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Development of GUI Type On-line Condition Monitoring Program for A Turboprop Engine in High Altitude Operation Using Inverse Performance Model

机译:基于逆性能模型的高空涡桨发动机GUI型在线状态监测程序开发

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Both improvement of reliability and reduction of operational cost of the aircraft propulsion system are important issues to engine users. Therefore if a precise engine condition and health monitoring is provided, the problems above are can be partly solved. Recently, the health monitoring system has been developedfor precaution and maintenance action against faults or performance degradations of the advanced propulsion system which may be occurred in severe environments such as high altitude, foreign object damage particles, hot and heavy rain and snowy atmospheric conditions. However to establish this health monitoring system, the on-line condition monitoring program is firstly required. This program has to monitor the engine performance trend through comparison between measuring engine performance data and base performance results calculated by base engine performance model. This work aims to develop a GUI type on-line condition monitoring program for PT6A — 67 turboprop engine using Lab VIEW. The base engine performance of the on-condition monitoring program is simulated using component maps inversely generated from the limited performance deck data provided by engine manufacturer. The base engine performance simulation program is evaluated because analysis results by this program are well agreed with the performance deck data. The proposed on-line condition program can monitor the real engine performance as well as the trend through precise comparison between performance results calculated by the base performance simulation program and measuring engine performance signals. In the development phase of this monitoring system, a signal generation module is proposed to evaluate the proposed on-line monitoring system. For user friendly purpose, all monitoring program are coded by LabVIEW, and monitoring examples are demonstrated using the proposed GUI type on-condition monitoring program.
机译:飞机推进系统的可靠性的提高和操作成本的降低都是发动机用户的重要问题。因此,如果提供精确的发动机状况和健康监测,则可以部分解决上述问题。近来,已经开发了健康监视系统,以针对高级推进系统的故障或性能降级的预防和维护措施,该故障或性能降级可能在诸如高海拔,异物损坏颗粒,炎热和大雨以及下雪的大气条件的严酷环境中发生。但是,要建立此健康监控系统,首先需要在线状态监控程序。该程序必须通过比较测量发动机性能数据和由基本发动机性能模型计算出的基本性能结果来监视发动机性能趋势。这项工作旨在使用Lab VIEW为PT6A — 67涡轮螺旋桨发动机开发GUI类型的在线状态监测程序。使用从发动机制造商提供的有限性能驾驶台数据中逆向生成的零部件图,可以模拟在役监控程序的基本发动机性能。评估基本引擎性能模拟程序是因为该程序的分析结果与性能平台数据完全吻合。所提出的在线状态程序可以通过基本性能模拟程序计算的性能结果与测量发动机性能信号之间的精确比较来监视实际发动机性能以及趋势。在此监视系统的开发阶段,提出了一个信号生成模块来评估所提议的在线监视系统。为了方便用户使用,所有监视程序均由LabVIEW编写,并使用建议的GUI类型实时监视程序演示了监视示例。

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