IP Library Granted Patent US 6,890,470
Granted Patent B2
US 6,890,470 · App. 10/385,288 · Granted May 10, 2005

Method for producing a fiber composite structural component

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Quick Facts
Patent No.
US 6,890,470
App. No.
10/385,288
Granted
May 10, 2005
Kind
B2
Abstract

A fiber composite structural component such as a fitting, bracket, mounting or the like is produced by applying fiber material such as fiber threads or fiber yarns in an automatic circular weaving operation to a core that has at least two sections, to form a fiber material body ( 6 ). One core section is removed from the fiber material body when the weaving is completed. The body is then deformed in a mold that has the contour of the finished structural component with at least one mold core section still in the fiber material body. The deformed configuration of the structural component is then impregnated in an RTM device with a resin and hardener followed by curing. Reinforcements may be inserted or secured to the fiber material body prior to the impregnated and curing step.

Claims (23)

1. A method for manufacturing a fiber composite structural component having a given contour by using fiber composite construction features, said method comprising the following steps:

a) using a mold core ( 1 ) having at least two separable core sections ( 2 , 3 ) which together have a mold core contour closely resembling said given contour of said fiber composite structural component,

b) performing an automatic circular weaving operation, thereby applying a fiber material ( 5 ) around said mold core ( 1 ) to form a fiber material body ( 6 ),

c) removing one of said separable core sections ( 3 ) out of said fiber material body ( 6 ) to provide an empty portion of said fiber material body,

d) shaping said fiber material body ( 6 ) including said empty portion with the other separable core section ( 2 ) still in said fiber material body ( 6 ), into said given contour to form a semi-finished product ( 7 ),

e) impregnating said semi-finished product with a resin matrix material and curing said impregnated semi-finished product to produce said fiber composite structural component, and

f) removing the other core section ( 2 ) from said structural component.

2. The method of claim 1 , wherein said impregnating and curing is performed in an RTM device.

3. The method of claim 1 , further comprising performing said shaping step (d) so that said empty portion is shaped into mounting flanges ( 8 ).

4. The method of claim 1 , further comprising the following steps:

a) stopping said automatic circular weaving operation when a predetermined number of plies has been applied to said mold core ( 1 ), and

b) securing at least one separately produced reinforcing member to said fiber material body ( 6 ) prior to said impregnating and curing step.

5. The method of claim 4 , further comprising using as said at least one reinforcing member a prefabricated fiber material layer or fiber material fabric.

6. The method of claim 3 , further comprising performing said shaping step (d) prior to said impregnating and curing step, by folding and pressing said empty portion of said fiber material body ( 6 ) against fixed surfaces of a jig or mold ( 17 ) to form said mounting flanges ( 8 ) on said fiber material body ( 6 ).

7. The method of claim 5 , further comprising dimensioning said fiber material layer or fiber material fabric to protrude partially from said fiber material body ( 6 ) and, prior to said impregnating and curing step, folding a partially protruding portion ( 15 , 15 A) of said fiber material layer or fiber material fabric against said fiber material body ( 6 ) to provide at least one reinforced connector surface area.

8. The method of claim 5 , comprising folding said partially protruding portion ( 15 , 15 A) against at least one end face of said fiber material body ( 6 ).

9. The method of claim 5 , comprising folding said partially protruding portion against at least one side wall of said fiber material body ( 6 ).

10. The method of claim 1 , further comprising performing, following said curing, an after treatment.

11. The method of claim 1 , further comprising the following steps:

a) temporarily stopping said automatic circular weaving operation when a given number of plies has been applied to said mold core,

b) attaching or placing at least one separately produced reinforcing member to said fiber material body ( 6 ), and

c) continuing said automatic circular weaving operation for securing said at least one reinforcing member in said fiber material body ( 6 ).

12. The method of claim 11 , further comprising using as said reinforcing member separately woven fiber fabric.

Assignments (1)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →