CN205779057U - Closed combined cooling and power energy storage system - Google Patents

Closed combined cooling and power energy storage system Download PDF

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CN205779057U
CN205779057U CN201620473716.8U CN201620473716U CN205779057U CN 205779057 U CN205779057 U CN 205779057U CN 201620473716 U CN201620473716 U CN 201620473716U CN 205779057 U CN205779057 U CN 205779057U
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air
compressor
cold
exhaust port
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季伟
孙郁
张武
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Technical Institute of Physics and Chemistry of CAS
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Technical Institute of Physics and Chemistry of CAS
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Abstract

The utility model provides a cold and electricity antithetical couplet of closed supplies energy storage system, include: the energy storage unit comprises an air bag, a compressor set and an air storage tank; the heat recovery unit comprises interstage coolers of all stages of compressors, a cold oil tank, a hot oil tank and interstage heat regenerators of all stages of turboexpanders; the energy release unit comprises a speed regulating valve, a turbo-expander set, a speed reducer, a generator, a grid-connected control cabinet and a cold air conditioner, the whole system is a closed circulation system, air is not required to be supplied from the outside, the air drying and purifying process is reduced, equipment investment and energy consumption are reduced, cold energy is output externally, cold energy is fully utilized for cold fire of exhaust air after expansion, cold-electricity combined supply is realized, the efficiency of the system is improved, and unstable and intermittent wind energy is converted into stable electric energy and cold energy to be output.

Description

Closed combined cooling and power energy storage system
Technical Field
The utility model relates to an energy conversion and storage field, in particular to cold electricity federation of closed supplies energy storage system.
Background
Among all renewable energy sources around the world, wind energy accounts for 42% of them. Meanwhile, the wind power generation technology has great advantages in the aspects of technical maturity and economic benefit and various renewable energy distributed generation technologies, so that the wind power generation technology is a new energy distributed generation technology with the fastest development speed in the world. According to the forecast of the China renewable energy industry Association, the China wind power general installation will exceed 300GW by the end of 2020.
However, wind energy is affected by natural conditions such as weather, geographical position, airflow variation and other factors, and has the characteristics of great uncertainty, randomness, intermittency and the like, and great impact is brought to the dispatching, operation mode, reliability, electric energy quality and operation cost of a power grid. With the increasing wind power scale, the compatibility problem of the wind power and the power grid becomes more prominent, and a feasible solution is urgently needed to promote the large-scale utilization of the wind power. Among various methods for solving the wind power grid connection, the energy storage technology is known as a main approach for fundamentally solving the large-scale wind power grid connection problem. At present, the energy storage technology in domestic industrial technology mainly comprises pumped storage, Compressed Air Energy Storage (CAES), flywheel energy storage, electromagnetic energy storage, electrochemical energy storage and the like. The compressed air energy storage is a novel energy storage technology and gets more and more extensive attention of scholars at home and abroad.
The compressed air energy storage technology utilizes electric energy generated by intermittent renewable energy sources to drive a compressor unit to compress air, stores the electric energy in a high-pressure air mode, and releases the high-pressure air to drive an expander to do work and generate power when the electric energy is needed. Since Stal Laval proposed the use of underground caverns for compressed air energy storage in 1949, both domestic and foreign scholars have conducted a great deal of research and practice work on this, and two large power plants have been put into commercial operation in germany (Huntorf) and the united states (McIntosh), respectively. In addition, compressed air energy storage power station projects are in the process of construction in Japan, Italy, Israel and other countries respectively. However, most of the existing compressed air energy storage technologies are open-cycle technologies, and cannot provide cooling capacity, so that the system circulation efficiency is not high.
SUMMERY OF THE UTILITY MODEL
In view of the above, there is a need for a closed combined cooling and power energy storage system for converting unstable and intermittent wind energy into stable electric energy and cold output.
In order to achieve the purpose, the following technical scheme is adopted in the application:
a closed cogeneration energy storage system comprising: the energy storage unit, the heat regeneration unit and the energy release unit;
the energy storage unit comprises an air bag (21), a primary compressor (1), a secondary compressor (2), a tertiary compressor (3) and an air storage tank (9);
the heat recovery unit comprises a primary cooler (4), a secondary cooler (5), a tertiary cooler (6), a cold oil tank (8), a hot oil tank (7), a primary heat recovery device (10), a secondary heat recovery device (11) and a tertiary heat recovery device (12);
the energy release unit comprises a speed regulating valve (13), a primary turbine expander (14), a secondary turbine expander (15), a tertiary turbine expander (16), a speed reducer (17), a generator (18), a grid-connected control cabinet (19) and a cold air conditioner (20);
an exhaust port of the air bag (21) is connected with an air inlet of the primary compressor (1), an exhaust port of the primary compressor (1) is connected with an air inlet of the primary cooler (4), an exhaust port of the primary cooler (4) is connected with an air inlet of the secondary compressor (2), an exhaust port of the secondary compressor (2) is connected with an air inlet of the secondary cooler (5), an exhaust port of the secondary cooler (4) is connected with an air inlet of the tertiary compressor (3), an exhaust port of the tertiary compressor (3) is connected with an air inlet of the tertiary cooler (6), and an exhaust port of the tertiary cooler (6) is connected with an air inlet of the air storage tank (9) to form a closed flow passage in an energy storage stage;
the exhaust port of the air storage tank (9) is connected with the air inlet of the speed regulating valve (13), the exhaust port of the speed regulating valve (13) is connected with the air inlet of the first-stage turbo expander (14), the exhaust port of the primary turbine expander (14) is connected with the air inlet of the primary heat regenerator (10), the exhaust port of the primary regenerator (10) is connected with the air inlet of the secondary regenerator (11), the exhaust port of the secondary heat regenerator (11) is connected with the air inlet of the secondary turbo expander (15), the exhaust port of the secondary turbine expansion machine (15) is connected with the air inlet of the tertiary heat regenerator (12), the exhaust port of the three-stage heat regenerator (12) is connected with the air inlet of the cold air conditioner (20), the exhaust port of the cold air conditioner (20) is connected with the air inlet of the air bag (21), and the air channels form a closed channel in an energy release stage;
the heat conducting oil in the cold oil tank (8) and the hot oil tank (7) flows in a reciprocating manner in an internal circulation mode in a tube pass formed by the primary cooler (4), the secondary cooler (5) and the tertiary cooler (6) and a tube pass formed by the primary turboexpander (14), the secondary turboexpander (15) and the tertiary turboexpander (16);
the output shafts of the first-stage turbo expander (14), the second-stage turbo expander (15) and the third-stage turbo expander (16) are connected with the high-speed shaft of the speed reducer (17) through a coupler, the input shaft of the generator (18) is connected with the low-speed output shaft of the speed reducer (17) through a coupler, and electric energy generated by the generator (18) is input into a power grid through a grid-connected control cabinet 19.
In some embodiments, the air bag is an atmospheric-pressure and normal-temperature air storage bag for storing dry and clean air.
In some embodiments, the compressor set formed by the first-stage compressor (1), the second-stage compressor (2) and the third-stage compressor is a multi-stage centrifugal compressor or a multi-stage axial compressor, or any combination of the two structures.
In some embodiments, the primary cooler (4), secondary cooler (5), tertiary cooler (6), primary regenerator (10), secondary regenerator (11), and tertiary regenerator (12) are any one of a shell and tube heat exchanger, a double tube heat exchanger, and a plate and fin heat exchanger.
In some embodiments, the cold oil tank (8) and the hot oil tank (7) are both normal-pressure oil tanks, and heat-storage medium heat-conducting oil is stored in the normal-pressure oil tanks.
In some embodiments, the speed valve is a single throttle or is connected in parallel by multiple throttles.
In some embodiments, the turboexpander set formed by the one-stage turboexpander (14), the two-stage turboexpander (15) and the three-stage turboexpander (16) is a multi-stage radial-axial flow type expander or a multi-stage axial flow type expander, or any combination of the two structures.
In some embodiments, the reducer (17) is a multi-stage parallel shaft structure or a multi-stage planetary gear structure.
In some embodiments, the heat exchange structure in the cold-air conditioner (20) is of a wound tube type, or a fin type; the medium is wind-wind type, or wind-water type, or the arbitrary combination of the above two structures.
In some embodiments, the pressure of the high-pressure air in the air storage tank (9) is 3-10 MPa, the exhaust flow is 6000-100000 Nm3/h, the temperature of each stage of expansion gas after heat recovery is 80-120 ℃, and the exhaust temperature of the last stage is-5-10 ℃; the system has the installed generating capacity of 0.5-10 MW and the output cold energy of 20-400 KW.
The utility model adopts the above technical scheme, its beneficial effect lies in:
the utility model provides a cold and electricity antithetical couplet of closed supplies energy storage system, include: the energy storage unit comprises an air bag, a compressor set and an air storage tank; the heat recovery unit comprises interstage coolers of all stages of compressors, a cold oil tank, a hot oil tank and interstage heat regenerators of all stages of turboexpanders; the energy release unit comprises a speed regulating valve, a turbo-expander set, a speed reducer, a generator, a grid-connected control cabinet and a cold air conditioner, the whole system is a closed circulation system, air is not required to be supplied from the outside, the air drying and purifying process is reduced, equipment investment and energy consumption are reduced, cold energy is output externally, cold energy is fully utilized for cold fire of exhaust air after expansion, cold-electricity combined supply is realized, the efficiency of the system is improved, and unstable and intermittent wind energy is converted into stable electric energy and cold energy to be output.
Drawings
Fig. 1 is the utility model provides a closed combined cooling and power energy storage system's schematic structure.
Wherein: the system comprises a primary compressor (1), a secondary compressor (2), a tertiary compressor (3), a primary cooler (4), a secondary cooler (5), a tertiary cooler (6), a hot oil tank (7), a cold oil tank (8), an air storage tank (9), a tertiary heat regenerator (10), a secondary heat regenerator (11), a primary heat regenerator (12), a speed regulating valve (13), a primary turboexpander (14), a secondary turboexpander (15), a tertiary turboexpander (16), a speed reducer (17), a generator (18), a grid-connected control cabinet (19), a cold air conditioner (20) and an air bag (21).
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, the terms "inside", "outside", "longitudinal", "lateral", "up", "down", "top", "bottom", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description of the present invention rather than requiring the present invention to be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
Please refer to fig. 1, which is a schematic structural diagram of a closed combined cooling and power energy storage system 100 according to the present invention, including: the energy storage unit, backheating unit and energy release unit.
The energy storage unit comprises an air bag (21), a primary compressor (1), a secondary compressor (2), a tertiary compressor (3) and an air storage tank (9).
The heat recovery unit comprises a primary cooler (4), a secondary cooler (5), a tertiary cooler (6), a cold oil tank (8), a hot oil tank (7), a primary heat recovery device (10), a secondary heat recovery device (11) and a tertiary heat recovery device (12).
The energy release unit comprises a speed regulating valve (13), a primary turbine expansion machine (14), a secondary turbine expansion machine (15), a tertiary turbine expansion machine (16), a speed reducer (17), a generator (18), a grid-connected control cabinet (19) and a cold air conditioner (20).
Wherein,
an exhaust port of the air bag (21) is connected with an air inlet of the primary compressor (1), an exhaust port of the primary compressor (1) is connected with an air inlet of the primary cooler (4), an exhaust port of the primary cooler (4) is connected with an air inlet of the secondary compressor (2), an exhaust port of the secondary compressor (2) is connected with an air inlet of the secondary cooler (5), an exhaust port of the secondary cooler (4) is connected with an air inlet of the tertiary compressor (3), an exhaust port of the tertiary compressor (3) is connected with an air inlet of the tertiary cooler (6), and an exhaust port of the tertiary cooler (6) is connected with an air inlet of the air storage tank (9) to form a closed flow passage in an energy storage stage;
the exhaust port of the air storage tank (9) is connected with the air inlet of the speed regulating valve (13), the exhaust port of the speed regulating valve (13) is connected with the air inlet of the first-stage turbo expander (14), the exhaust port of the primary turbine expander (14) is connected with the air inlet of the primary heat regenerator (10), the exhaust port of the primary regenerator (10) is connected with the air inlet of the secondary regenerator (11), the exhaust port of the secondary heat regenerator (11) is connected with the air inlet of the secondary turbo expander (15), the exhaust port of the secondary turbine expansion machine (15) is connected with the air inlet of the tertiary heat regenerator (12), the exhaust port of the three-stage heat regenerator (12) is connected with the air inlet of the cold air conditioner (20), the exhaust port of the cold air conditioner (20) is connected with the air inlet of the air bag (21), and the air channels form a closed channel in an energy release stage;
the heat conducting oil in the cold oil tank (8) and the hot oil tank (7) flows in a reciprocating manner in an internal circulation mode in a tube pass formed by the primary cooler (4), the secondary cooler (5) and the tertiary cooler (6) and a tube pass formed by the primary turboexpander (14), the secondary turboexpander (15) and the tertiary turboexpander (16);
the output shafts of the first-stage turbo expander (14), the second-stage turbo expander (15) and the third-stage turbo expander (16) are connected with the high-speed shaft of the speed reducer (17) through a coupler, the input shaft of the generator (18) is connected with the low-speed output shaft of the speed reducer (17) through a coupler, and electric energy generated by the generator (18) is input into a power grid through a grid-connected control cabinet 19.
It can be understood that in the energy storage process of the closed combined cooling and power energy storage system, a compressor unit formed by the primary compressor (1), the secondary compressor (2) and the tertiary compressor (3) compresses the processed dry and clean normal-pressure air in the air bag (21) into high-pressure air by using renewable intermittent energy such as wind energy, solar energy and the like to store the high-pressure air in the air storage tank (9). Meanwhile, as the energy storage process and the energy release process are not carried out simultaneously, when the compressor unit carries out interstage cooling, in order to improve the power generation efficiency of the system, the compression heat of the gas at the outlet of each stage of compressor needs to be stored in a hot oil tank (7) by taking heat conduction oil as a heat storage medium; in the energy release process, the air storage tank (9) releases high-pressure air, the air pressure is reduced to the design pressure of inlets of the first-stage turbo expander (14), the second-stage turbo expander (15) and the third-stage turbo expander (16) through throttling and pressure reduction of the speed regulating valve (13), and meanwhile, the gas flow is kept unchanged. Then, the gas in each stage of heat regenerator and the high-temperature heat conduction oil from the heat oil tank (7) perform sufficient heat exchange, the inlet temperature and enthalpy of each stage of expander are improved, and expansion work is performed. And the high-temperature heat conduction oil flows back to cold oil after heat exchange is completed, and waits for heat storage in the next energy storage process. The expanded normal-pressure low-temperature gas flows through a cold air conditioner (20) to provide cold air indoors or provide cold for a cold storage. Finally, the air flows back to the air bag. Therefore, the whole process is a closed cycle, air is not required to be supplied from the outside, the air drying and purifying process is reduced, meanwhile, unstable and intermittent wind energy and solar energy are converted into stable electric energy and cold energy to be output, and the cold-electricity combined supply type energy storage device is realized.
Preferably, the air bag (21) is a normal-pressure normal-temperature air storage bag for storing dry and clean air.
Preferably, the compressor unit formed by the first-stage compressor (1), the second-stage compressor (2) and the third-stage compressor is a multi-stage centrifugal compressor, a multi-stage axial compressor or any combination of the two structures.
Preferably, the primary cooler (4), the secondary cooler (5), the tertiary cooler (6), the primary regenerator (10), the secondary regenerator (11) and the tertiary regenerator (12) are any one of a shell-and-tube heat exchanger, a double-tube heat exchanger and a plate-fin heat exchanger.
Preferably, the cold oil tank (8) and the hot oil tank (7) are both normal-pressure oil tanks, and heat-storage medium heat-conducting oil is stored in the normal-pressure oil tanks.
Preferably, the speed regulating valve (13) is a single throttle valve or is connected in parallel by a plurality of throttle valves.
Preferably, the turbo expander set formed by the first-stage turbo expander (14), the second-stage turbo expander (15) and the third-stage turbo expander (16) is a multi-stage radial-axial flow type expander, a multi-stage axial flow type expander or any combination of the two structures.
Preferably, the speed reducer (17) is of a multi-stage parallel shaft structure or a multi-stage planetary gear structure.
Preferably, the heat exchange structure in the cold air conditioner (20) is a wound pipe type or a fin type; the medium is wind-wind type, or wind-water type, or the arbitrary combination of the above two structures.
Preferably, the pressure of high-pressure air in the air storage tank (9) is 3-10 MPa, the exhaust flow is 6000-100000 Nm3/h, the temperature of each stage of expanded gas after heat regeneration is 80-120 ℃, and the exhaust temperature of the last stage is-5-10 ℃; the system has the installed generating capacity of 0.5-10 MW and the output cold energy of 20-400 KW.
The utility model provides a cold electricity antithetical couplet of closed supplies energy storage system is a closed circulation system, does not need external supply air, has reduced the flow that the air drying purifies, and equipment investment and energy consumption are external output cold volume simultaneously, make full use of the cold fire of exhaust gas after the inflation usefulness, have realized the cold electricity antithetical couplet supplies, have improved the efficiency of system, have realized converting unstable and intermittent type nature wind energy into stable electric energy and cold volume output.
Although the present invention has been described with reference to the presently preferred embodiments, it will be understood by those skilled in the art that the foregoing preferred embodiments are merely illustrative of the present invention and are not intended to limit the scope of the present invention, and that any modifications, equivalent substitutions, improvements, etc. made within the spirit and scope of the present invention should be included within the scope of the present invention.

Claims (10)

1. The utility model provides a closed combined cooling and power energy storage system which characterized in that includes: the energy storage unit, the heat regeneration unit and the energy release unit;
the energy storage unit comprises an air bag (21), a primary compressor (1), a secondary compressor (2), a tertiary compressor (3) and an air storage tank (9);
the heat recovery unit comprises a primary cooler (4), a secondary cooler (5), a tertiary cooler (6), a cold oil tank (8), a hot oil tank (7), a primary heat recovery device (10), a secondary heat recovery device (11) and a tertiary heat recovery device (12);
the energy release unit comprises a speed regulating valve (13), a primary turbine expander (14), a secondary turbine expander (15), a tertiary turbine expander (16), a speed reducer (17), a generator (18), a grid-connected control cabinet (19) and a cold air conditioner (20);
an exhaust port of the air bag (21) is connected with an air inlet of the primary compressor (1), an exhaust port of the primary compressor (1) is connected with an air inlet of the primary cooler (4), an exhaust port of the primary cooler (4) is connected with an air inlet of the secondary compressor (2), an exhaust port of the secondary compressor (2) is connected with an air inlet of the secondary cooler (5), an exhaust port of the secondary cooler (4) is connected with an air inlet of the tertiary compressor (3), an exhaust port of the tertiary compressor (3) is connected with an air inlet of the tertiary cooler (6), and an exhaust port of the tertiary cooler (6) is connected with an air inlet of the air storage tank (9) to form a closed flow passage in an energy storage stage;
the exhaust port of the air storage tank (9) is connected with the air inlet of the speed regulating valve (13), the exhaust port of the speed regulating valve (13) is connected with the air inlet of the first-stage turbo expander (14), the exhaust port of the primary turbine expander (14) is connected with the air inlet of the primary heat regenerator (10), the exhaust port of the primary regenerator (10) is connected with the air inlet of the secondary regenerator (11), the exhaust port of the secondary heat regenerator (11) is connected with the air inlet of the secondary turbo expander (15), the exhaust port of the secondary turbine expansion machine (15) is connected with the air inlet of the tertiary heat regenerator (12), the exhaust port of the three-stage heat regenerator (12) is connected with the air inlet of the cold air conditioner (20), the exhaust port of the cold air conditioner (20) is connected with the air inlet of the air bag (21), and the air channels form a closed channel in an energy release stage;
the heat conducting oil in the cold oil tank (8) and the hot oil tank (7) flows in a reciprocating manner in an internal circulation mode in a tube pass formed by the primary cooler (4), the secondary cooler (5) and the tertiary cooler (6) and a tube pass formed by the primary turboexpander (14), the secondary turboexpander (15) and the tertiary turboexpander (16);
the output shafts of the first-stage turbo expander (14), the second-stage turbo expander (15) and the third-stage turbo expander (16) are connected with the high-speed shaft of the speed reducer (17) through a coupler, the input shaft of the generator (18) is connected with the low-speed output shaft of the speed reducer (17) through a coupler, and electric energy generated by the generator (18) is input into a power grid through a grid-connected control cabinet (19).
2. The closed combined cooling and power energy storage system according to claim 1, wherein the air bag is a normal-pressure normal-temperature air storage bag for storing dry and clean air.
3. The closed combined cooling and power energy storage system according to claim 1, wherein the compressor unit formed by the first-stage compressor (1), the second-stage compressor (2) and the third-stage compressor is a multi-stage centrifugal compressor, a multi-stage axial compressor or any combination of the two structures.
4. The closed cogeneration energy storage system of claim 1, wherein said primary cooler (4), secondary cooler (5), tertiary cooler (6), primary regenerator (10), secondary regenerator (11) and tertiary regenerator (12) are any one of a shell-and-tube heat exchanger, a double-tube heat exchanger, and a plate-fin heat exchanger.
5. The closed combined cooling and power energy storage system according to claim 1, wherein the cold oil tank (8) and the hot oil tank (7) are both normal pressure oil tanks, and heat transfer oil as a heat storage medium is stored therein.
6. The closed combined cooling and power energy storage system according to claim 1, wherein the speed regulating valve is a single throttle valve or a plurality of throttle valves are connected in parallel.
7. The closed combined cooling and power energy storage system according to claim 1, wherein the turbo-expander set formed by the one-stage turbo-expander (14), the two-stage turbo-expander (15) and the three-stage turbo-expander (16) is a multi-stage radial-axial flow type expander or a multi-stage axial-flow type expander or any combination of the two structures.
8. The closed cogeneration energy storage system of claim 1 wherein said reducer (17) is of a multi-stage parallel shaft configuration or a multi-stage planetary gear configuration.
9. The closed combined cooling and power energy storage system according to claim 1, wherein the heat exchange structure in the cold air conditioner (20) is a wound tube type or a fin type; the medium is wind-wind type, or wind-water type, or the arbitrary combination of the above two structures.
10. The closed combined cooling and power energy storage system according to any one of claims 1-9, wherein the pressure of the high-pressure air in the air storage tank (9) is 3-10 MPa, the exhaust flow is 6000-100000 Nm3/h, the temperature of the expanded gas after each stage of heat recovery is 80-120 ℃, and the exhaust temperature of the last stage is-5-10 ℃; the system has the installed generating capacity of 0.5-10 MW and the output cold energy of 20-400 KW.
CN201620473716.8U 2016-05-23 2016-05-23 Closed combined cooling and power energy storage system Active CN205779057U (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105863753A (en) * 2016-05-23 2016-08-17 中国科学院理化技术研究所 Closed combined cooling and power energy storage system
CN106677988A (en) * 2017-02-16 2017-05-17 中国科学院理化技术研究所 Wind-solar energy storage system
CN107542649A (en) * 2017-09-25 2018-01-05 中国科学院理化技术研究所 Low-temperature high-pressure liquid air energy storage system
CN107939654A (en) * 2017-10-24 2018-04-20 国家电网公司 Supply of cooling, heating and electrical powers compressed-air energy-storage system
CN107956523A (en) * 2017-11-20 2018-04-24 清华大学 A kind of 50MW adiabatic compressions air energy storage method
CN108331618A (en) * 2018-02-05 2018-07-27 清华大学 A kind of 10MW compressed-air energy storages method and system
CN108412563A (en) * 2018-03-27 2018-08-17 哈尔滨电气股份有限公司 Three turbines, three regenerator supercritical carbon dioxide cycle generating system for gas turbine waste heat recovery
CN111255720A (en) * 2020-01-19 2020-06-09 中国科学院工程热物理研究所 Temperature control variable working condition operation system based on heat accumulation type compressed air energy storage
CN114704456A (en) * 2022-03-31 2022-07-05 西安交通大学 Multisource heat storage compressed air energy storage system for coupling electric heat storage

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105863753A (en) * 2016-05-23 2016-08-17 中国科学院理化技术研究所 Closed combined cooling and power energy storage system
CN106677988A (en) * 2017-02-16 2017-05-17 中国科学院理化技术研究所 Wind-solar energy storage system
CN106677988B (en) * 2017-02-16 2023-06-20 中国科学院理化技术研究所 Wind-solar energy storage system
CN107542649A (en) * 2017-09-25 2018-01-05 中国科学院理化技术研究所 Low-temperature high-pressure liquid air energy storage system
CN107939654A (en) * 2017-10-24 2018-04-20 国家电网公司 Supply of cooling, heating and electrical powers compressed-air energy-storage system
CN107956523A (en) * 2017-11-20 2018-04-24 清华大学 A kind of 50MW adiabatic compressions air energy storage method
CN108331618A (en) * 2018-02-05 2018-07-27 清华大学 A kind of 10MW compressed-air energy storages method and system
CN108412563A (en) * 2018-03-27 2018-08-17 哈尔滨电气股份有限公司 Three turbines, three regenerator supercritical carbon dioxide cycle generating system for gas turbine waste heat recovery
CN111255720A (en) * 2020-01-19 2020-06-09 中国科学院工程热物理研究所 Temperature control variable working condition operation system based on heat accumulation type compressed air energy storage
CN111255720B (en) * 2020-01-19 2021-04-30 中国科学院工程热物理研究所 Temperature control variable working condition operation system based on heat accumulation type compressed air energy storage
CN114704456A (en) * 2022-03-31 2022-07-05 西安交通大学 Multisource heat storage compressed air energy storage system for coupling electric heat storage

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