航空发动机室内试车台推力测量及其溯源体系分析
Measurement of Thrust of Aero Engine’s Indoor Test Bench and its Traceability System
  
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中文摘要:
      航空发动机推力测量相关影响参数的准确获取是保障台架推力测试准确性的前提。本文通过梳理室内试车台架推力附加阻力气动修正方法中所用到的关键试验参数、航空发动机试验与推力测量相关的常见控制参数、测量工具以及溯源标准及要求,最终形成相对完整的溯源体系,为实际试车工况下发动机推力测量校准技术的研究提供了借鉴。
英文摘要:
Research on calibration technique of thrust force and related influence parameters,in order to solve the field calibration problem of the important test parameters related to the measurement and conversion of engine thrust. These parameters include thrust, fuel flow, temperature, humidity, pressure, speed, air flow, nozzle area, etc. The accurate measurement of these parameters is the premise to obtain the engine thrust and the converted thrust. In this paper, the test parameters, control parameters related to aero engine test and thrust measurement, measurement tools, and traceability standards and requirements used in the study of aerodynamic correction method for additional thrust resistance of indoor test bench are reviewed. A relatively complete traceability system is formed to guide the reliability requirements of the test data in the research work, so as to ensure that these basic work do not have problems as far as possible.
作者单位
黄成1,金炜1,瞿剑苏2,薛斌斌1,曹旸1 (1.中国航发上海商用航空发动机制造有限责任公司,上海 201306
2.航空工业北京长城计量测试技术研究所,北京 100095) 
中文关键词:  发动机推力  气动参数  附加阻力  溯源体系
英文关键词:engine thrust  aerodynamic parameters  additional drag  traceability system
基金项目:
DOI:doi:10.11823∕j.issn.1674-5795.2020.03.04
引用本文:黄成1,金炜1,瞿剑苏2,薛斌斌1,曹旸1.航空发动机室内试车台推力测量及其溯源体系分析[J].计测技术,2020,(3):.
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