发明名称 CALODUC EN MATERIAU COMPOSITE NOTAMMENT POUR PANNEAU DE SATELLITE ET SON PROCEDE DE FABRICATION
摘要 The heat transmitter includes a thermal joint (3) which forms an interface between an aluminium tube (1) and a girder (7, 9). The joint is made in advance and put around the tube without overlapping. The ends of mandrels (6) are covered with a layer (7) of composite material and pushed against the metal tube. Two plates are then placed on either side of the H-structure and an opposing pressure is applied to ensure polymerisation. The thermal joint is made by spreading out the substance on a sheet to obtain the required dimensions and to polymerise it. The mandrels used are shaped to correspond to the cross-section of the central tube.
申请公布号 FR2735565(B1) 申请公布日期 1997.08.22
申请号 FR19950006962 申请日期 1995.06.13
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 MAUDUIT DANIEL ANDRE
分类号 F28D15/02;F28F13/00;(IPC1-7):F28D15/02 主分类号 F28D15/02
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