Cylindrical lithium-ion structural batteries for drones

被引:20
|
作者
Hollinger, Adam S. [1 ]
McAnallen, Dylan R. [1 ]
Brockett, Matthew T. [1 ]
DeLaney, Scott C. [1 ]
Ma, Jun [2 ]
Rahn, Christopher D. [2 ]
机构
[1] Penn State Behrend, Dept Mech Engn, Erie, PA 16563 USA
[2] Penn State Univ, Dept Mech & Nucl Engn, University Pk, PA 16802 USA
关键词
battery; drone; lightweight; lithium-ion; multifunctional; multirotor aircraft; FINITE-ELEMENT SIMULATION; DEFORMATION; MECHANISMS; BEHAVIOR; FRACTURE; DESIGN; ENERGY; CELLS;
D O I
10.1002/er.4937
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The low cost, simplicity, and easy use of battery-powered multirotor aircraft has led to their adoption in commercial, industrial, agricultural, and military applications. These aircraft, however, have limited payloads and shorter endurance and range than fuel-powered conventional aircraft. To extend these key performance metrics, a structural battery is developed that uses commercially available battery cells as load bearing and power source elements for weight critical applications. The cylindrical structural battery is tested in three-point bending and is found to have four times higher stiffness and two times higher yield strength than the structure without battery reinforcement. Simulations of a quadcopter, redesigned with the proposed cylindrical structural batteries, demonstrate 41% longer hover time.
引用
收藏
页码:560 / 566
页数:7
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