发明名称 ISOLATION STRUCTURE FOR AIRCRAFT HEAT AND SOUND ISOLATION
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to isolation structure for aircraft heat and sound isolation, its application in aircraft and aircraft with such structure. Said isolation structure has heavy layer and extra absorbing layer. Said heavy layer is perforated in some zones. Fraction of holes surface is kept to make said heavy layer in fact a sound-conducting at frequencies below that of dual wall of isolation structure. Said dual wall is formed by aircraft outer skin and said heavy layer. ^ EFFECT: efficient isolation. ^ 14 cl, 12 dwg
申请公布号 RU2435704(C1) 申请公布日期 2011.12.10
申请号 RU20100107865 申请日期 2009.07.20
申请人 EHJRBAS OPEREJSHNZ GMBKH 发明人 MJULLER RAJNER;GRENTSING BEN'JAMIN;TOMAS KRISTIAN
分类号 B60R13/08;B64C1/40;F16L59/02;G10K11/168 主分类号 B60R13/08
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