LIU Lin-sheng 1 , WANG Bin 1 , PENG Ju 2 , YE Zhi-feng 1.Multi-Objective Optimal Control of Water-Saturated Fuel Based on Improved NSGA-II-FLC[J].航空发动机,2024,50(6):125-131
Multi-Objective Optimal Control of Water-Saturated Fuel Based on Improved NSGA-II-FLC
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Key Words:improved non-dominated sorting genetic algorithm-II  fuzzy logic controller  water-saturated fuel  multi-objective optimization  intermediate medium heat transfer oil
Author NameAffiliation
LIU Lin-sheng 1 , WANG Bin 1 , PENG Ju 2 , YE Zhi-feng 1 1. College of Energy and Power EngineeringNanjing University of Aeronautics and AstronauticsNanjing 210016China 2. AECC Sichuan Gas Turbine EstablishmentMianyang Sichuan 621703China 
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Abstract:To solve the problem of heat exchanger wall icing due to excessive temperature difference between fuel and heat transfer oil in the preparation of water-saturated fuel for fuel icing airworthiness tests, a multi-objective optimization method was proposed to improve the dynamic optimization of Non-dominated Sorting Genetic Algorithm-II (NSGA-II) optimal individual input fuzzy logic control? ler to achieve accurate temperature control of the water-saturated fuel. Based on the thermal hydraulicand two-phase pipe flow model, a water-saturated fuel temperature control system with intermediate medium heat transfer oil was built, and the reliability of the simulation model was verified with the test temperature control system, and the system under different temperature conditions was simulated and analyzed. The system temperature settling time defined in the control algorithm was optimized, and the fitness value of temperature differ? ence control was used as the decision objective, the Good Point Set method was introduced to initialize the population, and the Cauchy Mutation (CM) method with variable inertia weight was used to optimize the iterative process. The global optimal control parameters obtained from the improved NSGA-II optimization were fed into the fuzzy logic controller, and the Slope of the parameters in the controller were self-tuned to realize the dynamic optimization of the temperature control model. The results show that the improved NSGA-II-FLC multi-objective optimal control can shorten the temperature settling time, improve the temperature control accuracy by about 50%, and make the temperature difference close to but not exceeding 13℃, which meets the airworthiness requirements.
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