Tire pressure sensor device

Patent metadata

Field	Value
Publication number	US-10183534-B2
Application number	US-201615212085-A
Country	US
Kind code	B2
Filing date	Jul 15, 2016
Priority date	Jul 16, 2015
Publication date	Jan 22, 2019
Grant date	Jan 22, 2019

Abstract

A tire pressure sensor device (122) for a wheel (112) of an aircraft (102) including a pressure sensor (124) for measuring the internal pressure of a tire, a temperature sensor (126) for measuring a temperature local to the tire (116), a memory unit (131) local to the tire for storing data, and a control unit (128) local to the tire arranged to record in the memory unit (131) data of the readings taken at intervals of time. The data recorded for each reading includes an indication of the time of the reading, the tire pressure and the temperature local to the tire. Measurements may be taken and recorded over time, both when the aircraft is on the ground and when the aircraft is in flight. Data may be uploaded to a portable handheld device (140) for analysis when maintaining the tires in their correctly inflated state.

First claim

The invention claimed is:

1. A tire pressure sensor device for a wheel of an aircraft, wherein the tire pressure sensor device comprises:
a housing,
a pressure sensor configured to measure an internal pressure of a tire of the wheel,
a temperature sensor configured to measure a temperature local to the tire,
a motion sensor configured to ascertain a period within which the wheel has stopped spinning following take-off of the aircraft;
a memory unit local to the tire configured to store data, and
a control unit local to the tire arranged to record in the memory unit data in respect of multiple readings over time, wherein the multiple readings include a reading taken while the aircraft is on the ground and while the wheel is stopped, and another reading taken while the aircraft is in flight and at least 10 minutes after the wheel has stopped spinning;
wherein the housing accommodates at least the control unit and the memory unit, and
the data recorded for each of the multiple readings includes an indication of a time of the reading, a pressure as measured by the pressure sensor, and a temperature as measured by the temperature sensor.

2. The tire pressure sensor device according to claim 1 further including a communication module facilitating secure wireless communication with a reader device external to the aircraft.

3. The tire pressure sensor device according to claim 1 , wherein the motion sensor is configured to detect at least one of (a) whether the aircraft is in flight, and (b) whether the aircraft is on the ground.

4. The tire pressure sensor device according to claim 1 arranged such that the control unit records in memory both data relating to the reading taken when the aircraft is on the ground and data relating to the another reading taken when the aircraft is in flight.

5. The tire pressure sensor device according to claim 4 arranged such that the data so recorded for each of the multiple readings includes an indication of whether the aircraft is on the ground or an indication of whether the aircraft is in flight.

6. The tire pressure sensor device according claim 1 , wherein the memory unit includes an indication of a reference tire pressure for the tire.

7. The tire pressure sensor device according claim 1 , wherein the housing accommodates:
at least a part of the pressure sensor,
at least part of the motion sensor;
at least a part of the temperature sensor, and
a local source of electric power.

8. An aircraft on which there are mounted multiple tire pressure sensor devices, wherein each tire pressure sensor device is a tire pressure sensor device according to claim 1 , and each of the multiple self-contained tire pressure sensor devices is associated with a different respective wheel of the aircraft, the housing of each of the multiple self-contained tire pressure sensor devices being mounted locally to the wheel with which the self-contained tire pressure sensor device is associated.

9. A kit of parts including a tire pressure sensor device according to claim 1 and a portable reader device external to the aircraft, wherein the tire pressure sensor device and the portable reader device are configured to facilitate electronic communication between each other.

10. The kit of parts according to claim 9 , wherein each of the tire pressure sensor device and the portable reader device further includes a communication module facilitating secure wireless communication between the tire pressure sensor device and the portable reader device.

11. The kit of parts according to claim 9 , including multiple tire pressure sensor devices.

12. A self-contained tire pressure sensor device for a wheel of an aircraft comprising:
a housing,
a pressure sensor adapted to measure an internal pressure of a tire of the wheel,
a temperature sensor adapted to measure a temperature local to the tire,
a motion sensor configured to ascertain a period within which the wheel has stopped moving relative to the aircraft following take-off of the aircraft;
a non-transitory memory unit configured to store data,
a control unit adapted to:
receive readings from the pressure sensor and from the temperature sensor;
receive data generated by the motion sensor indicative of the period within which the wheel has stopped the movement;
record data from the readings in the non-transitory memory unit such that the data corresponds to at least three of the readings taken at intervals of at least ten minutes, wherein the multiple readings include a reading taken while the aircraft is on the ground and while the wheel is stopped, and another reading taken while the aircraft is in flight and at least 10 minutes after the wheel has stopped moving relative to the aircraft;
wherein the data recorded for each of the readings includes an indication of the time of the reading, an indication of the pressure measured by the pressure sensor, and an indication of the temperature measured by the temperature sensor, and
a source of electric power adapted to power at least the control unit,
wherein the housing accommodates:
at least a part of the pressure sensor,
at least a part of the temperature sensor,
the memory unit,
the control unit, and
the source of electric power.

13. The self-contained tire pressure sensor device according to claim 12 , wherein the housing accommodates a communication module facilitating secure wireless communication with a reader device external to the aircraft.

14. The self-contained tire pressure sensor device according to claim 12 , wherein
the housing accommodates the motion sensor,
the control unit is arranged to detect with the use of the motion sensor at least one of (a) whether the aircraft is in flight and (b) whether the aircraft is on the ground, and
each reading recorded in memory by the control unit includes at least one of (i) an indication of whether the aircraft is on the ground and (ii) an indication of whether the aircraft is in flight.

15. The self-contained tire pressure sensor device according to claim 12 , wherein the pressure sensor device is mounted on the wheel of an aircraft, which has at least one other wheel on which another self-contained tire pressure sensor device is mounted.

16. A method of monitoring the pressure of a tire on an aircraft comprising:
a control unit receiving data indicating whether the tire is spinning;
the control unit causing first measurements to be taken of tire pressure and of an associated temperature local to the tire,
the control unit recording in a memory unit first data including an indication of the time at which the first measurements are taken, an indication of the tire pressure and an indication of the temperature as so measured by the first measurements,
the control unit causing a second measurement to be taken of the tire pressure and of an associated temperature, and
the control unit recording in the memory unit second data including an indication of the time at which the second measurements are taken, an indication of the tire pressure and an indication of the temperature as so measured by the second measurements,
one of the first and second measurements being taken when the aircraft is on the ground and the tire is not spinning, and the other of the first and second measurements being taken when the aircraft is in flight and after at least ten minutes has elapsed since the tire has stopped spinning, wherein the second measurement is within twenty-four hours of the first measurement.

17. The method according to claim 16 wherein:
more than three successive sets of measurements ar

Assignees

• Airbus Operations Ltd

Inventors

• Bill Andrew Raymond

Classifications

• B60C23/0459

  self triggered by motion sensor · CPC title

• B60C23/0486 Primary

  comprising additional sensors in the wheel or tyre mounted monitoring device, e.g. movement sensors, microphones or earth magnetic field sensors · CPC title

• B60C2200/02

  for aircrafts · CPC title

• B60C23/0493

  for attachment on the tyre · CPC title

• G01K13/00

  Thermometers specially adapted for specific purposes · CPC title