AVIONICS COMMUNICATION SYSTEM AND METHOD UTILIZING MULTI-CHANNEL RADIO TECHNOLOGY AND A SHARED DATA BUS

• US 20080084861A1
• Filed: 04/26/2007
• Published: 04/10/2008
• Est. Priority Date: 10/10/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hunter, Jeffrey K.
• Application Number:
  US11/740,566
• Publication Number:
  US 20080084861A1
• Time in Patent Office: Days
• US Class Current: 370/343
• CPC Class Codes: G08G 5/00 Traffic control systems for aircraft , e.g. air-traffic control [ATC]
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An avionics communication system and method uses multi-channel radios. The system includes a plurality of multi-channel radios and a processor in signal communication with the multi-channel radios that is capable of sending at least one signal to at least one of an audio panel or an avionics control computer based on applying predefined channel switching logic to the channels received by the multi-channel radios. The method includes receiving a first signal from a first multi-channel radio at a processor, receiving a second signal from a second multi-channel radio at the processor, and sending at least one signal from the processor to at least one of an audio panel or an avionics control computer based on applying predefined channel switching logic to the first and second signals. The receive and transmit function on a given channel need not be accomplished by the same radio.

Claims

1. A method for conducting radio frequency communications using an avionics system including a plurality of multi-channel radios, the method comprising:

receiving a first signal from a first multi-channel radio at a processor, the first signal corresponding to at least a first channel and a second channel;

receiving a second signal from a second multi-channel radio at the processor, the second signal corresponding to at least a third channel and a fourth channel; and

sending at least one signal from the processor to at least one of an audio panel or an avionics control computer based on predefined channel switching logic.

2. The method of claim 1, wherein the predefined channel switching logic is based on previously assigned channel priority levels.

3. The method of claim 2, wherein the predefined channel switching logic is also based on received signal strength levels.

4. The method of claim 2, further comprising receiving a channel selection input signal at the processor from the avionics control computer, wherein sending at least one signal from the processor is also based on the received channel selection input signal.

5. The method of claim 1, further comprising:

receiving a transmission signal at the processor from at least one of an audio panel or an avionics control computer; and

sending a control signal from the processor to at least one of the first and second multi-channel radios,

wherein the control signal contains information directing at least one of the first and second multi-channel radios to operate in a transmit mode.

6. The method of claim 1, wherein the first and second channels are the same as the third and fourth channels, respectively.

7. The method of claim 1, wherein the first and second signals are received using a data bus.

8. The method of claim 1, further comprising receiving a third signal from a third multi-channel radio at the processor, the third signal corresponding to at least a fifth channel and a sixth channel, wherein the at least one signal sent from the processor is based on application of the predefined channel switching logic to the first through sixth channels.

9. The method of claim 8, further comprising:

receiving a combined receive signal at a radio frequency (RF) power combiner/splitter;

splitting the combined receive signal with the RF power combiner/splitter to form a first raw receive signal and a second raw receive signal;

receiving the first raw receive signal at the second multi-channel radio; and

receiving the second raw receive signal at the third multi-channel radio,

wherein the second signal from the second multi-channel radio is based on the first raw receive signal and the third signal from the third multi-channel radio is based on the second raw receive signal.

10. The method of claim 9, further comprising:

receiving a first transmission signal at the processor from at least one of the audio panel or the avionics control computer;

placing a first transmission data signal based on the received first transmission signal on a data bus using the processor;

receiving the first transmission data signal using at least one of the first, second, or third multi-channel radios; and

emitting a first radio transmission signal based on the first transmission data signal from at least one of the multi-channel radios that received the first transmission data signal,

wherein emission of the first radio transmission signal and receiving a raw receive signal are not performed using the same multi-channel radio at the same time.

11. The method of claim 10, wherein the first transmission data signal is received using the second multi-channel radio, wherein the first radio transmission signal is emitted from the second multi-channel radio, and further comprising:

receiving a second transmission signal at the processor from at least one of the audio panel or the avionics control computer;

placing a second transmission data signal based on the received second transmission signal on the data bus using the processor;

receiving the second transmission data signal using the third multi-channel radio;

emitting a second radio transmission signal based on the second transmission data signal from the third multi-channel radio;

receiving the first and second radio transmission signals at the RF power combiner/splitter; and

emitting a combined radio transmission signal based on the first and second transmission signals from the RF power combiner/splitter.

12. An avionics communications system comprising:

a first multi-channel radio configured to receive at least a first channel and a second channel;

a second multi-channel radio configured to receive at least a third channel and a fourth channel; and

a processor in signal communication with the first and the second multi-channel radios, wherein the processor is configured to send at least one signal to at least one of an audio panel or an avionics control computer based on applying predefined channel switching logic to the first through fourth channels.

13. The system of claim 12, wherein the channel switching logic is based on previously assigned channel priority levels stored in the processor.

14. The system of claim 13, further comprising an avionics control computer in signal communication with the processor, the avionics control computer including an input device, wherein the avionics control computer is capable of sending a channel selection input signal to the processor based on user input received at the input device.

15. The system of claim 12 wherein the processor is capable of receiving a transmission signal from at least one of an audio panel or an avionics control computer, and wherein the processor is capable of sending a control signal containing information directing at least one of the first and second multi-channel radios to operate in a transmit mode to at least one of the first and second multi-channel radios.

16. The system of claim 12, wherein the first and second multi-channel radios are in signal communication with the processor over a data bus.

17. The system of claim 12, further comprising a third multi-channel radio configured to receive at least a fifth channel and a sixth channel, the third multi-channel radio in signal communication with the processor, wherein the processor is configured to send at least one signal to at least one of an audio panel or an avionics control computer based on applying predefined channel switching logic to the first through sixth channels.

18. The system of claim 17, further comprising a radio frequency (RF) power combiner/splitter in signal communication with the second multi-channel radio over a first connection and in signal communication with the third multi-channel radio over a second connection, wherein the RF power combiner/splitter is capable of receiving a combined receive signal and forming a first raw receive signal on the first connection and a second raw receive signal on the second connection

19. The system of claim 18, wherein the processor is capable of receiving a first transmission signal from at least one of the audio panel or the avionics control computer, wherein the processor is capable of placing a first transmission data signal based on the first transmission signal on a data bus connected to the first and second multi-channel radios, and wherein at least one of the multi-channel radios are capable of emitting a first radio transmission signal based on the first transmission data signal.

20. The system of claim 19, wherein the processor is capable of receiving a second transmission signal from at least one of the audio panel or the avionics control computer, wherein the processor is capable of placing a second transmission data signal based on the second transmission signal on the data bus, wherein at least one of the multi-channel radios are capable of emitting a second radio transmission signal based on the second transmission data signal, wherein the RF power combiner/splitter is capable of receiving the first and second transmission signals and is capable of emitting a combined transmission signal based on the first and second radio transmission signals.