发明名称 Making a reflector R for space applications, comprises cutting a crude block of carbon-carbon composite material, milling a top of the crude block for fixing a back side of the reflector, and milling an underside of the crude block
摘要 <p>The process of making a reflector, comprises cutting a crude block (10) of carbon-carbon composite material according to the dimensions of the reflector, milling a top of the crude block for fixing a back side (14) of the reflector, milling an underside of the crude block for fixing a side before the reflector and to obtain a matrix, and combining the milled matrix with a mechanically and thermally structuring compound. A cradle (22) of profile is prepared and combined with back side of the block to receive one face milled matrix. The process of making a reflector, comprises cutting a crude block (10) of carbon-carbon composite material according to the dimensions of the reflector, milling a top of the crude block for fixing a back side (14) of the reflector, milling an underside of the crude block for fixing a side before the reflector and to obtain a matrix, and combining the milled matrix with a mechanically and thermally structuring compound. A cradle (22) of profile is prepared and combined with back side of the block to receive one face milled matrix. The matrix is combined with the structuring compound by subjecting a penetration of silicon carbide to the matrix. A housing (18) is fixed for receiving inserts in the back side of the block. The front face of the block undergoes a shaping or a smooth grinding. An independent claim is included for a reflector.</p>
申请公布号 FR2943184(A1) 申请公布日期 2010.09.17
申请号 FR20090051587 申请日期 2009.03.13
申请人 ANALYSE ET CONCEPTION DE STRUCTURES 发明人 GOUTENEGRE FRANCOIS
分类号 H01Q15/14;C04B35/83;H01Q19/10 主分类号 H01Q15/14
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