Combination tire pressure sensor and over-inflation pressure relief valve

Patent metadata

Field	Value
Publication number	US-9956831-B2
Application number	US-201414570890-A
Country	US
Kind code	B2
Filing date	Dec 15, 2014
Priority date	Dec 15, 2014
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

The present disclosure includes a combination sensor and pressure relief valve. The combination sensor and valve may be used with existing aircraft wheel systems. Wheel systems utilizing the combination sensor and valve are also disclosed.

First claim

What is claimed is:

1. A combination sensor and pressure release valve, comprising:
a housing defining at least two air exit openings and comprising a stem defining an air entry opening, wherein the stem is configured to be retained by a valve receptacle of a wheel and wherein the housing is configured to receive air from a tire through the air entry opening, wherein the stem is aligned along a longitudinal axis;
an over-inflation pressure relief valve segment within the housing, in fluid communication with the air entry opening, and comprising a frangible disk located upstream from the at least two air exit openings and configured to rupture at a predetermined pressure such that the air flows past the frangible disk and through the at least two air exit openings in response to the frangible disk rupturing, the frangible disk comprising a planar surface aligned perpendicular to the longitudinal axis, wherein the at least two air exit openings are orientated perpendicular to the planar surface of the frangible disk; and
a tire pressure sensor within the housing, aligned along the longitudinal axis, and in fluid communication with the air entry opening, the tire pressure sensor configured to sense a pressure of air received from the tire during inflation of the tire.

2. The combination sensor and pressure release valve of claim 1 , wherein the stem comprises a threaded pattern configured to mate with a threaded portion of the valve receptacle.

3. The combination sensor and pressure release valve of claim 1 , wherein the predetermined pressure is between 1400 kPa and 2000 kPa.

4. The combination sensor and pressure release valve of claim 3 , wherein the predetermined pressure is about 1700 kPa.

5. The combination sensor and pressure release valve of claim 1 , wherein the tire pressure sensor is configured to be powered and interrogated by an external magnetic field.

6. The combination sensor and pressure release valve of claim 1 , wherein the housing comprises a metal.

7. The combination sensor and pressure release valve of claim 1 , wherein the housing is manufactured by an additive process.

8. The combination sensor and pressure release valve of claim 1 , wherein the frangible disk is entirely positioned within the housing.

9. The combination sensor and pressure release valve of claim 1 , wherein the over-inflation pressure relief valve segment is located between the air entry opening and the tire pressure sensor.

10. An aircraft wheel system, comprising:
a wheel having a sensor receptacle; and
a combination pressure sensor and pressure relief valve comprising:
a housing defining at least two air exit openings and having a stem and an air entry opening, wherein the housing is configured to receive air from a tire through the air entry opening,
an over-inflation pressure relief valve segment within the housing, in fluid communication with the air entry opening, and comprising a frangible disk located upstream from the at least two air exit openings and configured to rupture at a predetermined pressure such that the air flows past the frangible disk and through the at least two air exit openings in response to the frangible disk rupturing, the frangible disk comprising a planar surface wherein the at least two air exit openings are orientated perpendicular to the planar surface of the frangible disk, the planar surface extending substantially perpendicular to a longitudinal axis; and
a tire pressure sensor within the housing and in fluid communication with the air entry opening, the tire pressure sensor configured to sense a pressure of air received from the tire during inflation of the tire, wherein the tire pressure sensor, the frangible disk and the over-inflation pressure relief valve segment intersect the longitudinal axis.

11. The aircraft wheel system of claim 10 , wherein the stem comprises a threaded pattern configured to mate with a complementary threaded pattern of the sensor receptacle in the wheel.

12. The aircraft wheel system of claim 10 , wherein the housing is manufactured by an additive process.

13. The aircraft wheel system of claim 10 , wherein the tire pressure sensor is configured to be powered and interrogated by an external magnetic field.

14. The aircraft wheel system of claim 13 , further comprising a sensor reading device, wherein the sensor reading device is configured to power and to interrogate the tire pressure sensor and receive a pressure datum from the tire pressure sensor.

15. The aircraft wheel system of claim 14 , further comprising an interface, wherein the sensor reading device transmits the pressure datum to the interface.

16. The aircraft wheel system of claim 10 , wherein the predetermined pressure is between 1400 kPa and 2000 kPa.

17. The aircraft wheel system of claim 16 , wherein the predetermined pressure is about 1700 kPa.

Assignees

• Goodrich Corp

Inventors

• Summers Paul
• Keller Steven
• Whittle Scott

Classifications

• B33Y80/00

  Products made by additive manufacturing · CPC title

• G01L19/086

  for remote indication · CPC title

• B60C23/0484

  Detecting an ongoing tyre inflation · CPC title

• F16K17/16

  with fracturing diaphragm {; Rupture discs} · CPC title

• F16K17/403

  with a fracturing valve member · CPC title