Sensors incorporated into semi-rigid structural members to detect physical characteristic changes
A disclosed vehicle component may include at least one split-ring resonator, which may be embedded within a material. The split ring resonator may be formed from a three-dimensional (3D) monolithic carbonaceous growth and may detect an electromagnetic ping emitted from a user device. The split ring resonator may generate an electromagnetic return signal in response to the electromagnetic ping. The electromagnetic return signal may indicate a state of the material in a position proximate to a respective split ring resonator. In some aspects, the split-ring resonator may resonate at a first frequency in response to the electromagnetic ping when the material is in a first state, and may resonate at a second frequency in response to the electromagnetic ping when the material is in a second state. A resonant frequency of the 3D monolithic carbonaceous growth may be based on physical characteristics of the material.
1. A vehicle component, comprising:
at least one split-ring resonator (SRR) embedded within a material of the vehicle component, wherein the at least one SRR is formed from a three-dimensional (3D) monolithic carbonaceous growth;
wherein the at least one SRR is configured to have a resonance frequency shift in response to at least one of a deformation, stress, or strain of the material.
2. The vehicle component of claim 1 , wherein the material is a non-elastomeric material or a semi-rigid material.
3. The vehicle component of claim 1 , wherein the material is a foam-based material.
4. The vehicle component of claim 3 , wherein the foam-based material amplifies the resonance frequency shift.
5. The vehicle component of claim 3 , wherein the foam-based material in combination with the at least one SRR creates an ensemble frequency effect, based on a combination of the resonance frequency shift of the at least one SRR and a frequency response of the foam-based material.
6. The vehicle component of claim 1 , wherein the vehicle component is a land-borne vehicle or an airborne vehicle.
7. The vehicle component of claim 6 , wherein the airborne vehicle is one of: a vertical take-off and landing (VTOL) aircraft, an electric vertical take-off and landing (eVTOL) aircraft, a drone, a passenger drone, a commercial aircraft, a military aircraft, or a rocket.
8. The vehicle component of claim 1 , wherein the resonance frequency shift is at a first frequency in response to an electromagnetic ping when the material is in a first state, and is at a second frequency in response to the electromagnetic ping when the material is in a second state.
9. The vehicle component of claim 1 , wherein the resonant frequency shift is based at least in part on one or more physical characteristics of the material.
10. The vehicle component of claim 1 , wherein a first frequency of the resonance frequency shift indicates a first condition of the material by generating a first electromagnetic return signal in response to an electromagnetic ping, and a second frequency of the resonance frequency shift indicates a second condition of the material by generating a second electromagnetic return signal in response to the electromagnetic ping.
11. The vehicle component of claim 10 , wherein the first frequency is different than the second frequency.
12. The vehicle component of claim 1 , wherein the resonance frequency shift is in response to the deformation of the material.
13. The vehicle component of claim 12 , wherein the at least one SRR is configured to indicate a first state of the deformation of the material by generating a first electromagnetic return signal in response to an electromagnetic ping, and is configured to indicate a second state of the deformation of the material by generating a second electromagnetic return signal in response to the electromagnetic ping.
14. The vehicle component of claim 1 , wherein the at least one SRR includes a resonance portion, wherein the resonance portion is configured to resonate at a first frequency in response to an electromagnetic ping when a state of the material exceeds a threshold, and is configured to resonate at a second frequency in response to the electromagnetic ping when the state of the material is beneath the threshold.
15. The vehicle component of claim 1 , wherein a resonant frequency of 3D monolithic carbonaceous growth is based at least in part on either or both of a permittivity and a permeability of the material.
16. The vehicle component of claim 1 , wherein the at least one SRR includes a plurality of first carbon particles configured to uniquely resonate in response to an electromagnetic ping based at least in part on a concentration level of the first carbon particles within the at least one SRR.
17. The vehicle component of claim 16 , further comprising:
a second SRR configured to be embedded within the material of the vehicle component;
wherein the second SRR includes a plurality of second carbon particles configured to uniquely resonate in response to an electromagnetic ping based at least in part on a concentration level of the second carbon particles within the second SRR.
18. The vehicle component of claim 17 , wherein each of the first carbon particles and second carbon particles is chemically bonded with the material.
19. The vehicle component of claim 17 , wherein the first carbon particles include first aggregates forming a first porous structure, and the second carbon particles include second aggregates forming a second porous structure.
20. The vehicle component of claim 1 , wherein an amplitude of resonance of each of the at least one SRR is indicative of an extent of wear of the material, and each SRR of the at least one SRR has an attenuation point, wherein the attenuation point of each SRR of the at least one SRR is associated with a frequency response to an electromagnetic ping.
21. The vehicle component of claim 1 , wherein the deformation is reversible.