Battery thermal control arrangement
US5310141A · kind A · utility
43Cited by
5References
12Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 21, 1992 |
| Grant date | May 10, 1994 |
| Priority date | — |
| Expiry date | Sep 21, 2012 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02E60/10
- WIPO fieldElectrical machinery, apparatus, energy
- WIPO sectorElectrical engineering
Abstract
Cylindrical battery cell vessels are coupled together in plural sets by pairs of half-shell sleeves. The sleeves conduct heat preferentially in an axial direction. Each sleeve set is mounted onto a heat rejection plate for direct radiation to space. Each satellite of a set of spacecraft has a North and/or South-facing region for mounting the heat rejection plates of the requisite number of cells. Each plate may be fitted with an optical solar reflector (OSR) for reflecting insolation, and for radiating heat energy.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.