发明名称 METHOD OF FORMING LAMINATED WING SPAN FOR AERODYNAMIC ROTOR BLADE
摘要 A simplified layup mandrel with no contour or twist is utilized by the method of this invention for forming the spar member of an aerodynamic rotor blade. A fiber glass tape is wrapped (laid-up) to a desired thickness onto the simplified mandrel to form a strap as the initial step. Because of the simple design of the mandrel, the laid-up strap when removed from the mandrel has a basic U-shaped configuration with straight extending legs having substantially parallel vertically oriented faces. This strap is then placed on a forming mandrel and contoured to the desired shape either by hand or by coining in a forming die. The contoured strap is then utilized in any of the various subassemblies or final assembly of the composite aerodynamic rotor blade.
申请公布号 JPS5330600(A) 申请公布日期 1978.03.22
申请号 JP19770105383 申请日期 1977.08.30
申请人 BOEING CO 发明人 REIMONDO PII BERUKO;EDO FURANKU
分类号 B64C3/18;B64C27/46;B64C27/473 主分类号 B64C3/18
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