Fiber composite component having an integrated structural health sensor arrangement
A fiber composite component includes an integrated structural health sensor arrangement, wherein the component includes a plurality of layers of fibers embedded in a matrix material, wherein the layers include at least two strain sensing fibers arranged parallel and at a distance to each other, wherein the strain sensing fibers are lithiated carbon fibers having piezoelectric characteristics.
1. A fiber composite component having an integrated structural health sensor arrangement,
the component comprising a plurality of layers of fibers embedded in a matrix material,
wherein the plurality of layers comprises at least two strain sensing fibers arranged parallel and at a distance to each other,
wherein the at least two strain sensing fibers are lithiated carbon fibers, and
wherein the component comprises an electrical connecting device accessible from an outer delimiting surface or an outer edge of the component, wherein the electrical connecting device is connected to the strain sensing fibers.
2. The fiber composite component according to claim 1 , wherein the at least two strain sensing fibers comprise at least two strain sensing fiber strands, each comprising a plurality of strain sensing fibers extending along the same direction.
3. The fiber composite component according to claim 1 , further comprising at least one reference layer that is capable of being lithiated, and at least one electrically insulating layer, permeable for Lithium ions and arranged between the at least one reference layer and all strain sensing fibers.
4. The fiber composite component according to claim 1 , wherein the at least two strain sensing fibers extend over at least a half of a surface extension of the component.
5. The fiber composite component according to claim 1 , wherein the plurality of layers comprises several layers of fibers arranged on top of each other, wherein at least two of the several layers each comprise at least one strain sensing fiber, wherein at least one group of strain sensing fibers is created with all strain sensing fibers of the at least one group extending in the same direction.
6. The fiber composite component according to claim 5 , wherein at least two layers each comprise at least one group of strain sensing fibers.
7. The fiber composite component according to claim 1 , wherein the plurality of layers comprises several layers of fibers arranged on top of each other, wherein at least two strain sensing fibers are arranged in different layers and extend along the same direction.
8. The fiber composite component according to claim 1 ,
wherein the plurality of layers comprises several layers of fibers arranged on top of each other,
wherein two groups of strain sensing fibers are arranged in at least one of the layers,
wherein the strain sensing fibers of each group extend along the same direction, and
wherein the strain sensing fibers of a first group and of a second group enclose an angle of at least 45°.
9. The fiber composite component according to claim 1 , wherein the electrical connection device comprises two independent electrical connection devices arranged at diametrically opposed ends of the component.
10. The fiber composite component according to claim 1 , wherein the strain sensing fibers comprise an electrically insulating coating.
11. The fiber composite component according to claim 1 , wherein the component is a carbon fiber reinforced component.
12. A component system with integrated structural health monitoring, comprising:
at least one fiber composite component according to claim 1 , and
at least one evaluation unit connected to the electrical connection device of the at least fiber composite component,
wherein the evaluation unit is configured to receive measurement parameters from a plurality of strain sensing fibers and to compare the parameters of at least two of the strain sensing fibers arranged in the at least one fiber composite component, extending in the same direction and provided in different layers and to generate a warning signal if a difference of the parameters is outside a predetermined tolerance.
13. The component system according to claim 12 , further comprising a power source selectively connectable to the electrical connection device and an at least one reference layer that is capable of being lithiated for selectively transferring Lithium ions from the at least one reference layer to the strain sensing fibers.
14. An aircraft, comprising at least one component system according to claim 12 .