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The Development of Test System for Aeroengine Test-run

机译:航空发动机试车测试系统的开发

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In this paper, the test system for certain aeroengine test-run is discussed. The system is developed with PXI-bus data acquisition cards and LabView Development System based on virtual instrument technique. The means such as isolation, shield, float, impedance matching and analog filter are utilized to strengthen the anti-interference ability. Considering the four basic types of signals in test-run: stable-random signals, low-frequency wavering signals, convergent-vibrant signals and chop-top signals, relevant digital filters are designed to filter noises. These digital filters can be used solely or nested to get the optimum parameter values. The test-run database system running under client/server environment is constructed to store the data and check results in all test-run states, which makes it’s impossible to share the data in Intranet. The database model is designed with entity relationship diagram. And multi-table design is introduced to improve the query efficiency.
机译:在本文中,讨论了用于某些航空发动机测试运行的测试系统。该系统是使用PXI总线数据采集卡和基于虚拟仪器技术的LabView开发系统开发的。利用隔离,屏蔽,浮动,阻抗匹配和模拟滤波器等手段来增强抗干扰能力。考虑到测试运行中的四种基本信号类型:稳定随机信号,低频波动信号,会聚振动信号和斩波信号,设计了相关的数字滤波器来过滤噪声。这些数字滤波器可以单独使用或嵌套使用以获得最佳参数值。在客户端/服务器环境下运行的测试运行数据库系统旨在存储数据并检查所有测试运行状态下的结果,从而无法在Intranet中共享数据。数据库模型是用实体关系图设计的。并引入了多表设计以提高查询效率。

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