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Innovative Materials Testing Technologies, Inc. Building Calibration Standard for Remote Field Eddy Current Technique Detecting Deeply Hidden Corrosion in Aircraft Structures Yushi Sun Innovative Materials Testing Technologies, Inc. 2501 N.


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Building Calibration Standard for Remote Field Eddy Current Technique Detecting Deeply Hidden Corrosion in Aircraft Structures

Innovative Materials Testing Technologies, Inc.

Yushi Sun Innovative Materials Testing Technologies, Inc. 2501 N. Loop Drive, Suite 1610, Ames IA, 50010

  • Tel. 515-296-5328 Fax. 515-296-9910 Email. Suny@iastate.edu

Zhongqing You & XXXX Magnetic Analysis Corporation 535 S. 4th Avenue, Mt. Vernon, NY 10550-4499

  • Tel. 800-463-8622
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Innovative Materials Testing Technologies, Inc.

Outline

  • Introduction
  • Distinguishing Features of RFEC Technique
  • Building Calibration Standards for RFEC Technique
  • Exploiting Fundamental Features of RFEC Technique
  • Location (Remaining Thickness) to Signal Phase Angle Relation
  • Corrosion Depth to Signal Magnitude Relation
  • Corrosion Depth to Signal Y Relation
  • Estimation of Corrosion Shapes
  • Correction Factor in Estimating Small-Sized Corrosion
  • Summary and Future Work
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Introduction

  • 1. Early detection of hidden corrosion in aircraft

becomes big public, manufacturer and government concern for economy and safety.

  • 2. Currently deeply hidden corrosion remains

undetectable unless aircraft components are disassembled that is costly and time consuming.

  • 3. A number of new techniques are currently under
  • development. The Remote Field Eddy Current

Technique is among the tops.

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RFEC Phenomenon in Metallic Tubes

Direct energy coupling path Indirect energy coupling path

ΦRF

Excitation coil Pick-up coil

Φ

Indirect energy coupling path

Phenomenon: Signals received by pick-up coils are sensitive to changes in wall thickness, conductivity, and permeability.

.

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SLIDE 5

Underlying Physics:

  • 1. Direct energy coupling is restricted by EC in the

wall.

  • 2. Pick-up coil signal, ΦRF, is dominated by the energy

diffusing along the indirect coupling path that traverses the wall twice.

  • 3. Changes in the phase of ΦRF are directly

proportional to the thickness of the wall.

RFEC Phenomenon in Metallic Tubes

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RFEC Phenomenon in Metallic Tubes

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Typical RFEC signals: double-peak signal Time Signals Real Component, X Imaginary Component, Y

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  • 2. RFEC Phenomenon In Flat Geometries

RFEC Probe Drive Coil Pickup Coil Direct Coupling Path Indirect Coupling Path

  • 1. In the absence of a test part, only direct coupling from the

drive coil is detected, i.e., No RFEC signal is present

  • 2. The RFEC probe is designed to minimize signal from direct

coupling and focuses on the indirect coupling path

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Distinguishing Features of RFEC Technique & SSEC System Compared to Commercial ECT:

  • Higher sensitivity: capable of detecting SCC.
  • Deep penetration: capable of detecting deeply hidden

corrosion & cracks.

  • Simple to use: similar to a conventional ECT system.
  • Lower power requirement Current drive power is ~ 0.4 [Ampere-

Volt]

  • Capable of accommodating alternative, non-coil, types of

magnetic sensors

  • Capable of driving multi-phase traveling/rotating

magnetic wave probes.

Innovative Materials Testing Technologies, Inc.

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Examples from Two RFEC Probes

RF-4 mm V.3

Footprint: 0.85” x 2.15”

RF-2 mm V.3

Footprint: 0.3” x 0.62”

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RF4mm V. 3 – Three Typical Examples

In Detecting Deeply Hidden Corrosion

It detects (in multi-layer Aluminum Structures) :

  • Φ 0.75” Spherical Metal Loss with Maximum Depth of

0.025” that is 0.600” below Surface. ~ 4.2% thinning.

  • 0.5”×0.5”×0.040” chemical thinning 0.603” below surface

(CNDE Specimen). ~ 6.6% thinning.

  • 0.5”×0.5”×0.006” chemical thinning 0.373” below surface

(CNDE Specimen). ~ 1.6% thinning.

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0.125” 0.500” 0.125”

RFEC Probe Rf4mm

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Φ 0.75” Φ 0.75”

  • Max. Depth = 0.075”
  • Max. Depth = 0.025”

Example 1: 3 Layer 7075 T6 Specimen, 0.125” + 0.5” + 0.125” Total Thickness = 0.750” Spherical-Shaped Corrosion on Bottom of 2th Layer Location = 0.600” Location = 0.575” #1 #2

Location Location

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Innovative Materials Testing Technologies, Inc.

Example 1.1 Φ 0.75” Spherical-Shaped Corrosion Max. Depth = 0.025” On 2nd Layer Bottom Side, f=200Hz Total Thickness = 0.750”, Remaining Thickness = 0.600”

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Example 1.2 Φ 0.75” Spherical-Shaped Corrosion Max. Depth = 0.075” On 2nd Layer Bottom Side, f=200Hz Total Thickness = 0.750”, Location = 0.575”

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Example 2.1: 5 Layer 2024 T3 Specimen 0.1” + 0.1” + 0.19” +0.19” + 0.063” Total Thickness = 0.643” Corrosion on Bottom of 5th Layer Location = 0.603”

0.100” 0.100” 0.063” 0.190” 0.190”

0.040” deep corrosion A Scan Direction

RFEC Probe Rf4mm Location = 0.603”

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Corrosion Sample #15

CNDE Specimen #15 (0.063” thick) 3.0” × 3.0” × 0.040" chemical thinning on the bottom side 0.5” × 0.5” × 0.040" chemical thinning on the bottom side

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EXAMPLE 2.1.1 3” × 3” × 0.040” 5th Layer Bottom Side Corrosion, f=200Hz Total Thickness = 0.643”, Location = 0.603”

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EXAMPLE 2.1.2 0.5” × 0.5” × 0.040” 5th Layer Bottom Side Corrosion, f=200Hz Total Thickness = 0.643”, Location = 0.603”

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Example 2.2 5 Layer 2024 T3 Specimen 0.1” + 0.1” + 0.19” +0.063” + 0.19” Total Thickness = 0.643” Corrosion on Bottom of 4th Layer Location = 0.413”

0.100” 0.100” 0.063” 0.190” 0.190”

0.040” deep corrosion

Remaining Depth = 0.413”

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RFEC Probe Rf4mm

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EXAMPLE 2.2.1 3” × 3” × 0.040” 4th Layer Bottom Side Corrosion, f=200Hz Total Thickness = 0.643”, Location = 0.413”

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EXAMPLE 2.2.2 0.5” × 0.5” × 0.040” 4th Layer Bottom Side Corrosion, f=200Hz Total Thickness = 0.643”, Location = 0.413”

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Example 3 3 Layer 2024 T3 Specimen 0.26” + 0.05” + 0.063” Total Thickness = 0.373” Corrosion on Bottom of 3rd Layer Location = 0.333”

0.260” 0.063” 0.050”

0.5” × 0.5” × 0.006” corrosion

Remaining Depth = 0.413”

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RFEC Probe Rf4mm

0.333”

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Corrosion Sample #5

CNDE Specimen #5 (0.063” thick) 0.5” × 0.5” × 0.006" chemical thinning on the bottom side

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EXAMPLE 3 0.5” × 0.5” × 0.006” 3rd Layer Bottom Side Corrosion, f=500Hz Total Thickness = 0.373”, Location = 0.333”

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RF2mm V. 3 - Two Typical Examples

In Detecting Deeply Hidden Corrosion

It detects (in multi-layer Aluminum Structures):

  • 0.5”×0.5”×0.002” chemical thinning 0.193” below surface

(CNDE Specimen). ~1.1% thinning. (in multi-layer Titanium Structures)

  • 0.5”×0.5”×0.006” chemical thinning 0.157” below surface

(CNDE Specimen). ~4.0% thinning.

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Example 4 4 Layer 2024 T3 Specimen 0.05” + 0.05” + 0.032” + 0.063” Total Thickness = 0.195” Corrosion on Bottom of 4th Layer Location = 0.193”

0.050” 0.063” 0.032”

0.5” × 0.5” × 0.002” corrosion

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RFEC Probe Rf4mm

0.193”

0.050”

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Corrosion Sample #1

CNDE Specimen #5 (0.063” thick) 0.5” × 0.5” × 0.002" chemical thinning on the bottom side

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Direction for Scanning & Probe Orientation Corrosion Area Detecting a 0.5”x0.5”x0.002" thinning 0.192” below surface 1.1% Thinning

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Example 5 3 Layer 2024 T3 Specimen 0.05” + 0.05” + 0.063” Total Thickness = 0.163” Corrosion on Bottom of 3rd Layer Location = 0.157”

0.063”

0.006” deep corrosion

0.050” 0.032”

0.157”

0.050”

Rf2mm Probe

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Corrosion Sample #5

CNDE Specimen #5 (0.063” thick) 0.5” × 0.5” × 0.006" chemical thinning on the bottom side

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1.0” × 1.0” × 0.006" chemical thinning on the bottom side

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EXAMPLE 5.1 1” × 1” × 0.006” 4th Layer Bottom Side Corrosion, f=2.0 kHz Total Thickness = 0.163”, Location = 0.157”

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EXAMPLE 5.2 0.5” × 0.5” × 0.006” 4th Layer Bottom Side Corrosion, f=2.0 kHz Total Thickness = 0.163”, Location = 0.157”

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Building Calibration Standards

Basic Corrosion Parameters We Need to Find out:

  • 1. Corrosion Depth, D.
  • 2. Location, L. Or, which layer? Top or Bottom Surface?
  • 3. Size and Approximate Shape.

D L

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Building Calibration Standards

Two Major Challenges: 1. Location & Depth Estimation – Knowing signal magnitude isn’t enough to tell anything, because it is a function of both Depth and Location. Phase angle is what used in ECT to tell a defect location. However, the relation is not straightforward. How the phase angle of an RFEC signal behaves? 2. Size & Shape Estimation – It is known, from RFECT for tube inspection, that RFEC probe gives a two-peaks signal when it passes a single defect and is difficult to be used for defect shape

  • characterization. Does an RFEC Probe for Inspection Flat

Geometry Objects (FG RFEC probe) tell defect shape information?

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Exploiting Fundamental Features of RFEC Technique Several experimental studies have been carried. They show:

1. For Location & Depth Estimation –

Signal phase angle obtained from a FG RFEC probe is a monotonic function of defect location.

2. For Size & Shape Estimation –

A FG RFEC probe does give a single-peak signal from defect if the defect is located at certain depth from the inspection surface. Therefore, the shape & size can be estimated from signal image.

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Location to Signal Phase Relation (1)

0.100” 0.040” 0.063” 0.032” 0.190” 0.040” 0.063” 0.032” 0.190” 0.000”, 0.010” or 0.02” 0.100” 0.040” 0.040” 0.063” 0.032” 0.100” 0.040” 0.190” 0.063”

L = 0.353” L = 0.163” L = 0.063”

Case 0.353” Case 0.163” Case 0.063”

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Remaining Thickness to Signal Phase Relation (2)

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Corrosion Depth to Signal Imaginary, Y, Relation

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Suggested Calibration Standard for Location & Depth

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A Single-Peak Signal from RF4mm V.3 Opt. 3 Probe

Varying # of layers & Location, D Material Break with air-gap length, G= 0.00”

F = 200Hz Corrosion Size & Shape Estimation

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Magnitude Imaginary, Y Phase Angle At L = 0.06”, it is a double-peak signal Drive coil passes Pickup coil passes Corrosion Size & Shape Estimation

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At L = 0.160”, it becomes a single-peak signal Magnitude Imaginary, Y Phase Angle

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Corrosion Size & Shape Estimation

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At L = 0.54”, signal peak approaching the defect position Magnitude Imaginary, Y Phase Angle Corrosion Size & Shape Estimation

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A Single-Peak Signal from A FG RFEC Probe

Varying # of layers & Location, L Material Break with air-gap length, G= 0.15”

To go deeper we use f = 100Hz & Air-gap Length = 0.15” Corrosion Size & Shape Estimation

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When f = 100 Hz signals when L ≥ 0.54 L = 0.54” L = 0.64” L = 0.73” Corrosion Size & Shape Estimation

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For shallow corrosion shape distortion decreases with increase of frequency RF4mm 200 Hz L=0.105” D=0.02” RF4mm 2 kHz L=0.105” D=0.02” Imaginary Y 0.32*Ymax Contours Corrosion Edges Corrosion Size & Shape Estimation

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Shape distortion can be minimized with small-sized probe Rf2mm 2 kHz L=0.123” D=0.003” Corrosion Size & Shape Estimation Rf2mm 2 kHz L=0.060” D=0.003”

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About Shape Factor “0.32” RF2mm Probe Corrosion Size & Shape Estimation

1”×1”×0.006”, L=0.157” 0.5”×0.5”×0.006”, L=0.157” 0.5”×0.5”×0.002”, L=0.192”

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About Shape Factor “0.32” - RF4mm Probe Corrosion Size & Shape Estimation

0.5”×0.5”×0.006”, L=0.413” 0.5”×0.5”×0.006”, L=0.413”

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Innovative Materials Testing Technologies, Inc.

About Shape Factor “0.32” - RF4mm Probe Corrosion Size & Shape Estimation

0.5”×0.5”×0.006”, L=0.603” 0.5”×0.5”×0.006”, L=0.603”

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Enhanced Edge in RFEC Signal Due to Designed Probe Structure Corrosion Size & Shape Estimation Φ 0.75 × 0.003”, L = 0.060” Φ 0.75 × 0.003”, L = 0.123”

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Summary and Future Work

  • 1. Corrosion defects can be calibrated based on the

following features of RFEC probe signals:

  • a. Monotonic relation of signal phase to defect

location, L;

  • b. At a given L imaginary,Y value increases with

increase of defect depth, D; c. An RFEC signal becomes of single-peak when L is greater a certain value.

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Summary and Future Work

  • 2. A possible calibration process has been suggested. It

consists of three steps:

  • a. Determine location L, or on which layer and top
  • r bottom surface, the defect is located;
  • b. Estimate corrosion depth, D, based on the

determined L and signal Y. c. Estimate defect size and shape based on the image of signal Y of a defect.

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SLIDE 53

Summary and Future Work

  • 3. The accuracy of size & shape estimation depends on:
  • a. Defect size/probe size ratio;
  • b. Frequency and defect location.
  • 4. The enhanced edge feature of current probes creates

error in defect size & shape estimation. Therefore, new probes with less edge enhancement need to be developed.

  • 5. Application of the suggested calibration process to

aircraft applications.

Innovative Materials Testing Technologies, Inc.