Communications system using high altitude relay platforms

• US 20040102191A1
• Filed: 11/22/2002
• Published: 05/27/2004
• Est. Priority Date: 11/22/2002
• Status: Abandoned Application

• Current Assignee: Aerofon Corporation
• Original Assignee: Aerofon Corporation
• Inventors: Wander, David L., Pewitt, Nelson D.
• Application Number:
  US10/302,579
• Publication Number:
  US 20040102191A1
• Time in Patent Office: Days
• US Class Current: 455/431
• CPC Class Codes: H04B 7/18504 Aircraft used as relay or high altitude atmospheric platform

Abstract

A communications system includes a single stage, turbocharged, piston-powered aircraft that is positioned to fly in the lower stratosphere (41,000 ft.). A first link for the system is established between the aircraft and a subscriber on the ground, and a second link is established between the aircraft and a telecommunications base station. With the aircraft in position, communications between the subscriber and another party is then established over the first and second links, and through the base station.

Claims

1. A communications system for transferring signals between ground-based stations, said system having a stratospheric airborne link which comprises:

an airborne platform positioned at a predetermined altitude in the stratosphere, wherein said platform is a single stage, turbocharged, piston-powered aircraft;

at least one spot beam antenna mounted on said platform for sending a signal between a first ground-based station and said platform using a carrier in a first frequency range;

an airborne antenna mounted on said platform for passing said signal between said platform and a second ground-based station using a carrier in a second frequency range; and

a communications relay unit mounted on said platform for converting carrier frequencies for said signal between said first frequency range and said second frequency range, and for transferring said signal between said spot beam antenna and said airborne antenna to establish communications between said first and second ground-based stations.

2. A system as recited in claim 1 wherein said predetermined altitude is approximately forty-one thousand feet.

3. A system as recited in claim 1 wherein said aircraft is a manned vehicle.

4. A system as recited in claim 1 wherein said aircraft has a turbocharger with a compression ratio of approximately 6.0:

1.

5. A system as recited in claim 1 wherein said first frequency range includes radio (RF) frequencies between 1,850 MHz and 1.910 MHz, and wherein said second frequency range includes microwave (MW) frequencies between 3.7 GHz and 18 GHz.

6. A system as recited in claim 1 wherein said relay unit comprises:

a stage for off-setting frequencies to match each said spot beam antenna on said platform with a transceiver; and

a control channel for varying a power level of said signal in said first frequency range to compensate for movement of said platform.

7. A system as recited in claim 1 wherein said first ground station is a system subscriber.

8. A system as recited in claim 1 further comprising a base station which comprises:

a base antenna for communication with said airborne antenna on said platform;

a stage for off-setting frequencies to match each said spot beam antenna on said platform with a transceiver at said base ground station; and

a control channel for making adjustments to frequencies in said second frequency range.

9. A system as recited in claim 8 wherein said second ground-based station is connected to said base station and is a public switched telephone network.

10. A communications system for transferring signals between ground-based stations which comprises:

a first link for sending a signal between a first ground-based station and an airborne platform using a carrier frequency in a first frequency range, wherein said airborne platform is positioned at a predetermined altitude in the stratosphere, and wherein said platform is a single stage, turbocharged, piston-powered aircraft;

a second link for passing said signal between a second ground-based station and said airborne platform using a carrier frequency in a second frequency range; and

a means mounted on said airborne platform for converting carrier frequencies for said signal between said first frequency range and said second frequency range to interconnect said first link with said second link.

11. A system as recited in claim 10 wherein said predetermined altitude is approximately forty-one thousand feet.

12. A system as recited in claim 10 wherein said aircraft is a manned vehicle, and wherein said aircraft has a demand oxygen system and a turbocharger with a compression ratio of approximately 6.0:

1.

13. A system as recited in claim 10 wherein said first frequency range includes radio (RF) frequencies between 1,850 MHz and 1,910 MHz, and wherein said second frequency range includes microwave (MW) frequencies between 3.7 GHz and 18 GHz.

14. A system as recited in claim 10 wherein said first link interconnects a system subscriber at said first ground-based station with a spot beam antenna on said airborne platform, and wherein said second link interconnects a base station with an airborne antenna mounted on said platform.

15. A system as recited in claim 14 wherein said converting means is a relay unit and comprises:

a stage for off-setting frequencies to match each said spot beam antenna on said platform with a transceiver; and

a control channel for varying a power level of said signal in said first frequency range to compensate for movement of said platform.

16. A system as recited in claim 15 wherein said base station comprises:

a stage for off-setting frequencies to match each said spot beam antenna on said platform with a transceiver at said base ground station; and

a control channel for making adjustments to frequencies in said second frequency range.

17. A method for transferring signals between ground-based stations which comprises the steps of:

positioning an airborne platform at a predetermined altitude in the stratosphere, wherein said platform is a single stage, turbocharged, piston-powered aircraft;

sending a signal over a first link between a first ground-based station and said platform using a carrier in a first frequency range;

passing said signal over a second link between said platform and a second ground-based station using a carrier in a second frequency range; and

transferring said signal between said first link and said second link at said airborne platform to establish communications between said first and second ground-based stations.

18. A method as recited in claim 17 wherein said positioning step is accomplished at an altitude of approximately forty-one thousand feet.

19. A method as recited in claim 17 further comprising the step of converting carrier frequencies for said signal between said first frequency range and said second frequency range during said transferring step.

20. A method as recited in claim 19 further comprising the steps of:

off-setting frequencies to match a spot beam antenna in said first link with a transceiver in said second link;

varying signals in said first frequency range to compensate for movement of said platform; and

making adjustments to frequencies in said second frequency range in response to said varying step.