Abstract: A mat product, includes a mat member including inorganic fibers and having a full length Lm; and a package member having an full length Lr; wherein the mat member is received in an inside space of the package member; the inside space of the package member is in gas-communication with an outside environment; and the full length Lr of the package member is greater than the full length Lm of the mat member and thereby the mat member can move in the inside space along a full length direction.

Abstract: An auxiliary pump system for a hybrid powertrain includes a hydraulic accumulator, a hydraulic transformer, a plurality of control devices, a sump, and a plurality of fluid flow paths. The accumulator is charged by a high flow, high pressure hydraulic fluid by opening a first of the control devices and closing a second of the control devices. The accumulator is discharged by closing the first of the control devices and opening the second of the control devices. A high pressure, low flow hydraulic fluid is communicated from the accumulator to the hydraulic transformer. The hydraulic transformer converts the high pressure, low flow hydraulic fluid into a high flow, low pressure hydraulic fluid that is employed by systems within the hybrid powertrain.

Abstract: A hydraulic system of a work machine with a hydraulically controlled implement includes: an operating oil flow passage for flowing operating oil from a main pump; a boost flow oil passage for supplying operating oil to the operating oil flow passage; a connection unit for connecting the implement which is provided downstream of the confluence on the operating oil flow passage; a controller for controlling the high-flow valve; and a high-flow switch which is connected to the controller and is configured to effect or cancel a command of the amount increase on a high-flow valve. Annunciation is made when the connection unit is connected to a high-flow actuator for the implement requiring an amount increase of the operating oil, and the amount increase is effected by the high-flow valve in accordance with an operation of the high-flow switch.

Abstract: A hydraulic device has a first pump, a second pump, an operating state detector configured and arranged to detect an operating state, a connection switching unit configured and arranged to selectively connect the second pump to either a first hydraulic oil line or a second hydraulic oil line, and a switching controller configured to control, based on the operating state detected by the operating state detector, a switching operation of the connection switching unit The switching controller is further configured to inhibit the switching operation of the connection of the second pump when the detected operating state is such that at least one of clutches of a multi-stage transmission and a steering device is in a state transition or at least one brake of the steering device is being operated.

Abstract: An engine provides torque by transmitting power in a fluid using optimally positioned lift-to-drag ratio blades with air-foil shape sections. The fluid may be liquid or gas. Various considerations of engine configuration, fluid density, fluid pressure and fluid temperature are design parameters that can be tuned to achieve high performance. The fluid flow created can be used to drive rotary motion of an output axle, for example.

Abstract: A compensating tank for a hydraulic motor vehicle brake system, having a housing including a housing upper part and a housing lower part and having a device for monitoring the tank filling level of the compensating tank, including a switching unit, which is welded to the housing and has a plug connector, and including a sensor or switching element which can be switched by a transducer at a switching point S at which the switching unit generates a signal for an electronic control unit. The housing has a depression for holding the switching unit, with the switching unit having a base body composed of plastic, which base body is welded to the housing in the depression, and with the depression being provided such that the base body of the switching unit forms a planar surface with the housing.

Abstract: A pressure system having at least two pressure circuits each including a respective positive-displacement element and each compression side of the positive-displacement elements being in operative communication via a compensation device in such a way that a pressure increase in the first pressure circuit leads to a pressure increase in the second pressure circuit, and the pressure increase of the first pressure circuit is essentially reduced by the amount of the pressure increase of the second pressure circuit, and the reduction in the pressure increase is less than a defined limit value.

Abstract: A flow regulator valve having multiple stages is described herein. The flow regulator valve provides a base amount of propane when the engine is idling and provides additional propane to the engine based on the engine's requirements.

Abstract: A stoichiometric compression ignition engine has a turbocharger coupled to it so that the exhaust from the engine feeds the turbine and the compressor provides combustion air past a throttle and intercooler to the engine intake manifold. An exhaust after treatment device is positioned before the exhaust of the engine. A power turbine is connected in parallel relation to the turbocharger turbine and is controlled by a valve to operate the power turbine whenever either the turbocharger compressor boost or the turbocharger turbine back pressure exceed given limits. The power turbine is connected by a power transmission device to either couple to the engine output or to an electrical generator. An EGR loop may be driven by a pump also connected to the power turbine to lower in cylinder pressures.

Abstract: An exhaust gas recirculation system for an internal combustion engine is disclosed. The exhaust gas recirculation system can include a first turbocharger and a second turbocharger with a particulate filter located between the two turbochargers. The first turbocharger can have a first exhaust turbine and a first charger while the second turbocharger can have a second exhaust turbine and a second charger. The particulate filter can be located between the first exhaust turbine and the second exhaust turbine and thereby remove particulates from an exhaust gas before it reaches the second exhaust turbine. In some instances, an exhaust gas recirculation line can be included and have an inlet that is located downstream from the particulate filter. In addition, the exhaust gas recirculation line can have an outlet that is located between the first charger and the second charger, or in the alternative downstream from the first charger.

Abstract: Methods for increasing the enthalpy of a geothermal brine, methods for recovering heat enthalpy stored in a geothermal brine, and methods for the production of a heated brine from a natural geothermal reservoir are provided. The methods may be incorporated into a geosolar electric power generation project to provide a steady and flexible source of renewable energy from a geothermal heat source in combination with solar insolation.

Abstract: A water recirculation system for a steam power plant includes a tapoff line which receives water from a downcomer, and an economizer link which receives water from the tapoff line and transports the water to an economizer.

Abstract: A waste heat recovery system includes a high pressure turbine and a low pressure turbine, in which the high pressure turbine receives high pressure working fluid vapor, the low pressure turbine receives low pressure working fluid vapor and the high pressure turbine also supplies low pressure working fluid vapor to the low pressure turbine. A recuperator receives working fluid vapor from the low pressure turbine. The recuperator produces heated condensate, at least a portion of which is provided to a high pressure vaporizer. The high pressure vaporizer is configured to receive from a high temperature heat source and produces high pressure working vapor used to power the high pressure turbine. The remaining condensed fluid is provided to a low pressure vaporizer which is configured to receive heat from a low-temperature heat source, thereby producing low pressure working fluid vapor used to power the low pressure turbine.

Abstract: The present invention relates to the processing of biomass, particularly but not exclusively poultry litter, to generate energy. A method is presented for generating power from biomass comprising a gasification process (44) involving the gasification of biomass to produce a combustible fuel gas and a power generation process (49) involving combustion of the combustible fuel gas to produce a combustion exhaust gas which is fed to a power generator (49) to generate power and a generator exhaust gas. The method further comprises placing compressed air (1) in thermal contact with the generator exhaust gas (47) to facilitate heat transfer between the compressed air and the generator exhaust gas, and feeding a first portion of compressed air that has thermally contacted the generator exhaust gas to the gasification process to assist in gasification of further biomass.

Abstract: Raw MSW is delivered through an organic digester (12) within which an organic fraction of the MSW is broken down by a combination of aerobic microbial activity and mechanical action and converted into a solid bio fuel material. Treated waste material comprising a mixture of the solid bio fuel material and insert inorganic waste material is discharged from the digester (12). The treated material is delivered through a separator (20) for removal of the inorganic fraction. A substantially homogenous solid bio fuel material is discharged from the separator (20), and passed through a dryer (26) and into a gasifier (30). Within the gasifier (30) the homogenous solid bio fuel material is heated in a depleted oxygen atmosphere to generate a bio fuel gas rich in methane, hydrogen and carbon monoxide. The bio fuel gas is delivered through a cleaner (35) and then collected in a storage tank. Bio fuel gas is fed as required from the storage tank to a power plant (50) for generating electrical energy.

Abstract: A power regulator and a process regulator, or a power regulating device for regulating hybrid energy sources are provided for an aircraft. The power regulator and process regulator is equipped such that the requirement of a required means of a consumer is measurable. In this arrangement the power regulating device is equipped such that a first operating characteristic of a first energy source and a second operating characteristic of a second energy source are determinable. By means of the first energy source a first requirement share can be generated, and by means of the second energy source a second requirement share of the required means can be generated. The power regulating device can regulate the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means can be provided to the consumer.

Abstract: Extremely cold (e.g., ?20° C.) air A is heated by a heat exchanger 30, which is supplied with steam S via a control valve 32, and heated air A? is taken into a gas turbine 10. The valve opening degree of the control valve 32 is feedback-controlled so that the deviation between the measured temperature t1 and the target temperature TO of the heated air A? is eliminated. Further, when the number of revolutions, N, of the gas turbine 10 increases, or when an IGV opening degree OP increases, the valve opening degree of the control valve 32 is feedforward-controlled in accordance with the increase in the number N of revolutions or the increase in the IGV opening degree OP. By so doing, the temperature of air A? can be maintained at a temperature enabling stable combustion without delay in control, and intake air can be heated without delay in control, even at the start of the gas turbine or during change in the opening degree of an inlet guide vane.

Abstract: A pilot burner (150, 350) for a gas turbine engine delivers an inner non-swirling fuel-oxidant mixture surrounded by an outer swirling fuel-oxidant mixture, thereby providing enhanced mixing with no recirculation zone. At least one fluid-restricting inlet port (166, 366) provides an oxidant to an inner mixing passage (160, 360). The inner mixing passage (160, 360) includes a plurality of fuel outlets (168). An outer annular mixing passage (180) receives oxidant from an upstream port (181) surrounding the inner mixing passage and includes at least one swirler element (186, 386) and fuel outlets (188).

Abstract: A fuel nozzle for delivery of fuel to a gas turbine engine. The fuel nozzle includes an outer nozzle wall and a center body located centrally within the nozzle wall. A gap is defined between an inner wall surface of the nozzle wall and an outer body surface of the center body for providing fuel flow in a longitudinal direction from an inlet end to an outlet end of the fuel nozzle. A turbulating feature is defined on at least one of the central body and the inner wall for causing at least a portion of the fuel flow in the gap to flow transverse to the longitudinal direction. The gap is effective to provide a substantially uniform temperature distribution along the nozzle wall in the circumferential direction.

Abstract: A fuel injector for a gas turbine combustor is disclosed which includes a fuel nozzle for issuing fuel into the combustor for combustion, at least one photodetector responsive to flame radiation indicative of an OH chemiluminescence peak, and at least one photodiode responsive to flame radiation indicative of a CH chemiluminescence peak.

Abstract: A combustor assembly in a gas turbine engine. The combustor assembly includes a combustor device coupled to a main engine casing, a first fuel injection system, a transition duct, and an intermediate duct. The combustor device includes a flow sleeve for receiving pressurized air and a liner disposed radially inwardly from the flow sleeve. The first fuel injection system provides fuel that is ignited with the pressurized air creating first working gases. The intermediate duct is disposed between the liner and the transition duct and defines a path for the first working gases to flow from the liner to the transition duct. An intermediate duct inlet portion is associated with a liner outlet and allows movement between the intermediate duct and the liner. An intermediate duct outlet portion is associated with a transition duct inlet section and allows movement between the intermediate duct and the transition duct.

Abstract: A combustor apparatus for use in a gas turbine engine. The combustor apparatus includes a liner, a flow sleeve, and a fuel injection system. The liner includes an inner volume, wherein a portion of the inner volume defines a main combustion zone. The flow sleeve receives compressed air, is positioned radially outward from the liner, and includes a forward end and an aft end. The fuel injection system is coupled to the flow sleeve and provides fuel into the inner volume of the liner downstream from the main combustion zone. The fuel injection system includes a fuel manifold and a fuel dispensing structure. The fuel manifold is coupled to the flow sleeve and includes a cavity for receiving fuel. The fuel dispensing structure is associated with the cavity and distributes fuel from the cavity to the liner inner volume.

Abstract: A gas turbine combustor for producing hot gas by burning a fuel in compressed air comprising a combustor central axis and multiple main swirlers with respective swirler axes disposed about and parallel to the combustor central axis, each main swirler delivering an air fuel mixture flowing through it and about its swirler axis, wherein each swirler imparts rotation to the air fuel mixture flowing through it in a direction opposite that of adjacent swirlers. This combustor configuration reduces shear where the outer edges of adjacent flows meet, allowing for greater tuning of the combustion chamber and reduced NOx and CO emissions.

Abstract: A combustor for an engine assembly includes a cylindrical wall forming a combustion chamber in which an air and fuel mixture is combusted; and a plurality of effusion cooling holes formed in the cylindrical wall, the plurality of effusion cooling holes oriented such that cooling air flowing therethrough cools the cylindrical wall with effusion cooling, convection cooling, and impingement cooling.

Abstract: A method for operating a power plant (2), which includes at least one compressor (3), at least one turbine (4), and a burner arrangement (5), involves, to enhance the power plant (2), feeding a combustion exhaust gas from a pre-burner (8) of the burner arrangement (5) to an oxygen-removal device (11), which removes gas of the oxygen from the combustion exhaust gas in which it is contained.

Abstract: A system and method for integrating gasification processes with membrane oxygen separation, advanced steam conditions, and effective heat recovery. Through the integration of synergistic technologies, a highly efficient Integrated Gasification Combined Cycle (IGCC) power plant can be constructed. A combined cycle power plant that includes substantial amounts of duct firing in its Heat Recovery Steam Generator (HRSG) can be used in conjunction with membrane oxygen separation to provide the necessary air heating to the range of 1470 to 1650° F. This high-end energy in the HRSG can also be utilized to create more steam at elevated conditions in the HRSG, and thus provide additional cold feedwater for cooling in the HRSG and for cooling in both the gasification and oxygen membrane separation processes. When CO2 release to atmosphere is to be minimized, the invention may utilize a synergistic hydrogen membrane separation technology.

Abstract: A transition member between a combustion section and a turbine section in a gas turbine engine. The transition member includes a casing inner wall and a plurality of spanning members. The spanning members extend radially outwardly from a radially outer surface of the casing inner wall. Each of the spanning members included a slot formed therein. Each slot is in communication with a first aperture formed in the radially inner surface of the casing inner wall and a plurality of second apertures formed in an aft side of the spanning member for effecting a passage of the cooling fluid from a first cooling fluid channel to an inner volume defined within the radially inner surface of the casing inner wall. The slots include a component in the radial direction and a component in the axial direction such that the first aperture is not radially aligned with the second apertures.

Abstract: A magnetic refrigeration device for transferring heat including a shaft rotatable about an axis, an inner magnet disposed at one of the axis and a radial distance from the axis, an outer magnet disposed a radial distance from the axis outside of the inner magnet defining a magnetic gap between the inner and outer magnets, and magnetocaloric material disposed at a radial distance from the axis between the radial distances of the inner and outer magnets. The magnetocaloric material is coupled to the shaft for rotation with the shaft about the axis such that during rotation of the shaft a portion of the magnetocaloric material alternates between a magnetized position disposed within the magnetic gap and a demagnetized position outside of the magnetic gap.

Abstract: An exemplary refrigeration system for cooling food or beverages may use a liquid cooling system of a vehicle. The refrigeration system may include a compartment in which the food or beverages may be placed and removed, a chilled liquid coolant system having a connection through which liquid coolant is received from the liquid cooling system of the vehicle, and a heat exchanger operationally coupled with the chilled liquid coolant system and the compartment to transfer heat from the compartment into the liquid coolant. The refrigeration system may also include a second chilled coolant system through which a second coolant flows and a second heat exchanger operationally coupled with the second chilled coolant system and the compartment to transfer heat from the compartment. The chilled liquid coolant system and the second chilled coolant system may operate together as a cascade cooling system.

Abstract: The present invention relates to a thermoelectric motor (3) in which a material is interposed between the external plate (12) of a thermoelectric module and an external heat exchanger (4), to reduce heat resistance therebetween; the present invention further relates to a thermoelectric motor (3) in which the heat-carrying fluid flows directly over the internal plate (13) of a thermoelectric module, a temperature controlled garment with an inner metal layer and a convex heat exchanger.

Abstract: The present invention relates to a cooling device (20) for installation in an aircraft, in particular a passenger aircraft. The cooling device (20) comprises a heat exchanger (26) configured for flow-through of a liquid coolant for pre-cooling a cooling chamber (34) of the cooling device (20) to a temperature of the liquid coolant, the heat exchanger (26) being coupled in a heat-transferring manner to a refrigerant (28) which is in thermal contact with the cooling chamber (34) of the cooling device (20) for cooling the cooling chamber (34) to a temperature which is below the temperature of the liquid coolant, wherein the heat exchanger (26) and the refrigerant (28) are disposed inside the cooling chamber (34) of the cooling device (20), and wherein the heat exchanger (26) is configured for connection to a liquid coolant supply system installed on board the aircraft.

Abstract: The method for cooling a liquid (2) in which a coolant comprising a refrigeration-liquefied gas is introduced into the liquid (2) and the corresponding device (1) make possible, in an advantageously simple manner, the production of cooled liquids (2), which, for example, can be used as process water in the production of freshly mixed concrete. In this case the enthalpy content of the coolant, preferably of liquid nitrogen, is utilized in a good manner, by firstly using the vaporization enthalpy, and secondly the heating of the nitrogen after vaporization up to ice temperature, for cooling the liquid.

Abstract: By cooling a metal plate, a water film is generated on a surface of the metal plate due to dew condensation, in a linear increase amount process and at before stage of saturation, the generation water is flipped off, and the generation water film is peeled off forcibly from the metal plate and water collection is carried out. It provides the metal plate, a cooler for cooling the metal plate, and a water film peeling-off mechanism for flipping off forcibly and peeling off forcibly the water film generated on the surface of the metal plate. A water collection metal plate wherein with the metal plate having the surface in which an effective surface of after processing is enlarged to a surface area before processing, the water film is generated to the surface of the metal plate by dew condensing moisture in atmosphere, the generation water film is flipped off forcibly and peeling off from the metal plate, thereby the water collection is carried out.

Abstract: The subject invention pertains to a method and apparatus for cooling. In a specific embodiment, the subject invention relates to a lightweight, compact, reliable, and efficient cooling system. The subject system can provide heat stress relief to individuals operating under, for example, hazardous conditions, or in elevated temperatures, while wearing protective clothing. The subject invention also relates to a condenser for transferring heat from a refrigerant to an external fluid in thermal contact with the condenser. The subject condenser can have a heat transfer surface and can be designed for an external fluid, such as air, to flow across the heat transfer surface and allow the transfer of heat from heat transfer surface to the external fluid. In a specific embodiment, the flow of the external fluid is parallel to the heat transfer surface.

Abstract: The subject invention pertains to a method and apparatus for cooling. In a specific embodiment, the subject invention relates to a lightweight, compact, reliable, and efficient cooling system. The subject system can provide heat stress relief to individuals operating under, for example, hazardous conditions, or in elevated temperatures, while wearing protective clothing. The subject invention also relates to a condenser for transferring heat from a refrigerant to an external fluid in thermal contact with the condenser. The subject condenser can have a heat transfer surface and can be designed for an external fluid, such as air, to flow across the heat transfer surface and allow the transfer of heat from heat transfer surface to the external fluid. In a specific embodiment, the flow of the external fluid is parallel to the heat transfer surface.

Abstract: A refrigerant system utilizes an expander that provides a more efficient expansion process and recovers at least a portion of energy from this expansion process. At least a portion of refrigerant that has been at least partially expanded in the expander is tapped and passed through an economizer heat exchanger. In the economizer heat exchanger, the tapped refrigerant cools a main circuit refrigerant increasing its thermodynamic potential. Further, a compression section is provided with at least two compressors operating in tandem and allowing for multiple stages of unloading. By selectively utilizing one or more of the tandem compressors, the economizer cycle, and the expander, the refrigerant system can achieve very efficient operation and provide enhanced control flexibility, in particular, for the CO2 refrigerant system operating in the transcritical cycle.

Abstract: A method is provided for mitigating two-phase refrigerant maldistribution in heat exchange channels of a parallel flow evaporator. An inlet manifold of the evaporator includes a first stage, at least one intermediate stage, and a final stage. Each stage includes an expansion chamber, a contraction chamber, and at least one heat exchange channel interconnecting the stage to an outlet manifold of the evaporator. The method includes throttling the two-phase refrigerant in the expansion chamber of each stage, flowing a portion of the throttled refrigerant through the at least one heat exchange channel to the outlet manifold, mixing and jetting the two-phase refrigerant in each contraction chamber to increase the velocity of the refrigerant, and passing the refrigerant out an exit of the outlet manifold.

Abstract: A life support system includes a refuge housing and a cooling system. The cooling system, which has a supply of liquefied gas and a cooling circuit, is operatively associated with the refuge housing. The supply of liquefied gas is operatively associated with the cooling circuit that contains a heat exchanger, a fan motor and a fan operatively associated with the fan motor. A conduit connects the heat exchanger to the fan motor that is driven by waste gas generated through a phase change of the liquefied gas in the heat exchanger.

Abstract: The invention described herein represents a significant improvement in the efficiency of heating and cooling processes for applications such as buildings. The working fluid condensation process is time separated from the working fluid vaporization process. Work on the working fluid through a phase transformation is performed at a first time and the heating or cooling of a building through a reverse phase transformation is done at a second time. A storage medium is provided to store the capacity to heat or the capacity to cool in the form of the phase transformed working fluid stored at a positive or a negative pressure. Controlling logic calculates what the heating and cooling load will be in the future and when least expensive and most efficient operating times are forecasted to be. The compression or vacuum energy input phase of operation is be performed during the most optimal window as seldom as once per week while the application heating or cooling process is performed continuously as needed.

Abstract: A portable cooler has a thermally isolating outer shell defining an internal compartment for holding contents to be kept cool, such as, for example, food, drinks and temperature-sensitive medicine. The portable cooler has a door connected to the outer shell for providing unrestricted access to the internal compartment. The portable cooler may have a shelf for holding a cold gel pack to help keep the contents cool. The cooler may also have a plurality of dividers (that are optionally reconfigurable) for defining variously sized storage spaces for the contents. The cooler may have an aesthetically pleasing curved outer shell and an adjustable shoulder strap so that the cooler can be carried on a person's shoulder. Because the cooler is easy and comfortable to carry and because its large swing-open door provides full and quick access to its contents, this cooler is more ergonomic and aesthetic than traditional designs.

Abstract: A cooling member for a variable speed drive is disclosed. The cooling member includes including at least two channels, each channel including at least one inlet and at least one outlet, a first passageway configured to provide fluid to the at least two channels through the at least one inlet of each channel, a second passageway configured to receive fluid from the at least one outlet of each channel the at least two channels, and a connector to connect the cooling member to a second cooling member.

Abstract: An ion generating device generates O2?(H2O)n (where n is a natural number) as negative ions and H+(H2O)m (where m is a natural number) as positive ions, and discharges those ions into the air so that airborne germs are killed through an oxidation reaction by hydrogen peroxide H2O2 or radical hydroxyl OH generated through as an active species a chemical reaction between the negative and positive ions. Satisfactory sterilization is achieved when the negative and positive ions are generated in such a way that the concentrations of the negative and positive ions are both 10,000 ion/cc at a distance of 10 cm from the point at which they are generated.

Abstract: An evaporator, in particular for a motor vehicle air conditioner, is provided that includes at least one block constructed largely of tube elements and rib elements, whereby it is possible for a refrigerant to flow through the tube elements, at least one section of the block being provided with a condensation water overflow protection means, which includes at least one restriction plate, the height of the restriction plate in at least one section being lower than a height in at least one second section adjacent to the first section.

Abstract: An easily-drainable dehumidifier that is designed to automatically or manually drain water stored in a water tank in accordance with a user selection is provided.

Abstract: A refrigerator includes an interior and an ice maker that is arranged in the interior and has a removable ice tray. A central module of the ice maker is firmly mounted on an inner wall of the refrigerator and the ice tray is detachably connected to the central module. A fresh water tank is detachably coupled to the central module such that fresh water can be transferred from the fresh water tank to the central module.

Abstract: Disclosed related to a refrigerator according to the present invention comprising a main body in which a cold air storage is provided; a door connected to the main body; a dispenser assembly mounted on the door; and a tray assembly selectively protrudably connected to the dispenser assembly therefrom in a front direction.

Abstract: An air conditioner has a function of carrying a mist of charged minute water particles on a ventilated air being blown into a room. The air conditioner includes a blower blowing the ventilated air and an atomizing unit configured to be supplied with water and to electrostatically atomize it into the mist of minute charged water particles. A housing of the air conditioner is divided by a partition into a flow channel leading from an air inlet to an air outlet and a compartment accommodating therein the atomizing unit. A feed conduit extends from a feed port of the atomizing unit into a flow channel through the partition to feed the mist to the air being blown out through the air outlet, while the atomizing unit is isolated from the flow channel to minimize flow resistance.

Abstract: A refrigerator is provided that has an interior that is surrounded by an inner shell, the interior for storing refrigerated or frozen products. The refrigerator includes a control system that has a cold generator. A temperature sensor is arranged in the interior, wherein the temperature sensor is connected to the control system. A screen prevents contact between the temperature sensor and the refrigerated or frozen products.

Abstract: Disclosed herein is a refrigerator, which prevents a filler unit from being worn away or broken. The refrigerator includes a main body, storage chambers divisionally provided in the main body, a pair of doors opening and closing one of the storage chambers, a filler unit rotatably connected to at least one of the pair of doors to seal a separation space between the doors, a guide member provided on the main body to guide rotation of the filler unit, and a protection unit mounted on the filler unit to rotate the filler unit according to insertion and separation of the protection unit into and from the guide member and to prevent the breakage of the filler unit due to collision with the guide member.

Abstract: An evaporator, applicable to a two-stage expansion cooling system, is used for receiving a high-pressure liquid working fluid. The evaporator includes a thermal-conductive block having a channel system. The channel system includes a high-pressure channel, a low-pressure channel, and a second stage expansion channel. The second stage expansion channel has an input end and an output end. The input end is communicated with the high-pressure channel. The output end is communicated with the low-pressure channel, and has a cross-sectional area smaller than that of the low-pressure channel. The high-pressure liquid working fluid flows into the thermal-conductive block from the high-pressure channel, and then enters the second stage expansion channel through the input end. A part of the high-pressure liquid working fluid flowing out of the output end expands into a saturated low-pressure liquid working fluid and enters the low-pressure channel.