IEEE IUS 2013 - Non-contact Ultrasonic Inspection of CFRP-prepreg for Aeronautical Application...
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Transcript of IEEE IUS 2013 - Non-contact Ultrasonic Inspection of CFRP-prepreg for Aeronautical Application...
M.D. Fariñas, E. Cuevas*, M. García Merino*, T. Gómez Álvarez-Arenas
US-BIOMAT, ITEFI, CSIC, Serrano 144, 28006, Madrid, Spain
*TECNATOM, S.A. Avda. de Montes de Oca 1 28703, San Sebastián de los Reyes, Madrid, Spain
A non-contact ultrasonic technique is proposed for the inspection of carbon fiber reinforced polymer (CFRP) prepreg laminates during lay-up fabrication. A through transmission technique is
proposed using air-coupled transducers to transmit ultrasonic signals through the prepreg laminate and the mold where it is fabricated using normal incidence. The results show the ability of
this technique to determine the degree of compaction of the laminate and the presence of delaminations.
NON-CONTACT ULTRASONIC INSPECTION OF CFRP PREPREGS FOR
AERONAUTICAL APPLICATIONS DURING LAY-UP FABRICATION
Ultrasonic Inspection System. Design Parameters for the
Air-coupled Ultrasounds Technique.
3
-80
-70
-60
-50
-40
Ma
gn
itude
(d
B)
cured
uncured
0.30 0.45 0.60 0.75 0.90
5
10
15
20
25
30
Phase
(ra
d)
Frequency (MHz)
cured
uncured
Transmission coefficient spectra
MATERIAL DENSITY (KG/M3)
RESONANT FREQUENCY (FRES) (KHZ)
ULTRASOUND
VELOCITY (M/S)
ULTRASOUND
ATTENUATION @ FRES (NP/M)
UNCURED CFRP
1580 ± 120 650 ± 80 1370 ± 175 540 ± 80
CURED CFRP
1850 ± 120 685 ± 6 2840 ± 40 20 ± 2
Transmission coefficient spectra of CFRP
Transmission coefficient spectra of CFRP laminated and the Aluminium Mold
thickness = 2 mm thickness = 6 mm
thickness = 13 mm thickness = 13 mm
@ 250 kHz
Compaction Attenuation
(dB/layer)
@ 0.25 MHz
Long 0.3-0.75
Short 2.5-3.0
None 7-10
Pulser/Receiver
• DASEL USB-Ultrascope
Tone burst [1-5] cycles
Up to 400 V
Gain up to 60 dB
• Panametrics P/R 5058 Spike
Up to 900 V
Gain up to 60 dB
Preamplifier = 30 dB
Transducers
• Air-Coupled
• Center frequency =
250 kHz
• Bandwidth = 500 kHz
B
Mechanics
• U-shaped holder
• Automatic and portable
scanning system
D
Mold
• Aluminium
• Thickness = 13 mm
Material
• Several samples
• 300 x 300 mm
• Up to 30 layers
• 3 different compaction: o None
o Short (15-30 min)
o Large (4-8 hours)
• Some with Teflón 10x10
mm insertions at
depths: o 2 layers
o 15 layers
o 28 layers
A
E
-2
-1
0
1
2
No sample
-0.2
-0.1
0.0
0.1
0.2
Am
plit
ude
(V
) 8 layers, long compaction
50 100 150 200 250 300 350
-0.2
-0.1
0.0
0.1
0.2 30 layers, long compaction
Time (s)
CHALLENGES/REQUIREMENTS
Contact with the material is prohibited to prevent any material contamination.
Non contact technique.
Very large Insertion loss: Very large attenuation in the CFRP.
CFRP must be inspected along with the fabrication mold.
BENEFITS o Cost reduction: Repairing or
discarding unsound material
before the autoclave stage
o Possibility to perform 2D scans
C
Experimental Results. Influence of
compaction. Detection of Teflon insertions.
4
0 20 40 60 80 100 120 140 160 180-14
-12
-10
-8
-6
-4
-2
0
Norm
aliz
ed R
eceiv
ed A
mplit
ude (
dB
)
Scan distance (mm)
• A non-contact method for the inspection of CFRP prepreg material during lay-up fabrication has been proposed.
• A detailed experimental study of the properties in uncured laminated prepregs was performed in order to determine velocity and attenuation of ultrasonic
waves in this material.
• A model of ultrasonic propagation through the whole system (laminates and mold) are used to design optimum inspection configuration. The design
variables of this set-up include: transducers center frequency and bandwidth, material to fabricate the mold and thickness of the mold and pulser / receiver
used.
• Finally, the method has been applied for the inspection of several 300 x 300 mm samples with up to 30 layers. Three different compactions and 10 x 10 mm
Teflon insertions at several depths have been used in order to test the technique.
Ultrasonic Properties of CFRP
Laminates. Cured versus Uncured material.
Description of the problem. Objectives and
Requirements.
1 2
Scan