System and method of performing fan trim balancing

Patent metadata

Field	Value
Publication number	US-12297748-B2
Application number	US-202318123659-A
Country	US
Kind code	B2
Filing date	Mar 20, 2023
Priority date	Mar 20, 2023
Publication date	May 13, 2025
Grant date	May 13, 2025

Abstract

A control system for a turbine engine assembly includes a controller operable to control operation of the turbine engine assembly and to determine a trim configuration to balance a rotating engine structure associated with the turbine engine assembly. The controller is programmed to determine the trim configuration based on information indicative of an out of balance condition of the rotating engine structure and an assigning a quality score based on a determined veracity of the information.

First claim

What is claimed is:

1. A control system for a turbine engine assembly, the control system comprising:
a controller programmed to control operation of the turbine engine assembly and to determine a trim configuration to balance a rotating engine structure associated with the turbine engine assembly, the controller including a processor and a memory for storing information indicative of operation of the rotating engine structure, wherein the controller is programmed to determine the trim configuration by:
receiving information from one or more sensors within the turbine engine assembly that is indicative of an out of balance condition of the rotating engine structure, wherein the information includes a speed of a rotating engine structure, tracked vibration magnitude and a tracked vibration phase angle for the rotating engine structure;
analyzing data provided by the one or more sensors to determine a veracity of the provided data and assigning a quality score based on the determined veracity, wherein the determination of data veracity is based on a stability of a signal received from the one or more sensors, wherein sensor stability is a measure of a signal remaining constant for a predetermined time;
storing the information and the quality score as a data set in the memory that corresponds with one of a predefined number of engine operating ranges, wherein the predefined number of engine operating ranges comprise multiple ranges of engine rotational speeds;
providing a means of selecting one or more stored data sets for use in determining a trim configuration; and
generating a new trim configuration based on selected ones of the data sets.

2. The control system as recited in claim 1 , wherein the determination of data veracity is based, at least in part, on data corresponding with predefined conditions indicative of inaccurate data.

3. The control system as recited in claim 1 , further comprising replacing a previously stored data set with a subsequent data set assigned a better quality score.

4. The control system as recited in claim 1 , further comprising referring to stored information indicative of a current trim configuration when generating the new trim configuration.

5. The control system as recited in claim 4 , further comprising replacing the current trim configuration with the new trim configuration and saving the new trim configuration in the memory.

6. The control system as recited in claim 1 , wherein the means for selecting one or more of the dates sets comprises a visible display accessible to a maintenance operator.

7. A method of determining a trim configuration for balancing rotating engine structure with a controller configured to control operation of an engine, the method comprises:
operating an aircraft engine assembly to drive rotation of a fan by expanding a gas flow generated by combustion of a compressed airflow from a compressor with fuel in a combustor section;
receiving information with the controller from one or more sensors associated with the engine that is indicative of an out of balance condition of the rotating engine structure, wherein the information includes a speed of a rotating engine structure, tracked vibration magnitude and a tracked vibration phase angle for the rotating engine structure;
analyzing data provided by the one or more sensors to determine a veracity of the provided data and assigning a quality score based on the determined veracity, wherein the determination of data veracity is based on a stability of a signal received from the one or more sensors, wherein sensor stability is a measure of a signal remaining constant for a predetermined time;
storing the information and the quality score as a data set corresponding with one of a predefined number of engine operating ranges;
providing a means of selecting one or more stored data sets for use in determining a trim configuration; and
generating a new trim configuration based on the selected data sets.

8. The method as recited in claim 7 , wherein the predefined engine operating ranges comprise multiple ranges of engine rotational speeds.

9. The method as recited in claim 8 , wherein each data set includes a rotational speed, a tracked vibration magnitude and tracked vibration phase angle for a predefined duration for each range of engine rotational speeds.

10. The method as recited in claim 7 , wherein the determination of data veracity is based, at least in part, on a stability of a signal received from the one or more sensors.

11. The method as recited in claim 7 , wherein the determination of data veracity is based, at least in part, on data corresponding with predefined conditions indicative of inaccurate data.

12. The method as recited in claim 7 , further comprising replacing a previously stored data set with a subsequent data set assigned a better quality score.

13. The method as recited in claim 7 , further comprising referring to information stored in a memory associated with the controller that is indicative of a current trim configuration when generating the new trim configuration and replacing the current trim configuration with the new trim configuration in the memory.

14. The method as recited in claim 7 , wherein the means for selecting one or more of the dates sets comprises a visible display accessible to a maintenance operator and the method further comprises generating a visible and manipulatable display for viewing that includes features enabling selection of one of the stored data sets for use in generating the new trim configuration.

15. An engine assembly for an aircraft comprising:
at least one rotating engine structure, the at least one rotating engine structure including a plurality of locations configured to receive a weight element according to a determined trim configuration, wherein the at least rotating engine structure is part of at least one of a compressor section, turbine section and a fan section;
one or more sensor systems configured for measuring rotation of the at least one rotating engine structure and for generating signals indictive of balance conditions of the at least one rotating engine structure; and
a controller operable to control operation of the engine assembly and for determining the trim configuration, the controller including a processor and a memory for storing information indicative of operation of the rotating engine structure, wherein the controller is programmed to determine the trim configuration by:
receiving information from the one or more sensor systems associated with the engine assembly that is indicative of an out of balance condition of the at least one rotating engine structure, wherein the information includes a speed of a rotating engine structure, tracked vibration magnitude and a tracked vibration phase angle for the rotating engine structure;
analyzing the information provided by the one or more sensor systems to determine a veracity of the provided information and assigning a quality score based on the determined veracity, wherein the determination of data veracity is based on a stability of a signal received from the one or more sensors, wherein sensor stability is a measure of a signal remaining constant for a predetermined time;
storing the information and the quality score as a data set in the memory that corresponds with one of a predefined number of engine operating ranges;
providing a means of selecting one or more stored data sets for use in determining a trim configuration; and
generating a new trim configuration based on selected ones of the data sets.

16. The engine assembly as recited in claim 15 ,

Assignees

• Pratt & Whitney Canada

Inventors

• Chiasson Matthew
• Shaverdi Golnaz
• Tremblay Jason
• Riverin Guy
• Hafeez Faran
• Calvert Bruce

Classifications

• F01D21/003

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• F01D5/027

  Arrangements for balancing (for balancing rotating bodies in general F16F15/32; for compensating imbalance G01M1/36) · CPC title

• F01D5/26 Primary

  Antivibration means not restricted to blade form or construction or to blade-to-blade connections {or to the use of particular materials} · CPC title