Abstract: A hydro electric power plant, specifically structured to operate by moving fluid, e.g. water, from a low level reservoir to a high level reservoir, and back through a turbine-generator, water wheel, etc. which is structured to be self sufficient, and to supply an unlimited amount of power.

Abstract: What is disclosed is a hydraulic control arrangement for attenuating travel vibrations of a mobile working tool, comprising a lift cylinder supporting a working tool, the cylinder chambers of which may be connected to a pressure medium source or to a tank via a control valve arrangement. The hydraulic control arrangement moreover includes an attenuation valve arrangement for connection of one cylinder chamber with an hydraulic accumulator and of the other cylinder chambers with a tank. In accordance with the invention, the attenuation valve arrangement includes a valve having a pressure limiting function and arranged between a check valve and the hydraulic accumulator, so that the pressure in the hydraulic accumulator may reliably be limited to a maximum value.

Abstract: In a Stirling cycle engine, a regenerator has a bobbin, a resin film wound around the outer surface of the bobbin, and a sheath fitted around the outer surface of the resin film and having a slit formed vertically therein. The resin film has one end fixed on the outer surface of the bobbin, and has the other end led out through the slit and fixed to an end surface of the slit or to the outer surface of the sheath. The sheath is press-fitted on the inner surface of the cylinderenclosure. Working gas flows between different layers of the resin film. This reduces the loss of heat due to gas leakage and thereby improves the heat exchange efficiency in the regenerator.

Abstract: Braking device comprising a master cylinder (2), a primary piston (3), a manual-control member (4), a booster (6) coupled to the manual-control member (4), and an emergency assist valve (VA) comprising a reaction piston (17) through which there passes a ratio control (24) having a head (25) located in a chamber (26) lying between the reaction piston (17) and a bushing (27) housed further forward in a bore (18) of the primary piston, this bushing (27) having an axial passage (28) in which there can slide a rapid piston (29), the rear end of which forms, with the head (25), a valve (36) capable of closing the inlet to a passage (30) in the rapid piston. The device comprises a means (E), consisting in the bushing (27) being mounted so that it can slide, for limiting the pressure difference between the chamber (26) and a zone (18a) of the bore situated forward of the bushing, to a value below the one which can cause the valve (36) to open.

Abstract: A negative pressure type brake hydraulic pressure generating device is proposed in which the stroke on the operating side can be set independently of the stroke on the output side. A slide resistance imparting means is provided between the fixed shell and a piston having a built-in control valve introducing atmospheric air to cancel the slide resistance which is the cause of increased stroke hysteresis of the piston, i.e. the slide resistance applied to the piston at airtight seal portions between the power plate and the piston.

Abstract: The invention relates to an exhaust gas turbocharger (1) having a housing and having a shaft (2) which is arranged so as to be capable of rotating about its longitudinal axis in the housing and on which a turbine wheel (4) and a compressor wheel (3) are seated and which is guided in radial bearings (5, 6) which are embodied as magnetic bearings and in at least one axial bearing (9), the bearings (5, 6, 9) each having a bearing plate (12, 14, 16) which is seated on the shaft (2) and at least one stator (19, 20, 21, 22, 49, 50) which lies axially opposite said axial bearing (9) on at least one side, forming a gap. In order to cool the bearings, it is proposed according to the invention that at least one flow duct (62, 65), via which at least one bearing gap can have an air stream applied to it, is formed in the housing.

Abstract: An exhaust device includes a housing, a drive unit, and an electric generator. The housing includes a tubular wall with a tube axis, and a mounting wall transverse to the tube axis. The tubular wall has an inlet end portion to be connected to a source of exhaust gas. The housing is formed with a vent for discharging the exhaust gas. The drive unit includes a drive shaft disposed in the housing, and an impeller connected to the drive shaft such that the exhaust gas received from the source can drive rotation of the drive shaft. The electric generator includes a stator mounted on the mounting wall, and a rotor coupled to the drive shaft such that the rotor is rotatable with the drive shaft relative to the stator to generate electricity for operating a load, such as a lamp unit.

Abstract: A supercharging apparatus for an engine comprising a high-pressure stage supercharger having a high-pressure stage turbine arranged in an exhaust gas passage of the engine and a high-pressure stage compressor that is arranged in an intake gas passage of the engine and is driven by the high-pressure stage turbine, and a low-pressure stage supercharger having a low-pressure stage turbine arranged in the exhaust gas passage on the downstream side of the high-pressure stage turbine and a low-pressure stage compressor that is arranged in the intake air passage on the upstream side of the high-pressure stage compressor and is driven by the low-pressure stage turbine, wherein the low-pressure stage compressor has a capacity larger than a capacity of the high-pressure stage compressor, and the low-pressure stage turbine has a capacity equal to, or smaller than, a capacity of the high-pressure stage turbine.

Abstract: A power generating system comprises a combustion arrangement in which combustion of fuel, and in particular sustainable or renewable fluid, is used to indirectly heat fluid, such as air to drive a turbine to generate power. The arrangement includes a combustion chamber at or near the top of which is a heat exchanger.

Abstract: The invention relates to a method for converting the energy into mechanical work, whereby a first (4) and a second means (9) for storing thermal energy are alternately connected into a turbine branch (T). In order to increase the efficiency of this method, the invention provides that a compressed oxidizing gas (11) is cooled to a second temperature T2 before passing through the first means (4) for storing thermal energy, and the oxidizing gas is then increased, in one step, to a third temperature T3 when passing through the first means (4) for storing thermal energy.

Abstract: A rotary drive mechanism for use as a motor, a pump or a compressor includes a housing (13) having a chamber (1) therein defined by a peripheral wall. A rotor (3) is rotatably mounted in the chamber (1) and has two longitudinal seal edges (5) that contact the profiled wall. The rotor (3) is mounted for rotation about a rotation axis (9) and for sliding movement relative to the rotation axis in a direction perpendicular thereto. The rotation axis (9) is offset form the centre of the chamber.

Abstract: A machine designed as a centrifugal compressor is applied as an organic rankine cycle turbine by operating the machine in reverse. In order to accommodate the higher pressures when operating as a turbine, a suitable refrigerant is chosen such that the pressures and temperatures are maintained within established limits. Such an adaptation of existing, relatively inexpensive equipment to an application that may be otherwise uneconomical, allows for the convenient and economical use of energy that would be otherwise lost by waste heat to the atmosphere.

Abstract: The impeller is preferably modified to use back swept, radial or forward swept blades to accommodate relatively low, medium and high lift, respectively applications for both centrifugal compressor and turbine rotor use.

Abstract: The invention relates to a method and a device for operating a steam turbine (10) comprising several no-load or light-load phases (11, 12). All phases (11, 12) are supplied with steam in order to ensure good preheating. According to the invention, the supply of a phase (11) is selected in such a way that said phase (11) produces the least possible output, in particular no output. The enthalpy differential (&Dgr;h) between the entrance (25) to and exit (26) from the phase (11) is thus preferably reduced to zero.

Abstract: A machine designed as a centrifugal compressor is applied as an organic rankine cycle turbine by operating the machine in reverse. In order to accommodate the higher pressures when operating as a turbine, a suitable refrigerant is chosen such that the pressures and temperatures are maintained within established limits. Such an adaptation of existing, relatively inexpensive equipment to an application that may be otherwise uneconomical, allows for the convenient and economical use of energy that would be otherwise lost by waste heat to the atmosphere.

Abstract: A machine designed as a centrifugal compressor is applied as an organic rankine cycle turbine by operating the machine in reverse. In order to accommodate the higher pressures when operating as a turbine, a suitable refrigerant is chosen such that the pressures and temperatures are maintained within established limits. Such an adaptation of existing, relatively inexpensive equipment to an application that may be otherwise uneconomical, allows for the convenient and economical use of energy that would be otherwise lost by waste heat to the atmosphere.

Abstract: A gas turbine unit which has a fuel gas compressor system for increasing the pressure of a fuel gas before entering a fuel system of the gas turbine unit is disclosed. The fuel gas compressor system comprises at least one compressor, gas inlet means for supplying the fuel gas to each compressor, and supply means for supplying the compressed fuel gas to the fuel system of the gas turbine unit. The fuel gas compressor system is placed inside a housing for the gas turbine unit.

Abstract: A method of repairing a damaged combustion gas transition liner for a gas turbine engine and an improved damage-resistant transition liner that mounts adjacent to the edge of one of the engine's combustion chambers. In a particular embodiment, the gas turbine engine is a reverse flow type and the transition liner has a scalloped, circular shape with a damaged outer edge portion. The outer edge portion of the liner is removed and replaced with a new ring-shaped edge portion. The new ring-shaped edge portion has a layer of damage-resistant material that is more robust than the original liner material. The layer of damage-resistant material is located such that it will be adjacent to the edge of the combustion chamber when the gas turbine engine is reassembled. A new transition liner assembly with the damage-resistant edge also is provided.

Abstract: A gas turbine engine having an exhaust casing that includes a plurality of fairings that shield struts that are affixed to and extend between concentric rings. Each fairing has a moveable tail section that is adjusted during turbine operation to change the angle of attack of the exhaust gases to minimize vortex shedding and the corresponding vibrations that result.

Abstract: A gas turbine combustion system and method used for generating electrical power includes a compressor that receives and compresses air. A first stage turbine nozzle is flowise connected to the compressor and receives a portion of the compressed air from the compressor within a first air flow. A torus configured combustion chamber is positioned around the first stage turbine nozzle and receives a portion of the compressed air from the compressor within a second air flow that is passed through the combustion chamber where air and fuel are mixed and combusted. The air is discharged at the first stage turbine nozzle to mix with the first air while achieving a dry low NOx combustion.

Abstract: Disclosed herein is a “real time” Time Limited Dispatch (TLD) fault management system and method for evaluating the operational suitability of an engine's electronic control system. The TLD system disclosed herein uses a software algorithm to compute or predict the probability of mission success for a given upcoming mission length (e.g., two hours) and the time remaining to repair control system faults before dispatch is disallowed or the flight suspended, regardless of the probability of success.

Abstract: An organic rankine cycle system is combined with a vapor compression cycle system with the turbine generator of the organic rankine cycle generating the power necessary to operate the motor of the refrigerant compressor. The vapor compression cycle is applied with its evaporator cooling the inlet air into a gas turbine, and the organic rankine cycle is applied to receive heat from a gas turbine exhaust to heat its boiler within one embodiment, a common condenser is used for the organic rankine cycle and the vapor compression cycle, with a common refrigerant, R-245a being circulated within both systems. In another embodiment, the turbine driven generator has a common shaft connected to the compressor to thereby eliminate the need for a separate motor to drive the compressor.

Abstract: An organic rankine cycle system is combined with a vapor compression cycle system with the turbine generator of the organic rankine cycle generating the power necessary to operate the motor of the refrigerant compressor. The vapor compression cycle is applied with its evaporator cooling the inlet air into a gas turbine, and the organic rankine cycle is applied to receive heat from a gas turbine exhaust to heat its boiler within one embodiment, a common condenser is used for the organic rankine cycle and the vapor compression cycle, with a common refrigerant, R-245a being circulated within both systems. In another embodiment, the turbine driven generator has a common shaft connected to the compressor to thereby eliminate the need for a separate motor to drive the compressor.

Abstract: In a gas turbine installation, an exhaust gas chimney is formed by the transition piece of a steam generator, into which transition piece exhaust gas from the gas turbine can be introduced and can be discharged from the transition piece to a chimney orifice. The transition piece includes a component of the steam generator by which the exhaust gas can be supplied to a boiler region of the steam generator. The boiler region follows the transition piece in the direction of flow of the exhaust gas and has, arranged in it, at least one heating surface for the generation of steam.

Abstract: The invention relates to method for cooling a gas turbine according to which compressed air is extracted from a compressor connected upstream from the gas turbine for feeding said gas turbine and is used as cooling air. Cooling efficiency and yield are increased by means of cooling the compressed air through heat exchange with an air stream and feeding the gas turbine with cooled compressed air for cooling it. The invention also relates to a gas turbine installation comprising a gas turbine and a compressor connected upstream from said gas turbine, with at least one cooling air duct extending from the compressor. The primary side of a heat exchanger is connected to the air cooling duct and its secondary side is connected to a duct through which an air stream flows for supplying the heat exchanger.

Abstract: A method and a device are described for the introduction of fuel into a premixing burner, with a pilot gas feed and a premix gas feed for the operation of a gas turbine in the entire load range, in which the pilot gas feed is carried out via a burner lance provided in the premixing burner and the premix gas feed is carried out via side wall shells of the premixing burner.

Abstract: In a method for operating a premix burner a water quantity is introduced into at least one of the burner and the reaction zone of the burner depending on at least one command variable formed from at least one measured value. The method can also be used if a burner is operated dry, i.e., without water injection for nitrogen oxide injection, and the injected water quantity is less than 20% of the fuel quantity. The method can be used advantageously especially if a characteristic value derived from combustion pulsations or material temperatures is used as a command variable. The method enables measured parameters to be kept below a permissible upper limit.

Abstract: The invention relates to a turbine 1, in particular a gas turbine, which along a swivel-mounted rotationally symmetrical rotor 2 has a compressor 3, a combustion chamber 5 and a turbine section 7 formed of a plurality of turbine stages 15, in which each turbine stage 15 contains mutually interacting blades 17 and vanes 16 which a hot working fluid 13 can flow around, with a coolant provided by the compressor 3 for cooling the blades 16, 17, which can flow in a channel along the rotor 2 from the compressor 3 to the turbine section 7 and into which a liquid can be introduced for cooling. In order to specify a turbine in which less wear occurs and in which the lifetime of the components is increased, it is proposed that the channel extends outside the rotor 2 and that the liquid can be introduced at the end of the channel which faces the compressor 2.

Abstract: A heat transfer member having an external heat transfer member including an insertion hole having an adaptor ring inserted thereinto, and at least one of a base blocking protrusion and a grove blocking protrusion formed on a predetermined portion of the surface of the base confronting the inserted adaptor ring inside the insertion groove, for increasing the coupling strength of the external radiating member and the adaptor ring and the transition member.

Abstract: An air cycle air conditioning system for treating air contained within a passenger compartment of a vehicle. The system includes a compressor for receiving air from the passenger compartment and compressing the air, thereby producing charged air. Further, an expander is provided selectively coupled to the compressor for expanding the air and cooling the air communicated to the passenger compartment. The system further includes an air-to-air heat exchanger that cools the air received by the compressor-and supplies cooled charged air to the vehicle's engine.

Abstract: An adsorption heat pump is provided in which water vapor can be efficiently adsorbed and desorbed using a heat source having a lower temperature than ones heretofore in use because the pump employs an adsorbent which has a large difference in water adsorption amount in adsorption/desorption and can be regenerated (release the adsorbate) at a low temperature.

Abstract: A humidity control method is provided for a multi-stage cooling system having two or more refrigerant circuits. A hot gas re-heat circuit having a hot gas re-heat coil is connected to one of the refrigerant circuits and is placed in fluid communication with the output airflow from the evaporator of that refrigerant circuit to provide additional dehumidification to the air. Humidity control is only performed during cooling operations and ventilation operations. During a first stage cooling operation using only one refrigerant circuit and having a low cooling demand, the request for humidity control activates the hot gas re-heat circuit for dehumidification and activates a second refrigerant circuit to provide cooling capacity. During a second stage cooling operation using two or more refrigerant circuits and having a high cooling demand, the request for humidity control is suspended and is initiated only upon the completion of the second stage cooling demand.

Abstract: According to the method, heat delivered to the cabin (H) comes from a hot source (18) of a heat pump (12) comprising a main refrigerant circuit (14) taking heat from a cold source (16) to transfer it to the hot source (18). Heat taken from the cold source (16) comes from a flow of air recycled from the cabin. The cold source (16) has a refrigerant/coolant heat exchanger (24) thermally coupling the main circuit (14) to a first secondary coolant circuit (26) capable of being selectively connected to an outside heat exchanger (30) and to a cold heat exchanger (32). Air flow circuits have an inlet for admitting air recycled from the cabin, an outlet for delivering air to the outside of the vehicle, first connection means for connecting the recycled air inlet to the upstream end of the cold heat exchanger (32), and second connection means for connecting the downstream end of said cold heat exchanger (32) to the outside outlet.

Abstract: A vehicle air-conditioning system of a dual air conditioner type includes a front seat air-conditioning unit for air-conditioning a front seat side and a rear seat air-conditioning unit for air-conditioning a rear seat side. The system includes parallel connected evaporators for the front seat air-conditioning unit and the rear seat air-conditioning unit. At a low flow rate of refrigerant, the system prevents a significant increase in the temperature of air blown into the rear seat area relative to the temperature in the front seat area. The system employs a variable capacity compressor that enables its discharge capacity to be controlled by an external control signal, allowing the discharge capacity of the compressor to be controlled in accordance with the higher evaporator temperature of the temperatures at the front seat evaporator and the rear seat evaporator and a target evaporator temperature.

Abstract: A vehicle air conditioner has an IR sensor that detects a temperature of air inside a vehicle compartment. The IR sensor is disposed on an instrument panel so that the sensor is disposed above switches and a face blowout port on the instrument panel. Accordingly, a detecting range of the IR sensor is prevented from interfering by hands of a driver or an occupant even when the switches are operated by the driver. Thus, the air conditioner is capable of stable air conditioning.

Abstract: In a vehicle air conditioner, air having passed through a heat exchanger of an air conditioner unit is introduced to a plurality of wall outlet portions formed on walls of a compartment and blown off into the compartment. The air conditioner unit includes a plurality of temperature control means for independently controlling at least one of volume and temperature of the air flowing into the compartment through the respective wall outlet portions.

Abstract: In a ceiling air-blowing device for a vehicle air conditioner, a ceiling wall is disposed along a vehicle ceiling portion to define an air passage so that air from an air conditioner unit is introduced into the air passage through a pillar duct. The ceiling wall is formed with a plurality of holes having openings on a lower surface of the ceiling wall, so that the air in the air passage is blown off into the passenger compartment through the holes. Further, the holes are formed such that a total area of the openings of the holes per unit area at a position that is proximate to the end of the duct is smaller than that at a second position that is farther from the end of the duct than the first position. Therefore, the air is uniformly blown into the passenger compartment over a wide range of the ceiling.

Abstract: A spray cooling system for efficiently thermally managing a single or multiple semiconductor chip package. The spray cooling system includes a heat exchanger unit having a pump unit and a reservoir, a coaxial tube fluidly connected to the heat exchanger unit, a coupler unit attached to the coaxial tube, and a spray module where the coupler unit is removably connected to the spray module. The heat exchanger unit has an air tolerant design that allows for the entry and release of air without interfering with the operation thereof.

Abstract: In a cooling system for cooling racks in a data center, cooling fluid is circulated in the data center by a cooling device having a fan. In addition, this system includes a plenum having a plurality of returns and an outlet. The outlet of the plenum is in fluid communication with the fan and the plurality of returns are configured for removing the cooling fluid from the data center. Furthermore, the returns and are operable to vary a characteristic of the removal of the cooling fluid.

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.

Abstract: In a Stirling refrigerator, waste heat rejected from the heat rejecter of a Stirling refrigerating device is transferred by way of dew prevention heat pipes to heat the open side of the refrigerator. This makes it possible to prevent condensation of moisture on the open side of the refrigerator, where dew tends to collect as a door is opened or closed or in other situations, in an effective and energy-saving manner without using a heater, and thereby alleviate the load on the heat-rejecting heat exchanger.

Abstract: In an apparatus for fixing a printed circuit board of a refrigerator, since a printed circuit board is slid to be coupled with or separated from the inside of a support plate fixed at a lower portion of a refrigerator main body, the printed circuit board can be readily and conveniently replaced.

Abstract: This temperature regulation apparatus comprises a heat pump (12) comprising a main compression circuit (14) for a refrigerant fluid taking heat from a cold source (16) and transferring it to a hot source (18). The cold source (16) comprises a first heat exchanger (24) for exchanging heat between the refrigerant fluid and a liquid coolant thermally coupling the main refrigerant circuit (14) to a first secondary coolant circuit (26). The first secondary circuit (26) has selective connection means (40, 52, 54) for selectively connecting it to the upstream and downstream ends (48A, 48B) of a “heater” branch (48) of a cooling liquid circuit (46) of an exothermal part of the vehicle. The exothermal part is preferably a heat engine of the vehicle. The invention is applicable to air conditioning a motor vehicle cabin.

Abstract: A humidity control method is provided for a multi-stage cooling system having two or more refrigerant circuits that balances humidity control and cooling demand. Each refrigerant circuit includes a compressor, a condenser and an evaporator. A hot gas reheat circuit having a hot gas reheat coil is connected to one of the refrigerant circuits and is placed in fluid communication with the output airflow from the evaporator of that refrigerant circuit to provide additional dehumidification to the air when humidity control is requested. The hot gas reheat circuit bypasses the condenser of the refrigerant circuit during humidity control. Humidity control is only performed during cooling operations and ventilation operations. During a first stage cooling operation using only one refrigerant circuit and having a low cooling demand, the request for humidity control activates the hot gas reheat circuit for dehumidification and activates a second refrigerant circuit to provide cooling capacity.

Abstract: An air conditioning system for an aircraft in which cabin air is recirculated and mixed with cold air from an air conditioning machine which includes at least one expansion turbine over which warm pressurised air is expanded and cooled, and wherein the system includes a heat exchanger in which a heat load from hot cabin air is exchanged with the warm pressurised air prior to the pressurised air being expanded by the expansion turbine, further including a condenser heat exchanger in which recirculating cabin air is used to cool and promote water removal from the warm pressurised air before it is expanded by the expansion turbine.

Abstract: An adsorption refrigeration system and method are provided, the system comprising an adsorption pump which, in use, is arranged in communication with a chamber containing liquid and gaseous coolant. The associated method comprises expanding the gaseous coolant into an auxiliary volume member so as to cause the removal of part of the gaseous coolant from the chamber. This causes a reduction in the temperature and pressure of the gaseous coolant in the chamber. The adsorption pump is then operated so as to further cool the chamber by causing the evaporation of the coolant liquid within the chamber.

Abstract: Refrigeration-cycle equipment using carbon dioxide (CO2) as the refrigerant can prevent problems such as the sharp elevation of high pressure on startup or the like, and the unsuccessful startup of the compressor due to the operation of the high-pressure protecting mechanism, by constituting the refrigeration-cycle equipment wherein an oil separator is installed as a refrigerant vessel in a part of the high-pressure-side circuit; a linear compressor of an oil-less type or an oil-poor type is used; or the quantity of the CO2 refrigerant filled in the circuit is 0.25 kg or less per liter on the basis of the total internal volume of the circuit.

Abstract: An ejector includes a nozzle and a needle valve formed in a tapered shape. The needle valve controls a throttle opening degree of the nozzle from a minimum degree to a maximum degree while an end section of the needle valve is positioned on a downstream side with respect to a throat section of the nozzle. Besides, a cross-sectional area of a nozzle diffuser is formed to be substantially constant, downstream of the throat section. Thus, a cross-sectional area of a substantial refrigerant passage defined by an inner surface of the nozzle and the needle valve is gradually widened in accordance with the tapered shape of the needle valve. Therefore, pressure loss accompanied with a rapid expanding can be suppressed. As a result, the throttle opening degree of the nozzle can be controlled while improving nozzle efficiency and ejector efficiency.

Abstract: The present invention provides an indoor unit in air conditioner, including two heat exchangers, a connection pipe connecting the heat exchangers, first means for guiding refrigerant flow, and second means provided to the connection pipe. The two heat exchangers, i.e., first and second heat exchangers, have one ends connected to first and second pipelines connected to parts outside of the indoor unit, for an example, a compressor or an outdoor expansion device. The first means selectively guides the refrigerant introduced thereto through the first or second pipeline to be discharged through the second or the first pipeline after being passed through both, or either of the first and second heat exchangers. The second means is provided to the connection pipe so that the refrigerant transferred from one of the first and second heat exchanger to the other one of the first and second heat exchanger is passed in an original state or in an expanded state.