High-precision measuring system for aeroengine thrust

YANG Quan-ting; YANG Ji-ming; HAN Xiao-quan

doi:10.13873/j.1000-97872008.12.004

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High-precision measuring system for aeroengine thrust

更新时间：2025-09-11

- High-precision measuring system for aeroengine thrust
- Vol. 27, Issue 12, Pages: 82-83+87(2008)
- 作者机构：
  
  空军工程大学工程学院
- 作者简介：
- 基金信息：
- DOI：10.13873/j.1000-97872008.12.004
  CLC： V263
- Published：2008
- 稿件说明：
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[1]杨全廷,杨纪明,韩小全.一种高精度的发动机推力测量系统[J].传感器与微系统,2008,27(12):82-83+87.

YANG Quan-ting, YANG Ji-ming, HAN Xiao-quan. High-precision measuring system for aeroengine thrust[J]. 2008, 27(12): 82-83+87.
[1]杨全廷,杨纪明,韩小全.一种高精度的发动机推力测量系统[J].传感器与微系统,2008,27(12):82-83+87. DOI： 10.13873/j.1000-97872008.12.004.

YANG Quan-ting, YANG Ji-ming, HAN Xiao-quan. High-precision measuring system for aeroengine thrust[J]. 2008, 27(12): 82-83+87. DOI： 10.13873/j.1000-97872008.12.004.

摘要

为了提高发动机推力测量的精度

从测量原理出发

着重讨论了制约精度提高的几个关键问题

采用AT89C52单片机设计了一种高精度的飞机发动机推力测量系统

给出了具体的硬件电路。实验结果表明:该系统可以大大提高发动机推力的测量精度

对于提高目前的测量手段具有重要意义。

Abstract

In order to improve the measuring precision of aeroengine thrust

based on the measuring principle

some pivotal factors that restricted the measuring precision are discussed

and a high-precision measuring system with AT89C52 single-chip processor is designed.Factual circuit is given.Experiment results show that the system can greatly improve measuring precision

so it is important to upgrade the current measuring method.

关键词

Keywords

references

动态推力校准系统设计 [J]. 赵自文. 自动化仪表 . 2007(S1)

对火箭发动机推力矢量测试系统的标定 [J]. 王志勇,孙宝元,张军,钱敏,翟怡,任宗金. 传感器与微系统 . 2007(01)

解耦算法在发动机推力矢量测量中的应用 [J]. 王红艳,孙宝元,钱敏,张军. 宇航计测技术 . 2005(06)

CS-01高空台推力测量和校准装置研制 [J]. 朱青,徐建阳. 燃气涡轮试验与研究 . 2002(03)

非电量电测技术[M]. 西安交通大学出版社 , 吴道悌编, 1990

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Related Institution

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