Broadband stacked multi-spiral antenna array integrated into an aircraft structural element
AssigneeThe Boeing Company
InventorsRonald O'Neil Lavin, Manny S. Urcia
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorsRonald O'Neil Lavin, Manny S. Urcia
Estimating the term…
A broadband stacked multi-spiral antenna array comprising two or more spiral antennas with a dielectric layer having a generally uniform thickness positioned between each pair of stacked antennas, which are all center-fed and in-phase. The antenna array may be embedded in a non-conductive material, such as fiberglass embedded in a resin, a honeycomb core sandwich, or structural foam, that may be used to form a structural element of a mobile platform. The structural element may include a via providing a pathway for coaxial cables. If two structural elements are hatch covers on the port and the starboard sides of an aircraft, the use of a stacked multi-spiral antenna array in each structural element provides two roughly hemispherical coverage patterns which together provide an omni-directional coverage pattern. The stacked multi-spiral antenna array may also include a reflecting cavity placed at the bottom of one of the spiral antennas.
A broadband stacked multi-spiral antenna array comprising:
A conformal broadband stacked multi-spiral antenna assembly for use in a mobile platform, the conformal broadband stacked multi-spiral antenna assembly comprising:
A method of forming a conformal integrated broadband stacked multi-spiral antenna assembly, comprising:
Dependencies are inferred from the claim text.