System and method for detecting vehicle system faults

Patent metadata

Field	Value
Publication number	US-9558601-B2
Application number	US-201514695081-A
Country	US
Kind code	B2
Filing date	Apr 24, 2015
Priority date	Apr 24, 2015
Publication date	Jan 31, 2017
Grant date	Jan 31, 2017

Abstract

A method for detecting vehicle system faults includes receiving, with a processor, a plurality of sensor signals from one or more sensors; thresholding, with the processor, the plurality of sensor signals for each respective sensor substantially in real time; and generating, with the processor, abnormal derivative frequency values for each of the plurality of thresholded sensor signals in real time and determining an operational status of at least each of the one or more sensors based on the abnormal derivative frequency values.

First claim

What is claimed is:

1. A method for detecting vehicle system faults, the method comprising:
detecting a predetermined characteristic of a vehicle with one or more sensors onboard the vehicle;
obtaining a plurality of sensor signals corresponding to the predetermined characteristic from the one or more sensors;
receiving, with a processor onboard the vehicle, the plurality of sensor signals from the one or more sensors onboard the vehicle;
thresholding, with the processor, the plurality of sensor signals for each respective sensor substantially in real time;
identifying transient instabilities in the dynamics of the plurality of sensor signals by generating, with the processor, abnormal derivative frequency values for each of the plurality of thresholded sensor signals in real time, where the transient instabilities are within a predetermined normal operating range of the one or more sensors, and determining an operational status of at least each of the one or more sensors based on the abnormal derivative frequency values identifying the transient instabilities; and

communicating the operational status of the one or more sensors to an operator or crew member of the vehicle.

2. The method of claim 1 , wherein the operational status of at least each of the one or more sensors includes a measure of health of a system in which the sensor is located.

3. The method of claim 1 , wherein the operational status of at least each of the one or more sensors includes a prognosis of a remaining useful life of a system in which the sensor is located.

4. The method of claim 1 , further comprising determining a plurality of thresholding parameters that are derived from vehicle system constraints and empirical observations of previously recorded sensor data from the one or more sensors, where the plurality of thresholding parameters effect thresholding the plurality of sensor signals for each respective sensor.

5. The method of claim 1 , wherein the processor determines the operational status of at least each of the one or more sensors in real-time.

6. The method of claim 1 , wherein the plurality of signals correspond to data acquisition and data communication in an aerospace, marine or land-based vehicle system with respect to an operational state of the aerospace, marine or land-based vehicle system.

7. The method of claim 1 , wherein determining an operational status of at least each of the one or more sensors includes
generating a time series of abnormal derivative frequency values; and
transforming the time series of abnormal derivative frequency values into abnormal derivative frequency vectors by time shifting, with overlapping time steps, a time window having a predetermined size across the time series of abnormal derivative frequency values.

8. The method of claim 1 , further comprising:
classifying the abnormal derivative frequency values for each of the plurality thresholded sensor signals as being normal or abnormal; and
predicting, based on classified abnormal derivative frequency values, an impending fault in a component of a system in which a respective one of the one or more sensors is located.

9. The method of claim 8 , further comprising thresholding, with the processor, the abnormal derivative frequency values for each of the plurality of thresholded sensor signals to effect classification of a respective abnormal derivative frequency value.

10. A fault detection system comprising:
one or more sensors onboard a vehicle, the one or more sensors being configured to detect a predetermined characteristic of the vehicle and generate a plurality of sensor signals corresponding to the predetermined characteristic;
a processor onboard the vehicle configured to receive the plurality of sensor signals from the one or more sensors;
a thresholding module of the processor configured to threshold the plurality sensor signals for each respective sensor in substantially real time; and
an abnormal derivative computation module of the processor configured to identify transient instabilities in the dynamics of the plurality of sensor signals by determining abnormal derivative frequency values for each of the plurality of thresholded sensor signals in substantially real time, where the transient instabilities are within a predetermined normal operating range of the one or more sensors,
wherein the processor is configured to determine an operational status of at least each of the one or more sensors based on the abnormal derivative frequency values and communicate the operational status of the one or more sensors to an operator or crew members of the vehicle.

11. The fault detection system of claim 10 , wherein the operational status of at least each of the one or more sensors includes a measure of health of a system in which the sensor is located.

12. The fault detection system of claim 10 , wherein the operational status of at least each of the one or more sensors includes a prognosis of a remaining useful life of a system in which the sensor is located.

13. The fault detection system of claim 10 , further comprising a threshold module connected to the processor and configured to determine a plurality of thresholding parameters that are derived from vehicle system constraints and empirical observations of previously recorded sensor data from the one or more sensors, where the plurality of thresholding parameters effect thresholding the plurality of sensor signals for each respective sensor.

14. The fault detection system of claim 10 , wherein the processor is configured to determine the operational status of at least each of the one or more sensors in real-time.

15. The fault detection system of claim 10 , wherein the plurality of signals correspond to data acquisition and data communication in an aerospace, marine or land-based vehicle system with respect to an operational state of the aerospace, marine or land-based vehicle system.

16. The fault detection system of claim 10 , further comprising an abnormal derivative vectoring module of the processor that is configured to
generate a time series of abnormal derivative frequency values; and
transform the time series of abnormal derivative frequency values into abnormal derivative frequency vectors by time shifting, with overlapping time steps, a time window having a predetermined size across the time series of abnormal derivative frequency values.

17. The fault detection system of claim 10 , further comprising a classification module of the processor configured to classify the abnormal derivative frequency values for each of the plurality of thresholded sensor signals as being normal or abnormal,
wherein the processor is configured to predict, based on classified abnormal derivative frequency values, an impending fault in a component of a system in which a respective one of the one or more sensors is located.

18. The fault detection system of claim 17 , wherein the processor is configured to threshold the abnormal derivative frequency values for each of the plurality of thresholded sensor signals to effect classification of a respective abnormal derivative frequency value.

19. A fault detection system comprising:
a plurality of sensors disposed in one or more vehicle systems of an aerospace, marine or land-based vehicle, each of the plurality of sensors being configured to detect a predetermined characteristics of the aerospace, marine or land-based vehicle and generate a plurality sensor signals corresponding to the predetermined characteristic; and
a processor in one or more of the

Assignees

• Boeing Co

Inventors

• Lu Tsai-Ching
• Martin Charles E
• Murphy Alice A
• Slaughter Stephen C
• Wezdenko Christopher R

Classifications

• G01D18/00 Primary

  Testing or calibrating apparatus or arrangements provided for in groups G01D1/00 - G01D15/00 · CPC title

• F02D2041/1432

  the system including a filter, e.g. a low pass or high pass filter · CPC title

• G07C5/02

  Registering or indicating driving, working, idle, or waiting time only (apparatus forming part of taximeters G07B13/00) · CPC title

• G01D21/02

  Measuring two or more variables by means not covered by a single other subclass · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title