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A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology

机译:用于空气汽车技术分布式电推进概念综述

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The emergence of distributed electric propulsion (DEP) concepts for aircraft systems has enabled new capabilities in the overall efficiency, capabilities, and robustness of future air vehicles. Distributed electric propulsion systems feature the novel approach of utilizing electrically-driven propulsors which are only connected electrically to energy sources or power-generating devices. As a result, propulsors can be placed, sized, and operated with greater flexibility to leverage the synergistic benefits of aero-propulsive coupling and provide improved performance over more traditional designs. A number of conventional aircraft concepts that utilize distributed electric propulsion have been developed, along with various short and vertical takeoff and landing platforms. Careful integration of electrically-driven propulsors for boundary-layer ingestion can allow for improved propulsive efficiency and wake-filling benefits. The placement and configuration of propulsors can also be used to mitigate the trailing vortex system of a lifting surface or leverage increases in dynamic pressure across blown surfaces for increased lift performance. Additionally, the thrust stream of distributed electric propulsors can be utilized to enable new capabilities in vehicle control, including reducing requirements for traditional control surfaces and increasing tolerance of the vehicle control system to engine-out or propulsor-out scenarios. If one or more turboelectric generators and multiple electric fans are used, the increased effective bypass ratio of the whole propulsion system can also enable lower community noise during takeoff and landing segments of flight and higher propulsive efficiency at all conditions. Furthermore, the small propulsors of a DEP system can be installed to leverage an acoustic shielding effect by the airframe, which can further reduce noise signatures. The rapid growth in flight-weight electrical systems and power architectures has provided new enabling technologies for future DEP concepts, which provide flexible operational capabilities far beyond those of current systems. While a number of integration challenges exist, DEP is a disruptive concept that can lead to unprecedented improvements in future aircraft designs.
机译:飞机系统的分布式电动推进(DEP)概念的出现使未来航空器的整体效率,能力和鲁棒性能够实现新功能。分布式电推进系统具有利用电驱动推进器的新方法,其仅电连接到能量源或发电设备。结果,可以以更大的灵活性地放置,尺寸的推进器,以利用航空推进耦合的协同效益,并提供更高的传统设计性能。已经开发了许多使用分布式电动推进的传统飞机概念,以及各种短期和垂直起飞和着陆平台。用于边界层摄取的电驱动推进器的仔细集成可以允许提高推进效率和唤醒填充益处。推进器的放置和配置也可用于减轻提升表面的尾部涡流系统,或者杠杆在吹风表面上的动态压力增加,以增加提升性能。另外,分布式电推进器的推力流可用于实现车辆控制中的新能力,包括降低传统控制表面的要求以及将车辆控制系统的公差增加到发动机输出或推进场景。如果使用一个或多个涡轮电流发电机和多个电动风扇,则整个推进系统的有效旁路比率增加也可以在起飞和起飞段的较低的社区噪声以及在所有条件下更高的推进效率。此外,可以安装DEP系统的小推进器以利用机身利用声学屏蔽效果,这可以进一步降低噪声签名。飞行重量电气系统和电力架构的快速增长为未来的DEP概念提供了新的启用技术,这为远远超出了当前系统的灵活操作能力。虽然存在许多整合挑战,但DEP是一种破坏性的概念,可以导致未来飞机设计的前所未有的改进。

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