固体发动机数字孪生框架及关键技术分析
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国防科技大学空天科学学院

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V19

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Analysis of the framework and key technologies of solid rocket motor digital twin system
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    摘要:

    固体发动机具有结构简单、可靠性高、推力大等优点,是航空运输、导弹武器的重要动力装置。为了突破固体发动机长期以来以经验、半经验为主的传统设计与管理模式,降低设计、研制、维护难度,建立起围绕固体发动机全生命周期的管理模式,满足固体发动机快速更新迭代、数字化、智能化的发展需求,本文从数字孪生概念出发,将数字孪生的发展历程分为四个阶段:物理仿真、计算机仿真、以虚映实、虚实结合,建立了固体发动机数字孪生各个阶段的系统框架,并总结了各阶段关键技术,以此作为技术路线,牵引相关学科发展和技术积累,为固体发动机数字孪生系统的研究与应用提供理论参考。

    Abstract:

    solid rocket motors have the advantages of simple structure, high reliability, and large thrust. They have become an important power device for air transportation and missile, are a key research object for aviation and aerospace superpower. In order to break through the traditional design and management model of solid engines that has long been based on experience and semi-experience, reduce the difficulty of design, development, and maintenance, A management model should be established around the entire lifecycle of solid rocket motors to meet the development needs of rapid iteration, digitization, and intelligence of solid rocket motors. Based on the concept of digital twins, this article divides the development process of digital twins into four stages: physical simulation, computer simulation, virtual reality mapping, virtual reality combination, establishes a digital twin system framework for each stage of solid rocket motors, and the key technologies at each stage were summarized. These can be used as technical routes to promote the development of related disciplines and technology accumulation, and provide theoretical reference for the research and application of solid engine digital twin systems.

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  • 收稿日期:2024-01-11
  • 最后修改日期:2024-11-01
  • 录用日期:2024-08-19
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