Electromagnetic Acoustic Transducer (EMAT) Analysis
Theory: making the source in the specimen surface
Overview
I want to measure wall thickness on a 300 °C pipe during operation, but ordinary ultrasonic probes can't touch it. Would an EMAT work?
That's an EMAT's strength. Ordinary probes transmit a piezo element's vibration through a water or gel couplant. An EMAT drives high-frequency current in a coil to induce eddy currents in the specimen surface, under a magnet's field; the eddy currents feel a Lorentz force and the surface itself becomes the source. No contact or couplant needed. The trade-offs are low transduction efficiency and sensitivity to the gap between coil and surface.
Lorentz force and skin depth
$\mathbf{J}_e$ is eddy-current density, $\mathbf{B}_0$ the magnet's static field and $\delta$ the skin depth over which eddy currents flow. Currents gather within about $\delta$ of the surface, so the force arises in that thin layer. In ferromagnets magnetostrictive forces add, and efficiency depends strongly on the material's magnetic state.
Effect of liftoff
$D$ is the spatial period of a meander coil or similar and $g$ the liftoff. A periodic field decays exponentially with distance relative to its period. It applies on both transmit and receive, doubling the dB loss. This is an idealised estimate for the periodic component; real coils add geometric effects.
Rails and hot steel strip
Electromagnetic generation of ultrasound was known from the mid-20th century, but practical use grew from the 1970s. Needing no couplant, EMATs found work on targets that can't be touched — measuring the thickness of steel strip at hundreds of degrees just after rolling, or searching rails for flaws from moving inspection cars. Strong rare-earth magnets and low-noise amplifiers for faint signals offset the low efficiency and broadened their use.
Worked examples
Example 1: skin depth and wavelength
| Material | Frequency | Skin depth | Shear wavelength | Ratio |
|---|---|---|---|---|
| Aluminium | 2 MHz | 0.060 mm | 1.55 mm | 0.04 |
| Austenitic stainless | 2 MHz | 0.30 mm | 1.55 mm | 0.19 |
| Carbon steel (μr = 100 assumed) | 2 MHz | 0.015 mm | 1.61 mm | 0.009 |
| Austenitic stainless | 0.5 MHz | 0.60 mm | 6.2 mm | 0.10 |
Usually skin depth is a few to a dozen or so percent of the wavelength, so forces can be treated as surface loads. In low-conductivity stainless, however, it approaches 20% of the wavelength, and including the through-depth force distribution is more accurate. Carbon steel's permeability varies strongly with field, so its skin depth depends on the magnet conditions.
Example 2: sensitivity loss with liftoff
| Liftoff | 6 mm coil period | 3 mm coil period |
|---|---|---|
| 0.2 mm | −3.6 dB | −7.3 dB |
| 0.5 mm | −9.1 dB | −18.2 dB |
| 1.0 mm | −18.2 dB | −36.4 dB |
| 2.0 mm | −36.4 dB | −72.8 dB |
Just 1 mm of liftoff cuts the signal to an eighth. I wanted a protective layer for the hot pipe…
A protective layer's thickness becomes liftoff, so it's a trade-off with sensitivity. A longer coil period reduces liftoff sensitivity, but the period is tied to the wavelength you want to excite and can't be chosen freely. Oxide scale, roughness and pipe curvature also change the gap, so check in analysis that the signal stays above noise at the worst-case liftoff. Magnets weaken with temperature too, so plan their thermal management.
How to approach the analysis
Procedure
- Solve the magnet's static field; for ferromagnetic specimens, obtain magnetisation state and permeability.
- Solve eddy currents from the coil's high-frequency current, resolving the skin depth with several mesh layers.
- Compute Lorentz (and magnetostrictive) forces and pass them to the elastic-wave analysis as surface loads.
- Solve elastic waves for reflections from flaws and back walls, with at least 10–20 elements per wavelength.
- For reception, compute coil voltage from surface vibration as the reverse process.
“Same steel, different signal size”
On carbon-steel pipe of one grade, EMAT signal size can vary by more than a factor of two from place to place. In carbon steel, magnetostrictive forces rival the Lorentz force, and their size depends on residual magnetisation, stress and microstructure — especially near welds or areas magnetised earlier by magnetic-particle testing. Thickness measurement uses arrival time, so amplitude differences matter little, but estimating flaw size from signal strength must allow for this variation.
Common mistakes
Mistakes and fixes
| Mistake | Effect | Fix |
|---|---|---|
| Coarse mesh in the skin layer | Wrong force magnitude | Several layers in δ |
| Using ideal liftoff | Insufficient signal in practice | Check worst-case liftoff |
| Ignoring magnetostriction in ferromagnets | Efficiency badly wrong | Add magnetostrictive forces |
| Coarse elastic-wave mesh | Distorted waveforms | 10–20+ elements per wavelength |
| Ignoring magnet temperature effects | Sensitivity loss when hot | Evaluate field at temperature |
I'd like to try elastic waves and skin depth myself.
Try the elastic wave simulator for elastic waves, the Lamb wave dispersion tool for plate waves and the skin depth calculator for skin depth. Force mechanisms are covered in Lorentz force and magnetostriction, and other transduction methods in piezoelectric analysis and electromagnetic forming.
Related Topics
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