IP Library Granted Patent US 9,964,525
Granted Patent B2
US 9,964,525 · App. 14/654,528 · Granted May 8, 2018

Automatic calibration method for checking by ultrasound a composite material structure during production

Inventors: Stéphane Auffray (Saint Lyphard, FR); Hubert Voillaume (Issy les Moulineaux, FR)
Assignee: Airbus SAS
G01N29/30G01N29/11G01N29/4436G01N2291/0231G01N2291/106
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Quick Facts
Patent No.
US 9,964,525
App. No.
14/654,528
Granted
May 8, 2018
Kind
B2
Abstract

A monitoring system comprising ultrasound sensors to monitor the structure of a composite material part during production is automatically calibrated using reference sensors mounted on reference blocks and placed in the production environment of the part. The automatic calibration comprises actuating a reference sensor to transmit an ultrasonic wave and measuring the amplitude of a reference echo constituted by the transmitted ultrasonic wave after it has passed through the reference block. The measured amplitude is compared to a set point value and the gain is applied to the reference sensor to obtain an amplitude value of the reference echo substantially equal to the set point value. The gain applied to the reference sensor is applied to the ultrasound sensors of the same type as the reference sensor. The operation is performed for each reference sensor, and successively for all of the stages of production of the part.

Claims (19)

1. A device for automatically calibrating an array of ultrasonic measurement sensors for monitoring a structure of a composite material part during its production, comprising:

an array of ultrasonic reference sensors placed in proximity to the composite material part and in an environment same as the composite material part, each ultrasonic reference sensor being mounted on a calibration block and configured to be actuated to perform an amplitude measurement of a reference echo constituted by an ultrasonic wave transmitted by said each ultrasonic reference sensor that passed through the calibration block on which said each ultrasonic reference sensor is mounted, the array of ultrasonic reference sensors comprising at least one ultrasonic reference sensor for each type of the ultrasonic measurement sensors used to monitor the structure of the composite material part;

a signal generator to actuate said each ultrasonic reference sensor at predetermined times during a production process of the composite material part; and

a controller to measure an amplitude of the reference echo received by said each ultrasonic reference sensor, to determine a value of a gain control to be applied to said each ultrasonic reference sensor to maintain the amplitude of the reference echo at a predetermined set point value, and to apply a second gain control to each ultrasonic measurement sensor, a value of the second gain control is a function of the value of the gain control determined for one of the array of ultrasonic reference sensors being of the same type as said each ultrasonic measurement sensor.

2. The device according to claim 1 , wherein the calibration blocks are made of silicon carbide or steel.

3. The device according to claim 1 , wherein each ultrasonic reference sensor is mounted on a separate calibration block.

4. The device according to claim 1 , wherein the calibration block is made of a material from which a variation of an attenuation of the ultrasonic waves, passing through the calibration block, as a function of temperature and pressure is known.

5. A device for automatically calibrating an array of ultrasonic measurement sensors for monitoring a structure of a composite material part during its production, comprising:

an array of ultrasonic reference sensors placed in proximity to the composite material part and in an environment same as the composite material part, each ultrasonic reference sensor being mounted on a calibration block and configured to be actuated to perform an amplitude measurement of a reference echo constituted by an ultrasonic wave transmitted by said each ultrasonic reference sensor that passed through the calibration block on which said each ultrasonic reference sensor is mounted, the array of ultrasonic reference sensors comprising at least one ultrasonic reference sensor for each type of the ultrasonic measurement sensors used to monitor the structure of the composite material part;

a signal generator to actuate said each ultrasonic reference sensor at predetermined times during a production process of the composite material part; and

a controller to measure an amplitude of the reference echo received by said each ultrasonic reference sensor, to determine a value of a gain control to be applied to said each ultrasonic reference sensor to maintain the amplitude of the reference echo at a predetermined set point value, and to apply a second gain control to each ultrasonic measurement sensor, a value of the second gain control is substantially equal to the value of the gain control determined for one of the array of ultrasonic reference sensors being of the same type as said each ultrasonic measurement sensor.

6. The device according to claim 5 , wherein the calibration block is made of a material from which a variation of an attenuation of the ultrasonic waves, passing through said calibration block, as a function of temperature and pressure is known.

7. The device according to claim 5 , wherein the calibration blocks are made of silicon carbide or steel.

8. The device according to claim 5 , wherein each ultrasonic reference sensor is mounted on a separate calibration block.

9. A method for automatically calibrating an array of ultrasonic measurement sensors for monitoring a structure of a composite material part during its production, comprising the steps of:

(a) applying an excitation signal to an reference sensor of an array of reference sensors to transmit an ultrasonic wave through a reference block on which said reference sensor is mounted and measuring an amplitude of a reference echo received by said reference sensor, the array of reference sensors being placed in proximity to the composite material in an environment same as the composite material part, and comprising at least one reference sensor for each type of the ultrasonic measurement sensors used to monitor the structure of the composite material part;

(b) determining a value of the gain control to be applied to said reference sensor to obtain a reference signal with an amplitude value substantially equal to a set point value;

(c) assigning the gain control determined for said reference sensor to the array of ultrasonic measurement sensors of a same type as said reference sensor;

(d) repeating the steps (a)-(c) for each reference sensor of the array of reference sensors at least once for each cycle of a process for producing the composite material part.

Assignments (4)
MERGER AND CHANGE OF NAME Recorded Feb 12, 2018
From: AIRBUS GROUP SAS; AIRBUS SAS
To: AIRBUS SAS
Reel/Frame 045788/0801 →
MERGER Recorded Jan 14, 2018
From: AIRBUS GROUP SAS
To: AIRBUS
Reel/Frame 044615/0737 →
CHANGE OF NAME Recorded Sep 28, 2015
From: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
To: AIRBUS GROUP SAS
Reel/Frame 036664/0021 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 23, 2015
From: AUFFRAY, STÉPHANE; VOILLAUME, HUBERT
To: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
Reel/Frame 036639/0059 →
Priority Claims (1)
FR 12 62545 · Dec 21, 2012 · national
Continuity (1)
Related Publication 20160041130A1 · Feb 11, 2016