Combustion chamber structure parameter design optimization method and device
By establishing a surrogate model and genetic algorithm in the combustion chamber design, the combustion chamber parameters are quickly optimized, solving the multi-objective optimization problem caused by large computational load and complex modeling in the existing technology, and realizing efficient thermoacoustic oscillation control under complex operating conditions.
Patent Information
- Application Number
- CN202511722991.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-21
- Publication Date
- 2026-03-06
AI Technical Summary
Existing technologies in combustion chamber design suffer from high computational demands, complex modeling, or sensitivity to boundary conditions, making it difficult to achieve multi-objective optimization quickly and cost-effectively. In particular, they struggle to effectively control thermoacoustic oscillations under complex operating conditions, thus limiting their application effectiveness.
By acquiring the basic structure and operating conditions of the combustion chamber, selecting the parameters to be optimized and determining their value range and constraints, establishing a surrogate model, using the modal growth rate as the optimization objective, and combining three-dimensional finite element analysis and genetic algorithm, the design parameters of the combustion chamber are iteratively optimized, and the modal frequency and growth rate of the combustion chamber are established, thus achieving rapid and low-cost multi-objective optimization.
It can quickly and cost-effectively obtain optimal design parameters under limited computing or experimental resources, simplify the experimental process, reduce the cost of experiments or large eddy simulations, improve the accuracy of thermoacoustic oscillation prediction and the robustness of design schemes, and is suitable for efficient prediction of multi-parameter, multi-dimensional combustion chamber thermoacoustic oscillation modes.
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