![]() ·Table of Contents ·Methods and Instrumentation | Comparative Analysis of the Ways to Increase Signal to Noise Ratio at NDT Inspection of Austenitic WeldsV.Grebennikov, V.Badalyan, D.Grebennikov, A.VopilkineScientific and production centrer "ECHO+", 1, Kurchatov sq., Moscow, 123182, Russia, Tel: +7-095-196-91-91; Fax: +7-095-935-73-90; E-mail : echo.ndt@ g23.relcom.ru Contact |
Testing Device.
Fig 1:The defect models in the defect free austenitic weld (the sample1) |
Test Specimens.
The studies were performed on austenitic weld samples made of 12H18N10T stainless steel, 40 and 55 mm thickness. The welding was executed automatically under flux using the wire SV-04H19N11M3. All welds had V- and X-shape. Two of them were apriory defect free with following fabrication in them models of defects (Fig.1). The defect models were shaped as notches and side drilled holes. The other samples had specially embedded real defects (Fig.2, 3). The types of the real defects were lack of fusion, lack of fusion located at weld boundary, slag inclusions.
Fig 2: The sample 2, three lacks of fusion.
|
Fig 3: The sample 3, two slag inclusions and three lacks of fusion on boundary of the weld
|
Testing Methods.
The ultrasonic holography testing was executed through automatic transverse scanning (axis of priority scanning was perpendicular to the weld axis). The aperture of transverse scanning (across the weld) was 70-100 mm, step - 0,3 mm. The step of longitudinal movement (along the weld) was 5 mm. The testing was performed: by shear wave - direct and reflected beam and by longitudinal wave - direct beam only. The scanning wasn't executed on the surface of the weld reinforcement.
Probes
The angle beam longitudinal and shear probes with frequencies 1.65 ; 2.5 MHz and beam incidence angles 45o, 50o, 55o, 60o, 65o were used. The used probes are marked by the following way: l - longitudinal wave; s - shear wave; 2 - frequency 1.65 MHz; 3 - frequency 2.5 MHz; h-one half directivity diagram angle -12o-20o; (d)- one half of directional diagram angle -10o-15o; two next numeral are incidence angle of probe.
Methods of Signal/Noise Increase.
To increase signal/structure noise ratio by holographic testing, two-frequency and two-mode methods were used in the work.
Two-frequency and two-mode methods were realized through combination of images that corresponds to the two frequencies (1.65 and 2.5 MHz) or the two wave modes (longitudinal and shear, both 2.5 MHz) using the following algorithm:
|
|
Fig 4: Dependence of signal/noise ratio on traversed path in austenitic weld metal. Longitudinal waves. Straight beam.
|
Fig 5: Dependence of signal/noise ratio on traversed path in austenitic weld metal
|
Fig 6: Dependence of signal/noise ratio on notch height in austenitic weld. Longitudinal waves (l2(3)-60). Straight beam.
|
Fig 7: Dependence of signal/noise ratio on notch height in austenitic weld. Shear waves (s2(3)-60). Straight beam.
|
Fig 8: Dependence of signal/noise ratio on notch height in austenitic weld of 55mm thickness.Straight beam.
|
Fig 9: Dependence of signal/noise ratio on notch height in austenitic weld of 40mm thickness. Shear waves (s2(3)-60). Reflected beam.
|
Fig 10: The non-holographic image (A - scan visualization) of defect models (see Fig. 1). Longitudinal waves, f=2,5MHz, a=60º. There are the crosscuts of the weld (B - to the left, D -to the right).
|
Fig 11: Holographic image of notches in austenitic weld (Fig. 1). There are the crosscut (B - to the left) and the plan of the weld (C -to the right). Longitudinal waves, f =2,5MHz a=60º. Satellite images occur due to the wave transformation.
|
Fig 12: Holography image of notches in austenitic weld. The crosscut (B - to the left) and the plan (C - to the right) of the weld. Shear waves, S3-60, f=2,5MHz a=60º.
|
Fig 13: Holography image of notches in austenitic weld (Fig.1). Two-frequency method (1.65MHz+2.5MHz), shear waves,a=60º. The images of the side drilled hole of Æ3 mm (z=20mm) are to the right side. Æ3mm.
|
Fig 14: Holographic image of notches and side drilled hole (z=20mm)in austenitic weld (see Fig. 1). Two-frequency method (1.65MHz+2.5MHz), longitudinal wave,a=60º.
|
Fig 15: Holographic image of notches and side drilled hole (z=20mm) in austenitic weld (see Fig. 1). Two-mode method, longitudinal +shear waves,a=60º.
|
Fig 16: Holographic image of two lack of fusion in the 40mm thickness austenitic weld ( 50mm and 15mm length , Fig.2). Two-mode method, a=60º.
|
Fig 17: Holography image of two lack of fusion on the boundary of the austenitic weld (50mm and 10mm length, Fig.3). Two-mode method, a=60º.
|
| © AIPnD , created by NDT.net | |Home| |Top| |