Low-temperature, low-pressure Zn-ion hybrid supercapacitor in extreme near-space application

被引:0
|
作者
Liu, Weijia [1 ]
Liu, Haiqing [1 ]
Sun, Yin [3 ]
Gao, Zhiyi [2 ]
Li, La [1 ]
Shen, Guozhen [1 ]
机构
[1] Beijing Inst Technol, Sch Integrated Circuits & Elect, Beijing 100081, Peoples R China
[2] Chinese Acad Sci, CAS Key Lab Magnet Mat & Devices, Ningbo Inst Mat Technol & Engn, Ningbo 315201, Peoples R China
[3] Beijing Inst Technol, MIT Key Lab Complex Field Intelligent Sensing, Beijing 100081, Peoples R China
基金
中国国家自然科学基金; 北京市自然科学基金;
关键词
D O I
10.1039/d5mh00233h
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
The development and utilization of airspace, especially near-space particularly rely on power units with superior tolerance in low-temperature and low-pressure environments to output a stable energy supply. Here we propose a strategy towards low-temperature, low-pressure Zn-ion hybrid supercapacitor based on a weakly hydrogen-bonded electrolyte and a hyacinth-shaped Ti2CTx MXene@CC cathode with hierarchical bridge-linked structure, which synergistically reduces the internal resistance of the device and enables the assembled supercapacitor showing a good low-temperature resistance while combining low-gas-voltage safety. The ACN additive weakens the hydrogen bond between water molecules and reshapes the solvation structure of Zn2+, thus reducing the ion transfer resistance and achieving a reversible Zn/Zn2+ chemical reaction. The bridge-linked hierarchical structure of the hyacinth-shaped Ti2CTx MXene@CC cathode provides a rich conductive network and optimizes the ion diffusion path, which reduces the ion diffusion resistance. At -40 degrees C, the assembled device can still achieve an area specific capacitance of 64.0 mF cm-2 at a scan rate of 500 mV s-1, and long-term stability after 20 000 cycles at a current density of 20 mA cm-2. An integrated temperature and pressure sensing system driven by the supercapacitor successfully realizes the monitoring of atmospheric indicators in extreme environments, providing new ideas for auxiliary power units in airspace and near-space.
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页数:12
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