Granted Patent B2

US 12,615,586 · App. 18/082,441 · Granted Apr 28, 2026

Inventors: Jeff Fischer (Duluth, MN); Brad Cyr (Duluth, MN); Doug Young (Duluth, MN)

Assignee: Cirrus Design Corporation

H04W48/18H04L43/0811H04W76/10H04W84/06

Abstract

Claims (66)

1 . An aircraft communication system comprising first and second communication modules, wherein:

the first communication module is configured to:

establish a first wireless data link with a first external communication network off the aircraft;

receive connection status information, wherein the connection status information is representative of availability of the second communication module to establish a second wireless data link with a second external communication network off the aircraft;

determine availability of the first and second data links, wherein the availability of the second data link is determined based upon the connection status information;

determine a highest priority data link of the first and second data links determined to be available;

couple one or more on-aircraft communication networks, including a wireless cabin communication network in a cabin of the aircraft, to the first external communication network via the first data link when the first data link is the highest priority data link; and

couple the one or more on-aircraft communication networks from the first communication module to the second communication module when the second data link is the highest priority data link; and

the second communication module is coupled to the first communication module, and is configured to:

establish the second wireless data link, and couple the one or more on-aircraft communication networks to the second external communication network via the second wireless data link, when the second wireless data link is the highest priority data link.

2 . The aircraft communication system of claim 1 , wherein the first and second external communication networks are different networks.

3 . The aircraft communication system of claim 1 , wherein:

the first communication module is configured to establish the first wireless data link with the first external communication network having a first cost basis; and

the second communication module is configured to establish the second wireless data link with the second external communication network having a second cost basis, and wherein one of the first and second cost bases is less than the other.

4 . The aircraft communication system of claim 1 , wherein the second communication module is configured to:

determine the availability of the second wireless data link; and

generate the connection status information based upon the determination of the availability of the second wireless data link.

5 . The aircraft communication system of claim 1 , wherein:

the one or more on-aircraft communication networks further comprises an aircraft avionics system;

the first communication module is coupled to the aircraft avionics system, and is configured to establish wireless communication between the aircraft avionics system and the first external communication network via the first wireless data link when the first wireless data link is the highest priority data link; and

the second communication module is coupled to the aircraft avionics system, and is configured to establish wireless communication between the aircraft avionics system and the second external communication network via the second wireless data link when the second wireless data link is the highest priority data link.

6 . The aircraft communication system of claim 1 , wherein the first communication module is further configured to store a record of priorities of the first and second wireless data links.

7 . An aircraft communication system for use in an aircraft including one or more on-aircraft communication networks, comprising:

a first communication module configured to establish communication with one or more external communication networks off the aircraft via one or more first module wireless data links; and

a second communication module configured to establish communication with one or more external communication networks off the aircraft via one or more second module wireless data links;

one or more connection detectors configured to determine availability of the one or more first module wireless data links and availability of the one or more second module wireless data links; and

a connection manager configured to:

store prioritization information associated with the one or more first module wireless data links and the one or more second module wireless data links;

determine a priority data link of the available one or more first module wireless data links and the available one or more second module wireless data links based upon the prioritization information;

when the priority data link is one of the one or more first module wireless data links, cause the first communication module to couple the one or more on-aircraft communication networks, via the priority data link of the first module wireless data links, to an associated external communication network; and

when the priority data link is one of the one or more second module wireless data links, cause the second communication module to couple the one or more on-aircraft communication networks, via the priority data link of the second module wireless data links, to an associated external communication network; and

wherein:

the one or more on-aircraft communication networks is coupled to the first communication module;

the communication system further comprises a data communication connection coupling the first communication module to the second communication module; and

when the priority data link is the one of the one or more second module wireless data links, the one or more on-aircraft communication networks are coupled to the second communication module via the data communication connection.

8 . The aircraft communication system of claim 7 , wherein:

at least one of the one or more first module data links is configured to establish wireless communication with a first external communication network; and

at least one of the one or more second module data links is configured to establish wireless communication with a second external communication network, and wherein the second external communication network is different than the first external communication network.

9 . The aircraft communication system of claim 7 , wherein:

the first communication module is configured to establish wireless communication with a first external communication network having a first cost basis; and

the second communication module is configured to establish wireless communication with a second external communication network having a second cost basis, and wherein one of the first and second cost bases is less than the other.

10 . The aircraft communication system of claim 7 , wherein:

the communication system further comprises a link status connection coupled between the connection manager and at least one of the one or more connection detectors configured to determine the availability of the one or more second module wireless data links;

the at least one of the one or more connection detectors configured to determine the availability of the one or more second module wireless data links provides a link status available signal to the connection manager via the link status connection when at least one of the one or more second module wireless data links is determined to be available; and

the connection manager causes the one or more on-aircraft communication networks to be coupled to the second communication module via the data communication connection in response to the link status available signal received via the link status connection.

11 . A method for controlling wireless communication between one or more on-aircraft communication networks, including a wireless cabin communication network, and a plurality of external communication networks by first and second communication modules, wherein the first communication module establishes wireless communication with one or more of the external communication networks via one or more first module data links, and the second communication module establishes wireless communication with one or more of the external communication networks via one or more second module data links, comprising:

determining availability of the one or more first module data links and the one or more second module data links;

determining a priority data link of the available one or more first module data links and the available one or more second module data links based upon a prioritization scheme;

causing the first communication module to couple one or more of the on-aircraft communication networks to one of the external communication networks via the priority data link when the priority data link is one of the first module data links; and

causing the second communication module to couple one or more of the on-aircraft communication networks to one of the external communication networks via the priority data link when the priority data link is one of the second module data links;

wherein:

the first communication module is coupled to the wireless cabin communication network;

the method further comprises providing link status information to the first communication module indicating status of availability of at least one of the second module data links;

determining availability of the second module data links includes determining availability based upon the link status information; and

causing the second communication module to couple one or more of the on-aircraft communication networks to one of the external communication networks includes (1) causing the wireless cabin communication network to be coupled to the second communication module via the first communication module, and (2) causing the second communication module to couple the wireless cabin communication network to one of the external communication networks via one of the second module data links.

12 . The method of claim 11 , wherein the method is performed by an electronic control system that is a component of one of the first and second communication modules.

13 . The method of claim 11 wherein the method is performed by an electronic control system that is a component of the first communication module.

14 . The method of claim 11 , wherein:

the first communication module is configured to establish wireless communication with at least a first external communication network; and

the second communication module is configured to establish wireless communication with at least a second external communication network that is different than the first external communication network.

15 . The method of claim 11 , wherein providing the link status information comprises providing the link status information from the second communication module to the first communication module.

16 . The method of claim 11 , wherein:

the one or more on-aircraft communication networks further comprises an aircraft avionics system, and wherein the aircraft avionics system is coupled to both the first and second communication modules; and

the method further comprises:

causing the first communication module to couple the aircraft avionics system to one of the external communication networks via one of the first module data links when the priority data link is one of the first module data links; and

causing the second communication module to couple the aircraft avionics system to one of the external communication networks via one of the second module data links when the priority data link is one of the second module data links.

Assignments (1)

Continuity (3)

References Cited (80)