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本文介绍了某小型航空涡喷发动机的基本情况,描述了使用的发动机试车台的基本情况,详细介绍了其各个组成部分。在某型航空涡喷发动机研制过程中,开展了对该发动机进行寿命试车的工作,为了准确地获取发动机的运行状态使用了包含振动、滑油温度、气路静电等监测手段的在线综合监测系统来采集发动机的状态数据。
This article describes the basic situation of a small aero turbojet engine, describes the basic situation of the engine test bed used, and details its various components. In a certain type of aviation turbojet engine development process, carried out on the engine life test work, in order to accurately obtain the engine running status using vibration, oil temperature, static electricity and other monitoring means monitoring system To collect the engine status data.