Stiffened beam assembly

Patent metadata

Field	Value
Publication number	US-10683078-B2
Application number	US-201916408282-A
Country	US
Kind code	B2
Filing date	May 9, 2019
Priority date	Apr 7, 2016
Publication date	Jun 16, 2020
Grant date	Jun 16, 2020

Abstract

Methods and apparatuses may include a stiffened beam assembly including a structural beam portion having a web and upper and lower flanges, and at least one continuous stiffening member extending back and forth between the upper and lower flanges on one side of the web, forming one or more trusses or other reinforcing structures. The beam portion and/or the stiffening member(s) may comprise formed sheet metal. The stiffening member(s) may be mechanically attached to the beam portion.

First claim

What is claimed is:

1. An internally-stiffened structural beam assembly comprising:
an elongate beam having a length and a web portion extending along the length of the beam, a first flange, and a second flange spaced from and opposing the first flange across an exterior face of the web portion; and
one or more stiffening members attached to the exterior face of the web portion, each comprising a continuous ribbon having a plurality of bends and extending alternatingly between the first flange and the second flange along the length of the beam, wherein each bend of the plurality of bends of the continuous ribbon is affixed to either the first flange or the second flange.

2. The assembly of claim 1 , wherein each stiffening member forms a plurality of trusses.

3. The assembly of claim 1 , wherein each stiffening member comprises a plurality of straight segments, each of the straight segments being fixed at a first end to the first flange and fixed at a second end to the second flange.

4. The assembly of claim 3 , wherein a long axis of at least one of the straight segments is oblique to the length of the beam.

5. The assembly of claim 1 , wherein the beam has a C-shaped cross section.

6. The assembly of claim 1 , wherein the first flange is curved along the length of the beam.

7. The assembly of claim 1 , wherein each stiffening member has an edge flange fixed to the web portion of the beam.

8. The assembly of claim 7 , wherein each stiffening member has a stiffening flange disposed opposite to the edge flange.

9. The assembly of claim 1 , wherein the continuous ribbon comprises a plastic.

10. The assembly of claim 1 , wherein the continuous ribbon comprises a metal.

11. A method of assembling a reinforced structural beam, the method comprising:
forming a plurality of bends in a continuous ribbon to create a corresponding plurality of straight segments configured to extend back and forth between opposing flanges of a beam, the opposing flanges of the beam extending orthogonal to a web plane defined by a web of the beam; and
attaching the continuous ribbon to the beam by disposing the ribbon adjacent an exterior face of the web of the beam and affixing the ribbon to the exterior face of the web and to one of the opposing flanges at each of the bends.

12. The method of claim 11 , wherein attaching the continuous ribbon to the beam further comprises affixing at least one segment of the ribbon to the web of the beam.

13. The method of claim 12 , wherein the ribbon comprises a plastic and affixing the at least one segment of the ribbon includes welding the ribbon.

14. An airfoil comprising:
a leading edge portion of the airfoil;
a trailing edge portion of the airfoil; and
one or more reinforced rib portions spanning a gap between the leading edge portion and the trailing edge portion, each reinforced rib portion including an elongate beam having a web portion, a first flange, and a second flange spaced from and opposing the first flange across a face of the web portion, and one or more continuous stiffening members disposed adjacent the face of the web portion, each stiffening member comprising a continuous ribbon having a plurality of bends and extending alternatingly between the first flange and the second flange along a respective length of the beam, wherein the continuous ribbon is affixed to one of the first and second flanges at each of the bends.

15. The airfoil of claim 14 , further including a skin enclosing an upper and a lower surface of the airfoil.

16. The airfoil of claim 15 , wherein the skin comprises the enlongate beam of at least one of the reinforced rib portions.

17. The airfoil of claim 14 , wherein the rib portions are disposed substantially parallel to each other along a length of the airfoil.

18. The airfoil of claim 14 , further comprising an aircraft having an airframe including the airfoil.

19. The airfoil of claim 18 , wherein the airfoil comprises a wing of the aircraft.

20. The airfoil of claim 14 , wherein the continuous ribbon comprises a plastic material.

Assignees

• Boeing Co

Inventors

• Sullivan Kevin Lee

Classifications

• B64C1/065

  Spars · CPC title

• E04C3/09

  at least partly of bent or otherwise deformed strip- or sheet-like material · CPC title

• E04C2003/0434

  the open cross-section free of enclosed cavities · CPC title

• E04C2003/0413

  being built up from several parts · CPC title

• E04C2003/0452

  H- or I-shaped · CPC title