Stiffened beam assembly

Patent metadata

Field	Value
Publication number	US-10315751-B2
Application number	US-201615093659-A
Country	US
Kind code	B2
Filing date	Apr 7, 2016
Priority date	Apr 7, 2016
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

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 continuous stiffening members attached to the exterior face of the web portion, each comprising a continuous metal 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 metal ribbon is affixed to either the first flange or the second flange.

2. The assembly of claim 1 , wherein each continuous 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 first flange and the second flange extend orthogonally with respect to the exterior face of the web portion.

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

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

8. A structural beam assembly comprising:
an elongate beam having a length and a web portion extending along the length of the beam between opposing flanges; and
a plurality of trusses attached to an exterior face of the web portion and spanning the web between the opposing flanges;
wherein the plurality of trusses are formed by a single continuous stiffening member comprising a continuous metal ribbon having a plurality of bends and extending back and forth between the opposing flanges along the length of the beam, wherein the continuous metal ribbon is affixed to one of the opposing flanges at each of the bends.

9. The assembly of claim 8 , wherein the stiffening member comprises a flat ribbon formed into a series of straight segments and oriented orthogonal to the web portion of the beam.

10. The assembly of claim 9 , wherein each segment has respective end portions affixed to at least one of the opposing flanges and an edge portion affixed to the web portion of the beam.

11. The assembly of claim 8 , wherein the stiffening member has an edge flange welded to the web portion of the beam.

12. The assembly of claim 11 , wherein the stiffening member has a stiffening flange disposed opposite to the edge flange.

13. A method of assembling a reinforced structural beam, the method comprising:
forming a plurality of bends in a continuous metal 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 metal ribbon to the beam by disposing the ribbon adjacent one 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.

14. The method of claim 13 , wherein attaching the continuous metal ribbon to the beam further comprises affixing at least one segment of the ribbon to the web of the beam.

15. The method of claim 13 , wherein the beam comprises sheet metal.

16. The method of claim 13 , wherein the beam has a C-shaped cross section.

17. The method of claim 13 , wherein at least one of the opposing flanges is curvilinear.

18. The method of claim 13 , wherein forming the plurality of bends comprises forming the plurality of bends using a brake press.

19. 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 metal 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 metal ribbon is affixed to one of the first and second flanges at each of the bends.

20. The airfoil of claim 19 , further including a skin enclosing an upper and a lower surface of the airfoil.

21. The airfoil of claim 20 , wherein the skin comprises the beam portion of at least one of the reinforced rib portions.

22. The airfoil of claim 19 , wherein the rib portions are disposed substantially parallel to each other along a length of the airfoil.

23. An aircraft comprising:
an airframe including an airfoil;
the airfoil comprising an elongate beam having a web portion and opposing flanges, a plurality of trusses coupled to the beam and spanning the web between the opposing flanges;
wherein the plurality of trusses are formed by at least one single continuous stiffening member disposed adjacent the face of the web portion and comprising a continuous metal ribbon having a plurality of bends and extending back and forth between the opposing flanges along a respective length of the beam, wherein the continuous metal ribbon is affixed to one of the opposing flanges at each of the bends.

24. The aircraft of claim 23 , wherein the airfoil comprises a wing of the aircraft.

25. The aircraft of claim 23 , wherein the elongate beam comprises a transverse rib of the airfoil.

Assignees

• Boeing Co

Inventors

• Sullivan Kevin Lee

Classifications

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• E04C2003/0473

  U- or C-shaped · CPC title

• E04C3/09

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

• B64C3/187 Primary

  Ribs · CPC title

• E04C2003/0434

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