High-pressure turbine blades in modern jet engines operate in environments that exceed the melting point of their underlying metal alloys. To survive these extreme conditions, advanced ceramic thermal barrier coatings are applied directly to turbine surfaces to insulate the base metal from destructive exhaust heat. These multi-layer ceramic coatings can lower the substrate alloy's surface temperature by up to 300 degrees Fahrenheit. While specialized internal cooling channels also circulate compressed air through the blade core, the ceramic barrier remains the primary defense against thermal degradation. Without this insulating ceramic layer, turbine components would rapidly suffer structural failure and creep deformation.
Which of the following statements best expresses the main idea of the passage?
- ASpecialized internal cooling channels circulate compressed air through the blade core to lower internal temperatures.
- BModern jet engines require all structural components to be constructed from multi-layer ceramic materials.
- Ceramic thermal barrier coatings are applied to protect jet engine turbine blades from damaging operational heat.Answer
- DCeramic coatings reduce the surface temperature of underlying turbine alloys by up to 300 degrees Fahrenheit.