Experimental investigation of inductive sensor characteristic for blade tip clearance measurement at high temperature

Engineering

• Experimental Investigation 100%
• Blade Tip 100%
• Turbine 66%
• Measurement Error 66%
• Repeatability 66%
• Aero-Engines 33%
• Environment Temperature 33%
• Engine Performance 33%
• Temperature Change 33%
• Calibration Experiment 33%
• Fast Response 33%
• Engine Efficiency 33%
• Measuring Sensor 33%
• Gas Leakage 33%