Methods and apparatus to determine engine status with plenum measurements

Patent metadata

Field	Value
Publication number	US-12510439-B2
Application number	US-202318329150-A
Country	US
Kind code	B2
Filing date	Jun 5, 2023
Priority date	Jun 5, 2023
Publication date	Dec 30, 2025
Grant date	Dec 30, 2025

Abstract

A disclosed example non-transitory machine readable storage medium includes instructions to cause programmable circuitry to at least determine, based on output from at least one sensor, (i) a first parameter corresponding to a first position in a casing of a gas turbine engine, the first position at or downstream of a volume at which flows from respective ones of bleed offtakes are combined, and (ii) a second parameter corresponding to a second position in a casing of a gas turbine engine, the second position upstream from the first position, determine a status of at least one of the bleed offtakes or the at least one sensor based on the first and second parameters, and provide or indicate the status in response to the status indicating improper operation of at least one of the bleed offtakes or the at least one sensor.

First claim

What is claimed is:

1 . An apparatus comprising:
interface circuitry; and programmable circuitry to at least one of instantiate or execute machine readable instructions to:
determine, based on output from at least one sensor, at least one parameter corresponding to: (i) a first plenum in a casing of a gas turbine engine, the first plenum positioned at or downstream of a volume at which flows from respective ones of bleed offtakes of the gas turbine engine are combined, and (ii) a second plenum in the casing, the second plenum positioned upstream of the first plenum,
determine a status of at least one of the bleed offtakes or the at least one sensor based on the at least one parameter, and
provide or indicate a notification of the status in response to the status indicating improper operation of at least one of the bleed offtakes or the at least one sensor.

2 . The apparatus as defined in claim 1 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to cause the notification with a service alert to be transmitted based on the status indicating the improper operation of at least one of the bleed offtakes or the at least one sensor.

3 . The apparatus as defined in claim 1 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to compare the at least one parameter to at least one threshold to determine the status.

4 . The apparatus as defined in claim 1 , wherein first and second parameters are measured by the at least one sensor at the first plenum or the second plenum, respectively, and wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to compare at least one of the first or second parameters to output of at least one model to determine the status of the gas turbine engine.

5 . The apparatus as defined in claim 1 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to cause the gas turbine engine to operate at a reduced performance based on the status indicating the improper operation of at least one of the bleed offtakes or the at least one sensor.

6 . The apparatus as defined in claim 1 , wherein first and second parameters are measured by the at least one sensor at the first plenum or the second plenum, respectively, and wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to apply a first weight to the first parameter to define a weighted first parameter and apply a second weight to the second parameter to define a weighted second parameter, and wherein the determination of the status is based on the first and second weighted parameters.

7 . The apparatus as defined in claim 6 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to determine a weighted average of the first and second weighted parameters based on the first and second weighted parameters for determination of the status.

8 . The apparatus as defined in claim 1 , wherein first, second and third parameters are measured by the at least one sensor with respect to the first plenum or the second plenum, and wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to disregard at least one of first, second and third parameters when the at least one of first, second and third parameters exceeds a difference threshold with respect to an average of the first, second and third parameters.

9 . The apparatus as defined in claim 8 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to average ones of the first, second and third parameters that are not disregarded.

10 . The apparatus as defined in claim 9 , wherein the programmable circuitry is to at least one of instantiate or execute the machine readable instructions to determine a presence of ingestion in the gas turbine engine based on the averaged ones of the first, second and third parameters that are not disregarded.

11 . A non-transitory machine readable storage medium comprising instructions to cause programmable circuitry to at least:
determine, based on output from at least one sensor, (i) a first parameter corresponding to a first position in a casing of a gas turbine engine, the first position at or downstream of a volume at which flows from respective ones of bleed offtakes are combined; and (ii) a second parameter corresponding to a second position in the casing of the gas turbine engine, the second position upstream from the first position; determine a status of at least one of the bleed offtakes or the at least one sensor based on the first and second parameters, and provide or indicate a notification of the status in response to the status indicating improper operation of at least one of the bleed offtakes or the at least one sensor.

12 . The machine readable storage medium as defined in claim 11 , wherein the instructions cause the programmable circuitry to determine the status of the at least one bleed offtake of the gas turbine engine based on a comparison of the first and second parameters.

13 . The machine readable storage medium as defined in claim 11 , wherein the instructions cause the programmable circuitry to apply a first weight to the first parameter to define a weighted first parameter and a second weight to the second parameter to define a weighted second parameter, and wherein the determination of the status is based on summing the first and second weighted parameters.

14 . The machine readable storage medium as defined in claim 11 , wherein the instructions cause the programmable circuitry to determine third and fourth parameters measured by the at least one sensor at the first position or the second position.

15 . The machine readable storage medium as defined in claim 14 , wherein the third and fourth parameters correspond to the first position, and wherein the instructions cause the programmable circuitry to disregard at least one of the first, third and fourth parameters based on difference thresholds of the first, third and fourth parameters with respect to an average of the first, third and fourth parameters.

16 . The machine readable storage medium as defined in claim 14 , wherein the third and fourth parameters correspond to the second position, and wherein the instructions cause the programmable circuitry to disregard at least one of the second, third and fourth parameters based on difference thresholds of the second, third and fourth parameters with respect to an average of the second, third and fourth parameters.

17 . The machine readable storage medium as defined in claim 16 , wherein the second, third and fourth parameters correspond to temperatures of the second position, and wherein the instructions cause the programmable circuitry to determine a presence of ingestion in the gas turbine engine based on the temperatures of the second position, the status further indicating the presence of the ingestion.

18 . A method comprising:
determining, by executing instructions with processor circuitry, first and second parameters measured by at least one sensor, the first parameter corresponding to a first position in a casing of a gas turbine engine, the first position downstream of or at a volume at which flows from respective ones of bleed offtakes of the gas turbine engine are combined, and the second pa

Assignees

• Gen Electric

Inventors

• Miller Brandon W
• Hank Andrew J
• Schilling John C
• Roehm Ryan T
• Graziano Kevin
• Whitener Geoffrey

Classifications

• F01D21/003

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

• F05D2260/83

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

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• G01M15/14 Primary

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• G01M15/02 Primary

  Details or accessories of testing apparatus · CPC title