发明名称 WING SPAR SPLICE JOINT
摘要 A wing spar joint is provided for coupling the inboard ends of a right wing spar and a left wing spar. The wing spar joint comprises a forward fitting, an aft fitting, a spar cap a lower chord fitting and a strap member. A first plurality of fasteners secure the forward fitting and the aft fitting together through a web portion of the wing spars. A second plurality of fasteners secure the upper spar cap, the lower spar cap and the forward fitting together through upper chords of the wing spars. A third plurality of fasteners secure the lower chord fitting, the strap member and the forward fitting together through lower chords of the wing spars. The forward fitting, aft fitting, spar cap and strap member are thus secured together with the wing spars to form a rigid connecting joint at the inboard ends of the wing spars.
申请公布号 US2011215202(A1) 申请公布日期 2011.09.08
申请号 US20100962506 申请日期 2010.12.07
申请人 GLOBAL AEROSYSTEMS, LLC 发明人 RHODEN CHARLES A.;DASCHEL STEPHEN C.;HENRY RANDOLPH L.;THIBAUT RUSSELL E.
分类号 B64C3/18 主分类号 B64C3/18
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