IP Library › Granted Patent US 9,387,628
Granted Patent B2
US 9,387,628 · App. 14/219,629 · Granted Jul 12, 2016

Method and apparatus for fabricating composite stringers

Inventors: Michael R. Chapman (Federal Way, WA); Khanh M. Pham (Kent, WA)
Assignee: THE BOEING COMPANY
B29C70/462B29L2031/001
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Quick Facts
Patent No.
US 9,387,628
App. No.
14/219,629
Granted
Jul 12, 2016
Kind
B2
Abstract

Method and tooling apparatus for forming a composite charge into a stringer having an I-shaped cross-section. A substantially flat composite charge is placed on a die set and pressed formed into a die set cavity to form a stringer hat. A stringer base is formed by press forming the composite charge against the die set. The die set is used to compress the stringer hat into a stringer web having a bulb on one end thereof. A stringer cap is formed by press forming the bulb within a recess in the die set.

Claims (19)

1. A method of fabricating a composite I-stringer, comprising:

folding a substantially flat charge into a partially formed stringer charge having a bulb, a base and a web extending between the bulb and the base;

placing a first plate against the base;

positioning die portions respectively on opposite sides of the web;

placing shims on the die portions on opposite sides of the bulb;

compressing the web using the die portions;

heating the bulb to its forming temperature;

placing a second plate against the bulb;

compressing the bulb into a substantially flat cap by applying pressure to the second plate; and

using the shims to control compression of the bulb into a desired flat cap thickness.

2. The method of claim 1 , wherein the first plate and the second plate are substantially parallel surfaces.

3. The method of claim 1 , wherein compressing the bulb comprises applying pressure in a substantially normal direction relative to a base of the composite I-stringer.

4. The method of claim 1 , wherein folding includes forming the bulb on an end of the web.

5. The method of claim 4 , wherein forming the bulb further comprises forming a portion of the web into a recess in the die portions.

6. The method of claim 1 , wherein compressing the bulb is performed using a punch.

7. The method of claim 6 , wherein compressing the web is performed by applying lateral pressure on the die portions.

8. The method of claim 1 , wherein heating the bulb comprises locally heating the bulb.

9. The method of claim 8 , wherein heating the bulb is performed before the bulb is compressed.

10. The method of claim 1 , wherein the shims have a thickness corresponding to a desired thickness of the substantially flat cap.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 19, 2014
From: CHAPMAN, MICHAEL R.; PHAM, KHANH M.
To: THE BOEING COMPANY
Reel/Frame 032477/0308 →
Continuity (3)
Continuation In Part 13916779 · Jun 13, 2013
Continuation In Part 13217109 · Aug 24, 2011
Related Publication 20140203477A1 · Jul 24, 2014