| 航空发动机机载压力测试设备自动校准系统设计 |
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| 引用本文： | 张冰凌,邢威.航空发动机机载压力测试设备自动校准系统设计[J].航空发动机,2010,36(5):44-46,55. |
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| 作者姓名： | 张冰凌 邢威 |
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| 作者单位： | [1]海军驻沈阳航空军事代表室,沈阳110045 [2]沈阳发动机设计研究所,沈阳110015 |
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| 摘 要： | 介绍了航空发动机机载压力测试设备的自动校准系统设计。该系统可实现机载压力测量设备的全自动现场校准,已成功应用于某型发动机机载压力测试设备的自动校准工作中。在0～7 MPa(表压、绝压)下进行测试、校准,准确度可达0.01%FS。
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| 关 键 词： | 航空发动机 机载 压力 测试 校准 |
Design of Automatic Calibration System for Aeroengine Airborne Pressure Measurement Instruments |
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| Authors: | ZHANG Bing-ling XING Wei |
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| Institution: | 1.Navy Shenyang Air Force Representative Office,Shenyang 110045,China;2.Shenyang Aeroengine Research Institue,Shenyang 110015,China) |
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| Abstract: | The automatic calibration system design of the aeroengine pressure measurement instruments was introduced.The automatic field calibration of airborne pressure measurement instruments was realized by the system which has been successfully adopted for the automatic calibration operation of an aeroengine airborne pressure measurement instruments.The testing and calibration accuracy reached to 0.01 % FS under 0~7 MPa（gauge pressure,absolute pressure）. |
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| Keywords: | aeroengine airborne pressure testing calibration |
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