Patent classifications
F25B11/04
HEAT RECOVERY APPARATUS
The present application relates to a heat recovery apparatus and method. According to the heat recovery apparatus and method, low-level heat sources at a temperature less than 100 C. discharged from industrial settings or various chemical processes, for example, a petrochemicals manufacturing process are not wasted but used to generate steam and the generated steam is used for various processes to reduce an amount of consumed high-temperature steam that is an external heat source to be used for a reactor or distillation column, thereby not only maximizing energy reduction efficiency but also autonomously producing power consumed by a compressor. Also, an evaporation phenomenon of a part of a refrigerant flow which passes through the compressor may be reduced, thereby recovering heat with excellent efficiency.
HEAT RECOVERY APPARATUS
The present application relates to a heat recovery apparatus and method. According to the heat recovery apparatus and method, low-level heat sources at a temperature less than 100 C. discharged from industrial settings or various chemical processes, for example, a petrochemicals manufacturing process are not wasted but used to generate steam and the generated steam is used for various processes to reduce an amount of consumed high-temperature steam that is an external heat source to be used for a reactor or distillation column, thereby not only maximizing energy reduction efficiency but also autonomously producing power consumed by a compressor. Also, an evaporation phenomenon of a part of a refrigerant flow which passes through the compressor may be reduced, thereby recovering heat with excellent efficiency.
COOLING SYSTEMS FOR HIGH MACH APPLICATIONS
A cooling system for an aircraft includes an air intake, a heat exchanger configured to receive air passing into the air intake when the aircraft is operating at Mach speed, and configured to receive compressed refrigerant from a first compressor at a first pressure, an evaporator positioned within the aircraft and configured to receive heated air from a compartment within the aircraft, at least one of an expansion device and an expansion machine, and the compressed refrigerant rejects heat in the heat exchanger to the air, expands in the at least one of the expansion device and the expansion machine, and receives heat in the evaporator from the heated air.
Refrigeration device and system
A framed, low-temperature refrigeration device is provided, which includes a working circuit that forms a loop and contains a working fluid, the working circuit forming a cycle that includes in series: a compression mechanism, a cooling mechanism, an expansion mechanism and a heating mechanism, wherein the mechanisms for cooling and heating the working fluid include a common heat exchanger in which the working fluid flows in opposite directions in two separate transit portions of the working circuit. The device may also include a refrigeration heat exchanger for extracting heat from at least one member by exchanging heat with the working fluid flowing in the working circuit, wherein the compression mechanism includes two separate compressors, wherein the mechanism for cooling the working fluid includes two cooling heat exchangers which are arranged respectively at the outlet of the two compressors and ensure heat exchange between the working fluid and a cooling fluid, wherein the frame extends in a longitudinal direction and includes a lower base intended to be mounted on a support, the cooling heat exchangers are located in the frame about the common heat exchanger, i.e. the cooling heat exchangers are not located below the common heat exchanger between the common heat exchanger and the lower base of the frame.
Refrigeration device and system
A framed, low-temperature refrigeration device is provided, which includes a working circuit that forms a loop and contains a working fluid, the working circuit forming a cycle that includes in series: a compression mechanism, a cooling mechanism, an expansion mechanism and a heating mechanism, wherein the mechanisms for cooling and heating the working fluid include a common heat exchanger in which the working fluid flows in opposite directions in two separate transit portions of the working circuit. The device may also include a refrigeration heat exchanger for extracting heat from at least one member by exchanging heat with the working fluid flowing in the working circuit, wherein the compression mechanism includes two separate compressors, wherein the mechanism for cooling the working fluid includes two cooling heat exchangers which are arranged respectively at the outlet of the two compressors and ensure heat exchange between the working fluid and a cooling fluid, wherein the frame extends in a longitudinal direction and includes a lower base intended to be mounted on a support, the cooling heat exchangers are located in the frame about the common heat exchanger, i.e. the cooling heat exchangers are not located below the common heat exchanger between the common heat exchanger and the lower base of the frame.
Method and device for cooling of a superconducting cable and corresponding system
The invention relates to a method for cooling a superconducting cable (1) using a coolant containing or consisting of liquid nitrogen, wherein at least a part of the coolant is subjected to a subcooling step and thereafter brought into thermal contact with the superconducting cable (1) in a cooling cycle, wherein said subcooling step is at least in part performed using a refrigerant provided in a Brayton process in which at least a part of the refrigerant is cooled and heated in a main heat exchanger (11). According to the present invention, a part of the coolant is withdrawn from the cooling cycle and heated in the same main heat exchanger (11) in which at least a part of the refrigerant is cooled and heated in the Brayton process. A corresponding device and a corresponding system are also part of the present invention.
GAS REFRIGERATING MACHINE, METHOD FOR OPERATING A GAS REFRIGERATING MACHINE AND METHOD FOR MANUFACTURING A GAS REFRIGERATING MACHINE HAVING A ROTATIONALLY SYMMETRICAL DESIGN
A gas refrigerating machine having: an input for gas; a recuperator including a first recuperator input, a first recuperator output, a second recuperator input, and a second recuperator output; a compressor having a compressor input and a compressor output, the compressor input being coupled to the first recuperator output; a heat exchanger having a first heat exchanger input and a first heat exchanger output on a primary side of the heat exchanger, and a second heat exchanger input and a second heat exchanger output on a secondary side of the heat exchanger, wherein the first heat exchanger input is coupled to the compressor output, and wherein the first heat exchanger output is coupled to the second recuperator input; a turbine having a turbine input and a turbine output, wherein the turbine input is connected to the second recuperator output, and wherein the gas output is coupled to the turbine output.
GAS REFRIGERATING MACHINE, METHOD FOR OPERATING A GAS REFRIGERATING MACHINE AND METHOD FOR MANUFACTURING A GAS REFRIGERATING MACHINE HAVING A HOUSING
A gas refrigerating machine comprising: an input for a gas to be cooled; a recuperator comprising a first recuperator output; a compressor comprising a compressor input, the compressor input being coupled to the first recuperator output; a heat exchanger; a turbine; a gas output; and a housing, wherein the housing comprises a wall, wherein the input for the gas to be cooled is located in the wall, wherein the gas output is located in the wall, and wherein the recuperator, the compressor, the turbine and the heat exchanger are arranged in the housing.