Patent ID: 11878793
Assignee: THE BOEING COMPANY
Field: Other special machines (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 15:
16. A wing comprising the apparatus of claim 1, comprising:
the panels comprising a first panel and a second panel;
a base skin including the second panel;
a top skin including the first panel;
a wing box including:
a forward spar section including:
a first spar chord attached to the first panel at a first position;
a second spar chord attached to the second panel at a second position; and
a first spar connecting the first spar chord and the second spar chord; an aft spar section including:
a third spar chord attached to the first panel at a third position;
a fourth spar chord attached to the second panel at a fourth position; and
a second spar connecting the third spar chord and the fourth spar chord; and

wherein:

the first spar and the second spar each extend along a length of an interior of the wing between a root end of the wing and a tip end of the wing; and
the first spar and the second spar each intersect with a plurality of ribs directly attached to the base skin and the top skin; and
each of the ribs are located within the wing box at a plurality of different locations along the length of the wing.