c. marvin, m.p. robinson & j. f. dawson. university of york r. kebel. airbus

21
The Effects of Contents and Apertures on the Structure of Electromagnetic Fields in Enclosed Spaces A. C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Upload: prue

Post on 11-Jan-2016

26 views

Category:

Documents


2 download

DESCRIPTION

The Effects of Contents and Apertures on the Structure of Electromagnetic Fields in Enclosed Spaces. C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus. Introduction. - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

The Effects of Contents and Apertures on the Structure of Electromagnetic

Fields in Enclosed Spaces  

A. C. Marvin, M.P. Robinson & J. F. Dawson.

University of York

R. Kebel. Airbus

Page 2: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Introduction

• Current practise is to prohibit the use of carry-on electronic devices with antennas and to restrict the use of other carry-on electronic devices in aircraft cabins when the doors are closed.

• Evidence of interference to aircraft systems is cited as the reason for these restrictions.

Page 3: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Operating Issues

• As the number and variety of such devices increases, passenger acceptance of the restrictions is likely to decrease

• Passengers would welcome the facility to continue their communications and IT activities in flight

• Appropriate cabin design could make a seamless transition from the departure lounge to the cabin

Page 4: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Electromagnetic Issues

• Many electromagnetic systems already operate in aircraft; as long as they are “designed in” there need be no problem.

• Can other carry-on electromagnetic systems be incorporated?

• What is the electromagnetic environment in the aircraft cabin?

Page 5: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Electromagnetic Field Properties

• The aircraft cabin is a conducting tube with apertures and contents.

• Comparable studies on missile bodies (GENEC) are tractable using full-wave or intermediate level models.

• The scale of a passenger cabin makes either of these approaches difficult and a statistical approach is required.

Page 6: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Preliminary Measurements

• Press reports have speculated that the interior of trains with multiple mobile phone users may contain “hot spots” that could cause exposure above current ICNIRP limits and, by implication, EMC problems.

• We have undertaken preliminary measurements in a simulated cabin environment.

Page 7: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

The cabin environment!

The simulatedcabin is a Screened Room4.7m long witha cross-section of 2.37m by 3m.It holds nine passengers with business class spacing!

Page 8: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

The cabin environment!

Windows are simulated by blocks of AN79 absorber.

Page 9: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

A flying screened room!! (Shorts 330 G-BEEO)

Photo by Richard Hunt,UK

Page 10: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Frequency Response and Statistics of the Empty Cabin

9 9.02 9.04 9.06 9.08 9.1 9.12 9.14 9.16 9.18 9.2

x 108

-60

-55

-50

-45

-40

-35

-30

-25

-20

-15

-10

frequency (Hz)

S21

(dB

)

0 0.05 0.1 0.15 0.2 0.250

50

100

150

200

250

300

E (normalised)

n(E

)

Measured coupling between two roof mounted 50mm monopoles in the frequency range 900MHz to 920MHz

Page 11: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Frequency Response and Statistics with nine Passengers

9 9.02 9.04 9.06 9.08 9.1 9.12 9.14 9.16 9.18 9.2

x 108

-60

-55

-50

-45

-40

-35

-30

-25

-20

-15

-10

frequency (Hz)

S21

(dB

)

0.004 0.006 0.008 0.01 0.012 0.014 0.016 0.018 0.02 0.0220

20

40

60

80

100

120

140

160

180

200

E (normalised)

n(E

)

Nine passengers seated (green) and standing (red). Statistics are for seated passengers.

Page 12: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Simulated Results I

9 9.02 9.04 9.06 9.08 9.1 9.12 9.14 9.16 9.18 9.2

x 108

-55

-50

-45

-40

-35

-30

-25

-20

-15

frequency (Hz)

S21

(dB

)

Results of simulation of response of room, for various values of Q. Blue: Q=10000; green: Q=1000; red: Q=100.  

Page 13: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Simulated Results II

• The simulation was done by combining the frequency responses of all modes with resonant frequencies in the range 880-940MHz, with random phase differences between the modes, and random coupling coefficients. Compare these curves with the measured responses of the room. I estimate that the empty room has a Q of about 10000. Putting in the ‘windows’ brings the Q down to about 1000. Filling the room with ‘passengers’ brings the Q down to about 100.

Page 14: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Simulated Results III

• We have also done some rough calculations of these Q-factors, using a paper by D Hill for the windows and resonant perturbation theory for the passengers. These give contributions of Q3=2400 for the windows, and Q2 of somewhere between 3.7 and 720 for the passengers, depending on their orientation. These figures are of the right order of magnitude compared to the measurements.

•  The statistics are also similar to those of the measurements. The blue curve (Q=10000) has Rayleigh-like statistics, the red and green curves don’t.

Page 15: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Simulated Coupling to Transmission Line using TLM

(0,0,0)

boundaryblockfield

xz

y

Page 16: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Equivalent Intermediate Level Circuit Model

)1(wgV

)2(wgV

)1(wgI

)2(wgI

+

+

_

_

)1()1( ,cZ

)2()2( ,cZ

W

)1(T

)2(T

nearV farV

0z dz lowzz highzz

377

FSI

sourceV

)1(loop

)2(loop

)(Nloop

+

+

+

+

_

_

_

_

Page 17: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Near end coupling

-160

-140

-120

-100

-80

-60

-40

-20

0 500 1000 1500 2000 2500 3000

Rece

ived

Pow

er (d

Bm)

Frequency (MHz)

Circuit ModelTLM

Page 18: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Statistics of near end coupling (1.25-3GHz)

0

200

400

600

800

1000

1200

1400

0 0.0005 0.001 0.0015 0.002 0.0025 0.003

PDF

Peak Voltage (V)

Circuit ModelTLM

Page 19: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Concluding Remarks I

• Empty cabin with no windows responses follow the expected highly resonant behaviour of an over-moded cavity with Rayleigh like statistics.

• The inclusion of representative apertures and passengers gives substantial damping of the resonant behaviour and completely alters the field statistics.

Page 20: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Concluding Remarks II

• The average coupling levels between antenna pairs is reduced in the presence of loss mechanisms.

• The assertion that vehicle bodies will act as resonant cavities resulting in “hot spots” for fields from multiple sources is cast into doubt.

Page 21: C. Marvin, M.P. Robinson & J. F. Dawson. University of York R. Kebel. Airbus

Concluding Remarks III

• We have rather more to do in this study!