Method and system for measuring the thickness of ice on a surface, notably of an aircraft, using a luminous pattern generated by diffusion in the ice

Patent metadata

Field	Value
Publication number	US-9568305-B2
Application number	US-201514974912-A
Country	US
Kind code	B2
Filing date	Dec 18, 2015
Priority date	Dec 19, 2014
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

Abstract

A system and method for providing an estimate of the thickness of the ice regardless of the shape of its surface at the level of the air/ice interface. To this end the system and method measure an intensity profile of a luminous pattern generated by diffusion in the ice, which enables the system to measure the thickness of the ice even when the air/ice surface is not plane.

First claim

The invention claimed is:

1. A system for measuring a thickness of ice on a surface of an aircraft, the system comprising:
a light source configured to project a collimated beam onto the surface to generate a luminous pattern by diffusion in the ice;
an imaging device configured to acquire an image of the ice including the luminous pattern;
a measuring unit configured to measure on the image a luminous intensity profile of the luminous pattern, wherein the luminous intensity profile comprises a curve representing intensity of the luminous pattern as a function of a distance from a point of penetration of the collimated beam into the ice, and wherein the light source is oriented with respect to the surface so that the luminous intensity profile has a summit at the point of penetration; and
a calculation unit configured to estimate the thickness of ice present on the surface as a function of the luminous intensity profile,
wherein the measuring unit is configured to measure a width of the summit of the intensity profile and the calculation unit is configured to estimate the thickness of ice as a function of the width of the summit of the intensity profile and from at least one predetermined table.

2. The system as claimed in claim 1 , wherein the light source has a wavelength between 200 nanometers and 1 micrometer inclusive.

3. The system as claimed in claim 1 , wherein the light source comprises:
a laser;
a pulsed light source;
a light source emitting radiation outside the visible band; or
a light source emitting radiation at a plurality of wavelengths.

4. The system as claimed in claim 1 , wherein the imaging device is configured for double image acquisition.

5. The system as claimed in claim 1 , wherein the imaging device is a high dynamic range imaging device.

6. A method of measuring a thickness of ice on a surface, in particular of an aircraft, the method comprising:
projecting a collimated light beam onto the surface in to generate a luminous pattern by diffusion in the ice;
acquiring an image of the ice including the luminous pattern;
measuring on the image a luminous intensity profile of the luminous pattern, wherein the luminous intensity profile comprises a curve representing intensity of the luminous pattern as a function of a distance from a point of penetration of the collimated beam into the ice, and wherein the light source is oriented with respect to the surface so that the luminous intensity profile has a summit at the point of penetration; and
estimating the thickness of ice present on the surface as a function of the luminous intensity profile and from at least one predetermined table,

wherein:
measuring the intensity profile comprises measuring a width of the summit of the intensity profile; and
estimating the thickness of ice comprises estimating the thickness of ice as a function of the measured width of the summit of the intensity profile and from at least one predetermined table.

7. The method as claimed in claim 6 , wherein the intensity profile is measured perpendicularly to the luminous pattern.

8. The method as claimed in claim 7 , wherein the method comprises:
measuring a width of the intensity profile; and
estimating the thickness of ice as a function of the width of the intensity profile and from the predetermined table.

9. The method as claimed in claim 8 , comprising measuring the width at half the height of the summit of the intensity profile.

10. The method as claimed in claim 9 , wherein the method comprises:
acquiring a first sub-image of the ice when the light source is operating and a second sub-image of the ice when the light source is turned off;
forming the image by superimposing the first and second sub-images.

11. The system as claimed in claim 1 , wherein the wherein the light source is oriented with respect to the surface so that the luminous intensity profile reduces monotonically from the summit at the point of penetration.

12. The system as claimed in claim 1 , wherein the luminous pattern comprises a line extending in an extension direction, and wherein the intensity profile of the luminous pattern is obtained for a section perpendicular to the extension direction.

13. The system as claimed in claim 1 , wherein the calculation unit is configured to estimate the thickness of ice from at least two predetermined tables established as a function of a type of ice, wherein the two predetermined tables comprise a first table for opaque ice and a second table for transparent ice.

14. The system as claimed in claim 1 , wherein the at least one predetermined table is established using an ice-free width of an ice-free intensity profile for the surface.

15. The system as claimed in claim 1 , wherein the position and orientation of the light source is configured to avoid a phenomenon of specular reflection.

Assignees

• Airbus Operations Sas
• Airbus Defence & Space Gmbh

Inventors

• Weber Marc Marcel
• Olchewsky François Antoine
• Entz Ricardo Maiko Uehoka

Classifications

• G01B11/0691 Primary

  of objects while moving (G01B11/0616 takes precedence) · CPC title

• G01B11/0625 Primary

  with measurement of absorption or reflection · CPC title

• B64D15/20

  Means for detecting icing or initiating de-icing · CPC title

• G06T11/60

  Creating or editing images; Combining images with text · CPC title

• H04N23/741

  by increasing the dynamic range of the image compared to the dynamic range of the electronic image sensors · CPC title