| Citation: | YIN Zeyong, MI Dong, ZHANG Lizhang, et al. Multidisciplinary design optimization method of overall aircraft power system[J]. Journal of Aerospace Power, 2022, 37（10）：2025-2045 doi: 10.13224/j.cnki.jasp.20220453
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In view of the difficulties in the design optimization of an overall aircraft power system, such as the considerable calculation scale, complex coupling relationships, sharp discipline conflicts and complicated implementation processes, a variety of advanced technologies such as the high-precision surrogate models, the efficient optimization strategies and the intelligent multi-objective optimization algorithms were developed and applied in three aspects: system decomposition, system modelling and system solution. Finally, the design method of an overall aircraft power system based on multidisciplinary design optimization (MDO) was established. Taking a turboshaft engine, a turbofan engine, a turbojet engine and a main transmission chain of the main reducer of a helicopter transmission system as examples, the engineering application research on MDO of the overall aircraft power system was carried out. Moreover, the performance and strength tests of the optimised compressor, and the optimised overall system test were carried out and verified for the turbojet engine. The research showed that the MDO of the overall aircraft power system could effectively unleash the design potential, significantly improve the comprehensive performance of products and considerably shorten the development cycle. Its engineering application prospect is quite broad, which will change the design and development of an aircraft power system.
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