Service life of heat resistant alloys with protective coatings in thermocyclic loading

1990 ◽  
Vol 22 (5) ◽  
pp. 664-671
Author(s):  
A. I. Rybnikov ◽  
L. B. Getsov ◽  
I. S. Malashenko
1996 ◽  
Vol 78 (1-3) ◽  
pp. 103-112 ◽  
Author(s):  
A.I. Rybnikov ◽  
L.B. Getsov ◽  
A.A. Tchizhik ◽  
I.S. Malashenko ◽  
A.S. Osyka

1991 ◽  
Vol 46 (2) ◽  
pp. 165-171
Author(s):  
E.V. Kuznetsov ◽  
M.A. Anisimova ◽  
V.A. Batyrev

2012 ◽  
Vol 30 (1) ◽  
pp. 59-72 ◽  
Author(s):  
Piotr Barszcz

Research studies that are conducted by both the Air Force Institute of Technology (AFIT) and other domestic and foreign organizations indicate that investigations of corrosion phenomena present a very important factor with respect to prolongation of technical resources and operation of aircraft driven by their actual technical condition. The investigation of the corrosion degree and deterioration of protective coatings must be carried out in a systemic manner with thorough analysis of information that bring together the aircraft operation and the processes of corrosion and deterioration of protective coatings. The investigation must comprise measurements of the atmospheric corrosion in order to determine corrosive aggressiveness of the atmosphere and establish frequency and scope of corrosion inspection. Only the analysis of gathered information with its characteristics may guarantee safe operation of structural components of aircrafts according to their actual technical condition. This paper outlines the approach to corrosion investigation that is in place in AFIT.


1982 ◽  
Vol 14 (9) ◽  
pp. 1173-1178 ◽  
Author(s):  
L. P. Lozitskii ◽  
A. N. Vetrov ◽  
V. A. Ivanenko

2010 ◽  
Vol 42 (3) ◽  
pp. 352-361 ◽  
Author(s):  
K. Yu. Yakovchuk ◽  
Yu. É. Rudoi ◽  
E. V. Onoprienko ◽  
V. G. Malysheva

Refractories ◽  
1965 ◽  
Vol 6 (7-8) ◽  
pp. 415-419
Author(s):  
L. D. Svirskii ◽  
Yu. A. Pirogov

1987 ◽  
Vol 19 (12) ◽  
pp. 1597-1602
Author(s):  
G. N. Tret'yachenko ◽  
C. R. Semenov ◽  
K. Yu. Yakovchuk ◽  
R. I. Kuriat ◽  
I. S. Malashenko ◽  
...  

2015 ◽  
Vol 72 (3-4) ◽  
pp. 100-103
Author(s):  
V. A. Rozenenkova ◽  
S. S. Solntsev ◽  
D. V. Grashchenkov ◽  
N. A. Mironova

2021 ◽  
Vol 2 ◽  
pp. 51-55
Author(s):  
V. M. Gusev ◽  
◽  
O. Yu. Elagina ◽  
A. G. Buklakov ◽  
◽  
...  

The quality of heat-resistant coatings deposited by flame spraying is largely determined by the adhesion of the coating to the surface of the part. One of the ways to increase adhesion is to deposition intermediate layers of thermosetting powders between the base material and the coating. In this work, two versions of heat-protective coatings are investigated — a two-layer coating consisting of an Al – Ni sublayer (20 – 80 wt. %) and a main ZrO2 layer, and a single-layer coating sprayed from an aluminum-clad zirconium oxide powder (20 ZrO2 – 80 Al, wt. % ). The method of differential thermal analysis was used to determine the temperature ranges and values of the exothermic effects of oxidation and redox reactions during heating of Al – Ni and ZrO2 clad powders. A significant exothermic effect was found during oxidation of the aluminum cladding shell in the temperature range of 360 °C and a stronger thermal effect due to the redox reaction at a temperature of 920 °C. The microstructure and microhardness of the obtained coatings have been studied, and their thermal conductivity and adhesion have been assessed. The resistance of the coatings during thermal cycling tests has been determined. It has been established that thermal protective coatings made of aluminum-clad zirconium oxide powder have the best characteristics under thermal cycling conditions. A higher level of adhesion and thermal cyclic resistance of such coatings are due to an increase in the enthalpy of aluminum-clad ZrO2 powders due to exothermic reactions and the presence of a metal binder.


1987 ◽  
Vol 29 (4) ◽  
pp. 302-307
Author(s):  
Yu. G. Veksler ◽  
V. P. Lesnikov ◽  
S. Ya. Paleeva ◽  
E. G. Lesnikova ◽  
G. F. Myal'nitsa

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