首页> 外文期刊>Energy Conversion & Management >On-design and off-design operation performance assessmentsof an aero turboprop engine used on unmanned aerial vehicles (UAVs) in terms of aviation, thermodynamic, environmental and sustainability perspectives
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On-design and off-design operation performance assessmentsof an aero turboprop engine used on unmanned aerial vehicles (UAVs) in terms of aviation, thermodynamic, environmental and sustainability perspectives

机译:在航空,热力学,环境和可持续性观点方面,无人驾驶航空公司(无人机)上使用的航空涡轮机(无人机)的航空涡轮机发动机的设计和非设计操作性能评估

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摘要

In this study, a turboprop engine (TPE) of an unmanned aerial vehicle (UAV) is investigated for "on-design" and "off-design" conditions at maximum operation mode. One project point is chosen for on-design case for the cycle analysis. Other constraints and requirements are considered at off-design analysis in which cycle analysis is not affected. The off-design condition is generally used in emergency situation such as one-engine take-off, extreme flight speed, extreme altitude, and hot day operation. The aviation, energy, exergy, environmental, and sustainability analyses are performed to the TPE. For on-design and off-design conditions of the UAV TPE, the specific fuel consumptions are 0.287 kg/kW h and 0.282 kg/kW h, specific powers are 0.067 kW h/kg and 0.069 kW h/kg, thermal limiting ratios are 3.735 and 3.785, entalphy ratios are 4.482 and 4.555, energy efficiencies are 29.067% and 29.652%, exergy efficiencies are 27.38% and 27.93%, exergetic improvement potentials are 159.26 kW and 182.23 kW, ecological objective functions are -436.366 kW and -488.78 kW, environmental effect factors are 2.652 and 2.580, ecological effect factors are 3.652 and 3.580, exergetic sustainability indexes are 0.38 and 0.39, sustainable efficiency factors are 1.38 and 1.39, respectively. The results show that off-design condition has better fuel consumption, power, efficiency, improvement potential, environmental damage and sustainability than on-design condition. Also, the combustion chamber is the first component to be handled for the improvement of the overall system. UAVs are used for very deligant and important duties and their efficiency and sustainability play important role for their missions. UAV engines such as TPEs are the major power units to operate the overall system. Even a slight increase in efficiency and sustainability for the TPE engine can cause important feedback for the UAV mission. It is also important to assess the TPE for its environmental effects, because UAVs will play important role in the future for the transportation. As a result, this study is useful to assess turboprop engines of unmanned aerial vehicles in efficiency, sustainability and environmental aspects.
机译:在该研究中,在最大操作模式下研究了无人驾驶飞行器(UAV)的涡轮机发动机(TPE),并以“开启设计”和“非设计”条件。选择一个项目点,用于循环分析的设计案例。在非偏移分析中考虑了其他限制和要求,其中循环分析不受影响。非设计条件通常用于紧急情况,如一发动机起飞,极端飞行速度,极端高度和炎热的日常运行。对TPE进行航空,能量,漏洞,环境和可持续性分析。对于UAV TPE的设计和非设计条件,特定的燃料消耗量为0.287kg / kW h和0.282 kg / kw h,特定功率为0.067 kW h / kg和0.069 kW h / kg,热限压比3.735和3.785,积极比率为4.482和4.555,能量效率为29.067%,29.652%,高出效率为27.38%,锻炼改善潜力为159.26千瓦,生态目标职能为-436.366 kW和-488.78 kW ,环境效果因素为2.652和2.580,生态效应因素为3.652和3.580,蜕膜可持续性指标分别为0.38且0.39,可持续效率因素分别为1.38和1.39。结果表明,非设计条件具有更好的燃料消耗,功率,效率,改善潜力,环境损害和可持续性而不是设计条件。而且,燃烧室是用于改善整个系统的第一组件。无人机用于非常截然的义务和重要职责,其效率和可持续性对其任务发挥着重要作用。诸如TPE的UAV发动机是操作整个系统的主要电源单元。即使为TPE发动机的效率和可持续性略有提高,也可能导致无人机任务的重要反馈。评估TPE的环境影响也很重要,因为无人机将在未来发挥重要作用进行运输。因此,本研究可用于评估无人机车辆的涡轮螺旋桨发动机,效率,可持续性和环境方面。

著录项

  • 来源
    《Energy Conversion & Management》 |2021年第9期|114403.1-114403.13|共13页
  • 作者

    Balli Ozgur; Caliskan Hakan;

  • 作者单位

    Minist Natl Def Ist Air Maintenance Factory Directorate 1 HBFM Gen Directorate Mil Factories AFGM Eskisehir Turkey|Eskisehir Osmangazi Univ Grad Sch Nat & Appl Sci Aviat Sci & Technol Bati Meselik Campus Eskisehir Turkey;

    Usak Univ Fac Engn Dept Mech Engn TR-64200 Usak Turkey;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Energy; Environmental impact; Exergy; On-design and off-design; Turboprop; Unmanned aerial vehicle;

    机译:能量;环境影响;ofergy;设计和非设计;涡轮螺旋桨;无人驾驶飞行器;
  • 入库时间 2022-08-19 02:46:04

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