中国飞机强度研究所建所 60 周年专刊

基于模型驱动的飞机强度积木式验证需求规划与能力匹配

  • 邹鹏 ,
  • 杨钧超 ,
  • 陈向明 ,
  • 李磊 ,
  • 梁勇 ,
  • 刘漪纹
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  • 1.中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065
    2.中航通飞华南飞机工业有限公司,珠海 519040
    3.中国航空综合技术研究所,北京 100028
.E-mail: zoupeng_0625@126.com

收稿日期: 2025-06-13

  修回日期: 2025-07-03

  录用日期: 2025-07-09

  网络出版日期: 2025-07-15

基金资助

国家级项目

Model-driven requirement capturing and capability matching of aircraft structural strength building-block verification

  • Peng ZOU ,
  • Junchao YANG ,
  • Xiangming CHEN ,
  • Lei LI ,
  • Yong LIANG ,
  • Yiwen LIU
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  • 1.National Key Laboratory of Strength and Structural Integrity,Aircraft Strength Research Institute of China,Xi’an 710065,China
    2.AVIC General Huanan Aircraft Industry Co. ,Ltd,Zhuhai 519040,China
    3.AVIC China Aero-polytechnology Establishment,Beijing 100028,China

Received date: 2025-06-13

  Revised date: 2025-07-03

  Accepted date: 2025-07-09

  Online published: 2025-07-15

Supported by

National Level Project

摘要

结构强度验证是飞行器研发过程中的重要环节,为了应对验证需求规划、技术能力匹配、成本预算控制和周期进度把控等诸多挑战,开展了基于模型驱动的飞机强度积木式验证需求规划与能力匹配研究。构建面向飞机强度积木式验证需求规划与能力匹配的数据捕获方法,形成需求与能力模型数据库,建立二者映射关系。基于捕获的强度验证需求数据,开展积木式验证规划,实现利益攸关方需求、顶层需求、系统需求到验证需求的全流程追溯,并能够根据结构、研制阶段、场景等进行分类规划与需求完善更新。依据虚实融合的积木式试验规划策略,构建成本、风险及周期等多约束下的积木式试验规划算法,实现验证能力的按需匹配与试验资源的有效管控。集成以上方法、数据、模型,构建基于MBSE(Model-Based Systems Engineering)的民机强度验证规划与管理平台,为民机研制提供强度验证规划手段。

本文引用格式

邹鹏 , 杨钧超 , 陈向明 , 李磊 , 梁勇 , 刘漪纹 . 基于模型驱动的飞机强度积木式验证需求规划与能力匹配[J]. 航空学报, 2025 , 46(21) : 532418 -532418 . DOI: 10.7527/S1000-6893.2025.32418

Abstract

The verification of aircraft structural strength is an important part of aircraft development process. In order to address many challenges such as verification system planning, technical capability matching, cost budget control, and cycle schedule control, this paper conducted research on model-driven requirement capturing and capability matching for aircraft structural strength building-block verification. A data capture method for aircraft strength building-block based verification requirement planning and capability matching was constructed, a model database was formed, and their mapping relationships were established. Based on the captured strength verification requirement data, a building-block verification plan was carried out to achieve full process traceability from stakeholder requirements, top-level requirements, and system requirements to verification requirements. And the plan can be classified and updated according to structure, development stage, scenario, etc. According to the building-block verification planning strategy of virtual-real integration, a planning algorithm with multiple constraints such as cost, risk, and cycle was constructed to achieve on-demand matching of verification capabilities and effective control of experimental resources. Integrating the above methods, data, and models, a Model-Based Systems Engineering (MBSE) based civil aircraft strength verification planning and management platform was built, providing strength verification planning tools for civil aircraft development.

参考文献

[1] 邹鹏, 杨钧超, 陈向明, 等. 航空飞行器结构强度物理试验技术成熟度评价方法[J]. 航空学报202445(24): 230414.
  ZOU P, YANG J C, CHEN X M, et al. Readiness assessment system method of physical testing of aircraft structural strength[J]. Acta Aeronautica et Astronautica Sinica202445(24): 230414 (in Chinese).
[2] 贺东风, 赵越让, 钱仲焱, 等. 中国商用飞机有限责任公司系统工程手册[M]. 上海: 上海交通大学出版社, 2017: 1-16.
  HE D F, ZHAO Y R, QIAN Z Y. COMAC systems engineering mannual[M]. Shanghai: Shanghai Jiao Tong University Press, 2017: 1-16 (in Chinese).
[3] 郭泰, 钱馨, 宫綦, 等. 基于模型的民机验证需求捕获及应用技术[J]. 北京航空航天大学学报202248(10): 1933-1942.
  GUO T, QIAN X, GONG Q, et al. Methodology for model based verification requirements capturing and application in civil aircraft development[J]. Journal of Beijing University of Aeronautics and Astronautics202248(10): 1933-1942 (in Chinese).
[4] 毕文豪, 范秋岑, 李德林, 等. 基于多视角的民机正向设计建模方法[J]. 航空学报202344(10): 227536.
  BI W H, FAN Q C, LI D L, et al. Modeling approach for forward design of civil aircraft based on multiple perspectives[J]. Acta Aeronautica et Astronautica Sinica202344(10): 227536 (in Chinese).
[5] 刘晚移, 冯蕴雯, 侯杰然, 等. Harmony SE在民用飞机设计中的应用[J]. 西北工业大学学报202442(1): 35-44.
  LIU W Y, FENG Y W, HOU J R, et al. Application of Harmony SE in civil aircraft design[J]. Journal of Northwestern Polytechnical University202442(1): 35-44 (in Chinese).
[6] 胡晓义, 王如平, 王鑫, 等. 基于模型的复杂系统安全性和可靠性分析技术发展综述[J]. 航空学报202041(6): 523436.
  HU X Y, WANG R P, WANG X, et al. Recent development of safety and reliability analysis technology for model-based complex system[J]. Acta Aeronautica et Astronautica Sinica202041(6): 523436 (in Chinese).
[7] 国际系统工程协会. 系统工程手册: 系统生命周期流程和活动指南[M]. 张新国, 译. 北京: 机械工业出版社, 2013.
  International Council on Systems Engineering. Systems engineering handbook: A guideline for system life cycle processes and activities[M]. ZHANG X G, translated. Beijing: China Machine Press, 2013 (in Chinese).
[8] 孙霄剑, 罗明强, 张驰, 等. 民用飞机预研论证权威真相源构建技术[J]. 航空学报202142(2): 224222.
  SUN X J, LUO M Q, ZHANG C, et al. Construction technology of authoritative source of truth for civil aircraft pre-research[J]. Acta Aeronautica et Astronautica Sinica202142(2): 224222 (in Chinese).
[9] 李德林, 毕文豪, 张安, 等. 基于MBSE的民机研制过程管理[J]. 系统工程与电子技术202143(8): 2209-2220.
  LI D L, BI W H, ZHANG A, et al. MBSE-based process management in the development of civil aircraft[J]. Systems Engineering and Electronics202143(8): 2209-2220 (in Chinese).
[10] 杨莹, 丁健, 李伟. 系统工程在飞机设计上的应用与实践[J]. 装备制造技术2019(11): 140-144, 155.
  YANG Y, DING J, LI W. Application and practice of system engineering on the aircraft design[J]. Equipment Manufacturing Technology2019(11): 140-144, 155 (in Chinese).
[11] 王文浩, 毕文豪, 张安, 等. 基于MBSE的民机系统功能建模方法[J]. 系统工程与电子技术202143(10): 2884-2892.
  WANG W H, BI W H, ZHANG A, et al. Function modeling method of civil aircraft system based on MBSE[J]. Systems Engineering and Electronics202143(10): 2884-2892 (in Chinese).
[12] 毛志威, 屈展文, 张彤, 等. 基于MBSE的民机审定试飞场景设计[J]. 系统工程与电子技术202042(8): 1768-1775.
  MAO Z W, QU Z W, ZHANG T, et al. Design of civil aircraft certification test flight scenario based on MBSE[J]. Systems Engineering and Electronics202042(8): 1768-1775 (in Chinese).
[13] DATTA S, ROY R, BENDARKAR M V, et al. MBSE-enabled risk reduction for certification of novel aircraft configurations[C]∥AIAA Scitech 2022 Forum. Reston: AIAA, 2022.
[14] FAZAL B, GLINSKI S, HARRISON E, et al. An MBSE framework for regulatory modeling of transport category airplanes[C]∥AIAA Aviation 2022 Forum. Reston: AIAA, 2022.
[15] 左雪雯, 吕岸, 谢文雅, 等. 基于MBSE的飞机级需求捕获与分析方法[C]∥2020(第九届)民用飞机航电国际论坛论文集, 2020: 117-124.
  ZUO X W, LV A, XIE W Y, et al. Method of aircraft-level requirements capture and analysis based on MBSE[C]∥Proceedings of the 2020 (9th) Civil Aircraft Avionics International Forum, 2020: 117-124 (in Chinese).
[16] 王彬文, 王育鹏. 飞机强度试验[M]. 北京: 航空工业出版社, 2017.
  WANG B W, WANG Y P. Aircraft strength test[M]. Beijing: Aviation Industry Press, 2017 (in Chinese).
[17] 林建鸿. 积木式方法与试验金字塔的历史沿革与发展趋势[J]. 航空工程进展202314(5): 8-18.
  LIN J H. The historical developments and trendencies of building block approach and testing pyramid[J]. Advances in Aeronautical Science and Engineering202314(5): 8-18 (in Chinese).
[18] 孙侠生. 民用飞机结构强度刚度设计与验证指南-第三册[M]. 北京: 航空工业出版社, 2012.
  SUN X S. Guide for design and verification of structural strength and stiffness of civil aircraft-Volume Ⅲ[M]. Beijing: Aviation Industry Press, 2012 (in Chinese).
[19] 任金虎, 许鸿杰, 王英儒, 等. 民用飞机研发过程中需求闭环验证技术研究与应用[J]. 智能制造2020(11): 60-63.
  REN J H, XU H J, WANG Y R, et al. Research and application of requirement closed loop verification technology in the development process of civil aircraft[J]. Intelligent Manufacturing2020(11): 60-63 (in Chinese).
[20] 范周伟, 余雄庆, 戴亚林. 基于综合评价优化的民机顶层需求指标权衡[J]. 北京航空航天大学学报202349(9): 2415-2422.
  FAN Z W, YU X Q, DAI Y L. Trade-off for top-level requirements of commercial aircraft using comprehensive evaluation and optimization[J]. Journal of Beijing University of Aeronautics and Astronautics202349(9): 2415-2422 (in Chinese).
[21] 范周伟. 基于模型的客机需求定义与概念设计一体化研究[D]. 南京: 南京航空航天大学, 2022.
  FAN Z W. Model-based integration of requirements definition and conceptual design for commercial aircraft[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022 (in Chinese).
[22] KIM D, VERBERNE J, SOTIROPOULOS-GEORGIOPOULOS E, et al. A model-based system engineering approach to the certification of transport type aircraft[C]∥AIAA Scitech 2022 Forum. Reston: AIAA, 2022.
[23] 王想生. 基于MBSE的大型灭火飞机寿命指标需求捕获与分析技术[J]. 中国科技信息202334(6): 235-236.
  WANG X S. Capture and analysis technology for life index requirements of large firefighting aircraft based on MBSE[J]. China Science and Technology Information202334(6): 235-236 (in Chinese).
[24] 赵佶男, 梁勇. 面向适航要求的强度评定需求捕获研究[J]. 科学技术创新2023(20): 1-4.
  ZHAO J N, LIANG Y. Strength assessment requirements capturing study for airworthiness of aircraft[J]. Scientific and Technological Innovation2023(20): 1-4 (in Chinese).
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