Aerial camera system, method for identifying route-related hazards, and microstrip antenna

• US 10,381,731 B2
• Filed: 11/21/2017
• Issued: 08/13/2019
• Est. Priority Date: 02/17/2014
• Status: Active Grant

• Current Assignee: GE Global Sourcing LLC (Westinghouse Air Brake Technologies Corporation)
• Original Assignee: GE Global Sourcing LLC (Westinghouse Air Brake Technologies Corporation)
• Inventors: DiDomenico, Dale Martin
• Primary Examiner(s): Williams, Howard
• Application Number:
  US15/819,877
• Publication Number:
  US 20180097288A1
• Time in Patent Office: 630 Days
• Field of Search: None
• CPC Class Codes: B61L 23/041 Obstacle detection
• CPC Class Codes: B61L 23/042 Track changes detection
• CPC Class Codes: B64C 1/36 adapted to receive antennas or radomes
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 47/08 Arrangements of cameras
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 50/37 Charging when not in flight
• CPC Class Codes: B64U 80/86 Land vehicles
• CPC Class Codes: G05D 1/0094 involving pointing a payload, e.g. camera, weapon, sensor, towards a fixed or moving target
• CPC Class Codes: G06V 20/13 Satellite images
• CPC Class Codes: G06V 20/17 taken from planes or by drones
• CPC Class Codes: G06V 20/56 exterior to a vehicle by using sensors mounted on the vehicle
• CPC Class Codes: H01Q 1/22 by structural association with other equipment or articles
• CPC Class Codes: H01Q 1/27 Adaptation for use in or on movable bodies H01Q1/08, H01Q1/12, H01Q1/18 take precedence
• CPC Class Codes: H01Q 9/0407 Substantially flat resonant element parallel to ground plane, e.g. patch antenna dipole H01Q9/285; monopole H01Q9/40
• CPC Class Codes: H04N 23/651 for reducing power consumption by affecting camera operations, e.g. sleep mode, hibernation mode or power off of selective parts of the camera
• CPC Class Codes: H04N 23/66 Remote control of cameras or camera parts, e.g. by remote control devices
• CPC Class Codes: H04N 23/661 Transmitting camera control signals through networks, e.g. control via the Internet
• CPC Class Codes: H04N 23/667 Camera operation mode switching, e.g. between still and video, sport and normal or high- and low-resolution modes
• CPC Class Codes: H04N 7/185 : from a mobile camera, e.g. for remote control

Abstract

An aerial device can be configured to fly above a route during movement of a vehicle along the route, such as for purposes of capturing image data of the route. The aerial device may include a microstrip antenna. The antenna includes a radiating patch layer, an aperture layer, a first insulator layer, a feed line, and a second insulator layer, all of which are parallel to and stacked on top of one another. The aperture layer is conductive and defines an aperture. The first insulator layer is sandwiched between the radiating patch layer and the aperture layer; thereby, the radiating patch layer and the aperture layer are spaced apart from one another by at least a thickness of the first insulator layer. The first insulator layer has a low dielectric constant. The second insulator layer is sandwiched between the aperture layer and the feed line.

Claims

1. An antenna comprising:

a radiating patch layer;

an aperture layer, wherein the aperture layer is conductive and defines an aperture;

a first insulator layer comprising a solid foam material sandwiched between the radiating patch layer and the aperture layer, wherein the radiating patch layer and the aperture layer are spaced apart from one another by at least a thickness of the first insulator layer, and wherein the first insulator layer has a low dielectric constant;

a conductive feed line;

a second insulator layer sandwiched between the aperture layer and the feed line;

a ground plane layer;

a third insulator layer sandwiched between the feed line and the ground plane layer, wherein the third insulator layer has a low dielectric constant, wherein the feed line extends from past a first outer edge of the aperture layer to past the aperture and terminates before a second outer edge of the aperture layer that is opposite the first outer edge; and

a radome covering at least the radiating patch layer,

wherein the radiating patch layer, the first insulator layer, the aperture layer, the second insulator layer, the conductive feed line, the third insulator layer, and the ground plane layer are all parallel to and stacked on top of one another.

2. The antenna of claim 1, wherein the first insulator layer has a dielectric constant of no more than 1.2.

3. The antenna of claim 2, wherein the third insulator layer has a dielectric constant of no more than 1.2 and comprises a same material as the solid foam material of the first insulator layer or a different solid foam material.

4. The antenna of claim 1, wherein the radiating patch layer and the aperture layer are spaced apart by at least 4 mm.

5. The antenna of claim 1, wherein the radiating patch layer, the aperture layer, and the ground plane layer are planar and have respective thicknesses of no more than 1/100 of a respective minimum cross dimension of the radiating patch layer, the aperture layer, or the ground plane layer.

6. The antenna of claim 1, wherein the antenna has a passive gain based on an area and a shape of the aperture of the aperture layer, and wherein the shape, normal to a major planar surface of the aperture layer, is one of a slot, a bowtie, an H-shape, an E-shape, or an hour glass.

7. The antenna of claim 6, wherein the passive gain is at least 10 dB.

8. The antenna of claim 1, wherein the feed line comprises a metal conductor having a long axis oriented transverse to an axis of the aperture.

9. The antenna of claim 8, wherein the aperture is a rectangular slot, and the axis of the aperture is a long axis of the rectangular slot, wherein the long axis of the aperture is oriented transverse to the long axis of the metal conductor of the feed line.

10. The antenna of claim 1, wherein the first insulator layer is adhered to the radiating patch layer by a first bonded layer and to the aperture layer by a second bonded layer, and the third insulator layer is adhered to the feed line by a third bonded layer and to the ground plane layer by a fourth bonded layer;

wherein the first bonded layer, second bonded layer, third bonded layer, and fourth bonded layer all have a respective low dielectric constant.

11. The antenna of claim 1, wherein the antenna has a polarity that has a difference of 10% or less when the antenna is oriented vertically versus being oriented horizontally.

12. The antenna of claim 1, wherein the antenna has a frequency bandwidth ranging from 5-50% octaves.

13. The antenna of claim 1, wherein the third insulator layer has a thickness corresponding to one-quarter of a wavelength of a frequency associated with the antenna.

14. The antenna of claim 1, wherein the feed line has a dimension corresponding to one-quarter of a wavelength of a frequency associated with the antenna.

15. The antenna of claim 1, wherein:

the radiating patch layer, the aperture layer, and the ground plane layer are planar and have respective thicknesses of no more than 1/100 of a respective minimum cross dimension of the radiating patch layer, the aperture layer, or the ground plane layer;

the radiating patch layer, the aperture layer, the first insulator layer, the conductive feed line, the second insulator layer, the ground plane layer, and the third insulator layer are all parallel to and stacked on top of one another;

the first insulator layer has a dielectric constant of no more than 1.2;

the third insulator layer has a dielectric constant of no more than 1.2 and comprises a same material as the solid foam material of the first insulator layer or a different solid foam material;

the radiating patch layer and the aperture layer are spaced apart by at least 4 mm;

the feed line comprises a metal conductor having a long axis oriented transverse to an axis of the aperture; and

the second insulator layer comprises a hydrocarbon ceramic laminate material.

16. A system, comprising:

an aerial vehicle configured to fly above a route;

a camera unit disposed onboard the aerial vehicle and configured to generate image data during flight of the aerial vehicle; and

a communication unit disposed onboard the aerial vehicle, the communication unit comprising the antenna of claim 1 and a transmitter, the communication unit configured to wirelessly communicate the image data to a location offboard the aerial vehicle.

17. An antenna comprising:

a radiating patch layer;

an aperture layer, wherein the aperture layer is conductive and defines an aperture;

a first insulator layer sandwiched between the radiating patch layer and the aperture layer, wherein the radiating patch layer and the aperture layer are spaced apart from one another by at least a thickness of the first insulator layer, and wherein the first insulator layer has a low dielectric constant;

a feed line that extends from past a first outer edge of the aperture layer to past the aperture and terminates before a second outer edge of the aperture layer that is opposite the first outer edge; and

a second insulator layer sandwiched between the aperture layer and the feed line, wherein the radiating patch layer, the first insulator layer, the aperture layer, the second insulator layer, and the feed line are parallel to and stacked on top of one another.

18. A system, comprising:

an aerial vehicle configured to fly above a route;

a camera unit disposed onboard the aerial vehicle and configured to generate image data during flight of the aerial vehicle; and

a communication unit disposed onboard the aerial vehicle, the communication unit comprising the antenna of claim 17 and a transmitter, the communication unit configured to wirelessly communicate the image data to a location offboard the aerial vehicle.

19. An antenna comprising:

a planar radiating patch layer, wherein the radiating patch layer is made of a first conductive metal;

a planar aperture layer, wherein the aperture layer is made of a second conductive metal and defines an aperture;

a first planar insulator layer sandwiched between the radiating patch layer and the aperture layer, wherein the radiating patch layer and the aperture layer are spaced apart from one another by at least a thickness of the first insulator layer, wherein the first insulator layer has a dielectric constant of no more than 1.5, and wherein there are no conductive elements disposed between the radiating patch layer and the aperture layer;

a conductive feed line, wherein a long axis of the conductive feed line is transverse to a long axis of the aperture, and wherein the feed line extends from past a first outer edge of the aperture layer to past the aperture, the feed line terminating before a second outer edge of the aperture layer that is opposite the first outer edge;

a second planar insulator layer sandwiched between the aperture layer and the feed line, wherein there are no conductive elements disposed between the feed line and the aperture layer, the second planar insulator layer comprises a hydrocarbon ceramic laminate material;

a planar ground plane layer made of a third conductive metal;

a third planar insulator layer sandwiched between the feed line and the ground plane layer, wherein the third insulator layer has a dielectric constant of no more than 1.5, and wherein there are no conductive elements disposed between the feed line and the ground plane layer; and

a radome covering at least the radiating patch layer,

wherein the radiating patch layer, the first insulator layer, the aperture layer, the second insulator layer, the conductive feed line, the third insulator layer, and the ground plane layer are all parallel to and stacked on top of one another.

20. The antenna of claim 19, wherein the aperture is rectangular, wherein the first planar insulator layer and the third planar insulator layer comprise a solid foam material, and wherein a thickness of the third planar insulator layer is equal to one-quarter of a wavelength of a frequency associated with the antenna.