Systems and methods for diagnosing engine components and auxiliary equipment associated with an engine
US-2015355054-A1 · Dec 10, 2015 · US
US2017328811A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017328811-A1 |
| Application number | US-201715664525-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 31, 2017 |
| Priority date | Feb 18, 2015 |
| Publication date | Nov 16, 2017 |
| Grant date | — |
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An abnormality diagnosing method includes a model generation step of generating a simulation model of a monitoring target, an operation start step of starting an operation of the monitoring target, a measurement step of measuring an internal state quantity in the operating state of the monitoring target and extracting a measured value, a prediction step of inputting into the simulation model same control input value used in the operating state of the monitoring target and calculating a predicted value of the internal state quantity of the monitoring target, a Mahalanobis distance calculation step of calculating a Mahalanobis distance from a difference between the measured value and the predicted value, and an abnormality diagnosis step of diagnosing whether the operating state of the monitoring target is abnormal based on the Mahalanobis distance.
Opening claim text (preview).
What is claimed is: 1 . An abnormality diagnosing method of diagnosing an abnormality of a monitoring target having an operating state that includes a non-steady state, the abnormality diagnosing method comprising: generating a simulation model of the monitoring target; measuring an internal state quantity in the operating state of the monitoring target and extracting a measured value; inputting into the simulation model same control input value used in the operating state of the monitoring target and calculating a predicted value of the internal state quantity of the monitoring target; calculating a Mahalanobis distance from a difference between the measured value and the predicted value; and diagnosing whether the operating state of the monitoring target is abnormal based on the Mahalanobis distance. 2 . The abnormality diagnosing method according to claim 1 , further comprising calculating an error vector that includes the difference and an integral value of the difference as components thereof. 3 . The abnormality diagnosing method according to claim 2 , wherein the calculating of the predicted value is made based on a measured value that was measured immediate previously in a time series. 4 . An abnormality diagnosing system for diagnosing an abnormality of a monitoring target having an operating state that includes a non-steady state, the abnormality diagnosing system comprising: a simulation model that simulates the monitoring target; a measuring unit configured to measure an internal state quantity in the operating state of the monitoring target; a diagnosing device that calculates a Mahalanobis distance from a difference between a predicted value calculated by the simulation model and a measured value extracted by the measuring unit and diagnoses whether the operating state of the monitoring target is abnormal based on the Mahalanobis distance; and a controlling unit configured to transmit same control input value to at least the monitoring target and the simulation model. 5 . The abnormality diagnosing system according to claim 4 , wherein the diagnosing device calculates the Mahalanobis distance based on an error vector that includes the difference and an integral value of the difference as components thereof. 6 . The abnormality diagnosing system according to claim 5 , wherein the simulation model calculates the predicted value based on a measured value that was measured immediate previously in a time series. 7 . The abnormality diagnosing system according to claim 4 , wherein the monitoring target is an engine for reusable spacecraft.
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