|Table of Contents|

Cause analysis and computative method of displacement measurement abnormality in static test(PDF)

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

Issue:
2010年05期
Page:
59-62
Research Field:
测控与试验
Publishing date:

Info

Title:
Cause analysis and computative method of displacement measurement abnormality in static test
Author(s):
SUN Bai-hong ZHOU Yun-duan
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V434-33
DOI:
-
Abstract:
The reason of abnormality appeared during the displacement measurement in the frame static test is analyzed. Some improvement approachs are put forward,including more smoother contact surface, bigger measuring block and so on. Based on the analysis of the stiffness of the whole frame, the derivation method for calculation the displacement of an abnormal measuring point by using the normal measuring points is proposed. The method is validated by additional two tests which do not contain abnormal displacement measuring points. The results show that the error of the computative method is less than 5%.

References:

[1]魏生道. 结构静力试验技术[M]. 北京: 宇航出版社, 1988. [2]罗彦, 林敏杜. 轴向位移影响因素的分析[J]. 电力系统及其自动化学报, 2002, 14(6): 44-48. [3]李锋, 邓长华, 鲍福廷. 液体火箭发动机冲击响应谱分析计算方法[J]. 西安工业大学学报, 2009, 29(1): 28-31. [4]段毅, 刘宇, 覃粒子, 等. 高室压脉冲液体火箭发动机特性试验[J]. 火箭推进, 2009, 35(2): 12-17. [5]王栋, 余陵, 武晓松. 火箭发动机六分力试验系统力学和误差特性[J]. 弹道学报, 2009, 21(3): 23-25. [6]李文成, 李岩, 姜伟伟, 等. 基于两轴角传感器的机动测控装备自动调平系统[J]. 现代电子技术, 2010 (14): 159-161. [7]李海涛. 火箭发动机推力矢量测量理论、方法与自动测试技术研究[D]. 长沙: 国防科学技术大学, 2005. [8]朱子环, 耿卫国, 陈锋. 液体火箭发动机试验推力校准控制系统的设计[J]. 计算机测量与控制, 2008, 16(11): 1575-1577. [9]夏露露, 许化龙, 田鹏飞. 基于PC/104的陀螺仪动态测试系统设计[J]. 现代电子技术, 2009 (22): 31-33. [10]罗艳强, 姚长虹, 张伟. 遥测技术在火箭发动机过载试验中的应用[J]. 现代电子技术, 2008 (23): 68-70. [11]吴庆鸣, 李国超, 杨文清, 等. 发动机质心测量中轴线位置测量的一种新方法[J]. 固体火箭技术, 2003, 26(1): 76-78. [12]费业泰. 误差理论与数据处理[M]. 北京: 机械工业出 版社, 2001. [13]伍文平, 张智盛, 张明. 环境试验室温、湿度模糊控制系统设计[J]. 现代电子技术, 2009 (21): 157-159.

Memo

Memo:
-
Last Update: 1900-01-01