Sandwich material

Details Sandwich material Sandwich material

2001-10-31

2004-07-20

Jones, Deborah (Department: 1775)

Stock material or miscellaneous articles

All metal or with adjacent metals

Having metal particles

C428S568000, C428S608000, C428S075000, C428S086000, C428S297400, C228S057000, C181S284000

Reexamination Certificate

active

06764772

ABSTRACT:

FIELD OF THE INVENTION
The present invention relates to a sandwich material, which is particularly useful in vehicle construction.
BACKGROUND TO THE INVENTION
It is well-recognised that sandwich structures, which are composed of stiff outer layers separated by a low density core, offer the potential for very high specific stiffness and other attractive mechanical properties. Such materials are generally rigid and strong, but are of relatively low mass. They are therefore particularly useful as construction materials or packaging materials, for example.
WO-A-9801295 discloses a sandwich material comprising metal plates separated by metal fibres arranged perpendicularly to the plates, and which are affixed thereto by an adhesive. The sandwich material is made by coating at least one of the metal plates with an adhesive, and then subjecting short metal fibres to an electrical charge. This causes the fibres to stand upright and propels them into the adhesive on one of the metal plates, where they become anchored. This process is commonly known as “flocking”.
A disadvantage of this type of sandwich material is, however, its rather complex, and therefore costly, method of manufacture. Furthermore, due to its relatively high electrical resistance, this type of sandwich material is not easy to weld. Ease of weldability is of course an essential property of materials for use in construction.
Therefore, there is a need for a sandwich material which is not only straightforward and therefore relatively cheap to manufacture, but which also has a relatively low electrical resistance and is therefore easy to weld.
SUMMARY OF THE INVENTION
According to a first aspect of the present invention, a sandwich material comprises two metal plates which are affixed to and separated by a fibrous core, and is characterised in that the core comprises a three-dimensional porous network comprising metal fibres, wherein substantially all of the fibres are inclined at an acute angle (&thgr;) to the plates.
The sandwich material may be prepared by simply affixing the fibrous core between two metal plates, for instance though the use of an adhesive or by brazing technology.
The sandwich material according to the present invention is more straightforward and therefore cheaper to manufacture than the materials known in the art. In addition, the sandwich material has a comparatively lower electrical resistance (because of the good contact between fibres and face-plates), rendering it easily weldable. It also exhibits improved beam stiffness and interfacial shear strength, at relatively low areal density, in comparison with the prior art materials. Such properties are particularly desirable for materials to be used in construction, for instance of vehicles including aircraft. The sandwich material according to the present invention may also display high acoustic and vibrational damping capacity, and efficient thermal insulation.
According to further aspects of the present invention, sandwich materials of the type described above may be used as vehicle parts, or in a variety of welded structures or components.
DESCRIPTION OF THE INVENTION
In order for the sandwich material according to the present invention to be suitable for use in aircraft or vehicle construction, it should be lightweight and relatively thin. Suitable total thicknesses of the sandwich material are of the order 0.5 mm-1 cm, preferably 0.5-5 mm and more preferably 0.5-3 mm.
The metal plates may be made from a variety of different metals, examples of which include stainless steel, steel, aluminium and titanium. Preferably, however, the metal plates will be made from stainless steel or aluminium.
The thicknesses of the metal plates should be such that they are not susceptible to tearing. Suitable thicknesses of the metal places lie in the range 100-600 &mgr;m, and more preferably in the range 150-300 &mgr;m.
The core of the sandwich material comprises a three-dimensional porous network of fibres which are preferably bonded together at crossover points within the network, for instance by the action of heat. The fibres may be arranged in a regular mesh, or be randomly arranged throughout the network. Preferably, the fibres are randomly orientated so that the core properties are isotropic.
The fibres are arranged within the core so that they form an angle to the plane of the core, and therefore the metal plates. The fibres may be arranged in regular arrays, in which case the angle formed by each fibre will be similar to the next, or randomly orientated to form different angles to the plane of the core. Substantially all of the fibres are inclined at an acute angle (&thgr;) to the plane of the core, and in the context of this Application by “substantially all” we mean at least 80%, and preferably at least 90% by volume of the fibres. The angle, or angles, at which the fibres are inclined to the metal plates is preferably substantially less than 90°, for instance less than 60°, and more preferably lies in the range 10-55°. Most preferably the angle lies in the range 20-50°, with the interlaminar shear stiffness and shear strength being optimised when the fibre angle approaches 45°.
The core has a relatively open structure, with the fibres in the core generally occupying 5-50%, and preferably 5-10%, of the core volume. The sizes of the pores within the network typically lie in the range 50-200 &mgr;m, and are preferably 75-125 &mgr;m, eg. about 100 &mgr;m.
The thickness of the core typically lies in the range 300-3000 &mgr;m, and preferably in the range 500-2000 &mgr;m.
The metal fibres may comprise a variety of different metals, examples of which include stainless steel, steel, aluminium and titanium. Preferably, the core will comprises stainless steel or aluminium fibres. In addition, the metal fibres may be made from the same or different metal as the plates, but are preferably the same metal.
Typically, the fibres will have lengths of less than 5000 &mgr;m, and preferably 100-3000 &mgr;m. The average diameter of fibres suitable for use in the present invention is typically less than 500 &mgr;m, for example 10-400 &mgr;m. Preferably, the average fibre diameter will lie in the range 60-350 &mgr;m, and will more preferably be in the range 100-300 &mgr;m. In the context of this Application, by “average diameter” we mean the mean fibre diameter as calculated from the sum of the individual diameters of a plurality of fibres divided by the number of fibres.
As a generality the sandwich material should be stiff but flexible, but need only be stiff enough to maintain the separation of the plates and to prevent excessive shearing between the plates when they are subjected to a bending moment, for example during manufacture or use. A minimum in-plane shear modulus of about 1 GPa would be sufficient to achieve suitable rigidity of the core.
The stiffness of the core is dependent on a number of factors including the fibre diameter, the fibre volume fraction and the degree of bonding of the fibres within the network. In general, the coarser the fibres, the greater the stiffness of the core. However, the use of fibres with very large diameters may lead to difficulties in the manufacture, handling and subsequent incorporation of the core into the sandwich materials.
A suitable, commercially available core is manufactured by Bekaert, a Belgian company, under the trade name BEKIPOR®.
One way in which the core may be prepared is by forming a slurry of the fibres in a liquid, eg. water, allowing the fibres to settle, and then removing the liquid from the resulting accumulated fibres by pressing and/or heating, for example. The resulting product may then be subjected to heat and optionally pressure, under slightly reducing conditions in order to avoid oxidation, to bond the fibres together.
The core may also comprise non-metallic fibres. The choice of non-metallic fibres suitable for use is likely to depend on the intended application of the sandwich material. For example, if the sandwich material is to be used in vehicle or aircraft construction, the non-metallic fibres

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