Testing device, testing method, and non-transitory storage medium storing testing program
US-2024142495-A1 · May 2, 2024 · US
US2016178352A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016178352-A1 |
| Application number | US-201514974912-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 18, 2015 |
| Priority date | Dec 19, 2014 |
| Publication date | Jun 23, 2016 |
| Grant date | — |
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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.
Opening claim text (preview).
1 . A system for measuring a thickness of ice on a surface, in particular 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; 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 intensity profile and the calculation unit is configured to estimate the thickness of ice as a function of the width 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; 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 intensity profile; and estimating the thickness of ice comprises estimating the thickness of ice as a function of the measured width 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 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.
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