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⇱ Electromagnetic reverberation chamber - Wikipedia


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Equipment for electromagnetic testing
πŸ‘ Image
A look inside the (large) Reverberation Chamber at the Otto-von-Guericke-University Magdeburg, Germany. On the left side is the vertical Mode Stirrer (or Tuner), that changes the electromagnetic boundaries to ensure a (statistically) homogeneous field distribution.

An electromagnetic reverberation chamber (also known as a reverb chamber (RVC) or mode-stirred chamber (MSC)) is an environment for electromagnetic compatibility (EMC) testing and other electromagnetic investigations. Electromagnetic reverberation chambers have been introduced first by H.A. Mendes in 1968.[1] A reverberation chamber is screened room with a minimum of absorption of electromagnetic energy. Due to the low absorption, very high field strength can be achieved with moderate input power. A reverberation chamber is a cavity resonator with a high Q factor. Thus, the spatial distribution of the electrical and magnetic field strengths is strongly inhomogeneous (standing waves). To reduce this inhomogeneity, one or more tuners (stirrers) are used. A tuner is a construction with large metallic reflectors that can be moved to different orientations in order to achieve different boundary conditions. The Lowest Usable Frequency (LUF) of a reverberation chamber depends on the size of the chamber and the design of the tuner. Small chambers have a higher LUF than large chambers.

The concept of a reverberation chamber is comparable to a microwave oven.

Glossary/notation

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Preface

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The notation is mainly the same as in the IEC standard 61000-4-21.[2] For statistic quantities like mean and maximal values, a more explicit notation is used in order to emphasize the used domain. Here, spatial domain (subscript πŸ‘ {\displaystyle s}
) means that quantities are taken for different chamber positions, and ensemble domain (subscript πŸ‘ {\displaystyle e}
) refers to different boundary or excitation conditions (e.g. tuner positions).

General

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Statistics

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Theory

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Cavity resonator

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A reverberation chamber is cavity resonatorβ€”usually a screened roomβ€”that is operated in the overmoded region. To understand what that means we have to investigate cavity resonators briefly.

For rectangular cavities, the resonance frequencies (or eigenfrequencies, or natural frequencies) πŸ‘ {\displaystyle f_{mnp}}
are given by

πŸ‘ {\displaystyle f_{mnp}={\frac {c}{2}}{\sqrt {\left({\frac {m}{l}}\right)^{2}+\left({\frac {n}{w}}\right)^{2}+\left({\frac {p}{h}}\right)^{2}}},}

where πŸ‘ {\displaystyle c}
is the speed of light, πŸ‘ {\displaystyle l}
, πŸ‘ {\displaystyle w}
and πŸ‘ {\displaystyle h}
are the cavity's length, width and height, and πŸ‘ {\displaystyle m}
, πŸ‘ {\displaystyle n}
, πŸ‘ {\displaystyle p}
are non-negative integers (at most one of those can be zero).

With that equation, the number of modes with an eigenfrequency less than a given limit πŸ‘ {\displaystyle f}
, πŸ‘ {\displaystyle N(f)}
, can be counted. This results in a stepwise function. In principle, two modesβ€”a transversal electric mode πŸ‘ {\displaystyle TE_{mnp}}
and a transversal magnetic mode πŸ‘ {\displaystyle TM_{mnp}}
β€”exist for each eigenfrequency.

The fields at the chamber position πŸ‘ {\displaystyle (x,y,z)}
are given by

 πŸ‘ {\displaystyle E_{x}=-{\frac {1}{j\omega \epsilon }}k_{x}k_{z}\cos k_{x}x\sin k_{y}y\sin k_{z}z}
πŸ‘ {\displaystyle E_{y}=-{\frac {1}{j\omega \epsilon }}k_{y}k_{z}\sin k_{x}x\cos k_{y}y\sin k_{z}z}
πŸ‘ {\displaystyle E_{z}={\frac {1}{j\omega \epsilon }}k_{xy}^{2}\sin k_{x}x\sin k_{y}y\cos k_{z}z}
πŸ‘ {\displaystyle H_{x}=k_{y}\sin k_{x}x\cos k_{y}y\cos k_{z}z}
πŸ‘ {\displaystyle H_{y}=-k_{x}\cos k_{x}x\sin k_{y}y\cos k_{z}z}
πŸ‘ {\displaystyle k_{r}^{2}=k_{x}^{2}+k_{y}^{2}+k_{z}^{2},\,k_{x}={\frac {m\pi }{l}},\,k_{y}={\frac {n\pi }{w}},\,k_{z}={\frac {p\pi }{h}}\,k_{xy}^{2}=k_{x}^{2}+k_{y}^{2}}
 πŸ‘ {\displaystyle E_{x}=k_{y}\cos k_{x}x\sin k_{y}y\sin k_{z}z}
πŸ‘ {\displaystyle E_{y}=-k_{x}\sin k_{x}x\cos k_{y}y\sin k_{z}z}
πŸ‘ {\displaystyle H_{x}=-{\frac {1}{j\omega \mu }}k_{x}k_{z}\sin k_{x}x\cos k_{y}y\cos k_{z}z}
πŸ‘ {\displaystyle H_{y}=-{\frac {1}{j\omega \mu }}k_{y}k_{z}\cos k_{x}x\sin k_{y}y\cos k_{z}z}
πŸ‘ {\displaystyle H_{z}={\frac {1}{j\omega \mu }}k_{xy}^{2}\cos k_{x}x\cos k_{y}y\sin k_{z}z}

Due to the boundary conditions for the E- and H field, some modes do not exist. The restrictions are:[3]

  • For TM modes: m and n can not be zero, p can be zero
  • For TE modes: m or n can be zero (but not both can be zero), p can not be zero

A smooth approximation of πŸ‘ {\displaystyle N(f)}
, πŸ‘ {\displaystyle {\overline {N}}(f)}
, is given by

πŸ‘ {\displaystyle {\overline {N}}(f)={\frac {8\pi }{3}}lwh\left({\frac {f}{c}}\right)^{3}-(l+w+h){\frac {f}{c}}+{\frac {1}{2}}.}

The leading term is proportional to the chamber volume and to the third power of the frequency. This term is identical to Weyl's formula.

πŸ‘ Image
Comparison of the exact and the smoothed number of modes for the Large Magdeburg Reverberation Chamber.

Based on πŸ‘ {\displaystyle {\overline {N}}(f)}
the mode density πŸ‘ {\displaystyle {\overline {n}}(f)}
is given by

πŸ‘ {\displaystyle {\overline {n}}(f)={\frac {d{\overline {N}}(f)}{df}}={\frac {8\pi }{c}}lwh\left({\frac {f}{c}}\right)^{2}-(l+w+h){\frac {1}{c}}.}

An important quantity is the number of modes in a certain frequency interval πŸ‘ {\displaystyle \Delta f}
, πŸ‘ {\displaystyle {\overline {N}}_{\Delta f}(f)}
, that is given by

πŸ‘ {\displaystyle {\begin{matrix}{\overline {N}}_{\Delta f}(f)&=&\int _{f-\Delta f/2}^{f+\Delta f/2}{\overline {n}}(f)df\\\ &=&{\overline {N}}(f+\Delta f/2)-{\overline {N}}(f-\Delta f/2)\\\ &\simeq &{\frac {8\pi lwh}{c^{3}}}\cdot f^{2}\cdot \Delta f\end{matrix}}}

Quality factor

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The Quality Factor (or Q Factor) is an important quantity for all resonant systems. Generally, the Q factor is defined by πŸ‘ {\displaystyle Q=\omega {\frac {\rm {maximum\;stored\;energy}}{\rm {average\;power\;loss}}}=\omega {\frac {W_{s}}{P_{l}}},}
where the maximum and the average are taken over one cycle, and πŸ‘ {\displaystyle \omega =2\pi f}
is the angular frequency.

The factor Q of the TE and TM modes can be calculated from the fields. The stored energy πŸ‘ {\displaystyle W_{s}}
is given by

πŸ‘ {\displaystyle W_{s}={\frac {\epsilon }{2}}\iiint _{V}|{\vec {E}}|^{2}dV={\frac {\mu }{2}}\iiint _{V}|{\vec {H}}|^{2}dV.}

The loss occurs in the metallic walls. If the wall's electrical conductivity is πŸ‘ {\displaystyle \sigma }
and its permeability is πŸ‘ {\displaystyle \mu }
, the surface resistance πŸ‘ {\displaystyle R_{s}}
is

πŸ‘ {\displaystyle R_{s}={\frac {1}{\sigma \delta _{s}}}={\sqrt {\frac {\pi \mu f}{\sigma }}},}

where πŸ‘ {\displaystyle \delta _{s}=1/{\sqrt {\pi \mu \sigma f}}}
is the skin depth of the wall material.

The losses πŸ‘ {\displaystyle P_{l}}
are calculated according to

πŸ‘ {\displaystyle P_{l}={\frac {R_{s}}{2}}\iint _{S}|{\vec {H}}|^{2}dS.}

For a rectangular cavity follows[4]

  • for TE modes:
 πŸ‘ {\displaystyle Q_{\rm {TE_{mnp}}}={\frac {Z_{0}lwh}{4R_{s}}}{\frac {k_{xy}^{2}k_{r}^{3}}{\zeta lh\left(k_{xy}^{4}+k_{x}^{2}k_{z}^{2}\right)+\xi wh\left(k_{xy}^{4}+k_{y}^{2}k_{z}^{2}\right)+lwk_{xy}^{2}k_{z}^{2}}}}
πŸ‘ {\displaystyle \zeta ={\begin{cases}1&{\mbox{if }}n\neq 0\\1/2&{\mbox{if }}n=0\end{cases}},\quad \xi ={\begin{cases}1&{\mbox{if }}m\neq 0\\1/2&{\mbox{if }}m=0\end{cases}}}
  • for TM modes:
πŸ‘ {\displaystyle Q_{\rm {TM_{mnp}}}={\frac {Z_{0}lwh}{4R_{s}}}{\frac {k_{xy}^{2}k_{r}}{w(\gamma l+h)k_{x}^{2}+l(\gamma w+h)k_{y}^{2}}}}
πŸ‘ {\displaystyle \gamma ={\begin{cases}1&{\mbox{if }}p\neq 0\\1/2&{\mbox{if }}p=0\end{cases}}}

Using the Q values of the individual modes, an averaged Composite Quality Factor πŸ‘ {\displaystyle {\tilde {Q_{s}}}}
can be derived:[5] πŸ‘ {\displaystyle {\frac {1}{\tilde {Q_{s}}}}=\langle {\frac {1}{Q_{mnp}}}\rangle _{k\leq k_{r}\leq k_{r}+\Delta k}}
πŸ‘ {\displaystyle {\tilde {Q_{s}}}={\frac {3}{2}}{\frac {V}{S\delta _{s}}}{\frac {1}{1+{\frac {3c}{16f}}\left(1/l+1/w+1/h\right)}}}

πŸ‘ {\displaystyle {\tilde {Q_{s}}}}
includes only losses due to the finite conductivity of the chamber walls and is therefore an upper limit. Other losses are dielectric losses e.g. in antenna support structures, losses due to wall coatings, and leakage losses. For the lower frequency range the dominant loss is due to the antenna used to couple energy to the room (transmitting antenna, Tx) and to monitor the fields in the chamber (receiving antenna, Rx). This antenna loss πŸ‘ {\displaystyle Q_{a}}
is given by πŸ‘ {\displaystyle Q_{a}={\frac {16\pi ^{2}Vf^{3}}{c^{3}N_{a}}},}
where πŸ‘ {\displaystyle N_{a}}
is the number of antenna in the chamber.

The quality factor including all losses is the harmonic sum of the factors for all single loss processes:

πŸ‘ {\displaystyle {\frac {1}{Q}}=\sum _{i}{\frac {1}{Q_{i}}}}

Resulting from the finite quality factor the eigenmodes are broaden in frequency, i.e. a mode can be excited even if the operating frequency does not exactly match the eigenfrequency. Therefore, more eigenmodes are exited for a given frequency at the same time.

The Q-bandwidth πŸ‘ {\displaystyle {\rm {BW}}_{Q}}
is a measure of the frequency bandwidth over which the modes in a reverberation chamber are correlated. The πŸ‘ {\displaystyle {\rm {BW}}_{Q}}
of a reverberation chamber can be calculated using the following:

πŸ‘ {\displaystyle {\rm {BW}}_{Q}={\frac {f}{Q}}}

Using the formula πŸ‘ {\displaystyle {\overline {N}}_{\Delta f}(f)}
the number of modes excited within πŸ‘ {\displaystyle {\rm {BW}}_{Q}}
results to

πŸ‘ {\displaystyle M(f)={\frac {8\pi Vf^{3}}{c^{3}Q}}.}

Related to the chamber quality factor is the chamber time constant πŸ‘ {\displaystyle \tau }
by

πŸ‘ {\displaystyle \tau ={\frac {Q}{2\pi f}}.}

That is the time constant of the free energy relaxation of the chamber's field (exponential decay) if the input power is switched off.

See also

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Notes

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  1. ^ Mendes, H.A.: A new approach to electromagnetic field-strength measurements in shielded enclosures., Wescon Tech. Papers, Los Angeles, CA., August, 1968.
  2. ^ IEC 61000-4-21: Electromagnetic compatibility (EMC) – Part 4-21: Testing and measurement techniques – Reverberation chamber test methods, Ed. 2.0, January, 2011. ([1])
  3. ^ Cheng, D.K.: Field and Wave Electromagnetics, Addison-Wesley Publishing Company Inc., Edition 2, 1998. ISBN 0-201-52820-7
  4. ^ Chang, K.: Handbook of Microwave and Optical Components, Volume 1, John Wiley & Sons Inc., 1989. ISBN 0-471-61366-5.
  5. ^ Liu, B.H., Chang, D.C., Ma, M.T.: Eigenmodes and the Composite Quality Factor of a Reverberating Chamber, NBS Technical Note 1066, National Bureau of Standards, Boulder, CO., August 1983.

References

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  • Crawford, M.L.; Koepke, G.H.: Design, Evaluation, and Use of a Reverberation Chamber for Performing Electromagnetic Susceptibility/Vulnerability Measurements, NBS Technical Note 1092, National Bureau od Standards, Boulder, CO, April, 1986.
  • Ladbury, J.M.; Koepke, G.H.: Reverberation chamber relationships: corrections and improvements or three wrongs can (almost) make a right, Electromagnetic Compatibility, 1999 IEEE International Symposium on, Volume 1, 1–6, 2–6 August 1999.