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Development of a Jet Engine Experiment for the Energy Systems Laboratory

机译:为能源系统实验室开发喷气发动机实验

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Recently, a jet engine experiment was added to the Energy Systems Laboratory at Kettering University (formerly GMI). The educational objectives of this experiment are: to familiarize the students with the operation of a turbojet engine, the theory behind the thermodynamic processes involved, and the linear momentum equation; to determine theoretical and measured engine thrust and the efficiencies of the compressor, the combustion chamber, and the turbine; to determine the effect of engine speed on thrust-specific fuel consumption (TSFC) and engine emissions; to analyze the combustion process; and to perform a complete energy balance on the jet engine. The apparatus used is a small TTL model SR-30 turbojet engine capable of kerosene and diesel liquid fuel start and operation. Using an automatic data acquisition system, the students operate the engine at 50,000-75,000 rpm and measure various pressures and temperatures as well as fuel flow rate, air flow rate, engine emissions and engine thrust. The data is then used to calculate the TSFC, component efficiencies and the A/F ratio. By using the linear momentum principle, engine thrust is calculated and compared with the measured value. This paper presents the measured test data and analytical results obtained by using the Engineering Equation Solver (EES). Experimental results compare favorably with theoretical predictions.
机译:最近,喷气发动机实验被添加到凯特林大学(原GMI)的能源系统实验室中。该实验的教学目的是:使学生熟悉涡轮喷气发动机的操作,所涉及的热力学过程的理论以及线性动量方程;确定理论和测量的发动机推力以及压缩机,燃烧室和涡轮的效率;确定发动机转速对推力比油耗(TSFC)和发动机排放的影响;分析燃烧过程;并在喷气发动机上实现完全的能量平衡。使用的设备是小型TTL型SR-30涡轮喷气发动机,能够启动和运行煤油和柴油液体燃料。学生使用自动数据采集系统,以50,000-75,000 rpm的转速运转发动机,并测量各种压力和温度以及燃油流量,空气流量,发动机排放物和发动机推力。然后将数据用于计算TSFC,组件效率和A / F比。通过使用线性动量原理,可以计算出发动机推力并将其与测量值进行比较。本文介绍了使用工程方程求解器(EES)获得的测得的测试数据和分析结果。实验结果与理论预测相吻合。

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