|Table of Contents|

Analysis and application of heterogeneous CAD 3D model assembly technology for liquid rocket engine (PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2023年02期
Page:
94-99
Research Field:
目次
Publishing date:

Info

Title:
Analysis and application of heterogeneous CAD 3D model assembly technology for liquid rocket engine
Author(s):
LIN Yuan XIONG Lifang HU Haifeng
(Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
Keywords:
liquid rocket engine heterogeneous CAD BOM structure 3D model assembly
PACS:
V434; TP391
DOI:
-
Abstract:
In view of the application status of liquid rocket engine 3D model assembly technology, the data formats of different 3D modeling tools are incompatible with each other and cannot be by called each other.In the management system of product data, the heterogeneous CAD 3D model assembly cannot automatically generate the product BOM structure, and the assembly information cannot be transmitted across software.The problems are studied in this paper, such as the study on the mutual transfer for Pro/E and NX 3D structure, the assembly of heterogeneous 3D structure, automatic generation of product BOM structure, and the synchronization of changes.The lightweight model JT and intermediate format are adopted to realize the assembly and management of heterogeneous CAD 3D models.Adopting the lightweight model JT assembly method can not only ensure the consistency between JT and 3D assembly model, but also realize the automatic generation and update of assembly BOM structure.The STEP intermediate format is adopted for assembly, which solves the conversion control of lightweight models in the management system of product data, reduces the assembly requirements of heterogeneous 3D models in the CAD integrated environment, ensures the consistency between STEP files and 3D models, and achieves the automatic update of BOM structure of heterogeneous CAD 3D models and the control of engine technical status in the unified environment.

References:

[1] 徐伟,姜丽红,蔡鸿明.基于BOM的企业异构信息系统集成[J].东华大学学报(自然科学版),2012,38(5):498-504.
[2] 赵罡,郑湃,闫光荣,等.一种基于复杂产品异构BOM的定制查询方法:CN102426587A[P].2012-04-25.
[3] 魏然.固体火箭发动机模板化设计与优化研究[D].西安:西北工业大学,2015.
[4] 行开新,田凌.支持异地协同设计的异构CAD虚拟装配系统[J].清华大学学报(自然科学版),2009,49(2):226-231.
[5] 刘巍.异构CAD模型虚拟装配技术研究[D].武汉:华中科技大学,2013.
[6] KIM Y,LEE H,SAFDAR M,et al.Exchange of parametric assembly models based on neutral assembly constraints[J].Concurrent Engineering,2019,27(4):285-294.
[7] 王耀东,魏强,李学林,等.基于特征参数化方法的异构CAD卫星三维协同布局设计[J].航天器工程,2018,27(4):28-33.
[8] 宫潘威,时小磊,陶高周,等.CREO环境下三维模型及信息集成共享实现方法研究[J].机械设计与制造,2019(2):218-221.
[9] 周培,刘敏,李莉,等.一种基于Creo软件的三维零件模型版本比对系统:CN201711116288.9[P].2018-04-20.
[10] 周培,刘铭,王腾,等.基于几何配准的三维模型几何比对方法研究[J].图学学报,2016,37(4):483-490.
[11] ZIENKIEWICZ J,TSIOTSIOS A,DAVISON A,et al.Monocular,real-time surface reconstruction using dynamic level of detail[C]//2016 Fourth International Conference on 3D Vision(3DV).Stanford,CA:IEEE,2016.
[12] AKENINE-MO L T,HAINES E,HOFFMAN N.Real-time rendering[M].Boca Raton,FL:A K Peters/CRC Press,2019.
[13] KWON S,KIM B C,MUN D,et al.User-assisted integrated method for controlling level of detail of large-scale B-rep assembly models[J].International Journal of Computer Integrated Manufacturing,2018,31(9):881-892.
[14] 邵晓东,陈锋,刘焕玲,等.基于特征的异构CAD模型转换技术研究[J].中国机械工程,2007,18(1):60-64.
[15] 王启富,杨磊,黄运保,等.协同产品开发中的产品模型轻量化技术[J].计算机辅助设计与图形学学报,2006,18(1):108-113.
[16] BRONSVOORT W F,BIDARRA R,NYIRENDA P J.Developments in feature modelling[J].Computer-Aided Design and Applications,2006,3(5):655-664.
[17] CHEN Z M,GAO S M,LI W D.An approach to incremental feature model conversion[J].The International Journal of Advanced Manufacturing Technology,2007,32(1/2):99-108.
[18] 李广文,黄翔,李迎光,等.CAD装配模型质量的研究[J].中国制造业信息化,2004,33(1):96-98.
[19] 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.
[20] 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(4):82-89.
HU H F,LIU F,XU T,et al.Key technologies of collaborative design platform for liquid rocket engine[J].Journal of Rocket Propulsion,2020,46(4):82-89.

Memo

Memo:
-
Last Update: 1900-01-01