Sensors incorporated into airborne vehicle components to detect physical characteristic changes

Patent metadata

Field	Value
Publication number	US-12196636-B2
Application number	US-202217940256-A
Country	US
Kind code	B2
Filing date	Sep 8, 2022
Priority date	Mar 27, 2019
Publication date	Jan 14, 2025
Grant date	Jan 14, 2025

Abstract

A disclosed airborne vehicle includes split-ring resonators (split ring resonators), which may be embedded within a material. Each 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. Each 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, each 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.

First claim

What is claimed is:

1. An airborne vehicle component comprising:
at least one meso-scale or micro-scale resonator embedded within a material that comprises at least a portion of the airborne vehicle component,
wherein the at least one meso-scale or micro-scale resonator is formed from a three-dimensional (3D) monolithic carbonaceous growth and wherein the at least one meso-scale or micro-scale resonator is configured to respond to an electromagnetic stimulus emitted from an antenna; and
wherein the at least one meso-scale or micro-scale resonator, in combination with the material of the airborne vehicle component that is at a position proximate to the at least one meso-scale or micro-scale resonator, modulates the electromagnetic stimulus to form an electromagnetic return signal that indicates a state of the material at the position proximate to the at least one meso-scale or micro-scale resonator.

2. The airborne vehicle component of claim 1 , 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.

3. The airborne vehicle component of claim 1 , wherein the at least one meso-scale or micro-scale resonator is used to locate a position of the airborne vehicle with respect to a landing pad.

4. The airborne vehicle component of claim 1 , wherein at least three resonators of the at least one meso-scale or micro-scale resonator are used to triangulate a position of the airborne vehicle component.

5. The airborne vehicle component of claim 1 , wherein the material is found on at least one of: a propeller blade, a body material, landing gear, a cockpit interface, or a structural component.

6. The airborne vehicle component of claim 1 , wherein the state of the material indicates at least one of surface flexion, propeller flexion, or landing gear flexion.

7. The airborne vehicle component of claim 1 , wherein the state of the material is correlated to indicate at least one of pressure, location, temperature, or elevation.

8. The airborne vehicle component of claim 1 , wherein the at least one meso-scale or micro-scale resonator is configured to resonate at a first frequency in response to the electromagnetic stimulus when the material is in a first state, and is configured to resonate at a second frequency in response to the electromagnetic stimulus when the material is in a second state.

9. The airborne vehicle component of claim 1 , wherein a tuned resonant frequency of the 3D monolithic carbonaceous growth is based at least in part on one or more physical characteristics of the material.

10. The airborne vehicle component of claim 1 , wherein the at least one meso-scale or micro-scale resonator is configured to indicate a first condition of the material by generating a first electromagnetic return signal in response to the electromagnetic stimulus, and is configured to indicate a second condition of the material by generating a second electromagnetic return signal in response to the electromagnetic stimulus.

11. The airborne vehicle component of claim 10 , wherein the first electromagnetic return signal has a first frequency, and the second electromagnetic return signal has a second frequency different than the first frequency.

12. The airborne vehicle component of claim 1 , wherein the state of the material includes a deformation of the material.

13. The airborne vehicle component of claim 12 , wherein the at least one meso-scale or micro-scale resonator is configured to indicate the deformation of the material by generating a first electromagnetic return signal in response to the electromagnetic stimulus, and is configured to indicate a lack of deformation of the material by generating a second electromagnetic return signal in response to the electromagnetic stimulus.

14. The airborne 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.

15. The airborne vehicle component of claim 1 , wherein the at least one meso-scale or micro-scale resonator further comprises a first resonator including a plurality of first carbon particles configured to uniquely resonate in response to the electromagnetic stimulus based at least in part on a concentration level of the first carbon particles within the first resonator.

16. The airborne vehicle component of claim 15 , wherein the at least one meso-scale or micro-scale resonator further comprises a second resonator including a plurality of second carbon particles configured to uniquely resonate in response to the electromagnetic stimulus based at least in part on a concentration level of the second carbon particles within the second resonator.

17. The airborne vehicle component of claim 16 , wherein at least one of:
each of the first carbon particles and second carbon particles is chemically bonded with the material;
the first carbon particles include first aggregates forming a first porous structure; or
the second carbon particles include second aggregates forming a second porous structure.

18. The airborne vehicle component of claim 16 , wherein an amplitude of resonance of at least one of the first resonator or the second resonator is indicative of an extent of wear of the material.

19. The airborne vehicle component of claim 16 , wherein at least one of:
the first resonator is configured to resonate at a first frequency in response to the electromagnetic stimulus, and the second resonator is configured to resonate at a second frequency in response to the electromagnetic stimulus;
the first frequency is different than the second frequency;
an extent of shift of a natural resonance frequency in response to the electromagnetic stimulus of the first resonator and the second resonator is indicative of an amount of deformation of the material;
each of the first resonator and the second resonator has an attenuation point; or
the attenuation point of each the first resonator and the second resonator is associated with a frequency response to the electromagnetic stimulus.

20. A landing pad comprising:
at least one meso-scale or micro-scale resonator configured to be embedded within a material that comprises at least a portion of the landing pad,
wherein the at least one meso-scale or micro-scale resonator is formed from a three-dimensional (3D) monolithic carbonaceous growth and wherein the at least one meso-scale or micro-scale resonator is configured to respond to an electromagnetic stimulus emitted from an antenna; and
wherein the at least one meso-scale or micro-scale resonator, in combination with the material of the landing pad and its environment, modulates the electromagnetic stimulus to form an electromagnetic return signal that indicates at least one environmental condition at the position proximate to the at least one meso-scale or micro-scale resonator.

Assignees

• Lyten Inc

Inventors

• Stowell Michael
• Cook Daniel
• Montalvo Carlos

Classifications

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• B60C2019/004

  Tyre sensors other than for detecting tyre pressure · CPC title

• B60C23/064

  comprising tyre mounted deformation sensors, e.g. to determine road contact area · CPC title

• B60C11/24

  Wear-indicating arrangements · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title