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基于MBSE的新一代航空发动机总体-部件多学科协同模式

景喜双 马嘉文 毕瀛 张承阳 谢福宝 陈思宇

景喜双, 马嘉文, 毕瀛, 等. 基于MBSE的新一代航空发动机总体-部件多学科协同模式[J]. 航空动力学报, 2025, 40(11):20240587 doi: 10.13224/j.cnki.jasp.20240587
引用本文: 景喜双, 马嘉文, 毕瀛, 等. 基于MBSE的新一代航空发动机总体-部件多学科协同模式[J]. 航空动力学报, 2025, 40(11):20240587 doi: 10.13224/j.cnki.jasp.20240587
JING Xishuang, MA Jiawen, BI Ying, et al. Multidisciplinary collaborative mode for overall-component design of next-generation aero-engines based on MBSE[J]. Journal of Aerospace Power, 2025, 40(11):20240587 doi: 10.13224/j.cnki.jasp.20240587
Citation: JING Xishuang, MA Jiawen, BI Ying, et al. Multidisciplinary collaborative mode for overall-component design of next-generation aero-engines based on MBSE[J]. Journal of Aerospace Power, 2025, 40(11):20240587 doi: 10.13224/j.cnki.jasp.20240587

基于MBSE的新一代航空发动机总体-部件多学科协同模式

doi: 10.13224/j.cnki.jasp.20240587
基金项目: 北京航空航天大学前沿交叉基金(501QYJC2024146013); 两机基础科学中心重点项目(P2022-B-Ⅰ-008-001)
详细信息
    作者简介:

    景喜双(1983-),男,教授,博士,主要研究方向为数字化设计制造一体化。E-mail:tom@buaa.edu.cn

    通讯作者:

    张承阳(1990-),男,讲师,博士,主要研究方向为飞机数字化装配测量技术。E-mail:zhangchengyang@buaa.edu.cn

  • 中图分类号: V37

Multidisciplinary collaborative mode for overall-component design of next-generation aero-engines based on MBSE

  • 摘要:

    为解决设计中的协同困难和多学科仿真集成问题,采用基于模型的系统工程(MBSE)方法,构建了需求-功能-逻辑-物理(RFLP)系统工程框架,并发展了针对总体-部件的高效分解综合模型,以实现流程化建模和管理。通过开发需求条目管理、系统建模语言(SysML)可视化建模工具,以及集成性能求解器支持的部件嵌入仿真方案,建立了一个多学科协同设计平台,实现了基于MBSE的航空发动机完整正向设计流程,构建了支持多厂所、多学科和多团队协同工作的 browser/server(B/S)架构环境,为航空发动机设计提供了高效可靠的解决方案。平台支持三维结构模型的轻量化、可视化及其管理与追溯,并通过部门权限管理和审批工作流打通了正向设计全流程。以高通流双变循环发动机为例进行验证,平台提高了设计的准确性,减少了重复劳动;SysML可视化建模为后续仿真提供了坚实基础;多学科仿真集成和多方案比选加快了设计迭代速度;三维结构管理模块提高了模型评审与优化效率。

     

  • 图 1  RFLP正向设计的建模过程

    Figure 1.  Modeling process of RFLP forward design

    图 2  RFLP正向设计过程的数据关联

    Figure 2.  Data associations in the RFLP forward design process

    图 3  总体-部件协同工作流程

    Figure 3.  Overall-component collaborative workflow

    图 4  性能协同仿真的工作模式

    Figure 4.  Working mode of performance co-simulation

    图 5  结构协同设计的工作模式

    Figure 5.  Working mode of structural co-design

    图 6  基于MBSE的航空发动机多学科协同设计平台系统架构

    Figure 6.  System architecture of the multidisciplinary collaborative design platform for aero-engines based on MBSE

    图 7  需求管理主界面分区

    Figure 7.  Main interface partitioning of requirements management

    图 8  需求条目增删改查总体逻辑

    Figure 8.  Overall logic of adding, deleting, modifying, and querying requirement items

    图 9  需求两级版本示意图

    Figure 9.  Two-level version diagram of requirements

    图 10  需求基线与版本控制的功能与实现

    Figure 10.  Function and implementation of requirements baseline and version control

    图 11  SysML在线功能建模模块界面

    Figure 11.  Online functional interface of SysML modeling

    图 12  SysML在线功能建模模块图类型说明

    Figure 12.  Diagram type description of SysML online functional modeling module

    图 13  自定义SysML节点和连接流程

    Figure 13.  Custom SysML node and connection process

    图 14  航空发动机逻辑建模仿真模块框架

    Figure 14.  Framework of aero-engine logical modeling and simulation module

    图 15  航空发动机逻辑建模仿真图形化交互界面

    Figure 15.  Graphical interactive interface of aero-engine logical modeling and simulation

    图 16  多方案比选功能

    Figure 16.  Function of multi-scheme comparison

    图 17  三维结构模型管理模块界面

    Figure 17.  Interface of 3D structural model management module

    图 18  平台技术架构与技术栈

    Figure 18.  Platform technical architecture and technology stack

    图 19  发动机前风扇部件需求示例

    Figure 19.  Example of engine front fan component requirements

    图 20  需求条目更改工作流程示例

    Figure 20.  Sample requirements entry change workflow

    图 21  发动机总体用例图

    Figure 21.  Overall use case diagram of engine

    图 22  发动机总体模块定义图

    Figure 22.  Module definition diagram of engine

    图 23  发动机正推力运行时内涵道活动图

    Figure 23.  Inner duct activity diagram during forward thrust operation of engine

    图 24  发动机总体性能仿真模型

    Figure 24.  Overall engine performance simulation model

    图 25  多方案比选结果

    Figure 25.  Result of multi-scheme comparison

    图 26  发动机整机三维结构模型

    Figure 26.  3D structure model of engine

    图 27  发动机前风扇部件三维结构模型

    Figure 27.  3D structure model of engine front fan components

    表  1  需求数据库表单设计

    Table  1.   Requirements database table design

    名称 类型 描述
    req_id bigint 需求id
    item bigint 需求标号
    version bigint 需求版本
    title varchar 需求标题
    description varchar 需求描述
    dept_id varchar 依托部门
    del_flag char 逻辑删除标志
    baseline char 需求基线版本
    parent_id bigint 父需求id
    下载: 导出CSV

    表  2  需求版本数据库表单设计

    Table  2.   Requirements version database table design

    名称 类型 描述
    id bigint 需求版本ID
    is_current bit 是否当前版本
    is_base bit 是否为基版本
    baseline varchar 版本基线
    version_name varchar 版本名称
    req_ids longtext 需求条目ID
    remark varchar 备注
    creator varchar 创建者
    create_time datetime 创建时间
    updater varchar 更新者
    update_time datetime 更新时间
    deleted bit 是否删除
    下载: 导出CSV

    表  3  三维结构模型数据库表单设计

    Table  3.   3D structural model database table design

    名称 类型 描述
    id bigint 物理模型ID
    item varchar 物理编号
    objectid varchar 模型结构树ID
    title varchar 模型主标题
    description varchar 模型内容
    parent_id bigint 父一级物理模型
    dept_id bigint 依托部门
    creator varchar 创建者
    create_time datetime 创建时间
    updater varchar 更新者
    update_time datetime 更新时间
    deleted bit 是否删除
    remark varchar 备注
    model_path varchar 物理模型地址
    req_id bigint 关联需求ID
    下载: 导出CSV
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  • 收稿日期:  2024-08-21
  • 网络出版日期:  2025-06-06

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