Method and apparatus for dielectric sensors and smart skin for aircraft and space vehicles

• US 7,032,457 B1
• Filed: 09/25/2003
• Issued: 04/25/2006
• Est. Priority Date: 09/27/2002
• Status: Expired due to Fees

• Current Assignee: Nanodynamics, Inc.
• Original Assignee: Nanodynamics, Inc.
• Inventors: Dorfman, Benjamin F.
• Primary Examiner(s): Noori, Max
• Assistant Examiner(s): Ellington, Alandra
• Application Number:
  US10/669,436
• Time in Patent Office: 943 Days
• Field of Search: 73762-769
• US Class Current: 73/762
• CPC Class Codes: B64C 1/12 Construction or attachment of skin panels
• CPC Class Codes: B64C 3/26 Construction, shape, or attachment of separate skins, e.g. panels
• CPC Class Codes: G01L 1/142 using capacitors
• CPC Class Codes: G01M 5/0016 of aircraft wings or blades
• CPC Class Codes: G01M 5/0041 by determining deflection or stress
• CPC Class Codes: G01M 5/0083 by measuring variation of impedance, e.g. resistance, capacitance, induction
• CPC Class Codes: G01M 9/06 Measuring arrangements specially adapted for aerodynamic testing

Abstract

A new family of multifunctional smart coatings based on diamond-like atomic-scale composite materials which can provide a real-time control of the surface stress distribution and potentially dangerous stress diagnostic for the most critical parts of flying vehicles. The coating is a silica-stabilized dielectric film, particularly, a diamond-like atomic-scale composite material.

Claims

1. A stress sensor comprising:

a first electrode;

at least one other electrode; and

a dielectric layer disposed in relation to the first and the at least one other electrode for the electrodes to supply an electric field (E) to the dielectric layer, wherein the dielectric layer comprises a diamond-like carbon film that exhibits a change in conductivity when exposed to an electric field (E) at a level above a critical electric field (E*), wherein the critical electric field (E*) of the diamond-like film shifts under an applied stress, and wherein the critical electric field (E*) comprises about 2×

10⁵ V/cm.

2. A stress sensor comprising:

a first electrode;

at least one other electrode; and

a dielectric layer disposed in relation to the first and the at least one other electrode for the electrodes to supply an electric field (E) to the dielectric layer, wherein the dielectric layer comprises a diamond-like carbon film that exhibits a change in conductivity when exposed to an electric field (E) at a level above a critical electric field (E*), wherein the critical electric field (E*) of the diamond-like film shifts under an applied stress, and wherein compressive forces on the diamond-like carbon film lowers the value of the critical electric field (E*) and wherein tensile forces on the diamond-like carbon film increases the value of the critical electric field (E*).

3. A stress sensor comprising:

a first electrode;

at least one other electrode; and

a dielectric layer disposed in relation to the first and the at least one other electrode for the electrodes to supply an electric field (E) to the dielectric layer, wherein the dielectric layer comprises a diamond-like carbon film that exhibits a change in conductivity when exposed to an electric field (E) at a level above a critical electric field (E*), wherein the critical electric field (E*) of the diamond-like film shifts under an applied stress, and wherein the diamond-like carbon film has a thickness and the electrodes are disposed laterally with respect to each other a distance no greater than the thickness of the diamond-like carbon film.

4. A stress sensor comprising:

a first electrode;

a plurality of other electrodes; and

a dielectric layer disposed in relation to the first and the at least one other electrode for the electrodes to supply an electric field (E) to the dielectric layer, wherein the dielectric layer comprises a diamond-like carbon film that exhibits a change in conductivity when exposed to an electric field (E) at a level above a critical electric field (E*), wherein the critical electric field (E*) of the diamond-like film shifts under an applied stress, and wherein the diamond-like carbon film is deposited onto a surface of a structure being measured for stress as a continuous layer to serve as a sensing layer for the plurality of the other electrodes.

5. A method for determining whether a particular level of stress has been applied to a structure using a stress sensor comprising:

a first electrode;

at least one other electrode; and

a dielectric layer disposed in relation to the first and the at least one other electrode for the electrodes to supply an electric field (E) to the dielectric layer, wherein the dielectric layer comprises a diamond-like carbon film that exhibits a change in conductivity when exposed to an electric field (E) at a level above a critical electric field (E*), wherein the critical electric field (E*) of the diamond-like film shifts under an applied stress,

the method comprising;

applying an electric field (E) with the first electrode and the at least one other electrode to the dielectric layer;

monitoring the conductivity of the dielectric layer; and

determining whether the particular level of stress has been applied to the structure based on a change in the conductivity of the dielectric layer.

6. The method of claim 5, comprising determining whether the particular level of stress has been applied based on a shift in the critical electric field (E*) of the dielectric layer resulting from the applied stress.

7. The method of claim 6, comprising applying an electric field (E) at a level less than the critical electric field (E*) and determining whether a particular compressive stress has been applied to the structure based on a change in the conductivity of the dielectric layer which results from a shift in the critical electric field (E*) of the dielectric layer as a result of the compressive stress.

8. The method of claim 7, comprising determining whether a particular compressive stress has been applied to the structure based on a change in conductivity of the dielectric layer which results from a shift in the critical electric field (E*) of the dielectric layer to that less than the electric field (E) applied.

9. The method of claim 6, comprising applying an electric field (E) at a level greater than the critical electric field (E*) and determining whether a particular tensile stress has been applied to the structure based on a change in the conductivity of the dielectric layer which results from a shift in the critical electric field (E*) of the dielectric layer as a result of the tensile stress.

10. The method of claim 9, comprising determining whether a particular tensile stress has been applied to the structure based on a change in conductivity of the dielectric layer which results from a shift in the critical electric field (E*) of the dielectric layer to that greater than the electric field (E) applied.