发明名称 FOAM COMPOSITE INSULATION FOR AIRCRAFT
摘要 Insulation for use in an aircraft fuselage is formed wherein at least one layer (40) made from an open-celled foam (39) that provides acoustic and thermal insulation. The open-celled foam (39) is compression fitted into the airplane fuselage so as to provide effective attachment to the fuselage. The open-celled foam (39) requires minimal attachment treatments. Further, compression fit of the open cell layer (40) is used as an interface around brackets and unrelated hardware to provide superior close-out of gaps that would normally occur using traditional insulation to bracket interfaces. The preferred foam for the open celled compression layer is also relatively moisture resistant (i.e. hydrophobic) in nature and is compressible to betwe en about 0.5 and 10 percent compression, with about 2% compression being ideal for most applications.
申请公布号 CA2561399(A1) 申请公布日期 2005.10.13
申请号 CA20052561399 申请日期 2005.03.28
申请人 THE BOEING COMPANY 发明人 SMITH, RANDALL S.;STRUVE, RICHARD G.;FARANGE, HOSSEIN;MOORES, NIGEL G.;WESTON, ADAM R.
分类号 B64C1/40 主分类号 B64C1/40
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