US20120102987A1 - Inlet Air Cooling and Moisture Removal Methods and Devices in Advance Adiabatic Compressed Air Energy Storage Systems - Google Patents

Inlet Air Cooling and Moisture Removal Methods and Devices in Advance Adiabatic Compressed Air Energy Storage Systems Download PDF

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Publication number
US20120102987A1
US20120102987A1 US12/915,422 US91542210A US2012102987A1 US 20120102987 A1 US20120102987 A1 US 20120102987A1 US 91542210 A US91542210 A US 91542210A US 2012102987 A1 US2012102987 A1 US 2012102987A1
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Prior art keywords
air
compressed
compressor
air flow
heat exchanger
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Abandoned
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US12/915,422
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English (en)
Inventor
Sanjay Anikhindi
Bhaskara KOSAMANA
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Nuovo Pignone Holding SpA
Nuovo Pignone SpA
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Nuovo Pignone SpA
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Priority to US12/915,422 priority Critical patent/US20120102987A1/en
Assigned to NUOVO PIGNONE HOLDING S.P.A. reassignment NUOVO PIGNONE HOLDING S.P.A. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ANIKHINDI, SANJAY, Kosamana, Bhaskara
Priority to JP2011233555A priority patent/JP5981704B2/ja
Priority to EP11186992.1A priority patent/EP2447505B1/en
Priority to CN2011103461275A priority patent/CN102538531A/zh
Priority to RU2011143462/07A priority patent/RU2559793C2/ru
Publication of US20120102987A1 publication Critical patent/US20120102987A1/en
Abandoned legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/14—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads
    • F02C6/16—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads for storing compressed air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids

Definitions

  • the embodiments of the subject matter disclosed herein generally relate to power generation systems and more specifically to advanced adiabatic compressed air energy storage systems.
  • step 3 a air is taken into an axial compressor 4 and compressed during which the air is put under pressure and undergoes an increase in temperature. This air is exhausted in step 3 b , and undergoes cooling at the Intercooler 6 to be cooled to the desired temperature for further compression.
  • step 3 c air is then entered in step 3 c to a first radial compressor 8 .
  • the air is then compressed by the first radial compressor 8 , exits the first radial compressor 8 and in step 3 d enters a second radial compressor 10 for further compression.
  • the air flow then goes, in step 3 e , from the second radial compressor 10 to an energy storage unit, e.g., a Thermal Energy Store 12 .
  • the hot compressed air from the second radial compressor 10 is then cooled by the Thermal Energy Store 12 .
  • the heat energy is stored in the Thermal Energy Store 12 for future use and any water that is generated by the cooling process is drained off.
  • the cooled compressed air is then sent to a Safety Cooler 14 in step 3 f , where the air is further cooled prior to being sent in step 3 g to a storage facility, e.g., cavern 16 .
  • This storage of the compressed air in the cavern 16 and the storage of the energy in the Thermal Energy Store 12 typically occurs during non-peak demand operation of the power generation system 2 .
  • energy output can be increased by releasing the stored compressed air back into the system to drive an expander 18 , e.g., a turbine.
  • the cavern 16 releases some of the stored compressed air, in step 3 h , to the Thermal Energy Store 12 for heating. Heat energy is transferred from the Thermal Energy Store 12 to the compressed air and the heated compressed air flows to a particle filter 20 in step 3 i . The heated compressed air then flows, in step 3 j , to an expansion section of turbine 18 . During expansion the air cools and undergoes a pressure drop while producing the work which drives the shaft 26 which in turn spins a portion of a generator 30 for power generation. After expansion the air flows from the turbine 18 to an air outlet 22 in step 3 k , typically for release to atmosphere.
  • Power generation system 2 can also include a shaft 24 for the compressors, a gear box 28 and a motor 32 .
  • FIG. 1 While the system shown in FIG. 1 does allow for storing energy for use during peak demand hours, it can be appreciated that power needs are going to grow and finding ways to meet the growing demand is desirable.
  • the system includes: an air handling unit configured to receive air, to cool the air and to remove moisture from the air; the first compressor fluidly connected to the air handling unit and configured to receive the air from the air handling unit and to exhaust a first compressed, heated air flow; a vapor absorption chiller connected to the first compressor and configured to transfer heat energy between a plurality of mediums and to cool the first compressed, heated air flow; a second compressor connected to the vapor absorption chiller and configured to receive the cooled first compressed, heated air flow and to exhaust a second compressed, heated air flow; an energy storage unit connected to the second compressor and configured to store heat energy from the second compressed, heated air flow; and a storage facility connected to the energy storage unit and configured to store a cooled, compressed air received from the energy storage unit and to selectively release the cooled, compressed air back into the power generation system.
  • a system for cooling air in a power generation system includes: an air handling unit configured to receive air, to cool the air and to remove moisture from the air; a first compressor fluidly connected to the air handling unit and configured to receive the air from the air handling unit and to exhaust a first compressed, heated air flow; a vapor absorption chiller connected to the first compressor and configured to transfer heat energy between a plurality of mediums and to cool the first compressed, heated air flow; and a second compressor connected to the vapor absorption chiller and configured to receive the cooled first compressed, heated air flow and to exhaust a second compressed, heated air flow.
  • the method includes: receiving air at an air handling unit; cooling the air at the air handling unit; removing moisture from the air at the air handling unit; compressing air by a first compressor; exhausting a first compressed, heated air flow from the first compressor; transferring heat energy between a plurality of mediums at an vapor absorption chiller; cooling the first compressed, heated air flow at the vapor absorption chiller; compressing the cooled first compressed, heated air flow; and exhausting a second compressed, heated air flow.
  • FIG. 1 depicts a power generation system and an Advanced Adiabatic Compressed Air Energy Storage (AA-CAES) system;
  • AA-CAES Advanced Adiabatic Compressed Air Energy Storage
  • FIG. 2 illustrates a power generation system and an efficient AA-CAES system according to exemplary embodiments
  • FIG. 3 shows the system of FIG. 2 with illustrative values according to exemplary embodiments
  • FIG. 4 illustrates a power generation system and an another efficient AA-CAES system according to exemplary embodiments
  • FIG. 5 shows the system of FIG. 4 with illustrative values according to exemplary embodiments
  • FIG. 6 illustrates an air cooling system in a power generation system according to exemplary embodiments
  • FIG. 7 illustrates an air handler and a vapor absorption chiller according to exemplary embodiments
  • FIG. 8 shows the system of FIG. 6 with illustrative values according to exemplary embodiments
  • FIGS. 9 and 10 are flowcharts showing a method for capturing heat energy in a power generation system according to exemplary embodiments.
  • FIG. 11 is a flowchart showing a method for cooling air in a power generation system according to exemplary embodiments.
  • exemplary embodiments described herein provide systems and methods for improving efficiency in power generation systems.
  • heat energy typically lost between compressors in a Compressed Air Energy Storage (CAES) system can be recovered for use in a modified adiabatic CAES (AA-CAES) system, an example of which is shown in FIG. 2 .
  • CAES Compressed Air Energy Storage
  • AA-CAES modified adiabatic CAES
  • FIG. 2 shows a power generation system 202 which includes a modified AA-CAES system which captures and stores the heat energy, which is typically lost between an axial compressor 204 and a radial compressor 206 , for use during peak or near peak load conditions. By capturing this heat energy there can be approximately an 8-10 percent improvement in overall operating efficiency of the power generation system 202 when compared with the system 2 shown in FIG. 1 .
  • This system will now be described by generally following the flow of air in the system starting with an air intake to the axial compressor 204 . Initially in step 5 a , air is taken into an axial compressor 204 and compressed during which the air is put under pressure and undergoes an increase in temperature.
  • This air is exhausted from the axial compressor 204 in step 5 b , and undergoes heat exchange in a heat exchanger, e.g., Intercooler 208 , with oil which is in its own closed loop system.
  • a heat exchanger e.g., Intercooler 208
  • the cooled air flow then enters, in step 5 c , the first radial compressor 206 .
  • the air is then compressed by the first radial compressor 206 , exits the first radial compressor 206 and in step 5 d enters a second radial compressor 210 for further compression.
  • the power generation system 202 can include an axial compressor 204 and a single radial compressor 206 .
  • the air flow then goes in step 5 e from the second radial compressor 210 to an energy storage unit, e.g., a Thermal Energy Store 212 .
  • the hot compressed air from the second radial compressor 210 is then cooled by the Thermal Energy Store 212 .
  • the heat energy is stored in the Thermal Energy Store 212 for future use and any water that is generated by the cooling process is drained off.
  • the cooled compressed air is then sent to a Safety Cooler 214 in step 5 f , where the air is further cooled prior to being sent in step 5 g to a storage facility, e.g., cavern 216 .
  • This storage of the compressed air in the cavern 216 and the storage of the energy in the Thermal Energy Store 212 typically occurs during non-peak demand operation of the power generation system 202 .
  • energy output can be increased by releasing the stored compressed air back into the system to drive an expander 218 , e.g., a turbine.
  • the cavern 216 releases some of the stored compressed air in step 5 h which undergoes preheating in an insulated hot oil tank 220 .
  • the released compressed air then flows to the Thermal Energy Store 212 for heating in step 5 i .
  • Heat energy is transferred from the Thermal Energy Store 212 to the compressed air and the heated compressed air flows (optionally) to a particle filter 222 in step 5 j .
  • the heated compressed air then flows in step 5 k from the particle filter 222 to an expansion section of turbine 218 .
  • the power generation system 202 can also include a shaft 230 for the compressors, a gear box 234 and a motor 232 for driving the compressor 204 .
  • oil is initially heated in the Intercooler 208 by the exhaust air from the axial compressor 204 .
  • Other types of compressors may be used in the power generation system 202 .
  • This heated oil is transferred from the Intercooler 208 by, e.g., a hot oil pump 236 , to the insulated hot oil tank 220 .
  • heat is transferred from the hot oil to the compressed air when released from the cavern 216 .
  • This cooled oil is then pumped by a cold oil pump 238 to a cold oil tank 240 which is typically not insulated.
  • the oil used for this closed loop heat transfer process can have a high specific heat.
  • the oil may be any di-thermic oil, for example, a Dowtherm fluid that has a specific heat of 2.3 kJ/kg-K at substantially 250° C.
  • FIG. 3 an illustrative example with values of pressures and temperatures of the air and oil at various points of the system shown in FIG. 2 is shown in FIG. 3 . These values are exemplary and not intended to limit the embodiments.
  • the system in FIG. 3 will operate as described above with respect to the system shown in FIG. 2 and thus this description is omitted.
  • heat energy can be captured and stored for future use in a power generation system 402 as shown in FIG. 4 .
  • the power generation system 402 includes a modified AA-CAES system which stores the heat energy, which is typically lost between an axial compressor 404 and a radial compressor 408 , for use during peak or near peak load conditions. By capturing this heat energy there can be approximately an 8-10 percent improvement in an overall operating efficiency of the power generation system 402 .
  • This system will now be described by generally following the flow of air in the system starting with air intake to the axial compressor 404 . Initially in step 7 a , air is taken into an axial compressor 404 and compressed during which the air is put under pressure and undergoes an increase in temperature.
  • This air is exhausted from the axial compressor 404 in step 7 b , and undergoes heat exchange (i.e., heats an oil or another flow of air) with an insulated hot oil tank 406 .
  • the cooled air flow then, in step 7 c , departs the insulated hot oil tank 406 and enters the first radial compressor 408 .
  • the air is then compressed by the first radial compressor 408 , exits the first radial compressor 408 and in step 7 d enters a second radial compressor 410 for further compression.
  • the number of radial compressors can be different and also the type of compressors may be different.
  • the air flow then goes in step 7 e from the second radial compressor 410 to an energy storage unit, e.g., a Thermal Energy Store 412 .
  • the hot compressed air from the second radial compressor 410 is then cooled by the Thermal Energy Store 412 .
  • the heat energy is stored in the Thermal Energy Store 412 for future use and any water that is generated by the cooling process is drained off.
  • the cooled compressed air is then sent to a Safety Cooler 414 in step 7 f , where the air is further cooled prior to being sent in step 7 g to a storage facility, e.g., cavern 416 .
  • This storage of the compressed air in the cavern 416 and the storage of the heat energy in the Thermal Energy Store 412 typically occurs during non-peak demand operation of the power generation system 402 .
  • energy output can be increased by releasing the stored compressed air back into the system to drive an expander 418 , e.g., a turbine.
  • the cavern 416 releases some of the stored compressed air in step 7 h which undergoes preheating at the insulated hot oil tank 406 .
  • the released compressed air then flows to the Thermal Energy Store 412 for heating in step 7 i .
  • Heat energy is transferred from the Thermal Energy Store 412 to the compressed air and the heated compressed air flows to a particle filter 420 in step 7 j .
  • the heated compressed air then flows in step 7 k from the particle filter 420 to an expansion section of turbine 418 .
  • Power generation system 402 can also include a shaft 428 for the compressors, a gear box 430 and a motor 432 .
  • FIG. 5 an illustrative example with values of the pressures and temperatures of the air and oil at various points of the system shown in FIG. 4 is shown in FIG. 5 . These values are exemplary and not intended to limit the embodiments.
  • the system in FIG. 5 will operate as described above with respect to the system shown in FIG. 4 thus this description is omitted.
  • an air handling unit 604 and a vapor absorption chiller 606 can be implemented in the beginning stages of a power generation system 602 as shown in FIG. 6 .
  • This system will now be described by generally following the flow of air in the system up to the first radial compressor 610 followed by describing the fluid loops in the air handling unit 604 and the vapor absorption chiller 606 .
  • step 9 a air is brought into the air handling unit 604 and cooled, moisture is removed and the air is then taken into the axial compressor 608 .
  • the air is then compressed in the axial compressor 608 , during which the air is put under pressure and undergoes an increase in temperature.
  • This air is exhausted from the axial compressor 608 in step 9 b , and undergoes heat exchange within a vapor absorption chiller 606 .
  • the cooled air flow then, in step 9 c , departs the vapor absorption chiller 606 and enters the first radial compressor 610 .
  • the air is then compressed by the first radial compressor 610 , exits the first radial compressor 610 and in step 9 d enters a second radial compressor 10 for further compression.
  • Elements 10 - 30 are similar to those shown in FIG. 1 thus their description is omitted.
  • the vapor absorption chiller 606 acts as a heat exchanger which in turn allows the exhaust air from the axial compressor 608 to be cooled to the desired temperature, as well as allowing the air handling unit 604 to cool the air prior to air entering the axial compressor 608 as will now be described with respect to FIG. 7 .
  • air enters the air handling unit 604 and is cooled by a cooling loop 702 .
  • Cooling loop 702 can include chilled water or a glycol solution. Additionally, moisture is removed from the air. This cooled air then goes to the axial compressor 608 .
  • the hot exhaust from the axial compressor 608 enters the vapor absorption chiller 606 and is cooled enroute to the first radial compressor 610 by exchanging heat with a refrigerant in a generation stage 704 .
  • the refrigerant vapor within the vapor absorption chiller 606 is evaporated during the generation stage 704 and flows to a condenser 706 .
  • the condenser 706 includes a heat exchanger 708 and outputs a liquid refrigerant which in turn cools the cooling loop 702 as shown in heat exchanger 710 .
  • This refrigerant is then cooled by cooling loop 712 and pumped back by pump 714 to the generation stage 704 .
  • some portion of the refrigerant that remains in a liquid form from the generation stage 704 enters the heat exchanger 710 and is also cooled by the cooling loop 712 prior to being pumped back to the generation stage 704 .
  • FIG. 8 an illustrative example with values of the pressures and temperatures of the air and oil at various points of the system shown in FIG. 6 is shown in FIG. 8 . These values are exemplary and not intended to limit the embodiments.
  • the system in FIG. 8 will operate as described above with respect to the system shown in FIG. 6 thus this description is omitted.
  • a method for capturing heat energy in a power generation system is shown in the flowchart of FIGS. 9 and 10 .
  • the method includes: a step 902 of exhausting a first compressed, heated air flow from a first compressor; a step 904 of storing an oil in an insulated storage tank; a step 906 of receiving the first compressed heated air flow at the insulated storage tank; a step 908 of transferring heat energy from the first compressed heated air flow to the oil at the insulated storage tank; a step 910 of transferring heat energy from the oil after being heated, to a cooled, compressed air at the insulated storage tank; a step 912 of exhausting a second compressed, heated air flow by a second compressor; a step 914 of storing heat energy from the second compressed, heated air flow at an energy storage unit; a step 916 of storing the cooled, compressed air received from the energy storage unit at a storage facility; and a step 918 of selectively releasing the cooled
  • a method for cooling air in a power generation system is shown in the flowchart of FIG. 11 .
  • the method includes: a step 1102 of receiving air at an air handling unit; a step 1104 of cooling the air at the air handling unit to obtain a cooled air; a step 1106 of removing moisture from the cooled air at the air handling unit to obtain a cooled, dry air; a step 1108 of compressing air by a first compressor; a step 1110 of exhausting a first compressed, heated air flow from the first compressor; a step 1112 of transferring heat energy between a plurality of mediums including the compressed, heated air at a vapor absorption chiller; a step 1114 of cooling the first compressed, heated air flow at the vapor absorption chiller; a step 1116 of compressing the cooled first compressed, heated air flow at a second compressor; and a step 1118 of exhausting a second compressed, heated air flow from the second compressor.
US12/915,422 2010-10-29 2010-10-29 Inlet Air Cooling and Moisture Removal Methods and Devices in Advance Adiabatic Compressed Air Energy Storage Systems Abandoned US20120102987A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US12/915,422 US20120102987A1 (en) 2010-10-29 2010-10-29 Inlet Air Cooling and Moisture Removal Methods and Devices in Advance Adiabatic Compressed Air Energy Storage Systems
JP2011233555A JP5981704B2 (ja) 2010-10-29 2011-10-25 先進的断熱圧縮空気エネルギー貯蔵システムの吸気冷却及び水分除去装置並びに方法
EP11186992.1A EP2447505B1 (en) 2010-10-29 2011-10-27 Inlet air cooling and moisture removal methods and devices in advanced adiabatic compressed air energy storage systems
CN2011103461275A CN102538531A (zh) 2010-10-29 2011-10-28 压缩空气蓄能系统中入口空气冷却和水分去除方法和装置
RU2011143462/07A RU2559793C2 (ru) 2010-10-29 2011-10-28 Способ и система для охлаждения воздуха в системе производства электроэнергии (варианты)

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US12/915,422 US20120102987A1 (en) 2010-10-29 2010-10-29 Inlet Air Cooling and Moisture Removal Methods and Devices in Advance Adiabatic Compressed Air Energy Storage Systems

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US (1) US20120102987A1 (zh)
EP (1) EP2447505B1 (zh)
JP (1) JP5981704B2 (zh)
CN (1) CN102538531A (zh)
RU (1) RU2559793C2 (zh)

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US20160326958A1 (en) * 2013-12-16 2016-11-10 Nuovo Pignone Srl Compressed-air-energy-storage (caes) system and method
US20220242581A1 (en) * 2018-03-23 2022-08-04 Raytheon Technologies Corporation Propulsion system cooling control
CN116241436A (zh) * 2023-03-17 2023-06-09 中国电力工程顾问集团中南电力设计院有限公司 全天候压缩机入口定参数运行的压缩空气储能系统及方法

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CN103225598B (zh) * 2013-04-27 2015-11-18 清华大学 一种压缩空气与储热介质同时储能的方法及系统
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WO2016047630A1 (ja) * 2014-09-25 2016-03-31 株式会社神戸製鋼所 コンテナ型圧縮空気貯蔵発電装置
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KR102403512B1 (ko) 2015-04-30 2022-05-31 삼성전자주식회사 공기 조화기의 실외기, 이에 적용되는 컨트롤 장치
JP6373794B2 (ja) * 2015-05-08 2018-08-15 株式会社神戸製鋼所 圧縮空気貯蔵発電装置及び圧縮空気貯蔵発電方法
JP6387325B2 (ja) * 2015-05-11 2018-09-05 株式会社神戸製鋼所 圧縮空気貯蔵発電装置
CN107218132B (zh) * 2016-04-17 2018-10-09 厦门典力节能科技有限公司 智能电网电力负荷储能调度方法
CN107299891B (zh) * 2016-10-12 2019-10-18 清华大学 一种非补燃式压缩空气储能系统
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