Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same

Patent metadata

Field	Value
Publication number	US-9387629-B2
Application number	US-201414312401-A
Country	US
Kind code	B2
Filing date	Jun 23, 2014
Priority date	Jun 24, 2012
Publication date	Jul 12, 2016
Grant date	Jul 12, 2016

Abstract

There is provided a method of making a composite hat stiffener. The method has the steps of curing a composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener. The pre-cured composite hat stiffener has a composite hat section, a plurality of composite stiffening plies with a body ply, a wrap ply, and a base ply, all coupled to the composite hat section, wherein the body ply is coupled to a first side of the composite hat section, the wrap ply is coupled to the body ply, and the base ply is coupled to the body ply and the wrap ply, a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies, and an outer ply coupled to the composite hat section. The method further includes bonding the pre-cured composite hat stiffener to a structure surface.

First claim

What is claimed is:

1. A method of making a composite hat stiffener, the method comprising the steps of:
adding a composite hat stiffener slot opening to the composite hat stiffener;
curing the composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener, the pre-cured composite hat stiffener comprising:
a composite hat section;
a plurality of composite stiffening plies comprising a body ply, a wrap ply, and a base ply, all coupled to the composite hat section, wherein the body ply is coupled to a first side of the composite hat section, the wrap ply is coupled to the body ply, and the base ply is coupled to the body ply and the wrap ply;
a vacant composite hat stiffener slot opening positioned at a base portion of the composite hat stiffener and formed by alignment of a wrap ply slot opening and a base ply slot opening;
a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies; and,
an outer ply coupled to the composite hat section; and,

bonding the pre-cured composite hat stiffener to a structure surface.

2. The method of claim 1 further comprising prior to the step of curing the composite hat stiffener, the step of coupling a peel ply to the composite hat stiffener, and after the step of curing, the step of removing the peel ply from the composite hat stiffener.

3. The method of claim 1 further comprising after the step of curing, optionally the step of enlarging the composite hat stiffener slot opening.

4. The method of claim 1 further comprising prior to the step of curing the composite hat stiffener, the step of chamfering edges of a pair of flanges of the composite hat stiffener.

5. The method of claim 1 wherein the step of bonding further comprises the step of bonding the pre-cured composite hat stiffener to an aircraft wheel well bulkhead pressure web.

6. The method of claim 1 further comprising prior to the step of curing the composite hat stiffener, the step of controlling a variable tool radius and a variable noodle radius, and wherein the step of bonding further comprises bonding the pre-cured composite hat stiffener to an aircraft horizontal pressure deck pressure web.

7. The method of claim 1 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises curing the composite hat stiffener to form the pre-cured composite hat stiffener comprising:
a cap;
a pair of webs extending from opposite ends of the cap,
a pair of flanges; and,
a pair of fillet radii coupling the pair of flanges to the pair of webs, respectively.

8. The method of claim 1 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises forming the composite hat section comprising a plurality of hat section composite plies comprised of a carbon fiber reinforced plastic (CFRP) tape.

9. The method of claim 1 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises forming the composite hat section comprising a plurality of hat section composite plies comprised of a carbon fiber reinforced plastic (CFRP) fabric.

10. The method of claim 1 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises forming the outer ply comprising a glass material.

11. The method of claim 1 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises forming the outer ply comprising a galvanic corrosion protection material and a drill breakout protection material.

12. A method of making a composite hat stiffener, the method comprising the steps of:
curing a composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener, the pre-cured composite hat stiffener comprising:
a composite hat section having a first side and a second side;
a plurality of composite stiffening plies coupled to the composite hat section, the plurality of composite stiffening plies comprising:
a body ply coupled to the first side of the composite hat section;
a wrap ply coupled to the body ply, the wrap ply having a wrap ply slot opening formed in a base portion of the wrap ply; and,
a base ply coupled to the body ply and the wrap ply, the base ply having a base ply slot opening;

a vacant composite hat stiffener slot opening positioned at a base portion of the composite hat stiffener and formed by alignment of the wrap ply slot opening and the base ply slot opening;
a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies; and,
an outer ply coupled to the second side of the composite hat section, the outer ply comprising a glass material and a galvanic corrosion protection material;

bonding the pre-cured composite hat stiffener to a structure surface.

13. The method of claim 12 further comprising prior to the step of curing the composite hat stiffener, the step of coupling a peel ply to the composite hat stiffener, and after the step of curing, the step of removing the peel ply from the composite hat stiffener.

14. The method of claim 12 further comprising prior to the step of curing the composite hat stiffener, the step of chamfering edges of a pair of flanges of the composite hat stiffener.

15. The method of claim 12 wherein the step of bonding further comprises the step of bonding the pre-cured composite hat stiffener to an aircraft wheel well bulkhead pressure web.

16. The method of claim 12 wherein the step of curing the composite hat stiffener to form the pre-cured composite hat stiffener further comprises curing the composite hat stiffener to form the pre-cured composite hat stiffener comprising:
a cap;
a pair of webs extending from opposite ends of the cap,
a pair of flanges; and,
a pair of fillet radii coupling the pair of flanges to the pair of webs, respectively.

17. A method of making a composite hat-stiffened pressure web to reduce effects of a pull-off load and to improve stability of a pressure web, the method comprising the steps of:
adding a composite hat stiffener slot opening to the composite hat stiffener;
curing the composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener, the pre-cured composite hat stiffener comprising:
a composite hat section;
a plurality of composite stiffening plies comprising a body ply, a wrap ply, and a base ply, all coupled to the composite hat section;
a vacant composite hat stiffener slot opening positioned at a base portion of the composite hat stiffener and formed by alignment of a wrap ply slot opening and a base ply slot opening;
a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies; and,
an outer ply coupled to the composite hat section; and,

bonding the pre-cured composite hat stiffener to an uncured composite pressure web to form a composite hat-stiffened pressure web,
wherein the composite hat-stiffened pressure web minimizes a pull-off load at the radius filler noodle and improves stability of a pressure web.

18. The method of claim 17 further comprising prior to the step of curing the composite hat stiffener, the step of coupling a peel ply to the composite hat stiffener, and after the step of curing, the step of removing the peel ply from the composite hat stiffener.

19. The method of claim 17 further compr

Assignees

• Boeing Co

Inventors

• Pearson Steven E
• Whitmer Matthew M
• Dixon Rebecca M
• Firko Jason L
• Marciniak Douglas G
• Cominsky Kenneth D
• Andrews Martin G

Classifications

• B29C70/865

  completely encapsulated · CPC title

• B29C70/545

  Perforating, cutting or machining during or after moulding · CPC title

• B64C1/10

  Bulkheads · CPC title

• Y10T428/24628

  Nonplanar uniform thickness material · CPC title

• B64C2001/0072

  from composite materials · CPC title