IP Library Granted Patent US 7,814,729
Granted Patent B2
US 7,814,729 · App. 11/766,177 · Granted Oct 19, 2010

Stiff panel having composite stiffeners with reduced shock sensitivity

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Quick Facts
Patent No.
US 7,814,729
App. No.
11/766,177
Granted
Oct 19, 2010
Kind
B2
Abstract

A stiff panel ( 1 ) comprises a skin ( 2 ) and at least one stiffener ( 3 ) of composite material on said skin. Free surface ( 311 ) of web ( 31 ) of stiffener ( 3 ) on the stiff panel according to the invention comprises a deformable core ( 33 ) and a covering ( 34 ) which covers core ( 33 ) and joins said core with structural part ( 35 ) of web ( 31 ). The width of core ( 33 ) is equal to or greater than the width of structural part ( 35 ) of web ( 31 ) of stiffener ( 3 ), depending on the shock energy against which panel ( 1 ) must be protected.

Claims (18)

1. A structural panel for a vehicle comprising:

a panel;

a plurality of stiffeners, each of said plurality of stiffeners constructed of a reinforcing material embedded in a matrix, said plurality of stiffeners mounted on the panel, each of the stiffeners comprising:

a web forming a structural part and extending outward from the panel, said web having a free surface on an apex of a distal end;

a core covering the free surface, said core constructed of a deformable, shock absorbing material; and

a cover, separate from the web, enclosing the core and fastened to a lateral surface of the web.

2. The structural panel of claim 1 wherein the core has a width substantially equal to or greater than the thickness of the web, and extends totally or partially over the length of a distal edge of the free surface.

3. The structural panel of claim 1 wherein the plurality of stiffeners are each constructed with a flange at an attachment end of the web, said flange providing an extended surface for securing each stiffener to the panel, and further wherein the web extends outward from the flange.

4. The structural panel according to claim 1 wherein the distal end of the web and a surface of the core have a complimentary form.

5. The structural panel according to claim 1 wherein the core has a cross-section of semicircular shape.

6. The structural panel according to claim 1 wherein the deformable material is resilient to absorb shock.

7. The structural panel according to claim 1 wherein the deformable material is a rigid or semi-rigid foam.

8. The structural panel according to claim 1 wherein the deformable material is an elastomer having at least one cavity.

9. The structural panel according to claim 1 wherein the core has a cross-section having a circular or polygonal shape.

10. The structural panel according to claim 1 wherein the core has a cross-section having a teardrop shape.

11. The structural panel according to claim 1 wherein the core has a flat surface approximately parallel to the plane of the panel.

12. The structural panel according to claim 1 wherein the cover is a metal material.

13. The structural panel according to claim 1 wherein the cover is a composite material.

Assignments (2)
MERGER Recorded May 18, 2011
From: AIRBUS FRANCE
To: AIRBUS OPERATIONS SAS
Reel/Frame 026298/0269 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 27, 2007
From: MATHIEU, NORMAND; LACOMBE, JEAN-CLAUDE
To: AIRBUS FRANCE
Reel/Frame 019887/0806 →