |
Limit short-term strength |
d5 |
Elongation after rupture |
Physical characteristics
Temperature |
Е, ГПа |
r, кг/м3 |
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 |