HIGH IMPACT ENERGY SENSOR

• US 20130317777A1
• Filed: 05/24/2012
• Published: 11/28/2013
• Est. Priority Date: 05/24/2012
• Status: Abandoned Application

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Codispoti, Benjamin, Lyttle, Charles Russ
• Application Number:
  US13/479,989
• Publication Number:
  US 20130317777A1
• Time in Patent Office: Days
• US Class Current: 702/141
• CPC Class Codes: B60R 21/01336 using filtering
• CPC Class Codes: B60R 21/0173 Diagnostic or recording means therefor
• CPC Class Codes: G01P 15/0891 with indication of predetermined acceleration values G01P15/135 takes precedence

Abstract

An impact energy sensor comprises a accelerometer, an analog signal filter, threshold circuitry, and a data processor. The analog signal filter is configured to filter signals from the accelerometer. The threshold circuitry is configured to output a non-zero threshold bit only in response to filtered signals from the accelerometer which exceed a specified sensitivity threshold. The data processor is configured to assess impact energy by accumulating threshold bits from the threshold circuitry, and is further configured to transmit an alarm message only if N or more threshold bits are accumulated within a time window of width T, where N and T are predetermined application-specific values.

Claims

1. An impact energy sensor comprising:

An accelerometer;

an analog signal filter configured to filter signals from the accelerometer;

threshold circuitry configured to output a non-zero threshold bit only in response to filtered signals from the accelerometer which exceed a specified sensitivity threshold; and

a data processor configured to assess impact energy by accumulating threshold bits from the threshold circuitry, and configured to transmit an alarm message only if N or more threshold bits are accumulated within a time window of width T, where N and T are application-specific values.

2. The impact sensor of claim 1, further comprising a built-in test processor configured to detect faults in the accelerometer.

3. The impact sensor of claim 2, wherein the built-in test processor is configured to monitor bias voltages on the accelerometer.

4. The impact sensor of claim 2, wherein the built-in test processor is configured to provide simulated built-in test patterns to the analog signal filter to verify that the data processor transmits alarm messages in response to appropriate shock events.

5. The impact sensor of claim 1, wherein the data processor reports alarm messages via interface circuitry including a controller area network bus.

6. The impact sensor of claim 1, wherein N and T are configurable parameters specific to a vehicle application.

7. The impact sensor of claim 1, wherein the alarm message is used to actuate emergency fire suppression or explosion inerting systems.

8. The impact sensor of claim 1, wherein accelerometer is a triaxial accelerometer, and the threshold circuitry compares an aggregated signal from all three axes of the triaxial accelerometer to an accelerometer reference value selected to exclude low-amplitude shocks.

9. The impact sensor of claim 1, wherein the accelerometer is a triaxial accelerometer, and the threshold circuitry compares a signal from each axis of the triaxial accelerometer to a corresponding accelerometer reference value selected to exclude low-amplitude shocks.

10. The impact sensor of claim 1, further comprising an amplifier which conditions signals from the analog signal filter with a preselected gain, and supplies the resulting amplified signal to the threshold circuitry.

11. A method for detecting high energy shock events with an impact energy sensor, the method comprising:

monitoring acceleration along three orthogonal axes using a triaxial accelerometer;

comparing outputs of the triaxial accelerometer to accelerometer sensitivity references;

generating threshold bits which are non-zero only if the outputs of the triaxial accelerometer exceed the accelerometer sensitivity references;

accumulating threshold bits over a time window of width T; and

transmitting an alarm notification if N or more non-zero threshold bits are accumulated within the time window.

12. The method of claim 11, wherein threshold bits are generated separately for each axis of the triaxial accelerometer.

13. The method of claim 11, wherein threshold bits are generated based on a comparison of the accelerometer sensitivity references with an aggregation of outputs of all three axes of the triaxial accelerometer.

14. The method of claim 11, further comprising identifying faults in the triaxial accelerometer with a built-in test processor.

15. The method of claim 14, wherein the built-in test processor checks bias voltages of the triaxial accelerometer for live voltages, and indicates a fault if any of the bias voltages are not live.

16. The method of claim 14, wherein the built-in test processor suppresses transmission of alarm messages when faults are detected, thereby allowing the triaxial accelerometer to be removed during operation of the impact energy sensor without alarm message transmission.

17. The method of claim 14, wherein the built-in test processor provides a simulated built-in test pattern which is used to verify that appropriate shock events trigger corresponding alarm notifications.

18. The method of claim 11, wherein the accelerometer sensitivity references are configurable during maintenance or operation of the impact energy sensor, and are specific to a particular vehicle application.

19. The method of claim 11, wherein values of T and N are configurable during maintenance or operation of the impact energy sensor, and are specific to a particular vehicle application.

20. The method of claim 11, further comprising actuating fire suppression or explosion inerting equipment in response to the alarm notification.