Large electric machines for aircraft electric propulsion

被引:123
|
作者
Zhang, Xiaolong [1 ]
Bowman, Cheryl L. [2 ]
O'Connell, Tim C. [3 ]
Haran, Kiruba S. [1 ]
机构
[1] Univ Illinois, Dept Elect & Comp Engn, 306 N Wright St, Urbana, IL 61801 USA
[2] NASA, John H Glenn Res Ctr, 21000 Brookpk Rd, Cleveland, OH 44135 USA
[3] PC Krause & Assoc Inc, 3000 Kent Ave,Suite C1-100, W Lafayette, IN 47906 USA
关键词
SWITCHED RELUCTANCE; POWER-DENSITY; DESIGN; MOTOR; TECHNOLOGIES; DRIVE; GENERATOR; SYSTEM; TRENDS;
D O I
10.1049/iet-epa.2017.0639
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
To achieve benefits similar to those seen in hybrid-/all-electric ground-based and marine vehicles, electric propulsion has been proposed for large commercial aircraft. Among the main drivers of this are improved fuel economy, reduced harmful emissions, and lower audible noise. In converting to electric propulsion, the added electrical components' masses must be minimised so that the benefits that the components enable - improved turbine efficiency, distributed propulsion and propulsion-airframe integration - are not cancelled out by their weight penalty. This puts stringent requirements on the large electric machines used in the system, both those that generate electric power from the turbine shaft and those that drive propellers or ducted fans, because they are among the heaviest of the added electric components. A key machine design metric in this application is the specific power (SP), or the power-to-mass ratio. This study gives a comprehensive overview of large electric machines for aircraft electric propulsion applications, with a focus on methods for mass reduction and SP improvement.
引用
收藏
页码:767 / 779
页数:13
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