초록 ▼

A method and apparatus for boosting the performance of gas turbine engines, pipelines, and other applications using gas turbine engine systems. A pressurizing device or other source is preferably used to deliver an intake air stream to the gas turbine engine at at least 2% above atmospheric pressure

A method and apparatus for boosting the performance of gas turbine engines, pipelines, and other applications using gas turbine engine systems. A pressurizing device or other source is preferably used to deliver an intake air stream to the gas turbine engine at at least 2% above atmospheric pressure. The pressurizing device of other source is preferably not mechanically driven by the gas turbine engine itself.

대표청구항 ▼

1. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2

1. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion; and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands;said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine;said method comprises the step of (a) automatically monitoring a parameter which has a direct or indirect relationship to an amount of an emission in said engine exhaust stream; andsaid method further comprises the step of (b) automatically controlling a density of said intake air stream, prior to said intake air stream entering said air intake section of said gas turbine engine, based upon said parameter monitored in step (a) such that said amount of said emission in said engine exhaust stream does not exceed a predetermined level,wherein said intake air stream is a stream of said atmospheric air and said density of said intake air stream is automatically controlled in step (b) by changing a pressure of said intake air stream,said density of said intake air stream is automatically controlled in step (b) at least in part by automatically controlling an air pressurizing device for pressurizing said intake air stream, andsaid air pressurizing device is a centrifugal fan. 2. The method of claim 1 wherein said centrifugal fan pressurizes said stream of said atmospheric air at an outlet to inlet pressure ratio in a range of from a lower range value of 1.02 to an upper range value of 1.5. 3. The method of claim 1 wherein said gas turbine engine drives a stationary apparatus installed in fixed position at said geographical site. 4. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion, and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands;said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine;said method comprises the step of (a) automatically monitoring a parameter which has a direct or indirect relationship to an amount of an emission in said engine exhaust stream; andsaid method further comprises the step, when said parameter automatically monitored in step (a) reaches a predetermined value, of (b) automatically activating at least one apparatus which is external to said gas turbine engine to increase a density of said intake air stream,wherein said intake air stream is a stream of said atmospheric air and said apparatus operates to increase said density of said intake air stream in step (b) by increasing a pressure of said intake air stream,said apparatus comprises an air pressurizing device, andsaid air pressurizing device is a centrifugal fan. 5. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion; and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands;said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine;said method comprises the step of (a) automatically monitoring a parameter which has a direct or indirect relationship to an amount of an emission in said engine exhaust stream; andsaid method further comprises the step of (b) automatically controlling a density of said intake air stream, prior to said intake air stream entering said air intake section of said gas turbine engine, based upon said parameter monitored in step (a) such that said amount of said emission in said engine exhaust stream does not exceed a predetermined level,wherein said intake air stream is a stream of said atmospheric air and said density of said intake air stream is automatically controlled in step (b) by changing a pressure of said intake air stream, andsaid density of said intake air stream is automatically controlled in step (b) at least in part by automatically controlling a centrifugal HVAC fan for pressurizing said intake air stream. 6. The method of claim 5 wherein said centrifugal HVAC fan pressurizes said intake air stream at an outlet to inlet pressure ratio in a range of from a lower range value of 1.02 to an upper range value of 1.5. 7. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion, and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands; said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine; said method comprises the step of (a) automatically monitoring a power production rate of a device driven by said gas turbine engine; andsaid method further comprises the step, when said power production rate of said device driven by said gas turbine engine automatically monitored in step (a) reaches a predetermined value, of (b) automatically activating at least one apparatus which is external to said gas turbine engine to increase a density of said intake air stream, wherein said intake air stream is a stream of said atmospheric air and said apparatus operates to increase said density of said intake air stream in step (b) by increasing a pressure of said intake air stream, and said apparatus comprises an air pressurizing device. 8. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion, and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands;said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine;said method comprises the step of (a) automatically monitoring a fluid throughput or power production rate of a device driven by said gas turbine engine; andsaid method further comprises the step, when said fluid throughput or power production rate of said device driven by said gas turbine engine automatically monitored in step (a) reaches a predetermined value, of (b) automatically activating at least one apparatus which is external to said gas turbine engine to increase a density of said intake air stream,wherein said intake air stream is a stream of said atmospheric air and said apparatus operates to increase said density of said intake air stream in step (b) by increasing a pressure of said intake air stream, andsaid apparatus comprises an air pressurizing device. 9. A method of improving emissions from a gas turbine engine wherein: said gas turbine engine is a unitary structure comprising an engine housing having (1) an air intake section of said engine housing in which an engine compressor is positioned for receiving and compressing an intake air stream, (2) an internal combustion section which produces an engine exhaust stream comprising products of combustion, and (3) an engine power turbine within said engine housing through which said engine exhaust stream flows and expands;said gas turbine engine is operated at a geographical site having atmospheric air at an actual ambient air pressure and an actual ambient air temperature external to said gas turbine engine;said method comprises the step of (a) automatically monitoring a temperature of said engine exhaust stream; andsaid method further comprises the step, when said temperature of said engine exhaust stream automatically monitored in step (a) reaches a predetermined value, of (b) automatically activating at least one apparatus which is external to said gas turbine engine to increase a density of said intake air stream,wherein said intake air stream is a stream of said atmospheric air and said apparatus operates to increase said density of said intake air stream in step (b) by increasing a pressure of said intake air stream, andsaid apparatus comprises an air pressurizing device.