IP Library Granted Patent US 8,096,092
Granted Patent B2
US 8,096,092 · App. 11/810,549 · Granted Jan 17, 2012

Lightweight structural panel

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,096,092
App. No.
11/810,549
Granted
Jan 17, 2012
Kind
B2
Abstract

What is described is a lightweight structural panel which comprises a planarly extended outer skin of given thickness and stiffening elements which are connected to this outer skin and are arranged at a given distance from one another. According to the invention, the outer skin is formed by component layers which are each extended in the planar direction of the lightweight structural panel and complement one another in the direction of thickness to form the thickness of the outer skin and are interconnected, the stiffening elements being formed in one piece with one of the component layers.

Claims (25)

1. A lightweight structural panel which comprises:

a planarly extended outer skin of predetermined thickness, the outer skin being formed by a plurality of component layers which are each extended in a planar direction of the lightweight structural panel and complement one another in a direction of thickness to form the thickness of the outer skin and are interconnected,

wherein the plurality of component layers comprises an inner component layer that is made of a plurality of planar elements, at least two of the plurality of planar elements being positioned adjacent to one another;

wherein each of the plurality of planar elements comprises two component elements arranged on one side of the respective planar elements;

wherein the component elements of adjacent planar elements form a plurality of stiffening elements, the plurality of stiffening elements being connected to the outer skin and arranged at a predetermined distance from one another, the plurality of stiffening elements being formed in one piece or integrally with the inner component layer;

wherein at least one of the plurality of stiffening elements comprises a web region arranged substantially perpendicularly to the planar direction of the outer skin and extending in a longitudinal direction along the outer skin, the web region being formed in one piece with the planar elements of the inner component layer;

wherein at least one of the plurality of stiffening elements comprises a flange region extending substantially parallel to the planar direction of the outer skin, the flange region being formed in one piece or integrally with the web region; and

wherein at least one of the plurality of stiffening elements has an inverted J-shaped cross section or box-shaped cross section, of which a vertical leg forms the web region and another leg forms the flange region.

2. The lightweight structural panel according to claim 1 , wherein the outer skin is formed by a first component layer and a second component layer.

3. The lightweight structural panel according to claim 1 , wherein the plurality of planar elements are joined together in the planar direction.

4. The lightweight structural panel according to claim 3 , wherein the planar elements of the inner component layer each include one or more of the stiffening elements.

5. The lightweight structural panel according to claim 1 ,

wherein the stiffening elements are interconnected, and

wherein the plurality of component elements forming the stiffening elements each have a same-direction inverted J-shaped cross section and are tailored to one another such that they lie flat against one another and complement one another to form the stiffening element with an inverted J shaped cross section.

6. A lightweight structural panel comprising:

a planarly extending outer skin of a predetermined thickness, the outer skin being formed by component layers comprising an inner component layer and a metal alloy, the component layers each extending in a planar direction of the lightweight structural panel and complement one another in the direction of thickness to form a thickness of the outer skin and are interconnected;

wherein the inner component layer comprises a plurality of planar elements, at least two of the plurality of planar elements being positioned adjacent to one another;

wherein and each of the plurality of planar elements comprises two component elements arranged on one side of the respective planar elements; and

wherein the component elements of adjacent planar elements form a plurality of stiffening elements, the plurality of stiffening elements being connected to the outer skin and being arranged at a predetermined distance from one another, the plurality of stiffening elements being formed in one piece or integrally with the inner component layer;

wherein at least one of the plurality of stiffening elements comprises a web region arranged substantially perpendicularly to the planar direction of the outer skin and extending in a longitudinal direction along the outer skin, the web region being formed in one piece with the planar elements of the inner component layer;

wherein at least one of the plurality of stiffening elements comprises a flange region extending substantially parallel to the planar direction of the outer skin, the flange region being formed in one piece or integrally with the web region; and

wherein at least one of the plurality of stiffening elements has an inverted J-shaped cross section or box-shaped cross section, of which a vertical leg forms the web region and another leg forms the flange region.

7. The lightweight structural panel according to claim 6 , wherein the planar elements join together in the planar direction.

8. The lightweight structural panel according to claim 1 , wherein the component layers comprise a metal alloy.

9. The lightweight structural panel according to claim 1 , wherein the component layers comprise a fiber composite material.

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