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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|