Systems and methods for energy conserving wireless sensing with situational awareness

• US 8,830,055 B2
• Filed: 10/14/2011
• Issued: 09/09/2014
• Est. Priority Date: 10/15/2010
• Status: Active Grant

• Current Assignee: Simmonds Precision Products, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Simmonds Precision Products, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Lynch, Michael A., Zakrzewski, Radoslaw R.
• Primary Examiner(s): Cheung, Calvin
• Assistant Examiner(s): HEINLE, COURTNEY D
• Application Number:
  US13/274,098
• Publication Number:
  US 20120095622A1
• Time in Patent Office: 1,061 Days
• Field of Search: 701/3, 701/29.1, 340/3.1, 340/539.22, 340/531, 340/539.3, 340/960, 340/945, 340/539.1, 737/63, 702/188, 244/75.1
• US Class Current: 340/539.3
• CPC Class Codes: B64C 25/00 Alighting gear air-cushion alighting gear B60V3/08
• CPC Class Codes: B64D 2045/008 Devices for detecting or indicating hard landing
• CPC Class Codes: B64D 45/0005 Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
• CPC Class Codes: G05B 23/0221 Preprocessing measurements, e.g. data collection rate adjustment; Standardization of measurements; Time series or signal analysis, e.g. frequency analysis or wavelets; Trustworthiness of measurements; Indexes therefor; Measurements using easily measured parameters to estimate parameters difficult to measure; Virtual sensor creation; De-noising; Sensor fusion; Unconventional preprocessing inherently present in specific fault detection methods like PCA-based methods
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C
• CPC Class Codes: G07C 5/08 Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

A system and method is provided for monitoring aircraft health and status using a situation-aware sensing system. The system includes an independent power source, a sensor that continuously measures a signal of interest to yield sensor data, and a processor that compares the sensor data to threshold data. The processor adjusts an operational parameter of the situation-aware sensing system to conserve power when the sensor data does not exceed the threshold data. The processor further adjusts the operational parameter of the situation-aware sensing system to stop conserving power when the sensor data exceeds the threshold data.

Claims

1. A situation-aware sensing system for aircraft monitoring comprising:

an independent power source;

a sensor that continuously measures a signal of interest to yield sensor data which is recorded and is indicative of an operational condition external to the system; and

a processor that compares the sensor data to a threshold based on an operational range of values for the operational condition external to the system, and adjusts an operational parameter of the situation-aware sensing system to conserve power when the sensor data does not exceed the threshold, wherein the processor adjusts the operational parameter to stop conserving power when the sensor data exceeds the threshold, and

wherein the sensor and the processor continuously draw power from the independent power source.

2. The system of claim 1, wherein the operational parameter includes a sampling rate and a data resolution.

3. The system of claim 1, further comprising:

a dependent power source; and

power management circuitry that switches the situation-aware sensing system from the independent power source to the dependent power source if aircraft power is present.

4. The system of claim 3, wherein the power management circuitry is further configured to recharge the independent power source when the aircraft power is present.

5. The system of claim 1, further comprising:

a memory, wherein the processor stores the sensor data in the memory when the sensor data exceeds the threshold data to yield an event record.

6. The system of claim 5, further comprising

a wireless transceiver;

and

an access point, and

wherein the processor transmits the event record from the memory to the access point, via the wireless transceiver.

7. The system of claim 1, wherein the threshold data includes an absolute value of a normal operating range of an aircraft, and a rate change in a measured value in time.

8. The system of claim 1, wherein the signal of interest is one selected from the group consisting of:

a temperature, a vibration, a strain, a pressure and an acceleration.

9. The system of claim 1, wherein the sensor is a first sensor, the system further comprising:

a second sensor that continuously measures a different signal of interest, wherein the processor further analyzes the different signal of interest throughout a period of time to determine if a transient condition is present, and

wherein the processor adjusts the operational parameter of the situation-aware sensing system to conserve power if the transient condition is present regardless of the threshold data.

10. The system of claim 9, wherein the second signal of interest is a vibration signal.

11. The system of claim 1, wherein when the processor adjusts the operational parameter to stop conserving power the processor causes the situation-aware sensing system to change between a low-power mode to a higher-energy mode.

12. A method for aircraft monitoring using situation-aware sensing comprising:

continuously drawing power from an independent power source;

continuously measuring a signal of interest to yield sensor data which is recorded and is indicative of an operational condition external to the system;

comparing the sensor data to a threshold based on an operational range of values for the operational condition external to the system;

adjusting an operational parameter of a situation-aware sensor to conserve power when the sensor data does not exceed the threshold; and

adjusting an operational parameter of the situation-aware sensor to stop conserving power when the sensor data exceeds the threshold.

13. The method of claim 12, further comprising:

continuously measuring a different signal of interest

comparing the different signal of interest to a period of time to determine if a transient condition is present;

adjusting an operational parameter of the situation-aware sensing system to conserve power if the transient condition is present regardless of the comparison of the sensor data to the threshold data.

14. The system of claim 12, wherein the operational parameter includes a sampling rate and a data resolution, wherein the threshold data includes an absolute value of a normal operating range of an aircraft and a rate of change in a measured value in time.

15. The system of claim 12 further comprising:

storing the sensor data in a memory when the sensor data exceeds the threshold data to yield an event record,

wirelessly transmitting the event record to an access point.

16. A situation-aware sensing system for aircraft monitoring comprising:

an independent power source;

a sensor that continuously measures a signal of interest to yield sensor data which is recorded and is indicative of an operational condition external to the system; and

a processor that is configured to adjust an operational parameter of the situation-aware sensing system to conserve power when the sensor data is within a first operational range and adjusts the operational parameter of the situation-aware sending system to stop conserving power when the sensor data is within a second operational range, wherein the first and second operational ranges are based on the operational condition external to the system.