IP Library Granted Patent US 10,024,822
Granted Patent B2
US 10,024,822 · App. 14/652,593 · Granted Jul 17, 2018

Method for characterising a part made of a composite material

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Quick Facts
Patent No.
US 10,024,822
App. No.
14/652,593
Granted
Jul 17, 2018
Kind
B2
Abstract

The invention consists in a method of characterizing a part made of composite material ( 30 ), the method comprising a step of determining a characteristic of a longitudinal ultrasound wave ( 41 ) traveling along a path within the part ( 30 ), and being characterized in that the travel time of a longitudinal ultrasound wave ( 42 ) transmitted by the part ( 30 ) is measured (E 4 ).

Claims (64)

1. A method of characterizing a part made of composite material, the method comprising a step of determining a characteristic of a longitudinal ultrasound wave traveling along a path within the part, and being characterized in that a travel time of a longitudinal ultrasound wave transmitted by the part is measured, and the travel time of the transmitted wave is measured by observing the beginning of the transmitted wave, wherein a propagation time of an ultrasound wave transmitted through a liquid in the absence of the part is measured, and the propagation times of ultrasound waves reflected respectively by a first face of the part and by a second face of the part are measured with a first transducer facing the first face and a second transducer facing the second face of the part in order to determine a dimension of the part traveled by the longitudinal ultrasound wave traveling along the path within the part, wherein an amplitude of the transmitted wave is also measured in order to determine an overall or unit length attenuation to which the longitudinal ultrasound wave is subjected on traveling within the part, wherein an overall attenuation (α 2 ) of the longitudinal ultrasound wave in the part is determined according to the following equation:

α

2

=

1

x

2

(

Ln

(

Y

1

Y

2

·

t

12

t

21

)

+

α

1

x

2

)

where Y 1 /Y 2 is an amplitude ratio, t 12 is an amplitude transmission coefficient from the liquid to the composite material, t 21 is an amplitude transmission coefficient from the composite material to the liquid, α 1 is a value of an attenuation of the transmitted wave in the liquid, and x 2 is the dimension of the part traveled by the transmitted wave traveling along the path within the part.

2. A method according to claim 1 , wherein a propagation speed of the longitudinal ultrasound wave in the part following the path within the part is determined.

3. A characterization method according to claim 1 , performed for a part made of 3D woven composite material.

4. A method according to claim 1 , wherein x 2 is determined according to the equation:

x 2 =( t X1+X2+X3 −t X3 −t X1 )× V liquid

where V liquid is a propagation speed of the wave in the liquid, t X1+X2+X3 is the propagation time of the ultrasound wave transmitted through the liquid in the absence of the part, t X1 is the propagation time of the ultrasound wave reflected by the first face of the part, and t X3 is the propagation time of the ultrasound wave reflected by the second face of the part.

5. A method according to claim 1 , wherein t 12 t 21 is determined according to the equation:

t

12

t

21

=

4

Z

1

Z

2

(

Z

1

+

Z

2

)

2

where Z 1 is an acoustic impedance of the liquid, and Z 2 is an acoustic impedance of the composite material.

6. A method according to claim 5 , wherein the acoustic impedance of the liquid, Z 1 , and the acoustic impedance of the composite material, Z 2 , are calculated according to equations:

Z 1 =ρ 1 ×V 1

Z 2 =ρ 2 ×V 2

where ρ 1 is a density of the liquid, ρ 2 is a density of the composite material, and V 1 is a propagation speed of the transmitted wave within the liquid, and V 2 is a propagation speed of the transmitted wave within the composite material.

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 Jun 17, 2015
From: CHATELLIER, JEAN-YVES FRANÇOIS ROGER; BROUSSAIS-COLELLA, NICOLAS; DUVAL, JÉRÉMY; MARQUIS, JÉRÉMY; MEYER, ANNE
To: SNECMA
Reel/Frame 035934/0549 →