Propeller balancing using inflight data

Patent metadata

Field	Value
Publication number	US-10981675-B2
Application number	US-202016804715-A
Country	US
Kind code	B2
Filing date	Feb 28, 2020
Priority date	Mar 23, 2016
Publication date	Apr 20, 2021
Grant date	Apr 20, 2021

Abstract

The present disclosure provides methods and systems for propeller balancing of an aircraft comprising a propeller. Acceleration data is obtained from an acceleration sensor coupled to the aircraft. The acceleration data is filtered using a filter to obtain propeller-specific vibration data, the filter defining a range of acceptable frequencies associated with a frequency of rotation of the propeller. The propeller-specific vibration data is compared to trend data associated with the propeller. When the propeller-specific vibration data differs from the trend data beyond a predetermined threshold, an alert indicative of a balancing need for the propeller is issued.

First claim

The invention claimed is:

1. A method for propeller balancing of an aircraft comprising a propeller, the method comprising:
obtaining acceleration data from an acceleration sensor coupled to the aircraft;
filtering the acceleration data using a filter to obtain propeller-specific vibration data, the filter defining a range of acceptable frequencies associated with a frequency of rotation of the propeller;
comparing the propeller-specific vibration data to trend data, the trend data associated with the propeller and based on at least one previous light of the aircraft; and
when the propeller-specific vibration data differs from the trend data beyond a predetermined threshold, issuing an alert indicative of a balancing need for the propeller.

2. The method of claim 1 , wherein the filter is a bandpass filter, and wherein the range of acceptable frequencies defines a passband having a central frequency based on the frequency of rotation of the propeller.

3. The method of claim 2 , further comprising determining the central frequency by measuring the frequency of rotation of the propeller using a speed sensor associated with the propeller.

4. The method of claim 1 , wherein obtaining the acceleration data from the acceleration sensor comprises obtaining the acceleration data from an accelerometer coupled to an engine associated with the propeller.

5. The method of claim 1 , wherein issuing an alert comprises indicating that a maintenance operation is required.

6. The method of claim 1 , wherein issuing an alert comprises indicating a remaining flight time for the aircraft until a maintenance operation is required.

7. The method of claim 1 , further comprising:
storing the propeller-specific vibration data in a memory store; and
updating the trend data based on the propeller-specific vibration data.

8. The method of claim 7 , wherein updating the trend data comprises updating a rolling average of a vibration level associated with the propeller.

9. The method of claim 1 , further comprising discarding portions of the propeller-specific vibration data associated with a period of ground operation for the aircraft.

10. The method of claim 1 , wherein obtaining acceleration data comprises obtaining acceleration data sets for a plurality of flight stages during a flight mission, wherein filtering the acceleration data to obtain the propeller-specific vibration data comprises filtering the acceleration data sets to obtain vibration data sets, and wherein comparing the propeller-specific vibration data to the trend data comprises comparing the vibration data sets to trend data sets of the trend data associated with the plurality of flight stages.

11. A system for propeller balancing of an aircraft comprising a propeller, the system comprising:
a processing unit; and
a non-transitory computer-readable medium having stored thereon instructions executable by the processing unit for:
obtaining acceleration data from an acceleration sensor coupled to the aircraft;
filtering the acceleration data using a filter to obtain propeller-specific vibration data, the filter defining a range of acceptable frequencies associated with a frequency of rotation of the propeller;
comparing the propeller-specific vibration data to trend data, the trend data associated with the propeller and based on at least one previous flight of the aircraft; and
when the propeller-specific vibration data differs from the trend data beyond a predetermined threshold, issuing an alert indicative of a balancing need for the propeller.

12. The system of claim 11 , wherein filtering the acceleration data using the filter comprises using a bandpass filter, and wherein the range of acceptable frequencies defines a passband having a central frequency based on the frequency of rotation of the propeller.

13. The system of claim 12 , wherein the instructions are further executable for determining the central frequency by measuring the frequency of rotation of the propeller using a speed sensor associated with the propeller.

14. The system of claim 11 , wherein obtaining the acceleration data from the acceleration sensor comprises obtaining the acceleration data from an accelerometer coupled to an engine associated with the propeller.

15. The system of claim 11 , wherein issuing an alert comprises indicating that a maintenance operation is required.

16. The system of claim 11 , wherein issuing an alert comprises indicating a remaining flight time for the aircraft until a maintenance operation is required.

17. The system of claim 11 , wherein the instructions are further executable for:
storing the propeller-specific vibration data in a memory store; and
updating the trend data based on the propeller-specific vibration data.

18. The system of claim 17 , wherein updating the trend data comprises updating a rolling average of a vibration level associated with the propeller.

19. The system of claim 11 , wherein the instructions are further executable for discarding portions of the propeller-specific vibration data associated with a period of ground operation for the aircraft.

20. The system of claim 11 , wherein obtaining acceleration data comprises obtaining acceleration data sets for a plurality of flight stages during a flight mission, wherein filtering the acceleration data to obtain the propeller-specific vibration data comprises filtering the acceleration data sets to obtain vibration data sets, and wherein comparing the propeller-specific vibration data to the trend data comprises comparing the vibration data sets to trend data sets of the trend data associated with the plurality of flight stages.

Assignees

• Pratt & Whitney Canada

Inventors

• Wirth Richard Brian
• Winchcomb Robert
• Calvert Bruce
• Wigny Robert

Classifications

• B64D45/00

  Aircraft indicators or protectors not otherwise provided for · CPC title

• B64F5/40 Primary

  Maintaining or repairing aircraft · CPC title

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title

• B64D2045/0085

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

• B64C11/008

  characterised by vibration absorbing or balancing means · CPC title