The invention discloses a method for three-dimensional representation of stratified structure 
micrometer CT imaging of a 
turbine blade heat barrier 
coating. The method comprises the following steps: preparing a double-layer-structure heat barrier 
coating micrometer CT scanning sample; firstly, carrying out 
micrometer CT scanning on the heat barrier 
coating sample, carrying out 
ring artifact and 
beam hardening correction on projection data, then carrying out three-dimensional reconstruction to obtain three-dimensional stratified structure information, establishing a three-dimensional 
structure analysis model, and carrying out characteristic segmentation and extraction on three components, namely a 
ceramic heat insulating layer, a bonding layer and matrix 
alloy; then, analyzing the thickness of the coating, extracting the distribution of holes in the coating, calculating the 
porosity, extracting the interface 
topography of the coating, and analyzing structure characteristics such as internal defects; and finally, estimating the preparation 
process quality of the heat barrier coating by integrating the composition, thickness, 
porosity distribution, interface 
topography and the like. The method for three-dimensional representation of the stratified structure of the heat barrier coating provided by the invention is suitable for 
estimation and optimization of the spraying 
process quality of the heat barrier coating, so that the quality of the heat barrier coating can be well controlled.