Assembly Process Bill Of Material Construction Technology For Spacecraft Assembly And Integration Based On Proengineer

DOI

10.2991/jimec-17.2017.114How to use a DOI?

Keywords

Digital Assembly; BOM; Pro/E;PDM.

Abstract

Spacecraft is a complex electromechanical thermocouple system, which composed of several subsystems and thousands of products. The spacecraft assembly process is to assemble the products in the main structure of the spacecraft, and completes the relevant detection and testing. The spacecraft development unit can be divided into overall design, subsystem design and manufacturing integration department. This paper introduces the PBOM automatic construction principle and workflow based on Pro/E. Finally, this paper describes the improved efficiency and reliability of the software.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Wan Bi-le
AU  - He Wen-xing
AU  - Chen Chang-yu
PY  - 2017/10
DA  - 2017/10
TI  - Assembly Process Bill Of Material Construction Technology For Spacecraft Assembly And Integration Based On Proengineer
BT  - Proceedings of the 2017 2nd Joint International Information Technology, Mechanical and Electronic Engineering Conference (JIMEC 2017)
PB  - Atlantis Press
SP  - 530
EP  - 533
SN  - 2352-538X
UR  - https://doi.org/10.2991/jimec-17.2017.114
DO  - 10.2991/jimec-17.2017.114
ID  - Bi-le2017/10
ER  -