CPC B64C 3/18 (2013.01) [B64C 1/1446 (2013.01); B64C 3/32 (2013.01); B64C 1/26 (2013.01)] | 20 Claims |
1. An aircraft structure comprising:
an aircraft wing comprising:
a center wing section having a continuous structure that spans beyond opposite sides of an aircraft fuselage and which terminates respectively at center wing section ends;
a pair of outboard wing sections each having an inboard end, and each outboard wing section is attached to a center wing section end by a truss system that is accessible via a closeout panel;
wherein:
the center wing section and the outboard wing sections each have a top portion and a bottom portion each having one or more span-wise extending stringers;
at least one stringer on the bottom portion of the center wing section terminates at a spaced distance from at least one stringer on the bottom portion of an outboard wing section to define a spanwise stringer gap at the location of the closeout panel;
each truss system comprises:
an upper fitting coupling a stringer on the top portion of the center wing section to a stringer on the top portion of an outboard wing section;
a lower fitting extending across the spanwise stringer gap and interconnecting a stringer on the bottom portion of the center wing section to a stringer on the bottom portion of an outboard wing section;
a center wing section strut extending between the upper fitting and the lower fitting at the center wing section end; and
an outboard wing section strut extending between the upper fitting and the lower fitting at the inboard end of the outboard wing section.
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