Rotational aid for self-cleaning filter

Patent metadata

Field	Value
Publication number	US-10124283-B2
Application number	US-201615358431-A
Country	US
Kind code	B2
Filing date	Nov 22, 2016
Priority date	Nov 22, 2016
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

A filter assembly for a gas turbine system includes a filter element configured to remove entrained particles from air which passes through the filter element in a first direction toward a central air passageway. A motion generator arranged to rotate the filter element about a longitudinal axis extending in an airflow direction of the air passageway to cause particles accumulated on the filter element to fall downwardly away from the filter element due to gravity.

First claim

What is claimed is:

1. A gas turbine system comprising:
a compressor;
a combustor connected to the compressor;
a turbine connected to the combustor; and
a filter house system connected as an input to the compressor, wherein the filter house system comprises a filter assembly, the filter assembly comprising,
a filter element having a porous structure configured to pass air therethrough, the filter element being arranged so as to define a hollow interior forming an air passageway, the filter element being configured to remove entrained particles from air which passes through the filter element in a first direction toward the air passageway;
a rotary motion generator arranged to rotate the filter element about a longitudinal axis extending in an airflow direction of the air passageway to cause particles accumulated on the filter element to fall downwardly away from the filter element due to gravity, wherein the rotary motion generator is one of a motor, a pneumatic-based device, a hydraulic-based device, or a magnet-based device;
piping extending into the air passageway and configured to convey air arranged to pass through the filter element in a second direction opposite the first direction to cause particles accumulated on the filter element to be removed from the filter element; and
a plurality of nozzles extending from the piping at spaced-apart locations in the first direction, wherein the piping is configured to rotate within the air passageway such that the nozzles are rotated about the longitudinal axis.

2. The gas turbine system of claim 1 , further comprising at least one microprocessor configured to cause the filter element to rotate after air is passed through the filter element in the second direction.

3. The gas turbine system of claim 1 , wherein the motion generator is configured to rotate the filter element at least 90 degrees.

4. The gas turbine system of claim 1 , further comprising a dynamic seal between the filter element and a filter house enclosure, wherein the filter element is arranged to rotate relative to the filter house enclosure, and wherein the dynamic seal seals the air passageway from the ambient area of the filter house enclosure.

5. The gas turbine system of claim 1 , wherein the filter element has a cylindrical shape and/or conical shape and/or oval shape.

6. The gas turbine system of claim 1 , wherein a wiper blade is arranged to remove accumulated particles from the filter element.

7. The gas turbine system of claim 1 , further comprising a blow nozzle positioned adjacent the filter element and configured to blow air across a surface of the filter element to cause particles accumulated thereon to be dislodged.

8. The gas turbine system of claim 1 , wherein the motion generator is a motor.

9. A gas turbine system comprising:
a compressor;
a combustor connected to the compressor;
a turbine connected to the combustor; and
a filter house system connected as an input to the compressor, wherein the filter house system comprises a filter assembly, the filter assembly comprising;
a filter element having a porous structure configured to pass air therethrough, the filter element being arranged so as to define a hollow interior forming an air passageway, the filter element being configured to remove entrained particles from air which passes through the filter element in a first direction toward the air passageway;
a motion generator arranged to rotate the filter element about a longitudinal axis extending in an airflow direction of the air passageway to cause particles accumulated on the filter element to fall downwardly away from the filter element due to gravity, wherein the motion generator is one of a motor, a pneumatic-based device, a hydraulic-based device, or a magnet-based device;
piping extending into the air passageway and configured to convey air arranged to pass through the filter element in a second direction opposite the first direction to cause particles accumulated on the filter element to be removed from the filter element; and
a plurality of nozzles extending from the piping at spaced-apart locations in the first direction, wherein the piping is configured to rotate within the air passageway such that the nozzles are rotated about the longitudinal axis.

10. The gas turbine system of claim 9 , further comprising at least one microprocessor configured to cause the filter element to rotate after air is passed through the filter element in the second direction.

11. The gas turbine system of claim 9 , wherein the motion generator is configured to rotate the filter element at least 90.

12. The gas turbine system of claim 11 , further comprising a dynamic seal between the filter element and a filter house enclosure, wherein the filter element is arranged to rotate relative to the filter house enclosure, and wherein the dynamic seal seals the air passageway from the ambient area of the filter house enclosure.

13. The gas turbine system of claim 12 , wherein the filter element has a cylindrical shape and/or conical shape and/or oval shape.

14. The gas turbine system of claim 13 , wherein a wiper blade is arranged to remove accumulated particles from the filter element.

15. The gas turbine system of claim 14 , further comprising a blow nozzle positioned adjacent the filter element and configured to blow air across a surface of the filter element to cause particles accumulated thereon to be dislodged.

16. The gas turbine system of claim 9 , wherein the motion generator is the motor.

Assignees

• Gen Electric

Inventors

• Frese Christopher Conrad
• Kippel Bradly

Classifications

• B01D46/682

  by nozzles · CPC title

• B01D46/681

  by scrapers, brushes or the like · CPC title

• B01D2273/14

  Filters which are moved between two or more positions, e.g. by turning, pushing · CPC title

• B01D46/0065

  Operations & Transport · mapped topic

• B01D2279/60

  for the intake of internal combustion engines or turbines · CPC title