49th week of 2020 patent applcation highlights part 33 |
Patent application number | Title | Published |
20200378292 | EXHAUST GAS MIXING APPARATUS, EXHAUST GAS PURIFIER AND EXHAUST GAS PURIFICATION METHOD - A exhaust gas mixing apparatus includes an outer cylinder being configured to an insulating ceramic; fins being configured to an insulating ceramic, the fins being provided on an inner side of the outer cylinder; and an electric heating portion embedded in at least a part of the outer cylinder and/or the fins. | 2020-12-03 |
20200378293 | IMPROVED DIESEL PARTICULATE FILTER LINEARITY WITH THIN ASH LAYER - A particulate filter for use in an exhaust aftertreatment system includes a ceramic substrate and an ash layer deposited atop the ceramic substrate. The ash layer has a uniform ash density of at least 0.4 g/L of the ceramic substrate. A method of depositing ash layers in a particulate filter of an exhaust aftertreatment system includes providing a ceramic substrate, preconditioning the ceramic substrate, depositing at least one ash layer atop the ceramic substrate during the preconditioning, monitoring uptake of soot into the particulate filter by measuring an increase in pressure drop across the particulate filter. | 2020-12-03 |
20200378294 | NOISE ATTENUATING EXHAUST TAIL PIPE - Methods and systems are provided for an exhaust system of a vehicle. In one example, the exhaust system includes an exhaust tail pipe with an asymmetric outlet. The asymmetric outlet of the tail pipe may flare outwards, away from a central axis of the tail pipe, circumferentially surrounded by a housing with a geometry matching a geometry of the asymmetric outlet. | 2020-12-03 |
20200378295 | COMPOSITE STRUCTURE, VEHICLE AND METHOD OF MANUFACTURING A COMPOSITE STRUCTURE - A composite structure comprises a cover plate and a plate-like fiber layer, one side of the plate-like fiber layer being fastened to one side of the cover plate with a solder at contact points of fibers of the plate-like fiber layer and the cover plate. Contacting fibers of the plate-like fiber layer are connected to each other with the solder in the plate-like fiber layer. A vehicle having a composite structure and a method of manufacturing a composite structure are furthermore disclosed. | 2020-12-03 |
20200378296 | EXHAUST DEVICE AND STRADDLE-TYPE VEHICLE - An exhaust device in which a muffler is disposed on a side of a straddle-type vehicle includes the muffler including a tail pipe configured to discharge exhaust gas and protruding rearward, a tail cover covering a periphery of the tail pipe behind the muffler, and a protector for heat shield interposed between the muffler and the tail cover. Inner sides of the tail cover and the protector in a vehicle width direction are configured to be fixed to each other by a fastening member. An elastic locking portion is formed on an outer side of one of the tail cover and the protector in the vehicle width direction, and a holding portion configured to hold the elastic locking portion is formed on an outer side of another of the tail cover and the protector in the vehicle width direction. | 2020-12-03 |
20200378297 | METHODS AND SYSTEMS FOR A COMPREX CHARGER - Methods and systems are provided for a comprex charger. In one example, a comprex charger is integrally arranged with an electric machine and shares a cooling arrangement therewith. | 2020-12-03 |
20200378298 | METHODS AND SYSTEMS FOR A COMPREX CHARGER - Methods and systems are provided for a comprex charger. In one example, a comprex charger is integrally arranged with an electric machine and shares a cooling arrangement therewith. | 2020-12-03 |
20200378299 | Rotating Internal Combustion Engine - An engine design of a rotating pistonless, non-reciprocating internal combustion engine having an engine block having a drive chamber formed in an interior combustion surface having a drive surface and a sloped transitionary portion, and a rotor rotatably supported within the engine block. The rotor having a radially extending disc portion having a plurality of rotor combustion chambers. Each of the rotor combustion chambers has a pyramidal-shaped volume having a driven surface and a sloped transitionary portion, wherein combustion pressure in the rotor combustion chamber and drive chamber is exerted upon the drive surface of the drive chamber and the driven surface of the rotor combustion chamber resulting in driven rotation of the rotor. | 2020-12-03 |
20200378300 | Rotary Roller Motor (RRM) - The Rotary Roller Motor (RRM) is a four cycle rotary internal combustion engine that uniquely overcomes many of the drawbacks of other rotary type engines, by having the Rotor ‘roll’ around the inside of the engine block, rather than scraping it. This is accomplished with a two part rotor. The inner part of the rotor is composed of a Rotor Shaft (RS- | 2020-12-03 |
20200378301 | TRANSMISSION DEVICE OF AN ENGINE, PARTICULARLY FOR AN ENGINE WITH VARIABLE COMPRESSION RATE AND/OR VARIABLE DISPLACEMENT - transmission device, particularly for an engine with variable compression rate and/or variable displacement, includes, in a cylinder housing: a combustion piston capable of moving in a combustion cylinder of the engine and secured to a transmission member; a gear engaging with a first rack of the transmission member and providing transmission of the movement between the combustion piston and a crankshaft of the engine; a connecting rod engaging, at a first end, with the gear and, at a second end, with the crankshaft; and a control member engaging with the gear and secured to a control piston. The combustion piston and the transmission member are slidably linked with the cylinder housing in a main direction. | 2020-12-03 |
20200378302 | Advanced 2-spool turboprop engine - A low cost, high power density, low emissions general aviation turbine engine (GATE) with improved fuel economy over current engines. Ideally suited for 50 to 500 shaft horsepower (SHP) range aircraft applications such as GA, UAS, UAS, air taxi, helicopters and commercial markets. The engine design features with centrifugal compressor and radial turbine rotors has a high-end practical limit of ˜800 (SHP). The new turboprop incorporates 2 non-concentric spools aero-thermal-pressure coupled wherein staged compressor rotors lend to a simple engine design, optimized high overall engine pressure ratio (OPR) and low specific fuel consumption (SFC). An integral starter-generator system further simplifies the engine design and offers high electrical output power capability for auxiliary power requirements. A 2-stage low emissions combustor with fuel-air premix chambers is incorporated lending to stable combustion at any engine spool speed/power requirement, further fuel optimization and use of a low cost simple fixed pitch propeller. Some other highlights include: any fuel or mixture thereof, TBO greater than piston or other turbine engines, less maintenance costs, oil/filter change at ˜15000 hrs. and other inherent advantages of a gas turbine engine. | 2020-12-03 |
20200378303 | DIFFUSER PIPE EXIT FLARE - A diffuser pipe has a tubular body defining a pipe center axis extending therethrough. The tubular body includes a first portion extending in a generally radial direction from an inlet of the tubular body, a second portion extending in a generally axial direction and terminating at a pipe outlet, and a bend portion fluidly linking the first portion and the second portion. The tubular body has a length defined between the inlet and the pipe outlet. The tubular body has cross-sectional profiles defined in a plane normal to the pipe center axis. An area of the cross-sectional profile at the pipe outlet is at least 20% greater than an area of the cross-sectional profile at a point upstream from the pipe outlet a distance corresponding to 10% of the length of the tubular body. | 2020-12-03 |
20200378304 | ACOUSTIC PANEL FOR A TURBOMACHINE AND METHOD FOR THE PRODUCTION THEREOF - An acoustic panel for a turbomachine, in particular for an aircraft, includes two skins that are substantially parallel and between which extend cavities forming Helmholtz resonators, one of the skins being perforated by orifices opening into the cavities and forming necks of the Helmholtz resonators, vibrating masses being provided in at least some of the cavities and connected to cavity walls by an elastic junction housed in the cavity. | 2020-12-03 |
20200378305 | PLUG RESISTANT EFFUSION HOLES FOR GAS TURBINE ENGINE - An effusion cooling hole for a component associated with a gas turbine engine extends along a longitudinal axis. The effusion cooling hole includes an inlet section spaced apart from a first surface of the component. The inlet section includes a face orientated transverse to the first surface and defines an inlet through the face that has a first diameter. The effusion cooling hole includes an outlet at a second surface of the component and downstream from the inlet section. The effusion cooling hole includes a diverging section downstream from the inlet section and upstream from the outlet. The diverging section is defined substantially external to a thickness of the component, and the effusion cooling hole transitions from the first diameter to a second diameter at the diverging section. The effusion cooling hole includes an intermediate section that fluidly connects the diverging section to the outlet. | 2020-12-03 |
20200378306 | CMC BOAS COOLING AIR FLOW GUIDE - A blade outer air seal assembly includes a support structure arranged about an axis. At least one blade outer air seal segment is mounted in the support structure. A flow guide is arranged between the support structure and the at least one blade outer air seal segment defining a passage between the flow guide and the blade outer air seal segment. The passage extends in a generally axial direction. | 2020-12-03 |
20200378307 | THERMAL MANAGEMENT OF A SHAFT - A gas turbine engine includes a fan, a compressor section, a combustor, and a turbine section where the turbine section is downstream of the combustor section. A shaft connects the turbine section to the compressor section. A bore tube is disposed within the shaft downstream of the compressor section. The bore tube includes an inlet connected to an air source for passing cooling air in an upstream direction of the shaft. | 2020-12-03 |
20200378308 | ISOLATION SEALS FOR GAS TURBINE ENGINES - Isolation seals for gas turbine engines are described. The isolation seals include a first interface member configured to be fixedly attached to a first case structure, the first interface member being a full-hoop structure, a housing configured to be mounted to a second case structure, a connector pin arranged within the housing and moveable relative to the housing, and a second interface member located on an end of the connector pin, the second interface member being a full-hoop structure. The first interface member and the second interface member are engageable to form a seal therebetween. | 2020-12-03 |
20200378309 | DISENGAGEABLE SPEED-REDUCING UNIT - A speed-reducing unit, particularly for transferring torque between a gas turbine and a fan in a turbine engine, includes an annular ring, at least one gear that is coupled to the ring, the ring including two annular half-rings that are offset relative to each other along the main axis of the speed-reducing unit and that are coupled with at least one gear, and a plate for supporting the two half-rings, in relation to which the two half-rings are rotationally fixed about the main axis of the speed-reducing unit. Each half-ring includes an internal helical tooth. Each half-ring is connected to the support plate so as to be able to be uncoupled from at least one gear when at least one gear exerts a disengaging action on each half-ring, with the amplitude of the action being greater than a determined amplitude value. | 2020-12-03 |
20200378310 | HIGH AND LOW SPOOL DIFFERENTIAL GEAR ASSEMBLY - An example embodiment of a turbine engine assembly includes a low spool including a low spool accessory drive gear driven by a low rotor shaft, a high spool including a high spool accessory drive gear driven by a high rotor shaft concentric around a portion of the low rotor shaft, and a differential gear assembly adapted to offtake power from rotation of one or both of the low spool and the high spool to drive one or more accessory loads. The differential gear assembly includes a differential bullgear and one or more idler gears each including a plurality of teeth meshed with the low spool accessory drive gear and the high spool accessory drive gear, and a bearing surface. The differential bull gear includes a plurality of teeth and a corresponding at least one bearing surface engaging with the bearing surface of each of the one or more idler gears. The plurality of teeth are adapted to mesh with an accessory drive system to transfer the power offtake and drive the one or more accessory loads. | 2020-12-03 |
20200378311 | ASSEMBLY FOR RETAINING A GEAR TRAIN IN A TURBOMACHINE - The invention relates to an assembly for holding ( | 2020-12-03 |
20200378312 | GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE - An example gas turbine engine includes a propulsor assembly including at least a fan module and a fan drive turbine module; a gas generator assembly including at least a compressor section, a combustor in fluid communication with the compressor section, and a turbine in fluid communication with the combustor; and a geared architecture driven by the fan drive turbine module for rotating a fan of the fan module. A weight of the fan module and the fan drive turbine module is less than about 40% of a total weight of a gas turbine engine. | 2020-12-03 |
20200378313 | FLOW DEFLECTOR FOR A DISCHARGE VALVE SYSTEM, DISCHARGE VALVE SYSTEM AND TURBOMACHINE COMPRISING SUCH A DISCHARGE VALVE SYSTEM - The disclosure relates to a flow deflector for a discharge valve system of a double flow turbomachine compressor. The flow deflector comprises a wall provided with a plurality of ejection channels positioned to discharge a discharge air flow. The ejection channels are arranged in rows along aligned directions, substantially parallel to an axial plane of the deflector. The ejection channels of each row are oriented at a defined angle between a normal line to the wall and axes of the ejection channels, and decreasing between an upstream edge and a downstream edge of the wall, as defined according to the direction of movement of the air flow. | 2020-12-03 |
20200378314 | AIR SYSTEM OF MULTI-ENGINE AIRCRAFT - A method of operating an engine of an aircraft, the engine having a bleed air system. The method includes in flight, directing pressurized air from a source of pressurized air external to the engine to the bleed air system of the engine. An aircraft, comprising a first engine having a bleed air system, a second engine having a bleed air system, and a source of pressurized air that is external to the first and/or the second engine, the source of pressurized air being selectively fluidly connectable to the bleed air system of the first and/or the second engine, is also disclosed. | 2020-12-03 |
20200378315 | FUEL SYSTEM WITH INTEGRATED THRUST CONTROL MALFUNCTION PROTECTION AND METHOD - A fuel system with integrated thrust control malfunction and overspeed protection includes a centrifugal pump for receiving filtered fuel and supplying fuel to a metering and pressure regulating valve, the metering and pressure regulating valve for metering discharge of filtered fuel flow to a gas turbine engine burner, a shut off valve downstream of the metering and pressure regulating valve movable from an open position to either a fully closed position configured for providing rapid shutoff or a partially closed position configured for reduction of fuel flow to the gas turbine engine burner, and a first solenoid and a second solenoid for controlling the shut off valve position. | 2020-12-03 |
20200378316 | CONTROL LOGIC FOR GAS TURBINE ENGINE FUEL ECONOMY - A method of operating a multi-engine aircraft includes operating a first engine of the aircraft to provide motive power; and operating a second engine of the aircraft in a standby mode to provide substantially no motive power, a rotor of the second engine having an idle rotational speed in the standby mode, and in the standby mode, sequentially executing cycles, a given cycle of the cycles including: opening a set of variable guide vanes upstream a compressor section of the second engine, spiking a rate of a fuel flow to a combustor of the second engine, the spiking and the opening timed to increase a rotational speed of the rotor of the second engine to an upper threshold above the idle rotational speed of the rotor, and in response to the rotational speed reaching the upper threshold, at least substantially closing the set of variable guide vanes. | 2020-12-03 |
20200378317 | AIR SYSTEM OF MULTI-ENGINE AIRCRAFT - A multi-engine aircraft includes first and second gas turbine engines for providing motive power to the aircraft, each of the first and second engines comprising an air system, an air pressure line extending between and fluidly connecting the air systems of the first and second engines, and a pressure wave damper communicating with the air pressure line extending between the first and second engines. | 2020-12-03 |
20200378318 | INTERNAL COMBUSTION ENGINE AND METHOD OF OPERATING SAME - An internal combustion engine has a crankshaft with at least one throw being formed as a complete disc over at least a portion of its thickness. Permanent magnets are attached to the disc of the at least one throw in an annular array. Electromagnets are attached to the engine block, a brace coupled to the engine block, and/or an oil pan mounted to the engine block. The brace may include one or more circular structures surrounding the discs of the throws, and may support the electromagnets. The electromagnets are positioned opposite the permanent magnets. A control system selectively provides electrical current to the electromagnets to affect the motion of the crankshaft, and may further selectively activate and deactivate at least one of the cylinders by stopping fuel flow, spark, and/or intake valve actuation. | 2020-12-03 |
20200378319 | METHOD AND SYSTEM FOR ENGINE START/STOP CONTROL - Methods and systems are provided for optimizing engine climate control performance and fuel economy in engines configured with start/stop capabilities. Climate control inhibits of start/stop actions are adjusted as a function of operator driving habits and climate control inputs and preferences. The approach enables climate performance to be improved while also allowing for frequent idle-stop operation. | 2020-12-03 |
20200378320 | A METHOD FOR CONTROLLING A TURBOCHARGER SYSTEM WITH A PRESSURIZED GAS TANK CONNECTED TO AN EXHAUST MANIFOLD OF A COMBUSTION ENGINE - A method for controlling a turbocharger system fluidly connected to an exhaust manifold of a combustion engine and an exhaust after treatment system. The turbocharger system comprises a turbocharger turbine operable by exhaust gases from the exhaust manifold, and a tank with pressurized gas, the tank being fluidly connectable to the turbocharger turbine. The method comprises the steps of: determining a NOx parameter being indicative of, or correlated to, NOx emissions from the exhaust after treatment system; and injecting pressurized gas from the tank to drive the turbocharger turbine based on the determined NOx parameter, wherein a determined NOx parameter above a pre-defined first threshold determines that pressurized gas from the tank is injected. | 2020-12-03 |
20200378321 | CONTROL METHOD AND CONTROL DEVICE FOR VEHICULAR INTERNAL COMBUSTION ENGINE - A vehicular internal combustion engine system includes an internal combustion engine and an electric intake air supply device. The internal combustion engine is shifted into a stoichiometric combustion mode, and a lean combustion mode. The electric intake air supply device is driven by an on-vehicle battery, and employed to contribute a part of intake air quantity at least under a specific operating condition when in the lean combustion mode. A control method includes: determining an electric energy of the electric intake air supply device that is required to maintain achievement of a target air fuel ratio of the lean combustion mode when in a lean combustion operation region; and causing a shift from the lean combustion mode into a stoichiometric combustion mode when the on-vehicle battery is in an insufficient state of charge with respect to the electric energy. | 2020-12-03 |
20200378322 | A SYSTEM FOR VENTILATION OF A CRANKCASE - The invention provides a system for ventilation of a crankcase ( | 2020-12-03 |
20200378323 | ACTIVE PURGE SYSTEM AND ACTIVE PURGE METHOD - An active purge system includes a canister in which a vaporized gas produced in an fuel tank is collected and a purge line that connects the canister to an intake pipe. A purge pump is mounted in the purge line, a purge valve is mounted in the purge line to be positioned between the purge pump and the intake pipe, and a cylinder is connected to the intake pipe. A valve controller changes the operation timing, operation maintenance time, and the operation degree of an intake valve and an exhaust valve disposed at the upper portion of the cylinder. A compression ratio variation device is mounted on a connecting rod and a crankshaft that are connected to a piston to change the top dead center or the bottom dead center of the piston reciprocating in the cylinder. | 2020-12-03 |
20200378324 | SYSTEMS AND METHODS FOR CYLINDER DEACTIVATION OPERATION IN RESPONSE TO ROUTE CONDITIONS - Systems, apparatus, and methods are disclosed that include a divided exhaust engine with at least one primary exhaust gas recirculation (EGR) cylinder and a plurality of non-primary EGR cylinders. The systems, apparatus and methods control the EGR fraction by deactivation of one or more of the cylinders. | 2020-12-03 |
20200378325 | CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE - A control device comprising a first exhaust temperature calculation part calculating a temperature of exhaust flowing into a PM trapping device as a first exhaust temperature, a second exhaust temperature calculation part calculating a temperature of exhaust flowing out from the PM trapping device as a second exhaust temperature, a rate of change over time calculation part calculating a rate of change over time of the first exhaust temperature and a rate of change over time of the second exhaust temperature, and a judgment part judging if the PM trapping device is in a removed state removed from the exhaust passage based on a difference between the rate of change over time of the first exhaust temperature and the rate of change over time of the second exhaust temperature. | 2020-12-03 |
20200378326 | CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE - A control device comprising a first exhaust temperature calculation part calculating a temperature of exhaust flowing into a PM trapping device as a first exhaust temperature, a second exhaust temperature calculation part calculating a temperature of exhaust flowing out from the PM trapping device as a second exhaust temperature, a rate of change over time calculation part calculating a rate of change over time of the first exhaust temperature and a rate of change over time of the second exhaust temperature, and a judgment part judging if the PM trapping device is in a removed state removed from the exhaust passage based on a difference between the rate of change over time of the first exhaust temperature and the rate of change over time of the second exhaust temperature. | 2020-12-03 |
20200378327 | CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE - A control device comprising a first exhaust temperature calculation part calculating a temperature of exhaust flowing into a PM trapping device as a first exhaust temperature, a second exhaust temperature calculation part calculating a temperature of exhaust flowing out from the PM trapping device as a second exhaust temperature, a rate of change over time calculation part calculating a rate of change over time of the first exhaust temperature and a rate of change over time of the second exhaust temperature, and a judgment part judging if the PM trapping device is in a removed state removed from the exhaust passage based on a difference between the rate of change over time of the first exhaust temperature and the rate of change over time of the second exhaust temperature. | 2020-12-03 |
20200378328 | METHOD FOR DYNAMIC GAS PARTIAL PRESSURE CORRECTION OF AN INTERNAL COMBUSTION ENGINE WITH EXTERNAL MIXTURE FORMATION - A method for dynamic gas partial pressure correction of an internal combustion engine with external mixture formation. A mixture formation is carried out in an intake manifold upstream of the cylinder of the internal combustion engine, and in which in addition to the gas partial pressure of the fresh air flowing continuously into the intake manifold, the gas partial pressure of the fuel, fed discontinuously into the intake manifold, is also taken into account. The gas partial pressure of the fuel, fed into the intake manifold, said pressure which is assumed to be stationary as a function of determined parameters, is dynamically adjusted for each of the cylinder-individual, temporally successive injections, discharged into the intake manifold, by means of a correction factor and a fresh air correction filling value. | 2020-12-03 |
20200378329 | SYSTEM FOR DETECTING ABNORMALITY IN BLOW-BY GAS FEED PATH IN INTERNAL COMBUSTION ENGINE - A learned neural network learned in weights using an engine load, an engine speed, and an intake pressure inside the engine intake passage downstream of the throttle valve ( | 2020-12-03 |
20200378330 | ABNORMALITY DETECTION SYSTEM OF EXHAUST GAS RECIRCULATION SYSTEM - A learned neural network in weights using at least the four parameters of the engine load, engine speed, intake pressure inside the intake passage downstream of the throttle valve ( | 2020-12-03 |
20200378331 | INTERNAL-COMBUSTION-ENGINE CONTROL DEVICE - Provided is an internal-combustion-engine control device that minimizes a detection error of a cylinder pressure sensor used in a control of an internal combustion engine. The internal-combustion-engine control device is an electronic control unit (ECU) | 2020-12-03 |
20200378332 | CYLINDER LINER - A cylinder liner for an internal combustion engine may have a running surface, in which by honing directed honing grooves may be introduced. The running surface may have a first region and a second region, wherein the first region may have a roughness that may be distinct from a roughness of the second region. A transition between the first region and the second region may proceed obliquely to a cylinder longitudinal axis at least in some portions. At least some of the honing grooves at the transition between the first region and the second region are uninterrupted. | 2020-12-03 |
20200378333 | SYSTEM FOR AN INTEGRATED HYBRID COMPOSITE CYLINDER HEAD AND TURBINE - Methods and systems are provided for a turbine integrally formed with a cylinder head. In one example, a system includes a cylinder head and a turbine shaped from a single, continuous piece of metal. | 2020-12-03 |
20200378334 | COMBUSTION CHAMBER STRUCTURE FOR ENGINES - A structure of a combustion chamber for an engine includes: a crown surface of a piston; a combustion chamber ceiling surface formed on a cylinder head; and an ignition plug mounted on the combustion chamber ceiling surface, and including an ignition portion disposed in such a way as to face the combustion chamber. The crown surface of the piston includes a cavity which is recessed in a cylinder axis direction in a region including a position below the ignition portion of the ignition plug in a plan view from the cylinder axis direction. A rim portion of the cavity includes a guide portion, raised in the cylinder axis direction with respect to an inner region of the rim portion, interposing the ignition portion when the piston is at a compression top dead center, and configured to guide an air-fuel mixture within the combustion chamber to the ignition portion. | 2020-12-03 |
20200378335 | COMBUSTION CHAMBER STRUCTURE FOR ENGINES - A structure of a combustion chamber for an engine includes a crown surface of a piston, a cylinder wall surface, a combustion chamber ceiling surface, and an ignition plug which includes an ignition portion. The crown surface of the piston includes: a cavity recessed in the cylinder axis direction; a parallel surface portion which is in parallel to a corresponding region on the combustion chamber ceiling surface at a position above the cylinder axis direction with a gap, when the piston is at a compression top dead center; and an inclined surface portion formed to continue to the parallel surface portion in such a way as to be directed to the ignition plug, when the piston is at a compression top dead center. The parallel surface portion and the corresponding region, in combination, constitute a squish flow generation portion generating a squish flow when the piston is lifted. | 2020-12-03 |
20200378336 | Steel Piston With Optimized Design - A steel piston ( | 2020-12-03 |
20200378337 | CYLINDER BLOCK ASSEMBLY - A cylinder block assembly has: a cylinder block having three cylinders aligned side-by-side; and four crank caps arranged side-by-side in an alignment direction of the cylinders and fastened to the cylinder block. The crank caps and the cylinder block are provided with crank bearings which rotatably support a crankshaft. The crank caps are arranged at both sides of each cylinder in the alignment direction. Intermediate crank caps positioned at intermediate positions in the plurality of the crank caps include removed parts so as to more easily deform when receiving a load from the crankshaft compared with the side crank caps. | 2020-12-03 |
20200378338 | Supercritical Stirling Cycle Heat Engine with Accumulators - The inventor claims a heat engine that follows a modification of the Stirling thermodynamic heat engine cycle. This cycle uses supercritical argon gas to take advantage of the attractive intermolecular forces of the working fluid to assist in compressing the working fluid, reducing the input compression work and the heat output during isothermal compression, as well as reducing the heat input during isothermal expansion, and increasing the overall heat engine efficiency. This cycle utilizes accumulators to ensure the working fluid is heated and cooled isochorically, and a proximate piston-cylinder filled with ideal-gas helium is used in lieu of a regenerator during the isochoric heating and cooling. All of these modifications serve to increase the overall thermodynamic efficiency of the heat engine cycle. | 2020-12-03 |
20200378339 | HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE - The invention proposes an assembly for a rear of a dual-flow turbomachine ( | 2020-12-03 |
20200378340 | TURBOFAN ENGINE COMPRISING A SERIES OF ROTARY BLADES FOR BLOCKING THE STREAM OF THE BYPASS AIR - A turbofan engine with a nacelle including a runner translationally mobile between advanced and back-off positions to open a window between a stream and an outside, a plurality of blades, each rotatable on the runner between retracted and deployed positions, and a maneuvering system displacing each blade and comprising, for each blade, a shaft rotatable on the runner and to which the blade is fixed, and a toothed segment on the shaft, and a toothed arc rotatable on the runner about a longitudinal axis, the tooth arc teeth meshing with the toothed segment teeth, a slip translationally mobile on the runner in a plane at right angles to the longitudinal axis between first and second positions, a connecting rod mounted articulated between the slip and the toothed arc, a rib integral to the fixed structure, and a guiding U integral to the slip and which straddles the rib. | 2020-12-03 |
20200378341 | PROPULSION UNIT INCLUDING LIFTING POINTS DISPOSED ON THRUST REVERSER CYLINDER SUPPORTS - A propulsion unit includes a nacelle, a turbojet engine, and a thrust reverser having gratings provided with movable thrust reversal gratings arranged around an annular duct for fresh air from the turbojet engine. The propulsion unit further includes actuators arranged around the annular duct and each actuator has a front end attached to the turbojet engine and a rear end which translates movable rear covers and gratings for opening, in the annular duct, radial passages which receive said gratings. The propulsion unit further has lifting points that are arranged around the annular duct for lifting the turbojet engine. At least one of the lifting points is formed on a beam for attaching an front end of an actuator. | 2020-12-03 |
20200378342 | HYDRAULIC THRUST REVERSER ACTUATION SYSTEM - A hydraulic thrust reverser system (TRAS) including a first return line having a first check valve therein, and a second return line having a second check valve therein, wherein the first return line and the second return line are in fluid communication with each other via a fluid restrictor located upstream of the first and second check valves, wherein the first return line extends from a piston system of the TRAS, the piston system being for moving at least one thrust reverser door, and wherein the second return line extends from a lock system of the TRAS, the lock system being for controlling locks to selectively prevent the movement of the at least one thrust reverser door. | 2020-12-03 |
20200378343 | PASSIVE CENTRIFUGAL BLEED VALVE SYSTEM FOR A GAS TURBINE ENGINE - A passive centrifugal valve for a gas turbine engine. The passive centrifugal valve includes an inner section with a flow control inlet orifice, a cantilevered valve adjacent to the flow control inlet orifice, and an outer section with a seal land geometry that operates to at least partially support the cantilevered valve in response to a first centrifugal force that deflects the cantilevered valve away from the flow control inlet orifice. | 2020-12-03 |
20200378344 | EVAPORATIVE EMISSIONS CONTROL FOR A VEHICLE - A fuel system comprising a fuel tank, a mixing volume configured to mix fuel vapor and air, the mixing volume comprising an outlet configured to be fluidly coupled to an engine, and a fuel vapor line configured to fluidly couple the fuel tank to the mixing volume. | 2020-12-03 |
20200378345 | SYSTEMS AND METHODS FOR VEHICLE FUEL SYSTEM AND EVAPORATIVE EMISSIONS SYSTEM DIAGNOSTICS - Methods and systems are provided for a fuel system of a hybrid vehicle. In one example, a system may include a fuel tank selectively fluidly coupled to a fuel vapor canister via a first conduit that includes a fuel tank isolation valve and via a second conduit that includes a tank pressure control valve and a pump. In one example, the pump is a vacuum pump. | 2020-12-03 |
20200378346 | Dual Armature Purge Valve - A purge valve for an EVAP system has a chamber including an inlet conduit for receiving fuel vapors from an EVAP canister, a first outlet conduit to the engine for the fuel vapors, and a second outlet conduit to the engine for the fuel vapors. Energizing the purge valve at a first current actuates a first armature from a closed position to an open position to open a first opening and allow fuel vapors to flow through the first outlet conduit to the engine, without actuating the second armature from a closed position. Energizing the purge valve at a second current that is greater than the first current actuates a second armature from a closed position to an open position to open the second opening and allow fuel vapors to flow through the second outlet conduit to the engine while maintaining the first armature in the fully open position. | 2020-12-03 |
20200378347 | SYSTEMS AND METHODS FOR AN EXHAUST GAS RECIRCULATION VALVE CARTRIDGE IN AN INTEGRATED EXHAUST MANIFOLD CYLINDER HEAD - Systems and methods are provided for an exhaust gas recirculation (EGR) system in a vehicle. In one example, a system may include a cylinder head including an integrated exhaust manifold (IEM), an EGR cartridge including an EGR valve positioned in the cylinder head at a central collector region of the IEM, and a water jacket formed within the cylinder head, the water jacket including at least one cooling passage that extends around a circumference of the EGR cartridge. In this way, an EGR system is provided that has a reduced volume between an exhaust valve of a cylinder to the EGR valve, reducing packaging space and complexity of the EGR system while increasing engine performance. | 2020-12-03 |
20200378348 | FUEL INJECTOR NOZZLE - Methods and systems are provided for a fuel injector for an engine. In one example, the injector may be adapted with a plurality of nozzles configured to enhance atomization of fuel. The plurality of nozzles may have geometries that increase turbulence and rotation of fuel flow therethrough. In some examples, the injector may also include a multi-stage counterbore that reduces a likelihood of coking at the injector. | 2020-12-03 |
20200378349 | DRIVE OF A PUMP - A pump includes a cylinder having a working chamber which contains a fluid. A drive system including at least two linear motors which are connected electrically and/or mechanically in parallel moves a piston in the working chamber to bound the working chamber in the cylinder and to pressurize the fluid in the working chamber. A piston rod is connected to the piston and bundles a force applied by the drive system. | 2020-12-03 |
20200378350 | FUEL INJECTION NOZZLE - The invention relates to a fuel injection nozzle for use in an internal combustion engine, having a nozzle body ( | 2020-12-03 |
20200378351 | Spring Casing and Starter Device with a Spring Casing - A spring casing of a starter device of an internal combustion engine has a base body provided with a spring receptacle. A cover plate is provided to cover at least partially the spring receptacle. A connecting device is provided that connects the cover plate and the base body to each other. The connecting device secures the cover plate against a movement relative to the base body in a direction of a center axis of the spring casing. The connecting device only has a first part that is a component of the base body and a second part that is a component of the cover plate and has no further parts. A starter device with such a spring casing is provided. | 2020-12-03 |
20200378352 | AUTO START/STOP CONTROL BASED ON COOLED SEAT SIGNAL SYSTEMS AND METHODS - Systems and methods for managing auto start of a vehicle during an auto-stop condition may include: determining an operational status of a vehicle climate control system; receiving a target air outlet temperature from the vehicle climate control system; receiving data indicating a state of a cooled seat of the vehicle; and inhibiting a start-engine command to restart an internal combustion engine of the vehicle because of a cabin cooling requirement when the data indicates that the cooled seat of the vehicle is activated. | 2020-12-03 |
20200378353 | ADAPTER ELEMENT WITH INTEGRATED WATER TURBINE GENERATOR - An adapter element for a solenoid valve assembly in an irrigation system includes an integral water turbine generator including an impeller positioned in an outlet flow path of a solenoid assembly thereof such that the impeller rotates when water flows to generate electricity. | 2020-12-03 |
20200378354 | Apparatus and Method for Generation of Electricity with Pressurized Water and Air Flow Media - A facility for generating electricity includes a hydroelectric generating apparatus including an elongate penstock in flow communication with a source of water and a hydro-turbine and a plurality of water refill pumps for supplying refill water to a plurality of horizontal pistons on a synchronized and coordinated basis to supply pressurized water to the penstock. A pressure regulator is provided for supplying pressurized air to a storage container for supplying air to the pistons and respective air exhaust/release valves release the pressurized air in the pistons to the atmosphere after use. Respective water inflow valves are provided for refilling the pistons after the air exhaust/release valves open. | 2020-12-03 |
20200378355 | ROTOR BLADE, WIND TURBINE AND METHOD FOR INSTALLING AND PRODUCING A ROTOR BLADE - A rotor blade, a wind turbine and a method for installing and producing a rotor blade. In particular, a rotor blade for a wind turbine having a longitudinal direction, a transverse direction, a thickness, and a pressure side and a suction side opposite the pressure side, comprising a front pressure-side spar cap and/or a rear pressure-side spar cap, a front suction-side spar cap and/or a rear suction-side spar cap, a load introduction device, which is arranged between at least one of the pressure-side spar caps and at least one of the suction-side spar caps, wherein the load introduction device has a load coupling device, which is arranged and designed so as to receive a lifting device passed through a lifting opening, a lifting opening is arranged on the pressure side and/or the suction side, and the lifting opening is arranged between the front pressure-side spar cap and the rear pressure-side spar cap in the transverse direction and/or between the front suction-side spar cap and the rear suction-side spar cap in the transverse direction. | 2020-12-03 |
20200378356 | A WIND TURBINE AND AN AIRBORNE WIND ENERGY SYSTEM SHARING YAW SYSTEM - A wind installation comprising a wind turbine ( | 2020-12-03 |
20200378357 | FLOATING WIND TURBINE PLATFORM CONTROLLED TO OPTIMIZE POWER PRODUCTION AND REDUCE LOADING - A method for controlling an inclination of a floating wind turbine platform to optimize power production, or to reduce loads on the turbine, tower, and platform, or both, includes receiving data associated with the inclination of the floating wind turbine platform and wind speed and direction data. An angle of difference between the turbine blade plane and the wind direction is determined, where the angle of difference has a vertical component. A platform ballast system is then caused to distribute ballast to reduce the vertical component to a target angle chosen to optimize power production, or reduce turbine, tower, and platform loads, or both. | 2020-12-03 |
20200378358 | ROTOR FOR A WIND TURBINE AND WIND TURBINE - Provided is a rotor for a wind turbine, including: a blade, a hub, a pitch bearing being configured to support the blade rotatably about a longitudinal axis of the blade and relative to the hub, and one or more metal arcs for conducting a lightning current from the blade to the hub, the one or more metal arcs including: a first arc portion electrically and mechanically connected to the blade, a second arc portion electrically and mechanically connected to the hub, and a bent portion connecting the first and second arc portions. The metal arcs being configured such that, when the blade rotates relative to the hub, the first arc portion is shifted relative to the second arc portion and a length of the first arc portion is reduced or increased at the expense of an increase or decrease of a length of the second arc portion. | 2020-12-03 |
20200378359 | CONTROLLING A WIND TURBINE USING CONTROL OUTPUTS AT CERTAIN TIME STAGES OVER A PREDICTION HORIZON - The invention provides a method for controlling a wind turbine. The method predicts behaviour of the wind turbine components for the time stages over a prediction horizon using a wind turbine model describing dynamics of the wind turbine, where the time stages include a first set of time stages from an initial time stage and a second set of time stages subsequent to the first set. The method determines control outputs, e.g. individual blade pitch, for time stages based on the predicted behaviour. The method then transmits a control signal to implement only the control outputs for each of the second set of time stages so as to control the wind turbine. Advantageously, the invention reduces both average and peak computational loads relative to standard predictive control algorithms. | 2020-12-03 |
20200378360 | METHODS AND SYSTEMS FOR GENERATING WIND TURBINE CONTROL SCHEDULES - Generating a control schedule for a wind turbine, the control schedule indicating how the turbine maximum power level varies over time. Generating the control schedule includes determining a value indicative of the current remaining fatigue lifetime of the turbine, or one or more turbine components, based on measured wind turbine site and/or operating data; applying an optimisation function that varies an initial control schedule to determine an optimised control schedule by varying the trade off between energy capture and fatigue life consumed by the turbine or the one or more turbine components until an optimised control schedule is determined. | 2020-12-03 |
20200378361 | CONTROLLING FLAP LOADING ON A WIND TURBINE BLADE BASED ON PREDICTED FLAP LOADING - Techniques for controlling loading on a wind turbine blade in the flap-wise direction. A system model has a description of flap loading on the blade and is used to predict flap loading on the blade over a prediction horizon using the system model. A dynamic flap loading limit is determined based on predicted flap loading and a measured flap loading, and a constraint is defined to limit flap loading on the blade based on the dynamic flap loading limit. The predicted flap loading is used in a cost or performance function, and the cost function is optimized subject to the constraint to determine pitch for the blade to control flap loading on the blade. Advantageously, the dynamic limit varies based on discrepancies between predicted and measured flap loading to allow for adaptive back-off from extreme loads prior to such loads building up or being exceeded. | 2020-12-03 |
20200378362 | A Wind Park - The present disclosure relates to a wind park ( | 2020-12-03 |
20200378363 | WIND DRIVEN ELECTRIC GENERATOR - A wind driven electric generator comprises: a fan element including a fan blade and a transmission shaft, the fan blade being served to receive a wind force for rotation, the transmission shaft transferring the rotary motion of the fan blade; a first generator being driven by the transmission shaft to generate electric energy; a motor receiving the electric energy generated by the first generator to rotate the transmission shaft; and a generating device including a second generator, a maximum power point tracker and an energy storage element, the second generator being driven by the transmission shaft to generate electric energy, the electric energy generated by the second generator being stored to the energy storage element under the control of the maximum power point tracker. | 2020-12-03 |
20200378364 | SUPPORT STRUCTURE FOR A WIND TURBINE - The invention relates to a support structure, in particular for a wind turbine, having at least two segments, which are joined to one another such that their longitudinal axes extend substantially collinearly to one another. At least one of the segments is a pipe section, which has at least two mutually facing abutment surfaces that are joined to one another, at least in parts. A support structure is provided that is producible in less time and is more cost-effective because the join between the abutment surfaces involves at least one welded join, the thickness of the welding join being less than the wall thickness of the pipe section, and/or the join between the abutment surfaces involves at least one retaining clip. | 2020-12-03 |
20200378365 | TRANSPORTATION SYSTEM AND METHOD FOR LOADING A WIND TURBINE TOWER SEGMENT - A transportation system ( | 2020-12-03 |
20200378366 | Estimating The Clearance Between A Tower And Foundations Of A Wind Turbine - The invention relates to a method for estimating a clearance ( | 2020-12-03 |
20200378367 | METHOD OF RETROFITTING A WIND TURBINE WITH AN ENERGY GENERATING UNIT - A method of retrofitting a wind turbine having a tower and a first energy generating unit with a second energy generation unit is disclosed. The wind turbine has been operated for a first period of time at a first tower life rate and has a first tower life expectancy design value. The method includes determining the tower life of the wind turbine tower used during the first period of time; determining the remaining tower life of the wind turbine tower; replacing the first energy generating unit with the second energy generating unit; and operating the retrofitted wind turbine at a second tower life rate less than the first tower life rate so as to extend the life expectancy value of the tower beyond the first tower life expectancy design value. | 2020-12-03 |
20200378368 | LIFT SYSTEM MOUNTABLE IN A NACELLE OF A WIND TURBINE - A lift system mountable in a nacelle of a wind turbine has a mounting interface removably securable to a generator in the nacelle of the wind turbine, and a knuckle boom rotatably and removably mounted on the mounting interface. The knuckle boom has an extendable boom arm having a translatable boom section slidably mounted on the boom arm. Modularity of the lift system permits lifting components of the lift system up to the nacelle using an existing service crane of the wind turbine, and rapidly dismounting the knuckle boom to permit closing doors of the nacelle in the event of inclement weather without dismounting all of the lift system components. | 2020-12-03 |
20200378369 | ARTIFICIAL MUSCLE TENTACLES - An artificial muscle tentacle and method for manufacturing an artificial muscle tentacle, and a computer readable medium for controlling an artificial muscle tentacle are disclosed. The artificial muscle tentacle includes two spacers and a central core that connects the two spacers. The artificial muscle tentacle also includes at least two Z-Twist actuators and at least two S-Twist actuators. The Z-Twist actuators and the S-Twist actuators are disposed around the central core and in between the two spacers connecting the two spacers. The actuation of one or more of the Z-Twist actuators and the S-Twist actuators actuates the artificial muscle tentacle. | 2020-12-03 |
20200378370 | SMA-DRIVEN ROTARY ACTUATOR - A SMA-driven rotary actuator comprises as actuating elements two U-shaped SMA wires ( | 2020-12-03 |
20200378371 | PROPULSION SYSTEMS INCLUDING AN ELECTRICALLY ACTUATED VALVE - Propulsion systems, such as electrospray thrusters, may include an electrically actuated valve to permit a selective flow of propellant to a thruster. The valve may be located and arranged such that it physically separates a propellant, such as a source of ions, from a thruster of the propulsion system. In some embodiments, the application of a voltage potential to the valve may wet a plurality of through holes formed in the valve with the propellant such that the propellant flows through the valve to the thruster. After the valve has been opened, the propulsion system may be operated normally. | 2020-12-03 |
20200378372 | COMPACT PLASMA THRUSTER - According to certain aspects, an electric-propulsion thruster is used as part of a base or platform which also includes a power converter, having a plurality of inductors and other electrical components, and a printed circuit board (PCB). The PCB includes a layer at which the other electrical components and printed circuit inductor traces, for the plurality of inductors, are secured. The electric-propulsion thruster includes a housing (e.g., as part of the base or platform) providing a cavity and having at least one structurally-rigid side wall along the cavity, where the PCB is integrated with the electric-propulsion thruster for a compact arrangement which can be used to propel the apparatus. Such a compact design might be used as an important part of thruster spacecraft architecture such as micro-satellites (e.g., CubeSats). | 2020-12-03 |
20200378373 | PUMP DEVICE - A pump device includes a first piezoelectric pump, a second piezoelectric pump connected in series to the first piezoelectric pump on an upstream side of the first piezoelectric pump, a driver unit that supplies alternating-current input power to the first piezoelectric pump and the second piezoelectric pump, and a distribution setting unit that sets a distribution ratio of the input power to be supplied from the driver unit to each of the first piezoelectric pump and the second piezoelectric pump, wherein the distribution setting unit sets a ratio of the input power for the second piezoelectric pump to the input power for the first piezoelectric pump to a value greater than 1 and equal to or less than 1.57. | 2020-12-03 |
20200378374 | SUBMERSIBLE PUMP ASSEMBLY AND METHOD FOR OPERATING THE SUBMERSIBLE PUMP ASSEMBLY - A submersible pump assembly ( | 2020-12-03 |
20200378375 | MICROPUMP | 2020-12-03 |
20200378376 | HAND AIR PUMP HANDLE ASSEMBLY AND HAND AIR PUMP - Embodiments of the present invention include a hand air pump handle assembly and a hand air pump, including a pressure gauge elastically attached thereto. The hand air pump handle assembly comprises a handle shell that defines an accommodating space for placement of the pressure gauge. The accommodating space is provided with an air vent for connecting the accommodating space to an inflatable body, such as an inflatable mattress. The pressure gauge measures an internal air pressure for the inflatable body via the air vent and is connected to the handle shell with an elastic connector. The elastic connector can elastically deform to prevent the pressure gauge from being damaged or broken under external forces such as an impact. | 2020-12-03 |
20200378377 | COMPRESSOR ASSEMBLY FOR OPERATING A COMPRESSED AIR SUPPLY SYSTEM, COMPRESSED AIR SUPPLY SYSTEM, AND VEHICLE - A compressor arrangement for operating a compressed air supply installation includes a pneumatic compressor and an electric motor arranged inside a drive housing, the electric motor having an internal stator and an external outer rotor. The external outer rotor is arranged in a rotatable manner about the internal stator. The external outer rotor is supported in a rotatable manner about a center axis with respect to the drive housing via a bearing arrangement. The bearing arrangement has at least one bearing. The external outer rotor is supported by the bearing arrangement on an outer circumference of the outer rotor. | 2020-12-03 |
20200378378 | CRYOPUMP - A cryopump includes a cryopump housing and a water absorbing layer mounted on an outer side of the cryopump housing. | 2020-12-03 |
20200378379 | PERISTALTIC PUMP HAVING IMPROVED PUMPING FINGERS - A pumping finger subassembly for a peristaltic infusion pump has a housing, a pinch member, a block member, and at least one biasing spring. The housing includes a transverse slot, a first side wall, and an open second side through which the pinch member and biasing spring(s) are inserted into the transverse slot. The block member includes a foot portion and a side wall portion. The foot portion is insertable into the housing through the open second side such that the block member is constrained against movement relative to the housing and the side wall portion of the block member opposes the first side wall of the housing, whereby the pinch member is supported on both lateral sides to prevent tilting of the pinch member. | 2020-12-03 |
20200378380 | FLUID CONTROL DEVICE - A fluid control device includes a piezoelectric pump, a piezoelectric pump, a valve, and a container. The piezoelectric pump and the piezoelectric pump repeat the operation and the stop in accordance with a drive control cycle. The valve starts a control to close at the start timing of one cycle of the drive control cycle and starts a control to open at the stop of the piezoelectric pump and the piezoelectric pump. The time from the start timing of one cycle of the drive control cycle to the time at which the piezoelectric pump on the upstream side pump reaches a normal operation drive voltage is longer than the time from the start timing to the time at which the piezoelectric pump on the downstream side reaches a normal operation drive voltage. | 2020-12-03 |
20200378381 | Quick Pull Valve and Seat Assembly - A valve seat assembly comprises a valve. The assembly further comprises a removable upper seat associated with the valve. The assembly further comprises a lower seat configured to be inserted into a fluid end of a pump and releasably couplable to the upper seat. The upper seat is decouplable from the lower seat while the lower seat remains inserted in the fluid end of the pump. The valve is configured to contact the upper seat to prevent a flow of fluid through the fluid end of the pump. | 2020-12-03 |
20200378382 | VARIABLE DISPLACEMENT ROTARY VANE PUMP - A variable displacement rotary vane pump. The pump has a pump body, a rotor with vanes that rotates inside the pump body around a rotation axis, an oscillating stator arranged in an eccentric position around the rotor, a fulcrum for the rotation of the oscillating stator with respect to the pump body, and adjusting means for adjusting the displacement of the pump. The adjusting means act on the oscillating stator to move it with respect to the rotor and the pump body. The fulcrum is integrally formed with the oscillating stator and is housed in a recess formed in the pump body. The pump has a sliding element between the fulcrum and the recess. The sliding element is at least partially free to rotate within the recess. | 2020-12-03 |
20200378383 | CO-ROTATING SCROLL COMPRESSOR - A co-rotating scroll compressor includes a driving-side scroll member, a driven-side scroll member, and a housing that accommodates both of the scroll members. The housing includes partition surfaces partitioned at a plane including both of the scroll members and approximately orthogonal to rotational axes of the scroll members, and flange parts that fasten the partition surfaces in a region on a periphery of the scroll members and on a lateral side when seen from a straight line connecting the rotational axes of the scroll members to each other. | 2020-12-03 |
20200378384 | SCROLL COMPRESSOR - Provided is an efficient scroll compressor capable of suppressing deformation of a fixed scroll during operation. The scroll compressor includes: a fixed scroll ( | 2020-12-03 |
20200378385 | Screw Compressor - A screw compressor includes: a screw rotor including a rotor section and a shaft section; a casing having a shaft hole through which the shaft section is inserted, the casing housing the screw rotor; and a delivery side shaft sealing unit configured to seal a clearance between the shaft section and the shaft hole against leakage of a working fluid. The delivery side shaft sealing unit includes an annular groove provided in the shaft section, a seal ring disposed movably in an axial direction of the shaft section within the annular groove, the seal ring being capable of sliding contact with the shaft hole and a side wall surface of the annular groove, and a shaft sealing fluid supply passage communicating with the shaft hole and supplying a fluid to one side, in an axial direction, of the seal ring. The pressure of the fluid that is supplied to the one side, in the axial direction, of the seal ring via the shaft sealing fluid supply passage is set higher than pressure that acts on another side, in the axial direction, of the seal ring. Thus, high shaft sealing performance can be exerted even when the working fluid on the delivery side of the screw rotor has a pressure distribution in a circumferential direction. | 2020-12-03 |
20200378386 | ROTARY COMPRESSOR - A rotary compressor may include a rotary shaft; a plurality of plates that supports the rotary shaft; a cylinder provided between the plurality of plates to define a compression space, and provided with a vane slot; a roller slidably coupled to the rotary shaft inside of the cylinder, and having a hinge groove on an outer circumferential surface thereof; and a vane, a first end of which is slidably coupled to the vane slot of the cylinder, and a second end of which is rotatably coupled to the hinge groove of the roller. At least one of first and second axial end surfaces of the roller facing the plurality of plates is provided with a dimple portion having a predetermined depth. With this structure, contact surfaces between the roller and the plate may be prevented from being in close contact with each other, preventing the roller or the plate from being damaged or a performance of the compressor from deteriorating due to friction loss, thereby improving reliability and performance of the compressor. | 2020-12-03 |
20200378387 | MICROPUMP - A pump includes: a stator ( | 2020-12-03 |
20200378388 | CONTRA-ROTATING FAN STRUCTURE - A contra-rotating fan structure includes a first base, a first fan, a second base, and a second fan. The first fan is rotatably disposed on the first base and includes a first hub. The first hub has a first largest width. The second fan is rotatably disposed on the second base and includes a second hub. The second hub has a second largest width. The first base and the second base are located between the first fan and the second fan. The second largest width is greater than the first largest width. | 2020-12-03 |
20200378389 | ELECTRIC SUPERCHARGER - An electric supercharger includes: a compressor impeller; a motor configured to transmit a driving force to the compressor impeller via a rotational shaft; a back-surface side casing facing a back surface of the compressor impeller via a gap and surrounding the rotational shaft; a bearing disposed between the back-surface side casing and the rotational shaft so as to support the rotational shaft rotatably; and a mechanical seal positioned between the back surface of the compressor impeller and the bearing in an axial direction of the compressor impeller and configured to seal a gap between the rotational shaft and the back-surface side casing. | 2020-12-03 |
20200378390 | SMALL-SIZED ELECTRIC FAN - A small-sized electric fan using a USB power source has such a structure that the small-sized electric fan is provided with: a body case | 2020-12-03 |
20200378391 | PARAMETER CONSTANCY - A method for regulating fluidic parameters of a ventilator in a system that includes regulating at least one fluidic parameter Pi, actual to a predetermined target value Pi, target by at least one motor parameter Mi of a ventilator in a system, wherein the ventilator is operated with a motor parameter Mi regulated to a constant value, wherein first, actual values of the motor parameters Mi are acquired and actual values of fluidic parameters Pi, actual are determined, and a comparison of the actual values and the target values is carried out, wherein, in the case of a deviation of the actual-target comparison of the parameters, an adjustment of the rotational speed occurs, in order to reach the predetermined target value. | 2020-12-03 |