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Case study: maintenance cost optimization through on-condition maintenance schedules and advanced component repairs

机译:案例研究:通过在条件维护时间表和高级组件维修的维护成本优化

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The main costs in gas turbine maintenance are the cost of major hot section overhaul and the cost of hot section replacement parts. This paper presents two methods that have been used to reduce these cost drivers. Conventionally, overhauls are scheduled based on generalized formulas for operating hours provided by the OEM for each engine model. On-Condition Maintenance scheduling uses a computer model to monitor the condition of the key hot section components, and enables the overhaul to occur at the optimum time for each engine in the fleet. This method has the advantage of extending the time between overhauls, while ensuring that the components are repairable at the time of overhaul. After one or two service intervals, hot section components are typically retired based on OEM service bulletin instructions. Laboratory analysis can be performed on parts removed from service to determine the factors limiting further service. Advanced repair processes are then applied to correct the life limiting factors and enable the parts to be reliably returned for further service, and extend the total life cycle of the parts through to retirement. The paper uses a case study based on a fleet of GE LM1600 engines to demonstrate how these practices have been applied to extend engine service intervals, and component life cycles, to reduce maintenance costs for the operator's fleet.
机译:燃气轮机维护的主要成本是主要的热部分大修的成本和热部分更换部件的成本。本文介绍了两种方法,已用于减少这些成本驱动因素。传统上,基于由OEM为每个发动机模型提供的运行时间的广义式公式来调度OVERHUS。在条件维护调度使用计算机模型来监视密钥热部分组件的条件,并启用在舰队中每个发动机的最佳时间发生的大修。该方法具有延伸横向之间的时间的优点,同时确保在大修时可修复部件。在一个或两个服务间隔之后,热部分组件通常基于OEM服务公告指令退出。实验室分析可以在从服务中取出的部件上进行,以确定限制进一步服务的因素。然后应用先进的修复过程以纠正寿命限制因素,并使零件可靠地返回以进行进一步的服务,并将部件的总生命周期扩展到退休。本文采用基于GE LM1600发动机队列的案例研究,以展示这些实践如何应用于扩展发动机服务间隔和组件寿命周期,以降低操作员车队的维护成本。

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