Turbine inlet air heat pump-type system

US9470149B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9470149-B2
Application numberUS-33238308-A
CountryUS
Kind codeB2
Filing dateDec 11, 2008
Priority dateDec 11, 2008
Publication dateOct 18, 2016
Grant dateOct 18, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.

First claim

Opening claim text (preview).

We claim: 1. A heating and cooling system for inlet air of a gas turbine compressor, comprising: one or more water chillers comprising an evaporator and a condenser; a thermal energy storage tank charging loop comprising the evaporator of the one or more water chillers; a cooling loop comprising the condenser of the one or more water chillers, wherein the cooling loop is in communication with the thermal energy storage tank charging loop via the one or more water chillers; and a heating loop in communication with the cooling loop via a heat exchanger such that waste heat from the condenser of the one or more water chillers is exchanged in the heat exchanger to the heat loop, wherein the heating loop is in communication with the inlet air of the turbine compressor. 2. The heating and cooling system for inlet air of claim 1 , wherein the heating loop comprises a fluid coil positioned about the gas turbine compressor and in communication with the inlet air. 3. The heating and cooling system for inlet air of claim 1 , wherein the cooling loop comprises a cooling tower. 4. The heating and cooling system for inlet air of claim 1 , wherein the thermal energy storage tank charging loop comprises a thermal energy storage tank. 5. A method of operating an inlet air heating and cooling system for a compressor inlet as a heat pump, comprising: operating a chiller to charge a thermal energy storage tank; directing waste heat from the chiller to a heat exchanger; heating a fluid in communication with the compressor inlet and the waste heat of the chiller in the heat exchanger; and heating the inlet air about the compressor with the waste heat of the chiller. 6. The method of claim 5 , wherein the step of operating a chiller to charge a thermal energy storage tank comprises circulating a fluid about a chiller evaporator and a thermal energy storage tank. 7. The method of claim 5 , wherein the step of directing waste heat from the chiller to a heat exchanger comprises circulating a fluid about a chiller condenser and a heat recovery heat exchanger. 8. The method of claim 7 , wherein the step of heating a fluid in communication with the compressor inlet with the waste heat of the chiller in a heat exchanger comprises heating the fluid in the heat recovery heat exchanger. 9. The method of claim 5 , wherein the step of heating the inlet air about the compressor with the waste heat of the chiller comprises heating the inlet air via a fluid coil. 10. A heating and cooling system for inlet air of a gas turbine compressor, comprising: a thermal energy storage tank charging loop with a thermal energy storage tank and a chiller evaporator; a cooling loop in communication with the thermal energy storage tank charging loop; the cooling loop comprising a chiller condenser and a heat recovery heat exchanger; a heating loop in communication with the cooling loop and the inlet air of the gas turbine compressor; and the heating loop comprising a fluid coil positioned about the turbine compressor and in communication with the heat recovery heat exchanger. 11. The heating and cooling system for inlet air of claim 10 , wherein the cooling loop comprises a cooling tower. 12. The heating and cooling system for inlet air of claim 10 , wherein the thermal energy storage tank charging loop comprises a primary water pump. 13. The heating and cooling system for inlet air of claim 10 , wherein the cooling loop comprises a secondary water pump. 14. The heating and cooling system for inlet air of claim 10 , wherein the heating loop comprises a condenser water pump.

Assignees

Inventors

Classifications

  • F02C7/143Primary

    before or between the compressor stages · CPC title

  • Heating to prevent icing · CPC title

  • Combined heat and power generation [CHP] · CPC title

  • with exhaust fluid of one cycle heating the fluid in another cycle (F01K17/025 takes precedence) · CPC title

  • Plants modified to use their waste heat, other than that of exhaust, e.g. engine-friction heat · CPC title

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What does patent US9470149B2 cover?
A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.
Who is the assignee on this patent?
Motakef Abbas, Feher Peter, Gen Electric
What technology area does this patent fall under?
Primary CPC classification F02C7/143. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 18 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).