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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:使用反向性能模型,高海拔操作中涡轮机发动机的GUI型在线状态监测程序的开发

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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 LabVIEW. 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:两者的可靠性和降低飞机推进系统的可靠性和降低的改善是发动机用户的重要问题。因此,如果提供了精确的发动机状态和健康监测,则可以部分解决上述问题。最近,已经开发了用于防止出现预防性的故障或性能降低的预防性和维护措施,这是可能发生在高海拔,异物损伤颗粒,热和大雨和雪大气条件下可能发生的预防性和维护措施的预防措施或性能降低。然而,要建立这种健康监测系统,首先需要在线状态监测计划。该程序必须通过测量发动机性能数据和基本发动机性能模型计算的基本性能结果之间的比较来监测发动机性能趋势。这项工作旨在使用LabVIEW开发PT6A - 67涡轮螺旋桨发动机的GUI型在线状态监控程序。使用发动机制造商提供的有限性能甲板数据逆生成的组件映射模拟了内部发动机性能。评估基本发动机性能仿真程序,因为该程序的分析结果与性能甲板数据很好。所提出的在线条件程序可以监控真实的发动机性能以及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计算的性能结果之间的精确比较。在该监控系统的开发阶段,提出了一种信号生成模块来评估所提出的在线监测系统。为用户友好目的,所有监控程序都由LabVIEW编码,并使用所提出的GUI类型的通信监控程序演示监视示例。

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