发明名称 Sleeve for battery element for space vehicles, satellites or probes
摘要 The sleeve (30) for the battery is made of thermally conductive graphite fibres laid in the same direction and supported in an electrically insulating adhesive such as an epoxy resin. The sleeve is placed over a tubular cylinder (22) which terminates in a base flange (48) with fixing holes (60) round its periphery. The flange provides a thermal bridge from the graphite fibres to the mounting.
申请公布号 FR2774513(A1) 申请公布日期 1999.08.06
申请号 FR19990001185 申请日期 1999.02.02
申请人 SPACE SYSTEMS / LORAL INC 发明人 HALL JOHN C;MEHLMAN MITCHELL J;WEIGHT TERRY;LEVINE ERIK L
分类号 B64G1/66;B64G1/42;H01M2/10;H01M10/34;H01M10/50 主分类号 B64G1/66
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