IP Library Granted Patent US 10,160,076
Granted Patent B2
US 10,160,076 · App. 13/722,526 · Granted Dec 25, 2018

Edge stabilizing system and method for composite barrel segments

Inventors: Li C Chang (Mount Pleasant, SC); Richard M Coleman (Renton, WA); Ronald J Steckman (North Charleston, SC); Andrew M Huckey (Mount Pleasant, SC); Nicholas A Norman (Summerville, SC)
Assignee: THE BOEING COMPANY
B23Q3/00B64F5/10B64F5/50Y10T29/49998
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Quick Facts
Patent No.
US 10,160,076
App. No.
13/722,526
Granted
Dec 25, 2018
Kind
B2
Abstract

An edge stabilizer for a composite structure includes an elongate edge support segment, defining a geometric shape of an edge of the composite structure, and a connector, configured to attach the edge support segment to the edge of the composite structure. The edge support segment comprises first and second halves configured to attach together around the edge, each half including a shoulder, opposing mating relationship of the shoulders defining a slot for receiving the edge. The edge stabilizer can be part of a system for stabilizing an edge of a composite barrel section. The system can also include a moveable cart, the barrel section being supportable upon the cart.

Claims (33)

1. An edge stabilizer for a composite structure, comprising:

an elongate edge support segment, defining a geometric shape of an edge of the composite structure, comprising separable first and second halves configured to attach together around the edge, each half including a shoulder, opposing mating relationship of the shoulders defining a slot for receiving the edge; and

a connector, configured to attach the edge support segment to the edge of the composite structure, wherein the connector is a clamp that fits over an outer edge of each of the first and second halves of the elongate edge support segment and wherein at least one of the halves includes indexing pins, configured to insert into indexing holes disposed near the edge of the composite structure.

2. An edge stabilizer in accordance with claim 1 , wherein the slot has a thickness that is less than a thickness of the composite structure.

3. An edge stabilizer in accordance with claim 1 , wherein at least one of the first and second halves further comprise an integral flange, extending substantially perpendicularly with respect to the composite structure.

4. An edge stabilizer in accordance with claim 1 , wherein the edge support segment includes cutout portions in which the edge of the composite structure is exposed.

5. An edge stabilizer in accordance with claim 4 , wherein the cutout portions each have a front, and further comprising a reinforcing bar, disposed across the front.

6. An edge stabilizer in accordance with claim 1 , wherein the edge support segment includes a tab extending therefrom, substantially in a plane of the composite structure.

7. An edge stabilizer in accordance with claim 1 , wherein the edge support segment is configured to bridge across an end of an opening in the composite structure.

8. An edge stabilizer in accordance with claim 1 , wherein the elongate edge support segment further comprises interlocking structure at longitudinal ends thereof, the interlocking structure configured to attach a plurality of elongate edge support segments end-to-end in series.

9. An edge stabilizer in accordance with claim 1 , wherein the elongate edge support segment defines about one sixth of a circle.

10. The edge stabilizer of claim 1 , wherein the slot defined by the opposing mating relationship of the shoulders is between the shoulders.

11. The edge stabilizer of claim 1 , wherein the clamp further comprises a two-part clamp.

12. The edge stabilizer of claim 4 , wherein the cutout portions are configured to receive the clamp.

13. A system for stabilizing edges of a composite barrel section, comprising:

a plurality of elongate edge support segments, defining a geometric shape of an edge of the composite barrel section, comprising first and second halves, the halves configured to attach together around the edge, each half including a shoulder, opposing mating relationship of the shoulders defining a slot for receiving the edge;

a connector, configured to attach the edge support segment to the edge, wherein the connector is a clamp that fits over an outer edge of each of the first and second halves of the elongate edge support segment; and

a moveable cart, the barrel section being supportable upon the cart.

14. A system in accordance with claim 13 , wherein at least one of the first and second halves further comprise an integral flange, extending substantially perpendicularly with respect to the barrel section.

15. A system in accordance with claim 13 , wherein the plurality of elongate edge support segments comprise interlocking structure at longitudinal ends thereof, the interlocking structure configured to attach a plurality of elongate edge support segments end-to-end in series.

16. A system in accordance with claim 13 , wherein the plurality of elongate edge support segments include one of cutout portions in which the edge of the composite barrel section is exposed, and an integral tab extending therefrom, configured for mechanical gripping.

17. A system in accordance with claim 13 , wherein the edge support segment is configured to bridge across an end of an opening in the composite barrel section.

18. The system of claim 13 , wherein the slot defined by the opposing mating relationship of the shoulders is between the shoulders.

19. The system of claim 13 , wherein the clamp further comprises a two-part clamp.

20. The system of claim 13 , further comprising a pair of pins, each pin extends from a longitudinal end of the first and second halves of the elongate edge support segment.

21. The system of claim 20 , wherein the pair of pins are configured to insert into corresponding holes in an adjacent elongate edge support segment.

22. The system of claim 13 , wherein the slot further comprises a U-shaped slot.

23. The system of claim 13 , wherein the first and second halves of the elongate edge support segment each further comprise at least one clamp slot.

24. An edge stabilizer, for a composite structure, comprising:

an elongate edge support segment, defining a geometric shape of an edge of the composite structure, comprising separable first and second halves configured to attach together around the edge, each half including a shoulder, opposing mating relationship of the shoulders defining a slot for receiving the edge; and

a connector, configured to attach the edge support segment to the edge of the composite structure, wherein the connector is a clamp that fits over an outer edge of each of the first and second halves of the elongate edge support segment and wherein the slot further comprises a U-shaped slot.

25. The edge stabilizer of claim 24 , further comprising a pair of pins, each pin extends from a longitudinal end of the first and second halves of the elongate edge support segment.

26. The edge stabilizer of claim 25 , wherein the pair of pins are configured to insert into corresponding holes in an adjacent elongate support segment.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 27, 2018
From: CHANG, LI C.; HUCKEY, ANDREW M.; COLEMAN, RICHARD M.; NORMAN, NICHOLAS A.; STECKMAN, RONALD J.
To: THE BOEING COMPANY
Reel/Frame 047158/0254 →
Continuity (2)
Continuation In Part 13622035 · Sep 18, 2012
Related Publication 20140077434A1 · Mar 20, 2014
Cited By (5)
US 12,234,085 US 12,378,064 US 12,466,639 US 12,570,199 US 12,649,405