Gas turbine combined cycle heat pump system

Abstract

This invention provides a gas turbine-type combined cycle heat pump system, belonging to the field of heat pump technology. An external air passage connects to the combustion chamber via a compressor; an external fuel passage connects to the combustion chamber; the combustion chamber also has a gas passage connecting to the outside via a gas turbine, a high-temperature steam generator, and a low-temperature steam generator; a second compressor connects to a heater; the heater connects to the low-temperature steam generator via a booster pump; the heater connects to an evaporator via a throttling valve; the evaporator connects to the low-pressure steam inlet of the ejector; the low-temperature steam generator connects to the high-pressure steam inlet of the ejector; the ejector connects to the second compressor; an external liquid medium pipeline connects to the high-pressure steam inlet of the second ejector via a second booster pump and a high-temperature steam generator; an external heated medium passage connects to the low-pressure steam inlet of the second ejector via the heater; the second ejector also has a user steam passage connecting to the outside; and the evaporator also has a low-temperature heat medium passage connecting to the outside, forming a gas turbine-type combined cycle heat pump system.

Description

Technical fields:

[0001] This invention belongs to the field of thermodynamics and heat pump technology. Background technology:

[0002] People need cold / heat / steam / power in their lives and production processes. Using heat pump technology to obtain cold / heat / steam / power is an important means to achieve efficient and high-value energy utilization. In practical applications, it is necessary to comprehensively consider the heat pump's operating parameters, performance index, manufacturing cost, adaptability, as well as the characteristics of different energy sources and targeted technical means.

[0003] High-quality fuels, typically represented by natural gas, gasoline, and diesel, are high-temperature heat sources with temperatures exceeding several thousand degrees Celsius. Achieving efficient and high-value utilization of these fuels in refrigeration, heating, steam production, and power generation, and leveraging their leading role as high-quality energy sources, presents a significant technological challenge.

[0004] Vapor compression heat pump technology, which operates on the principle of reverse Rankine cycle, has the advantage of being able to achieve constant-temperature heat absorption; however, meeting the demand for high-parameter heating or steam is technically challenging.

[0005] An ejector is a pressure-boosting component that effectively utilizes high-temperature heat resources. It has the advantages of simple structure, reliable operation, low investment and long service life. In addition, compared with compressors, ejectors are more adaptable to the compression of wet steam.

[0006] Based on the fundamental principles of simple and efficient use of high-quality fuels for refrigeration / heating / steam production / power, this invention presents a gas turbine combined cycle heat pump system with integrated technology, a reasonable process, a simple structure, and optimized performance index. Summary of the Invention:

[0007] The main objective of this invention is to provide a gas turbine-based combined cycle heat pump system. The specific contents of the invention are described in detail below:

[0008] 1. A gas turbine-type combined cycle heat pump system mainly consists of a compressor, combustion chamber, gas turbine, high-temperature steam generator, low-temperature steam generator, second compressor, heater, booster pump, throttle valve, evaporator, ejector, second booster pump, and second ejector. It has an external air passage connecting to the compressor, an external air passage connecting to the combustion chamber, an external fuel passage connecting to the combustion chamber, a gas passage connecting the combustion chamber to the gas turbine, and a gas passage connecting the gas turbine to the high-temperature and low-temperature steam generators before connecting to the outside. The second compressor has a refrigerant vapor passage connecting to the heater, and the heater also has a condensate line connected to the low-temperature steam generator via the booster pump. The heater also has a condensate line connected to the throttle valve... The valve is connected to the evaporator, which also has a refrigerant vapor channel connecting to the low-pressure steam inlet of the ejector. The low-temperature steam generator also has a steam channel connecting to the high-pressure steam inlet of the ejector. The ejector also has a medium-pressure refrigerant vapor channel connecting to the second compressor. An external liquid medium pipeline connects to the high-temperature steam generator via the second booster pump. The high-temperature steam generator then has a steam channel connecting to the high-pressure steam inlet of the second ejector. An external heated medium channel connects to the heater and then to the low-pressure steam inlet of the second ejector. The second ejector also has a user steam channel connecting to the outside. The evaporator also has a low-temperature heat medium channel connecting to the outside. The gas turbine connects to the compressor and the second compressor and transmits power, forming a gas turbine-type combined cycle heat pump system.

[0009] 2. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system described in item 1, wherein a high-temperature regenerator is added, the compressor is modified from having an air passage connected to the combustion chamber to having an air passage connected to the combustion chamber via the high-temperature regenerator, and the gas turbine is modified from having a gas passage connected to the high-temperature steam generator to having a gas passage connected to the high-temperature steam generator via the high-temperature regenerator, thus forming a gas turbine-type combined cycle heat pump system.

[0010] 3. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system described in item 1, with the addition of a high-temperature regenerator. The compressor is changed from having an air passage connected to the combustion chamber to having an air passage connected to the combustion chamber via the high-temperature regenerator. The gas turbine is changed from having a gas passage connected to the high-temperature steam generator to having a gas passage connected to itself via the high-temperature regenerator, and then having a gas passage connected to the high-temperature steam generator, thus forming a gas turbine-type combined cycle heat pump system.

[0011] 4. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system described in item 1, with the addition of a high-temperature regenerator. The compressor's air passage connection to the combustion chamber is adjusted to a connection between the compressor and itself via the high-temperature regenerator, and then the compressor has an air passage connecting to the combustion chamber. The gas turbine's gas passage connection to the high-temperature steam generator is adjusted to a connection between the gas turbine and the high-temperature steam generator via the high-temperature regenerator, thus forming a gas turbine-type combined cycle heat pump system.

[0012] 5. A gas turbine-type combined cycle heat pump system is formed by adding a regenerator to any of the gas turbine-type combined cycle heat pump systems described in items 1-4. The original system is modified so that the condensate pipe of the heater is connected to the evaporator via a throttling valve, and the condensate pipe of the heater is connected to the evaporator via the regenerator and the throttling valve. The original system is modified so that the injector has a refrigerant vapor passage connected to the second compressor, and the injector has a refrigerant vapor passage connected to the second compressor via the regenerator, thus forming a gas turbine-type combined cycle heat pump system.

[0013] 6. A gas turbine-type combined cycle heat pump system, in any of the gas turbine-type combined cycle heat pump systems described in items 1-4, with the addition of a regenerator, the refrigerant vapor passage of the evaporator connected to the low-pressure steam inlet of the ejector is adjusted so that the refrigerant vapor passage of the evaporator passes through the regenerator and then connects to the low-pressure steam inlet of the ejector, and the condensate pipeline of the heater is connected to the evaporator through a throttling valve is adjusted so that the condensate pipeline of the heater passes through the regenerator and the throttling valve and then connects to the evaporator, thus forming a gas turbine-type combined cycle heat pump system.

[0014] 7. A gas turbine-type combined cycle heat pump system, comprising any one of the gas turbine-type combined cycle heat pump systems described in items 1-4, wherein a regenerator and a second regenerator are added, the refrigerant vapor passage of the evaporator is adjusted to connect to the low-pressure steam inlet of the ejector via the second regenerator, the refrigerant vapor passage of the evaporator is adjusted to connect to the low-pressure steam inlet of the ejector, the condensate pipe of the heater is adjusted to connect to the evaporator via the regenerator, the second regenerator and the throttling valve, and the refrigerant vapor passage of the ejector is adjusted to connect to the second compressor via the regenerator, thus forming a gas turbine-type combined cycle heat pump system.

[0015] 8. A gas turbine-type combined cycle heat pump system, comprising any one of the gas turbine-type combined cycle heat pump systems described in items 1-4, wherein a regenerator, an expander, and a second heater are added. The second compressor is adjusted so that it has a refrigerant vapor channel connected to the heater, and then splits into two paths—the first path connects to the heater and the second path connects to the expander. The expander also has a refrigerant vapor channel connected to the regenerator, and then connected to the second compressor through an intermediate port. The heater has a condensate pipeline connected to the evaporator via a throttling valve, and is adjusted so that the heater has a refrigerant medium pipeline with either fully condensed or partially condensed refrigerant connected to the evaporator via the regenerator and the throttling valve. The second heater also has a heated medium channel connected to the outside. The expander is connected to the second compressor and transmits power, forming a gas turbine-type combined cycle heat pump system.

[0016] 9. A gas turbine-type combined cycle heat pump system, comprising any one of the gas turbine-type combined cycle heat pump systems described in items 1-4, with the addition of a regenerator, a second regenerator, an expander, and a second heater. The evaporator is configured to have a refrigerant vapor channel connected to the low-pressure steam inlet of the ejector, and the refrigerant vapor channel of the evaporator is adjusted to connect to the low-pressure steam inlet of the ejector after passing through the second regenerator. The second compressor is configured to have a refrigerant vapor channel connected to the heater, and the refrigerant vapor channel of the second compressor is adjusted to connect to the second heater and then split into two paths—the first path connects to the heater and the second path connects to the expander. The expander also has a refrigerant vapor channel connected to the regenerator and then connected to the second compressor via an intermediate port. The heater has a condensate pipeline connected to the evaporator via a throttling valve, and the refrigerant medium pipeline (whether fully condensed or partially condensed) is adjusted to connect to the evaporator after passing through the regenerator, the second regenerator, and the throttling valve. The second heater also has a heated medium channel connected to the outside. The expander is connected to the second compressor and transmits power, thus forming a gas turbine-type combined cycle heat pump system.

[0017] 10. A gas turbine-type combined cycle heat pump system is formed by adding a two-phase expander to replace the throttle valve in any of the gas turbine-type combined cycle heat pump systems described in items 1-9. The two-phase expander is connected to a second compressor and transmits power to form a gas turbine-type combined cycle heat pump system.

[0018] 11. A gas turbine-type combined cycle heat pump system is formed by adding a nozzle and replacing the throttle valve to any of the gas turbine-type combined cycle heat pump systems described in items 1-9 to form a gas turbine-type combined cycle heat pump system.

[0019] 12. A gas turbine-type combined cycle heat pump system is formed by adding a nozzle and replacing the throttle valve to any of the gas turbine-type combined cycle heat pump systems described in items 8-9, adding a dual-energy compressor and replacing the second compressor, and adding an expander speed-up unit and replacing the expander.

[0020] 13. A gas turbine-type combined cycle heat pump system, wherein in any of the gas turbine-type combined cycle heat pump systems described in items 1-4, a nozzle and a steam distribution chamber are added, and the heating unit is adjusted so that the condensate pipe is connected to the evaporator via a throttling valve, and the heating unit is connected to the steam distribution chamber via a nozzle. The steam distribution chamber also has a refrigerant vapor passage connected to the second compressor through an intermediate port, and the steam distribution chamber also has a condensate pipe connected to the evaporator via a throttling valve, thus forming a gas turbine-type combined cycle heat pump system.

[0021] 14. A gas turbine-type combined cycle heat pump system, comprising any one of the gas turbine-type combined cycle heat pump systems described in items 1-4, wherein a regenerator, a nozzle, and a steam distribution chamber are added; the evaporator is modified so that the refrigerant vapor passage connecting to the low-pressure steam inlet of the ejector is changed to the evaporator having a refrigerant vapor passage that connects to the low-pressure steam inlet of the ejector after passing through the regenerator; the heater is modified so that the condensate pipeline connecting to the evaporator through a throttling valve is changed to the heater having a condensate pipeline that connects to the steam distribution chamber through the nozzle; the steam distribution chamber also has a refrigerant vapor passage that connects to the second compressor through an intermediate port; and the steam distribution chamber also has a condensate pipeline that connects to the evaporator through the regenerator and the throttling valve, thus forming a gas turbine-type combined cycle heat pump system.

[0022] 15. A gas turbine-type combined cycle heat pump system is formed by adding a second nozzle and replacing the throttle valve to any of the gas turbine-type combined cycle heat pump systems described in items 13-14, thereby forming a gas turbine-type combined cycle heat pump system.

[0023] 16. A gas turbine-type combined cycle heat pump system is any one of the gas turbine-type combined cycle heat pump systems described in items 1-15, with the addition of a high-temperature heat exchanger, changing the air passage connecting to the combustion chamber to connect to the high-temperature heat exchanger before connecting to the combustion chamber, and the high-temperature heat exchanger also having a high-temperature heat medium passage connecting to the outside, thus forming a gas turbine-type combined cycle heat pump system.

[0024] 17. A gas turbine-type combined cycle heat pump system is any one of the gas turbine-type combined cycle heat pump systems described in items 1-16, with the addition of a heater and a heat source regenerator. An external fuel passage connects to the heater, and an external air passage connects to the heater via the heat source regenerator. The heater also has a gas passage connecting to the outside via the heat source regenerator. The air passage connecting to the combustion chamber is changed to connect to the heater and then to the combustion chamber, thus forming a gas turbine-type combined cycle heat pump system. Attached image description:

[0025] Figure 1 This is a first principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0026] Figure 2This is a second principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0027] Figure 3 This is a third principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0028] Figure 4 This is the fourth principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0029] Figure 5 This is the fifth principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0030] Figure 6 This is the sixth principle thermodynamic system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0031] Figure 7 This is the seventh principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0032] Figure 8 This is the eighth principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0033] Figure 9 This is the ninth principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0034] Figure 10 This is the tenth principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0035] Figure 11 This is the 11th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0036] Figure 12 This is the 12th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0037] Figure 13 This is the 13th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0038] Figure 14 This is the 14th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0039] Figure 15This is the 15th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0040] Figure 16 This is the 16th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0041] Figure 17 This is the 17th principle thermal system diagram of a gas turbine-type combined cycle heat pump system provided by the present invention.

[0042] In the diagram, 1-compressor, 2-combustion chamber, 3-gas turbine, 4-high temperature steam generator, 5-low temperature steam generator, 6-second compressor, 7-heater, 8-boost pump, 9-throttle valve, 10-evaporator, 11-ejector, 12-second boost pump, 13-second ejector, 14-high temperature regenerator, 15-regenerator, 16-second regenerator, 17-expander, 18-second heater, 19-two-phase expander, 20-nozzle, 21-dual-energy compressor, 22-expander speed increaser, 23-steam separator, 24-second nozzle, A-high temperature heat exchanger, B-heat furnace, C-heat source regenerator. Detailed implementation method:

[0043] First, it should be noted that the structure and process are not repeated unless necessary, and obvious processes are not described. The invention will now be described in detail with reference to the accompanying drawings and examples.

[0044] Figure 1 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0045] (1) Structurally, it mainly consists of a compressor, combustion chamber, gas turbine, high-temperature steam generator, low-temperature steam generator, second compressor, heater, booster pump, throttle valve, evaporator, ejector, second booster pump, and second ejector; it has an external air passage connecting to compressor 1, compressor 1 has an air passage connecting to combustion chamber 2, an external fuel passage connecting to combustion chamber 2, combustion chamber 2 also has a gas passage connecting to gas turbine 3, gas turbine 3 also has a gas passage connecting to high-temperature steam generator 4 and low-temperature steam generator 5 before connecting to the outside, second compressor 6 has a refrigerant vapor passage connecting to heater 7, heater 7 also has a condensate pipeline connected to low-temperature steam generator 5 via booster pump 8, heater 7 also has a condensate pipeline connected to low-temperature steam generator 5 via throttle valve 9. Evaporator 10 is connected, and evaporator 10 also has a refrigerant vapor channel connected to the low-pressure steam inlet of ejector 11. Low-temperature steam generator 5 also has a steam channel connected to the high-pressure steam inlet of ejector 11. Ejector 11 also has a medium-pressure refrigerant vapor channel connected to the second compressor 6. An external liquid medium pipeline connects to the high-temperature steam generator 4 via the second booster pump 12. The high-temperature steam generator 4 then has a steam channel connected to the high-pressure steam inlet of the second ejector 13. An external heated medium channel connects to the heater 7 and then to the low-pressure steam inlet of the second ejector 13. The second ejector 13 also has a user steam channel connected to the outside. Evaporator 10 also has a low-temperature heat medium channel connected to the outside. Gas turbine 3 connects to compressor 1 and the second compressor 6 and transmits power.

[0046] (2) In terms of process, external air flows through compressor 1 to increase pressure and temperature before entering combustion chamber 2. External fuel enters combustion chamber 2, where fuel and compressed air mix and burn to form high-temperature gas. This gas then enters gas turbine 3 to reduce pressure and perform work. The gas discharged from gas turbine 3 flows through high-temperature steam generator 4 and low-temperature steam generator 5 to gradually release heat and reduce temperature before being discharged to the outside. The refrigerant vapor discharged from the second compressor 6 enters heater 7 to release heat and condense. It then splits into two paths: the first path flows through booster pump 8 to increase pressure before entering low-temperature steam generator 5 to absorb heat and vaporize; the second path flows through throttle valve 9 to reduce pressure and temperature before entering evaporator 10 to absorb heat and vaporize. The steam generated by low-temperature steam generator 5 enters ejector 11 through high-pressure steam inlet. The high-pressure steam flows through nozzle to reduce pressure and increase speed, forming low pressure. The refrigerant vapor discharged from evaporator 10 is drawn into the low-pressure zone of ejector 11. The two steam paths mix and flow through diffuser to reduce speed and increase pressure, forming medium-pressure refrigerant vapor, which then enters the second compressor 6. The heating medium is pressurized and heated, and flows through the heater 7 to absorb heat and vaporize. The liquid medium is pressurized by the second booster pump 12, flows through the high-temperature steam generator 4 to absorb heat and vaporize, and then enters the second ejector 13 through the high-pressure steam inlet. The high-pressure steam flows through the nozzle to reduce pressure and increase speed to form a low pressure. The steam generated by the heater 7 is drawn into the low-pressure zone of the second ejector 13. After the two steams are mixed, they flow through the diffuser to reduce speed and increase pressure to form medium-pressure steam and supply it to users. The fuel provides driving heat load through combustion, and the low-temperature heat medium provides low-temperature heat load through the evaporator 10. Users receive steam-type heat load. Air and gas carry away the emission heat load through the inlet and outlet processes. The mechanical energy output by the gas turbine 3 is used to power the compressor 1 and the second compressor 6, or the mechanical energy output by the gas turbine 3 is used to power the compressor 1, the second compressor 6 and the outside, or the gas turbine 3 and the outside jointly provide power to the compressor 1 and the second compressor 6, forming a gas turbine type combined cycle heat pump system.

[0047] Figure 2 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0048] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a high-temperature regenerator is added. The compressor 1 is changed from having an air passage connected to the combustion chamber 2 to having an air passage connected to the combustion chamber 2 via the high-temperature regenerator 14. The gas turbine 3 is changed from having a gas passage connected to the high-temperature steam generator 4 to having a gas passage connected to the high-temperature steam generator 4 via the high-temperature regenerator 14.

[0049] (2) In terms of process, with Figure 1Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the compressed air discharged from the compressor 1 flows through the high-temperature regenerator 14 to absorb heat and increase its temperature, and then enters the combustion chamber 2 to participate in combustion; the gas discharged from the gas turbine flows through the high-temperature regenerator 14, the high-temperature steam generator 4 and the low-temperature steam generator 5 to gradually release heat and decrease its temperature, and then is discharged to the outside, forming a gas turbine-type combined cycle heat pump system.

[0050] Figure 3 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0051] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a high-temperature regenerator is added. The air passage of compressor 1 is connected to combustion chamber 2, and the air passage of compressor 1 is connected to combustion chamber 2 via high-temperature regenerator 14. The gas passage of gas turbine 3 is connected to high-temperature steam generator 4, and the gas passage of gas turbine 3 is connected to itself via high-temperature regenerator 14, and then gas turbine 3 has a gas passage connected to high-temperature steam generator 4.

[0052] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the compressed air discharged from the compressor 1 flows through the high-temperature regenerator 14 to absorb heat and increase its temperature, and then enters the combustion chamber 2 to participate in combustion; the high-temperature gas discharged from the combustion chamber 2 enters the gas turbine 3 to reduce its pressure and do work, and after reaching a certain level, it flows through the high-temperature regenerator 14 to release heat and decrease its temperature, and then enters the gas turbine 3 to continue to reduce its pressure and do work, and flows through the high-temperature steam generator 4 and the low-temperature steam generator 5 to gradually release heat and decrease its temperature, and then is discharged to the outside, forming a gas turbine-type combined cycle heat pump system.

[0053] Figure 4 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0054] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a high-temperature regenerator is added. The compressor 1 is changed from having an air passage connected to the combustion chamber 2 to having an air passage connected to itself via the high-temperature regenerator 14, and then the compressor 1 has an air passage connected to the combustion chamber 2. The gas turbine 3 is changed from having a gas passage connected to the high-temperature steam generator 4 to having a gas passage connected to the high-temperature steam generator 4 via the high-temperature regenerator 14.

[0055] (2) In terms of process, with Figure 1Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: external air enters the compressor 1, is pressurized and heated, and after reaching a certain level, it flows through the high-temperature regenerator 14 to absorb heat and be heated, then enters the compressor 1 to continue being pressurized and heated, and then enters the combustion chamber 2 to participate in combustion; the gas emitted by the gas turbine 3 flows through the high-temperature regenerator 14, the high-temperature steam generator 4 and the low-temperature steam generator 5 to gradually release heat and cool down, and then is discharged to the outside, forming a gas turbine-type combined cycle heat pump system.

[0056] Figure 5 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0057] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a regenerator is added. The condensate line of the heater 7 is connected to the evaporator 10 via the throttle valve 9. The condensate line of the heater 7 is then connected to the evaporator 10 via the regenerator 15 and the throttle valve 9. The refrigerant vapor passage of the ejector 11 is connected to the second compressor 6. The refrigerant vapor passage of the ejector 11 is then connected to the second compressor 6 via the regenerator 15.

[0058] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the second condensate discharged from the heater 7 flows through the regenerator 15 to release heat and cool down, then flows through the throttling valve 9 to reduce pressure and temperature, and then enters the evaporator 10 to absorb heat and vaporize; the refrigerant vapor discharged from the ejector 11 flows through the regenerator 15 to absorb heat and increase temperature, and then enters the second compressor 6 to increase pressure and temperature, thus forming a gas turbine-type combined cycle heat pump system.

[0059] Figure 6 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0060] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a regenerator is added. The refrigerant vapor passage of evaporator 10 is connected to the low-pressure steam inlet of ejector 11. The refrigerant vapor passage of evaporator 10 is then connected to the low-pressure steam inlet of ejector 11 via regenerator 15. The condensate pipeline of heater 7 is connected to evaporator 10 via throttling valve 9. The condensate pipeline of heater 7 is then connected to evaporator 10 via regenerator 15 and throttling valve 9.

[0061] (2) In terms of process, with Figure 1Compared to the gas turbine-type combined cycle heat pump system shown, the difference is that the second condensate discharged from the heater 7 flows through the regenerator 15 to release heat and cool down, flows through the throttling valve 9 to reduce pressure and cool down, flows through the evaporator 10 to absorb heat and vaporize, flows through the regenerator 15 to absorb heat and increase temperature, and then enters the low-pressure zone of the ejector 11 through the low-pressure steam inlet to form the gas turbine-type combined cycle heat pump system.

[0062] Figure 7 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0063] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a regenerator and a second regenerator are added. The refrigerant vapor passage of evaporator 10 is connected to the low-pressure steam inlet of ejector 11. The refrigerant vapor passage of evaporator 10 is then connected to the low-pressure steam inlet of ejector 11 via the second regenerator 16. The condensate line of heater 7 is connected to evaporator 10 via throttle valve 9. The condensate line of heater 7 is then connected to evaporator 10 via regenerator 15, second regenerator 16 and throttle valve 9. The refrigerant vapor passage of ejector 11 is connected to the second compressor 6. The refrigerant vapor passage of ejector 11 is then connected to the second compressor 6 via regenerator 15.

[0064] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the second condensate discharged from the heater 7 flows through the regenerator 15 and the second regenerator 16 to gradually release heat and cool down, flows through the throttling valve 9 to reduce pressure and temperature, flows through the evaporator 10 to absorb heat and vaporize, flows through the second regenerator 16 to absorb heat and increase temperature, and then enters the low-pressure zone of the ejector 11 through the low-pressure steam inlet; the refrigerant vapor discharged from the ejector 11 flows through the regenerator 15 to absorb heat and increase temperature, and then enters the second compressor 6 to increase pressure and temperature, forming a gas turbine-type combined cycle heat pump system.

[0065] Figure 8 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0066] (1) Structurally, in Figure 1In the gas turbine-type combined cycle heat pump system shown, a regenerator, an expander, and a second heater are added. The second compressor 6 is connected to the heater 7 via a refrigerant vapor channel. The connection is adjusted so that the second compressor 6 has a refrigerant vapor channel connected to the second heater 18, which then splits into two paths—the first path connects to the heater 7, and the second path connects to the expander 17. The expander 17 also has a refrigerant vapor channel connected to the regenerator 15, which then connects to the second compressor 6 via an intermediate port. The heater 7 has a condensate line connected to the evaporator 10 via a throttling valve 9. The connection is adjusted so that the heater 7 has a refrigerant medium line (either fully condensed or partially condensed) connected to the evaporator 10 via the regenerator 15 and the throttling valve 9. The second heater 18 also has a heated medium channel connected to the outside. The expander 17 is connected to the second compressor 6 and transmits power.

[0067] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the refrigerant vapor discharged from the second compressor 6 flows through the second heater 18 to release heat and cool down, and then splits into two paths—the first path enters the heater 7 to release heat and then condenses completely or partially; the second path flows through the expander 17 to reduce pressure and do work, flows through the regenerator 15 to absorb heat and heat up, and enters the second compressor 6 through the intermediate air inlet port to increase pressure and temperature; the refrigerant medium discharged from the heater 7 is split into two paths—the first path flows through the booster pump 8 to be pressurized and then enters the low-temperature steam generator 5 to absorb heat and vaporize; the second path flows through the regenerator 15 and releases heat, flows through the throttle valve 9 to reduce pressure and temperature, and then the evaporator 10 absorbs heat and vaporizes; the heated medium obtains a medium-temperature heat load through the second heater 18, and the mechanical energy output from the expander 17 provides power to the second compressor 6, forming a gas turbine-type combined cycle heat pump system.

[0068] Figure 9 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0069] (1) Structurally, in Figure 1In the gas turbine-type combined cycle heat pump system shown, a regenerator, a second regenerator, an expander, and a second heater are added. The refrigerant vapor passage of evaporator 10 is adjusted to connect to the low-pressure steam inlet of ejector 11 after passing through the second regenerator 16. The refrigerant vapor passage of the second compressor 6 is adjusted to connect to the heater 7, so that the refrigerant vapor passage of the second compressor 6 connects to the second heater 18 and then splits into two paths—the first path connects to the heater 7. 7 connects to the second expander 17. The expander 17 also has a refrigerant vapor passage that connects to the regenerator 15 and then to the second compressor 6 via an intermediate port. The condensate pipeline of the heater 7 is connected to the evaporator 10 via the throttle valve 9. The heater 7 is adjusted so that the refrigerant medium pipeline, whether fully condensed or not fully condensed, connects to the evaporator 10 via the regenerator 15, the second regenerator 16, and the throttle valve 9. The second heater 18 also has a heated medium passage that connects to the outside. The expander 17 is connected to the second compressor 6 and transmits power.

[0070] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: The refrigerant vapor discharged from the second compressor 6 flows through the second heater 18 to release heat and cool down, and then splits into two paths—the first path enters the heater 7 to release heat and then condenses completely or partially; the second path flows through the expander 17 to reduce pressure and do work, flows through the regenerator 15 to absorb heat and heat up, and enters the second compressor 6 through the intermediate air inlet port to increase pressure and temperature; the refrigerant medium discharged from the heater 7 is split into two paths—the first path flows through the booster pump 8 to increase pressure and then enters the low-temperature steam generator 5 to absorb heat and vaporize; the second path flows through the regenerator 15 and the second regenerator 16 and gradually releases heat, flows through the throttling valve 9 to reduce pressure and cool down, flows through the evaporator 10 to absorb heat and vaporize, flows through the second regenerator 16 to absorb heat and heat up, and then enters the low-pressure zone of the ejector 11; the heated medium obtains a medium-temperature heat load through the second heater 18, and the mechanical energy output from the expander 17 provides power to the second compressor 6, forming a gas turbine-type combined cycle heat pump system.

[0071] Figure 10 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0072] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a two-phase expander 19 is added and replaces the throttle valve 9. The two-phase expander 19 is connected to the second compressor 6 and transmits power.

[0073] (2) In terms of process, with Figure 1Compared to the gas turbine-type combined cycle heat pump system shown, the difference is that the second condensate discharged from the heater 7 flows through the two-phase expander 19 to reduce pressure and do work, and then enters the evaporator 10 to absorb heat and vaporize; the mechanical energy output by the two-phase expander 19 is provided to the second compressor 6 to provide power, forming a gas turbine-type combined cycle heat pump system.

[0074] Figure 11 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0075] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a nozzle 20 is added and the throttle valve 9 is replaced.

[0076] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference is that the second condensate discharged from the heater 7 flows through the nozzle 20 to reduce pressure and increase speed, and then enters the evaporator 10 to absorb heat and vaporize, forming a gas turbine-type combined cycle heat pump system.

[0077] Figure 12 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0078] (1) Structurally, in Figure 9 In the gas turbine-type combined cycle heat pump system shown, a nozzle 20 is added and replaces the throttle valve 9, a dual-energy compressor 21 is added and replaces the second compressor 6, and an expander accelerator 22 is added and replaces the expander 17.

[0079] (2) In terms of process, with Figure 9 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the condensate discharged from the second regenerator 16 flows through the nozzle 20 to reduce pressure and increase speed, flows through the evaporator 10 to absorb heat and vaporize, flows through the second regenerator 16 to absorb heat and increase temperature, and then enters the low-pressure zone of the ejector 11; the refrigerant vapor discharged from the second heater 18 is divided into two paths - the first path enters the heater 7, and the second path flows through the expander 22 to reduce pressure and do work and increase speed, flows through the regenerator 15 to absorb heat and increase temperature, and enters the dual-energy compressor 21 to increase pressure and temperature and reduce speed, thus forming a gas turbine-type combined cycle heat pump system.

[0080] Figure 13 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0081] (1) Structurally, in Figure 1In the gas turbine-type combined cycle heat pump system shown, a nozzle and a steam distribution chamber are added. The condensate pipe of the heater 7 is connected to the evaporator 10 through the throttling valve 9. The heater 7 is adjusted to have a condensate pipe connected to the steam distribution chamber 23 through the nozzle 20. The steam distribution chamber 23 also has a refrigerant vapor passage connected to the second compressor 6 through the intermediate port. The steam distribution chamber 23 also has a condensate pipe connected to the evaporator 10 through the throttling valve 9.

[0082] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the second condensate discharged from the heater 7 flows through the nozzle 20 to reduce pressure and increase speed, and then enters the steam separator 23 for gas-liquid separation; the refrigerant vapor discharged from the steam separator 23 enters the second compressor 6 through the intermediate port to increase pressure and temperature, and the condensate discharged from the steam separator 23 flows through the throttle valve 9 to reduce pressure and temperature before entering the evaporator 10 to absorb heat and vaporize, thus forming the gas turbine-type combined cycle heat pump system.

[0083] Figure 14 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0084] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a regenerator, nozzle, and steam distribution chamber are added. The refrigerant vapor passage of evaporator 10 connected to the low-pressure steam inlet of ejector 11 is adjusted so that the refrigerant vapor passage of evaporator 10 connects to the low-pressure steam inlet of ejector 11 after passing through regenerator 15. The condensate pipeline of heater 7 connected to evaporator 10 through throttle valve 9 is adjusted so that heater 7 has a condensate pipeline connected to steam distribution chamber 23 through nozzle 20. Steam distribution chamber 23 also has a refrigerant vapor passage connected to the second compressor 6 through an intermediate port. Steam distribution chamber 23 also has a condensate pipeline connected to evaporator 10 through regenerator 15 and throttle valve 9.

[0085] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: the second condensate discharged from the heater 7 flows through the nozzle 20 to reduce pressure and increase speed, and then enters the steam separator 23 for gas-liquid separation; the refrigerant vapor discharged from the steam separator 23 enters the second compressor 6 through the intermediate port to increase pressure and temperature; the condensate discharged from the steam separator 23 flows through the regenerator 15 to release heat and reduce temperature, flows through the throttling valve 9 to reduce pressure and reduce temperature, flows through the evaporator 10 to absorb heat and vaporize, flows through the regenerator 15 to absorb heat and increase temperature, and then enters the low-pressure zone of the ejector 11 to form the gas turbine-type combined cycle heat pump system.

[0086] Figure 15 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0087] (1) Structurally, in Figure 13In the gas turbine-type combined cycle heat pump system shown, a second nozzle 24 is added and replaces the throttle valve 9.

[0088] (2) In terms of process, with Figure 13 Compared to the gas turbine-type combined cycle heat pump system shown, the difference is that the condensate discharged from the regenerator 15 flows through the second nozzle 24 to reduce pressure and increase speed, and then enters the evaporator 10 to absorb heat and vaporize, forming a gas turbine-type combined cycle heat pump system.

[0089] Figure 16 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0090] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a high-temperature heat exchanger A is added, and the air passage connecting to the combustion chamber 2 is changed to connect to the high-temperature heat exchanger A before connecting to the combustion chamber 2. The high-temperature heat exchanger A also has a high-temperature heat medium passage connected to the outside.

[0091] (2) In terms of process, with Figure 1 Compared to the gas turbine-type combined cycle heat pump system shown, the difference is that the compressed air discharged from the compressor 1 flows through the high-temperature heat exchanger A to absorb heat and increase its temperature, and then enters the combustion chamber 2 to participate in combustion; the high-temperature heat medium provides the driving heat load through the high-temperature heat exchanger A, forming a gas turbine-type combined cycle heat pump system.

[0092] Figure 17 The gas turbine-type combined cycle heat pump system shown is implemented as follows:

[0093] (1) Structurally, in Figure 1 In the gas turbine-type combined cycle heat pump system shown, a heater and a heat source regenerator are added. There is an external fuel channel connected to the heater B, and an external air channel connected to the heater B via the heat source regenerator C. The heater B also has a gas channel connected to the outside via the heat source regenerator C. The air channel connecting to the combustion chamber 2 is changed to connect to the heater B and then to the combustion chamber 2.

[0094] (2) In terms of process, with Figure 1Compared to the gas turbine-type combined cycle heat pump system shown, the difference lies in the following: external fuel enters the heater B, and external air flows through the heat source regenerator C to absorb heat and increase its temperature before entering the heater B. The fuel and air mix and burn in the heater B to form gas. The gas generated in the heater B releases heat to the compressed gas flowing through it, then flows through the heat source regenerator C to release heat and decrease its temperature before being discharged to the outside. The compressed air discharged from the compressor 1 flows through the heater B to absorb heat and increase its temperature before entering the combustion chamber 2 to participate in combustion. External fuel provides high-temperature driving heat load through the heater B, and air and gas carry away the discharged heat load by entering and exiting the heater B, forming a gas turbine-type combined cycle heat pump system.

[0095] The effects achievable by this invention—the gas turbine-type combined cycle heat pump system proposed in this invention has the following effects and advantages:

[0096] (1) New ideas and technologies for utilizing temperature difference are presented.

[0097] (2) The fuel forms a high-grade heat source, which is utilized step by step and in depth, significantly improving energy utilization efficiency.

[0098] (3) New technologies for the efficient and high-value utilization of high-quality fuels in refrigeration / heating / steam / power production and combined cooling / heating / steam / power supply are presented.

[0099] (4) Energy sharing to enhance the efficient and high-value utilization of different energy types.

[0100] (5) When necessary, external power can be used to raise the temperature of thermal energy, which is flexible and adaptable.

[0101] (6) The compressor and the ejector jointly obtain the low temperature heat load, which significantly improves the heating parameters or reduces the compressor's pressure boosting share.

[0102] (7) Provide reasonable regeneration technology to effectively improve the coordination of the device in terms of load, performance index, and pressure ratio.

[0103] (8) The injector enables efficient utilization of gas emission heat load and temperature increase of low temperature heat load, thereby reducing the size of the compressor and effectively reducing the manufacturing cost of the device.

[0104] (9) The process is reasonable, the structure is simple, the manufacturing cost is low, and the system economy is effectively improved.

[0105] (10) Provides a variety of specific technical solutions that can cope with many different actual situations, which is conducive to expanding the application scope and value of gas turbine combined cycle heat pump system technology.

Claims

1. A gas turbine-type combined cycle heat pump system, mainly composed of a compressor, combustion chamber, gas turbine, high-temperature steam generator, low-temperature steam generator, second compressor, heater, booster pump, throttle valve, evaporator, ejector, second booster pump, and second ejector; an external air passage connects to the compressor (1), the compressor (1) has an air passage connects to the combustion chamber (2), an external fuel passage connects to the combustion chamber (2), the combustion chamber (2) also has a gas passage connects to the gas turbine (3), the gas turbine (3) also has a gas passage connects to the high-temperature steam generator (4) and the low-temperature steam generator (5) and then connects to the outside, the second compressor (6) has a refrigerant vapor passage connects to the heater (7), the heater (7) also has a condensate pipeline connected to the low-temperature steam generator (5) via the booster pump (8), the heater (7) also has a condensate pipeline connected to the evaporator (10) via the throttle valve (9). The evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) via a refrigerant steam channel. The low-temperature steam generator (5) is connected to the high-pressure steam inlet of the ejector (11) via a steam channel. The ejector (11) is connected to the second compressor (6) via a medium-pressure refrigerant steam channel. The external liquid medium pipeline is connected to the high-temperature steam generator (4) via the second booster pump (12). The high-temperature steam generator (4) is then connected to the high-pressure steam inlet of the second ejector (13) via a steam channel. The external heated medium channel is connected to the heater (7) via a channel. The second ejector (13) is then connected to the low-pressure steam inlet of the second ejector (13). The second ejector (13) is also connected to the external user steam channel. The evaporator (10) is also connected to the external low-temperature heat medium channel. The gas turbine (3) is connected to the compressor (1) and the second compressor (6) and transmits power to form a gas turbine type combined cycle heat pump system.

2. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system as described in claim 1, wherein a high-temperature regenerator is added, the compressor (1) is connected to the combustion chamber (2) via an air passage, and the compressor (1) is connected to the combustion chamber (2) via an air passage through a high-temperature regenerator (14), and the gas turbine (3) is connected to the high-temperature steam generator (4) via a gas passage through a high-temperature regenerator (14), thereby forming a gas turbine-type combined cycle heat pump system.

3. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system as described in claim 1, wherein a high-temperature regenerator is added, the compressor (1) is adjusted to have an air passage connected to the combustion chamber (2) and the compressor (1) is connected to the combustion chamber (2) via the high-temperature regenerator (14), and the gas turbine (3) is adjusted to have a gas passage connected to the high-temperature steam generator (4) and the gas turbine (3) is connected to itself via the high-temperature regenerator (14), and then the gas turbine (3) has a gas passage connected to the high-temperature steam generator (4), thus forming a gas turbine-type combined cycle heat pump system.

4. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system as described in claim 1, wherein a high-temperature regenerator is added, the compressor (1) is adjusted to have an air passage connected to the combustion chamber (2) so that the compressor (1) has an air passage connected to itself via the high-temperature regenerator (14), and then the compressor (1) has an air passage connected to the combustion chamber (2), and the gas turbine (3) is adjusted to have a gas passage connected to the high-temperature steam generator (4) so ​​that the gas turbine (3) has a gas passage connected to the high-temperature steam generator (4) via the high-temperature regenerator (14), thus forming a gas turbine-type combined cycle heat pump system.

5. A gas turbine-type combined cycle heat pump system is formed by adding a regenerator to any of the gas turbine-type combined cycle heat pump systems described in claims 1-4, adjusting the condensate pipe of the heater (7) to connect to the evaporator (10) via the throttle valve (9), and adjusting the condensate pipe of the heater (7) to connect to the evaporator (10) via the regenerator (15) and the throttle valve (9), and adjusting the refrigerant vapor passage of the ejector (11) to connect to the second compressor (6), and adjusting the refrigerant vapor passage of the ejector (11) to connect to the second compressor (6) via the regenerator (15), thereby forming a gas turbine-type combined cycle heat pump system.

6. A gas turbine-type combined cycle heat pump system, wherein in any of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a regenerator is added, and the refrigerant vapor passage of the evaporator (10) connected to the low-pressure steam inlet of the ejector (11) is adjusted so that the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) after passing through the regenerator (15), and the condensate pipe of the heater (7) connected to the evaporator (10) through the throttling valve (9) is adjusted so that the condensate pipe of the heater (7) is connected to the evaporator (10) after passing through the regenerator (15) and the throttling valve (9), thereby forming a gas turbine-type combined cycle heat pump system.

7. A gas turbine-type combined cycle heat pump system, wherein in any of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a regenerator and a second regenerator are added, the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) and the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) after passing through the second regenerator (16), the condensate pipe of the heater (7) is connected to the evaporator (10) through the throttle valve (9) and the condensate pipe of the heater (7) is connected to the evaporator (10) after passing through the regenerator (15), the second regenerator (16) and the throttle valve (9), and the refrigerant vapor passage of the ejector (11) is connected to the second compressor (6) and the refrigerant vapor passage of the ejector (11) is connected to the second compressor (6) through the regenerator (15), thereby forming a gas turbine-type combined cycle heat pump system.

8. A gas turbine-type combined cycle heat pump system, wherein in any one of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a regenerator, an expander, and a second heater are added, and the refrigerant vapor passage of the second compressor (6) is connected to the heater (7) and then the refrigerant vapor passage of the second compressor (6) is connected to the second heater (18) and then split into two paths—the first path is connected to the heater (7) and the second path is connected to the expander (17), and the expander (17) also has a refrigerant vapor passage connected to the regenerator. (15) Then, it is connected to the second compressor (6) through the intermediate port. The condensate pipeline of the heater (7) is connected to the evaporator (10) through the throttle valve (9). The heater (7) is adjusted to have a refrigerant medium pipeline that is fully condensed or not fully condensed, which is connected to the evaporator (10) through the regenerator (15) and the throttle valve (9). The second heater (18) also has a heated medium channel connected to the outside. The expander (17) is connected to the second compressor (6) and transmits power to form a gas turbine type combined cycle heat pump system.

9. A gas turbine-type combined cycle heat pump system, wherein in any one of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a regenerator, a second regenerator, an expander, and a second heater are added; the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11), and the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) after passing through the second regenerator (16); the refrigerant vapor passage of the second compressor (6) is connected to the heater (7), and the refrigerant vapor passage of the second compressor (6) is connected to the second heater (18), and then split into two paths—the first path connects to the heater (7). 7) The second expansion unit (17) is connected to the second expansion unit (17). The expansion unit (17) also has a refrigerant vapor channel connected to the regenerator (15) and then connected to the second compressor (6) through the intermediate port. The condensate pipeline of the heater (7) is connected to the evaporator (10) through the throttle valve (9) and adjusted so that the heater (7) has a refrigerant medium pipeline that is fully condensed or not fully condensed, which is connected to the evaporator (10) through the regenerator (15), the second regenerator (16) and the throttle valve (9). The second heater (18) also has a heated medium channel connected to the outside. The expansion unit (17) is connected to the second compressor (6) and transmits power to form a gas turbine type combined cycle heat pump system.

10. A gas turbine-type combined cycle heat pump system is formed by adding a two-phase expander (19) to replace the throttle valve (9) in any of the gas turbine-type combined cycle heat pump systems described in claims 1-9. The two-phase expander (19) is connected to a second compressor (6) and transmits power to form a gas turbine-type combined cycle heat pump system.

11. A gas turbine-type combined cycle heat pump system is formed by adding a nozzle (20) and replacing the throttle valve (9) to any of the gas turbine-type combined cycle heat pump systems described in claims 1-9, thereby forming a gas turbine-type combined cycle heat pump system.

12. A gas turbine-type combined cycle heat pump system is formed by adding a nozzle (20) and replacing the throttle valve (9) to any of the gas turbine-type combined cycle heat pump systems described in claims 8-9, adding a dual-energy compressor (21) and replacing the second compressor (6), and adding an expander speed increaser (22) and replacing the expander (17).

13. A gas turbine-type combined cycle heat pump system, wherein in any of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a nozzle and a steam distribution chamber are added, and the condensate pipe of the heater (7) is connected to the evaporator (10) via a throttle valve (9) is adjusted so that the condensate pipe of the heater (7) is connected to the steam distribution chamber (23) via a nozzle (20), and the steam distribution chamber (23) also has a refrigerant vapor passage connected to the second compressor (6) through an intermediate port, and the steam distribution chamber (23) also has a condensate pipe connected to the evaporator (10) via a throttle valve (9), thus forming a gas turbine-type combined cycle heat pump system.

14. A gas turbine-type combined cycle heat pump system, wherein in any of the gas turbine-type combined cycle heat pump systems described in claims 1-4, a regenerator, a nozzle, and a steam distribution chamber are added, and the refrigerant vapor passage of the evaporator (10) connected to the low-pressure steam inlet of the ejector (11) is adjusted so that the refrigerant vapor passage of the evaporator (10) is connected to the low-pressure steam inlet of the ejector (11) after passing through the regenerator (15), and the condensate pipe of the heater (7) connected to the evaporator (10) through the throttle valve (9) is adjusted so that the condensate pipe of the heater (7) is connected to the steam distribution chamber (23) through the nozzle (20), and the steam distribution chamber (23) also has a refrigerant vapor passage connected to the second compressor (6) through an intermediate port, and the condensate pipe of the steam distribution chamber (23) is connected to the evaporator (10) through the regenerator (15) and the throttle valve (9), thus forming a gas turbine-type combined cycle heat pump system.

15. A gas turbine-type combined cycle heat pump system is formed by adding a second nozzle (24) and replacing the throttle valve (9) to any of the gas turbine-type combined cycle heat pump systems described in claims 13-14, thereby forming a gas turbine-type combined cycle heat pump system.

16. A gas turbine-type combined cycle heat pump system is formed by adding a high-temperature heat exchanger (A) to any of the gas turbine-type combined cycle heat pump systems described in claims 1-15, changing the air passage connecting the combustion chamber (2) to connect the high-temperature heat exchanger (A) and then connecting the combustion chamber (2), and the high-temperature heat exchanger (A) also having a high-temperature heat medium passage connected to the outside, thus forming a gas turbine-type combined cycle heat pump system.

17. A gas turbine-type combined cycle heat pump system is a gas turbine-type combined cycle heat pump system according to any one of claims 1-16, with the addition of a heater and a heat source regenerator. An external fuel passage connects to the heater (B), and an external air passage connects to the heater (B) via the heat source regenerator (C). The heater (B) also has a gas passage connecting to the outside via the heat source regenerator (C). The air passage connecting to the combustion chamber (2) is changed to connect to the heater (B) before connecting to the combustion chamber (2), thus forming a gas turbine-type combined cycle heat pump system.

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