Alloy ВТ35
Alloy VT8M-1
Alloy VT32
Alloy VT35
Alloy VT4
Alloy VT41
Alloy VT5
Alloy VT5-1
Alloy VT6 (VT6sv.)
Alloy VT6C
Alloy VT6h
Alloy VT8
Alloy VT8-1
Alloy VT3-1
Alloy VT9
OT4 alloy
Alloy OT4-0
Alloy OT4-1
Alloy OT4-2
Alloy PT-1M
Alloy PT-3B
Alloy PT-7M
Alloy SPT-2
Alloy TC5
Alloy TC6
Alloy VT15
Alloy 14
Alloy 19
Alloy 27
Alloy 2B
Alloy 37
Alloy 3M
Alloy 40
Alloy 5B
Alloy AT3
Alloy AT6
Alloy VT14
Alloy VT25U
Alloy VT16
Alloy VT18
Alloy VT18U
Alloy VT2 (VT2sv.)
Alloy VT20
Alloy VT20-1 (VT20-1sv.)
Alloy VT20-2 (VT20-2sv.)
Alloy VT22
Alloy VT22I
Alloy VT23
Designation
| Name | The value |
|---|---|
| Designation GOST Cyrillic | ВТ35 |
| Designation GOST Latin | BT35 |
| Transliteration | VT35 |
| The chemical elements | ВTe35 |
Description
Alloy ВТ35 used: for the manufacture of sheets, foils, shaped castings; in aircraft honeycomb structures, anchor nuts and long sheet member.
Note
ВТ35 alloy high-alloy weldable high-tech pseudo-β-alloy with strength up to 1200 MPa. Alloy capable of hardening during heat treatment in vacuum furnace (or in a protective atmosphere). Alloy ВТ35Л retains the β phase in the process of natural cooling.
The alloy has a high hardenability. In the tempered condition the alloy has high ductility and is capable of cold deformation. Aging leads to a significant hardening (σin > 1200 MPa; δ=6%) with high fracture toughness.
The alloy is treated satisfactorily by the pressure in the hot state.
The alloy after quenching is capable of cold deformation.
