发明名称 Blade seal for an aircraft
摘要 A blade seal (20) for an aircraft has a mounting structure (22). A composite blade (26) is attached to the mounting structure (22). The composite blade (26) has a plurality of holes (28). An elastomer substance (30) is used to fill the plurality of holes (28).
申请公布号 US5913494(A) 申请公布日期 1999.06.22
申请号 US19970900634 申请日期 1997.07.25
申请人 MCDONNELL DOUGLAS 发明人 BURBRIDGE, THOMAS EDWARD;TOMKO, HARVEY JOHN;WILLE, ROBERT HENRY
分类号 B64C3/26;B64C9/02;(IPC1-7):B64C3/58;B64C1/38;F16J15/00 主分类号 B64C3/26
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