摘要
介绍了一种航空镉镍蓄电池温度控制装置的改进设计方案和控制原理。通过该温度控制系统改进,保证了飞机长时间滞空时应急电源所需的合适温度范围,满足了飞机的使用。
The improving design and control principle of the temperature-controlling device for aircraft Ni-Cd battery were introduced. By adjusting the temperature-controlling device, the most desirable temperature range needed for the emergency power operation is ensured during the long fly time in the sky, and the device can meet the requirement of aircraft Ni-Cd battery.
出处
《电源技术》
CAS
CSCD
北大核心
2008年第11期772-775,共4页
Chinese Journal of Power Sources
关键词
航空
镉镍蓄电池
温度控制装置
aircraff
Ni-Cd battery
temperature-controlling device
