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Eddy current interaction between a probe coil and a

conducting plate

Marion Darbas, Edouard Demaldent, Olivier Goubet, Vianney Real

To cite this version:

Marion Darbas, Edouard Demaldent, Olivier Goubet, Vianney Real. Eddy current interaction between

a probe coil and a conducting plate. 2nd ECCOMAS Young Investigators Conference (YIC 2013),

Sep 2013, Bordeaux, France. �hal-00855873�

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2–6 September 2013, Bordeaux, France

Eddy current interaction between a probe coil and a conducting plate

M. Darbas

a

, E. Demaldent

b

, O. Goubet

a

, V. Real

a,∗

,

aLAMFA UMR CNRS 7352

Universit´e de Picardie Jules Verne, 33 rue Saint-Leu, 80039 Amiens

bCEA, LIST, Saclay, 91191 Gif-sur-Yvette Cedexvianney.real@u-picardie.fr

Abstract. Consider a coil above a conducting plate. The interaction between the probe-coil and the plate is modeled by a quasi-static approximation of Maxwell’s equations: the eddy current model. The associated electromagnetic transmission boundary-value problem can be solved by the integral equations method. However, the discretization of integral operators gives dense, complex and ill-conditioned linear systems. We present here a method to compute the reaction field and the coil impedance variation by solving only surface partial differential equations.

Keywords: Eddy currents; integral equations; Pad´e approximation.

1

INTRODUCTION

We are interested in eddy current non-destructive testing of a conducting plate. Eddy current method is based on the principle of measuring changes in the impedance of an electromagnetic coil as it is scanned over a surface of a conductive material. This method is modeled as a low-frequency electromagnetic transmission problem between two media: the air containing the probe-coil and the conducting workpiece. Integral equations method is one of the principal tools to solve this problem (e.g. [3, 5, 6]). This approach applies the Green’s function formalism to reduce equivalently the governing boundary value problem to an integral equation set on the interface between the media. The discretization of boundary integral formulations leads to fully-populated and in general, ill-conditioned complex linear systems. We propose an alternative to compute the impedance variation of the coil in a simplified configuration. This approach is based on the knowledge of the Steklov-Poincar´e operator (or Dirichlet-to-Neumann map) which is expressed by non-local square-root operators. To localize this operator, we propose the so-called Pad´e approximation. This leads to solve only a finite number of sparse linear systems.

2

AN ELECTROMAGNETIC TRANSMISSION PROBLEM

2.1 Configuration

Consider the following configuration. The interface Γ = {x ∈ R3|x3= 0} divides the whole space into two media:

a non-conducting air domain Ωext= R3

+containing the coil, and a conducting plate Ωc= R3−(without defect). We

denote by n the outgoing unit normal to the surface Γ.

We make the following assumptions. The coil creates a current source Js with sinusoidal angular frequency ω

and fixed amplitude. The impressed current Js has only support in Ωextand divJs = 0 and Js · n = 0 on ∂Ωs

with Ωs := supp(Js). Assume that the coil does not affect the electromagnetic parameters of Ωext. The exterior

domain Ωextis homogeneous with magnetic permeability µ = µ0, electric permittivity  = 0and zero conductivity

σ = 0. As a first step, assume further that magnetic permeability µc and electric permittivity cof the conductor

are constants. We are only interested in the variation of the electrical conductivity σc. For a workpiece Ωcwithout

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2 M. Darbas et al. | Young Investigators Conference 2013

Figure 1: Configuration

2.2 Functional setting

The results of this section can be found in [5]. Ω is equally Ωcand Ωext. The normal vector n is the outward normal

to Ωc. We define the trace operators: let u ∈ (C∞ 0 (Ω))3

γ×(u) = u|Γ× n (Dirichlet vectorial trace),

γT(u) = n × (u|Γ× n) (tangential component),

γN(u) = curl(u)|Γ× n (Neumann vectorial trace).

We extend the trace operators to H(curl, Ω) = {u ∈ (L2(Ω))3| curl(u) ∈ (L2(Ω))3}.

Definition 1 We define Y the range of γ×as follows

Y = {λ ∈ H−1/2(Γ); ∃E ∈ H(curl, Ω); E × n = λ}. The space Y with the normkλkY = inf

E×n=λkEkH(curl,Ω)is a Hilbert space.

Theorem 1 We have

Y = {λ ∈ H−1/2(Γ); λ · n = 0 et divΓλ ∈ H−1/2(Γ)}.

We define the Hilbert space Z by

γT : H(curl, Ω) → Z = {λ ∈ H−1/2(Γ), curlΓλ ∈ H−1/2(Γ)}

E 7→ n × E × n.

Spaces Y and Z are in duality by the following duality product < γ×(E), γT(v) >=

Z

curl E · v − Z

E · curl v ∀E, v ∈ H(curl, Ω). 2.3 The electromagnetic transmission problem

We consider the E-field formulation. We introduce the notations:

• the total exterior field E|Ωext = Er+ Einc, with Erand Eincthe reaction and incident fields,

• the total interior field E|Ωc = Ec.

Consider the following time-harmonic model (with a time dependence in eiωt) with the condition ω 

σc

 1. Under this condition, we can consider the quasi-static approximation of Maxwell’s equations: the eddy current model (see [1]). The dielectric displacement currents are neglected in the Maxwell’s equations in the exterior domain. Furthermore, the assumptions on the current source and  ' 0 yield divEr= 0 in Ωext.

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• Input : an incident electric field Eincgenerated by the coil and such that

curl curl Einc = −iωµ0Jsδcoil, divEinc= 0, in Ωext.

• E-field formulation : find (Er, Ec) such that

(P)                   

curl curl Er= 0, divEr= 0, in Ωext,

curl curl Ec+ k2Ec= 0, in Ωc, Ec× n = Er |Γ× n + Einc|Γ × n, on Γ, curl Ec× n = curl Er |Γ× n + curl Einc|Γ × n, on Γ, E(x) = O( 1 |x|), curl E(x) = O( 1 |x|2), |x| → +∞,

with the complex wavenumber k = √

2 2 (1+i)

ωµ0σc. To overcome the unboundedness of the computational

domain, the method of integral equations (e.g. [5, 6]) can be applied. The Stratton-Chu integral representation formula allows to express the field Er(resp. Ec) in terms of the surfacic unknowns Er

|Γ× n and curl Er|Γ× n

(resp. Ec

|Γ× n and curl Ec|Γ× n). The surfacic fields become the new unknows of the problem. Applying

the trace operators to the Stratton-Chu representation formula, and translating the boundary transmission conditions yield boundary integral equations on Γ. We have to solve these integral equations to obtain: • Output :

Er× n and curl Er |Γ× n.

These surface data are not experimentally observable. The only quantity which is accessible is the coil impedance variation. This quantity of interest can be expressed with these data. We have:

• Impedance variation [2] : ∆Z = − i I2ωµ 0 Z Γ curl Einc × n · Er× nds − Z Γ curl Er× n · Einc × nds  , (1) with u · v =P3

i=1uivi, uv ∈ C3and I the current energizing the coil.

3

SOLVING THE PROBLEM

In order to solve the electromagnetic transmission problem (P), we define the exterior and interior Steklov-Poincar´e operators SPint k : Z → Y γT−(Ec) 7→ γ− N(E c), SPext 0 : Z → Y γT+(Er) 7→ γN+(Er).

In the configuration described in Fig. 1, Fourier analysis allows us to obtain expressions in terms of surface differ-ential operators: SPint k = k2IdΓ− ∆Γ −1/2 k2Id Γ+ curlΓcurlΓ , and SPext 0 = − (−∆Γ)−1/2curlΓcurlΓ, with ∆Γv =   ∆Γv1 −∆Γv2 0  =   ∂12v1+ ∂22v1 ∂2 1v2+ ∂22v2 0  , curlΓv =   ∂2v −∂1v 0 

et curlΓv = ∂1v2− ∂2v1. Then, the

transmission problem (P) is equivalently reduced to solving the surface problem: find γT+(Er) ∈ H−1/2(curlΓ, Γ)

solution to (SPint k − SP ext 0 )γ + T(E r) = −(SPint k + SP ext 0 )γ + T(E inc), on Γ. (2)

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4 M. Darbas et al. | Young Investigators Conference 2013

To this end, we use the Helmholtz decomposition of the fields. In the case of the interface Γ = {x3 = 0}, the

Helmholtz decomposition of γT+(Er) and γ+

T(Einc) ∈ H−1/2(curlΓ, Γ) are given respectively by

γT+(Einc) = ∇Γe1+ curlΓe2, (e1, e2) ∈ H1/2(Γ) × H3/2(Γ),

γT+(Er) = ∇Γϕ1+ curlΓϕ2, (ϕ1, ϕ2) ∈ H1/2(Γ) × H3/2(Γ).

Solving equation (2) means to seek (ϕ1, ϕ2) ∈ H1/2(Γ) × H3/2(Γ) that is solution of the differential system

   ϕ1= −e1on Γ. (3) ϕ2=  −1 + 2∆Γ k2 + 2 −∆Γ k2 1/2 1 −∆Γ k2 1/2 e2, on Γ, (4)

where (e1, e2) are known. The operators involved in equation (4) are non-local operators. We propose to localize

the square-root operators thanks to a Pad´e paraxial approximation of order Npwith a rotating branch-cut technique

of angle θ [7, 4]  1 − ∆Γ k2 1/2 ≈ C0− Np X k=1 Aj∆Γ  k2− Bj∆Γ −1 , (5)

with C0, Aj, Bj, j = 1, . . . , Np complex coefficients depending on θ. Now, we can compute the impedance

variation using the following formula ∆Z = 2 I2 σc k2 Z Γ curlΓ(−∆Γ)1/2e2· curlΓϕ2ds. (6)

4

CONCLUSIONS

In this paper, we propose an approach to solve a low-frequency electromagnetic transmission problem by solving only a finite number of sparse linear systems. On the contrary, the usual method of integral equations involves the solution of dense complex and ill-conditioned linear systems. We have to implement the method in order to study its accuracy. The solution of this direct problem is the first step of the research program PINCEL which is devoted to the solution of an inverse problem related to the location of defects in a conducting plate.

ACKNOWLEDGEMENT

We acknowledge the support of the European Community and of the Conseil Regional de Picardie.

REFERENCES

[1] Ammari, H., Buffa, A., Nedelec, J.C.. A justification of eddy currents model for the Maxwell equations. SIAM J. Appl. Math. 60, 1805-1823, 2000.

[2] Auld, B.A., Moulder, J.C.. Review of advances in quantitative eddy current nondestructive evaluation. Journal of Nonde-structive evaluation. 18:3-36, 1999.

[3] Christiansen, S. H.. Mixed boundary element method for eddy current problems. Research Report No. 2002-16, september 2002, Z¨urich.

[4] Darbas, M.. Pr´econditionneurs analytiques de types Calder`on pour les formulations int´egrales des probl`emes de diffraction d’ondes. PhD Thesis, INSA de Toulouse, 2004.

[5] Engleder, S.. Boundary Element Methods for Eddy Current Transmission Problems. Thesis, Technische Universitt Graz, 2011.

[6] Lim, T.. Formulation int´egrale surfacique des ´equations de Maxwell pour la simulation de contrˆoles non destructifs par courants de Foucault. Etude pr´eliminaire `a la mise en oeuvre de la m´ethode multipˆole rapide. PhD Thesis, Ecole Polytech-nique, 2011.

[7] Milinazzo, F.A., Zala, C.A., Brooke, G.H.. Rational square-root approximations for parabolic equation algorithms. J. Acous. Soc. Am..101:760-766, 1997.

Figure

Figure 1: Configuration

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