首页> 外国专利> GAS TURBINE SYSTEM-MONITORING METHOD AND GAS TURBINE ENGINE-MONITORING SYSTEM TO MONITOR COMBUSTION SYSTEM HAVING WELL-SELECTED BINDER

GAS TURBINE SYSTEM-MONITORING METHOD AND GAS TURBINE ENGINE-MONITORING SYSTEM TO MONITOR COMBUSTION SYSTEM HAVING WELL-SELECTED BINDER

机译:粘结剂选型的燃气轮机监测方法及燃气轮机监测系统

摘要

PURPOSE: A gas turbine system-monitoring method and gas turbine engine-monitoring system are provided to decide wear and maintenance plans and to reduce poisonous release by detecting and monitoring UV-photosensitive material release from a coating and obtaining exact information and specific position information. CONSTITUTION: A gas turbine system-monitoring method comprises steps of selecting a binder(14) to monitor temperature by releasing an indicator(12) within a temperature range decided to make a substrate(16) of a gas turbine system take high-temperature operation till the temperature under the critical turbine substrate degradation temperature; combining the indicator and the binder; and coating the substrate with the combined indicator and binder to form monitoring deposits.
机译:目的:提供一种燃气轮机系统监测方法和燃气轮机发动机监测系统,以决定磨损和维护计划,并通过检测和监测涂料中的紫外线光敏材料释放量并获得确切的信息和特定的位置信息来减少有毒物质的释放。构成:一种燃气轮机系统的监测方法,包括以下步骤:选择粘合剂(14),以在决定使燃气轮机系统的基板(16)进行高温操作的温度范围内释放指示剂(12)来监测温度直到温度低于涡轮机基片的临界降解温度;结合指标和粘合剂;并用指示剂和粘合剂的组合物涂覆基板,以形成监控沉积物。

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