Device for fixing a lightweight panel on a support

A technology for fixing devices and boards, which can be used in aircraft flooring, sheet connection, transportation and packaging, etc., and can solve problems such as damage to the mechanical properties of boards

Inactive Publication Date: 2010-09-29
AIRBUS OPERATIONS (SAS)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

So when the plate is assembled on the support, a large part of the bolt shank is unconstrained and causes stress on the insert 7
The stresses exerted on the insert 7 may weaken the core of the sandwich structure, which may lead to severe damage to the mechanical properties of the panels

Method used

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  • Device for fixing a lightweight panel on a support
  • Device for fixing a lightweight panel on a support
  • Device for fixing a lightweight panel on a support

Examples

Experimental program
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Embodiment Construction

[0023] figure 2 Shown is a floor panel body for a passenger transportation vehicle according to an embodiment of the present invention. The floor panel 10 comprises a central sandwich structure comprising at least two walls 11 , 12 respectively located on opposite outer surfaces of a honeycomb core 13 .

[0024] These walls 11, 12 are some fibrous skeletons. Fibers can be selected in the group given by way of non-limitation: carbon fibers, graphite fibers, glass fibers, silica fibers, silicon carbide fibers, or have the required Any other fiber that is defined in relation to light weight.

[0025] The honeycomb core 13 is formed of, for example, aramide. Aramid fibers actually have low flammability, great fracture resistance and high modulus of elasticity.

[0026] A floor covering 14 , for example a carpet, is located on the floor panel 10 . The covering 14 serves to protect the floor panel 10 against movement-related erosion or other erosion associated with occupying th...

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PUM

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Abstract

The invention concerns a device for fixing a lightweight panel on a support. Said device comprises an insert (18) including at least one flange (20), said insert being designed to receive a bolt-type fixing member (16). The invention is characterized in that said flange (20) has an outer surface comprising tooth elements (23) and the device comprises a part made of ductile material (24) includingan opening for passing through the fixing member (16). The tooth elements (23) are designed to co-operate, when the panel is being fixed on the support, with the ductile part (24) to enable said panel to be fixed without deforming it.

Description

technical field [0001] The invention relates to a fastening device for fastening lightweight panels, such as sandwich panels, to supports. Another object of the invention is a passenger transport, such as an aircraft, comprising such a fastening device. Background technique [0002] Sandwich structures of composite materials have some properties, especially mechanical properties, especially for the smallest mass. These structures are therefore used extensively in the aviation industry (doors, floors, wing leading edges, ailerons, inner bulkheads, etc.). [0003] Fig. 1 schematically shows a partial sectional view of a prior art cabin floor. The floor panel is composed of a floor panel body 1 of sandwich structure. Each panel 1 comprises at least two walls 2 , 3 situated respectively on opposite outer surfaces of a honeycomb core 4 . These plate bodies 1 have a small thickness, generally about 10mm, and said plate bodies 1 are fixed on the side flanges 5, 6 of the seat in...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16B5/01
CPCF16B5/01B64C2001/0072B64C1/06Y02T50/43Y02T50/433B64C1/12B64C2001/0081B64C1/18Y02T50/40
Inventor D·奇普里安
Owner AIRBUS OPERATIONS (SAS)
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