Battery Cell-to-Pack Scaling Trends for Electric Aircraft Jeffrey

被引:2
|
作者
Chin, Jeff C. [1 ]
Look, Karsten [2 ]
McNichols, Ezra O. [2 ]
Hall, Dustin L. [1 ]
Gray, Justin S. [1 ]
Schnulo, Sydney L. [1 ]
机构
[1] NASA, Glenn Res Ctr, Prop Syst Anal Branch, Cleveland, OH 44135 USA
[2] NASA, Glenn Res Ctr, Turbomachinery & Turboelect Syst Branch, Cleveland, OH 44135 USA
关键词
D O I
10.2514/6.2021-3316
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Battery pack gravimetric energy density is one of the most important, yet often miss-estimated, design parameters for sizing all-electric aircraft. Proper accounting for thermal, structural, and operational safety margins are frequently lost when extrapolating performance from the cell level to the aircraft level. This paper summarizes the relevant engineering and certification details needed to better account for the penalties associated with assembling battery packs. The overhead penalty when scaling from cell to pack energy density is not constant, as is often assumed. Furthermore, the scaling relationship varies depending on pack requirements, cell chemistry, and architecture. Parametric, high-fidelity models are used to determine optimal battery pack sizes over a range of conditions to better quantify technology scaling effects. Simply stated, doubling cell energy density doesn't translate to doubled pack energy density.
引用
收藏
页数:15
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