Wing spar splice joint
AssigneeGlobal Aerosystems, LLC
InventorsCharles A. Rhoden, Stephen C. Daschel, Randolph L. Henry, Russell E. Thibaut
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AssigneeGlobal Aerosystems, LLC
InventorsCharles A. Rhoden, Stephen C. Daschel, Randolph L. Henry, Russell E. Thibaut
Estimating the term…
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.
A wing spar joint for coupling the inboard ends of a right wing spar and a left wing spar, each wing spar comprising an elongated structural member including a planar web portion terminating in longitudinal edges, a top chord and a bottom chord extending from the longitudinal edges of the web portion, the top and bottom chords terminating in longitudinal edges and including a flange integral with the longitudinal edge of each of the top chord and the bottom chord, the wing spar joint comprising:
Dependencies are inferred from the claim text.