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Design of A New Type Thrust Measuring System for Micro-turbojet Engine

机译:微型涡轮喷气发动发动机新型推力测量系统的设计

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摘要

In order to measure thrust of the micro-turbojet engine accurately, a new type of thrust measurement system was designed. The measuring system includes test bench, load cells, data acquisition modules and computer. The test bench utilizes a suspended test bed, which is different from the test bench supported by springs for aero-engine. It has simple structure and is easy to install and debug. The errors of the measuring system are analyzed from the influence factors of the thrust line and the error of the test instrument. At last, the axial loading static calibration method of the measuring system is introduced. Calibration results show that the thrust measuring system can achieve accuracy of ±0.33%, which is satisfied with the requirement of the test.
机译:为了准确测量微涡轮喷气发动机的推力,设计了一种新型推力测量系统。测量系统包括测试台,称重传感器,数据采集模块和计算机。试验台利用悬浮试验床,该试验床不同于用于空气发动机的弹簧支撑的测试台。它具有简单的结构,易于安装和调试。从推力线的影响因素和测试仪器的误差分析测量系统的误差。最后,介绍了测量系统的轴向加载静态校准方法。校准结果表明,推力测量系统可实现±0.33%的精度,这对测试的要求满意。

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