Methods and systems to develop an experience-based probabilistic lifing process

• US 7,822,577 B2
• Filed: 08/15/2007
• Issued: 10/26/2010
• Est. Priority Date: 08/15/2007
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Sathyanarayana, Dileep, Eisenzopf, Peter J.
• Primary Examiner(s): Lau; Tung S
• Assistant Examiner(s): SUN, XIUQIN
• Application Number:
  US11/839,333
• Publication Number:
  US 20090048787A1
• Time in Patent Office: 1,168 Days
• Field of Search: 702/182, 702/184, 702/34, 701/29
• US Class Current: 702/182
• CPC Class Codes: G06F 2111/02 CAD in a network environment, e.g. collaborative CAD or distributed simulation
• CPC Class Codes: G06F 2111/08 Probabilistic or stochastic CAD
• CPC Class Codes: G06F 2119/04 Ageing analysis or optimisation against ageing
• CPC Class Codes: G06F 30/20 Design optimisation, verification or simulation optimisation, verification or simulation of circuit designs G06F30/30

Abstract

A method of facilitating a probabilistic lifting process is provided. The method includes obtaining operational data for at least one turbine engine, defining a plurality of cool-down curves for the at least one turbine engine, identifying a plurality of different start types of the at least one turbine engine, and developing a formula for the at least one turbine engine. The method also includes determining an operating strategy and establishing a design useful life for the at least one turbine engine, developing at least one histogram and a probabilistic model using the operational data, and determining a mission mix for the operating strategy by performing a simulation of the probabilistic model combined with cyclic life expenditure data of the at least one turbine engine.

Claims

1. A system for facilitating a probabilistic mission mix-based lifing process for turbine engine systems and sub-systems, said system comprising:

at least one computer configured as a server, said server containing a database, said server configured to;

store within said database operational data for at least one turbine engine, a plurality of cool-down curves for said at least one turbine engine, a plurality of different start types for said at least one turbine engine, at least one operating strategy and a design useful life of said at least one turbine engine;

analyze said operational data stored within said database;

develop at least one histogram and at least one probabilistic model using said operational data and store said at least one histogram and said at least one probabilistic model within said database;

determine a mission mix for said at least one operating strategy;

perform a simulation of said at least one probabilistic model combined with turbine engine cyclic life expenditure data of said at least one turbine engine;

obtain a probability distribution of a total cyclic life expenditure by extending a life expended over said design useful life of said at least one turbine engine; and

optimize a total turbine engine run-time.

2. A system in accordance with claim 1 wherein said server is further configured to determine a start temperature of said at least one turbine engine for the simulation using at least one of said plurality of cool-down curves.

3. A system in accordance with claim 1 wherein said server is further configured to calculate a life expended during said simulation using said turbine engine cyclic life expenditure data.

4. A system in accordance with claim 1 wherein said server is further configured to define a plurality of cold temperature starts of said at least one turbine engine, a plurality of warm temperature starts of said at least one turbine engine, and a plurality of hot temperature starts of said at least one turbine engine.

5. A system in accordance with claim 1 wherein said server is configured to optimize the total turbine engine run-time by changing a manner in which said at least one turbine engine is started when said total turbine engine run-time is less than said design useful life of said at least one turbine engine.

6. A system in accordance with claim 1 wherein said server is further configured to develop a model of the at least one turbine engine including actual turbine engine operating strategies and mission mix data such that all parameters effecting performance of the at least one turbine engine in the simulation are inherently considered.

7. An apparatus for facilitating a probabilistic mission mix-based turbine engine system and sub-system lifing process, said apparatus comprising:

means for storing operational data for at least one turbine engine, a plurality of cool-down curves for said at least one turbine engine, a plurality of different start types for said at least one turbine engine, at least one operating strategy and a design useful life of said at least one turbine engine;

means for analyzing said operational data stored within said database;

means for developing at least one histogram and at least one probabilistic model using said operational data and means for storing said at least one histogram and said at least one probabilistic model, wherein said means for developing at least one histogram comprise a means for optimizing a total turbine engine run-time;

means for determining a mission mix for said at least one operating strategy;

means for performing a simulation of said at least one probabilistic model combined with cyclic life expenditure data; and

means for calculating a life expended during said simulation using said cyclic life expenditure data.

8. An apparatus in accordance with claim 7 further comprising means for obtaining a probability distribution of a total cyclic life expenditure by extending a life expended over said design useful life.

9. An apparatus in accordance with claim 7 further comprising means for determining a start temperature of said at least one turbine engine for the simulation using at least one of said plurality of cool-down curves.

10. An apparatus in accordance with claim 7 wherein said means for optimizing a total turbine engine run-time comprise changing a manner in which said at least one turbine engine is started when the total turbine engine run-time is less than the design useful life of said at least one turbine engine.

11. An apparatus in accordance with claim 7 wherein means for determining a mission mix further comprises means for defining a plurality of cold temperature starts of said at least one turbine engine, a plurality of warm temperature starts of said at least one turbine engine, and a plurality of hot temperature starts of said at least one turbine engine.

12. An apparatus in accordance with claim 7 further comprising means for including actual turbine engine operating strategies and mission mix data such that all parameters effecting performance of the at least one turbine engine in the simulation are inherently considered.