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基于模型的系统工程在高速飞行器引气系统设计中的应用研究

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针对组合动力高速飞行器面对的严峻热负载与高电气负载问题,采用基于模型的系统工程方法,从冲压模态无轴功输出、冲压空气温度过高等新约束出发,以需求为基线进行了高速飞行器引气系统逻辑架构、物理架构、组件方案的设计,并进行了系统方案的集成验证,设计方案基本满足约束.结果表明:由进气道引气、空气-燃油换热器预冷、冲压空气涡轮发电制冷等核心硬件组成的引气系统方案可以满足高速飞行器巡航阶段能源需求,采用基于模型的系统工程方法能够有效推动系统迭代设计,提升复杂系统设计的可靠性和效率.
Research on the application of model-based system engineering in the design of bleed air system of high-speed vehicle
In view of the severe thermal load and high electrical load problems faced by the combined power high-speed vehicle,a model-based system engineering method is adopted for the design.The design starts from the new constraints of no shaft power output and high stamping air temperature in stamping mode.Based on the requirements,the logical architecture,physical architecture and component solution of the bleed air system of high-speed vehicle are designed.The system solution consists of core hardware such as air inlet,air-fuel heat exchanger and ram air turbine.The integration verification of the system solution is also carried out,which basically meets the constraints.The results show that the bleed air system solution can meet the energy requirements of high-speed vehicle during the cruise phase.It also shows that the model-based system engineering method can effectively promote the iterative system design and improve the reliability and efficiency of complex system design.

model-based system engineeringhigh-speed vehiclebleed air systemmodeling meth-odsimulation verification

李昕、褚显应、郭健、王全平、张洪礼

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北京空天技术研究所,北京 100074

基于模型的系统工程 高速飞行器 引气系统 建模方法 仿真验证

2024

空天技术
北京海鹰科技情报研究所(中国航天科工集团第三研究院310研究所)

空天技术

CSTPCD北大核心
影响因子:0.402
ISSN:2097-0714
年,卷(期):2024.(1)
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