Aero-engine compressor stator blade ice crystal icing prediction system

The invention relates to the field of ground simulation tests for simulating ice crystal icing of aero-engine compressor blades, in particular to an ice crystal icing prediction system for aero-engine compressor stator blades. The system comprises a test piece blade system and a ground simulation aero-engine blade ice crystal icing test system. The test piece blade system is used for simulating a real aero-engine compressor stator blade, is used as an ice crystal icing part in a test, and is mounted in the ground simulation aero-engine blade ice crystal icing test system; the ground simulation aero-engine blade ice crystal icing test system is used for conveying ice crystals to the test piece blade system for an ice crystal icing test. The system can be used for predicting whether ice crystal freezing occurs on the aero-engine compressor stator blade or not according to the temperature change of the aero-engine compressor stator blade. 本发明涉及模拟航空发动机压气机叶片冰晶结冰地面模拟试验领域，尤其是涉及一种航空发动机压气机静子叶片冰晶结冰预测系统。系统包含试验件叶片系统和地面模拟