Bonded splice joint

• US 8,915,471 B2
• Filed: 02/12/2014
• Issued: 12/23/2014
• Est. Priority Date: 03/07/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Nordman, Paul, Nelson, Paul
• Primary Examiner(s): Bonzell, Philip J
• Application Number:
  US14/178,543
• Publication Number:
  US 20140161512A1
• Time in Patent Office: 314 Days
• Field of Search: 244/131, 244/132, 244/119, 244/123.1, 244/123.7, 244/123.2
• US Class Current: 244/131
• CPC Class Codes: B64C 1/26 Attaching the wing or tail units or stabilising surfaces
• CPC Class Codes: B64C 3/182 Stringers, longerons
• CPC Class Codes: Y10T 403/472 including mechanical interlock
• CPC Class Codes: Y10T 403/50 Bridged by diverse connector

Abstract

An apparatus for an aircraft structure comprising first and second stringers, each having a vertical stringer portion defining a lengthwise gap. The structure may include a fitting having a central rib attachment member and first and second extensions extending in opposite directions from said central rib attachment member. Stringer attachment portions extending up from said first and second extensions are inserted into the lengthwise gaps of the first and second stringer portions, respectively. The rib attachment member may be attached to a side-of-body rib.

Claims

1. A joint assembly, comprising:

first and second stringers, each having a vertical stringer portion; and

a fitting having a central rib attachment member and first and second fitting extensions extending in opposite directions from said central rib attachment member, said first and second fitting extensions having vertical stringer attachment portions coupled to the vertical stringer portion of said first and second stringers, respectively, at a distal end of said first and second stringers.

2. The joint assembly of claim 1, further comprising a disbond arrest fastener fastened through said vertical stringer portions of said first and second stringers and through said stringer attachment portions of said first and second fitting extensions.

3. The joint assembly of claim 1, wherein said vertical stringer portion of each of the first and second stringers defines a lengthwise gap in the vertical stringer portion, and said vertical stringer attachment portions are inserted into said lengthwise gap in the vertical stringer portion.

4. The joint assembly of claim 3, wherein said vertical stringer attachment portions are inserted into said lengthwise gap at the distal end of the first and second stringers, each of the stringers having a thickness that gradually increases from the distal end.

5. The joint assembly of claim 4, wherein the stringers are t-shaped and comprise a horizontal stringer portion and the vertical stringer portion, the vertical stringer portion extending up from the horizontal stringer portion.

6. The joint assembly of claim 5, further comprising first and second flat stringer bases coupled to said horizontal stringer portion of said first and second t-shaped stringers, respectively.

7. The joint assembly of claim 6, further comprising a continuous skin section coupled to bottom surfaces of said first and second stringer bases and said fitting.

8. The joint assembly of claim 7, wherein said first and second stringers, said first and second stringer bases, said skin section and said fitting are co-cured.

9. The joint assembly of claim 6, wherein said first and second flat stringer bases have greater stiffness than said first and second t-shaped stringer.

10. The joint assembly of claim 9, wherein said first and second fitting extensions are sandwiched between said first and second t-shaped stringers and said first and second flat stringer bases within first and second transition areas, thereby forming a spliced joint.

11. The joint assembly of claim 10, wherein each of the flat stringer bases has a thickness that gradually reduces from a distal end of the transition areas to said proximal end of the transition areas.

12. The joint assembly of claim 10, further comprising one or more fillers shaped and positioned to occupy voids not occupied by said first and second t-shaped stringers, said first and second flat stringer bases, and said first and second fitting extensions, within said first and second transition areas.

13. The joint assembly of claim 1, wherein each of the fitting extensions has a thickness that gradually decreases from said central rib attachment member.

14. The joint assembly of claim 13, wherein the fitting extensions are t-shaped and comprise a horizontal fitting portion and the vertical stringer attachment portions, the vertical stringer attachment portions extending up from the horizontal fitting portion.

15. The joint assembly of claim 14, wherein the horizontal fitting portion has diagonal edges such that a width of the horizontal fitting portion is greater closer to a bottom surface and smaller near a top surface of the horizontal fitting portion.

16. A joint assembly coupled to a rib web having a plurality of vertical stiffeners, said joint assembly comprising:

first and second stringers, each having a vertical stringer portion; and

a fitting having a central rib attachment member and first and second fitting extensions extending in opposite directions from said central rib attachment member, said first and second fitting extensions having vertical stringer attachment portions coupled to said first and second stringers, respectively, at a distal end of said first and second stringers;

said central rib attachment member being coupled to said rib web.

17. The joint assembly of claim 16, wherein said vertical stringer portion in each of the first and second stringers defines a lengthwise gap in the vertical stringer portion, and the vertical stringer attachment portions are inserted into said lengthwise gap of said first and second stringers.

18. The joint assembly of claim 16, wherein said central rib attachment member is coupled to said rib web through the use of a fastener extending through said central rib attachment member, at least one of said plurality of vertical stiffeners and said rib web.

19. The joint assembly of claim 16, wherein said fitting is a cruciform fitting comprising titanium.

20. The joint assembly of claim 16, wherein said first and second stringers comprises a horizontal stringer portion and the vertical stringer portion extends up from the horizontal stringer portion;

and further comprising first and second stringer bases coupled to said horizontal stringer portion of said first and second t-shaped stringers, respectively.

21. The joint assembly of claim 20, further comprising a continuous skin section coupled to said first and second stringer bases and to said fitting;

said first and second t-shaped stringers, said first and second flat stringer bases, said skin section and said fitting being co-cured.

22. An aircraft having a side-of-body joint, said side of body joint comprising:

a rib web; and

a plurality of side of body joint assemblies arranged side by side, each side of body joint assembly comprising;

first and second stringers, each having a vertical stringer portion;

a fitting having a central rib attachment member and first and second fitting extensions extending in opposite directions from said central rib attachment member, said first and second fitting extensions having vertical stringer attachment portions coupled to said first and second stringers, respectively, at a distal end of said first and second stringers;

each of said central rib attachment members of said plurality of side of body joint assemblies being coupled to said rib web; and

the fittings of the plurality of side of body joint assemblies arrayed to form a segmented outer chord of a side of body rib.

23. The aircraft of claim 22, wherein said vertical stringer portion in each of the first and second stringers defines a lengthwise gap in the vertical stringer portion, and the vertical stringer attachment portions are inserted into said lengthwise gap of said first and second stringers.