Air data probe replacement determination system

Patent metadata

Field	Value
Publication number	US-11422153-B2
Application number	US-202016752399-A
Country	US
Kind code	B2
Filing date	Jan 24, 2020
Priority date	Jan 24, 2020
Publication date	Aug 23, 2022
Grant date	Aug 23, 2022

Abstract

Method and systems of determining when to replace an air data probe are provided. The method includes estimating air data probe temperatures based at least in part on available vehicle sensor data; tracking an amount of time an estimated temperature of the heating element is within at least one temperature range; and providing an air data probe replacement indication when a replacement threshold is met that is at least in part based on reaching a cumulative amount of time the heating element has an estimated temperature within the at least one temperature range.

First claim

The invention claimed is:

1. A method of determining when to replace an air data probe, the method comprising:
estimating air data probe temperatures based at least in part on available vehicle sensor data used for an operation of a vehicle that includes the air data probe;
tracking an amount of time an estimated temperature of a heating element of the air data probe is within at least one temperature range; and
providing an air data probe replacement indication when a replacement threshold is met that is at least in part based on reaching a cumulative amount of time the heating element has an estimated temperature within the at least one temperature range.

2. The method of claim 1 , wherein the available vehicle sensor data includes at least one of weight on wheels data, engine total air temperature data, avionic total air temperature data, flight condition data, outside temperature data and air speed data.

3. The method of claim 1 , wherein estimating air data probe temperatures based on available vehicle sensor data further comprises:
selecting an estimated air data probe temperature from a priori look up table that includes estimated temperatures associated with vehicle sensor data.

4. The method of claim 1 , wherein the available vehicle sensor data is read off an avionic data bus.

5. The method of claim 1 , further comprising:
storing estimated temperatures verses time in a strip chart.

6. The method of claim 1 , wherein when more than one temperature range is used, the method further comprises:
applying a cumulated weighted system that tracks the usage and predicts the life expectancy of the air data probe based on temperatures of the heating element over time within each temperature range.

7. The method of claim 1 , further comprising:
adjusting the replacement threshold based at least in part on gathered data relating to the remaining life of the air data probe.

8. The method of claim 1 , further comprising;
generating a remaining life estimate based at least in part on the estimated temperature of the heating element and the tracked amount of time the heating element is within at least one temperature range.

9. The method of claim 1 , further comprising:
setting temperature ranges; and
associating a period of time of life expectancy with each temperature range.

10. A method of determining when to replace an air data probe, the method comprising:
estimating a temperature of at least one heating element of the air data probe from data read off of a data bus;
tracking time when the at least one heating element has a measured temperature within defined temperature ranges;
applying a cumulated weighted system that predicts the life expectancy of the air data probe based on the tracked time of the at least one heating element within each temperature range; and
generating a remaining life expectancy signal of the air data probe based on the prediction of the cumulated weighted system.

11. The method of claim 10 , further comprising:
setting the temperature ranges; and
associating a period of time of life expectancy with each temperature range.

12. The method of claim 10 , wherein applying a cumulated weighted system further comprises:
summing period of time of life expectancies over a length of time the at least one heating element can survive under a given temperature range across all temperature ranges.

13. The method of claim 10 , further comprising:
providing an air data probe replacement indication when a replacement threshold is met that is at least in part based on reaching a cumulative amount of time the heating element has an estimated temperature within the at least one temperature range.

14. The method of claim 10 , further comprising:
adjusting the replacement threshold based at least in part on gathered data relating to the remaining life of the air data probe.

15. An air data probe operating and monitoring system, the system comprising:
at least one heating element housed within an air data probe;
at least one clock;
at least one memory to store at least operating instructions;
at least one controller in operational communication with a data bus, the at least one controller configured to estimate a temperature of the air data probe based at least in part on data read off the data bus, the at least one controller further configured to implement the operating instructions in the at least one memory to track time that the at least one heating element of the air data probe has an estimated temperature within defined temperature ranges using the at least one clock, the at least one controller further configured to apply a cumulated weighted function that predicts the life expectancy of the air data probe based on an accumulated time the heating element is tracked within each temperature range; and
an output in communication with the at least one controller, the at least one controller configured to communicate a replace air data probe message to the output when a result of the cumulated weighted system reaches a select threshold.

16. The system of claim 15 , wherein the at least one controller is further configured to estimate the temperature of the at least one heating element by comparing the data read off the data bus with a priori look up table with estimated temperatures.

17. The system of claim 15 , wherein the at least one controller is further configured to sum a period of time of life expectancies over a length of time the at least one heating element can survive under a given temperature range across all temperature ranges in applying the cumulated weighted function.

18. The system of claim 15 , wherein the at least one controller is further configured to generate a remaining life expectancy signal that is communicated to the output.

19. The system of claim 15 , further comprising:
an input in communication with the at least one controller, the input configured to communicate the temperature ranges and an association of period of time of life expectancies with each temperature range to the at least one controller for storage in the at least one memory.

20. The system of claim 15 , wherein the at least one controller is further configured to update the temperature ranges and associated period of time of life expectancies with each temperature range.

Assignees

• Honeywell Int Inc

Inventors

• Gordon Grant A
• Sand Merle L
• Anderson Morris G

Classifications

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title

• G01K13/00

  Thermometers specially adapted for specific purposes · CPC title

• G01P5/165

  Arrangements or constructions of Pitot tubes · CPC title

• G01P5/10

  by measuring thermal variables · CPC title

• G06Q10/04

  Forecasting or optimisation specially adapted for administrative or management purposes, e.g. linear programming or "cutting stock problem" (market predictions or forecasting for commercial activities G06Q30/0202) · CPC title