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.