Read the following passage:
Modern aviation turbofan engines operate at combustion temperatures exceeding the melting thresholds of high-strength nickel-base superalloys. To protect high-pressure turbine blades, manufacturers deposit thin ceramic thermal barrier coatings, predominantly yttria-stabilized zirconia, onto metallic components via electron-beam physical vapor deposition. Rather than directly cooling the underlying metal, this ceramic layer exhibits extremely low thermal conductivity, creating a steep temperature drop across its thickness while internal compressor bleed air circulates through cast cooling passages within the blade core. Consequently, the ceramic insulation permits elevated combustor discharge temperatures without subjecting the supporting structural metal to thermal deformation.
Based on the passage, the ceramic coating prevents structural distortion of turbine components by resisting heat transmission and establishing a sharp thermal gradient across its depth.
Answer: Answer