发明名称 COMBINED THERMAL PROTECTION AND SURFACE TEMPERATURE CONTROL SYSTEM
摘要 The invention relates to a combined thermal protection and surface temperature control apparatus. In one embodiment, a combined thermal protection and surface temperature control apparatus comprises a porous member having an entrance side, and a separate exit side. One or more coolant entrance channels extend through the entrance side, extend part-way through the porous member, and end within the porous member before reaching the exit side. Conversely, one or more coolant exit channels begin within the porous member, extend through a portion of the porous member, and extend through the exit side. The coolant entrance and exit channels may be parallel and may alternate. The channels may only extend across a portion of the thickness of the porous member.
申请公布号 EP2077962(B1) 申请公布日期 2013.09.04
申请号 EP20070863825 申请日期 2007.11.02
申请人 THE BOEING COMPANY 发明人 BEHRENS, WILLIAM W;TUCKER, ANDREW R
分类号 B64C1/38;B60R99/00 主分类号 B64C1/38
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