首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >DEVELOPMENT OF THE ELECTRIC FUEL SYSTEM FOR THE MORE ELECTRIC ENGINE
【24h】

DEVELOPMENT OF THE ELECTRIC FUEL SYSTEM FOR THE MORE ELECTRIC ENGINE

机译:用于更多电力发动机的电燃油系统的开发

获取原文
获取外文期刊封面目录资料

摘要

This paper describes the experimental rig test result of the electric motor-driven fuel pump system for the MEE (More Electric Engine). The MEE is an aircraft engine system concept, which replaces conventional mechanical/hydraulic driven components with electric motor-driven components. Various MEE approaches have been studied since the early 2000s and one of its key concepts is an electric motor-driven fuel pump . The authors commenced a feasibility study of the electric motor-driven gear pump system for what was assumed to be a small-sized turbofan engine. The concept study and system design were conducted, whereupon technical issues for the electric fuel pump system, which both supplies and meters fuel via the motor speed control, were clarified. Since one of the key issues is fuel-metering accuracy, the electric fuel system, including a flow feedback closed-loop control, was designed to ensure accurate fuel-flow metering for aircraft engine applications. To verify the rig system, an experimental model of the electric fuel pump system is assumed for a small-sized turbofan engine. The hardware of the motor-driven fuel pump and flow measurement mechanism, including an FPV (Fuel-Pressurizing Valve) and orifice, were designed, manufactured and fabricated and a differential pressure sensor for flow feedback was selected. Other equipment was also prepared, including a motor controller, power source and measurement devices, and the entire rig set-up was constructed. A bench test using the rig test set-up was conducted to verify the fuel-metering accuracy, response and system stability. Data, including the static performance and frequency response, were obtained for the electric motor, motor-driven fuel pump and entire fuel system respectively. The rig test results indicate the feasibility of the system, which will provide an accurate engine fuel flow (Wf) measurement and frequency response required for actual engine operation, via an electric motor speed control and fuel-flow feedback system, as proposed in the MEE electric fuel system.
机译:本文介绍了用于MEE(More Electric Engine)的电动机驱动的燃油泵系统的试验台测试结果。 MEE是飞机发动机系统的概念,它用电动机驱动的组件代替了传统的机械/液压驱动的组件。自2000年代初以来,已经研究了各种MEE方法,其主要概念之一是电动机驱动的燃油泵。这组作者开始对假设为小型涡扇发动机的电动机驱动齿轮泵系统进行可行性研究。进行了概念研究和系统设计,从而阐明了电动燃油泵系统的技术问题,该系统通过电动机速度控制来供应和计量燃油。由于关键问题之一是燃油计量的准确性,因此设计了包括流量反馈闭环控制在内的电动燃油系统,以确保飞机发动机应用中的燃油流量计量准确。为了验证钻机系统,假设了小型涡轮风扇发动机的电动燃油泵系统的实验模型。设计,制造和制造了电动燃油泵和流量测量机构的硬件,包括FPV(燃油压力阀)和节流孔,并选择了用于流量反馈的差压传感器。还准备了其他设备,包括电机控制器,电源和测量设备,并完成了整个钻机设置。使用钻机测试装置进行了台架测试,以验证燃油计量的准确性,响应性和系统稳定性。分别获得了电动机,电动燃油泵和整个燃油系统的数据,包括静态性能和频率响应。钻机测试结果表明了该系统的可行性,该系统将通过MEE中提出的电动机速度控制和燃料流量反馈系统,为发动机实际运行提供准确的发动机燃料流量(Wf)测量和频率响应。电动燃油系统。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号