Monitoring a parameter with low power consumption for aircraft landing gear-data logger

• US 20060106582A1
• Filed: 04/28/2003
• Published: 05/18/2006
• Est. Priority Date: 04/26/2002
• Status: Active Grant

• Current Assignee: Messier-Dowty Incorporated (Safran SA)
• Original Assignee: Messier-Dowty Incorporated (Safran SA)
• Inventors: Schmidt, Robert Kyle
• Granted Patent: US 7,680,630 B2
• Time in Patent Office: Days
• US Class Current: 702/189
• CPC Class Codes: B64D 2045/008 Devices for detecting or indicating hard landing
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: G01D 9/005 Solid-state data loggers

Abstract

Apparatus for monitoring a parameter associated with a structural component comprises a module (1) which is attachable to the structural component and which is associated with a sensor (2) for making measurements of said parameter. The module incorporates a power supply (7) for powering the apparatus; a memory (4) for storing data from the sensor, and a processor (3) to process measurement signals from the sensor (2) and to store data in said memory (4). A display (5) for displaying measurements made by the sensor (2) may also be provided. The processor may make use of an algorithm such as a rainflow counting algorithm to reduce data stored. For energy saving, the sensor (2) is only powered on as required to take a measurement. The sensor (3) is interfaced to the processor through a signal processing subsystem (6) consisting of an amplifier and A to D converter, and each is turned on and off as required to power the sensor (2) for measuring. A sensor such as a tilt-switch (8) may also be used to control powering of the sensor (2). A communication link allows downloading of data from the memory, and recharging of the battery (7). Alternatively, the memory (4) and battery (7) are incorporated in a unit which is removable from the apparatus so that the data in the memory can be processed elsewhere.

Claims

1. An apparatus for monitoring a parameter associated with a structural component comprising a monitor which is attachable to the structural component and which incorporates a processor for receiving and processing measurement signals corresponding to said parameter from a sensor, a memory for storing data from said processor, and a power supply for powering operation of the processor and memory, wherein the memory and power supply are incorporated in the unit which is removable from the module.

2. An apparatus as claimed in claim 1 in which the processor makes use of an algorithm when processing the measurement signals so as to reduce the amount of data stored.

3. An apparatus as claimed in claim 2 in which the algorithm is a rainflow counting algorithm.

4. An apparatus as claimed in claim 1 in which the sensor is interfaced to the processor through a signal processing subsystem.

5. An apparatus as claimed in claim 4 in which the subsystem consists of an instrumentation amplifier to provide gain to the measurement signal, and an analogue-to-digital converter to convert the amplified analogue measurement signal to a digital signal compatible with the processor.

6. An apparatus as claimed in claim 5 in which each element in the subsystem is turned on and off as required to power on the sensor so as to take a measurement.

7. An apparatus as claimed in claim 1 including a sensor switch which determines when measurement do and do not need to be made.

8. An apparatus as claimed in claim 7 in which the sensor switch determines when a structural component in an aircraft landing gear is in a stowed condition.

9. An apparatus as claimed in claim 1 having a low power “

sleep”

mode of operation which it assumes under certain conditions.

10. An apparatus as claimed in claim 9 in which said certain conditions comprise when sensor measurements remain substantially constant.

11. An apparatus as claimed in claim 1 having a data port to allow downloading of data from the memory, and recharging of the battery at the same time.

12. An apparatus as claimed in claim 1 including display means which displays information about the structural component as well as data derived from measurements of the sensor.

13. An apparatus as claimed in claim 12 in which the display shows data derived over a period of time, or gives an indication of the function, status or performance of the component such as its fatigue life or remaining service life.

14. An apparatus as claimed in claim 1 including a sensor to measure said parameter.

15. An apparatus as claimed in claim 14 in which the sensor is incorporated into the module.

16. A monitoring system comprising multiple modules for monitoring parameters associated with different parts of a structure, each module being as claimed in claim 1 and having associated with it a sensor for making measurements of one of said parameters.

17. The system as claimed in claim 16 which includes additional sensor producing inputs determined by other aspects of the structure, such as the operating system of a vehicle or aircraft.

18. An apparatus as claimed in claim 12 in which the display means comprises an LCD display.

19. An apparatus as claimed in claim 1 in which the power supply comprises a battery.

20. Apparatus as claimed in any one of the preceding claims in which the power supply comprises a battery. An apparatus for monitoring a parameter associated with a structural component comprising a module which is attachable to the structural component and which incorporates a processor for receiving and processing measurement signals corresponding to said parameter from a sensor, and memory for storing data from said processor, and a power supply for powering operation of the apparatus, the apparatus further comprising display means which displays information about the structural components as well as data derived from measurement of the sensor.

21. An apparatus as claimed in claim 20 in which the display means comprises an LCD display.

22. An apparatus as claimed in claim 20 in which the power supply comprises a battery.