System and method for aircraft data transmission

Patent metadata

Field	Value
Publication number	US-11012146-B2
Application number	US-202016783244-A
Country	US
Kind code	B2
Filing date	Feb 6, 2020
Priority date	Feb 11, 2019
Publication date	May 18, 2021
Grant date	May 18, 2021

Abstract

A communication system and a method for transmitting data from an aircraft, the aircraft comprising at least one engine. A data collection and transmission unit is configured to collect and transmit data received from one or more locations in the aircraft, the data collection and transmission unit comprising at least one radio transmitter. At least one engine controller for the at least one engine is communicatively coupled to the data collection and transmission unit and configured to transmit, while the aircraft is airborne, engine data to the data collection and transmission unit, and, responsive to determining that the aircraft is on ground, cause the at least one radio transmitter to activate for transmitting the engine data from the data collection and transmission unit to at least one ground equipment.

First claim

The invention claimed is:

1. A communication system for transmitting data from an aircraft, the aircraft comprising at least one engine, the system comprising:
a data collection and transmission unit configured to collect and transmit data received from one or more locations in the aircraft, the data collection and transmission unit comprising at least one radio transmitter; and
at least one engine controller for the at least one engine, the at least one engine controller communicatively coupled to the data collection and transmission unit and configured to transmit, while the aircraft is airborne, engine data to the data collection and transmission unit, and, responsive to determining that the aircraft is on ground, cause the at least one radio transmitter to activate for transmitting the engine data from the data collection and transmission unit to at least one ground equipment, the at least one engine controller configured to prevent activation of the at least one radio transmitter, and accordingly prevent transmission of the engine data from the data collection and transmission unit to the at least one ground equipment, while the aircraft is in flight.

2. The system of claim 1 , wherein the at least one engine controller comprises an electrical switch controllable between an open position and a closed position and configured to, when in the closed position, connect the at least one radio transmitter to electrical ground.

3. The system of claim 2 , wherein the at least one engine controller is configured to bring the electrical switch to the closed position to cause the at least one radio transmitter to activate.

4. The system of claim 1 , wherein the at least one engine controller comprises an electrical switch controllable between an open position and a closed position and configured to, when in the closed position, supply electrical power to the at least one radio transmitter.

5. The system of claim 4 , wherein the at least one engine controller is configured to bring the electrical switch to the closed position to cause the at least one radio transmitter to activate.

6. The system of claim 1 , wherein the at least one engine controller is configured to output, to the data collection and transmission unit, a discrete control signal comprising instructions to activate the at least one radio transmitter.

7. The system of claim 1 , wherein the Design Assurance Level (DAL) associated with the at least one engine controller is higher than the DAL associated with the data collection and transmission unit, the at least one engine controller having a DAL of “A” and the data collection and transmission unit having a DAL lower than “C”.

8. The system of claim 7 , wherein the data collection and transmission unit is a DAL “E” certified device.

9. A computer-implemented method for transmitting data from an aircraft, the aircraft comprising at least one engine, the method comprising:
at at least one engine controller for the at least one engine,
transmitting, while the aircraft is airborne, engine data to a data collection and transmission unit of the aircraft; and
responsive to determining that the aircraft is on ground, causing at least one radio transmitter of the data collection and transmission unit to activate for transmitting the engine data from the data collection and transmission unit to at least one ground equipment, accordingly preventing activation of the at least one radio transmitter, and transmission of the engine data from the data collection and transmission unit to the at least one ground equipment, while the aircraft is in flight.

10. The method of claim 9 , wherein causing at least one radio transmitter of the data collection and transmission unit to activate comprises bringing an electrical switch of the at least one engine controller to a closed position, the electrical switch configured to, when in the closed position, connect the at least one radio transmitter to electrical ground.

11. The method of claim 9 , wherein causing at least one radio transmitter of the data collection and transmission unit to activate comprises bringing an electrical switch of the at least one engine controller to a closed position, the electrical switch configured to, when in the closed position, supply electrical power to the at least one radio transmitter.

12. The method of claim 9 , wherein causing at least one radio transmitter of the data collection and transmission unit to activate comprises outputting, to the data collection and transmission unit, a discrete control signal comprising instructions to activate the at least one radio transmitter.

Assignees

• Pratt & Whitney Canada

Inventors

• Fortin Frederic
• Jarvo James
• Miller Jonathan

Classifications

• H01Q1/28

  Adaptation for use in or on aircraft, missiles, satellites, or balloons · CPC title

• G07C5/008

  communicating information to a remotely located station (transmission systems for measured values G08C) · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• G07C5/0825

  using optical means · CPC title

• H04B7/18506 Primary

  Communications with or from aircraft, i.e. aeronautical mobile service · CPC title