发明名称 Hinge line skin system for an aircraft
摘要 A hinge line system (52) for an aircraft has a structural block (22) attached to a first edge of a hinge line. The structural block (22) has a flange (28) attached to a first end of an elastic sheet (32). A second structural block (24) is attached to a second edge of the hinge line. The second structural block (24) has a second flange (30) attached to a second end of the elastic sheet (32).
申请公布号 US5941480(A) 申请公布日期 1999.08.24
申请号 US19970852870 申请日期 1997.05.08
申请人 MCDONNELL DOUGLAS 发明人 WILLE, ROBERT HENRY
分类号 B64C3/48;B64C9/02;(IPC1-7):B64C1/06;B64C3/58 主分类号 B64C3/48
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