It may be favorable if the shielding element is fastened to the base element via a connecting element, wherein a material of the connecting element, for example a first polymer material, is preferably fused and/or melted on by means of a heating device, for example an infrared heating device, whereby in particular a material bond is formed between the first material of the connecting element and the composite element of the base element and a material bond is formed between the material of the connecting element and the shielding element.

For example, the shielding element is coated with a connecting element and directly back compression molded.

The shielding element can preferably also be detached from the base element again, for example in a recycling process.

In particular, the shielding element is heated, for example on one side from a side facing away from the base element, by means of a heating device until the connecting element becomes low-viscous but the properties of the base element remain substantially unchanged. Subsequently and/or meanwhile, the shielding element is preferably detached from the base element.

In order to detach the shielding element from the base element, the shielding element in a low-viscous state is preferably removed, for example by suction, by means of a suction device, for example a vacuum suction device. In this way, end-of-life recycling can take place.

“Low-viscous” is preferably understood to mean a viscosity η of the corresponding material in the heated state, for example of approximately 145° C. to approximately 150° C., of approximately 0.8 mPa·s to approximately 10 mPa·s.

It may be favorable if a thermoplastic material is applied to the at least one composite element of the base element, for example by injection molding or compression molding.

For example, the base element is trimmed. In this way, an optimized tightness at the edges can be formed.

In accordance with a preferred embodiment, it may be provided that the shielding element comprises a plurality of foils, the plurality of foils being heated together, in particular together with the base element, and that the plurality of foils and in particular the base element are formed as a composite. In this way, the component can be manufactured on-line.

For example, the shielding element is fastened to the base element by one or more of the following techniques:

- riveting; and/or
- gluing; and/or
- stapling; and/or
- joining, for example, toxing and/or crimping.

By means of the techniques mentioned, the component can be produced off-line.

Further preferred features and/or advantages of the invention form the subject-matter of the following description and the drawings illustrating exemplary embodiments.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a schematic perspective view of a battery module which contains an embodiment of a component that contains a base element and a shielding element, the shielding element being formed by a metal foil;

FIG. 2 shows a detail of a schematic sectional view of the component from FIG. 1 through a plane extending parallel to a main extension plane of the component;

FIG. 3 shows a detail of a schematic sectional view of a further embodiment of a component, in which the base element is or comprises a sandwich element, wherein the sandwich element comprises a first layer element, a second layer element and a core element arranged between the first layer element and the second layer element;

FIG. 4 shows a detail of a schematic sectional view of a further embodiment of a component in which the base element comprises a first layer element and a second layer element, which are separated from one another by a separating layer element, wherein the separating layer element comprises or is made of a foil, for example of a polymer material; and

FIG. 5 shows a schematic perspective view of a further embodiment of a component in which the shielding element comprises a plurality of foils.

Identical or functionally identical elements are denoted by the same reference numerals in all figures.

DETAILED DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a component denoted as a whole by 100. The component 100 preferably forms a component of a housing 102 of a battery module 104, for example a battery box. In particular, the component 100 forms a cover element 106 of the battery module 104.

The component 100 preferably comprises a base element 108 which comprises or is made of at least one (in the present case exactly one) composite element 110.

In particular, the component 100 comprises a shielding element 112 for electrical and/or electromagnetic shielding.

The shielding element 112 preferably serves to shield an interior of the battery module 104 from electrical and/or electromagnetic influences, for example from the outside.

In particular, the shielding element 112 improves an electromagnetic compatibility of the component 100 and/or of the battery module 104 as a whole.

Electromagnetic compatibility preferably refers to the ability of a technical device, for example of the housing 102 which contains the component 100, not to disturb other devices by unwanted electrical or electromagnetic effects or not to be disturbed by other devices.

It may be advantageous if the shielding element 112 comprises or is made of one or more foils 114, for example one or more metal foils 115.

The shielding element 112 is connected to the base element 108. For example, the shielding element 112 and the base element 108 are connected to one another in a bonded and/or force-locking and/or positive-locking manner.

The base element 108 preferably forms a carrier element 116 for the shielding element 112.

The base element 108 is preferably planar and/or at least approximately plate-shaped.

It may be favorable if the shielding element 112 is arranged on an outer side of the housing 102 facing away from an interior of the housing 102. The interior of the housing 102 and in particular components contained therein can thus be protected against interference caused by electrical and/or electromagnetic effects.

The battery module 104 is in particular suitable for use in a vehicle (not shown in the drawing), for example an electric vehicle.

In addition or as an alternative to the housing 102 of a battery module 104 being formed partially or completely by a component 100, it may be provided that part of a housing of one or more battery cells of the battery module 104 is formed by a component. For example, the cover element of one or more battery cells is formed by a component 100 (not shown in the drawing).

Additionally or alternatively, it may be provided for an underbody (not shown in the drawings) of the vehicle (a vehicle underbody) to be partially or completely formed by a component 100. For example, the component 100 forms a cladding of a vehicle underbody or a part thereof.

The composite element 110 preferably comprises or is made of a polymer matrix material and a fiber material. The fiber material is preferably an endless fiber material and/or a long fiber material.

An “endless fiber material” is preferably a fiber material in which 90% or more, in particular 95% or more, of the fibers have a length of approximately 40 mm or more, preferably approximately 50 mm or more.

A “long fiber material” is preferably a fiber material in which 90% or more, in particular 95% or more, of the fibers have a length of approximately 1 mm or more and/or of approximately 50 mm or less.

For example, the fiber material comprises glass fibers or is made of glass fibers.

Additionally or alternatively, it may be provided that the fiber material comprises or is made of aramid fibers and/or carbon fibers.

In accordance with the embodiment shown in FIGS. 1 and 2, a homopolymer, for example a polypropylene homopolymer, is, for example, used as the polymer matrix material.

For example, it is also conceivable that a low-weight reinforced thermoplastic (LWRT) is used as the composite element 110.

It may be provided that the composite element 110 is produced from the fiber material pre-impregnated with the polymer matrix material, the fiber material being in particular completely or partially impregnated with polymer matrix material.

It may be favorable if the fiber material contained in the composite element 110 comprises or is made of a woven fabric and/or a non-woven fabric.

A woven fabric is preferably a flat textile structure which preferably consists of at least two thread systems, the warp and the weft. In particular, the at least two thread systems are arranged in a pattern, for example they cross with inclusion of an angle of at least approximately 90°.

In particular when the fiber material contained in the composite element 110 comprises or is made of a non-woven fabric, it may be provided that an angle between two or more thread systems is at least approximately 30° and/or at most approximately 90°, for example at least approximately 30°, at least approximately 45°, at least approximately 60° or at least approximately 90°.

The threads or thread systems preferably comprise or are made of one or more fibers. For example, the threads or thread systems are formed from one or more fiber bundles, for example so-called rovings.

It may be favorable if a proportion of the fibers in the composite element 110 is approximately 70% by weight or more, in particular approximately 80% by weight or more, in relation to a total mass of the composite element 110.

In particular, the proportion of the fibers in the composite element 110 is approximately 95% by weight or less, for example approximately 92% by weight or less, in relation to the total mass of the composite element 110.

In particular for an optimized shielding effect, it may be favorable if the shielding element 112 comprises or is made of aluminum or an aluminum alloy.

The shielding element 112 preferably has an average thickness of approximately 0.02 mm or more, in particular approximately 0.4 mm or more, for example approximately 0.5 mm or more.

In particular, the shielding element 112 has an average thickness of approximately 1.2 mm or less, in particular 1.0 mm or less.

In accordance with a preferred embodiment, it may be provided that the shielding element 112 has an average thickness in a range of approximately 0.02 mm to approximately 0.05 mm.

The thickness is preferably defined along a direction extending at least approximately perpendicularly to a main extension plane of the component 100.

The average thickness preferably refers to an average material thickness of the respective element.

It may be provided that the average thickness of the screening element 112 is selected as a function of an electromagnetic compatibility that is to be achieved. The greater the electromagnetic compatibility required of the component 100, the greater the average thickness of the shielding element 112 will be set and/or selected.

It may be advantageous if the shielding element 112 is fastened to the base element 108 via a connecting element 118 of the component 100. The connecting element 118 is, for example, an adhesive layer and/or bonding layer.

It may be favorable if the connecting element 118 comprises or is made of a first polymer material. Preferably used for the connecting element 118 is a first polymer material which has a melting point which is approximately 10% or more, in particular approximately 20% or more, for example approximately 30% or more, higher than a melting point of a polymer matrix material of the composite element 110.

In accordance with a preferred embodiment, it may be provided that the first polymer material of the connecting element 118 comprises or is made of a thermoplastically processable polymer material. The thermoplastically processable polymer material preferably comprises or is made of a random copolymer, for example a random copolymer polypropylene.

A copolymer is preferably a polymer which consists of two or more different types of monomer units. For example, in a random copolymer, the different types of monomer units are randomly distributed in polymer chains.

It may be advantageous if the first polymer material is a low-melting polymer material. For example, a melting point of the first polymer material is approximately 140° C. or less, for example approximately 135° C. or less.

In particular, the melting point of the first polymer material is approximately 110° C. or more, for example approximately 120° C. or more.

In accordance with a preferred embodiment, a random copolymer is used as the first polymer material and the corresponding homopolymer is used as the polymer matrix material of the composite element 110.

A PP-R polypropylene random copolymer has proven to be particularly suitable as random copolymer. For example, a copolymerizate of propylene and ethylene is used as the first polymer material of the connecting element 118.

In order to produce the component 100, the shielding element 112 is preferably fastened to the base element 108.

In particular, the shielding element 112 is firmly bonded to the base element 108, for example by and/or via the connecting element 118.

A material of the connecting element 118, for example a first polymer material, is preferably fused and/or melted on by means of a heating device. In particular by fusing and/or melting on the material of the connecting element 118, a material bond is formed between the material of the connecting element 118 and the composite element 110 of the base element 108 and a material bond is formed between the material of the connecting element 118 and the shielding element 112.

An infrared heating device, for example an infrared emitter, is used as the heating device, for example.

The shielding element 112 can preferably also be detached again from the base element 108, for example in a recycling process.

In particular, the shielding element 112 is heated by means of the heating device, for example on one side from a side facing away from the base element 108, until the connecting element 118 becomes low-viscous, but the properties of the base element 108 remain essentially unchanged.

After and/or during the heating of the connecting element 118, the shielding element 112 is preferably detached from the base element 108.

In order to detach the shielding element 112 from the base element 108, the shielding element 108 in a low-viscosity state is preferably removed, for example by suction, by means of a suction device, for example a vacuum suction device.

“Low-viscous” is preferably understood to mean a viscosity η of the corresponding element in the heated state, for example of approximately 145° C. to approximately 150° C., of approximately 0.8 mPa·s to approximately 10 mPa·s.

A further embodiment of a component 100 shown in FIG. 3 differs substantially in its structure and function from the embodiment shown in FIGS. 1 and 2 in that the base element 108 comprises a plurality of composite elements 110.

It may be favorable if the base element 108 comprises or is a sandwich element 120. The sandwich material 120 preferably comprises a first layer element 122, a second layer element 124 and a core element 126 arranged between the first layer element 122 and the second layer element 124.

A first composite material 110 in the form of an organic sheet 128 is preferably used as the first layer element 122.

For example, an asymmetrical sandwich element 120 is formed in which materials that are different from one another are used as the first layer element 122 and as the second layer element 124.

In accordance with the embodiment shown, it may be provided that the first composite element 110 is adhesion-promoter-free. For example, only partial impregnation of the fiber material with the polymer matrix material is thus effected. As a result, the first composite element 110 in particular has improved impact properties.

In a particularly preferred adhesion-promoter-free embodiment, the polymer matrix material is preferably a thermoplastic polymer material.

The “adhesion-promoter-free” composite element 110 preferably contains no substances that are provided to produce a close physical and/or chemical bond at an interface of immiscible substances. For example, the first composite element 110 is free of silanes, for example aminosilanes.

For example, the organic sheet 128 is reversibly deformable. The organic sheet 128 can thus be used several times.

As a result of incomplete impregnation of the fiber material, fibers can slip in a load case and not be held in a fixed position. As a result, additional energy can in particular be absorbed, which can be additionally dissipated, for example, by friction effects.

In particular, forces can be reliably conducted from the fibers of the respective fiber material into the polymer matrix material and/or from the polymer matrix material into the fibers.

In contrast, complete impregnation of the fibers typically prevents slipping under load, so that in comparison with structures whose fibers are not completely impregnated, less energy is absorbed and/or the structure tears.

Adhesion-promoter-free composite elements 110 can be produced by the same methods and/or in the same installations as composite elements 110 which contain adhesion promoters. As a result, conversion measures are not needed in the installations in the event of a change of method.

For example, the first composite element 110 has an energy absorption of 100% or more. The energy absorption is determined, for example, in accordance with a puncture test in accordance with DIN EN ISO 6603-2. The adhesion-promoter-free first composite element 110 in the form of an organic sheet 128 preferably cannot be punctured in accordance with the puncture test in accordance with DIN EN ISO 6603-2.

Thermoplastic polymer matrix materials have, in particular, the advantage over thermosetting polymer materials that they have an increased elongation at break compared to other polymer materials.

For example, an energy absorption capacity of the first composite element 110 comprising a thermoplastic polymer matrix material is increased up to a factor of 10 in comparison with the energy absorption capacity of composite elements 110 comprising a thermosetting polymer matrix material.

The energy absorption capacity of the first composite element 110 which is adhesion-promoter-free and comprises a thermoplastic polymer matrix material is preferably greater by a factor of 3 or more and/or 4 or less than the energy absorption capacity of a composite element 110 which comprises an adhesion promoter and comprises a thermoplastic polymer matrix material.

It may be favorable if a thermoplastic material is applied to the at least one composite element 110 of the base element 108, for example by injection molding or compression molding.

For example, the base element 108 is trimmed.

In this way, an optimized tightness at the edges can be formed.

In an assembled state, the first layer element 122 is preferably arranged on a side of the component 100 facing a compressive load. For example, the first layer element 122 is arranged on a side of the sandwich element 120 facing the shielding element 112.

It may be favorable if the second layer element 124 comprises or is made of a second composite element 110. For example, the second composite element 110 is a composite element 110 which comprises endless fibers arranged parallel to one another. In accordance with a preferred embodiment, the second layer element 124 is a unidirectional fiber tape (UD tape).

It may be advantageous if the core element 126 comprises or is made of a third composite element 110. The third composite element 110 is, for example, a direct long-fiber-reinforced thermoplastic material (a so-called “direct long-fiber thermoplastic” (DLFT) material).