Tire pressure sensor with included position sensor

• US 9,950,701 B2
• Filed: 11/03/2014
• Issued: 04/24/2018
• Est. Priority Date: 11/03/2014
• Status: Active Grant

• Current Assignee: Goodrich Corporation (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Keller, Steven, Summers, Paul L., Robbins, Lane B., Streng, Scott
• Primary Examiner(s): Desta, Elias
• Application Number:
  US14/531,746
• Publication Number:
  US 20160214585A1
• Time in Patent Office: 1,268 Days
• CPC Class Codes: B60C 2200/02 for aircrafts
• CPC Class Codes: B60C 23/00 Devices for measuring, signalling, controlling, or distributing tyre pressure or temperature, specially adapted for mounting on vehicles; Arrangement of tyre inflating devices on vehicles, e.g. of pumps or of tanks; Tyre cooling arrangements
• CPC Class Codes: B60C 23/0408 transmitting the signals by non-mechanical means from the wheel or tyre to a vehicle body mounted receiver
• CPC Class Codes: B60C 23/0488 Movement sensor, e.g. for sensing angular speed, acceleration or centripetal force
• CPC Class Codes: B60T 8/1703 for aircrafts
• CPC Class Codes: B60T 8/1725 Using tyre sensors, e.g. Sidewall Torsion sensors [SWT] for tyre pressure and temperature detection B60C23/00
• CPC Class Codes: G01M 17/02 Tyres
• CPC Class Codes: G01P 3/44 for measuring angular speed G01P3/56 takes precedence

Abstract

What is described is a tire pressure sensor for use in a wheel of aircraft landing gear. The tire pressure sensor includes a position sensor configured to detect a movement of the wheel and generate a wheel movement signal based on the movement. The tire pressure sensor also includes a processor coupled to the position sensor. The processor is configured to receive the wheel movement signal, determine a wheel rotational speed of the wheel based on the wheel movement signal and generate a wheel rotational speed signal based on the wheel rotational speed.

Claims

1. A tire pressure sensor for use in a wheel of landing gear of an aircraft, the tire pressure sensor comprising:

a housing having features to facilitate connection of the housing to the wheel such that the housing rotates with the wheel;

a position sensor positioned at least one of in or on the housing and configured to rotate with the wheel relative to the aircraft, to detect a movement of the wheel, and to generate a wheel movement signal based on the movement; and

a processor coupled to the position sensor and configured to;

receive the wheel movement signal,

determine a wheel rotational speed of the wheel based on the wheel movement signal, and

generate a wheel rotational speed signal based on the wheel rotational speed.

2. The tire pressure sensor of claim 1, wherein the position sensor is an accelerometer.

3. The tire pressure sensor of claim 1, wherein the position sensor is a gyroscope.

4. The tire pressure sensor of claim 1, wherein the landing gear is at least one of a main landing gear or a nose landing gear.

5. The tire pressure sensor of claim 1, wherein the processor is coupled to a brake control system and further configured to transmit the wheel rotational speed signal to the brake control system.

6. The tire pressure sensor of claim 1, further comprising a power supply module configured to provide direct current power to the position sensor and to the processor.

7. The tire pressure sensor of claim 1, further comprising a demodulation module coupled to the processor and configured to demodulate a first signal and a modulation module coupled to the processor and configured to modulate a second signal.

8. The tire pressure sensor of claim 1, wherein the wheel movement signal indicates an angular acceleration of the wheel.

9. The tire pressure sensor of claim 1, wherein the processor is further configured to determine at least one of a status of a wheel bearing of the wheel, a status of a hubcap of the wheel or a status of the landing gear based on the wheel movement signal.

10. A system for determining a rotational speed of a wheel for use in landing gear of an aircraft, the system comprising:

a tire pressure sensor mounted to the wheel, configured to rotate with the wheel, and having a pressure transducer module configured to detect pressure data corresponding to a tire pressure of a tire positioned on the wheel; and

a position sensor positioned at least one of in or on the tire pressure sensor and configured to rotate along with the wheel, to detect a movement of the wheel, and to generate a wheel movement signal based on the movement.

11. The system of claim 10, further comprising a processor coupled to the position sensor and configured to:

receive the wheel movement signal; and

determine the rotational speed of the wheel based on the wheel movement signal.

12. The system of claim 11, wherein the processor is coupled to a brake control system and is further configured to generate a wheel rotational speed signal based on the rotational speed of the wheel and transmit the wheel rotational speed signal to the brake control system.

13. The system of claim 11, wherein the processor is further configured to determine at least one of a status of a wheel bearing of the wheel, a status of a hubcap of the wheel or a status of the landing gear based on the wheel movement signal.

14. The system of claim 10, wherein the position sensor is an accelerometer.

15. The system of claim 10, wherein the position sensor is a gyroscope.

16. The system of claim 12, wherein the processor is further configured to transmit, to the brake control system, pressure output data corresponding to the pressure data detected by the pressure transducer module.

17. The system of claim 12, further comprising:

a wheel rotational speed transducer configured to output a transducer wheel rotational speed signal; and

the brake control system, wherein the brake control system is configured to control a braking operation based on the transducer wheel rotational speed signal in response to determining that the transducer wheel rotational speed signal has a value greater than zero, and to control the braking operation based on the wheel rotational speed signal in response to determining that the transducer wheel rotational speed signal is at least one of zero or a failure signal.