发明名称 Satellite battery thermal/capacity design
摘要 A method is disclosed of operating a nickel-hydrogen battery when the battery is less than fully charged. Specifically, battery recharge is completed at a temperature T1, in the range of approximately -10 DEG C. to -30 DEG C. which is lower than a temperature T2 in the range of approximately -10 DEG C. to +5 DEG C., at which discharge begins. The temperature T1 is chosen to maximize the extent of the reaction represented by the equation: Ni(OH)2+OH-=NiOOH+H2O+e-. versus the reaction represented by the equation: H2O+2e-=OH-+1/2O2 Subsequently, it is desirable to heat the battery to the temperature T2 in readiness for discharge. A preferred recharge temperature is less than approximately -10 DEG C. The battery includes a positive electrode which may include electrochemically active Ni(OH)2 possibly mixed with Co(OH)2 and electrically conductive material having a resistivity less than approximately 0.1 ohm-cm, a negative electrode which is of a material which catalyzes the oxidation and reduction of H2, and an electrolyte which is a solution of KOH.
申请公布号 US5395706(A) 申请公布日期 1995.03.07
申请号 US19940182224 申请日期 1994.01.14
申请人 SPACE SYSTEMS/LORAL, INC. 发明人 HALL, JOHN G.
分类号 H01M10/34;H01M10/44;H01M10/50;(IPC1-7):H01M10/44 主分类号 H01M10/34
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