发明名称 SET TO INSULATE AIRCRAFT AIRFRAME INNER SURFACE
摘要 FIELD: transport. ^ SUBSTANCE: insulation set (19-22) for airframe is fastened on lengthwise side (41, 41a, 41b) of ribs (32, 32a, 32b, 32c) and arranged to be completely closed by foil (11) and to stay inside airframe covered by inner and outer coatings. Proposed design uses fireproof insulation and fireproof barrier layer fitted either separately or in combination thereof inside airframe insulation set (19-22) attached with the help of flat insulation end section (12, 12a, 12b) in rib attachment area (15) located below lengthwise sides (41, 41a, 41b) of rib (32, 32a, 32b, 32c) and nearby stringer (31). Aforesaid insulation is fastened by fireproof attachment elements (4, 13). In rib attachment area (15), there is through hole (24). Leading-through sleeve and insulation end section (12, 12a, 12b) are arranged in airframe sets (19-22). Aforesaid end section has hole-like recess. ^ EFFECT: higher anti-fire safety. ^ 21 cl, 10 dwg
申请公布号 RU2373109(C2) 申请公布日期 2009.11.20
申请号 RU20060127019 申请日期 2005.01.05
申请人 EHJRBAS DOJCHLAND GMBKH 发明人 MJULLER RAJNER;TURANSKI PETER;EHSTERAJKH VIL'KO;RAJNEL'T TORSTEN
分类号 B64C1/12;B64C1/40 主分类号 B64C1/12
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