IP Library Granted Patent US 7,963,483
Granted Patent B2
US 7,963,483 · App. 11/981,432 · Granted Jun 21, 2011

Stiffening element carbon-glass layered foot section

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Quick Facts
Patent No.
US 7,963,483
App. No.
11/981,432
Granted
Jun 21, 2011
Kind
B2
Abstract

The present invention provides a stiffening element for stiffening a step-like substructure, in particular in an aircraft or spacecraft, having a foot section which is composed of a fiber composite material and is shaped in the form of a step such that it essentially fills the substructure. A method is also provided for production of a stiffening element for stiffening of a step-like substructure in an aircraft or spacecraft, according to which a profile part with a foot section which is composed of a carbon-fiber-reinforced plastic is provided, at least one layer of a glass-fiber-reinforced plastic is laminated onto the foot section, and the glass-fiber-reinforced plastic is milled corresponding to a step-like shape which essentially fills the substructure.

Claims (11)

1. A stiffening element for stiffening a step-like substructure in an aircraft or spacecraft, the stiffening element having a foot section which comprises:

a carbon-fiber-reinforced plastic material;

a shape in the form of a step such that it essentially fills the adjacent portion of the substructure; and

at least one layer of machined glass-fiber-reinforced plastic material bonded on top of the carbon-fiber-reinforced plastic material and configured on that surface of the foot section which matches the shape of the substructure.

2. The stiffening element according to claim 1 , further comprising a boundary surface between the carbon-fiber-reinforced plastic and the at least one layer of glass-fiber-reinforced plastic, wherein the carbon-fiber-reinforced plastic comprises carbon fibers running parallel to the boundary surface, and the at least one layer of glass-fiber-reinforced plastic comprises glass fibers running parallel to the boundary surface.

3. The stiffening element according to claim 2 , wherein the carbon fibers and the glass fibers run parallel to the boundary surface and to each other.

4. The stiffening element according to claim 1 , wherein the at least one layer of glass-fiber-reinforced plastic has a step-like change in thickness along the foot section.

5. The stiffening element according to claim 4 , wherein some of the glass fibers in the at least one layer of the glass-fiber-reinforced plastic are cut off adjacent to the step-like change.

6. The stiffening element according to claim 1 , wherein the at least one layer of the glass-fiber-reinforced plastic has a maximum thickness of 1 mm to 20 mm along the foot section.

7. The stiffening element according to claim 6 , wherein the minimum thickness along the foot section is between 0.1 mm and 0.2 mm.

8. The stiffening element according to claim 1 , wherein the at least one layer of the glass-fiber-reinforced plastic has a minimum thickness of at least 0.1 mm along the foot section.

Assignments (3)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →
CHANGE OF NAME Recorded May 9, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026243/0153 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 27, 2008
From: ROMING, THORSTEN; SCHROEER, THORSTEN
To: AIRBUS DEUTSCHLAND GMBH
Reel/Frame 020594/0731 →