Volume 48 Issue S1
May  2019
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Yang Zipeng, Liu Min, Zhou Youjun, Dong Peng, Yang Chuancheng. Study on processing scheme and precision measurement method of payload adapter with irregular shape[J]. Infrared and Laser Engineering, 2019, 48(S1): 72-77. doi: 10.3788/IRLA201948.S117001
Citation: Yang Zipeng, Liu Min, Zhou Youjun, Dong Peng, Yang Chuancheng. Study on processing scheme and precision measurement method of payload adapter with irregular shape[J]. Infrared and Laser Engineering, 2019, 48(S1): 72-77. doi: 10.3788/IRLA201948.S117001

Study on processing scheme and precision measurement method of payload adapter with irregular shape

doi: 10.3788/IRLA201948.S117001
  • Received Date: 2018-11-08
  • Rev Recd Date: 2018-12-18
  • Publish Date: 2019-04-25
  • The structure of the payload adapter was becoming more and more complex to meet the needs of the new spacecraft. In order to offset the large deviation of the center of mass of a reentry spacecraft and realize the self-leveling of separation design, a payload adapter with irregular shape was designed according to the structural characteristics of a reentry spacecraft. Based on the analysis of the characteristics of riveting technology and additive manufacturing technology, two different process schemes of riveting and additive manufacturing were compared and analyzed. According to the actual manufacturing precision measurement needs of the payload adapter with irregular shape, laser tracking measurement technology was selected as the precision measurement method. Through the application case analysis of axis measurement after the installation of a certain type of upper-stage engine nozzle, it can be seen that the measurement and data processing method based on laser tracker and least square method could be applied to the payload adapter with irregular shape. And the obtained accuracy data could be used as the basis for the separation of spring selection in the subsequent separation design.
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    [2] Liu Wei, Liu Feng, Ni Yangyong, et al. Application research of intelligent assembly technology for complicate products[J]. Astronautical Systems Engineering Technology, 2018, 1(2):33-36. (in Chinese)刘炜, 刘峰, 倪阳咏, 等. 航天复杂产品智能化装配技术应用研究[J]. 宇航总体技术, 2018, 1(2):33-36.
    [3] Huang Chunping, Huang Shuowen, Liu Fencheng. Metal material additive manufacturing technology[J]. MW Metal Forming, 2016(2):34-38. (in Chinese)黄春平, 黄硕文, 刘奋成. 金属材料增材制造技术[J]. 金属加工(热加工), 2016(2):34-38.
    [4] Tian Guoqiang, Lu Zhongliang, Li Dichen. Digital manufacturing method of complex-structure mould based on additive manufacturing technology[J]. Aeronautical Manufacturing Technology, 2014(9):38-41. (in Chinese)田国强, 鲁中良, 李涤尘. 基于增材制造技术的复杂结构模具数字化制造方法[J]. 航空制造技术, 2014(9):38-41.
    [5] Dong Peng, Liang Xiaokang, Zhao Yanhua, et al. Research status of laser additive manufacturing in integrity and lightweight[J]. Aerospace Manufacturing Technology, 2018(1):7-11. (in Chinese)董鹏, 梁晓康, 赵衍华, 等. 激光增材制造技术在航天构件整体化轻量化制造中的应用现状与展望[J]. 航天制造技术, 2018(1):7-11.
    [6] Yan Bingcong. Research on key technologies of measuring assembly precision of a certain type of product based on laser tracker[D]. Harbin:Harbin Institute of Technology, 2015. (in Chinese)颜丙聪. 基于激光跟踪仪的某型号产品总装精测技术研究[D]. 哈尔滨:哈尔滨工业大学, 2015.
    [7] Deng Hui. Analysis and improvement of measurement method of laser tracker[J]. Science and Technology Innovation, 2017(21):72-73. (in Chinese)邓辉. 激光跟踪仪测量方法分析与改进[J]. 科技与创新, 2017(21):72-73.
    [8] Zhan Yufeng, Han Yongwei, Ning Rui, et al. Application of installation accuracy of measurement in aircraft radar antenna panel with laser tracker[J]. Aeronautical Science Technology, 2012(2):47-49. (in Chinese)詹玉凤, 韩永伟, 宁锐, 等. 激光跟踪仪在飞机雷达天线面板安装精度测量中的应用[J]. 航空科学技术, 2012(2):47-49.
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Study on processing scheme and precision measurement method of payload adapter with irregular shape

doi: 10.3788/IRLA201948.S117001
  • 1. Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China;
  • 2. Capital Aerospace Machinery Corporation Limited,Beijing 100076,China

Abstract: The structure of the payload adapter was becoming more and more complex to meet the needs of the new spacecraft. In order to offset the large deviation of the center of mass of a reentry spacecraft and realize the self-leveling of separation design, a payload adapter with irregular shape was designed according to the structural characteristics of a reentry spacecraft. Based on the analysis of the characteristics of riveting technology and additive manufacturing technology, two different process schemes of riveting and additive manufacturing were compared and analyzed. According to the actual manufacturing precision measurement needs of the payload adapter with irregular shape, laser tracking measurement technology was selected as the precision measurement method. Through the application case analysis of axis measurement after the installation of a certain type of upper-stage engine nozzle, it can be seen that the measurement and data processing method based on laser tracker and least square method could be applied to the payload adapter with irregular shape. And the obtained accuracy data could be used as the basis for the separation of spring selection in the subsequent separation design.

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