Gas turbine system
AssigneeEnisEnerGen, LLC
InventorsBen M. Enis, Paul Lieberman
Life of this patent
Estimating the term…
Abstract
The present invention is a centrifuge to be used for removing ice particles from the air fed to a gas turbine system. In an embodiment, the centrifuge is comprised of three ducts defining an air-path which comprises of two bends greater than 90 degrees. In an embodiment, the first two ducts extend past the bends to provide a dead air zone to trap ice particles which have been introduced by cooling air containing moisture. The dead air zones are further provided with revolving doors which remove the ice particles from the system. In an embodiment, the centrifuge receives cold air from the compander and removes ice particles before exhausting the cold air to a gas turbine electric generator, such that the blades of the gas turbine generator are not damaged by the ice particles.
Claims19
A centrifuge having:
- a. a first duct having:
- i. a first end to receive air from a compander, and
- ii. a second end having a first revolving door;
- b. a second duct having:
- i. a first end to receive air from the first duct, and
- ii. a second end having a second revolving door, and
- c. a third duct having:
- i. a first end to receive air from the second duct, and
- ii. a second end leading to a gas turbine generator,
- wherein the centrifuge defines an air-path, and wherein the air-path follows a bend greater than 90-degrees from the first duct to the second duct, and wherein the air-path follows a bend greater than 90-degrees from the second duct to the third duct.
A method of supplying super cold air to a gas turbine generator comprising the steps of:
- a. compressing air with a compressor;
- b. sending the compressed air to a compander;
- c. releasing cold air from the compander;
- d. removing ice particles from the cold air using a centrifuge, the centrifuge having:
- i. a first duct having:
- 1. a first end to receive air from a compander, and
- 2. a second end having a first revolving door;
- ii. a second duct having:
- 1. a first end to receive air from the first duct, and
- 2. a second end having a second revolving door, and
- iii. a third duct having:
- 1. a first end to receive air from the second duct, and
- 2. a second end leading to a gas turbine generator, wherein the centrifuge defines an airpath, and wherein the airpath follows a bend greater than 90-degrees from the first duct to the second duct, and wherein the airpath follows a bend greater than 90-degrees from the second duct to the third duct;
- and
- e. sending the cold air to the gas turbine generator,
- wherein intake of the cold air improves the efficiency of the gas turbine generator.
A gas turbine system having:
- a. a compander to exhaust cold air to a centrifuge;
- b. a centrifuge to remove ice particles for the cold air, the centrifuge having:
- i. a first duct having:
- 1. a first end to receive air from a compander, and
- 2. a second end having a first revolving door;
- ii. a second duct having:
- 1. a first end to receive air from the first duct, and
- 2. a second end having a second revolving door, and
- iii. a third duct having:
- 1. a first end to receive air from the second duct, and
- 2. a second end leading to a gas turbine generator,
- iv. wherein the centrifuge defines an air-path, and wherein the air-path follows a bend greater than 90-degrees from the first duct to the second duct, and wherein the air-path follows a bend greater than 90-degrees from the second duct to the third duct;
- and
- c. a natural gas turbine generator to provide electricity, wherein the cold air from the centrifuge, which is free from ice particles, improves efficiency of the natural gas turbine generator.
Dependencies are inferred from the claim text.