Industrial technology of deposition of two-layer plasma heat-protective coatings on gas turbine blades

2020 ◽  
Vol 2020 (4) ◽  
pp. 28-31
Author(s):  
V.A. Akrimov ◽  
◽  
I.M. Grechanyuk ◽  
Yu.O. Smashnyuk ◽  
V.G. Grechanyuk ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Protective Coatings ◽  
Turbine Blades ◽  
Industrial Technology ◽  
Gas Turbine Blades

Heat resistance of gas turbine blades with protective coatings

1986 ◽  
Vol 18 (5) ◽  
pp. 610-615 ◽  
Author(s):  
A. P. Voloshchenko ◽  
G. N. Tret'yachenko ◽  
L. B. Getsov ◽  
B. M. Zinchenko ◽  
I. S. Malashenko ◽  
...  
Keyword(s):  
Heat Resistance ◽  
Gas Turbine ◽  
Protective Coatings ◽  
Turbine Blades ◽  
Gas Turbine Blades

An X-ray study of residual macrostresses in protective coatings for gas-turbine blades

1997 ◽  
Vol 39 (11) ◽  
pp. 484-488
Author(s):  
Yu. D. Yagodkin ◽  
K. M. Pastukhov ◽  
E. V. Milyaeva ◽  
S. A. Muboyadzhyan ◽  
S. A. Budinovskii
Keyword(s):  
Gas Turbine ◽  
Protective Coatings ◽  
Turbine Blades ◽  
X Ray ◽  
Gas Turbine Blades ◽  
Residual Macrostresses

scholarly journals Investigation of the Relationship between Degradation of the Coating of Gas Turbine Blades and Its Surface Color

Materials ◽  
2021 ◽  
Vol 14 (24) ◽  
pp. 7843
Author(s):  
Mariusz Bogdan ◽  
Józef Błachnio ◽  
Artur Kułaszka ◽  
Dariusz Zasada
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Protective Coatings ◽  
Turbine Blades ◽  
Operating Time ◽  
Surface Color ◽  
Metallographic Examination ◽  
Gas Turbine Blades ◽  
Study Results ◽  
The Relationship

This article presents issues concerning the relationship between the degradation of the coating of gas turbine blades and changes in the color of its surface. Conclusions were preceded by the determination of parameters characterizing changes in the technical condition of protective coatings made based on a metallographic examination that defined the morphological modifications of the microstructure of the coating, chemical composition of oxides, and roughness parameters. It has been shown that an increased operating time causes parameters that characterize the condition of the blades to deteriorate significantly. Results of material tests were compared with those of blade surface color analyses performed using a videoscope. Image data were represented in two color models, i.e., RGB and L*a*b* with significant differences being observed between parameters in both representations. The study results demonstrated a relationship between the coating degradation degree and changes in the color of the blade’s surface. Among others, this approach may be used as a tool to assess the condition of turbine blades as well as entire gas turbines.

Influence of temperature, protective coatings, and accrued service life on the fatigue resistance of gas turbine blades of cast �p539LM high-temperature strength alloy

1986 ◽  
Vol 18 (11) ◽  
pp. 1486-1491
Author(s):  
V. I. Romanov ◽  
B. A. Gryaznov ◽  
A. A. Rabinovich ◽  
O. G. Zhiritskii ◽  
I. S. Malashenko ◽  
...  
Keyword(s):  
High Temperature ◽  
Service Life ◽  
Gas Turbine ◽  
Fatigue Resistance ◽  
Protective Coatings ◽  
Turbine Blades ◽  
High Temperature Strength ◽  
Influence Of Temperature ◽  
Gas Turbine Blades ◽  
Strength Alloy

Corrosion longevity of gas turbine blades protective coatings

2010 ◽  
Vol 57 (1) ◽  
pp. 28-33 ◽  
Author(s):  
V. I. Nikitin
Keyword(s):  
Gas Turbine ◽  
Protective Coatings ◽  
Turbine Blades ◽  
Gas Turbine Blades

Thermal fatigue resistance of protective coatings for gas turbine blades

1995 ◽  
Vol 13 (3) ◽  
pp. 125-131 ◽  
Author(s):  
A. I. Rybnikov ◽  
L. B. Getsov
Keyword(s):  
Gas Turbine ◽  
Fatigue Resistance ◽  
Thermal Fatigue ◽  
Protective Coatings ◽  
Turbine Blades ◽  
Thermal Fatigue Resistance ◽  
Gas Turbine Blades
Sign in / Sign up

Export Citation Format

Share Document