Features of the structure of weld metal at restoration argon-arc surfacing of titanium alloy VT22

2020 ◽  
Vol 2020 (4) ◽  
pp. 44-49
Author(s):  
S.L. Shvab ◽  
◽  
S.V. Akhonin ◽  
I.K. Petrichenko ◽  
S.L. Antonyuk ◽  
...  
Keyword(s):  
Titanium Alloy ◽  
Weld Metal ◽  
Alloy Vt22 ◽  
Titanium Alloy Vt22

scholarly journals Producing Of High-strength Titanium Alloy Vt22 By Method Of Electron Beam Melting

2018 ◽  
Vol 2018 (3) ◽  
pp. 8-15
Author(s):  
S.V. Akhonin ◽  
◽  
V.A. Berezos ◽  
A.N. Pikulin ◽  
A.Yu. Severin ◽  
...  
Keyword(s):  
Titanium Alloy ◽  
Electron Beam ◽  
Electron Beam Melting ◽  
High Strength ◽  
Alloy Vt22 ◽  
Titanium Alloy Vt22

Influence of tensile stresses on the corrosion resistance of titanium alloy VT22 in aqueous solution of NaCl

2017 ◽  
Vol 8 (1) ◽  
pp. 94-99 ◽  
Author(s):  
V. M. Polyanskiy ◽  
Yu. A. Puchkov ◽  
M. R. Orlov ◽  
S. A. Napriyenko ◽  
A. V. Lavrov
Keyword(s):  
Aqueous Solution ◽  
Corrosion Resistance ◽  
Titanium Alloy ◽  
Alloy Vt22 ◽  
Tensile Stresses ◽  
Titanium Alloy Vt22

Heat treatment of titanium alloy VT22

1990 ◽  
Vol 32 (3) ◽  
pp. 212-216 ◽  
Author(s):  
V. N. Moiseev ◽  
Yu. I. Zakharov ◽  
Yu. G. Kirillov ◽  
Yu. M. Dolzhanskii ◽  
T. G. Danilina
Keyword(s):  
Heat Treatment ◽  
Titanium Alloy ◽  
Alloy Vt22 ◽  
Titanium Alloy Vt22

COMPARATIVE ANALYSIS OF METHODS FOR DETERMINING THE MASS OF THE SHAFT OF A SPORTS AND AEROBATIC AIRCRAFT, MADE OF TITANIUM AND COMPOSITE MATERIAL

2020 ◽  
pp. 14-19
Author(s):  
T. M. Avdukhina ◽  
T. S. Druzhinin
Keyword(s):  
Composite Material ◽  
Titanium Alloy ◽  
Comparative Analysis ◽  
Composite Materials ◽  
Prediction Method ◽  
Weight Fraction ◽  
Wing Loading ◽  
Alloy Vt22 ◽  
Landing Impact ◽  
Titanium Alloy Vt22

Comparative analysis of an acrobatic aircraft's weight and shaft which is made of a titanium alloy and composite materials. The article contained requirements and specificities of an acrobatic aircraft's landing gear shaft design. The article describes prediction method of an acrobatic aircraft’s weight fraction of shaft which is allows to take into account shaft mass on wing loading upon condition that composite materials will be used in construction. Research objectives include: –Documentation of an acrobatic aircraft’s shaft design. – Analytic dependence conclusions on shaft mass by applying energy absorption of landing impact. – To quantify the algorithm of shaft mass based on strength prediction of shaft construction. –To quantify the mass and construction of shaft based on patterns that are made of titanium and composite materials. – Comparative analysis and references to practical using these methods to quantify shaft’s mass. –To quantify how shaft mass influenced by wing loading. –Designing shaft construction that is made of titanium alloy VT22 and composite material VKU26 by taking into account quantity and ply layup. Comparative analysis shaft mass which is made by different variety of composite materials. The constructive analysis is distinguished for decreasing the shaft mass that is made by composite material and references on ply layup.

Decomposition of? phase in titanium alloy VT22

1971 ◽  
Vol 13 (9) ◽  
pp. 751-753
Author(s):  
I. S. Pol'kin ◽  
O. V. Kasparova ◽  
O. S. Korobov ◽  
Yu. M. Lebedev ◽  
N. M. Semenova
Keyword(s):  
Titanium Alloy ◽  
Alloy Vt22 ◽  
Titanium Alloy Vt22

Metallographic study of ?-solid solution decomposition for titanium alloy VT22

1986 ◽  
Vol 28 (1) ◽  
pp. 73-77 ◽  
Author(s):  
L. M. Orlova ◽  
A. D. Lemesh ◽  
G. P. Belozub ◽  
T. V. Filatova
Keyword(s):  
Solid Solution ◽  
Titanium Alloy ◽  
Alloy Vt22 ◽  
Metallographic Study ◽  
Solid Solution Decomposition ◽  
Titanium Alloy Vt22
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