发明名称 REDUCED AMPLITUDE CORRUGATED WEB SPAR
摘要 A reduced amplitude corrugated web spar for use in airplane wings and the like is disclosed. The amplitude of the corrugation is determined based upon gen eral stability requirements of the spar, and the fasteners are offset from the center line of the web corrugations. The resulting spar is easier to manufacture and still prov ides the structural integrity required of the wings.
申请公布号 CA2207403(A1) 申请公布日期 1997.12.20
申请号 CA19972207403 申请日期 1997.06.10
申请人 THE BOEING COMPANY 发明人 GILLESPIE, TIMOTHY E.
分类号 B64C9/18;E04C3/28;(IPC1-7):B64C3/18 主分类号 B64C9/18
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