IP Library Granted Patent US 10,393,720
Granted Patent B2
US 10,393,720 · App. 14/357,900 · Granted Aug 27, 2019

System and method for dynamically locating a fault observed on a component

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Quick Facts
Patent No.
US 10,393,720
App. No.
14/357,900
Granted
Aug 27, 2019
Kind
B2
Abstract

A method and system for dynamic locating of a fault observed in a defective component related to a forging operation, in which: a processor models a shaping operation of a component by forging, as per a set of successive models of the component; a processor adds a fault plotter to a first model of the set of models, in a zone corresponding to a region of the fault in the defective component to obtain a first plotted model; and a processor tracks the plotter in time from the first plotted model during the modelling to locate an origin of the fault.

Claims (21)

1. A system for dynamic diagnosis of a fault observed in a component obtained after a forging operation of a blank, the system comprising:

a processor configured to:

model the forging operation by modelling working of the component during the forging operation as a function of forging parameters, the modeling leading to a set of time successive models of forming of the component during the forging operation, the set comprising an initial model corresponding to the blank, intermediate models corresponding to intermediate forging operations, and a final model corresponding to the forged component,

input data relating to a fault observed in the component, the component having a fault being a defective component,

add a fault plotter to a first model belonging to the set of models, in a zone corresponding to a region of the fault in the defective component, to obtain a first plotted model representing the defective component at a time of detection of the fault, and

track the fault plotter over time during the modelling starting from the first plotted model, retrospectively or prospectively, to diagnose dynamics of the fault.

2. The system according to claim 1 , wherein dimensions and positioning of the zone associated with the fault plotter in the first plotted model are substantially similar to dimensions and positioning of the region of the fault in the defective component.

3. The system according to claim 1 , wherein the modelling of the forging operation is dynamic modelling with finite elements forming a polygon mesh at each iteration representing the component at the corresponding forging operations.

4. The system according to claim 3 , wherein the processor is configured to define at each iteration dimensions and position of the fault plotter as a function of elementary elements of the polygon mesh at the operation in time.

5. The system according to claim 3 , wherein the fault plotter is a contrast element associated with the polygon mesh.

6. The system according to claim 1 , wherein the first model corresponds to the final model and the first plotted model corresponds to a final plotted model, and the processor is configured to track in time the fault plotter by reversing a sequence of the modelling starting from the final plotted model.

7. The system according to claim 6 , wherein the processor is configured to locate the fault plotter in the initial model to identify the region in which the fault would have been in the component before forging.

8. The system according to claim 6 , wherein the processor is configured to locate the fault plotter in the intermediate models comprising particular configurations to verify whether the particular configurations are likely to cause the fault.

9. The system according to claim 1 , wherein the first model corresponds to the initial model and the first plotted model corresponds to an initial plotted model, and the processor is configured to locate the fault plotter in the final model to verify whether the fault in the forged component lies outside a machining region of the forged component.

10. The system according to claim 1 , wherein the processor is configured to determine whether the fault is isolated or reproducible on a series of components to perform corrective action to avoid the reproduction of the fault.

11. The system according to claim 1 , wherein the processor is configured to locate an origin of the fault.

12. A method for dynamic diagnosis of a fault observed in a component obtained after a forging operation of a blank, the method comprising:

modelling, using a processor, the forging operation by modelling working of the component during the forging operation as a function of forging parameters, the modelling leading to a set of time successive models of the forming of the component during the forging operation, the set comprising an initial model corresponding to the blank, intermediate models corresponding to intermediate forging operations, and a final model corresponding to the forged component;

obtaining data relating to a fault observed in the component, the component having a fault being a defective component;

adding a fault plotter to a first model belonging to the set of models using the processor, in a zone corresponding to a region of the fault in the defective component to obtain a first plotted model representing the defective component at a time of detection of the fault; and

tracking the fault plotter in time during the modelling starting from the first plotted model, retrospectively or prospectively, to diagnose dynamics of the fault.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 13, 2014
From: LEBLANC, JONATHAN
To: SNECMA
Reel/Frame 032880/0170 →