In one embodiment, a system (100) includes an aircraft body (105) and a propeller (110) coupled to the aircraft body (105) . The propeller (110) includes a plurality of blades forming a rearward-facing curvature with respect to an axis running longitudinally with the aircraft body (105). The system (100) further includes a surface (115) coupled to a first blade of the propeller (110) that is operable to reflect radio frequency (RF) waves.
ANTENNA SYSTEMS USING AIRCRAFT PROPELLERS
ANTENNENSYSTEME MIT FLUGZEUGPROPELLERN
SYSTÈMES D'ANTENNE UTILISANT DES HÉLICES D'AVIONS
2020-07-22
Patent
Electronic Resource
English
SAE Technical Papers | 1929
|Engineering Index Backfile | 1929
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