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Model-based Engine Health for Turboshaft Engines with Limited Instrumentation

机译:仪表有限的涡轮轴发动机基于模型的发动机运行状况

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Helicopter health and usage monitoring has lagged large commercial aircraft due to the limited instrumentation and high mission complexity of typical rotorcraft. To counteract these challenges, a model-based framework is introduced to utilize knowledge of engine and aircraft operation to determine (either on-board or off-board) the overall engine health and margin as well as module health based solely on aircraft Health and Usage Monitoring System (HUMS) data. The engine and module health can then be used to estimate remaining Time on Wing (TOW) as well as most likely condition-based maintenance for the engine.
机译:由于典型旋翼飞机的仪器有限和任务复杂性高,直升机的健康和使用情况监视已经落后于大型商用飞机。为了应对这些挑战,引入了基于模型的框架,以利用发动机和飞机运行的知识来(仅基于飞机的运行状况和使用情况)确定(机上或机外)总体发动机运行状况和裕度以及模块运行状况监控系统(HUMS)数据。然后,可以使用引擎和模块的运行状况来估计剩余的机翼停留时间(TOW)以及最可能的基于状况的引擎维护。

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