Method of identifying and/or tracking deformation of a turbine engine part

Patent metadata

Field	Value
Publication number	US-10124547-B2
Application number	US-201314431517-A
Country	US
Kind code	B2
Filing date	Sep 26, 2013
Priority date	Sep 28, 2012
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

A method of identifying and/or tracking deformation of a mechanical part made of composite material for a turbine engine, in which the part includes a preform of fiber material and a resin, is provided. The method includes incorporating metal particles in the preform or the resin during fabrication of the part, and subjecting the mechanical part to two X-ray inspections on two different occasions so as to identify the part and/or so as to deduce deformation of its internal structure.

First claim

The invention claimed is:

1. A method of identifying and/or tracking deformation in a mechanical part made of composite material for a turbine engine, the part comprising a preform of fiber material together with resin, the method comprising:
incorporating metal particles in at least one of the preform and the resin while fabricating the mechanical part;
subjecting the mechanical part to a first X-ray inspection so as to obtain first information about positions of the metal particles within the mechanical part;
subjecting the mechanical part to a second X-ray inspection on a later occasion so as to obtain second information about positions of the metal particles within the mechanical part; and
at least one of identifying the part and deducing the deformation of an internal structure of the mechanical part by comparing the first information about the positions of the metal particles within the mechanical part as obtained respectively with the first X-ray inspection and the second information about the positions of the metal particles as obtained with the second X-ray inspection,
wherein the metal particles incorporated in the mechanical part form a three-dimensional pattern within the mechanical part,
wherein the first and second X-ray inspections include X-ray tomography inspections so as to obtain respective first and second three-dimensional measurements of the positions of metal particles within the mechanical part, and
wherein a diameter of the metal particles is less than a resolution of an X-ray tomography device which performs the X-ray tomography inspections and greater than 10% of the resolution of the X-ray tomography device, the material used in the metal particles having a volumetric mass lying in a range of 2 g/cm 3 to 10 g/cm 3 .

2. The method according to claim 1 , wherein the first information is obtained from the mechanical part before any use is made thereof.

3. The method according to claim 1 , wherein at least some of the metal particles are introduced into a flow channel for a stream of resin, a downstream end of the flow channel leading into a mold housing the preform of fiber material.

4. The method according to claim 3 , further comprising controlling a flow rate of the metal particles in the stream of resin.

5. The method according to claim 1 , further comprising depositing at least some of the metal particles on the preform prior to injecting the resin.

6. The method according to claim 5 , wherein the metal particles are deposited on the preform by a screen having a plurality of orifices of different diameters distributed in a predetermined pattern.

7. The method according to claim 1 , further comprising giving one or more predetermined orientations to the metal particles by applying a magnetic field.

8. The method according to claim 1 , wherein the metal particles are of density greater than densities of the preform and of the resin.

9. The method according to claim 1 , wherein the mechanical part is a turbine engine blade or vane.

10. The method according to claim 7 , wherein a magnetic flux is controlled to modify a viscosity and a speed of a stream resin flowing inside a mold housing the preform of fiber material, thereby giving the one or more predetermined orientations to the metal particles.

Assignees

• Safran Aircrafts Engines
• Safran Aircraft Engines

Inventors

• Schneider Julien
• Molliex Ludovic Edmond Camille

Classifications

• B29K2505/00

  Use of metals, their alloys or their compounds, as filler · CPC title

• G01N2223/419

  computed tomograph · CPC title

• B29C70/48

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29C70/88 Primary

  characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced · CPC title

• B29C70/62

  the filler being oriented during moulding (for short fibres B29C70/14) · CPC title