发明名称 Thermal protection device for use in thermal protection system of atmospheric re-entry vehicle, has skirt extending to outer side from stiffening wall whose edges are aligned with edges to delimit drain space between internal face and skirt
摘要 <p>The device (10) has a panel (11) receiving heat flow on an external face (11e), where the panel is provided with a stiffening wall (12) extended perpendicularly from an internal face of the panel. A skirt (14) extends towards outer side from the stiffening wall whose edges (14a, 14c, 14d) are aligned with edges (11a-11d) of the panel to delimit a drain space between the internal face of the panel and the skirt. The stiffening wall is extended by fixation tabs (13a, 13b, 13d), where each tab comprises an orifice (133a, 133b) for housing an element of a fixation unit. 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 FR2945792(A1) 申请公布日期 2010.11.26
申请号 FR20090053311 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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