航天推进技术研究院主办
双曲梁传感器推力测量技术应用
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
35
期数:
2009年06期
页码:
57-60
栏目:
测控与试验
出版日期:
2009-12-30
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 为提高小推力发动机的测量精度，对原测量误差大、测量结果易受环境情况影响的应变梁推力测量装置进行了改进。改进后采用双曲梁推力测量系统。从安装、校准等方面介绍了系统的改进措施及实际应用情况。试验结果表明，双曲梁推力测量系统测量精度高，内阻输出低、抗电干扰性能好。
- Abstract:
- For improvement of thrust level measurment accuracy of liquid rocket engine, measurement system modification was conducted. The previously used strain-beam system was replaced by dual-curved-beam measuring system. System modification measures and application results were introduced in this paper. Test results show that the dual-curved-beam measuring system has higher accuracy and better enviornment adaptability.
参考文献/References:
[1]卞水思， 张文声． 脉冲火箭发动机动态推力测量系统[Ｊ]． 试验技术通讯． １９８１, １(１): １－２７．
[2]张迎新． 火箭发动机参数测量技术[Ｍ]． 长沙： 国防科技大学出版社， １９８７．
[3]刘伟亮， 吴建军． 机电一体化推力测量系统的研制及应用[Ｊ]． 火箭推进， ２００４， １２(６): ５０－５４， ４９．
[4]王洪业． 传感器工程[Ｍ]． 长沙: 国防科技大学出版社, １９９７．
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备注/Memo
收稿日期：200９-０５-１３；修回日期：200９-0８-1７。
作者简介： 刘丽宁（19６5—），女，工程师，研究领域为发动机试验测控技术。
更新日期/Last Update:
1900-01-01