TIRE PRESSURE SENSOR DEVICE

• US 20170015151A1
• Filed: 07/15/2016
• Published: 01/19/2017
• Est. Priority Date: 07/16/2015
• Status: Active Grant

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: BILL, Andrew Raymond
• Granted Patent: US 10,183,534 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B60C 23/0457 self triggered by timer
• CPC Class Codes: B60C 23/0459 self triggered by motion sensor
• CPC Class Codes: B60C 23/0474 Measurement control, e.g. setting measurement rate or calibrating of sensors; Further processing of measured values, e.g. filtering, compensating or slope monitoring
• CPC Class Codes: B60C 23/0479 Communicating with external units being not part of the vehicle, e.g. tools for diagnostic, mobile phones, electronic keys or service stations
• CPC Class Codes: B60C 23/0486 comprising additional sensors in the wheel or tyre mounted monitoring device, e.g. movement sensors, microphones or earth magnetic field sensors
• CPC Class Codes: B60C 23/0488 Movement sensor, e.g. for sensing angular speed, acceleration or centripetal force
• CPC Class Codes: G01K 13/00 Thermometers specially adapted for specific purposes

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.

Claims

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,

a temperature sensor configured to measure a temperature local to the tire,

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 housing accommodates at least the control unit and the memory unit, and

the data so recorded for each such reading 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 tire pressure sensor device includes a motion sensor and wherein the control unit is configured 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.

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

a local source of electric power.

12. 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 tire pressure sensor device is associated with a different respective wheel of the aircraft, the housing of each device being mounted locally to the wheel with which the device is associated.

13. 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.

14. The kit of parts according to claim 13, 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

15. The kit of parts according to claim 13, including multiple tire pressure sensor devices.

8. 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,

a temperature sensor adapted to measure a temperature local to the tire,

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;

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 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.

9. The self-contained tire pressure sensor device according to claim 8, wherein the housing accommodates a communication module facilitating secure wireless communication with a reader device external to the aircraft.

10. The self-contained tire pressure sensor device according to claim 8, wherein

the housing accommodates a 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.

11. The self-contained tire pressure sensor device according to claim 8, wherein the pressure sensor device is mounted on a 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 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 second measurements 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 other of the first and second measurements being taken when the aircraft is in flight, the time between the first and second measurements being taken being between one minute and twenty-four hours.

17. The method according to claim 16 wherein:

more than three successive sets of measurements are taken, including at least one set taken when the aircraft is in flight, and

corresponding multiple successive sets of data are recorded in the memory unit, and wherein the interval between successive measurements is between 10 minutes and 7.5 hours.

18. The method according to claim 17, wherein data is recorded in the memory unit on a rolling basis, such that old data is deleted from the memory unit as new data is stored in the memory unit.

19. The method according to claim 16, wherein one of the first and second measurements is triggered by detection of a change in the speed of spinning, if any, of the tire.

20. The method according to claim 19, wherein the other of the first and second measurements is taken after a set time delay dependent on the detection of the change in the speed of spinning.