Design of Thermal Barrier Coatings Thickness for Gas Turbine Blade Based on Finite Element Analysis

Figure 1

Geometries of a gas turbine rotor blade: (a) blades mounted around a rotor disk, (b) suction side view, (c) pressure side view, (d) top view, (e) dimensions of cross section A-A, and (f) internal cooling passages.

(a)

(b)

(c)

(d)

(e)

(f)