RECONFIGURABLE AIRCRAFT COMMUNICATIONS SYSTEM WITH INTEGRATED AVIONICS COMMUNICATION ROUTER AND AUDIO MANAGEMENT FUNCTIONS

• US 20090298451A1
• Filed: 05/29/2008
• Published: 12/03/2009
• Est. Priority Date: 05/29/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Judd, Tom D., Malaga, Alfonso
• Granted Patent: US 8,019,338 B2
• Time in Patent Office: Days
• US Class Current: 455/129
• CPC Class Codes: H04B 1/40 Circuits
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

A reconfigurable radio communication subsystem is provided comprising a first radio communication unit communicatively coupled to a first antenna and a second antenna, and a second radio communication unit communicatively coupled to a third antenna and the first or second antenna. The first, second, and third antennas are operable in a first frequency band. The subsystem includes a first antenna subsystem coupled to the first radio communication unit and a fourth antenna operable in a second frequency band, and a second antenna subsystem coupled to the second radio communication unit and the fourth antenna. The first and second radio communication units include reconfigurable voice/data functions operating in the first frequency band, voice/data functions operating in the second frequency band, and a radio communications system management function. Cross-connecting buses couple the first radio communication unit and the second radio communication unit.

Claims

1. A reconfigurable radio communication subsystem, comprising:

a first radio communication unit communicatively coupled to a first antenna and a second antenna, the first and second antennas operable in a first frequency band;

a second radio communication unit communicatively coupled to a third antenna and either one of the first antenna or the second antenna, the third antenna operable in the first frequency band;

a first antenna subsystem communicatively coupled to the first radio communication unit and communicatively coupled to a fourth antenna operable in a second frequency band; and

a second antenna subsystem communicatively coupled to the second radio communication unit and communicatively coupled to the fourth antenna;

wherein the first and second radio communication units each include;

one or more reconfigurable voice/data functions operating in the first frequency band;

one or more voice/data functions operating in the second frequency band; and

a radio communications system management function,

wherein the first radio communication unit and the second radio communication unit each further include one of;

an avionics data communications router function;

an audio management function;

or

both the avionics data communications router function and the audio management function, and wherein cross-connecting buses communicatively coupled the first radio communication unit and the second radio communication unit.

2. The reconfigurable radio communication subsystem of claim 1, wherein the first frequency band is a very high frequency band, the second frequency band is a high frequency band,

wherein the first antenna, is a first very high frequency antenna, the second antenna is a second very high frequency antenna, the third antenna is a third very high frequency antenna and the fourth antenna is a high frequency antenna,

wherein the reconfigurable voice/data functions operating in the first frequency band are reconfigurable VHF radio functions,

wherein the voice/data functions operating in the second frequency band are HF radio functions, and

wherein the first antenna subsystem is a first high frequency antenna subsystem, and the second antenna subsystem is a second high frequency antenna subsystem.

3. The reconfigurable radio communication subsystem of claim 2, wherein the first and second radio communication units each further comprise:

two very high frequency transceivers at least one of which is communicatively coupled to at least one of the very high frequency antennas;

two very high frequency power amplifiers communicatively coupled to a respective one of the very high frequency transceivers; and

a high frequency transceiver communicatively coupled to the high frequency antenna.

4. The reconfigurable radio communication subsystem of claim 3, wherein the first and second radio communication units each further comprise a switch system that is communicatively coupled to the very high frequency power amplifiers in the respective radio communication units.

5. The reconfigurable radio communication subsystem of claim 4, wherein the first and second radio communication units each further comprise two digital signal processing modules each associated with a respective one of the very high frequency transceivers and each digital signal processing module associated with the high frequency transceiver.

6. The radio communication subsystem of claim 5, wherein the first and second radio communication units each further comprise:

an input/output module to interface the very high frequency functions and the high frequency functions of the first and second radio communication units via serial communication bus connections to the two digital signal processing modules in each of the first and second radio communication units, and wherein the input/output modules in the first and second radio communication units are communicatively coupled to each other via at least one point-to-point serial data bus; and

at least one power supply module to power the input/output module, the digital signal processing modules, the high frequency transceiver, the very high frequency transceivers, and the very high frequency power amplifiers.

7. The radio communication subsystem of claim 2, wherein the first and second antenna subsystems each comprise:

a high frequency coupler communicatively coupled with the high frequency antenna; and

a high frequency power amplifier communicatively coupled to a respective one of the first and second radio communication units.

8. A radio communication unit, comprising:

an avionics communication router;

two very high frequency transceivers at least one of which is communicatively coupled to at least one very high frequency antenna;

two very high frequency power amplifiers communicatively coupled to a respective one of the high frequency transceivers; and

a high frequency transceiver communicatively coupled to a high frequency antenna, wherein the avionics communication router routes data link messages received via the two very high frequency transceivers and the high frequency transceiver, the radio communication unit configured to send signals to and receive signals from another radio communication unit.

9. The radio communication unit of claim 8, further comprising:

a switch system that is communicatively coupled to the very high frequency power amplifiers.

10. The radio communication unit of claim 9, further comprising:

two digital signal processing modules each associated with a respective one of the very high frequency transceivers and each digital signal processing module associated with the high frequency transceiver.

11. The radio communication unit of claim 10, further comprising:

an input/output module to interface the very high frequency functions and the high frequency functions of the radio communication unit.

12. The radio communication unit of claim 11, further comprising:

at least one power supply module to power the input/output module, the digital signal processing modules, the high frequency transceiver, the very high frequency transceivers, and the very high frequency power amplifiers

13. The radio communication unit of claim 8, further comprising:

an audio management unit configured to deliver audio signals to and from communication system radios having multiple very high frequency functions and high frequency functions.

15. The radio communication unit of claim 8, further comprising:

a switch system that is communicatively coupled to the very high frequency power amplifiers.

16. The radio communication unit of claim 15, further comprising:

two digital signal processing modules each associated with a respective one of the very high frequency transceivers and each digital signal processing module associated with the high frequency transceiver.

17. The radio communication unit of claim 16, further comprising:

an input/output module to interface the very high frequency and high frequency functions of the radio communication unit.

18. The radio communication unit of claim 17, further comprising:

at least one power supply module to power the input/output module, the digital signal processing modules, the high frequency transceiver, the very high frequency transceivers, and the very high frequency power amplifiers

14. A radio communication unit, comprising:

an audio management unit configured to deliver audio signals to and from radios having multiple very high frequency functions and high frequency functions;

two very high frequency transceivers at least one of which is communicatively coupled to at least one very high frequency antenna;

two very high frequency power amplifiers communicatively coupled to a respective one of the high frequency transceivers; and

a high frequency transceiver communicatively coupled to a high frequency antenna, wherein the radio communication unit configured to send signals to and receive signals from another radio communication unit.

19. The radio communication unit of claim 14, further comprising:

an avionics communication router wherein the avionics communication router routes data link messages received via the two very high frequency transceivers and the high frequency transceiver.

20. The radio communication unit of claim 19, further comprising:

an input/output module to interface the very high frequency and high frequency functions of the radio communication unit; and

at least one power supply module to power the input/output module.