发明名称 Sandwich panels with subsonic shear wave speed
摘要 Aircraft panels are formed of a honeycomb core material and the skin. The honeycomb core material and the skin are selected to provide subsonic wave speed across the panel, thereby reducing sound transmission.
申请公布号 US2007134466(A1) 申请公布日期 2007.06.14
申请号 US20060495901 申请日期 2006.07.28
申请人 发明人 RAJARAM SHANKAR;WANG TONGAN;NUTT STEVEN R.
分类号 B32B3/12;B32B3/00 主分类号 B32B3/12
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