IP Library Granted Patent US 10,352,824
Granted Patent B2
US 10,352,824 · App. 14/538,996 · Granted Jul 16, 2019

Method for evaluating turbine engine system stability

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Quick Facts
Patent No.
US 10,352,824
App. No.
14/538,996
Granted
Jul 16, 2019
Kind
B2
Abstract

Systems and methods for determining turbine engine system stability encompass measuring or otherwise determining values of performance parameters, storing a data set of such values in memory, generating a stability indicator, and displaying the stability indicator on an operator interface. The stability indicator is generated by a processor operating in data communication with the computer memory, utilizing customized software algorithms to remove high frequency components, apply an adaptive filter to adjust selected parameters according to a target value of a selected target parameter, and apply a stochastic filters to estimate true values of the selected parameters, based on the remaining variation.

Claims (41)

1. A method for turbine engine system stability, the method comprising:

operating a data acquisition computer processor with one or more sensors configured to measure performance parameters for operation of the turbine engine system;

determining values of the performance parameters for the turbine engine system, the performance parameters including independent parameters and dependent parameters forming a data set generated over a selected data acquisition period;

storing the data set in computer memory;

with the computer processor in communication with the computer memory:

removing high frequency components from the determined values of the performance parameters;

applying an adaptive filter to adjust the determined values of the dependent parameters according to a target value of a selected independent parameter, wherein the adaptive filter is corrected based on prior determined values of the performance parameters;

applying a stochastic filter to reduce noise in each of the determined values;

estimating true values of the dependent parameters, based on a remaining variation in the determined values; and

generating a stability indicator for the turbine engine system, based on variation in the estimated true values of the dependent parameters;

displaying the stability indicator on an operator interface in communication with the computer processor, and respectively:

validating the data set for the target value of the selected independent parameter in response to the stability indicator indicating stable operation of the turbine engine system over the selected data acquisition period, wherein a second target value of the selected independent parameter is selected and the stochastic filter is applied to adjust the determined values of the dependent parameters according to the second target value; or

invalidating the data set for the target value in response to the stability indicator indicating unstable operation of the turbine engine system over the selected data acquisition period, wherein additional data are required to validate the data set for the target value.

2. The method of claim 1 , wherein removing the high frequency components, applying the adaptive filter, applying the stochastic filter, estimating the true values and generating the stability indicator are performed in respective time order.

3. The method of claim 2 , wherein displaying the stability indicator comprises plotting the estimated true values of at least one selected independent or dependent parameter on the operator interface, over the selected data acquisition period.

4. The method of claim 1 , further comprising the computer processor advancing to the second target value based on the stability indicator, after validating the data set for the target value, and:

collecting a second data set of the performance parameters, wherein the stochastic filter is applied to adjust the determined values of the dependent parameters according to the second target value of the selected independent parameter; and

validating the second data set for the second target value of the selected independent parameter, in response to the stability indicator indicating stable operation of the turbine engine system over the second data set.

5. The method of claim 1 , wherein the stability indicator describes a change between different operational states of the turbine engine system within the selected data acquisition period, the different operational states characterized by different estimated true values of a selected dependent parameter.

6. The method of claim 1 , wherein the stability indicator describes a slope in the estimated true values of a selected dependent parameter, the slope characterized over the selected data acquisition period.

7. The method of claim 1 , wherein the stability indicator describes a jitter characterized by deviations in the estimated true values of a selected dependent parameter, over the selected data acquisition period.

8. The method of claim 1 , wherein the true values are estimated based on a difference between the determined values of the selected independent parameter and the target value, and further comprising updating the adaptive filter based on the difference.

9. The method of claim 8 , wherein the estimated true values describe thrust generated by the turbine engine system and the selected independent parameter describes a spool speed of the turbine engine system.

10. The method of claim 8 , wherein the estimated true values describe power or torque generated by the turbine engine system and the selected independent parameter describes a shaft speed of the turbine engine system.

11. The method of claim 1 , wherein applying a stochastic filter comprises recursively estimating a signal portion of the determined values in which the noise is reduced, using the determined values and previous estimates of the signal portion.

12. The method of claim 11 , wherein recursively estimating the signal portion comprises recursively applying the stochastic filter to the determined values of the performance parameters.

13. A non-transitory computer readable data storage medium having program code stored thereon, the program code executable by a data acquisition computer processor to perform a method comprising:

operating the data acquisition computer processor with one or more sensors configured to measure performance parameters of a turbine engine system;

determining values of the performance parameters in operation of the turbine engine system, the performance parameters forming a data set generated over a selected data acquisition period;

storing the data set in computer memory, and, with the computer processor in communication with the computer memory:

removing high frequency components from the determined values of the performance parameters;

applying an adaptive filter to adjust the determined values of a selected subset of the performance parameters according to a target value of a target parameter selected from the performance, wherein the adaptive filter is corrected based on prior determined values of the performance parameters;

applying a stochastic filter to reduce noise in each of the determined values;

estimating true values of the subset of performance parameters, based on a remaining variation in the determined values; and

displaying a stability indicator for the turbine engine on a graphical user interface in communication with the computer processor, the stability indicator indicating whether the turbine engine operated stably over the data set by characterizing variation in the estimated true values of the selected subset of performance parameters over the selected data acquisition period; and

validating the data set for the target value of the target parameter in response to the stability indicator indicating stable operation of the turbine engine system over the selected data acquisition period, wherein the stochastic filter is applied to adjust the determined values of the dependent parameters according to a second target value of the selected independent parameter; or

invalidating the data set for the target value of the target parameter in response to the stability indicator indicating stable operation of the turbine engine system over the selected data acquisition period, wherein additional data are required to validate the data set for the target value.

14. The data storage medium of claim 13 , wherein applying a stochastic filter comprises recursively applying the stochastic filter to the determined values of the performance parameters to estimate a signal portion in which the noise is reduced, using the determined values and previous estimates of the signal portion.

15. The data storage medium of claim 13 , wherein the selected subset of performance parameters describes a shaft speed or spool speed of the turbine engine and the target parameter describes thrust, torque or power output.

16. The data storage medium of claim 13 , the method further comprising the computer processor advancing to the second target value based on the stability indicator, after validating the first data set for the first target value.

17. The data storage medium of claim 16 , the method further comprising reducing a predetermined time scale or wait time between collecting the first and second data sets, using the stability indicator.

Assignments (19)
SECURITY INTEREST Recorded Jun 26, 2024
From: CALSPAN JETS LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 067851/0765 →
SECURITY INTEREST Recorded Jun 26, 2024
From: CALSPAN JETS LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 067851/0715 →
SECURITY INTEREST Recorded Jun 26, 2024
From: ADAMS RITE AEROSPACE, INC.; AMSAFE, INC.; CALSPAN JETS LLC; HARCOSEMCO LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 067851/0731 →
SECURITY INTEREST Recorded Jun 26, 2024
From: ADAMS RITE AEROSPACE, INC.; AMSAFE, INC.; CALSPAN JETS LLC; HARCOSEMCO LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 067851/0750 →
SECURITY INTEREST Recorded Jun 26, 2024
From: ADAMS RITE AEROSPACE, INC.; AMSAFE, INC.; CALSPAN JETS LLC; HARCOSEMCO LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.
To: GOLDMAN SACHS BANK USA
Reel/Frame 067851/0665 →
SECURITY INTEREST Recorded Jun 26, 2024
From: ADAMS RITE AEROSPACE, INC.; AMSAFE, INC.; CALSPAN JETS LLC; HARCOSEMCO LLC; MASON ELECTRIC CO.; PEXCO AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 067851/0704 →
RELEASE OF PATENT SECURITY AGREEMENT RECORDED JUNE 8, 2023 AT REEL/FRAME 063891/0803 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: MASON ELECTRIC CO.; TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROSONIC LLC; MOUNTAINTOP TECHNOLOGIES, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; SHIELD RESTRAINT SYSTEMS, INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS, INC.; AEROSONIC CORPORATION; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE INC.; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; PURE TECHNOLOGIES LTD.; HARCO LABORATORIES, INC.; HARCO LLC; HARCO TECHNOLOGIES CORPORATION; CORRPRO COMPANIES, INC.; HARCO CORPORATION; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL GMBH; TELAIR INTERNATIONAL AB; NORDISK AVIATION PRODUCTS AS; TURNTIME TECHNOLOGIES AB; AEROCONTROLEX GROUP, INC.; TRANSICOIL INC.; SOUTHCO, INC.; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS COMPANY; JOSLYN SUNBANK COMPANY LLC; LEACH INTERNATIONAL CORPORATION; SOURIAU USA, INC.; NMC GROUP, INC.; TA AEROSPACE CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; ROLLS-ROYCE PLC; MEMTRON TECHNOLOGIES CO.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.; AERO-INSTRUMENTS CO., LLC; AIRBORNE SYSTEMS NA, INC.; HARCOSEMCO LLC; HARCO, LLC (N/K/A HARCOSEMCO LLC); PEXCO AEROSPACE, INC.; TELAIR US LLC; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; ADAMS RITE AEROSPACE, INC.; ACME AEROSPACE, INC.; SCHNELLER, INC.; CEF INDUSTRIES, INC.
Reel/Frame 067640/0726 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 31, 2024
From: CALSPAN AERO SYSTEMS ENGINEERING LLC
To: CALSPAN JETS, LLC
Reel/Frame 067573/0143 →
CHANGE OF NAME Recorded May 1, 2024
From: CALSPAN AERO SYSTEMS ENGINEERING, INC.
To: CALSPAN AERO SYSTEMS ENGINEERING LLC
Reel/Frame 067301/0923 →
SECURITY INTEREST Recorded Nov 29, 2023
From: TRANSDIGM INC.; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; APICAL INDUSTRIES, INC.; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE, INC.; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; HARCO LABORATORIES, INCORPORATED (N/K/A HARCOSEMCO LLC); HARCO, LLC (N/K/A HARCOSEMCO LLC); HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PALOMAR PRODUCTS, INC.; PEXCO AEROSPACE, INC.; SCHNELLER LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; TACTAIR FLUID CONTROLS, INC.; TELAIR INTERNATIONAL LLC (N/K/A NORDISK AVIATION PRODUCTS LLC); TELAIR US LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC DEFENSE PRODUCTS CO.; NMC GROUP, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; KORRY ELECTRONICS CO.; MASON ELECTRIC CO.; AIRBORNE SYSTEMS NA INC.; HARCOSEMCO LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 065724/0903 →
SECURITY INTEREST Recorded Aug 22, 2023
From: TRANSDIGM INC.; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PALOMAR PRODUCTS, INC.; PEXCO AEROSPACE, INC.; SCHNELLER LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; TACTAIR FLUID CONTROLS, INC.; TELAIR INTERNATIONAL LLC (N/K/A NORDISK AVIATION PRODUCTS LLC); TELAIR US LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC DEFENSE PRODUCTS CO.; NMC GROUP, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; KORRY ELECTRONICS CO.; MASON ELECTRIC, CO.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 064661/0654 →
SECURITY INTEREST Recorded Jun 8, 2023
From: CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063891/0803 →
SECURITY INTEREST Recorded Jun 8, 2023
From: CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063891/0875 →
SECURITY INTEREST Recorded Jun 8, 2023
From: CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC
To: GOLDMAN SACHS BANK USA, AS AGENT
Reel/Frame 063891/0929 →
RELEASE OF SECURITY INTEREST Recorded May 10, 2023
From: KEYBANK NATIONAL ASSOCIATION
To: CALSPAN AERO SYSTEMS ENGINEERING, INC. (F/K/A/ AERO SYSTEMS ENGINEERING, INC.)
Reel/Frame 063596/0240 →
CHANGE OF NAME Recorded Jan 31, 2023
From: AERO SYSTEMS ENGINEERING, INC.
To: CALSPAN AERO SYSTEMS ENGINEERING, INC.
Reel/Frame 062592/0751 →
SECURITY INTEREST Recorded Sep 22, 2020
From: AERO SYSTEMS ENGINEERING, INC.
To: KEYBANK NATIONAL ASSOCIATION
Reel/Frame 053843/0730 →
SECURITY INTEREST Recorded May 9, 2017
From: ASE HOLDINGS, INC.; AERO SYSTEMS ENGINEERING, INC.; AS ACQUISITION, INC.
To: FIRSTBANK, AS ADMINISTRATIVE AGENT
Reel/Frame 042307/0912 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 21, 2015
From: LONG, DEAN FREDERICK; SIMON, KENNETH WILLIAM; RADINZEL, GRANT AUGUST
To: AERO SYSTEMS ENGINEERING, INC.
Reel/Frame 034767/0915 →