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US 10,179,640 B2Granted
Wing and method of manufacturing
AssigneeThe Boeing Company
InventorJeffrey A. Wilkerson
Life of this patent
Estimating the term…
Abstract
A wing includes a wing box including interconnected spars, an interior system installed within the wing box, an opposed pair of skins fastened to and covering the wing box, wherein one of the skins closes out the wing, and a plurality of fastening systems configured to fasten the skins to the spars and provide protection from electromagnetic effects, wherein each one of the fastening systems includes a threaded fastener, a nut plate including a body and a cover, and a nut enclosed within the nut plate between the body and the cover, wherein the nut is restricted from rotation within the nut plate about a nut plate axis and is free to move linearly within the nut plate orthogonal to the nut plate axis.
Claims20
A wing comprising:
- a wing box comprising interconnected spars, wherein each one of said spars comprises a plurality of spar fastener holes and each one of said spar fastener holes has a spar fastener hole central axis;
- an interior system installed within said wing box;
- a plurality of skins abutted with said spars and covering said wing box, wherein each one of said skins comprises a plurality of skin fastener holes and each one of said skin fastener holes has a skin fastener hole center axis;
- and
- a plurality of fastening systems coupling said skins and said spars together, wherein each one of said fastening systems comprises:
- a threaded fastener located in one of said skin fastener holes;
- a nut plate coupled to one of said spars, wherein said nut plate has a nut plate center axis and comprises:
- a tubular sleeve located in one of said spar fastener holes;
- a dome extending from said sleeve;
- and
- a flange located between said sleeve and said dome and defining an interior recess, wherein said flange is abutted with said one of said spars opposite one of said skins;
- and
- a nut enclosed by said nut plate, wherein said nut has a nut center axis and comprises:
- a nut body located in said dome and threadably coupled with said threaded fastener;
- and
- collar extending from said nut body and located in said interior recess of said flange,
- wherein said interior recess of said flange is complementary to said collar of said nut to prevent rotational movement of said nut about said nut center axis and to allow linear movement of said nut perpendicular to said nut plate center axis when said skin fastener hole center axis is parallel to said spar fastener hole central axis.
14 more elements
A wing comprising:
- a spar comprising a spar fastener hole having a spar fastener hole diameter and a spar fastener hole central axis;
- a skin abutted with said spar and comprising a skin fastener hole having a skin fastener hole center axis, wherein said skin fastener hole is aligned with said spar fastener hole so that, in plan view, said skin fastener hole is circumscribed by said spar fastener hole and said skin fastener hole center axis is one of parallel to or coincident with said spar fastener hole central axis;
- a threaded fastener located in said skin fastener hole and having a fastener center axis coincident with said skin fastener center axis;
- a nut plate coupled to said spar, said nut plate has a nut plate center axis and comprises:
- a tubular sleeve extending along said nut plate center axis and located in said spar fastener hole so that said nut plate center axis is coincident with said spar fastener hole central axis;
- a dome extending from said sleeve along said nut plate center axis;
- and
- a flange located between said sleeve and said dome and defining an interior recess, wherein said flange is abutted with said spar opposite said skin and has a maximum flange dimension, measured in a direction perpendicular to said nut plate center axis, that is larger than said spar fastener hole diameter of said spar fastener hole;
- a nut enclosed by said nut plate, said nut has a nut center axis and comprises:
- a nut body extending along said nut center axis and located in said dome, wherein said nut body is threadably coupled with said threaded fastener;
- and
- a collar extending from said nut body perpendicular to said nut central axis and located in said interior recess of said flange,
- wherein said interior recess of said flange is complementary to said collar of said nut to prevent rotational movement of said nut about said nut central axis and to allow linear movement of said nut in a direction perpendicular to said nut plate center axis to coaxially align said nut center axis with said fastener center axis when said skin fastener hole center axis is parallel to said spar fastener hole central axis.
10 more elements
Dependencies are inferred from the claim text.