Structural antenna for flight aggregates or aircraft
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Oct 21, 2003
Grant Date -
Jul 11, 2002
app pub date -
Nov 2, 2001
filing date -
Nov 2, 2000
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A folded microstrip antenna for a flight aggregate or aircraft can be arranged around edges of thin structural parts, such as wings, tail units or control flaps, such that its surface is identical with the structure and folding takes place at the edge of the structure. The antenna is constructed such that its characteristic impedance is much higher at the folding edge than at ends of the structural antenna away from the edge. As a result, an approximately omnidirectional characteristic can be achieved.
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