Abstract: A gas turbine engine composite disk includes dovetail slots between disk posts extending radially inwardly from a periphery, a hub ring of composite plies circumscribed about a centerline axis, and radial plies extending radially away from hub ring into disk posts. A segmented intermediate ring concentric with and located radially outwardly of hub ring includes intermediate ring segments having nested plies with annular bases circumscribed about centerline axis and substantially radially extending clockwise and counter-clockwise radial ply arms. An outer segmented ring may be concentric with and located radially outwardly of intermediate ring, include annular outer ring segments with circumferentially stacked composite plies disposed within intermediate ring segments between clockwise and counter-clockwise radial ply arms and radially outwardly of annular bases. An outer skin of outermost composite covering plies may extend circumferentially around composite disk.

Abstract: A runner for a tidal power plant, comprising a hub body provided with openings for receiving blades, individual rotating means for rotating each blade with respect to the hub body, around an axis that is perpendicular to a rotation axis of the runner. The rotating means include at least one linear servomotor or an electric motor capable of rotating a corresponding blade independently of the other blades, over an angle superior or equal to 180° around its axis.

Abstract: A component for a gas turbine engine according to an example of the present disclosure includes, among other things, a body having circumferential sides between a forward face and an aft face, each of the circumferential sides defining a mate face, an attachment member extending from the body, and a transition member adjacent to the body and the attachment member. The transition member and the body define a slot configured to receive a seal member. The transition member is sloped inwardly from one of the circumferential sides. A method of fabricating a gas turbine engine component is also disclosed.

Abstract: A mid-turbine frame (MTF) for a gas turbine engine includes an inner manifold directing air to a turbine rotor of the gas turbine engine. The MTF includes an outer MTF case and an inner MTF case. The inner manifold of the MTF is located in the inner case of the MTF.

Abstract: Anti-rotation knife edge seals and gas turbine engines including the same are provided. The anti-rotation knife-edge seal includes a first end portion having at least one knife edge, an opposing second end portion including an outside peripheral edge having a nut anti-rotation feature and an inside peripheral edge having a shaft anti-rotation feature, and an intermediate portion extending between the first end portion and the opposing second end portion. The first end portion, the opposing second end portion, and the intermediate portion form a one-piece annular seal member. A method is also provided for substantially preventing rotation of a stack nut against an adjacent rotatable component.

Abstract: A rotor for a turbomachine having at least a first rotor main body and a second rotor main body, the second rotor main body having a rotor arm having an arrangement for form-fittingly flange-mounting the first rotor main body to the second rotor main body, the arrangement having a balancing ring disposed on the radially outer side of the rotor arm is provided. The balancing ring is integrally connected to the rotor arm for form-fittingly flange-mounting the second rotor main body to the first rotor main body, the arrangement being disposed at the upstream and/or downstream end of the rotor arm. A compressor of a turbomachine having a rotor is also provided.

Abstract: A component which can be subjected to hot gas for a gas turbine, the component having at least one wall, which includes a first surface as far as an edge, the first surface for delimiting a hot gas flow path of the gas turbine, and which includes a second surface, which adjoins the edge and is arranged transversely to the first surface. A groove for receiving a sealing element is arranged in the second surface and extends at least partially along the edge at a distance from the edge. The groove includes a groove base lying opposite the groove opening and two mutually facing side walls which adjoin the groove base and extend along the edge. At least one of the side walls has at least one groove-shaped recess.

Abstract: Turbine and compressor casing/housing abradable component embodiments for turbine engines, have abradable surfaces with ridges projecting from the abradable surface, separated by grooves. The ridges have one or both sidewalls inclined against the opposing turbine blade tip rotational direction for redirecting and/or dissipating blade tip gap leakage airflow energy. In some embodiments the ridge tip and/or groove base have inclined profiles for redirecting airflow leakage away from the blade tip gap. In some embodiments, the inclined ridge tip profile provides a progressive wear zone that increases abradable surface area as the inclined ridge is abraded by the rotating blade tip.

Abstract: An electrical generator for an aircraft includes a gas turbine engine having an exhaust section defining an exhaust cavity through which combustion exhaust gases are emitted in a direction defining an exhaust vector, and a magnetohydrodynamic generator having a magnetic field generator forming a magnetic field having at least some magnetic field lines perpendicular to the exhaust vector, and at least one electrode pair, comprising at least one positive electrode and at least one negative electrode, arranged relative to the exhaust section wherein movement of charged particles entrained in the exhaust gas along the exhaust vector generates a DC power output at the at least one electrode pair.

Abstract: A system and method for improved system efficiency of an integrated power and control unit (IPCU) of an aircraft is disclosed. The system uses an open-loop cooling system and turbo machine power matching to provide wide operation range without over-sizing. In order to reduce the temperature of the air flow through the cooling heat exchanger, the cooling turbine need to expand further in the same time generating power but the power could be higher than the compressor could absorb so a generator that would convert the power and used in supplying the aircraft would result in more efficient system.

Abstract: The present invention provides a system for detecting abnormal axial movement of a shaft in a gas turbine engine. The system comprises a detection circuit including a detector element including a frangible link portion (32) forming part of an electrical detection circuit and a plunger integral (38) with the frangible link portion (32). The plunger (38) is arranged such that it is displaced by abnormal axial movement of the gas turbine shaft to break the frangible link portion (32) from the remainder of the detection circuit and thereby break the electrical detection circuit. The system includes two connection blocks (33, 35) each having a connection at a respective first portion for electrical connection to a signal sensing unit, and being connected at respective second portions to opposite ends of the frangible link portion such that the electrical circuit running through the detector element and a signal sensing unit is modified when the frangible link portion (32) is broken by movement of the plunger (38).

Abstract: A gas turbine engine is provided with a controller configured to detect a spool shaft failure and to initiate an engine shut-down in response to the shaft failure. The controller evaluates the compressor speed probe, the speed probe continuity, P30 pressure and compressor surge to determine whether a shaft failure has occurred.

Abstract: The present disclosure relates to a damping device for absorbing structural vibrations or high excitation frequencies between a first component and a second component of a turbomachine, particularly in connection with high temperature operating conditions. The first component may be a combustor or a burner of a gas turbine and the second component may be a fuel supply line, connected to or passed through a wall of the first component. The damping device may include at least one wire mesh element which is inserted into a housing with a radially outer surface of the wire mesh element being compressed by the housing, and a radially inner surface of the wire mesh element closely surrounding the second component, wherein the housing is fixedly connected to the wall of the first component by a weld seam. In addition.

Abstract: Mechanical drive architectures can include a gas turbine having a compressor section, a turbine section, and a combustor section. A load compressor is driven by the gas turbine. A rotor shaft extends through the gas turbine and the load compressor. The rotor shaft has rotating blades arranged in a circumferential array to define a plurality of moving blade rows in the gas turbine and the load compressor. At least one of the rotating blades in one of the gas turbine and the load compressor includes a low-density material. Bearings support the rotor shaft within the gas turbine and the load compressor, wherein at least one of the bearings is a hybrid-type low-loss bearing.

Abstract: A case for a gas turbine engine incudes a radial flange with a partial scallop along an inner diameter of the radial flange.

Abstract: A structural component construction that is suitable and provided for the purpose of being further processed into a structural component of a gas turbine is provided. It is provided that the structural component construction has been manufactured by means of metal injection molding and subsequent sintering, and that it includes a support structure as an integral part of the structural component construction which is suitable for supporting the structural component during sintering, wherein the support structure is either not contained or not contained in its entirety in the finished structural component.

Abstract: The invention relates to turning gear system for a turbine. The system comprises a pinion configured and arranged to engage a turning gear so as to turn a shaft of the turbine and further includes a higher pressure oil system having a hydraulic motor and a lower pressure oil system having a hydraulic pump coupled to the hydraulic motor so as to enable a generation of a flow rate using the high pressure oil system as a motive force. A pressure control system for controlling a pressure of the flow rate to enable engagement of the pinion during reverse turning operation is provided.

Abstract: A method for generating electricity by means of a nuclear power plant and a liquid vaporization apparatus involves, during a first period, producing heat energy by means of the nuclear power plant and using the heat energy to vaporize water or to heat water vapour, expanding the water vapour formed in a first turbine and using the first turbine to drive an electricity generator in order to produce electricity, vaporizing liquefied gas coming from a cryogenic store in order to produce pressurized gas, reheating the pressurized gas with a part of the water vapour intended for the first turbine of the nuclear power plant and expanding the pressurized fluid in a second turbine to produce electricity and, during the second period, liquefying the gas to be vaporized.

Abstract: This combined cycle gas turbine plant has a gas turbine (104) and a steam turbine (106) mounted on the same shaft. A control system is configured for switching the plant from a rated mode of operation, in which the plant is operated on gas turbine output and steam turbine output, to a reduced load mode of operation, in which the plant is operated on gas turbine output alone. The switch from the rated mode of operation to the reduced load mode of operation occurs if plant demand decreases below a predetermined threshold. The steam turbine is run under full speed no load conditions in the reduced load mode of operation, and is heated using controlled steam admission, to maintain the steam turbine in a heated ‘stand-by’ state.

Abstract: The present disclosure relates to systems and methods that provide power generation using predominantly CO2 as a working fluid. In particular, the present disclosure provides for particular configurations for startup of a power generation system whereby the combustor may be ignited before the turbine is functioning at a sufficiently high speed to drive the compressor on a common shaft to conditions whereby a recycle CO2 stream may be provided to the combustor at a sufficient flow volume and flow pressure. In some embodiments, a bypass line may be utilized to provide additional oxidant in place of the recycle CO2 stream.

Abstract: A method of controlling an intermediate phase Continuous Variable Valve Timing (CVVT) includes, in order to determine whether a CVVT operation of an engine can be performed, a voltage of a battery, a pressure of an engine oil, and a temperature of the engine oil are detected, and it is determined whether a CVVT operation can be performed on the basis of the detected voltage of the battery, the detected pressure of the engine oil, and the detected temperature of the engine oil.

Abstract: A multiple variable valve lift apparatus may include a camshaft rotating by driving of an engine, a cam portion formed in a cylindrical shape having a hollow that the camshaft is inserted into, rotating together with the camshaft, configured to move along an axial direction of the camshaft, and forming a zero cam and a normal cam, a valve opening/closing device configured to be operated by at least one of the zero cam or the normal cam which are formed at the cam portion, an operating device disposed on an exterior circumference of the camshaft so as to move together with the cam portion, and a solenoid configured to selectively move the operating device along an axial direction of the camshaft, in which a journal, which has a radius being equal to a radius of the zero cam, is formed at the cam portion.

Abstract: Methods and systems are provided for deactivating a valve actuation mechanism. In one example, a system may include a hydraulic gallery that may deliver a restricted flow of hydraulic fluid from a hydraulic flow restrictor to a pressure relief valve within a valve deactivation oil control valve, and during a second condition may deliver an unrestricted flow of hydraulic fluid from the valve deactivation oil control valve to the hydraulic flow restrictor. The hydraulic flow restrictor may comprise two vertical bores within the camshaft carrier that are fluidically coupled via a restrictive groove on the bottom surface of the camshaft carrier.

Abstract: The present disclosure provides a cylinder deactivation engine which is configured to prevent abrasion on a pad portion of a valve opening/closing unit and improves reliability of the cylinder deactivation. The cylinder deactivation engine selectively performing deactivation of a cylinder may include: a cylinder deactivation apparatus including an inner body which contacts with a cam formed at a camshaft and makes a lever motion by rotation of the camshaft; and an outer body which moves together with the inner body by selectively latching to the inner body so as to open/close a valve; and a stopper integrally formed with a cam carrier disposed to surround a part of a lower portion of the camshaft and disposed between the camshaft and the outer body so as to function as a stopper for blocking the outer body which is pushed toward the camshaft by the valve.

Abstract: A valve for a vehicle may include a housing including a first inflow hole, a second inflow hole, a first exhaust hole, and a second exhaust hole, an inner body inserted in the housing and having a fixing groove, a fixing rod fixed to the fixing groove, a movable member slidably engaged to the lower end portion of the fixing rod to upwardly or downwardly move along the fixing rod according to a temperature of the transmission oil being flowed in the inside of the housing, a relief member including a penetration hole, wherein the lower end portion of the movable member is selectively movable therein, and slidably mounted in the lower end portion of the inner body, a first elastic member interposed between the movable member and the relief member, and a second elastic member interposed between the inner body and the relief member.

Abstract: An oil separating module for an internal combustion engine, comprises an oil separator, an oil return which is arranged such that separated oil can flow through the oil return to an oil sump, a mounting and a non-return valve. The non-return valve comprises a valve housing, wherein the valve housing has a throughbore having a first end opening and a second end opening and a valve body, wherein the valve body is movably mounted in the valve housing such that the valve body transitions between an open position and a closed position. In the open position, fluids are able to pass from the first end opening to the second end opening and fluids are able to pass from the second end opening to the first end opening. In the closed position, fluids are not able to pass from the first end opening to the second end opening and fluids are not able to pass from the second end opening to the first end opening.

Abstract: A PCED can include an outer can, an upper lid having an upper lid intake and an upper lid exhaust, a lower lid having a lower lid exhaust, and an internal frame disposed within the can. With the internal frame disposed within the can, first, second, third, and fourth chambers can be formed, with the first chamber containing a coalescing material. Gases from a combustion engine crankcase can enter the PCED via the upper lid intake, move through the chambers, and exit the PCED via the upper lid exhaust and return to the crankcase. While moving through the chambers, impurities within the gas convert to liquid form via condensation, collect in the second chamber, and can be subsequently drained from the PCED via the lower lid exhaust.

Abstract: There is provided an engine capable of reducing oil consumption. The engine includes a cylinder head, a cylinder head cover mounted above the cylinder head, a rocker arm covered by the cylinder head cover, and a breather chamber provided inside the cylinder head cover. As a front-rear direction is defined by a longitudinal direction of the cylinder head cover, the breather chamber has a blow-by gas inlet at one side in the front-rear direction, a blow-by gas outlet at another side in the front-rear direction, and an oil discharging guide chamber at an intermediate part in the front-rear direction. The blow-by gas inlet is opened on a bottom wall of the breather chamber, and a peripheral wall of the oil discharging guide chamber is protruded downwardly from the bottom wall of the breather chamber toward between the rocker arm provided at a side of the blow-by gas outlet and the blow-by gas inlet.

Abstract: Sound-attenuating mufflers and muffler inserts, and systems and methods for fabricating such muffler inserts. Continuous fiberglass roving is fed to a pneumatic jet head which fluffs the roving and presents the fluffed roving to a delivery wand at the exit end of the jet head. A jet head/wand assembly is moved along a three-dimensional path such that the wand delivery tip travels along a predetermined three-dimensional path inside a mold thereby depositing the continuous, fluffed fiberglass strands in the mold along the predetermined path. A terminal end portion of a liquid resin conduit is mounted to the fiberglass-dispensing wand, as part of the delivery tip, and drip-feeds liquid resin onto the fiberglass as the fiberglass is being deposited in the mold. The undulating, up and down movement of the delivery tip produces a wave-like undulating pattern in the appearance of the rovings in the resulting molded product.

Abstract: A method for a vehicle comprises responsive to installation of a new exhaust particulate filter, doping fuel with an ash-producing additive, and combusting the doped fuel to produce ash, wherein the ash deposits as an ash coating on the new exhaust particulate filter. In this way, a filtration efficiency of an exhaust particulate filter can be increased quickly as compared to a filter with no deposited ash coating, inexpensively as compared to conventional methods using membranes, and with a lower back pressure drop as compared to conventional methods.

Abstract: A diesel particulate filter (DPF) canister for an exhaust gas aftertreatment module is disclosed. The DPF canister may include a canister housing having an inlet flange and an outlet flange attached at opposite ends, and a canister sealing flange installed there between. The outlet flange may have a greater outer diameter than the inlet flange, and the canister sealing flange may have a greater outer diameter than the inlet and outlet flanges. A DPF receptacle may include a cylindrical receptacle housing with a receptacle sealing flange attached at one end and having a receptacle sealing flange inner diameter that is greater than the outer diameter of the inlet flange, but less than the outer diameters of the outlet flange and the canister sealing flange so that the DPF canister can only be installed with the inlet flange inserted through the receptacle sealing flange.

Abstract: A gas treatment system for a vehicle contains: a gas charging unit, a gas exhausting unit, and a tail gas treating unit. The gas charging unit includes a plurality of air inlets arranged on a roof and a peripheral side of the vehicle and communicating with a body of the vehicle, the plurality of air inlets also connect with an air inlet channel for charging fresh air. The gas exhausting unit includes a gas discharge channel for discharging waste gas, and the gas discharge channel has an outlet segment arranged on an upper side thereof and extending out of a top surface of a tail end of the vehicle. The tail gas treating unit includes an electrode absorber disposed on a lower end of the outlet segment of the gas discharge channel to treat the waste gas from the gas discharge channel.

Abstract: An exhaust gas control system includes: a housing, an exhaust gas purification catalyst, and a microwave irradiator. The microwave irradiator is configured to irradiate the exhaust gas purification catalyst with a microwave such that a standing wave that has: a high magnetic field region; and a high electric field region. The exhaust gas purification catalyst includes a carrier substrate and a catalytic substance that purifies the exhaust gas. The catalytic substance is disposed on the carrier substrate. The carrier substrate includes a magnetic body region and a dielectric region. The magnetic body region of the carrier substrate is disposed in the high magnetic field region in the housing. The dielectric region of the carrier substrate is disposed in the high electric field region in the housing. The magnetic body region has a magnetic body that absorbs the microwave. The dielectric region has a dielectric that absorbs the microwave.

Abstract: Methods and systems are provided for controlling and coordinating control of a post-catalyst exhaust throttle and an EGR valve to expedite catalyst heating. By closing both valves during an engine cold start, an elevated exhaust backpressure and increased heat rejection at an EGR cooler can be synergistically used to warm each of an engine and an exhaust catalyst. The valves may also be controlled to vary an amount of exhaust flowing through an exhaust venturi so as to meet engine vacuum needs while providing a desired amount of engine EGR.

Abstract: A NOx catalyst is provided that can realize a favorable NOx reduction in a broad temperature region and that can lighten the overhead involved in production.

Abstract: The disclosure relates to a multi-chamber container made of thermoplastic plastic as a service-fluid container for a motor vehicle, which multi-chamber container comprises at least two chambers, which constitute separated volumes that are not in fluid connection with each other, at least not directly, and which are each designed to hold a different service fluid, wherein at least two surrounding walls of the chambers adjoin each other, the chambers are components of a continuous container body combination, the surrounding walls of at least two chambers that adjoin each other are connected to each other in a bonded manner by means of at least one material bridge or in a form-closed manner and/or by means of fasteners, and the connection is designed to independently release under the influence of deformation forces caused by impact such that the container body combination is divided into at least two separate container body parts or two container bodies under the influence of deformation forces caused by impact

Abstract: A method for determining the quantity of reducing agent in a tank vehicle, including: a storage material in the tank for storing and releasing the reducing agent according to demand; a heating device to supply heat to release the reducing agent, and a control device for driving the heating device. After the motor vehicle is started, driving the heating device so that it delivers constant power during an initial phase over which the pressure inside the tank increases until it reaches a predetermined value. The heating device then regulating the pressure around a datum value; then measuring the time of the initial phase or the derivative of pressure with respect to time during this initial phase; and comparing the measured time against various calibrated values of the initial phase in order to determine the quantity of reducing agent in the tank.

Abstract: An exhaust elbow includes an upstream sidewall defining an upstream portion of the exhaust elbow, a downstream sidewall defining a downstream portion of the exhaust elbow, and a deflector. The upstream portion is configured to receive an upstream exhaust gas. The deflector is coupled to the upstream sidewall of the exhaust elbow upstream and is configured to deflect a portion of the upstream exhaust gas received by the upstream portion of the exhaust elbow away from a region of an interior of the exhaust elbow into which an injected reductant from a dosing module is injected. The deflector may reduce and/or prevent formation of reductant deposits on a downstream sidewall. In some implementations, an exhaust assisted flow separator may also be included to direct a portion of the upstream exhaust gas received by the upstream portion of the exhaust elbow through a dosing opening.

Abstract: A heater for a plastic tank for storing urea. The heater includes a part and an electrical heating element. The part is fixed to the electrical heating element. The electrical heating element is surrounded by a plastic sheath. The part further includes a plastic material which is fusion bonded to the plastic sheath. The plastic material of the part is overmolded on the plastic sheath.

Abstract: An internal combustion engine comprises an upstream side air-fuel ratio sensor, a downstream side air-fuel ratio sensor, an air-fuel ratio control means, a learning means and an abnormality judging means. When the air-fuel ratio control means sets the target air-fuel ratio to a first side of a rich side or a lean side, if it is judged that the air-fuel ratio of the outflowing exhaust gas is maintained at a second side at an opposite side to the first side for a predetermined air-fuel ratio maintenance judgment time or more, the learning means corrects a parameter relating to the feedback control so that the air-fuel ratio of the inflowing exhaust gas changes to the first side. A correction amount of the parameter at the stuck learning is made small when the abnormality judging means judges that the downstream side air-fuel ratio sensor exhibits abnormal response delay.

Abstract: Methods and systems are provided for detecting NOx sensor degradation based on results from a NOx sensor self-diagnostic (SD) test. In one example, a method may comprise: determining that a nitrogen oxide (NOx) sensor is degraded if outputs received from the sensor via a CAN bus during a self-diagnostic test are outside a threshold range. Additionally, only outputs received from the sensor during a self-diagnostic (SD) test performed after a first completed SD test after a key-off event, where the outputs are generated under conditions where a temperature at the sensor is less than a threshold, and an oxygen concentration is within a threshold range may be used to determine if the sensor is degraded.

Abstract: The invention relates to a method for diagnosing a gas-permeable object, such as a catalyst (15) or a filter, that was removed from an exhaust gas tract connected downstream of an internal combustion engine, in particular removed from a motor vehicle. In order to obtain particularly precise information about a function of the catalyst (15), according to the invention, an end face of the catalyst (15) is subjected to a test medium of a defined composition, such as propane gas or carbon monoxide, through an opening (5) by means of a device (2) in order to measure a catalytic reactivity. At a position located downstream, a concentration of at least one reduced or oxidized constituent of the test medium is measured after having passed the catalyst (15) and/or a temperature of the object after being subjected to the test medium is measured.

Abstract: An engine includes an exhaust gas system which flows exhaust gasses through an aftertreatment device. A method is provided for detecting the aftertreatment device during a transient operating condition. The method includes sensing temperature of the exhaust gas at an inlet and at an outlet of exhaust aftertreatment system. The inlet temperature is filtered and an inlet temperature difference between the filtered and unfiltered inlet temperatures is calculated. If the absolute value of the inlet temperature difference is greater than the predetermined threshold, then an outlet temperature difference is calculated. If the absolute value of the outlet temperature difference is greater than the second threshold, then a fault signal is generated, indicating that an aftertreatment device is missing. The aftertreatment device includes an SCR catalyst and an ammonia oxidation catalyst.

Abstract: To provide a controller that can slow down progression of deterioration of an internal combustion engine caused by repeated occurrence of LSPI. An index value of the degree of deterioration of the internal combustion engine caused by LSPI is calculated. If the index value exceeds a first threshold, when the temperature of cooling water that cools a part of the peripheral wall of a cylinder that is close to a combustion chamber is lower than a threshold temperature, and the internal combustion engine is running in a determined operational region set in a low speed and high load region, the proportion of fuel injection by an in-cylinder injection valve is reduced to increase the proportion of fuel injection by a port injection valve compared with before the index value exceeds the first threshold, thereby suppressing occurrence of LSPI.

Abstract: A piston oil jet apparatus of an engine includes a control valve guide installed inside a cylinder block which includes a cylinder in which a piston is lifted and including an oil inlet provided at one side and oil supply holes controlling oil supply at another side. A control valve is coupled to the control valve guide and opens/closes the oil supply holes. A piston cooling jet is connected to the oil supply holes to inject a cooling oil toward the piston. An actuator moves the control valve.

Abstract: A device for convective cooling of a functional assembly for a motor vehicle includes a fan, which in operation, is designed to move air along a flow axis defined by the design and placement of the fan. A flapper valve device is provided having an air transit opening and a flapper valve assembly disposed therein, with at least one flapper valve provided to change the open-flow cross section of the air transit opening and being adjustable between a closed position and an open position. A control unit is provided. The fan and the flapper valve device are arranged at a distance from each other such that air moved due to operation of the fan then flows through the air transit opening at least when the flapper valve device is in the open position. The control unit is designed to detect at least one operating parameter of the fan.

Abstract: A first valve portion and a second valve portion are formed in a rotary valve, wherein the first and the second valve portions are arranged in an axial direction thereof. The first valve portion includes a first and a second valve windows formed in a valve member, and a first and a second valve port openings formed in a valve housing. The second valve portion includes a third valve window formed in the valve member and a third valve port opening formed in the valve housing. The valve member is rotatable in both directions of a clockwise direction and an anti-clockwise direction, so that each of the first to the third valve port openings is respectively opened or closed by the first to third valve windows. Each of the valve windows and the valve port openings of the first valve portion is formed in a rectangular shape in its developed figure in a rotational direction of the valve member.

Abstract: A control method for engine thermal management that provides an electronic fan clutch and an electronic water pump in cooperation with an operation of an electronic thermostat, thereby achieving efficient engine thermal management and reducing a loss of load. The control method includes the steps of obtaining an engine coolant temperature and engine driving information and calculating a required fan rotational speed based on the obtained current coolant temperature information and the obtained engine driving information. The method calculates a control value for controlling a rotational speed of a cooling fan and checks a current operating state of the electronic thermostat. The method determines whether to operate the electronic water pump and control the cooling fan rotational speed based on the checked current operating state of the electronic thermostat, and controls the electronic water pump and the electronic fan clutch of the cooling fan based on the determination result.

Abstract: A heat exchange apparatus of a vehicle includes a coolant circuit, to which a water pump, an EGR cooler in which exhaust gas flowing through an EGR passage and a coolant exchange heat, an oil cooler in which engine oil and the coolant exchange heat, and an ATF warmer in which an automatic transmission fluid as a hydraulic fluid of an automatic transmission and the coolant exchange heat are connected, between a water jacket exit and a water jacket entry of an internal combustion engine. In the coolant circuit, the oil cooler and the ATF warmer are connected to a downstream side of the EGR cooler.

Abstract: An integrated air shroud assembly is provided for a motor vehicle. That air shroud assembly includes a body having a radiator opening, a charge air cooler opening and a cooling fan opening. The charge air cooler opening is offset from the radiator opening and the radiator opening and the charge air cooler opening are in parallel communication with the cooling fan opening.