Air pressure regulator

Patent metadata

Field	Value
Publication number	US-10125880-B2
Application number	US-201514823345-A
Country	US
Kind code	B2
Filing date	Aug 11, 2015
Priority date	Aug 11, 2015
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

An air pressure regulator includes a regulator body defining a hollow interior, an air inlet in communication with the hollow interior and configured to connect with a source of pressurized air, an air outlet fluidly coupled with the air inlet, and a valve stem positioned at the air inlet and configured to regulate the pressure of the pressurized air for the air outlet by way of movement of the valve stem relative to the air inlet.

First claim

What is claimed is:

1. An air pressure regulator comprising:
a regulator body having a housing and defining a hollow interior;
an air inlet in communication with the hollow interior and configured to connect with a source of pressurized air;
an air outlet fluidly coupled with the air inlet;
a valve stem positioned at the air inlet and configured to regulate the pressure of the pressurized air for the air outlet by way of slidable movement of the valve stem relative to the air inlet;
a restraining element disposed within the hollow interior and coupled with the valve stem such that the valve stem and the restraining element move in unison wherein the restraining element includes an electrically conductive sleeve encircling a hollow bore; and
a magnet having a magnetic field mounted to the regulator body wherein the magnet is received by the hollow bore and the magnetic field encompasses at least part of the conductive sleeve;
wherein movement of the conductive sleeve relative to the magnetic field is retarded by Eddy currents generated in the conductive sleeve by the movement, and wherein the magnet is fixed relative to the housing and includes an adjuster configured to adjust the position of the magnet relative to the conductive sleeve.

2. The air pressure regulator of claim 1 wherein vibrational movement of at least one of the regulator body, the valve stem, the air inlet, the air outlet, or the restraining element is retarded by Eddy currents generated in the conductive sleeve by the movement of the conductive sleeve relative to the magnetic field.

3. The air pressure regulator of claim 2 wherein at least one of the magnet or conductive sleeve is configured to retard vibrational movement in an aircraft.

4. The air pressure regulator of claim 1 wherein the restraining element includes a mechanical restraining element.

5. The air pressure regulator of claim 4 wherein the mechanical restraining element is a spring.

6. The air pressure regulator of claim 4 wherein the mechanical restraining element is a diaphragm.

7. The air pressure regulator of claim 1 wherein the restraining element is configured to restrain the valve stem such that the pressurized air from the air inlet is regulated for the air outlet.

8. The air pressure regulator of claim 1 wherein the magnet is at least one of a permanent magnet or an electromagnet.

9. The air pressure regulator of claim 8 wherein the magnet is axially magnetized.

10. The air pressure regulator of claim 8 wherein the electromagnet is configured to adjust the magnetic field based at least in part on the movement of the conductive sleeve.

11. The air pressure regulator of claim 1 wherein the valve stem includes a poppet valve configured to regulate the pressure of the pressurized air for the air outlet by way of movement of the poppet valve relative to the air inlet.

12. The air pressure regulator of claim 1 further including a cooling path configured to dissipate heat generated on the conductive sleeve.

13. The air pressure regulator of claim 1 wherein the regulator body includes a first housing defining a first interior having the air inlet, the air outlet, and at least a portion of the valve stem, and a second housing defining a second interior having the restraining element, the conductive sleeve, and the magnet.

14. An air pressure loading element comprises:
a housing defining a hollow interior;
a restraining element disposed within the hollow interior, having an electrically conductive sleeve encircling a hollow bore, and coupled with a valve stem positioned at an air inlet and configured to regulate the pressure of pressurized air for an air outlet by way of slidable movement of the valve stem relative to the air inlet, wherein the valve stem and the restraining element move in unison; and
a magnet having a magnetic field mounted to the housing wherein the magnet is received by the hollow bore and the magnetic field encompasses at least part of the conductive sleeve;
wherein movement of the conductive sleeve relative to the magnetic field is retarded by Eddy currents generated in the conductive sleeve by the movement, and wherein the magnet is fixed relative to the housing and includes an adjuster configured to adjust the position of the magnet relative to the conductive sleeve.

15. The air pressure loading element of claim 14 wherein vibrational movement of at least one of the housing, the valve stem, the air inlet, the air outlet, or the restraining element is retarded by Eddy currents generated in the conductive sleeve by the movement of the conductive sleeve relative to the magnetic field.

16. The air pressure loading element of claim 15 wherein at least one of the magnet or conductive sleeve is configured to retard vibrational movement in an aircraft.

17. An air pressure regulator comprising:
a restricting element configured to provide variable restriction to regulate the pressure of pressurized air at an air inlet for an air outlet, by way of slidable movement of the restricting element relative to the air inlet;
a restraining element coupled with the restricting element and having an electrically conductive sleeve encircling a hollow bore, wherein the restricting element and the restraining element move in unison; and
a magnet adjustably fixed proximate to the conductive sleeve by an adjuster and having a magnetic field, wherein the magnet is received by the hollow bore, the magnetic field encompasses at least part of the conductive sleeve, and the conductive sleeve is movable relative to the magnet;
wherein movement of the conductive sleeve relative to the magnetic field is retarded by Eddy currents generated in the conductive sleeve by the movement, and wherein the adjuster is configured to adjust the position of the magnet relative to the conductive sleeve.

18. The air pressure regulator of claim 17 wherein vibrational movement of at least one of the restricting element, the air inlet, the air outlet, or the restraining element is retarded by Eddy currents generated in the conductive sleeve by the movement of the conductive sleeve relative to the magnetic field.

19. The air pressure regulator of claim 18 wherein at least one of the magnet or conductive sleeve is configured to retard vibrational movement in an aircraft.

Assignees

• Ge Aviation Systems Llc

Inventors

• Hielkema Jerry Dean

Classifications

• G05D16/02 Primary

  Modifications to reduce the effects of instability, e.g. due to vibrations, friction, abnormal temperature, overloading or imbalance · CPC title

• G05D16/2013 Primary

  using throttling means as controlling means · CPC title

• F16K1/00

  Lift valves {or globe valves}, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces ({in combination with sliding valves F16K3/246, F16K3/267} ; diaphragm valves F16K7/00) · CPC title

• F02C9/00 Primary

  Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants (controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05) · CPC title

• F16K31/082

  using a electromagnet and a permanent magnet · CPC title