Broadband unmanned aerial vehicle (UAV) patch antenna

Patent metadata

Field	Value
Publication number	US-10734716-B2
Application number	US-201816178772-A
Country	US
Kind code	B2
Filing date	Nov 2, 2018
Priority date	Nov 2, 2018
Publication date	Aug 4, 2020
Grant date	Aug 4, 2020

Abstract

Embodiments of the present disclosure relate to a UAV comprising a fuselage, a rotor, and a patch antenna element. The patch antenna element, which is provided from a patch antenna stack-up, is conformally disposed on an outer surface of the UAV's fuselage. The patch antenna comprises a first substrate, patch conductor, intermediate substrate, bottom substrate, and ground plane. The patch conductor is disposed on a top surface of the first substrate. A first surface of the intermediate substrate, which is a magneto-dielectric material, is disposed on a bottom surface of the first substrate. A top surface of the bottom substrate is disposed on a second surface of the intermediate substrate. A ground plane conductor is disposed on a bottom surface of the bottom substrate.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) comprising:
a fuselage having an inner surface and an outer surface;
at least one rotor coupled to said fuselage; and
a patch antenna element conformally disposed on the outer surface of said UAV fuselage in a recess of the outer surface having dimensions configured to receive the patch antenna element, said patch antenna element provided from a patch antenna stack-up comprising:
a first substrate having top and bottom opposing surfaces, the first substrate having a thickness of approximately 0.105 inches;
a patch conductor disposed on the top surface of said first substrate, the patch conductor comprising an array of a plurality of antenna elements;
an intermediate substrate having a first surface and a second opposing surfaces, with the first surface of said intermediate substrate disposed on the bottom surface of said first substrate, said intermediate substrate corresponding to a magneto-dielectric material, the intermediate substrate having a thickness of approximately 0.040 inches;
a bottom substrate having top and bottom opposing surfaces, with the top surface of said bottom substrate disposed on the second surface of said intermediate substrate, such that said intermediate magneto-dielectric substrate is provided as an inner layer in the patch antenna stack-up, the bottom substrate having a thickness of approximately 0.105 inches;
a ground plane conductor disposed on the bottom surface of said bottom substrate, the ground plane having a thickness of approximately 0.0014 inches; and
an adhesive surface coupled to the ground plane of the patch antenna element, thereby allowing the patch antenna element to be conformally disposed on and adhered to the outer surface of the fuselage,

wherein the patch antenna element is conformally disposed on the outer surface of the fuselage at a location based on one or more of: a location of a control station, an intended UAV travel direction, locations of other antenna systems on the UAV to prevent self-interference, location to reduce detection by enemy radar.

2. The UAV of claim 1 wherein the first and bottom substrates comprise a polytetrafluoroethylene (PTFE) material.

3. The UAV of claim 1 wherein the intermediate substrate comprises a magneto-dielectric material.

4. The UAV of claim 1 further comprising a feed circuit coupled to the patch antennal element.

5. The UAV of claim 1 wherein the feed circuit is a coaxial cable.

6. The UAV of claim 1 further comprising an interface configured to conformally dispose the patch antenna element on the outer surface.

7. The UAV of claim 1 wherein the patch antenna element is configured to form a datalink with a control station.

8. The UAV of claim 1 wherein the control station is a ground-based vehicle or platform and/or an aerial vehicle or platform.

9. The UAV of claim 1 wherein the patch antenna element is adhered to a rear side portion of the fuselage.

Assignees

• Raytheon Co

Inventors

• Wangsvick Chad
• Campbell Drew

Classifications

• B64U20/80

  Arrangement of on-board electronics, e.g. avionics systems or wiring · CPC title

• H01Q9/0414

  in a stacked or folded configuration · CPC title

• H01Q1/52

  Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure (absorbing means H01Q17/00) · CPC title

• H01Q1/48

  Earthing means; Earth screens; Counterpoises · CPC title

• H01Q1/286 Primary

  substantially flush mounted with the skin of the craft · CPC title