发明名称 Thermal protection device for protecting device of atmospheric re-entry vehicle, has supports distributed on internal face of panel at nearer to edges, where supports receive strip in sliding manner
摘要 <p>The device (10) has a panel receiving heat flow on an external face (11e). A strip (20) is mounted relative to an internal face (11f) of the panel. The strip extends along edges (11a-11d) of the panel, where the strip moves between a position in which the strip is withdrawal from the edges of the panel and another position in which the strip exceeds from the edges of the panel. Supports (40) are distributed on the internal face of the panel at nearer to the edges, where the supports receive the strip in a sliding manner. The device is made of composite material with ceramic matrix and composite material with reinforcement of carbon fibers and silicon carbide matrix.</p>
申请公布号 FR2945793(A1) 申请公布日期 2010.11.26
申请号 FR20090053312 申请日期 2009.05.19
申请人 SNECMA PROPULSION SOLIDE 发明人 GIRARD FLORENT
分类号 B64G1/58 主分类号 B64G1/58
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