Method for determining remaining useful life of turbine components

• US 5,042,295 A
• Filed: 05/29/1990
• Issued: 08/27/1991
• Est. Priority Date: 06/21/1985
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Seeley, Robert E.
• Primary Examiner(s): MYRACLE, JERRY
• Application Number:
  US07/528,891
• Time in Patent Office: 455 Days
• Field of Search: 73/117.3, 73/116, 364/431.02, 415/118
• US Class Current: 73/112.03
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles

Abstract

A method for determining the portion of life expended for a turbomachine component during a predetermined interval uses the rate at which creep strain accumulates to provide an indication of the portion of life expended.

Claims

1. A method for accumulating, in digital data processing circuits, a measure of cumulative component life damage D_T incurred by a turbomachine component during use in an environment wherein creep of material in the component is a major factor in determining remaining useful life of the component, said component exhibiting predetermined but changing rates of creep strain ξ

_k as a function of corresponding successive elapsed time intervals Δ

t_k at predetermined operating conditions after initiating each turbomachine cycle of operation, k being an integer 1,2, . . . n, said method comprising the steps of;

(a) for each of successive elapsed time intervals Δ

t_k when said predetermined operating conditions prevail, generating in digital data processing circuits an incremental measure of component life damage Δ

D_k equal to the ratio of the time interval Δ

t_k to a time-to-rupture t_rk for the rate of creep strain ξ

_k corresponding to time interval Δ

t_k ; and

(b) accumulating in said digital data processing circuits said incremental measures of component life damage Δ

D_k to generate therein said cumulative component life damage D_T.

2. The method of claim 1 wherein said predetermined but changing rate of creep strain for a given component are based on the known mass of said component operating at a predetermined angular velocity and temperature.

3. The method of claim 2 further including the step of:

selecting said predetermined but changing rates of creep strain corresponding to a particular said turbomachine component for use in said digital data processing circuits.

4. The method of claim 1 further including the steps of:

determining from said cumulative component life damage the remaining useful life of the component; and

removing said component from service when the determination indicates that substantially no useful life remains.

5. System apparatus for measuring cumulative component life damage to a turbomachine component employed in an environment wherein creep of material in the component is a major factor in determining the remaining useful life of the component, said component exhibiting predetermined but changing rates of creep strain, and hence correspondingly changing times-to-rupture, as a function of respectively corresponding successive elapsed time intervals at predetermined turbomachine component operating conditions, said apparatus comprising:

(a) means for detecting the occurrence of said predetermined operating conditions;

(b) means responsive to said detecting means for measuring said successive elapsed time intervals from each initial occurrence of said predetermined operating conditions so long as such operating conditions persist;

(c) means for generating an incremental measure of component life damage for each said elapsed time interval based on the predetermined rate of creep strain and time-to-rupture prevailing during such time interval; and

(d) means for generating a measure of cumulative component life damage by accumulating said incremental measures of component life damage.

6. System apparatus as in claim 5 wherein said means for detecting includes:

(e) means for measuring the angular velocity of said turbomachine component; and

(f) means for measuring the temperatures of said turbomachine component; and

7. System apparatus as recited in claim 5 wherein said predetermined rate of creep strain and time-to-rupture are dependent on the mass, angular velocity and temperature of said turbomachine component.

8. A method of measuring cumulative component life damage to a turbomachine component employed in an environment wherein creep of material in the component is a major factor in determining the remaining useful life of the component, said component exhibiting predetermined but changing rates of creep strain, and hence correspondingly changing times-to-rupture, as a function of respectively corresponding successive elapsed time intervals at predetermined turbomachine component operating conditions, said method comprising the steps of:

(a) detecting the occurrence of said predetermined operating conditions;

(b) measuring said successive elapsed time intervals from each initial occurrence of said predetermined operating conditions so long as such operating conditions persist;

(c) generating an incremental measure of component life damage for each said elapsed time interval based on the predetermined rate of creep strain and time-to-rupture prevailing during such time interval; and

(d) generating a measure of cumulative component life damage by accumulating said incremental measures of component life damage.

9. A machine system for accumulating a measure of cumulative component life damage D_T incurred by a turbomachine component during use in an environment wherein creep of material in the component is a major factor in determining remaining useful life of the component, said component exhibiting predetermined but changing rates of creep strain ξ

_k as a function of corresponding elapsed time intervals Δ

t_k at predetermined operating conditions after initiating each turbomachine cycle of operation, k being an integer 1,2 . . . n, said system comprising in combination;

(a) circuit means for generating an incremental measure of component life damage Δ

D_k for each of successive elapsed time intervals Δ

t_k when said predetermined operating conditions prevail, said incremental measure being equal to the ratio of the time interval Δ

t_k to a time-to-rupture t_rk for the rate of creep strain ξ

_k corresponding to time interval Δ

t_k ; and

(b) circuit means for accumulating said incremental measures of component life damage Δ

D_k to generate therein said cumulative component life damage D_T.

10. A method of measuring in situ the life expended for turbomachine component parts using digital data processing circuits to determine an indication of cumulative component part life damage incurred by cyclic use in an environment wherein creep of material in the component parts is a major factor in determining remaining useful life of the component parts, said parts exhibiting predetermined but changing rates of creep strain and correspondingly changing times-to-rupture, as a function of corresponding successive elapsed time intervals at predetermined temperature and velocity operating conditions, said method comprising the steps of:

detecting the occurrence of said predetermined temperature and angular velocity conditions;

measuring the successive elapsed time intervals upon the detection of each occurrence of said predetermined conditions;

generating an incremental measure of a particular component part life damage for each said elapsed time intervals based on the predetermined rate of creep strain and time-to-rupture for said particular part prevailing during such time interval;

generating a measure of cumulative component part life damage for said particular part by accumulating said incremental measures of component part life damage; and

generating a measure of the estimated remaining useful life of said particular component part.

11. The measuring method of claim 10 further including the step of removing said particular component part from service when the estimated remaining useful life indicates that substantially no useful life remains.