发明名称 ACOUSTICALLY DAMPED COMPOSITE CONSTRUCTION FOR THE FORWARD PORTION OF A ROCKET OR MISSILE
摘要 Apparatus is provided for an acoustical composite construction especially designed for use in a launch vehicle fairing. The acoustical composite construction includes a low density core material (14) having a first side and a second side. A first sheet (10) of rigid face material is bonded to the first side with a visco elastic adhesive (16), and a second sheet (12) of rigid face material is bonded to the second side with a visco elastic adhesive (18). The construction is then oven cured or air cured under vacuum bag pressure only.
申请公布号 WO2005068295(A2) 申请公布日期 2005.07.28
申请号 WO2004US31010 申请日期 2004.09.15
申请人 THE BOEING COMPANY 发明人 CLEVELAND, MARK, A.
分类号 B64G1/00;D04H13/00;G10K11/162;G10K11/168 主分类号 B64G1/00
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