Predictive aircraft maintenance systems and methods incorporating classifier ensembles
First Claim
1. A method (100), executed on a predictive aircraft maintenance computer system (10), of determining a performance status of a selected component (24) in an aircraft (20), the method comprising:
- extracting (104), by the predictive aircraft maintenance computer system, feature data from flight data collected during a flight of the aircraft, wherein the feature data relates to performance of one or more components (24) of the aircraft;
applying (106), by the predictive aircraft maintenance computer system, an ensemble of related classifiers (66) configured to identify categories to which the feature data belong to produce a classifier indicator for each classifier of the ensemble of related classifiers, wherein each classifier is configured to indicate a category of the selected component of the aircraft within a given number of future flights, and wherein the given number for each classifier is different;
aggregating (108), by the predictive aircraft maintenance computer system, the classifier indicators to produce an aggregate indicator that indicates an aggregate category of the selected component for a threshold number of future flights, wherein the threshold number is greater than or equal to a maximum of the given numbers of the classifiers;
determining (110), by the predictive aircraft maintenance computer system, the performance status of the selected component relative to the threshold number of future flights based on the aggregate indicator; and
based on the performance status indicating a predicted impending non-performance event of the selected component, causing a maintenance schedule for the aircraft to be modified, wherein modifying the maintenance schedule comprises generating a schedule event to have the selected component repaired prior to the predicted impending non-performance event.
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Abstract
Predictive aircraft maintenance systems and methods are disclosed. Predictive maintenance methods may include extracting feature data from flight data collected during a flight of the aircraft, applying an ensemble of related classifiers to produce a classifier indicator for each classifier of the ensemble of classifiers, aggregating the classifier indicators to produce an aggregate indicator indicating an aggregate category of a selected component for a threshold number of future flights, and determining the performance status of the selected component based on the aggregate indicator. The classifiers are each configured to indicate a category of the selected component within a given number of flights. The given number of flights for each classifier is different. The threshold number of future flights is greater than or equal to the maximum of the given numbers of the classifiers. Predictive maintenance systems may include modules configured to extract feature data, classify feature data, and aggregate classifications.
23 Citations
20 Claims
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1. A method (100), executed on a predictive aircraft maintenance computer system (10), of determining a performance status of a selected component (24) in an aircraft (20), the method comprising:
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extracting (104), by the predictive aircraft maintenance computer system, feature data from flight data collected during a flight of the aircraft, wherein the feature data relates to performance of one or more components (24) of the aircraft; applying (106), by the predictive aircraft maintenance computer system, an ensemble of related classifiers (66) configured to identify categories to which the feature data belong to produce a classifier indicator for each classifier of the ensemble of related classifiers, wherein each classifier is configured to indicate a category of the selected component of the aircraft within a given number of future flights, and wherein the given number for each classifier is different; aggregating (108), by the predictive aircraft maintenance computer system, the classifier indicators to produce an aggregate indicator that indicates an aggregate category of the selected component for a threshold number of future flights, wherein the threshold number is greater than or equal to a maximum of the given numbers of the classifiers; determining (110), by the predictive aircraft maintenance computer system, the performance status of the selected component relative to the threshold number of future flights based on the aggregate indicator; and based on the performance status indicating a predicted impending non-performance event of the selected component, causing a maintenance schedule for the aircraft to be modified, wherein modifying the maintenance schedule comprises generating a schedule event to have the selected component repaired prior to the predicted impending non-performance event. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A predictive aircraft maintenance computer system (10) comprising:
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at least one processing unit (202); a computer-readable memory (206) storing non-transitory computer-readable instructions (220) that, when executed by the at least one processing unit, cause the predictive aircraft maintenance computer system to; extract feature data from flight data collected during a flight of an aircraft (20), wherein the feature data relates to performance of one or more components of the aircraft; produce a classifier indicator for each classifier of an ensemble of related classifiers (66), wherein each classifier is configured to indicate a category of a selected component (24) of the aircraft within a given number of future flights based upon the feature data, and wherein the given number for each classifier is different; produce an aggregate indicator that indicates a performance category of the selected component for a threshold number of future flights, wherein the threshold number is greater than or equal to a maximum of the given numbers of the classifiers; and modify, based on the aggregate indicator indicating a predicted impending non-performance event of the selected component, a maintenance schedule for the aircraft to have the selected component repaired prior to the predicted impending non-performance event. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification