DocumentCode :
1527754
Title :
Axial ratio of a curl antenna
Author :
Nakano, H. ; Mimaki, H.
Author_Institution :
Coll. of Eng., Hosei Univ., Tokyo, Japan
Volume :
144
Issue :
6
fYear :
1997
fDate :
12/1/1997 12:00:00 AM
Firstpage :
488
Lastpage :
490
Abstract :
The axial ratio of a curl antenna composed of vertical linear, horizontal linear, and curled sections is investigated using the method of moments. Axial ratio contours are presented for various values of antenna height h at a test (centre) frequency of 11.85 GHz. As the horizontal linear section length Lf increases, the number of curl turns n required for radiation of a circularly polarised (CP) wave decreases. It is also found that the ranges of choices for Lf and n for radiation of a CP wave becomes wider as the antenna height increases. Further calculations show that, as the antenna height increases: (i) the frequency bandwidth over which the axial ratio is less than 3 dB becomes wider, and (ii) the cross-polarisation component increases in a direction off the z-axis normal to the antenna plane, reducing the gain. A curl antenna of (height h, spiral constant asp , horizontal linear section length Lf, number of curl turns n, =4.6 mm, 0.26 mm/rad, 3.01 mm, 1.23 turns respectively) has a frequency bandwidth of 10.3% for a 3 dB axial ratio criterion, with a maximum gain of approximately 8 dB
Keywords :
antenna radiation patterns; electromagnetic wave polarisation; integral equations; method of moments; microwave antennas; wire antennas; 11.85 GHz; Pocklington type integral equation; antenna height; antenna radiation; axial ratio contours; centre frequency; circularly polarised wave; cross-polarisation component; curl antenna; curled section; frequency bandwidth; gain; horizontal linear section length; method of moments; vertical linear section; wire antennas;
fLanguage :
English
Journal_Title :
Microwaves, Antennas and Propagation, IEE Proceedings
Publisher :
iet
ISSN :
1350-2417
Type :
jour
DOI :
10.1049/ip-map:19971329
Filename :
649305
Link To Document :
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