Methods and apparatus for assessing gas turbine engine damage
First Claim
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1. A method of assessing damage to machine components, said method comprising:
- calculating an expected parameter value based on a first parameter value indicator wherein the first parameter value indicator is responsive to a damage symptom;
calculating an estimate of an actual parameter value based on a second parameter value indicator wherein the second parameter value indicator is different than the first parameter value indicator and comprises calculating an estimate of an actual effective nozzle area using an estimator that computes at lease one of a linear function of the engine cycle data inputs, a neural network function of the engine cycle data inputs, and a nonlinear function of the engine cycle data inputs;
training the estimator using at least one of real engine data from an undamaged engine, real engine data from a damaged engine and simulated engine data from an undamaged engine, and simulated engine data from an undamaged engines;
determining if the calculated expected parameter value is different than the calculated estimate of the actual parameter value by a predefined limit; and
generating a damage flag based on a result of the comparison.
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Abstract
A method and apparatus for assessing damage to machine components is provided. The method includes calculating an expected parameter value based on a first parameter value indicator, calculating an estimate of an actual parameter value based on a second parameter value indicator, the second parameter value indicator being different than the first parameter value indicator, determining if the calculated expected parameter value is different than the calculated estimate of the actual parameter value by a predefined limit, and generating a damage flag based on a result of the comparison. The apparatus includes a computing device including a processor and a memory communicatively coupled to the processor, the processor programmed to execute a software product code segment that includes a detection boundary module, an estimator, and a comparator wherein the computing device is programmed to assess damage within an engine.
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Citations
2 Claims
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1. A method of assessing damage to machine components, said method comprising:
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calculating an expected parameter value based on a first parameter value indicator wherein the first parameter value indicator is responsive to a damage symptom;
calculating an estimate of an actual parameter value based on a second parameter value indicator wherein the second parameter value indicator is different than the first parameter value indicator and comprises calculating an estimate of an actual effective nozzle area using an estimator that computes at lease one of a linear function of the engine cycle data inputs, a neural network function of the engine cycle data inputs, and a nonlinear function of the engine cycle data inputs;
training the estimator using at least one of real engine data from an undamaged engine, real engine data from a damaged engine and simulated engine data from an undamaged engine, and simulated engine data from an undamaged engines;
determining if the calculated expected parameter value is different than the calculated estimate of the actual parameter value by a predefined limit; and
generating a damage flag based on a result of the comparison.
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2. A method of assessing damage to machine components, said method comprising:
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calculating an expected parameter value based on a first parameter value indicator wherein the first parameter value indicator is responsive to a damage symptom;
calculating an estimate of an actual parameter value based on a second parameter value indicator wherein the second parameter value indicator is different than the first parameter value indicator and comprises calculating an estimate of an actual effective nozzle area using an estimator that computes at lease one of a linear function of the engine cycle data inputs, a neural network function of the engine cycle data inputs, and a nonlinear function of the engine cycle data inputs;
calculating an estimate of an actual effective nozzle area using an estimator that includes a physics-based model of effective nozzle area that includes upstream parameter value indicators as inputs;
determining if the calculated expected parameter value is different than the calculated estimate of the actual parameter value by a predefined limit; and
generating a damage flag based on a result of the comparison.
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Specification
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Current AssigneeGeneral Electric Company
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Original AssigneeGeneral Electric Company
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InventorsWiseman, Matthew William
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Primary Examiner(s)LOUIS JACQUES, JACQUES H
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Application NumberUS10/376,510Publication NumberTime in Patent Office802 DaysField of Search701 34- 35, 701/99, 701/100, 701/29, 702186-187, 702 81- 84, 702182-185, 706 15- 16, 706 23- 25, 706912-915, 706 20- 21, 706903-907, 73112-113, 731/16, 731/172, 731/173, 731/181, 731/182, 714 25- 26, 714 47- 48, 60236-243, 602/33, 60770-773US Class Current701/100CPC Class CodesG05B 23/0218 characterised by the fault ...
