FREE SPACE LASER AND MILLIMETRE WAVE(MMW) NETWORK FOR AIRBORNE RELAY NETWORKS
First Claim
1. An aircraft system comprising:
- a first transceiver configured to transmit and receive radio signals in a first millimeter wave (mmW) frequency band via a first antenna;
a second transceiver configured to transmit and receive radio signals in a second mmW frequency band via a second antenna;
a processing unit configured to provide the data signals to the first and second transceivers for transmission and to receive demodulated signals from the first and second transceivers;
wherein the processing unit is further configured to output signals to alter the orientation of the first antenna to establish a first point-to-point connection with a first aircraft and to output signals to alter the orientation of the second antenna to establish a second point-to-point connection with a second aircraft;
the first point-to-point connection and the second point-to-point connection forming part of a point-to-point aircraft relay ring network communicatively coupling a plurality of aircraft in a shared flight route area to each other.
1 Assignment
0 Petitions
Accused Products
Abstract
An aircraft system comprises a first and second transceiver each configured to transmit and receive radio signals in respective first millimeter wave (mmW) frequency band and second mmW frequency band; and a processing unit configured to provide the data signals to the first and second transceivers for transmission and to receive demodulated signals from the first and second transceivers. The processing unit is further configured to output signals to alter the orientation of the first antenna to establish a first point-to-point connection with a first aircraft and to output signals to alter the orientation of the second antenna to establish a second point-to-point connection with a second aircraft; the first point-to-point connection and the second point-to-point connection forming part of a point-to-point aircraft relay ring network communicatively coupling a plurality of aircraft in a shared flight route area to each other.
52 Citations
24 Claims
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1. An aircraft system comprising:
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a first transceiver configured to transmit and receive radio signals in a first millimeter wave (mmW) frequency band via a first antenna; a second transceiver configured to transmit and receive radio signals in a second mmW frequency band via a second antenna; a processing unit configured to provide the data signals to the first and second transceivers for transmission and to receive demodulated signals from the first and second transceivers; wherein the processing unit is further configured to output signals to alter the orientation of the first antenna to establish a first point-to-point connection with a first aircraft and to output signals to alter the orientation of the second antenna to establish a second point-to-point connection with a second aircraft;
the first point-to-point connection and the second point-to-point connection forming part of a point-to-point aircraft relay ring network communicatively coupling a plurality of aircraft in a shared flight route area to each other. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A point-to-point aircraft relay ring network comprising:
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a plurality of aircraft flying in a flight route area; and one or more ground stations communicatively coupled to one or more of the plurality of aircraft; wherein each of the plurality of aircraft includes an aircraft system comprising; a receive antenna configured to receive radio signals in a first millimeter wave (mmW) frequency band; a receiver configured to demodulate radio signals received via the receive antenna; a transmitter configured to modulate data signals for transmission; a transmit antenna configured to direct radiated radio signals in a second mmW frequency band; a processing unit configured to provide the data signals to the transmitter for transmission via the transmit antenna and to receive the demodulated signals from the receiver; wherein the processing unit is further configured to output signals to alter the orientation of the transmit antenna to establish a first point-to-point connection with a respective first aircraft from the plurality of aircraft in the flight route area; wherein the processing unit is further configured to output signals to alter the orientation of the receive antenna to establish a second point-to-point connection with a respective second aircraft from the plurality of aircraft in the flight route area; wherein the first point-to-point connection and the second point-to-point connection form part of the point-to-point aircraft relay ring network communicatively coupling the plurality of aircraft together; wherein the processing unit in the aircraft system of at least one of the plurality of aircraft is configured to analyze signal characteristics of signals received via the respective receiver to determine weather conditions of the area through which the received signals passed. - View Dependent Claims (9, 10, 11, 12, 13, 14)
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15. A method of communicating data through an aircraft relay network, the method comprising:
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orienting a transmit antenna on a first aircraft to establish a first millimeter wave (mmW) point-to-point connection with a second aircraft; orienting a receive antenna on the first aircraft to establish a second mmW point-to-point connection with a third aircraft, the first mmW point-to-point connection and the second mmW point-to-point connection forming part of a point-to-point aircraft relay ring network communicatively coupling aircraft together; demodulating data received over the second mmW point-to-point connection; and modulating data for transmission over the first mmW point-to-point connection. - View Dependent Claims (16, 17, 18, 19, 20)
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21. An aircraft system comprising:
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a free space optical (FSO) transmitter configured to transmit optical signals through free space; an FSO receiver configured to receive optical signals through free space and convert the optical signals to electrical signals; a processing unit configured to provide the data signals to the FSO transmitter for transmission and to receive the electrical signals from the FSO receiver; wherein the processing unit is configured to output signals to alter the orientation of the FSO transmitter and FSO receiver in order to establish a point-to-point laser connection with another FSO transceiver located on another aircraft. - View Dependent Claims (22, 23, 24)
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Specification