发明名称 De-icing device for aircraft outer skin
摘要 The de-icer consists of a duct (7) delivering hot air to a cavity (6) inside the skin (4) fitted with an inner closed envelope (10) with an inlet (9) for the pipe. The envelope has a supple wall with air permeable zones (12, 13) that form a thin channel with the skin's inner surface when the envelope is inflated through which hot air can circulate. The envelope is made from a fabric with fibres adapted to the air temperature and impregnated with an anti-friction coating. The inlet (9) is in the form of a neck that is fastened to the end of the hot air pipe by a fixing (11).
申请公布号 EP1318283(A1) 申请公布日期 2003.06.11
申请号 EP20020293014 申请日期 2002.12.06
申请人 HUREL-HISPANO 发明人 GONIDEC, PATRICK
分类号 B64D15/04;B64D33/02;F02C7/047;(IPC1-7):F02C7/047 主分类号 B64D15/04
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