CurtainCall
Aerospace
- Oct 26, 2010
- 14
Hello,
TL;DR: If someone could please confirm that this is right, (more details and thought process below) attenuation for thin-walled enclosures can be approximated by:
Attenuation [dB] = 20 log ( (?/2a)*(r/a) ) - 20 log (n[sup]1/2[/sup]);
Where:
? = wavelength
a = largest cross-sectional dimention of the aperture
r = distance of frequency source to aperture
n = number of similar apertures with edge-to-edge distances of less than ?/2
d = depth of the aperture (material thickness)
NB: s < ?/2 > a > d to be valid
Thank you,
- Kirk
My boss has asked me to put together a design reference for EM/RF sheilding for internal and external support. Unfortuately being a mechanical/aerospace engineer this is a little out of my league. If anyone would mind going over and critiquing what I have learned so far I would appriciate it.
EM/RF sheilding is used to isolate the component to prohibit interference from the environment to the component and vise-versa.
To isolate the component a conductive structure is required to "balence" internal and external charges.
A perfectly sealed Faraday cage would be the ideal solution, but is not always practical or desired.
The two main sources of leaks/losses are seams and apertures.
NB: Due to the similarity between apertures as "holes" and antenna apertures, for simplicity I will refer to "holes" from now on.
Seams are caused by the manufacturing process and can be treated with gaskets or specialized fabrication techniques such as double flanging to maximize contact area between the conductive materials.
Screws and other fasteners can be used to create discontinuties in seams to reduce losses.
Untreated seams can be considered as narrow, lengthy holes.
Holes in enclosures are required for cooling/ventalation, external access (power/data transfer), etc.
The exact geometrical shape of the hole is irrelevant to the losses occured (to a point).
Though different shapes can have unrelated benificial effects, ie honeycomb structures for airflow.
The largest of the cross-sectional (CS) dimensions of a hole is important.
If the holes have significant depth, ie the material is thick, or are coupled to tubes; the holes can be assumed to act as waveguides.
A waveguide will attenuate the signal of any signal below a certain cutt-off frequency.
The cutt-off frequency is approximately the frequency at which the largest CS dimension is equal to a half wavelength.
For waveguide-like holes a simple approximation of signal attenuation is:
Attenuation = C * (d/a) * sqrt( (1-(f/fc)[sup]2[/sup]) ) [ignore][dB][/ignore];
Where:
C = waveguide coefficient; Generally 30, rectangular hole 27, circular hole 32
d = depth of hole (material thickness or length of coupled tube)
a = largest CS dimension
f = frequency of the field
fc = cutt-off frequency
NB: this equation is only valid for waveguide like holes, ie d>>a
For thin-walled enclosures:
Wavelengths smaller than twice the largest CS dimension (2a) will not be attenuated.
Wavelengths equal to 2a will have 0dB shielding, inferring the cutt-off frequency to be:
fc = C/2a;
Where:
C = propogation velocity of an EM wave (ie speed of light)
For Wavelengths greater than 2a attenuation can be approximated via:
Attenuation [ignore][dB][/ignore] = 20 log(?/2d);
Where:
? = wavelength
NB: This is only valid for ?/2 > a > d
NB: Maximum attenuation is the attenuation of a solid barrier with no holes, aka faraday cage construction
NB: To neglect the effects of signal noice within the enclosure the component must be atleast distance, d, away from the enclousure
If you cannot place the component far enough away, then you can approximate the effect of signal noise:
fc = (C/2a)*(r/a);
Where:
r = distance to the hole
and
Attenuation [ignore][dB][/ignore] = 20 log(fc/f) = 20 log( (?/2a)*(r/a) )
If there are multiple similar holes and spaced closely together, ie s < ?/2, where s is the spacing between holes. The attenuation can be approximated by:
Attenuation [ignore][dB][/ignore] = 20 log(?/2) - 20 log(n[sup]1/2[/sup]);
Where:
n = number of holes
s < ?/2 > a > d
s = edge to edge hole spacing
Now there is a whole lot more to go through with: different arrays of holes, absorbtion loss of waveguides, thick and thin conductive coatings, etc. However, I just wanted to make sure I was on the right track, before I start learning something inconsistant.
Thanks for taking the time to go through this rather lengthy brain dump.
Attached you will find a brief PDF I was using as one reference. If anyone can recommend something better I'd appreciate it.
- Kirk
TL;DR: If someone could please confirm that this is right, (more details and thought process below) attenuation for thin-walled enclosures can be approximated by:
Attenuation [dB] = 20 log ( (?/2a)*(r/a) ) - 20 log (n[sup]1/2[/sup]);
Where:
? = wavelength
a = largest cross-sectional dimention of the aperture
r = distance of frequency source to aperture
n = number of similar apertures with edge-to-edge distances of less than ?/2
d = depth of the aperture (material thickness)
NB: s < ?/2 > a > d to be valid
Thank you,
- Kirk
My boss has asked me to put together a design reference for EM/RF sheilding for internal and external support. Unfortuately being a mechanical/aerospace engineer this is a little out of my league. If anyone would mind going over and critiquing what I have learned so far I would appriciate it.
EM/RF sheilding is used to isolate the component to prohibit interference from the environment to the component and vise-versa.
To isolate the component a conductive structure is required to "balence" internal and external charges.
A perfectly sealed Faraday cage would be the ideal solution, but is not always practical or desired.
The two main sources of leaks/losses are seams and apertures.
NB: Due to the similarity between apertures as "holes" and antenna apertures, for simplicity I will refer to "holes" from now on.
Seams are caused by the manufacturing process and can be treated with gaskets or specialized fabrication techniques such as double flanging to maximize contact area between the conductive materials.
Screws and other fasteners can be used to create discontinuties in seams to reduce losses.
Untreated seams can be considered as narrow, lengthy holes.
Holes in enclosures are required for cooling/ventalation, external access (power/data transfer), etc.
The exact geometrical shape of the hole is irrelevant to the losses occured (to a point).
Though different shapes can have unrelated benificial effects, ie honeycomb structures for airflow.
The largest of the cross-sectional (CS) dimensions of a hole is important.
If the holes have significant depth, ie the material is thick, or are coupled to tubes; the holes can be assumed to act as waveguides.
A waveguide will attenuate the signal of any signal below a certain cutt-off frequency.
The cutt-off frequency is approximately the frequency at which the largest CS dimension is equal to a half wavelength.
For waveguide-like holes a simple approximation of signal attenuation is:
Attenuation = C * (d/a) * sqrt( (1-(f/fc)[sup]2[/sup]) ) [ignore][dB][/ignore];
Where:
C = waveguide coefficient; Generally 30, rectangular hole 27, circular hole 32
d = depth of hole (material thickness or length of coupled tube)
a = largest CS dimension
f = frequency of the field
fc = cutt-off frequency
NB: this equation is only valid for waveguide like holes, ie d>>a
For thin-walled enclosures:
Wavelengths smaller than twice the largest CS dimension (2a) will not be attenuated.
Wavelengths equal to 2a will have 0dB shielding, inferring the cutt-off frequency to be:
fc = C/2a;
Where:
C = propogation velocity of an EM wave (ie speed of light)
For Wavelengths greater than 2a attenuation can be approximated via:
Attenuation [ignore][dB][/ignore] = 20 log(?/2d);
Where:
? = wavelength
NB: This is only valid for ?/2 > a > d
NB: Maximum attenuation is the attenuation of a solid barrier with no holes, aka faraday cage construction
NB: To neglect the effects of signal noice within the enclosure the component must be atleast distance, d, away from the enclousure
If you cannot place the component far enough away, then you can approximate the effect of signal noise:
fc = (C/2a)*(r/a);
Where:
r = distance to the hole
and
Attenuation [ignore][dB][/ignore] = 20 log(fc/f) = 20 log( (?/2a)*(r/a) )
If there are multiple similar holes and spaced closely together, ie s < ?/2, where s is the spacing between holes. The attenuation can be approximated by:
Attenuation [ignore][dB][/ignore] = 20 log(?/2) - 20 log(n[sup]1/2[/sup]);
Where:
n = number of holes
s < ?/2 > a > d
s = edge to edge hole spacing
Now there is a whole lot more to go through with: different arrays of holes, absorbtion loss of waveguides, thick and thin conductive coatings, etc. However, I just wanted to make sure I was on the right track, before I start learning something inconsistant.
Thanks for taking the time to go through this rather lengthy brain dump.
Attached you will find a brief PDF I was using as one reference. If anyone can recommend something better I'd appreciate it.
- Kirk