WANG Jia-wen 1 , HUANG Xiang-hua 2 , JI Run-min 2.Correction Method of Component Characteristics for Gas Turbine Based on Characteristic Data[J].航空发动机,2024,50(3):114-121
Correction Method of Component Characteristics for Gas Turbine Based on Characteristic Data
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Key Words:component level model  characteristic correction  off-design point matching  gas turbine engine
Author NameAffiliation
WANG Jia-wen 1 , HUANG Xiang-hua 2 , JI Run-min 2 1. AECC Aero Engine Control System InstituteWuxi Jiangsu 214013China 2. College of Energy and Power EngineeringNanjing University of Aeronautics and AstronauticsNanjing 210016China 
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Abstract:A gas turbine engine component characteristic correction method based on characteristic data is proposed to address the problem of errors between the model calculation parameters and the actual test parameters caused by the mismatch of gas turbine engine component characteristics. By varying the scaling reference center, overall corrections of the design point and the idle point are carried out sequentially to achieve a rough coverage of the characteristic map over the entire range of working conditions. By locally correcting the characteristic data of the rectangular area defined by the adjacent constant speed lines and β lines where the off-design points are located, and additionally correcting other data points of the constant speed line by interpolation method and ellipse fitting method, the characteristic map matching with the test data obtained finally. The simulation verification was conducted on a turbofan engine, and the results show that the method can accurately and quickly correct the engine component characteristics. Compared with the test data, the error of each corrected steady-state point is within 1.5%, which meets the engineering accuracy requirements and can be used for engine control system research.
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