System and method to determine engine thrust of a taxiing aircraft

Patent metadata

Field	Value
Publication number	US-12399073-B2
Application number	US-202318158609-A
Country	US
Kind code	B2
Filing date	Jan 24, 2023
Priority date	Feb 16, 2022
Publication date	Aug 26, 2025
Grant date	Aug 26, 2025

Abstract

A computing device to determine engine thrust of an aircraft during taxiing. The computing device includes memory circuitry configured to store computer-readable program code. Processing circuitry is configured to execute the computer-readable program code to cause the computing device to: identify an aircraft on an airport surface; calculate an acceleration of the aircraft during the taxiing of the aircraft; compare the acceleration with predetermined data from similar aircraft; and based on the comparison, determine an engine thrust for the aircraft while the aircraft is taxiing.

First claim

The invention claimed is:

1. A method of determining engine thrust of an aircraft during taxiing, the aircraft comprising a number of engines, the method comprising:
identifying an aircraft on an airport surface;
calculating an acceleration of the aircraft during the taxiing of the aircraft;
comparing the acceleration of the aircraft to acceleration data of other aircraft with an equal number of engines, the acceleration data comprising clusters of data points with a number of clusters being the same as the number of engines and with each of the clusters of data points corresponding to a different engine thrust;
determining that the acceleration of the aircraft is aligned within one of the cluster of data points;
determining an engine thrust for the aircraft based on the cluster in which the acceleration coincides.

2. The method of claim 1 , wherein the comparing the acceleration with the acceleration data from similar aircraft comprises comparing the acceleration and a time period during taxiing of the aircraft with acceleration data and time period data for other aircraft each with a common manufacturer and model.

3. The method of claim 1 , comprising determining the number of engines on the aircraft based on an identified model of the aircraft.

4. The method of claim 3 , comprising identifying a model of the aircraft from records maintained at the airport.

5. The method of claim 3 , wherein for each of the engines, determining whether each of the engines is operating at a higher thrust level or a lower thrust level.

6. The method of claim 5 , wherein the lower thrust level is a zero thrust level.

7. The method of claim 1 , further comprising:
determining a starting point of the aircraft on the airport surface when the aircraft is stationary;
determining an ending point that is positioned away from the starting point with the aircraft moving along the airport surface at the ending point; and
calculating the acceleration based on a change in velocity between the starting and ending points and a time period for the aircraft to move between the starting and ending points.

8. The method of claim 1 , comprising determining the number of engines and a thrust level of each of the engines.

9. The method of claim 1 , wherein the acceleration data are stored at a monitoring node.

10. The method of claim 9 , wherein the monitoring node is selected from the group consistently essential of a control tower of an airport that monitors the overall operation of the airport, an airline that schedules the arrival and departure of aircraft, a flight tracker that monitors the status of flights, and a governmental unit.

11. A computer program product comprising a non-transitory computer-readable medium having computer-executable program code instructions that, when executed by a computing device, cause the computing device to:
identify an aircraft on an airport surface and determine a number of engines on the aircraft;
calculate an acceleration of the aircraft during the taxiing of the aircraft;
compare the acceleration with predetermined data from similar aircraft with an equal number of engines, the data comprising clusters of data points with each of the clusters corresponding to a different engine thrust;
determine that the acceleration of the aircraft corresponds to one of the clusters of data points; and
based on the comparison, determine the engine thrust for the aircraft while the aircraft is taxiing.

12. The computer program product of claim 11 , wherein the computing device is further configured to
determine that the aircraft is taxiing with the same number of engines and the same thrust levels as the cluster.

13. The computer program product of claim 11 , wherein the computing device is further configured to identify a model of the aircraft from records maintained at an airport.

14. The computer program product of claim 11 , wherein the calculating the acceleration of the aircraft comprises determining a change in velocity of the aircraft between first and second points along the airport surface relative to a time period for the aircraft to move between the first and second points with a velocity of the aircraft at the first point being zero.

15. The computer program product of claim 11 , wherein the computing device is further configured to obtain the data points from one or more remote entities that monitor other aircraft.

16. A computing device for determining engine thrust of an aircraft during taxiing, the computing device comprising:
memory circuitry configured to store computer-readable program code; and
processing circuitry configured to execute the computer-readable program code to cause the computing device to:
identify the aircraft by model and a number of engines of the aircraft;
identify a direction of travel of the aircraft;
determine an acceleration of the aircraft over a time period during taxiing of the aircraft;
compare the acceleration and the time period with predetermined data of other aircraft of the same model, the same direction of travel, and with the same number of engines and with the other aircraft having an acceleration over a time period during taxiing;
determine that the acceleration and time period is within a cluster of data points in the predetermined data with the cluster corresponding to an engine thrust for the aircraft; and
determine that the aircraft is taxiing with a same number of engines that are operating at same thrust levels as other aircraft from the corresponding cluster.

17. The computing device of claim 16 , wherein the processing circuitry calculates the acceleration between a first point where the aircraft is stationary and a second point where the aircraft is moving.

18. The computing device of claim 17 , wherein the processing circuitry calculates the acceleration during the time period with a velocity of the aircraft constantly increasing.

19. The computer program product of claim 11 , wherein the computing device is further configured to determine whether the engines on the aircraft are operating at a high thrust level or a low thrust level.

20. The computer program product of claim 19 , wherein the computing device is further configured to determine whether the engines are at a zero-thrust level.

Assignees

• Boeing Co

Inventors

• Cabos Ralf Rene
• Sakkas Spyridon

Classifications

• G08G5/51

  for control when on the ground, e.g. taxiing or rolling · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• G08G5/727

  from a ground station · CPC title

• B64D31/00

  Power plant control systems; Arrangement of power plant control systems in aircraft · CPC title

• G08G5/22

  located on the ground · CPC title