航天推进技术研究院主办
[1]胡海峰,刘 芬,许 婷,等.液体火箭发动机协同设计平台关键技术[J].火箭推进,2020,46(04):82-89.
HU Haifeng,LIU Fen,XU Ting,et al.Key technologies of collaborative design platform for liquid rocket engine[J].Journal of Rocket Propulsion,2020,46(04):82-89.
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HU Haifeng,LIU Fen,XU Ting,et al.Key technologies of collaborative design platform for liquid rocket engine[J].Journal of Rocket Propulsion,2020,46(04):82-89.
液体火箭发动机协同设计平台关键技术
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
46
期数:
2020年04期
页码:
82-89
栏目:
研究与设计
出版日期:
2020-08-18
- Title:
- Key technologies of collaborative design platform for liquid rocket engine
- 文章编号:
- 1672-9374(2020)04-0082-08
- Keywords:
- collaborative design platform; MBD; MBSE; IPT; big data
- 分类号:
- V433
- 文献标志码:
- A
- 摘要:
- 针对液体火箭发动机协同设计工程实际需求,围绕研制数据高效流转与协同,面向产品全生命周期跨地域、跨专业特点,提出了协同设计平台框架。针对协同平台中的5项关键技术,给出了相应解决途径。基于PLM系统构建协同环境,建立统一编码,整合研制过程中的标准件、原材料等共性基础数据; 通过基于MBD的三维结构设计,采用MBSE理念,以模型为载体升级发动机设计流程; 采用线上IPT模式提升产品设计效率,同时实现全过程数据记录知识累积。采用BOM结构组织和展示不同设计阶段形成的数据; 基于Hadoop平台分布式数据存储模式,实现结构化和非结构化数据综合管理。通过工程实践验证表明,构建的协同平台实现了基于数字化模型的设计工艺定制化协同,科研生产全过程的信息整合和多维度监控,促进了业务流程持续优化和研制效率不断提升,支撑发动机研制模式的转型升级。
- Abstract:
- According to the requirement of liquid rocket engine development, the framework of collaborative design platform is proposed.The platform is focused on the efficient transfer and collaboration of research data, and the cross-region and cross-professional characteristics of the product’s full life cycle.Five key technologies in the collaborative platform are analyzed and the corresponding solutions are proposed.Based on the PLM system, collaborative environment is built, unified coding is established, and common basic data such as standard parts and raw materials are integrated in the development process.Through the MBD-based three-dimensional structure design, the MBSE concept is adopted to upgrade the engine design process with the model as the medium.The online IPT mode is adopted to improve the efficiency of product design, and the data recording in the whole process is also realized.BOM is used to organize and display data formed at different design stages.Based on the distributed data storage mode of Hadoop platform, comprehensive management of structured and unstructured data is achieved.The verification through engineering practice shows that the constructed collaborative platform realizes customized collaboration of design process based on digital model.The information integration and multi-dimensional monitoring of the whole process of scientific research and production promotes the continuous optimization of business process and the continuous improvement of development efficiency, and supports the transformation and the upgrade of development model for liquid rocket engine.
参考文献/References:
[1] 王小军, 陈海东.运载火箭数字样机工程[M].北京: 中国宇航出版社, 2017.
[2] ERIC R, JOSEPH P.Requirements development for the NASA advanced engineering environment(AEE)[C]// 42nd AIAA Aerospace Sciences Meeting and Exhibit.Reno, Nevada:AIAA,2004.
[3] 陈海东, 沈重, 张冶, 等.航天数字化应用技术的发展与趋势[J].导弹与航天运载技术, 2008(3): 23-27.
[4] SHOLBERG J, ILLBACK J.Application integration framework for a large business process redesign project[C]//Proceedings of the Conference on Object-Oriented Programming, Systems, Languages, and Applications(Addendum).Minneasota,USA:[s.n.],2000.
[5] 于勇, 陶剑, 范玉青.波音787飞机装配技术及其装配过程[J].航空制造技术, 2009(14): 44-47.
[6] CHING T H.A Comparative analysis of supply chain management practices by boeing and airbus: long-term strategic implications [D].Taiwan: Civil Engineering National Taiwan University, 2007.
[7] MATTHEW A, DEANM J.Model-based advancements at lockheed martin space systems company [C]//AIAA SPACE 2015 Conference and Exposition.Pasadena, California:AIAA,2015.
[8] OSTER C.The lockheed martin digital tapestry, 2012 INCOSE international workshop model-based systems engineering workshop[R/OL].2012.http://www.omgwiki.org/MBSE/lib/exe/fetch.php?media=mbse:mbse_iw_2012-lm_digital_tapestry-oster.pptx.
[9] MATTHEW R L, HEIDI D.Design-to-cost and robust liquid rocket engine design using PMDA/PMDO and MBSE[C]// AIAA SPACE 2014 Conference and Exposition.San Diego:AIAA, 2014.
[10] JEFFREY Z, RAYMOND K.Digital thread and twin for systems engineering: pre-MDD through TMRR[C]//55th AIAA Aerospace Sciences Meeting.Grapevine, Texas:AIAA, 2017.
[11] MARK E C.Digital engineering and U.S.army air vehicle technical description reports[C]//AIAA Scitech 2020 Forum.Orlando, FL:AIAA, 2020.
[12] DREDWARD M K.Value-creating decision analytics in a lifecycle digital engineering environment[C]//AIAA Scitech 2019 Forum.San Diego, California:AIAA, 2019.
[13] DEREGIS F, BERGOMI G.Model based approach for test and operations procedures [C]//2018 Space Ops Conference.Marseille, France:[s.n.], 2018.
[14] SEBASTIAN J I, HERZIG S J, ROBERT K.Towards a reference architecture for model-based engineering environments [C]//AIAA SPACE.Long Beach, California:AIAA,2016.
[15] 范瑞祥, 程堂明, 李彩霞, 等.长征七号运载火箭“2+9+2”可靠性工程综述[J].载人航天, 2017, 23(3): 285-289.
[16] 方建平, 宋凯歌, 米弘.并行工程在航天型号研制中的应用与实践[J].航天工业管理, 2018(5): 3-9.
[17] 姜海丽.AVIDM在航天企业中的应用[J].现代制造工程, 2005(11): 47-49.
[18] 李伟, 侯凯, 俞玉澄, 等.三维可视化装配工艺设计系统及应用[J].制导与引信, 2018, 39(2): 54-60.
[19] 刘晓玉, 杨宁.航空发动机数字化协同研制技术的应用研究[J].科技视界, 2018(11): 40-41.
[20] 秦红强, 王猛, 杨亚龙, 等.液体火箭发动机三维数字化协同设计研究[J].火箭推进, 2016, 42(3): 76-80.QIN H Q, WANG M, YANG Y L, et al.Study on 3D digital collaborative design of liquid rocket engine[J].Journal of Rocket Propulsion, 2016, 42(3): 76-80.
备注/Memo
收稿日期:2019-03-09; 修回日期:2020-04-22
作者简介:胡海峰(1986—),男,博士,高级工程师,研究领域为液体火箭发动机数字化设计技术
更新日期/Last Update:
2020-07-30