Wing and method of manufacturing

Patent metadata

Field	Value
Publication number	US-10179640-B2
Application number	US-201615245769-A
Country	US
Kind code	B2
Filing date	Aug 24, 2016
Priority date	Aug 24, 2016
Publication date	Jan 15, 2019
Grant date	Jan 15, 2019

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.

First claim

What is claimed is:

1. 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.

2. The wing of claim 1 wherein said sleeve, said flange, and said dome form a unitary nut plate.

3. The wing of claim 2 wherein said nut plate is made by an additive manufacturing process.

4. The wing of claim 1 wherein:
each one of said spar fastener holes has a spar fastener hole diameter;
each one of said skin fastener holes has a skin fastener hole diameter;
said spar fastener hole diameter is larger than said skin fastener hole diameter; and
said flange has a maximum flange dimension, measured in a direction transverse to said nut plate center axis, that is larger than said spar fastener hole diameter.

5. The wing of claim 4 wherein said plurality of spar fastener holes are drilled in said spars by a determinate assembly process, and wherein said plurality of said skin fastener holes are drilled in said spars by said determinate assembly process.

6. The wing of claim 1 wherein:
said fastener has a fastener center axis that is coincident with said skin fastener hole center axis; and
linear movement of said nut in said direction perpendicular to said nut plate center axis coaxially aligns said nut center axis with said fastener center axis.

7. The wing of claim 4 wherein:
said sleeve has a maximum sleeve diameter; and
said maximum sleeve diameter is expanded by a cold working process to be equal to said spar fastener hole diameter to couple said sleeve to said one of said spars within said one of said spar fastener holes by circumferential tension.

8. The wing of claim 1 wherein said sleeve comprises a dielectric coating disposed on an interior surface of said sleeve.

9. The wing of claim 1 wherein:
said sleeve comprises a sleeve height;
said spar comprises a spar thickness; and
said spar height is approximately equal to said spar thickness.

10. The wing of claim 1 wherein:
said flange of said nut plate comprises a flange conductive surface that at least partially defines said interior recess;
said nut comprises a nut conductive surface that at least partially forms said collar; and
said nut conductive surface and said flange conductive surface are in direct contact with each other.

11. The wing of claim 1 wherein said skin fastener holes are aligned with said spar fastener holes so that, in plan view, each one of said skin fastener holes is circumscribed by a corresponding one of said spar fastener holes and said skin fastener hole center axis is one of parallel to or coincident with said spar fastener hole central axis.

12. The wing of claim 1 further comprising a lubricant applied to a threaded interface between said threaded fastener and said nut.

13. The wing of claim 1 wherein:
said dome of said nut plate defines an interior chamber that has a volume;
a first portion of said volume accommodates said nut;
a second portion of said volume is open; and
said second portion of said volume is at least 50 percent of said first portion of said volume.

14. The wing of claim 6 wherein:
said sleeve extends along said nut plate center axis;
said flange extends perpendicular to said nut plate center axis;
said dome extends along said nut plate center axis; and
said nut plate center axis is coincident with said spar fastener hole center axis.

15. The wing of claim 14 wherein:
said nut body extends along said nut center axis;
said collar extends perpendicular to said nut center axis; and
said nut center axis is one of parallel to or coincident with said nut plate center axis.

16. 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.

17. The wing of claim 16 wherein said sleeve, said flange, and said dome form a unitary member made by an additive manufacturing process.

18. The wing of claim 16 wherein:
said sleeve has a maximum sleeve diameter; and
said

Assignees

• Boeing Co

Inventors

• Wilkerson Jeffrey A

Classifications

• B64C3/26 Primary

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title

• F16B37/044

  Nut cages · CPC title

• F16B5/0225

  allowing for adjustment parallel to the plane of the plates · CPC title

• B64C3/185

  Spars · CPC title

• B64F5/0009

  Operations & Transport · mapped topic