Aero-engine blade in-service in-situ video eddy current infrared detection system
By designing an integrated in-situ video eddy current infrared detection system for aircraft engine blades, the eddy current detection coil assembly, endoscope video head and infrared camera are used to achieve refined detection of eddy currents in the complex structure of aircraft engine blades, solving the problems of low detection efficiency and weak data fusion in the prior art, and improving detection accuracy and efficiency.
Patent Information
- Application Number
- CN202411743485.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-30
- Publication Date
- 2025-03-18
AI Technical Summary
The prior art is difficult to achieve rapid in-situ detection of refined eddy current in-service blades in complex structures of aircraft engines, and conventional methods have low detection efficiency and weak data fusion.
A system for in-situ video eddy current infrared detection system for aircraft engine blades is designed, using an integrated probe and a multi-mode detector. The probe is equipped with an eddy current detection coil assembly, a binocular endoscope video head and a micro infrared camera. The detection of multiple defects is achieved through time sharing, multi-mode operation and attitude adjustment.
It realizes rapid in-situ detection of various defects on the thermal barrier coating of aircraft engine blades, improves detection sensitivity and accuracy of infrared thermal imaging signals, eliminates the impact of coils on infrared signals, and integrates sensors and miniaturizes them, and significantly improves detection efficiency.