IP Library Granted Patent US 10,914,690
Granted Patent B2
US 10,914,690 · App. 15/106,154 · Granted Feb 9, 2021

Method for characterising a part

Inventors: Julien Schneider (Moissy-Crayamel, FR); Francois Hild (Chatenay Malabry, FR); Hugo Leclerc (Cachan, FR); Stephane Roux (Rosny Sous Bois, FR)
Assignees: SAFRAN AIRCRAFT ENGINES; CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE; ECOLE NORMALE SUPERIEURE DE CACHAN
G01N23/046G06K9/00624G06T7/001G01N2223/1016G01N2223/419G01N2223/425G01N2223/426G01N2223/615G01N2223/63G01N2223/645G06T2207/10081G06T2207/30164
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Quick Facts
Patent No.
US 10,914,690
App. No.
15/106,154
Granted
Feb 9, 2021
Kind
B2
Abstract

A method of characterizing a part including obtaining an X-ray tomography image of the part and then a step of correlating the image with a reference wherein the correlation step includes searching among a predefined set of X-ray tomography image transformations for a transformation that minimizes the difference between the image and the reference in order to characterize the inside of the part.

Claims (24)

1. A method of characterizing a part, the method comprising a step of obtaining an X-ray tomography image of the part and then a correlation step of correlating said image of the part with a reference comprising an image of a standard part differing from the part, wherein the correlation step comprises applying each of a predefined set of X-ray tomography image transformations to the image of the part to produce transformed images, determining respective differences between the transformed images and the reference, and searching among the predefined set of X-ray tomography image transformations for a transformation that minimizes a difference between the image of the part and the reference in order to characterize an inside of said part and determine a topological difference between the image of the part and the reference to find defects in the part.

2. A method according to claim 1 for characterizing a part, using a continuous parameterization of said set of transformations.

3. A method according to claim 1 for characterizing a part, wherein said set of transformations includes at least one set of continuous displacements, at least one set of alterations of brightness and of contrast, or at least one set of scale changes.

4. A method according to claim 1 , for characterizing a part, further comprising determining whether the part is acceptable by using an extracted transformation.

5. A method according to claim 1 , for characterizing a part, wherein said set of transformations comprises at least transformations corresponding to modifications of at least one parameter of a model of the part.

6. A method according to claim 1 , for characterizing a part, wherein the reference comprises a virtual part constructed from a computer assisted design model.

7. A method according to claim 1 , for characterizing a part, including modifying a parameterization of a computer assisted design model of the part by using a transformation identified at the end of the search.

8. A method according to claim 1 , for characterizing a part, wherein said set of transformations comprises at least a class of transformations that conserve topology.

9. A method according to claim 1 , for characterizing a part, wherein the reference comprises an explicit representation of boundaries of an element of the part.

10. A method according to claim 1 , for characterizing a part, including segmenting the image of the part by using a transformation identified at the end of the search.

11. A method according to claim 1 , for characterizing a part, wherein the reference comprises a representation of an elementary pattern.

12. A method according to claim 1 , for characterizing a part, comprising identifying at least one of strands, fibers and elementary patterns in the image of the part.

13. A method according to claim 1 , for characterizing a part, wherein the part is a composite material part.

14. A method according to claim 1 , for characterizing a part, wherein the part is an aircraft turbojet blade.

15. A method according to claim 1 , comprising:

identifying a specific component within the image of the part;

situating the specific component from a reference image in the image of the part; and

using the set of transformations to deform the specific component in the reference image to match the image of the part.

16. The method according to claim 1 , wherein:

the set of transformations comprises a plurality of transformations; and

the searching comprises:

reconstructing an image using each transformation of the set of transformations to generate the set of transformed images, and

finding a difference between the reference and each of the transformed images.

17. The method according to claim 1 , wherein the set of transformations comprises a plurality of transformations.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 13, 2020
From: SCHNEIDER, JULIEN; HILD, FRANCOIS; LECLERC, HUGO; ROUX, STEPHANE
To: SAFRAN AIRCRAFT ENGINES; CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE; ECOLE NORMALE SUPERIEURE DE CACHAN
Reel/Frame 054357/0282 →
CHANGE OF NAME Recorded Oct 7, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 047087/0545 →
Priority Claims (1)
FR 13 63095 · Dec 19, 2013 · national
Continuity (1)
Related Publication 20180195978A1 · Jul 12, 2018
Cited By (1)
US 12,442,634