Landing pylon

B - Operations – Transporting – 64 – F

Patent

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Details

240/56

B64F 1/18 (2006.01)

Patent

CA 2015859

LANDING PYLON Inventor: Reginald S. Bennett A B S T R A C T A truncated pyramidal pylon, has outwardly reflectant side walls each sloping at 8° - 10° to the vertical for helicopters and 3° - 6° to the vertical for fixed wing aircraft. The outwardly reflectant side walls are adapted to give a stronger reflection to an aircraft or helicopter on a desired approach path and a lesser but substantial reflection in other directions. The pylon may be constructed from hingedly connected flat surfaces with a surface corresponding to each side, foldable to provide the assembled pylon.

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