航空发动机二次空气系统密封设计的多保真度仿真

A. Nasti, I. Voutchkov, David J. J. Toal, A. Keane
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引用次数: 1

摘要

航空发动机的二次空气系统密封位于系统物理的所有主要方面之间的交叉点。它们的行为受到空气系统、热物理、飞行载荷的影响,并高度依赖于发动机部件的运动、运行条件和配套硬件。由于发动机中存在大量的功能和物理接口,因此密封设计是一个高度耦合的多物理场问题,需要在设计过程中进行多次迭代,以收敛到满足系统要求并优化发动机特定油耗的解决方案。在设计过程的不同阶段,可以建立具有不同保真度的仿真模型。由于高保真耦合多学科模型的长时间运行和过程的迭代性,工业密封设计面临着巨大的计算成本挑战,特别是在需要多次模拟运行的设计阶段。代理建模和优化的多保真度计算技术,如Kriging和co-Kriging,已经在许多工业应用中得到了证明,并且有可能显著减少计算成本高昂的优化问题的功能评估数量,提高代理模型预测的准确性,并允许针对特定产品设计开发改进的仿真策略。本文演示了多保真度仿真技术在航空发动机二次空气系统密封设计中的应用,并展示了这些技术如何在系统、子系统和部件设计中应用。这是通过将简单的二维有限元分析结果与耦合二次风系统-热力学模型的结果相结合来实现的。根据设计过程的阶段和所做的具体设计决策,在模拟中计算能力的使用通常归结为减少总体计算时间和提高结果准确性之间的权衡。多保真度仿真框架为驱动仿真策略的整体选择提供了环境,降低了设计成本,并在工业响应市场变化或新技术方面提供了灵活性。此外,该方法建立了在产品生命周期的每个步骤更新虚拟产品的基础设施,允许实验或服务数据馈送系统级仿真模型以产生数字孪生。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Multi-Fidelity Simulation for Secondary Air System Seal Design in Aero Engines
Secondary air system seals in aero engines sit at the intersection between all the major aspects of the physics of the system. Their behavior is affected by the air system, the thermal physics, the effect of flight loads and is highly dependent on the engine component movements, the operating conditions, and the supporting hardware. Due to the number of functional and physical interfaces in the engine, seal design is therefore a highly coupled multi-physics problem and requires multiple iterations during the design process to converge to a solution that meets system requirements and optimizes engine specific fuel consumption. At different stages of the design process, simulation models with different levels of fidelity can be built. Due to the long runtimes of high-fidelity coupled multi-disciplinary models and to the iterative nature of the process, seal design in industry presents significant computational cost challenges, in particular in the phases of the design that require multiple simulation runs. Multi-fidelity computational techniques for surrogate modelling and optimization such as Kriging and co-Kriging have been demonstrated on a number of industrial applications and have the potential to significantly reduce the number of function evaluations for computationally expensive optimization problems, improve the accuracy of the predictions of surrogate models and allow the development of improved simulation strategies for a specific product design. This paper demonstrates the use of multi-fidelity simulation techniques on aero engine secondary air system seal design and shows how these techniques can be used in the context of system, sub-system and component design. This is achieved by combining results from a simple two-dimensional Finite Element Analysis with those from a coupled secondary air system-thermomechanical model. Depending on the stage of the design process and on the specific design decisions being made, the use of computational power in simulation often comes down to a trade-off between reduced overall computational time and improved result accuracy. Multi-fidelity simulation frameworks provide the environment to drive holistic choices on the simulation strategy, reducing the cost of the design and offering agility in the industrial response to market changes or new technologies. Moreover, this methodology establishes an infrastructure for updating the virtual product at each step of the product lifecycle, allowing experimental or service data to feed the system-level simulation models to produce a digital twin.
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