Jet CAT P80 Thermal Analyses and Performance Assessment Using Different Fuels Types

作     者：Grigore CICAN Adina TOMA Cristian PUSCASU Razvan CATANA 

作者机构：Politehnica University of Bucharest Faculty of Aerospace Engineering 1-7 Polizu Street 011061 Bucharest 1 Romania National Research and Development Institute for Gas Turbines - COMOTI 220D Iuliu Maniu Ave Bucharest 6 Romania 

出 版 物：《Journal of Thermal Science》 (热科学学报（英文版）)

年 卷 期：2018年第27卷第4期

页      面：389-393页

核心收录：

学科分类：082502[工学-航空宇航推进理论与工程] 08[工学] 0805[工学-材料科学与工程（可授工学、理学学位）] 082503[工学-航空宇航制造工程] 0825[工学-航空宇航科学与技术] 0702[理学-物理学] 

主　　题：燃料 喷气 打字 P80 热分析 评价 表演 操作条件 

摘      要：The micro gas turbine propulsion systems represent a good choice for the unmanned aerial vehicles(UAVs). The present work monitors the engine parameters, correlating them with other important engine instrumentation data. The aim of this research was to study the operation of the Jet CAT using various types of fuels under various operating conditions: normal acceleration and sudden acceleration. The measured parameters were monitored under different conditions:(A) Engine operation at two different ambient temperatures – outdoor at 0oC and inside at 19oC; and(B) Using 4 fuel types: kerosene, diesel fuel, kerosene with 5% gasoline and kerosene with 10% gasoline. The relevance of this work is given by the fact that a detailed analysis is performed for the idle regime. The paper will present the detailed test plan used and the most relevant charts with the obtained results for: start time, force, temperature before turbine, fuel flow, depending on micro turbo engine speed.