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10th week of 2022 patent applcation highlights part 33
Patent application numberTitlePublished
20220074283A SOCK FOR A FLOATING VESSEL - A sock for a floating platform including a plurality of tubulars coupled together and defining a bore and a catcher assembly. The catcher assembly including a plurality of orifices formed in at least one of the plurality of tubulars, a catcher releasably coupled to the plurality of tubulars by a plurality of shearable members, wherein the catcher is disposed in the bore, and wherein the catcher is movable from a first position to a second position, and a stop flange having at least one aperture.2022-03-10
20220074284METHOD OF DRILLING STRING ASSEMBLY FOR SECONDARY OPENING OF A PRODUCTIVE FORMATION - A method of a drilling string assembly for drilling small-diameter branched channels, including installation of operating elements arranged in a dynamically perturbed section of a loaded part of the drilling string. Moreover, a drilling string assembly, comprising oscillators arranged as coupled oscillators, a bit, a spindle section of a bottom-hole motor, power sections of a screw bottom-hole motor, assemblies of rigid and flexible pipes, as well as a device for regulating the axial load, are installed on a test bench. Bench tests are carried out according to modelled programs of possible emergency or non-emergency operating modes of the assembly, both as a whole and of the separate elements.2022-03-10
20220074285COALIFICATION AND CARBON SEQUESTRATION USING DEEP OCEAN HYDROTHERMAL BOREHOLE VENTS - Systems and methods are described for sequestering carbon stored in organic matter while minimizing the release of carbon dioxide (CO2022-03-10
20220074286Waveform Energy Generation Systems and Methods of Enhandling Matrix Permeability in a Subsurface Formation - A waveform energy generation system, the system including at least one joint of production casing, and one or more energy generators residing along the joint of production casing. The energy generators are configured to be in substantial mechanical contact with a subsurface formation within a wellbore. The energy generators may include either explosive devices or a piezo-electric material. The system also includes a signal transmission system. The signal transmission system is used to send control signals from the surface down to the energy generators for activation at the formation's resonant frequency. Methods of enhancing the permeability of a rock matrix within a subsurface formation using the wellbore as an energy generator are also provided.2022-03-10
20220074287METHOD FOR CONSTRUCTING AND EXPLOITING A HYDROCARBONS PRODUCTION FACILITY, NOTABLY ON AN EXPANSE OF WATER, AND ASSOCIATED EXPLOITATION FACILITY - The method comprises supplying, at a construction site, of a functional module comprising a hybrid cooler; verifying onsite the exploitation of the equipment of the functional module; mounting the functional module on a support structure; moving the structure to an exploitation site on the expanse of water. The verification involves passing a flow to be cooled through the air cooler of the hybrid cooler, the flow being cooled exclusively by a flow of air circulating through the air cooler of the hybrid cooler. The exploitation of hydrocarbons on the expanse of water involves the passage of a flow to be cooled through the water cooler of the hybrid cooling system, the flow being cooled by heat exchange with water taken from the expanse of water circulating through the water cooler.2022-03-10
20220074288SHAPED CHARGE UTILIZING POLYMER COATED PETN - A shaped charge for perforating a formation surrounding a wellbore. The shaped charge including a casing having a section with polymer-coated explosives and a liner encapsulating the section with the polymer coated explosives. The polymer-coated explosives includes a booster explosive and a main load explosive. The booster explosive and the main load explosive are PETN. The polymer is a low-density polyethylene.2022-03-10
20220074289OILFIELD PERFORATING SELF-POSITIONING SYSTEMS AND METHODS - A self-positioning system for a perforating gun or gun string is provided. The self-positioning system includes a plurality of protrusions extending outwardly from the perforating gun or the gun string for providing a finite number of rotational positions and/or for providing a desired water clearance. The protrusions include one or more groupings of at least three protrusions, the protrusions being angularly offset from each other about the outer circumference of the perforating gun or gun string.2022-03-10
20220074290HYDRAULIC Y-TOOL SYSTEM - A submersible pump system includes a Y-tool system including a Y-Block having a production tubing branch, a submersible pump branch, and a bypass branch, an electrical submersible pump coupled to the submersible pump branch, a valve assembly coupled to the bypass branch, and a hydraulic system coupled to the valve assembly, the hydraulic system providing a hydraulic fluid to a chamber of the valve assembly. A method includes lowering production tubing into a wellbore, the production tubing including a submersible pump system with a Y-tool system including a Y-Block, and actuating a valve assembly disposed in a bypass tubing coupled to a bypass branch of the Y-Block to open or close a bore of the bypass tubing, the actuating including providing a hydraulic fluid to a chamber of the valve assembly.2022-03-10
20220074291SYSTEM AND METHOD FOR RESERVOIRED OIL PRODUCTION BASED ON CALCULATED COMPOSITION OF NATURAL TRACERS - A method for production prediction using tracers in an oilfield system is disclosed. The method involves reading, by a computer processor, a set of subsurface field properties characterizing a field system, generating, by the computer processor, a base field model, creating, by the computer processor, a plurality of static models of the field system, running, by the computer processor, a suite of dynamic simulations to produce a plurality of tracer compositions, creating, by the computer processor, a filling envelope function based on the plurality of tracer compositions, calculating, by the computer processor, a production prediction for a measured tracer composition based on the filling envelope function, and executing, by the computer processor, a field operation based on the production prediction, wherein the field operation results in hydrocarbon being extracted from a trap reservoir.2022-03-10
20220074292TREATMENT OF OTSG BLOWDOWN - A method and system generate steam for SAGD operation wherein steam generator blowdown water is acidified, cooled and clarified before reuse. Acid Clarification Treatment, or “ACT”, mitigates organic fouling in Once-Through Stream Generators. Lab tests quantitatively and qualitatively show that ACT reduces Total organic carbon (TOC) and ‘bad actors’ TOC, respectively, in blowdown streams.2022-03-10
20220074293A CONTROL SYSTEM FOR CONTROLLING FLOW RATES OF TREATMENTS USED IN HYDRAULIC FRACTURING - A system for use in hydraulic fracturing of at least one reservoir. The system including at least one pump for injecting a friction modifier into a wellbore, at least one friction modifier controller for controlling an amount of friction modifier channeled through at least one well bore, and at least one injector. The friction modifier controller is configured to monitor at least one of a fluid flow rate and pressure associated with each wellbore, compare the at least one of the fluid flow rate and the pressure with at least one of a desired flow rate and desired pressure, and adjust a friction modifier level for at least one wellbore based on results of the comparison. The injector is configured to control the pump to deliver an amount of a friction modifier into the wellbore based on the friction modifier level.2022-03-10
20220074294METHODS OF FORMING NEAR WELLBORE BARRIERS AND REDUCING BACKWASHING OF PROPPANTS - Methods of treating a portion of a wellbore include introducing a first treatment fluid to a far-field area of a subterranean formation, the first treatment fluid comprising a first proppant, and introducing a second treatment fluid to a near wellbore area of the subterranean formation, the second treatment fluid comprising a second proppant different from the first proppant. The method includes reducing flowback of the first proppant into the wellbore while permitting liquid passage into the wellbore by forming a near wellbore barrier containing the second proppant.2022-03-10
20220074295Methods and Systems of Creating Fractures in a Subsurface Formation - Methods and systems for creating fractures in rock are disclosed herein. In an exemplary method, reactive fluid is delivered into a wellbore. Formation fracture pressure is added to the reactive fluid in the wellbore sufficient to create a fracture network in a formation. The reaction pressure rubblizes the portion of a rock face of the fracture wall face to generate propping rubble that props the fracture open.2022-03-10
20220074296WELL CONFIGURATION FOR COINJECTION - A well configuration for co-injection processes, wherein a horizontal producer well at the bottom of the pay is combined with injection or injection and producer wells that are vertical and above the lower horizontal production well. This well arrangement minimizes “blanket” effects by non-condensable gases.2022-03-10
20220074297Power Management at a Wellsite - Apparatus and methods for managing power at a wellsite. An example apparatus may include a well construction equipment operable to construct a well at the wellsite, a power supply system operable to output electrical power to the well construction equipment to facilitate operation of the well construction equipment, and a control system for controlling the well construction system. The control system may be operable to store a digital drilling program and cause the well construction equipment to perform planned well construction operations based on the digital drilling program. The digital drilling program may include an equipment operational plan indicative of the planned well construction operations to be performed by the well construction equipment to construct the well, and an electrical power plan indicative of a planned electrical power demand of the well construction equipment to perform the planned well construction operations.2022-03-10
20220074298GROUND TREATMENT ASSISTANCE METHOD - Ground treatment assistance method comprising providing a machine comprising a ground treatment tool is provided, providing geographic coordinates of at least one treatment area, determining positioning data of the ground treatment tool using an optical acquisition device, displaying at least a first object representative of the ground treatment tool or of said at least one treatment area on a display device, and positioning said first object on the display device using the previously determined positioning data of the ground treatment tool and the geographic coordinates of said treatment area.2022-03-10
20220074299SYSTEM AND METHOD FOR DIAGNOSING BOREHOLE STRUCTURE VARIANCES USING INDEPENDENT COMPONENT ANALYSIS - A method and system to be used in well inspection. An acoustic signal is transmitted from a well inspection tool into a well structure and one or more return signals is detected using at least one receiver. At least one processor is used to generate variable density log (VDL) data that includes multiple waveforms in a time domain from the one or more return signals. A number of independent components to be used based on variances in the VDL data is determined and the multiple waveforms are decomposed into multiple components associated with one or more local structure variances of the well structure using independent component analysis (ICA) and the number of independent components. Characteristics of the well structure is determined based in part on patterns or features associated with one or more independent components from the multiple components.2022-03-10
20220074300SYSTEM AND METHOD FOR RETRIEVING A SOURCE ELEMENT FROM A LOGGING TOOL LOCATED IN A WELL - A system for retrieving a source element from a well may include a logging tool made of a first material, a milling tool, and a control device. The logging tool may include a cylindrical housing having a central chamber housing the source element and extending through a portion of the cylindrical housing along a central axis thereof. The logging tool may include a first communication device mounted on the cylindrical housing. The milling tool may include a tubing mounting structure that secures the milling tool to a tubing of the well. The milling tool may include a drill bit head made of a second material, the drill bit head may be configured for milling through the first material. The control device may include a second communication device configured to communicate with the first communication device.2022-03-10
20220074301DETERMINING FLUID DISTRIBUTION AND HYDRAULIC FRACTURE ORIENTATION IN A GEOLOGICAL FORMATION - A system can calculate estimated strain data for a fracture in a geological formation at each of a plurality of selected locations detectable by a strain measurement device. The system can receive real strain data from the strain measurement device for the geological formation. The system can perform a linear inversion to determine a probable distribution of fluid volume and hydraulic fracture orientation in the geological formation based on the estimated strain data and real strain data. The system can determine adjustments for a fracturing operation based on the linear inversion.2022-03-10
20220074302FLUID SATURATED FORMATION CORE SAMPLING TOOL - Downhole core sampling apparatus including first and second sealing elements and at least one pump configured to pump wellbore fluid from the annular space defined by the sealing elements. The downhole core sampling apparatus is capable of obtaining formation fluid saturated core samples for laboratory testing and reservoir evaluation. Method and system for obtaining formation fluid saturated core samples from the sidewall of subterranean wellbores is provided.2022-03-10
20220074303DETERMINING RESERVOIR FLUID PROPERTIES FROM DOWNHOLE FLUID ANALYSIS DATA USING MACHINE LEARNING - Methods for determining in situ the value of a formation fluid parameter using a downhole fluid analysis (DFA) tool. The methods utilize advanced statistical learning tools to build a predictive model to estimate a fluid property given a set of input parameters. In one embodiment the fluid saturation pressure parameter is determined by using the DFA tool to obtain the fluid and to obtain weight fractions of at least C2022-03-10
20220074304DETERMINING FLUID PARAMETERS - A method of determining a fluid parameter includes receiving, by a processor and from a plurality of sensors coupled to a flexible tube, fluid information. The flexible tube includes a throat arranged in a first position with respect to a fixed end. The fluid information includes a strain or pressure at a first portion of the flexible tube and a strain or pressure at a second portion of the flexible tube. The method also includes determining a first fluid parameter of the fluid and transmitting, from the processor to a controller operationally coupled to the throat, second position information including a second position of the throat different than the first position. The method also includes receiving, with the throat in the second position, second fluid information and determining, based on the second fluid information, a second fluid parameter of the fluid.2022-03-10
20220074305CUTTING HEAD FOR ROCK CUTTING MACHINE - A cutting head for a mining machine includes a drum, a vane, and a cutting bit assembly positioned adjacent a surface of the vane. The drum includes a first end, a second end, and an outer surface, and the drum is rotatable about a drum axis. The vane is coupled to the outer surface of the drum and protrudes radially away from the drum axis. In some aspects, the vane includes a planar member extending at least partially around the drum axis and at least partially between the first end of the drum and the second end of the drum. In some aspects, the drum includes a plurality of planar walls extending between the first end and the second end.2022-03-10
20220074306EXCAVATION TOOL REPLACEMENT DEVICE AND TUNNEL BORING MACHINE - A guide of an excavation tool replacement device includes an inner guide member configured to guide advancing and retreating of an excavation tool, and an outer guide member configured to support the inner guide member such that the inner guide member is movable to a face side and an anti-face side. The inner guide member has, at a face side end thereof, a first sealing member configured to come into close contact with a gate plate from the anti-face side.2022-03-10
20220074307GAS TURBINE ENGINE ROTOR BLADE HAVING A ROOT SECTION WITH COMPOSITE AND METALLIC PORTIONS - A rotor blade for a gas turbine engine includes an airfoil section and a root section extending along a longitudinal direction between an upstream surface and a downstream surface. The root section further extends along a radial direction between an inner surface positioned at an inner end of the root section and an outer end coupled to the airfoil section. Moreover, the root section extends along a circumferential direction between a first side surface and a second side surface. Furthermore, the root section defines a longitudinal centerline extending along the longitudinal direction and positioned equidistant from the inner surface and the outer end in the radial direction. The root section includes a first portion formed from a composite material and a second portion formed from a metallic material, with the longitudinal centerline extending through the second portion of the root section.2022-03-10
20220074308AIRCRAFT ENGINE - An aircraft engine comprising a fan, the fan having a diameter D and including a plurality of fan blades, the fan blades having a sweep metric S, each fan blade having a leading edge, and a forward-most portion on the leading edge of each fan blade being in a first reference plane. The aircraft engine further comprises a nacelle, comprising an intake portion forward of the fan, a forward edge on the intake portion being in a second reference plane, wherein the intake portion has a length L measured along an axis of the aircraft engine between the first reference plane and the second reference plane, the aircraft engine having a cruise design point condition M2022-03-10
20220074309FIBER-REINFORCED COMPOSITE PART WITH INCREASED VIBRATION RESISTANCE - A part of a turbomachine made of composite material includes a fiber reinforcement having a three-dimensional weaving including a first set of yarns made of a first material, wherein the fiber reinforcement includes a vibration-damping element formed by a second set of yarns including a second material which is viscoelastic and which is different to the first material, the second set of yarns being woven with the first set of yarns.2022-03-10
20220074310AIRFOIL WITH BODY AND COVER PANEL - An airfoil a metal body, a cover panel carried on the metal body, and push fasteners extending through the cover panel and locking the cover panel on the metal body.2022-03-10
20220074311ROTOR AND TURBO MACHINE INCLUDING SAME - A rotor and a turbo machine including the same are provided. The rotor includes a disk including a disk slot, a blade including a root member inserted into the disk slot and an airfoil disposed radially outside the root member, and configured to form a cooling cavity between an inner surface of the disk slot and the root member, a lifting part installed in the cooling cavity and configured to press the root member in a radially outward direction, and a supporting part installed in the cooling cavity, disposed in contact with the lifting part, and configured to support the lifting part.2022-03-10
20220074312NOZZLE FOR A TURBINE, TURBOMACHINE TURBINE EQUIPPED WITH SAID NOZZLE AND TURBOMACHINE EQUIPPED WITH SAID TURBINE - The invention concerns a turbine nozzle, comprising a plurality of angular nozzle sectors (2022-03-10
20220074313HIGH-TEMPERATURE COMPONENT AND METHOD OF PRODUCING THE HIGH-TEMPERATURE COMPONENT - A high-temperature component according to an embodiment is a high-temperature component which requires cooling by a cooling medium, and includes: a plurality of cooling passages through which the cooling medium is able to flow; a header portion to which downstream ends of the plurality of first cooling passages are connected; and at least one outlet passage for discharging the cooling medium flowing into the header portion to outside of the header portion. A roughness of an inner wall surface of the at least one outlet passage is not greater than a roughness of an inner wall surface of the plurality of first cooling passages in a region where a flow-passage cross-sectional area of the outlet passage is the smallest.2022-03-10
20220074314ENTRYWAY SYSTEM INCLUDING A DIVIDED VOLUTE TURBOCHARGER HAVING VARIABLE TURBINE GEOMETRY WITH AERODYNAMIC SPACERS AND VANE RING WITH PLURALITY OF ROTATABLE VANES - A system includes a divided volute turbocharger having variable turbine geometry. The turbocharger includes a turbine housing, first and second volutes separated by a wall having a first and second tongue, and a turbine housing outlet. The system also includes a turbine wheel disposed in the turbine housing and a vane ring disposed in the turbine housing between the turbine wheel and the volutes. The vane ring includes a plurality of rotatable vanes disposed on a vane ring surface of an annular disk in an asymmetric or asymmetric vane pattern that receives the turbine wheel therewithin and a pair of aerodynamic spacers spaced circumferentially outward of the plurality of vanes with each spacer positioned adjacent to a respective one tongue, with the spacers and vanes directing and controlling the flow of exhaust from the volutes into the turbine wheel with generally equal flow while significantly reducing HCF forcing function.2022-03-10
20220074315TURBINE ENGINE WITH A SHROUD ASSEMBLY - A shroud assembly for a turbine engine having a centerline axis. The shroud assembly having a shroud hanger, at least one shroud segment, and at least one biasing element extending between the two. The biasing element configured to radially bias the at least one shroud segment between an outboard position and an inboard position radially outward from the outboard position with respect to the centerline axis.2022-03-10
20220074316COMPRESSOR CLEANING APPARATUS AND METHOD, AND GAS TURBINE INCLUDING SAME APPARATUS - A compressor cleaning apparatus to clean a compressor of a gas turbine is provided. The compressor cleaning apparatus includes a nozzle configured to inject a cleaning fluid into an interior of a compressor, a fluid supply tube connected to the nozzle to supply the cleaning fluid to the nozzle, a first cleaning fluid supply connected to the fluid supply tube to supply a first cleaning fluid, and a second cleaning fluid supply connected to the fluid supply tube to supply a second cleaning fluid having a temperature higher than that of the first cleaning fluid.2022-03-10
20220074317ROTOR CONSTRUCTION FOR HIGH SPEED MOTORS - A rotor shaft for a high speed motor that has a coating that is secured to a shaft body. The coating and the shaft body are formed from dissimilar materials. More specifically, the coating may be an alloy material, such as, for example, a copper alloy, while the shaft body may be a steel material. According to certain embodiments, the alloy material of the coating may be secured to at least a portion of a rotor body blank in a solution treated condition via a low temperature welding procedure. Additionally, the coating may be hardened, such as for example, through the use of an age hardening process. The coating and the rotor body blank may be machined together to form the rotor shaft. According to certain embodiments, such machining may configure the rotor shaft for use with a turbo-compressor that is configured for air compression.2022-03-10
20220074318TURBOCHARGER BUSHING AND TURBOCHARGER - A turbocharger bushing of cylindrical shape has at least one recess formed on an inner peripheral surface of the bushing at a position away from at least one end of both ends of the bushing.2022-03-10
20220074319STEAM TURBINE AND EXHAUST CHAMBER THEREFOR - An exhaust chamber is equipped with: a diffuser that forms a diffuser space; an exhaust casing that forms an exhaust space communicating with the diffuser space; and an auxiliary exhaust frame that forms an auxiliary exhaust space having an annular shape centered around an axis, on the inside of the diffuser in the radial direction. The auxiliary exhaust frame has an opening that opens toward the outside in the radial direction from the interior of the auxiliary exhaust space, and that enables the exhaust space and the auxiliary exhaust space to communicate with each other.2022-03-10
20220074320VARIABLE VALVE DRIVING MECHANISM OF ENGINE, AND ENGINE - A variable valve driving mechanism of an engine, and the engine. The variable valve driving mechanism comprises a rocker arm (2022-03-10
20220074321SWITCHABLE ACTUATION DEVICE FOR A POPPET VALVE IN AN INTERNAL COMBUSTION ENGINE, INTERNAL COMBUSTION ENGINE AND MOTOR VEHICLE - The present invention relates to a switchable actuation device (2022-03-10
20220074322OIL COOLING FOR ELECTROMAGNETIC LATCH HOUSED IN ROCKER ARM - A valvetrain includes a rocker arm assembly basing a rocker arm and an electromagnetic latch assembly. An electromagnet of the latch assembly is housed within a chamber formed by the rocker arm. Passageways suitable for oil cooling of the electromagnet are formed through and inside the rocker arm. In some embodiments, oil for cooling is supplied through a pivot. In some embodiments, oil for cooling is obtained from oil splash. Oil cooling may allow modes of operation such as of dynamic cylinder deactivation and dynamic variable valve actuation to be used without overheating the electromagnet.2022-03-10
20220074323CONTROL VALVE USED IN VALVE TIMING CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE AND VALVE TIMING CONTROL SYSTEM FOR INTERNAL COMBUSTION ENGINE - In a first state: a spool valve of a control valve is disposed such that a second spool oil passage is closer to a second side in a longitudinal direction than a first spool oil passage; and as the spool valve has traveled toward the second side against a biasing force of a biasing member, a first port communicates with a second port via the first spool oil passage, a first sleeve oil passage, and the second spool oil passage. In a second state: the spool valve is disposed such that the first spool oil passage is closer to the second side than the second spool oil passage; and as the spool valve has traveled toward a first side in the longitudinal direction, the first port communicates with the second port via the first spool oil passage, the first sleeve oil passage, and the second spool oil passage.2022-03-10
20220074324PRESSURE SHIFTED VALVE TIMING - A hydraulic pump-motor includes a cylinder block including a plurality of fluid chambers, a piston in each of the fluid chambers, a cam, a fixed valve area profile, and a timing adjustment actuator. The cam includes a cam surface that engages the pistons and drives movement of the pistons relative to the fluid chambers in response to relative rotation between the cam and the fluid chambers. The fixed valve area profile is configured to control fluid flows between the fluid chambers and first and second ports. The timing adjustment actuator is configured to adjust an angular orientation of the fixed valve area profile relative to an angular orientation of the cam based on a pressure differential between a pressure at the first port and a pressure at the second port.2022-03-10
20220074325METHOD OF MANUFACTURE AND DESIGN OF CAST-IN-PLACE VALVE SEATS - A cylinder head having a cast-in-place valve seat for an automobile vehicle includes a valve seat having an inner wall. At least one retaining feature integrally and homogeneously extends from the inner wall. The valve seat when positioned into a casting mold has the at least one retaining feature assisting in retaining the valve seat in the casting mold. A metal in a molten form is received in the casting mold. A cast component formed after cooling of the metal has the valve seat cast-in-place.2022-03-10
20220074326LIQUID FILTER ARRANGEMENT FOR NO-MESS LIQUID CHANGE - An easily serviceable liquid filter assembly having a housing with a drain to provide draining of fluid (e.g., liquid) from the housing. The filter assembly has a fluid inlet to receive dirty fluid into the housing, a fluid outlet to expel filtered fluid from the housing, and a drain, when open, to expel unfiltered (dirty) fluid from the housing. By removing a cover from the housing, the filter element opens the drain so that all fluid in the housing can be directly collected or can flow into the oil pan to be collected with the fluid present in the pan. All fluid, now in the drain pan, can be drained and collected in a disposable container such as a plastic pouch, which can be recycled. The filter element can be removed from the housing via the removed cover.2022-03-10
20220074327OIL FILTER ASSEMBLY - A one-piece cast metallic adaptor for a filtering assembly that provides for direct threading of associated components to the adaptor. The adaptor provides an enclosed flow path for lubricant to flow between an engine lubrication network and a filter housing.2022-03-10
20220074328CYLINDER HEAD - An internal combustion engine-includes at least one cylinder crankcase, at least one cylinder head (2022-03-10
20220074329PROPULSION FLOW PATH DUCT SYSTEMS AND METHODS - A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.2022-03-10
20220074330Engine - An engine that suppresses damage on a support mechanism of a diesel particulate filter (DPF) due to vibration in the pitch direction, in which the DPF, which purifies exhaust gas from an exhaust manifold, is disposed in an orientation orthogonal or approximately orthogonal to a rotational axis of a crankshaft in a plan view. A support mechanism is provided, which enables a cylinder head, an intake manifold, and an intake collector to support the DPF. The support mechanism includes a first support position in which the cylinder head supports the DPF, a second support position in which the intake manifold supports the DPF, and a third support position in which the intake collector supports the DPF. The third support position deviates from the first support position and the second support position in a direction of the rotational axis of the crankshaft.2022-03-10
20220074331EVAPORATIVE FUEL VAPOR EMISSION CONTROL SYSTEMS - An evaporative emission control canister system comprises an initial adsorbent volume having an effective incremental adsorption capacity at 25° C. of greater than 35 grams n-butane/L between vapor concentration of 5 vol % and 50 vol % n-butane, and at least one subsequent adsorbent volume having an effective incremental adsorption capacity at 25° C. of less than 35 grams n-butane/L between vapor concentration of 5 vol % and 50 vol % n-butane, an effective butane working capacity (BWC) of less than 3 g/dL, and a g-total BWC of between 2 grams and 6 grams. The evaporative emission control canister system has a two-day diurnal breathing loss (DBL) emissions of no more than 20 mg at no more than 210 liters of purge applied after the 40 g/hr butane loading step.2022-03-10
20220074332METHOD FOR CONTROLLING EXHAUST AFTERTREATMENT SYSTEM FOR VEHICLES - A method for controlling an exhaust aftertreatment system for vehicles includes: determining, by a controller, whether or not a designated regeneration operation is finished; accumulating, by the controller, a first amount of NO2022-03-10
20220074333Exhaust Gas Heater - An exhaust gas heater for an exhaust gas system of a combustion engine includes a carrier and at least one heating conductor through which a current flows. The heating conductor is mounted on the carrier. The heating conductor is provided via separation from a metal flat material blank. A method of making an exhaust gas heater includes a step of separating the heating conductor from the metal flat material blank.2022-03-10
20220074334ENGINE FUEL REFORMING SYSTEM - A fuel reforming system includes a fuel injection device capable of injecting fuel into an EGR passage, a reforming catalyst provided in the EGR passage, an oxidation catalyst provided in the vicinity of the reforming catalyst in the EGR, and an air supply device that supplies air to the EGR passage. When clogging occurs in the reforming catalyst and a temperature of the reforming catalyst is less than a first temperature, air is supplied to the EGR passage by the air supply device, and fuel is injected by the fuel injection device. When clogging occurs in the reforming catalyst and the temperature of the reforming catalyst is greater than or equal to the first temperature, air is supplied to the EGR passage by the air supply device, and fuel injection of the fuel injection device is stopped.2022-03-10
20220074335TWO-PART TWO-STAGE MIXER - A mixer comprises a first subassembly including a first holder fixed to a first mixing element. The first holder includes a base interconnecting a first sidewall with a spaced apart second sidewall. The first mixing element includes a base interconnecting first and second spaced apart mounting flanges that are fixed to the first and second sidewalls. A second subassembly includes a second holder fixed to a second mixing element. The second holder includes a base interconnecting a third sidewall with a spaced apart fourth sidewall. The second mixing element including a base interconnecting third and fourth spaced apart mounting flanges that are fixed to the third and fourth sidewalls. Distal ends of the first sidewall and the third sidewall are fixed to one another. Distal ends of the second sidewall and the fourth sidewall are fixed to one another.2022-03-10
20220074336EXHAUST GAS AFTER-TREATMENT MIXING DEVICE - An exhaust gas after-treatment mixing device comprises a casing, a mixing pipe located in the casing and a partition plate separating the casing into an upstream space and a downstream space. The mixing pipe comprises a first pipe portion located in the upstream space and a second pipe portion located in the downstream space. The first pipe portion is provided with at least two first openings located on two sides of the first pipe portion, respectively. A shielding plate shields an upstream portion of at least one of the first openings. The shielding plate is shaped and positioned within the casing to urge exhaust gas flowing through the upstream space away from the first end of the mixing pipe and around the shielding plate prior to entering the first openings.2022-03-10
20220074337VEHICLE HEAT EXCHANGE SYSTEM - A vehicle heat exchange system may include a first heat exchanger for exchanging heat between a first medium and a second medium, a second heat exchanger for exchanging heat between the first medium and a third medium, a third heat exchanger for exchanging heat between the second medium and the third medium, a switch valve, and a control unit. The switch valve may be configured to enable selective switching between (i) a first path that supplies the second medium that has passed through the third heat exchanger to an inverter via an inverter radiator and (ii) a second path that supplies the second medium that has passed through the third heat exchanger to the inverter via the first heat exchanger. The control unit may be configured to control the switch valve such that the second path is selected when the first medium is in a predetermined low-temperature state.2022-03-10
20220074338CONTROL SYSTEM AND METHOD FOR A FAN - A system that may include an engine, and a fan configured to vary a measured engine temperature of the engine during operation. A vehicle controller may also be provided having one or more processors that may be configured to determine an ice risk characteristic of the engine, operate the fan to cool the engine based on the ice risk characteristic, and operate the fan to rotate in reverse based on the ice risk characteristic.2022-03-10
20220074339DEVICE FOR PREVENTING BACKWARD AIR FLOW OF RESERVOIR TANK FOR VEHICLE - The present disclosure provides a device for preventing the backward air flow of a reservoir tank for a vehicle, which may mount an backward air flow prevention tube extending to coolant on a connector of a reservoir tank to which a degassing hose is connected, and form an air collection slit hole communicating with an upper space of the reservoir tank in the upper portion of the tube to be openable or closable, thereby easily preventing the phenomenon in which the air within the reservoir tank flows back toward an engine, and easily collecting the air introduced from the engine side.2022-03-10
20220074340VEHICLE ENGINE FLUSHING MACHINE WITH HEATING AND REVERSE FLOW - A fluid flushing machine for a vehicle engine component uses a pre-heated cleaner/fluid to increase the effectiveness of the cleaning procedure and reduce the time needed to clean the component. The invention is designed to clean air charged coolers, EGR valves, EGR coolers, and other components that over time have become contaminated with carbon build up, oil, and debris. The machine of the present invention has the option to direct heated cleaning fluid through the vehicle engine's cooling system to remove carbon build up, oil, and debris in the vehicle's EGR valve and cooler component. The machine of the present invention is adapted to perform the operation in an engine-off condition by incorporating an integrated or external electronic device to open the vehicle's EGR valve to allow the cleaning fluid to flow through the engine while it is turned off.2022-03-10
20220074341CYLINDER HEAD FOR AN INTERNAL COMBUSTION ENGINE - A cylinder head for an internal combustion engine comprising a prechamber (2022-03-10
20220074342SUPERCHARGER WITH TWO COMPRESSORS DRIVEN TOGETHER ON A SINGLE SHAFT - A supercharger for an internal combustion engine includes two compressors, each having a compressor wheel mounted on a common shaft, and a mechanical linkage for transmitting power from a running engine to the common shaft to provide a desired boost with less torque by using two smaller compressor wheels rather than a single larger compressor wheel.2022-03-10
20220074343TURBOCHARGER WITH TWO COMPRESSORS DRIVEN BY A SINGLE TURBINE - A turbocharger for an internal combustion engine includes two compressors, each having a compressor wheel mounted on opposite ends of a common shaft, and a turbine having a turbine wheel mounted on the same shaft as the compressor wheel and between the compressor wheels, to reduce turbo-lag, while providing a reliable and robust structural design.2022-03-10
20220074344ADDITIVELY MANUFACTURED BOOSTER SPLITTER WITH INTEGRAL HEATING PASSAGEWAYS - A booster splitter for a gas turbine engine and a method of additively manufacturing the booster splitter are provided. The booster splitter includes an annular inner wall defining a radially outer boundary of a compressor flow path defined through a compressor section of the gas turbine engine, an annular outer wall spaced apart from the annular inner wall along the radial direction, the annular outer wall adjacent to the annular inner wall at a forward end, the forward end defining an inlet to the compressor flow path, an annular bulkhead spanning between the annular inner wall and the annular outer wall substantially along the radial direction, the bulkhead defining an inlet port, and a passageway defined within the annular outer wall, the passageway extending from the inlet port, into the bulkhead, radially outward to the outer wall, and through the annular outer wall towards the inlet defined by the forward end.2022-03-10
20220074345SYSTEMS AND METHODS TO ENHANCE INTAKE AIR FLOW TO A GAS TURBINE ENGINE OF A HYDRAULIC FRACTURING UNIT - Systems and methods to increase intake air flow to a gas turbine engine of a hydraulic fracturing unit when positioned in an enclosure may include providing an intake expansion assembly to enhance intake air flow to the gas turbine engine. The intake expansion assembly may include an intake expansion wall defining a plurality of intake ports positioned to supply intake air to the gas turbine engine. The intake expansion assembly also may include one or more actuators connected to a main housing of the enclosure and the intake expansion assembly. The one or more actuators may be positioned to cause the intake expansion wall to move relative to the main housing between a first position preventing air flow through the plurality of intake ports and a second position providing air flow through the plurality of intake ports to an interior of the enclosure.2022-03-10
20220074346MONOLITHIC SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION - The present disclosure generally relates to monolithic superstructures for supporting a rotating shaft coupled to a rotor relative to a stator. An integral superstructure supports the rotating component. The superstructure includes a bearing portion that contacts the shaft. A stator portion, is spaced a critical dimension radially outward, from the rotor. A first annular transfer portion extends axially forward from the bearing to the stator portion. A second annular transfer portion extends axially aft from the stator portion to a mounting flange. The mounting flange connects the superstructure to a frame. The superstructure maintains a critical dimension between the rotor and the stator as the temperature of the superstructure increases. The rotor may be a compressor impeller in a gas turbine engine and the stator may be an aero component that transfers air into a combustor.2022-03-10
20220074347BURNER, COMBUSTOR INCLUDING SAME, AND GAS TURBINE - A burner comprises: at least one mixing tube extending inside a fuel plenum and having an interior configured to be supplied with an air; and a plurality of fuel injection holes for injecting a fuel supplied to the fuel plenum into the interior of the at least one mixing tube. When the at least one mixing tube is viewed in an axial direction of the mixing tube, a central axis of each of the plurality of fuel injection holes is oblique in a same direction with respect to a circumferential direction of the mixing tube, to a radial direction of the mixing tube.2022-03-10
20220074348TURBINE ENGINE WITH SHOCKWAVE ATTENUATION - Aspects of the disclosure generally relate to a turbine engine and method of operating a turbine engine having an engine core including a compressor, combustor, and turbine in axial flow arrangement, whereby a working airflow passes through the engine core from the compressor to the turbine to define a flow direction through the engine core. The method includes generating a shockwave in the working airflow that propagates in the flow direction, and at least partially attenuating the shockwave.2022-03-10
20220074349SPLIT COMPRESSOR GAS TURBINE ENGINE - A turboprop or turboshaft gas turbine engine includes a low pressure turbine drivingly engaged to an output shaft for driving a rotatable load. A low pressure compressor is de-coupled from the low pressure turbine, the low pressure compressor and turbine rotating independently from one another. A high pressure compressor is disposed downstream from the low pressure compressor and is in fluid communication therewith to receive pressurized air therefrom. A high pressure turbine is disposed downstream from the high pressure compressor and is drivingly engaged thereto via a high pressure shaft. The high pressure turbine is disposed upstream from the low pressure turbine and is in fluid communication therewith. An electric motor receives power from a power source, is drivingly engaged to the low pressure compressor, and is operable to drive the low pressure compressor independently from the low pressure turbine, the high pressure compressor and the high pressure turbine.2022-03-10
20220074350GAS TURBINE ENGINE FRONT SECTION - A turbofan engine includes a geared architecture for driving a fan about an axis. The geared architecture includes a sun gear rotatable about an axis, a plurality of planet gears driven by the sun gear and a ring gear circumscribing the plurality of planet gears. A carrier supports the plurality of planet gears. The geared architecture includes a power transfer parameter (PTP) defined as power transferred through the geared architecture divided by gear volume multiplied by a gear reduction ratio.2022-03-10
20220074351GAS TURBINE ENGINE WITH NON-EPICYCLIC GEAR REDUCTION SYSTEM - A gas turbine engine comprises a fan drive turbine driving a shaft. The shaft engages a gear reduction. The gear reduction drives a fan rotor at a speed that is less than the speed of the fan drive turbine. The gear reduction is a non-epicyclic gear reduction.2022-03-10
20220074352TURBINE SECTION OF GAS TURBINE ENGINE - A gas turbine engine according to an example of the present disclosure includes, among other things, a propulsor including a circumferential array of blades, a low pressure compressor section including a low pressure compressor section inlet with a low pressure compressor section inlet annulus area and a low pressure turbine section. The low pressure turbine section includes a maximum gas path radius, the blades include a maximum radius, and a ratio of the maximum gas path radius to the maximum radius of the blades is equal to or greater than 0.35, and is less than 0.55.2022-03-10
20220074353METHOD OF ASSEMBLY FOR GEAR SYSTEM WITH ROTATING CARRIER - A method of assembling a gear system for a gas turbine engine according to an example of the present disclosure includes the steps of providing a unitary carrier, positioning baffles between side walls of the carrier such that an end of each of the baffles abuts a respective mount of the carrier, inserting intermediate gears through a central opening of the carrier, and then moving the intermediate gears radially outwardly into respective gear pockets of the carrier, inserting a sun gear through the central opening, moving the intermediate gears radially inwardly to engage the sun gear, coupling a shaft to the carrier, including attaching a torque frame to the carrier such that the torque frame interconnects the carrier and the shaft, placing first and second ring gear halves of a ring gear onto an outer periphery of the intermediate gears, and fixedly attaching the ring gear to an engine static structure. A gear system is also disclosed.2022-03-10
20220074354TURBOGENERATOR METHOD AND APPARATUS - A method for maximising the total power output of a power generation system is described the method comprising providing a power generation system comprising a turbocharged prime mover and a turbogenerator system driven by a flow of exhaust fluid from the prime mover, the turbogenerator system creating a backpressure on the turbocharged prime mover, comparing a parameter of the power generation system to a threshold value of the parameter, and adjusting the turbogenerator system to vary the backpressure on the turbocharged prime mover to change the parameter to become closer to the threshold value and increase the total power output or fuel efficiency of the power generation system. An apparatus for performing the method is also described.2022-03-10
20220074355ENGINE CORE SPEED REDUCING METHOD AND SYSTEM - A method for reducing an engine core speed is disclosed, which includes determining a condition of an engine during operation of the engine, and controlling an engine turbine clearance based on the condition of the engine so as to influence the engine core speed. An engine system comprising an engine core speed reducing system is also disclosed.2022-03-10
20220074356THERMAL MANAGEMENT OF EXHAUST GAS VIA CYLINDER DEACTIVATION - A system includes a controller coupled to an exhaust gas aftertreatment system coupled to a plurality of combustion cylinders of an engine. The controller is structured to: determine that the engine is operating in a low load operating condition; deactivate a combustion cylinder based on the determination that the engine is operating in the low load operating condition such that an exhaust gas temperature threshold corresponds with when the combustion cylinder is deactivated; increase an engine exhaust gas temperature while the combustion cylinder is deactivated via at least one thermal management command; and reactivate the deactivated combustion cylinder in response to the engine operating with a load greater than a preset threshold for a certain period of time.2022-03-10
20220074357CONTROL SYSTEM AND METHOD FOR MULTI-FUEL GENERATOR ENGINE - A control system and method for a multi-fuel generator engine are mainly applied to multi-fuel generator products. The control system comprises a controller, a first signal input terminal, a second signal input terminal, a third signal input terminal, and an output terminal connected to an ignition device of a generator engine. When the third signal input terminal of the controller receives a generator engine start signal and either the first signal input terminal or the second signal input terminal receives a signal corresponding to an on state of the corresponding valve assembly, the controller controls the ignition device to ignite. According to control system and method, the controller detects signals corresponding to the states of the two fuel valve assemblies to determine whether or not fuels are normally supplied, so that operating instabilities or faults caused by synchronous supply of two fuels to the generator engine are avoided.2022-03-10
20220074358INTERNAL COMBUSTION ENGINE HAVING CARBON DIOXIDE CAPTURE AND FUEL ADDITIVE SYNTHESIS SYSTEM - Separation of carbon dioxide from the exhaust of an internal combustion engine, the production of hydrogen from water, and reformation of carbon dioxide and hydrogen into relatively high-octane fuel components.2022-03-10
20220074359THROTTLE CONTROLLED INTAKE SYSTEM - A throttle-controlled intake system is disclosed that provides a driver of a vehicle with greater control over engine functions and vehicle performance. The throttle-controlled intake system includes a control module that is coupled with an aircharger air intake. The control module processes input signals from a throttle pedal of the vehicle and sends modified throttle position signals to a throttle body of the vehicle so as to increase throttle responsiveness of the vehicle. The throttle-controlled intake system further includes a wiring harness and a signal adjuster. The wiring harness electrically couples the control module with the throttle pedal and the throttle body. The control module sends signals directly to the throttle body of the engine, bypassing an electronic control unit of the vehicle. The signal adjuster includes a rheostat that enables manual adjustment of the throttle responsiveness of the vehicle.2022-03-10
20220074360SYNCHRONISATION OF AN INTERNAL COMBUSTION ENGINE - Sensor delivering detection information in the form of a variation of a current, including a sensitive portion adapted to detecting the passage of a mobile target, an electronic module able to control and shape signals coming from the sensitive portion, an embedded intelligence module adapted, inter alia, to receive information from an electronic computer and to process and generate information intended for the electronic computer, characterized in that the sensor includes a random-number generation module able to generate a random number.2022-03-10
20220074361ENGINE TORQUE SMOOTHING - Methods, devices, estimators, controllers and algorithms are described for estimating the torque profile of an engine and/or for controlling torque applied to a powertrain by one or more devices other than the engine itself to manage the net torque applied by the engine and other device(s) in manners that reduce undesirable NVH. The described approaches are particularly well suitable for use in hybrid vehicles in which the engine is operated in a skip fire or other dynamic firing level modulation manner—however they may be used in a variety of other circumstances as well. In some embodiments, the hybrid vehicle includes a motor/generator that applies the smoothing torque.2022-03-10
20220074362METHOD FOR CONTROLLING EXHAUST AFTERTREATMENT SYSTEM FOR VEHICLE ENGINE - A method for controlling an exhaust aftertreatment system for a vehicle includes: determining, by a controller, whether or not a driving state of the vehicle satisfies a clogging determination condition; estimating, by the controller, a normal temperature of a rear end of a catalytic converter upon determining that the clogging determination condition is satisfied; calculating, by the controller, clogging indexes using an actual temperature of the rear end of the catalytic converter measured by a temperature sensor and the estimated normal temperature; determining, by the controller, whether or not it is necessary to settle clogging of the catalytic converter by comparing the clogging indexes with reference ranges; and executing, by the controller, a clogging settlement mode upon determining that it is necessary to settle clogging of the catalytic converter.2022-03-10
20220074363A METHOD FOR CONTROLLING THE BRAKING OF A VEHICLE COMPRISING A DIESEL ENGINE - The invention relates to a method for controlling braking of a vehicle (2022-03-10
20220074364EVAPORATIVE FUEL PROCESSING DEVICE - An evaporative fuel processing device for determining a leak of an evaporation piping system also determined pump abnormality by including a pump, a pressure sensor and an abnormality determiner, i.e., by pressuring/de-pressuring the system to a positive/negative value against an atmospheric pressure for leak determination, by detecting a pressure of the system, and by determining a leak hole in a normal leak determination mode based on an absolute value of the detected pressure reaching or not reaching a target value after pump operation and based on an assumption that the pump is normal. Specifically, after lapse of a determination time from a pump stop, the absolute value equal to or less than a normal leak determination threshold value is determined that a leak hole is present in the system. Further, the absolute value not reaching the target value even after pump operation triggers a pump abnormality determination mode.2022-03-10
20220074365CYLINDER HEAD - A cylinder head configured for dividing coolant introduced thereinto to a combustion chamber side and an exhaust manifold side to increase the amount of coolant introduced to the combustion chamber side, improving cooling performance, may include a head water jacket having a combustion chamber coolant inlet, through which coolant is introduced from a cylinder block to a combustion chamber side, and an exhaust coolant inlet, through which the coolant is introduced from the cylinder block to an exhaust manifold side, the combustion chamber coolant inlet and the exhaust coolant inlet being separated from each other such that the coolant introduced through the combustion chamber coolant inlet flows to the combustion chamber side in an expanded state.2022-03-10
20220074366PISTON CROWN FOR A COMBUSTION SYSTEM AND AN ASSOCIATED METHOD THEREOF - A piston crown for a combustion system is disclosed. The piston crown includes a piston bowl having a circumferential recess and a plurality of first recesses arranged spaced apart from each other along a circumferential direction. The circumferential recess is disposed proximate to a circumference of the piston crown. Each recess of the plurality of the first recesses extends between a center of the piston crown and the circumferential recess, and a width and a depth of each recess of the plurality of first recesses are extended along a radial direction for an entire length of each recess of the plurality of first recesses.2022-03-10
20220074367ENGINE APPARATUS AND METHOD FOR OPERATION - A piston apparatus may include a plurality of piston assemblies respectively having a first piston body and a first piston disposed within a first volume defined by the first piston body, a second piston body and a second piston disposed within a second volume defined by the second piston body, and a connection member coupled to the first piston and the second piston. The first and second volume may respectively include an expansion chamber and a compression chamber defined by opposite sides of the corresponding piston. The respective expansion chambers may fluidly communicate with a corresponding compression chamber of another one of the piston assemblies. The first volume of a first piston assembly may fluidly communicate with the first volume and the second volume of a second piston assembly, and the first volume of a third piston assembly may fluidly communicate with the first volume and the second volume of the second piston assembly.2022-03-10
20220074368GAS TURBINE ENGINE WITH AIRFLOW MEASUREMENT SYSTEM - A turbofan gas turbine engine having a bypass duct, and a bypass airflow measurement system. The bypass airflow measurement system comprises: at least one acoustic transmitter configured to transmit an acoustic waveform across the bypass duct of the gas turbine engine though which a bypass airflow passes to at least one acoustic receiver; where the at least one acoustic transmitter and the at least one acoustic receiver are located on an axial plane that is substantially perpendicular to the bypass flow. A method of measuring bypass airflow properties of a turbofan gas turbine engine is also described.2022-03-10
20220074369AIRFRAME INTEGRATED SCRAMJET WITH FIXED GEOMETRY AND SHAPE TRANSITION FOR HYPERSONIC OPERATION OVER A LARGE MACH NUMBER RANGE - Airframe integrated scramjet engines are disclosed. Scramjet engines within the scope of this disclosure may be configured to integrate smoothly with an airframe of a hypersonic flight aircraft or vehicle. The scramjet engine may include capture shape of an inlet configured to capture airflow, a combustor configured for combustion of fuel and air, and an exit shape of a nozzle configured for expansion of the combusted fuel and air to provide hypersonic thrust. In some embodiments, the scramjet engine has a fixed geometry and a transitioning cross-sectional shape over its full length. The scramjet engine is configured to be a component of launch vehicle system.2022-03-10
20220074370MAGNETICALLY LATCHING VALVE FOR FUEL VAPOR MANAGEMENT SYSTEMS AND SYSTEMS INCORPORATING SAME - Magnetic latching valves have a housing with first and second ports in controlled fluid communication with one another. Enclosed within the housing is a linearly translatable armature within a solenoid. The armature is movable between open and closed positions and is connected to a poppet valve. A permanent magnet is fixedly seated at a position for magnetically latching the armature in the open position, and a spring is seated with a first end against the poppet valve and a second end against the housing. The spring biases the poppet valve closed when the armature is in the closed position and has a pre-selected spring rate that mechanically relieves pressure if the spring rate is exceeded. The armature is moved to the open position after a pulse of voltage to the solenoid and is in an unpowered state thereafter. Vehicle fuel refueling system are disclosed that include a magnetic latching valve.2022-03-10
20220074371THREE PORT, FIVE-WAY MAGNETICALLY LATCHING VALVE FOR FUEL VAPOR MANAGEMENT SYSTEMS AND SYSTEMS INCORPORATING SAME - Three-port latching valves have a housing with a first port, a second port, and a third port in controlled fluid communication with one another by three, individually electronically controllable magnetically latching valves for a combination of five different flow options. Each valve has a solenoid with an armature movable between an open position and a closed position, a poppet valve connected to the armature, a permanent magnet fixedly seated at a position for magnetically latching the armature in the open position, and a spring positioned to bias the poppet valve closed when the armature is in the closed position. The spring has a pre-selected spring rate that mechanically relieves pressure if the spring rate is exceeded. The armature is movable to the open position after a pulse of voltage to the solenoid and is in an unpowered state after translation to either of the open position or the closed position.2022-03-10
20220074372CARBON CANISTER - A carbon canister includes a main body with a chamber containing activated carbon, an end cover mounted to the main body, the end cover and the main body enclosing and forming a cavity, the end cover having a desorption port for connecting with and engine, a Venturi tube mounted in the cavity and including an inlet segment, and a throat and a back suction tube. An inner diameter of the throat is smaller than an inner diameter of the inlet segment. The inlet segment communicates with the activated carbon containing chamber, the throat communicates with the desorption port, the back suction tube connects to the throat, and the back suction tube extends to the bottom of the cavity. Thereby, a negative pressure is created, the fuel collected within the carbon canister is desorbed to the engine so that the fuel utilization is improved, and the exhaust emission is reduced.2022-03-10
20220074373SYSTEM AND METHOD FOR SUSTAINABLE GENERATION OF ENERGY - A system for sustainable generation of energy, comprising at least one device for converting natural power into useful energy, and at least one internal combustion engine or heat engine. The internal combustion engine or heat engine may be connected to a gas cleaning device for fuel or heat supply. A method for sustainable generation of energy, comprising the steps of generating a first amount of useful energy by converting natural power; and generating a second amount of energy by operating at least one internal combustion engine or heat engine, wherein the internal combustion engine or heat engine is driven by fuel or heat derived from cleaning a waste gas.2022-03-10
20220074374INTERCOOLER ASSEMBLY - An intercooler assembly for an intercooler supercharger system comprising a plurality of separate, contiguous intercooler cores, each including a top and a bottom, wherein the tops of the intercooler cores are coplanar and at least two of the bottoms of the intercooler cores are not coplanar.2022-03-10
20220074375Physical Quantity Detection Device - To obtain a physical quantity detection device capable of reducing an intake amount of air accompanied by foreign matter. A physical quantity detection device (2022-03-10
20220074376INTERNAL COMBUSTION ENGINE - An internal combustion engine that includes a first fuel pump that sucks fuel through a fuel filter, and a second fuel pump that supplies the fuel to a fuel injection device. The internal combustion engine comprises: a first fuel pipe that interconnects the fuel filter, the first fuel pump, and the second fuel pump set to have a pressure higher than a pressure of the first pump; and a second fuel pipe that connects the second fuel pump to the fuel injection device that injects fuel into a combustion chamber formed in a cylinder portion of the internal combustion engine, a shielding wall covering an outside of the cylinder portion is provided between at least a part of the second fuel pipe and the cylinder portion, and the shielding wall includes a holding portion that holds at least the first fuel pipe and the second fuel pipe.2022-03-10
20220074377MULTIPLE PUMP FUEL SYSTEM - In at least some implementations, a fuel pump assembly includes a first fuel pump and a second fuel pump that each have an electric motor, a pumping element driven by the motor, an inlet and an outlet through which fuel is discharged. The assembly also includes a passage communicated with the outlet of the first fuel pump and with the outlet of the second fuel pump, a fuel outlet in communication with the passage and through which fuel exits the fuel pump assembly, and a valve having an inlet in communication with the passage between the outlet of the first fuel pump and the outlet of the second fuel pump. The valve also having an outlet through which fuel exits the passage and a valve body that controls fuel flow through the valve.2022-03-10
20220074378FUEL INJECTOR AND NOZZLE ASSEMBLY HAVING DUAL CONCENTRIC CHECK ASSEMBLY AND DUCTED SPRAY ORIFICES - A fuel injector includes a nozzle assembly having a nozzle case, and a concentric check assembly within the nozzle case. Transfer passages are formed in an outer check of the check assembly, and spray orifices are formed in the nozzle case. A fuel volume is formed between the outer check and an inner check, and the inner check is movable to fluidly connect the transfer passages to the fuel volume. The outer check is rotatable between a first angular orientation and a second angular orientation to fluidly connect separate sets of the transfer passages to separate sets of the spray orifices. Spray ducts are in spray path alignment with at least one of the sets of spray orifices.2022-03-10
20220074379VARIABLE ENERGY IGNITION SYSTEMS, METHODS, AND APPARATUSES - A method of controlling an ignitor for a spark-ignition engine includes receiving, by a controller, at least one of fuel quality data regarding a fuel for the spark-ignition engine or a characteristic regarding the ignitor for the spark-ignition engine. The method additionally includes controlling, by the controller, an ignition energy characteristic of the ignitor in response to the at least one of the fuel quality data regarding the fuel or the characteristic regarding the ignitor for the spark-ignition engine.2022-03-10
20220074380HYDROELECTRIC/HYDROKINETIC TURBINE AND METHODS FOR MAKING AND USING SAME - The application relates to unidirectional hydrokinetic turbines having an improved flow acceleration system that uses asymmetrical hydrofoil shapes on some or all of the key components of the turbine. These components that may be hydrofoil shaped include, e.g., the rotor blades (2022-03-10
20220074381CONDUIT TURBINE FOR SUPPORTING CONDUIT OF WATER WHEEL ROTATIONAL BODY, AND HYDROELECTRIC GENERATOR HAVING CONDUIT TURBINES SERIALLY PROVIDED IN MULTIPLE LEVELS - The hydroelectric generator using a conduit turbine, is characterized in that at least two conduit turbine units are serially arranged in multiple levels, the conduit turbine units each comprising: a driving shaft which penetrates the center of a conduit through which a flow for electric generation passes to the inside; a conduit support main body which is provided so as to support the driving shaft, and has an arm extending towards the inner surface of the conduit; a propeller which is between two conduit support main bodies, is fixed to the driving shaft, and rotates by means of the movement of the flow; an internal gear which rotates together with the driving shaft from between the conduit support main bodies; an external gear which is driven together with a shaft, outside the conduit, as a rotational force is delivered to the internal gear; and an electric generator.2022-03-10
20220074382APPARATUS AND METHOD - An apparatus (2022-03-10
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