Abstract: A method for closing a box (1) by folding a lateral closing flap (5) extending from an upper edge (6) of a lateral aperture (7) of the box (1) and having at least one foldable edge (8), while the box (1) is being moved along a packaging line (L) in a forward movement direction (W), includes the steps of folding the lateral flap (5) until a connection line (9) of the foldable edge (8) touches stop means (15), then folding the foldable edge (8) on the striking means (15) and toward the lateral aperture (7) of the box (1), so that an outer edge (8a) of the foldable edge (8) interacts with contrast means (17), which keep elastically the edge (8) in a position raised with respect to a bottom wall (1a) of the box (1), and lastly introducing the edge (8) into the box (1). A device for carrying out the methods has folding means (14) for folding the said lateral flap.

Abstract: An adjustable stripper/moistener system for a mailing system is provided. The stripper blade and moistening assembly are adjustable in a direction transverse to the movement of a mail piece being passed through the mailing machine. By allowing the stripper blade to move with respect to the feed deck, the position of the stripper blade can be optimally set to reliably strip different size and shape flaps from different types of envelopes. Additionally, by allowing the moistening assembly to move in conjunction with the stripper blade, there is better control of the amount and location of deposition of the moistening fluid on the envelope flap, thereby preventing possible damage to the envelope or its contents. The position of the stripper blade and moistening assembly may be manually adjustable by an operator, or automatically adjusted based on an input or sensed profile of the envelope flap.

Abstract: A gel saddle (20) comprising of a gel seat (15) that is attached to stirrup riggings (92) which lie under skirts (44). Seat (15), skirts (44) and stirrup riggings (92) are attached to gel seat cushion (57) and rest on flaps (18). Flaps (18) cover girth straps (73) which are on top of sweat flaps (62) and all are attached and rest upon gel panels (10). Panels (10) rest on each side of the spine of the animal (400) creating an open space or gullet (17) over the spine of the animal (400). A girth (47) connects to one side of the girth straps (73) encircle the animal (400) and connects to the other side of girth straps (73).

Abstract: The present invention is a separation apparatus that combines the effects of a cylindrical vortex and a series of partial toroidal vortices. The toroidal vortex and cylindrical vortex fluid flows combined provide better separation than either fluid flow alone. Moreover, the present invention may be constructed such that an arbitrary number of partial toroidal vortices, in series, having relatively small radii are formed thereby allowing any level of separation to be achieved.

Abstract: A coalescing assembly for coalescing entrained oil from a high temperature, high velocity gas stream comprises a coalescing element of compacted high temperature polyamide fibers, such as those available under the trademark Nomex®, rigidly held by concentric cylindrical support structures of a dense fibrous material such as stainless steel. The coalescing assembly forms a component of an oil coalescer having a unique hole configuration in its outer shell to prevent coalesced oil from being re-entrained into the gas stream. The oil coalescer is a component of an oil separator for use in aircraft operational environments and features high durability and longevity of 10 years or more.

Abstract: An air cleaning apparatus includes a blowing unit and a filtering unit which are easily removed from and installed in a cabinet, allowing the air cleaning apparatus to be easily cleaned. The cabinet included in the air cleaning apparatus may be used as a table. The cabinet is provided with a top panel of a predetermined area, is opened at a bottom thereof, and is provided on at least one side wall thereof with an air outlet port. A fan casing is installed in the cabinet to be drawn out from the cabinet in a horizontal direction. A blowing fan is installed in the fan casing to move air to the air outlet port. A filter casing is installed under the fan casing to be drawn out from the cabinet in the horizontal direction, and at least one filter is installed in the filter casing.

Abstract: The object is to provide an Air clean appratus that cleans up floating dusts in air in a room and is configured in a shape that can be placed in dead space in a room and will not be an obstacle when it is placed in a room. [Means for Achieving the Object] An Air clean appratus comprising an air intake 13 intended to be located at a lower position in a corner of a room and an air outlet 14 intended to be located at an upper position in the corner of the room, and at least a filter 15 and a blower 18 both inside the Air clean appratus, characterized in that, when the Air clean appratus is installed in a room, a given quantity of circulating blowing air, the said quantity is decided according to the height from the floor underneath the air intake and the underside-open area determined on the basis of particles of the maximum size to be eliminated at the air intake.

Abstract: A honeycomb structure 1 has a large number of through-holes 3 divided by partition walls 2 and extending in the axial direction, characterized in that the honeycomb structure contains a Si phase having a lattice constant controlled at 0.54302 to 0.54311 nm at room temperature. A process for producing the honeycomb structure 1, includes a firing step of firing a precursor of honeycomb structure, wherein the precursor contains a Si phase and the firing step is conducted using a furnace material free from any boron-containing compound. A process for producing the honeycomb structure 1, includes a firing step of firing a precursor of honeycomb structure, wherein a reduction percentage of Si content in Si phase after firing step relative to Si content in Si phase before firing step is suppressed at 10% by mass or less. Having an improved thermal conductivity, the honeycomb structure is superior in thermal shock resistance.

Abstract: A chassis (10) for a grass treatment machine and which is adapted to mount thereon an elongate grass treatment module (20, 21, 22, 23) having opposed outer ends (24) by which it is mounted on the chassis (10), and in which: the chassis (10) is intended to be mounted in, or form part of the frame of a grass treatment machine; the chassis (10) has two module mountings (11) which are laterally spaced from each other with respect to the direction of travel of the machine, and each mounting (11) being adapted to receive a respective outer end (24) of the module (20); and the chassis comprises two chassis portions (12, 13) which can be asssembled in order to hold the outer ends (24) of the module (20) in the module mountings (11) in order to mount the module (20) on the chassis (10), and which can be relatively separated in order to provide access to the module mountings (11) for the purposes of mounting or de-mounting the ends (24) of the module (20) relative to the chassis (10).

Abstract: A control apparatus for a lawn mower which includes two coupling members pivotable about a single axis. The coupling members are connected to a drive mechanism and a braking mechanism for the lawn mower. The lawn mower device has a drive configured to rotate a shaft in a first direction. A drive wheel is coupled to the shaft and is coupled to a driven wheel by a drive belt. A tensioning system is shown coupled to the drive belt. The tensioning system has a first idler plate configured to bias a first idler pulley against the drive belt when the drive is rotating the shaft in the first direction and a second idler plate configured to bias a second idler plate against the drive belt when the drive is rotating the shaft in a second direction. A brake mechanism is further coupled to the tensioning system. The brake mechanism is configured to resist the rotation of the driven wheel. A brake lockout is provided which resist the inadvertent engagement of the brake when the mower is driven in a reverse direction.

Abstract: Apparatus for forming a spliced yarn includes a yarn conduction member with an intermingling jet disposed forwardly thereof. The yarn conduction member has respective yarn conduction channels through which the first and second yarns are conveyed to the intermingling jet. The axis of each yarn conduction channel from the inlet to the outlet of the member is a straight line, with no bends or deviations. The yarn conduction member has a knife blade disposed adjacent to a respective yarn conduction channel. Each knife blade has a passage defining a cutting edge and a solid portion disposed between the passage and the tip of the blade. The first and second knives are insertable into and retractable from the channel to which they are adjacent. In the inserted position the passage in the knife aligns with the channel into which it is inserted, while in the retracted position the solid portion of the blade interdicts the passage to prevent movement of a yarn therethrough.

Abstract: A method for producing a spliced yarn comprising alternating predetermined lengths of a first and a second yarn and to the yarn are disclosed.

Abstract: A method for making a wire package for use as staples or brads is recited as forming a plurality of round wires, forming a plurality of flattened bonding sides on each wire to prepare even bonding surfaces on each wire and bonding each wire to an adjacent wire by adhering the surfaces of each wire. Each staple includes two or more flat surfaces to improve the bonding strength of each staple.

Abstract: The flow path of the exhaust of a recuperator of a microturbine engine system is routed to insulate the turbine exhaust in the recuperator. The recuperator is encapsulated for defining a passage for flowing the exhaust over the outer diameter of the recuperator so as to insulate the heat within the recuperator. A by-pass system that is operable mechanically or automatically directs turbine exhaust to by-pass the recuperator is disclosed in another embodiment. The by-pass serves to trim the efficiencies of the original manufactured microturbine engines so that all the engines attain a given preselected matching efficiency level. The by-pass can also be utilized to control the temperature of a boiler, chiller or other elements incorporated in the microturbine system by controlling the turbine exhaust to by-pass the recuperator.

Abstract: A wide-angle diffuser for a combustion turbine system having a turbine provides multiple expanding flow paths for the turbine exhaust. Each flow path is arranged to have the ideal diffusion angle for the given flow thus allowing for complete and efficient expansion of the turbine exhaust with a shorter length diffuser. An inner tube having an ideal diffusion angle is surrounded by a plurality of frustoconical tubes having larger opening angles producing a plurality of interstitial flow paths.

Abstract: The engine for a rocket is suitable for using for an educational program. The engine uses a liquid phase propellant having a predetermined boiling point and a heating substance having a temperature higher than the boiling point. The engine has an inner wall having a circumferential surface; an outer wall surrounding the inner wall, the outer wall having an interior surface spaced from the circumferential surface of the inner wall by a predetermined distance such that the space between the circumferential surface and the interior surface form a mixing chamber having an opening; and injector for injecting the liquid-phase propellant and the heating substance into the mixing chamber so that the propellant is evaporated by the heating substance thereby creating a jet stream moving from the opening of the mixing chamber to the outside of the mixing chamber.

Abstract: A method enables thrust to be generated from a gas turbine engine using a pulse detonation system is provided. The engine includes an inlet portion and an exhaust portion, and the pulse detonation system includes a multi-staged pulse detonation augmentor including predetonator. The method comprises supplying a less than stoichiometric fuel/air mixture to the pulse detonation system during a first operating stage, detonating the fuel/air mixture with the predetonator to increase the temperature and pressure within the engine and to generate engine thrust, and supplying additional fuel and air to the pulse detonation system during a second operating stage.

Abstract: A fluid flow actuated valve for controlling the fluid flow in a conduit comprises a support structure adapted to be mounted within the conduit and at least one flap member pivotally mounted to the support structure. The at least one flap member is pivotable between an first position for a minimum fluid flow and a second position for a maximum fluid flow. A torsion spring is attached to the at least one flap member to urge the same to pivot against a fluid pressure differential, from the first position to the second position when the fluid pressure differential is smaller than a predetermined level.

Abstract: An emissions control system is used with a compression ignition engine capable of producing an exhaust gas stream to be treated by a reduction agent which is mixed with the exhaust gas stream to convert the exhaust gas stream prior to being directed into an SCR catalyst capable of reducing NOx in the exhaust gas stream. An exhaust gas recirculation valve is associated with the compression ignition engine for directing the exhaust gas stream back into the compression ignition engine. An electronic control unit and sensors determine whether the temperature of the exhaust gas stream is at a predetermined temperature, and if so control operation of the valve to allow a portion of the exhaust gas stream to be directed into the SCR catalyst. A bypass valve may also be provided to prevent the exhaust gas stream from entering into the SCR catalyst.

Abstract: An engine control system in a vehicle including a variable displacement internal combustion engine, a controller for controlling the displacement of the variable displacement internal combustion engine, and where the controller operates the variable displacement internal combustion engine in a partially displaced operating mode upon startup to increase exhaust gas temperature.

Abstract: A device and a method for controlling an exhaust-gas aftertreatment system, in particular for an internal combustion engine, are described. The exhaust-gas aftertreatment system includes at least one catalytic converter. A reducing agent is supplied to the exhaust-gas aftertreatment system. An exhaust gas mass flow is preselectable on the basis of the power consumption by a sensor and/or on the basis of a pressure variable.

Abstract: A selective catalytic reduction emissions control system of a compression ignition engine is provided with enhanced ammonia feed control for improved emissions control performance. The reduction agent is provided in two doses, and the reactor is provided with two reacting beds. The second dose of reactant is provided between the first and second reacting beds.

Abstract: A particulate filter regenerating device is configured to prevent the uneven distribution of particulate matter that results from interruption of the regeneration process and protect the particulate filter. The frequency with which regeneration is executed is increased by determining that it is time to regenerate the particulate filter at a time t1 when the exhaust gas temperature Texhin has reached or exceeded a prescribed temperature Texh1. Additionally, particulate filter regenerating device determines that it is time to regenerate the particulate filter when the quantity of accumulated particulate matter reaches or exceeds a prescribed value PM1. The particulate filter is regenerated by raising the temperature of the exhaust gas and combusting the accumulated particulate matter.

Abstract: An exhaust purification system for use with diesel or other compression ignited systems to remove particulate and gaseous pollutants from the exhaust. The system includes a catalytic converter assembly that heats the exhaust to a level sufficient to incinerate particulate pollutants in the exhaust prior to the pollutants contacting the catalytic element and a plurality of gas cooling elements communicating with the exhaust outlet in the catalytic converter assembly for reducing the temperature of the exhaust passing from that assembly to about 100° F. whereupon the cooled exhaust is directed back to the engine for further combustion.

Abstract: A torque converter is provided to improve the transmission efficiency of a torque converter having a low flatness ratio. An impeller 21, a turbine 22, and a stator 23 constitute a torus. The flatness ratio of the torus, which is the ratio of the axial length L to the radial length H (L/H), is less than 0.8 and the impeller 21 has at least thirty-seven impeller blades 27 on the side facing the turbine 22.

Abstract: A torque converter having an improved capacity coefficient at high-speed ratios is provided. An impeller 11, a turbine 12, and a stator 13 constitute a torus. The torus rotates about a rotational axis O-O. The impeller 11, turbine 12, and stator 13 each have blades 22, 32, and 42. Furthermore, the radius R1 of the impeller inflow part 22a, i.e., the distance between the radially inside end part of the impeller blades 22 and the rotational axis, is smaller than the radius R2 of the stator inflow/outflow part 42a, i.e., the distance between the radially inside end parts of the stator blades 42 and the rotational axis.

Abstract: A fan drive system includes a pump, at least one implement arrangement in fluid communication with the pump and a fan drive unit driveably connected to the pump. The fan drive unit is in fluid communication with the pump through a modulation valve. A signal operator is structured and arranged to receive at least one implement signal and a fan drive signal and generate a load signal output, wherein the pump is adapted to modify an output flow of the pump in response to the load signal. A control valve is urged to respond under the influence of a sensed condition and is in fluid communication with the modulation valve and the signal operator through a signal conduit.

Abstract: One preferred embodiment of the present invention, provides an auxiliary hydraulic drive system having a total hydraulic flow. The system includes a primary hydraulic pump operable to provide hydraulic flow for an implement, and a flow control valve in communication with the hydraulic flow. The flow control valve operates to allow an optimum flow rate and diverts the excess flow amount when the total hydraulic flow exceeds the optimum flow rate. A secondary hydraulic pump is selectively operable to provide additional hydraulic flow. A control system is operable to engage the secondary pump when the total hydraulic flow drops below a minimum flow level; and the control system operates to disengage the secondary pump when the total hydraulic flow exceeds a maximum flow level. In a further embodiment, the invention provides a control unit for a hydraulic system. The control unit includes a sensor to measure total hydraulic fluid flow in a system; and a controller coupled to the sensor.

Abstract: A liquid primary fuel is ignited by HCCI with the assistance of the early injection of a liquid pilot fuel. Pilot fuel injection and/or ignition are preferably controlled so as to permit the injected pilot fuel to become thoroughly distributed through and mixed with the primary fuel/air charge in the combustion chamber and vaporized prior to ignition. Pilot fuel having a lower autoignition temperature will be ignited by compression ignition, followed by the ignition of the homogeneous mixture of the primary fuel and air. HCCI combustion of the primary fuel is facilitated by 1) selection of the properties of the primary and pilot fuels and 2) obtaining a homogenous mixture of primary fuel and air by injecting primary fuel into the engine's intake air stream in the form of finely atomized droplets having a mean diameter in the micron range.

Abstract: A control system controls a turbo-charged throttled engine having intake air compressor, an exhaust turbine which receives engine exhaust. The control system includes an air throttle between the compressor and the engine, a wastegate communicated with engine exhaust upstream and downstream from the turbine, and a control unit for controlling the air throttle and the wastegate. The control unit generates a desired air mass value per engine stroke value as a function of a desired fuel flow amount and a stored a compressor surge characteristic, generates a desired manifold air pressure value as a function of the desired air mass value and sensed engine parameters, and controls the air throttle so that an actual manifold air pressure matches the desired manifold air pressure.

Abstract: A method of operating an internal combustion engine, including at least one cylinder and a piston slidable in the cylinder, may include supplying pressurized air from an intake manifold to an air intake port of a combustion chamber in the cylinder, selectively operating an air intake valve to open the air intake port to allow pressurized air to flow between the combustion chamber and the intake manifold substantially during a majority portion of a compression stroke of the piston, and operably controlling a fuel supply system to inject fuel into the combustion chamber after the intake valve is closed.

Abstract: A premix secondary fuel nozzle for use in transferring a flame from a first combustion chamber to a second combustion chamber is disclosed. The secondary fuel nozzle includes multiple fuel circuits, each of which are fully premixed, and neither of which are injected in a manner to directly initiate or support a pilot flame, thereby lowering emissions. Multiple embodiments are disclosed for alternate configurations of a first fuel injector, including an annular manifold and a plurality of radially extending tubes.

Abstract: A premix secondary fuel nozzle for use in transferring a flame from a first combustion chamber to a second combustion chamber is disclosed. The secondary fuel nozzle includes multiple fuel circuits, each of which are fully premixed, and neither of which are injected in a manner to directly initiate or support a pilot flame, thereby lowering emissions. Multiple embodiments are disclosed for alternate configurations of a first fuel injector, including an annular manifold and a plurality of radially extending tubes. Alternate premix secondary fuel nozzles are also disclosed incorporating improved tip cooling schemes that reduce the amount of cooling flow and increase the local heat transfer effectiveness. Reduced cooling flow to the tip region helps to improve flame stability and lower combustion dynamics by eliminating unnecessary cooling air from the fuel nozzle recirculation zone.

Abstract: A floating collar assembly for damping vibration and sealing between a combustor and a fuel nozzle of a gas turbine engine. The combustor has a nozzle opening with an outer peripheral abutment surface and the nozzle is integral with an internal fuel manifold that is secured to the engine core relative to the combustor. The nozzle has a cylindrical body aligned with the nozzle opening and has a shoulder laterally extending from the nozzle body. An annular floating collar has a combustor face adapted for radial sliding engagement with the abutment surface, a central aperture adapted for axial sliding engagement with the cylindrical body and an outer bearing surface. A wave spring is disposed between the outer bearing surface of the floating collar and an inner surface of the nozzle shoulder, for maintaining sealing engagement, for damping vibration, and for impeding relative rotation between the nozzle and the combustor, while accommodating axial and radial relative displacement.

Abstract: A mounting assembly for a forward end of a liner in a combustor of a gas turbine engine including a dome and a cowl, wherein a longitudinal centerline axis extends through the gas turbine engine. The mounting assembly includes a pin member extending through each one of a plurality of circumferentially spaced openings formed in the forward end of the liner, an aft portion of the cowl, and a portion of the dome, with each pin member including a head portion at one end thereof. A nut is adjustably connected to an end of each pin member opposite the head portion. A bushing is located on each pin member at a position intermediate the head portion and the nut, wherein the openings in the liner forward end are sized to fit around the bushings.

Abstract: In order to develop a combustion chamber with a closed cooling system for a turbine with an inner wall and an outer wall (1) bounding the combustion area, wherein there is an intermediate space between the inner wall and the outer wall (1) through which cooling fluid can flow, and which comprises a cooling fluid feed system opening out into the intermediate space and a cooling fluid discharge system for discharging the cooling fluid from the intermediate space, so that it has a reduced extension in the radial direction, it is proposed with the invention that the cooling fluid discharge system should comprise channel-type drainage structures (8) running essentially along the axial orientation of the combustion chamber, which are interrupted by inlet structures (4) of the cooling fluid feed system arranged between the drainage structures (8).

Abstract: In order to develop a flow control body (6) for separate control of a cooling fluid inflow and a cooling fluid outflow for combustion chambers with a closed cooling system for turbines such that a simplified cooling fluid flow control is made possible in the combustion chamber wall, it is proposed with the invention that the flow control body (6) has a non-rotationally symmetrical cross-sectional shape (7) in a flow control section.

Abstract: A turbine inlet air-cooling system improves turbine performance and efficiency. A dehumidifier receives process airflow and reduces a moisture content of the process airflow. An indirect evaporative cooler receives the process airflow from the dehumidifier and is driven by the process airflow from the dehumidifier such that a first portion of the process airflow is contacted directly with water and a second portion of the process airflow is cooled without any addition of moisture. A direct evaporative cooler receives the second portion of the process airflow, which is contacted directly with water to provide evaporative cooling. Subsequently, the direct evaporative cooler outputs the second portion of the process airflow to the turbine.

Abstract: A chemical solvent is utilized to preferentially remove CO2 from a H2S-rich acid gas stream, the acid gas stream being absorbed by the chemical solvent from a sour syngas stream. A chemical solvent such as alkanolamine is used in a unique process configuration to separate CO2 from the acid gas stream. The resulting acid gas is significantly higher in H2S concentration with a substantial quantity of CO2 being removed. The resulting CO2-rich gas is recovered at minimal pressure loss, and can be remixed with the resulting sweet syngas stream as a feed for a gas combustion turbine for increased power generation.

Abstract: A mounting assembly for an aft end of a liner of a gas turbine engine combustor including a support member, wherein a longitudinal centerline axis extends through the gas turbine engine. The mounting assembly includes a pin member extending through each one of a plurality of circumferentially spaced openings in a portion of the support member for the combustor and into a plurality of partial openings formed in the aft end of the liner, with each pin member including a head portion at one end thereof, and a device positioned within each opening in the support member so as to retain the pin members therein. The pin members and the support member are able to slide radially and/or axially with respect to the liner aft end as the support member experiences thermal growth greater than the liner.

Abstract: A mounting system, for installing a starter-generator to an accessory housing, where the starter-generator has a mounting end with a connecting flange and a cooling air outlet radially inward of a peripheral starter-generator housing edge, and where the accessory housing has a matching connecting flange radially inward of a peripheral accessory housing edge. The mounting system includes a cooling air outlet collection shroud enveloping the peripheral starter-generator housing edge and the peripheral accessory housing edge, the shroud having a discharge outlet. A V-band clamp releasably secures the connecting flanges together and is enveloped within the shroud in a compact mounting system that collects and discharges the exhausted cooling air.

Abstract: Apparatus and methods in accordance with the present invention utilize thermoelectric cooling (TEC) technology to provide enhanced power distribution and/or dissipation from a microelectronic die and/or microelectronic packages. Individual TEC devices are thermally interconnected with the microelectronic die in a number of placement configurations, including between the microelectronic die and the heat sink, on the integrated heat spreader (IHS) inner surface, and on the IHS outer surface. TEC devices comprise p- and n-type semiconducting material created using similar process as the microcircuits. The TEC devices are located in various regions within or on the microelectronic die, including directly below the microcircuits, on the backside of the microelectronic die, and on a separate substrate of microelectronic die material fabricated apart from the microelectronic die and subsequently thermally coupled to the backside of the microelectronic die.

Abstract: An apparatus and method which is particularly suitable for maintaining a wafer at an optimum temperature for the alignment and exposure step during photolithography. The apparatus includes a cooling plate having at least one cooling channel. A coolant is continually circulated through the cooling channel to cool the cooling plate and the wafer resting thereon prior to transfer of the wafer to a wafer stage in a stepper, for example. The cooling plate may be mounted on an OF table inside the stepper and include a central opening for receiving the wafer-engaging shaft of the OF table. The cooling plate maintains all regions of the wafer at substantially the same temperature as the wafer stage in the stepper prior to transfer of the wafer to the wafer stage.

Abstract: A system for enhancing the cooling of a product stream, wherein the product stream is a livestock feed product, is disclosed. The system has a reduction station and a conveyor system with a conveyor belt routed through the reduction station. The conveyor belt is used to transport the product stream through the reduction station. The reduction station increases the surface area to volume ratio of the product stream.

Abstract: A lubricant still for use in a compressor for separating oil from refrigerant, includes a vessel having an inlet for incoming oil laden refrigerant, an outlet for gaseous refrigerant, and an outlet for refrigerant laden oil. A separating structure is provided for separating transitioning oil laden refrigerant from the incoming oil-laden refrigerant, wherein the oil laden refrigerant progressively changes to the refrigerant laden oil closer to the outlet for refrigerant laden oil. A heating device is used for heating the incoming oil laden refrigerant and transitioning oil laden refrigerant, for facilitating the formation of the gaseous refrigerant and the refrigerant laden oil.

Abstract: A dehumidifying air-conditioning apparatus comprises a pressurizer (4) for raising a pressure of a refrigerant, a condenser (5) for condensing the refrigerant to heat a high-temperature heat source fluid, and an evaporator (1) for evaporating the refrigerant to cool process air to a temperature lower than its dew point. The dehumidifying air-conditioning apparatus further comprises a refrigerant path branched into a plurality of branched refrigerant paths (42, 43, 44) between the condenser (5) and the evaporator (1). A first heat exchanging portion (21) is disposed in the branched refrigerant path for evaporating the refrigerant under an intermediate pressure between the condensing pressure of the condenser (5) and the evaporating pressure of the evaporator (1) to cool the process air by evaporation of the refrigerant under the intermediate pressure.

Abstract: A refrigerating device is provided in which a compressor, a gas cooler, an expansion mechanism and an evaporator are sequentially connected by using refrigerant pipes. The refrigerating device uses a refrigerant mixture in which a combustible nature refrigerant and a carbon dioxide refrigerant are mixed, and an amount of the carbon dioxide refrigerant in the mixture refrigerant is 20 to 50 mass %. Alternatively, a maximum fill amount of the combustible nature refrigerant is 150 g. Therefore, the refrigerating device has a higher coefficient of performance, a high refrigerating capacity and its safety is higher than that of using only hydrocarbon refrigerant.

Abstract: Disclosed are an air conditioner, which reduces an electric power consumption rate and rapidly copes with the requirements of a user, and a method for operating the air conditioner in a cooling mode for cooling air in a room by an independent or simultaneous operation of small-capacity and large-capacity compressors in accordance with the variation of a cooling load.

Abstract: A system and method for cooling a room configured to house a plurality of computer systems. A heat exchanger unit is configured to receive air from the room and to deliver air to the room. The heat exchanger unit is supplied with cooling fluid operable to cool the received air in the heat exchanger unit. At least one of the temperature of the cooling fluid supplied to the heat exchanger unit and the air delivery to the room may be controlled in response to temperatures sensed at one or more locations in the room.

Abstract: A system and method for cooling a room configured to house a plurality of computer systems. A heat exchanger unit is configured to receive air from the room and to deliver air to the room. The heat exchanger unit is supplied with cooling fluid operable to cool the received air in the heat exchanger unit. At least one of the temperature of the cooling fluid supplied to the heat exchanger unit and the air delivery to the room may be controlled in response to temperatures sensed at one or more locations in the room.