Plasma-Sprayed Thermal Barrier Coatings (TBC) for Aero-Engine Turbine Blades

Plasma-Sprayed Thermal Barrier Coatings (TBC) for Aero-Engine Turbine Blades

Plasma spraying feeds powder into a plasma jet hotter than 10 000 °C. Particles melt or soften, are accelerated to several hundred metres per second, strike the substrate, flatten into lamellae and freeze instantly. A thermal barrier coating therefore grows as thousands of stacked, overlapping splats — a layered structure with a controlled level of porosity (typically 4–20% for APS) and a small amount of oxide inclusion. Vacuum or shrouded-plasma spraying reduces those defects where required.

TBC Structure

LayerMaterialFunction
Top coat7–8YSZ (ZrO₂-Y₂O₃), 0.1–0.4 mmLow thermal conductivity, phase stability to 1200 °C
Bond coatNiCoCrAlY / MCrAlY, 0.1–0.15 mmOxidation barrier, stress relief
SubstrateNickel-base superalloyLoad-carrying blade or vane

With film cooling, such a coating can reduce superalloy surface temperature by roughly 100–170 °C, extending blade creep life by an order of magnitude and enabling higher turbine inlet temperatures.

What Controls Coating Quality

  • Powder quality – flowability, size distribution and phase content of the YSZ powder set the ceiling for density and stability.
  • Plasma parameters – arc power, gas mixture and stand-off determine particle melting and velocity; improper settings leave unmelted particles and weak splat boundaries.
  • Bonding – attachment is mostly mechanical interlocking with the roughened substrate, aided by diffusion; grit-blasting cleanliness is critical.
  • Directional properties – because the structure is lamellar, conductivity and modulus differ through-thickness and in-plane; spray angle consistency keeps this predictable.

The equipment side is covered in plasma spraying ceramic coating process and our SX-80 plasma spraying system.

Frequently Asked Questions

What is a thermal barrier coating made of?

A typical air-plasma-sprayed TBC is a 100-400 um top coat of 7-8 wt% yttria-stabilised zirconia (YSZ) over an MCrAlY or NiCoCrAlY bond coat. YSZ has very low thermal conductivity and a thermal expansion close to that of superalloys, which keeps thermal stresses low.

Why does a TBC deliberately contain porosity?

Layered, slightly porous microstructure lowers thermal conductivity by 20-40% versus dense material and relieves thermal expansion mismatch stress. Too much porosity, however, weakens erosion resistance, so porosity is specified, not left to chance.