IP Library Granted Patent US 12,150,061
Granted Patent B2
US 12,150,061 · App. 18/134,975 · Granted Nov 19, 2024

Aviation connectivity gateway module for remote data offload

Inventors: Matt Dondoneau (Horace, ND); Johan Wiig (Billancourt, FR); Ross Eickhoff (Fargo, ND); Andy Stromme (Billings, MT); Justin Koob (Harwood, ND); Bradley T. Cyr (Duluth, MN); Austin Matthew Murch (Esko, MN); David Andrew Rathbun (Hermantown, MN)
H04W52/0235H04W4/14H04W4/38H04W4/42H04W36/26H04W36/32H04W76/15H04W76/22H04W88/16
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Quick Facts
Patent No.
US 12,150,061
App. No.
18/134,975
Granted
Nov 19, 2024
Kind
B2
Abstract

An aviation connectivity gateway module for remote access to an aircraft's systems and remotely offloading its aircraft data. The module broadly comprises a CPU, a first set of communication elements, a second set of communication elements, a memory, a battery, an IMU, a GPS module, and a number of antennas. The module responds to remote prompts and offloads aircraft data when the aircraft is powered off. An aviation connectivity gateway module for complete BVLOS cellular network connectivity broadly comprises a CPU, a set of electronic connectors, a memory, an IMU, a GPS module, a first cellular connectivity element, a second cellular connectivity element, and a number of antennas. The module switches between the first cellular communication element and the second communication element based a status of the aircraft.

Claims (35)

1. An aviation connectivity gateway module for remotely offloading aircraft data from avionics of an aircraft, the avionics including a plurality of sensors, the aviation connectivity gateway module comprising:

a processor configured to receive a remote wake-up command when the avionics are in a powered off state and the aircraft is not flying, the remote wake-up command indicating an invocation to wake up and power on the avionics to obtain sensor readings from the sensors; and

a first communication element configured to communicatively couple the processor to the avionics when the processor receives the remote wake-up command;

a second communication element configured to communicatively couple the processor to a remote computing device; and

wherein the processor is further configured to:

power on the avionics when the processor receives the remote wake-up command;

obtain the aircraft data from the avionics when the avionics have been powered on; and

transmit the aircraft data to the remote computing device via the second communication element so as to remotely acquire aircraft data when the avionics are in the powered off state and the aircraft is not flying.

2. The aviation connectivity gateway module of claim 1 , further comprising:

a memory configured to store the aircraft data obtained from the avionics.

3. The aviation connectivity gateway module of claim 2 , wherein the processor is further configured to:

store the aircraft data on the memory when the avionics have been powered on, and

transmit the aircraft data from the memory to the remote computing device via the second communication element.

4. The aviation connectivity gateway module of claim 3 , wherein the aviation connectivity gateway module only transmits the aircraft data when the aircraft is not flying.

5. The aviation connectivity gateway module of claim 3 , wherein the aviation connectivity gateway module transmits the aircraft data in reverse order.

6. The aviation connectivity gateway module of claim 1 , wherein the aviation connectivity gateway module is configured to operate in an airborne mode, a ground mode, a sleep mode, a deep sleep mode, and a pilot data request mode, the aviation connectivity gateway module being configured to switch from the deep sleep mode to the pilot data request mode when the processor receives the remote wake-up command.

7. The aviation connectivity gateway module of claim 1 , wherein the remote wake-up command is in a Short Message Service (SMS) format.

8. The aviation connectivity gateway module of claim 1 , wherein the processor is further configured to selectively power on avionics components.

9. The aviation connectivity gateway module of claim 1 , wherein the aviation connectivity gateway module is configured to remotely install firmware and software updates to the avionics.

10. The aviation connectivity gateway module of claim 1 , wherein the aviation connectivity gateway module is configured to generate aircraft data independently from the avionics.

11. A method of remotely offloading aircraft data from avionics of an aircraft, the method comprising the steps of:

receiving, via a processor of an aviation connectivity gateway module, a remote wake-up command when the avionics are in a powered off state and the aircraft is not flying, the remote wake-up command indicating an invocation to wake up and power on the avionics to obtain sensor readings from sensors of the aircraft; and

powering on the avionics when the processor receives the remote wake-up command and the avionics are in the powered off state;

obtaining the aircraft data from the avionics; and

transmitting the aircraft data to a remote computing device so as to remotely acquire aircraft data when the avionics are in a powered off state and the aircraft is not flying.

12. The method of claim 11 , further comprising the steps of:

storing the aircraft data on a memory of the aviation connectivity gateway module; and

transmitting the aircraft data from the memory to a remote computing device.

13. The method of claim 12 , wherein the step of transmitting the aircraft data is only performed when the aircraft is not flying.

14. The method of claim 12 , wherein the step of transmitting the aircraft data includes transmitting the aircraft data in reverse order.

15. The method of claim 11 , wherein each step is performed in one of an airborne mode, a ground mode, a sleep mode, a deep sleep mode, and a pilot data request mode.

16. The method of claim 11 , wherein the remote wake-up command is in a Short Message Service (SMS) format.

17. The method of claim 11 , wherein the step of powering on the avionics includes selectively powering on avionics components.

18. The method of claim 11 , further comprising the step of remotely installing firmware and/or software updates to the avionics.

19. The method of claim 11 , further comprising the step of generating aircraft data independently from the avionics.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 12, 2025
From: CYR, BRADLEY T.; MURCH, AUSTIN MATTHEW; RATHBUN, DAVID ANDREW
To: CIRRUS DESIGN CORPORATION D/B/A CIRRUS AIRCRAFT
Reel/Frame 073200/0644 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 12, 2025
From: DONDONEAU, MATT; WIIG, JOHAN; EICKHOFF, ROSS; STROMME, ANDY; KOOB, JUSTIN
To: APPAREO SYSTEMS, LLC
Reel/Frame 073201/0013 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 12, 2025
From: APPAREO SYSTEMS, LLC
To: CIRRUS DESIGN CORPORATION D/B/A CIRRUS AIRCRAFT
Reel/Frame 073201/0123 →
Continuity (3)
Continuation 17104500 · Nov 25, 2020
Provisional Application 62941443 · Nov 27, 2019
Related Publication 20230254772A1 · Aug 10, 2023