发明名称 Acoustic absorption system for an aircraft interior trim panel system
摘要 An acoustic absorption trim panel includes a composite core, a decoupler layer, and a mass barrier layer. By ensuring that the mass barrier layer remains limp in a limp area but in contact with the composite core through the decoupling layer, damping greater than that imparted in conventional construction is achieved.
申请公布号 US2006145004(A1) 申请公布日期 2006.07.06
申请号 US20040017281 申请日期 2004.12.20
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 DROST STUART K.;FORCIER JARED L.
分类号 B64D11/00 主分类号 B64D11/00
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