Utilization of circulating fluidized bed combustors for compressed air energy storage application

• US 4,936,098 A
• Filed: 05/13/1987
• Issued: 06/26/1990
• Est. Priority Date: 05/13/1987
• Status: Expired due to Fees

• Current Assignee: Ue&C Urban Services Corporation
• Original Assignee: Gibbs & Hill, Inc.
• Inventors: Nakhamkin, Michael
• Primary Examiner(s): Husar, Stephen F.
• Application Number:
  US07/049,649
• Time in Patent Office: 1,140 Days
• Field of Search: 60/650, 60/652, 60/659, 60/679, 60/682, 60/684, 60/655, 122/4 D
• US Class Current: 60/652
• CPC Class Codes: F02C 3/205 in a fluidised-bed combustor in combination with a steam cycle see F01K23/061; fluidised-bed apparatus in general B01J8/18; fluidised-bed combustors in general F23C10/00
• CPC Class Codes: F02C 6/16 for storing compressed air
• CPC Class Codes: F02C 7/143 before or between the compressor stages
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

A thermal energy peaking/intermediate power plant is disclosed having an atmospheric Fluidized Bed Combustor (FBC) for heating compressed air which is input to a turbine. Low-grade fuels such as coal may be combusted in the FBC, eliminating the need for additional combustors requiring premium fuels.

Claims

1. A Compressed Air Energy Storage (CAES) system comprising:

an electrical machine for use as a motor during a compression mode and for use as a generator during an expansion mode;

a compression train which compresses air and stores such compressed air in an air storage device during said compression mode, said compression train being selectively coupled to said motor by way of a first clutch means;

a turbine train which expands said compressed air from said air storage device during said expansion mode, said turbine train being selectively coupled to said generator by way of a second clutch means;

a heat recuperator for pre-heating said compressed air from said air storage device prior to expansion in said turbine train; and

an atmospheric fluidized bed combustor (FBC) for further heating said compressed air from said pre-heating means prior to expansion in said turbine train, said atmospheric FBC including a combustion chamber for combustion of low-grade fuel, said combustion chamber having a fuel input, a bed of fluidizable solid particles, an input to receive said fluidizable solid particles, a primary combustion air inlet and a secondary fluidizing air inlet.

2. The CAES system of claim 1 wherein said compression train comprises:

a low pressure compressor to initially compress ambient air to a first pressure level;

a high pressure compressor having an input connected to an output of said low pressure compressor for further compressing air at said first pressure level to an increased second pressure level and subsequently storing such air at said second pressure level in said air storage device.

3. The CAES system of claim 1 wherein said turbine train comprises:

a high pressure turbine to initially expand compressed air output by said atmospheric fluidized bed combustor; and

a low pressure turbine to further expand compressed air output by said high pressure turbine.

4. The CAES system of claim 3 wherein said compressed air output by said high pressure turbine is heated in said atmospheric fluidized bed combustor prior to input to said low pressure turbine.

5. The CAES system of claim 3 wherein the compressed air from said air storage device is heated in said atmospheric fluidized bed combustor prior to input to said high pressure turbine.

6. In a thermal power plant of the type which produces compressed air by use of excess energy generated during off-peak load periods and accumulates such compressed air in a storage device, the stored compressed air being withdrawn from said storage device and delivered to a turbine during peak load periods for generation of additional energy, the improved comprising:

a heat recuperator for pre-heating said compressed air from said storage device prior to delivery to said turbine, said heat recuperator obtaining heat from a turbine exhaust of said turbine; and

an atmospheric fluidized bed combustor (FBC) for heating said compressed air from said heat recuperator prior to expansion of said compressed air in said turbine.

7. The thermal power plant of claim 6 wherein said atmospheric FBC comprises a combustion chamber for combustion of low-grade fuel, said combustion chamber having a fuel input, a bed of fluidizable solid particles, an input to receive said fluidizable solid particles, a primary combustion air inlet and a second fluidizing air inlet.

8. The thermal power plant of claim 7 wherein said turbine comprises a high pressure turbine and a low pressure turbine, and said atmospheric FBC heats said compressed air from said heat recuperator prior to expansion of said compressed air in said high pressure turbine, and said atmospheric FBC heats an exhaust gas output by said high pressure turbine prior to expansion in said low pressure turbine.

9. The thermal power plant of claim 8 wherein said atmospheric FBC further comprises a convection bank and a solid particle fluidized bed air heater having a high pressure section, said compressed air being heated in said convection bank and said high pressure section, and said solid particle fluidized bed air heater having a low pressure section, said exhaust gas being heated in said convection bank and said low pressure section.

10. A method for generating peaking or intermediate electricity from expansion of compressed air comprising the steps of:

compressing a quantity of air during an off-load period;

storing said compressed air in an air storage device;

pre-heating compressed air from said air storage device in a heat recuperator;

heating said pre-heated compressed air in an atmospheric fluidized bed combustor (FBC) during a peaking or intermediate period, said atmospheric FBC including a combustion chamber for combusting low-grade fuels;

expanding said heated compressed air in a high pressure turbine coupled to an electric generator; and

supplying said expanded heated air from the turbine to the recuperator to pre-heat the compressed air.

11. The method of claim 10 further comprising the steps of:

heating an exhaust gas output by said high pressure turbine in said atmospheric fluidized bed combustor during a peak period; and

expanding said heated exhaust gas in a low pressure turbine coupled to said electric generator.

12. In a Compressed Air Energy Storage (CAES) system having a compression train and a turbine train, the improvement which permits the use of low grade fuel comprising the steps of:

supplying heat in the form of exhaust gas from said turbine train to a heat recuperator;

pre-heating, in said heat recuperator, compressed air from a compressed air storage device by transferring heat from said exhaust gas to said compressed air;

heating said pre-heated compressed air in an atmospheric fluidized bed combustor during a peak period; and

expanding said heated compressed air in a high pressure turbine.

13. The Compressed Air Energy Storage (CAES) system of claim 12 further comprising the steps of heating said expanded compressed air from the high pressure turbine in said atmospheric fluidized bed combustor and expanding said heated expanded compressed air in a low pressure turbine.

14. In a Compressed Air Energy Storage (CAES) system having a compression train and a turbine train in which the turbine train comprises a high pressure turbine and a low pressure turbine, the improvement comprising the steps of:

heating compressed air prior to expansion in said high pressure turbine, said heating including heating in an atmospheric fluidized bed combustor (FBC), said atmospheric FBC combusting low-grade fuel in a combustion chamber having a fuel input, a bed of fluidizable solid particles, an input to receive said fluidizable solid particles, a primary combustion air inlet and a secondary fluidizing air inlet;

expanding said heated compressed air in said high pressure turbine;

heating an exhaust gas output by said high pressure turbine in said atmospheric fluidized bed combustor; and

expanding said heated exhaust gas in said low pressure turbine.

15. The Compressed Air Energy Storage (CAES) system of claim 14 wherein said compressed air is supplied by an air storage device and is pre-heated prior to input to said atmospheric fluidized bed combustor.

16. The Compressed Air Energy Storage (CAES) system of claim 14 wherein said step of heating compressed air in an atmospheric FBC includes heating said compressed air in a convection bank and in a high pressure section of a solid particle fluidized bed air heater, and said step of heating said exhaust gas includes heating said exhaust gas in said convection bank and in a low pressure section of said solid particle fluidized bed air heater.

17. A Compressed Air Energy Storage (CAES) system comprising:

an electrical machine for use as a motor during a compression mode and for use as a generator during an expansion mode;

a compression train which compresses air and stores such compressed air in an air storage device during said compression mode, said compression train being selectively coupled to said motor by way of first clutch means;

a turbine train which expands said compressed air from said air storage device during said expansion mode, said turbine train being selectively coupled to said generator by way of said second clutch means;

means for pre-heating said compressed air from said air storage device prior to expansion in said turbine train; and

an atmospheric fluidized bed combustion (FBC) for further heating said compressed air from said pre-heating means prior to expansion in said turbine train, said atmospheric FBC including a combustion chamber for combustion of low-grade fuel, said combustion chamber having a fuel input, a bed of fluidizable solid particles, an input to receive said fluidizable solid particles, a primary combustion air inlet and a secondary fluidizing air inlet.

18. The CAES system of claim 17 wherein said atmospheric fluidized bed combustor further comprises a convection bank operatively associated with said combustion chamber for heating compressed air from said air storage device for subsequent expansion in a high pressure turbine of said turbine train.

19. The CAES system of claim 17 wherein said atmospheric fluidized bed combustor further comprises a convection bank operatively associated with said combustion chamber for heating exhaust gas output by a high pressure turbine of said turbine train for subsequent expansion in a low pressure turbine of said turbine train.

20. In a thermal power plant of the type which produces compressed air by use of excess energy generated during off-peak load periods and accumulates such compressed air in a storage device, the stored compressed air being withdrawn from said storage device and delivered to a turbine during peak load periods for generation of additional energy, the improvement comprising:

an atmospheric fluidized bed combustor for heating said compressed air from said storage device prior to expansion of said compressed air in said turbine, said atmospheric fluidized bed combustor including a combustion chamber for combustion of low-grade fuel, said combustion chamber having a fuel input, a bed of fluidizable solid particles, an input to receive said fluidizable solid particles, a primary combustion air inlet and a secondary fluidizing air inlet.

21. The thermal power plant of claim 20 wherein heated ambient air is input to said primary combustion air inlet and to said secondary fluidizing air inlet.

22. The thermal power plant of said claim 20 wherein said atmospheric fluidized bed combustor further comprises a convection bank operatively associated with said combustion chamber for heating high pressure compressed air from said air storage device for subsequent expansion in a high pressure turbine.

23. The thermal power plant of claim 20 wherein said atmospheric fluidized bed combustor further comprises a convection bank operatively associated with said combustion chamber for heating exhaust gas output by a high pressure turbine for subsequent expansion in a low pressure turbine.