| 45th week of 2021 patent applcation highlights part 31 |
| Patent application number | Title | Published |
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| 20210348545 | Pre-Combustion Chamber Apparatus and Method for Pre-Combustion - The present invention uses an improved engineered metal seal with or without an internal energized spring that is disposed in a pre-combustion chamber apparatus assembly to improve sealing over the flat washer seals that are currently used. The seals of the present invention comprise at least three different geometrical configurations of seals that are manufactured from titanium, Inconel, and/or hastelloy. The design of the tip and body of the pre-combustion chamber provide for movement of the seal without leaking. The sealing is provided on the axial surfaces of the tip and the body instead of the face of the tip and body by a flat washer seal, as is currently done. | 2021-11-11 |
| 20210348546 | SPARK-IGNITION INTERNAL COMBUSTION ENGINE - A spark-ignition internal combustion engine includes a cylinder head and a piston. A crown surface of the piston includes a central portion, and first outer portions and second outer portions located outside the central portion. The central portion and the first outer portions have a combustion chamber height higher than a predetermined value. The combustion chamber height of the second outer portions is equal to or lower than the predetermined value. The crown surface is composed of a mirror surface region and a rough surface region. The mirror surface region has a surface roughness of less than 0.05 μm. The rough surface region has a surface roughness of 0.05 μm or more and 2.5 μm or less. All of the central portion and the first outer portions are included in the mirror surface region. At least one of the second outer portions is included in the rough surface region. | 2021-11-11 |
| 20210348547 | TWO-STAGE TURBOCHARGED INTERNAL COMBUSTION ENGINE - A two-stage turbocharged internal combustion engine comprises a low-pressure stage turbocharger mounted at a first end side of an engine block and a high-pressure stage turbocharger mounted at the same first end side of the engine block. The respective turbochargers are mounted via a mounting structure, Which also accommodates the charge air coolers associated with the turbochargers. In order to obtain a compact arrangement and reduce a length of pipe connections between the different components, the different charge air coolers are mounted to mounting structure such that they overlap in a plan view of the internal combustion engine. Further, flow directions of charge air in the different charge air coolers are opposite to each other. | 2021-11-11 |
| 20210348548 | Cross-Port Air Flow To Reduce Pumping Losses - Cross-port air flow that improves engine fuel economy and reduces pumping losses during part-throttle operation can be implemented in various types of internal combustion engine systems using ports that interconnect the intake ports of different cylinders, thus allowing different cylinders to share combustion air. Cross-port air flow is commenced during part-throttle engine operation to disrupt the primary combustion air flow from each throttle to its associated cylinder, which reduces charge density and engine power. The engine compensates for the reduced power by incrementally opening the throttles, thus increasing the primary combustion air flow, reducing pumping losses and improving fuel economy. | 2021-11-11 |
| 20210348549 | ELECTRIC POWER DISSIPATER FOR ELECTRICALLY-ACTUATED TURBOCHARGER - An electric power dissipater assembly for an electrically-actuated turbocharger that includes: a power switch configured to be electrically connected to an electric power output of an electrically-actuated turbocharger; at least one resistor that is electrically connected to the power switch such that, when the power switch is in a closed position and connected to the electric power output, the at least one resistor is electrically coupled to the electric power output so that electric power provided by the electrical power output is received at and dissipated by the at least one resistor; a controller that controls whether the power switch is in the closed position or an open position; and a substrate that is physically coupled to the at least one resistor and that includes a coolant path that is used to cool the at least one resistor when coolant is received within the coolant path. | 2021-11-11 |
| 20210348550 | HYDRAULIC CONTROL VALVE FOR A LONGITUDINALLY ADJUSTABLE CONNECTING ROD WITH AN END-FACE CONTROL PISTON - A longitudinally adjustable connecting rod for a piston engine, where the connecting rod includes a first connecting rod end for receiving a piston pin and a second connecting rod end for receiving a crankshaft journal, where the distance between the piston pin and the crankshaft journal is adjustable in the longitudinal direction (A) of the connecting rod by way of a hydraulic control device with a hydraulic control valve. The hydraulic control valve comprises a control cylinder and a control slide which is guided in a slidable manner in the control cylinder and which can be pressurized, and at least one outlet valve which can be actuated by the control slide. The control slide comprises a control piston which is arranged on the end face, with a control pressure surface which can be subjected to the hydraulic control pressure and which defines a control pressure chamber in the control cylinder. The use of such a longitudinally adjustable connecting rod with a hydraulic control device in a piston engine as well as a corresponding piston engine is also provided. | 2021-11-11 |
| 20210348551 | LENGTH-ADJUSTABLE CONNECTING ROD WITH REDUCED-MASS OUTLET VALVE - A length-adjustable connecting rod for an internal combustion engine, where the connecting rod includes at least one switchable outlet valve for opening and closing a pressure chamber, where the outlet valve comprises a valve body and a closing body that is operatively connected to the valve body, and a closing mechanism is present acting upon the closing body for directly moving the closing body and indirectly moving the valve body from a closed to an open position or vice versa. Such an outlet valve is to be configured to be operable. For this purpose, this closing body has a mass which is smaller than the volume defined by the envelope contour of the closing body multiplied by the density of steel (7.85 g/mm | 2021-11-11 |
| 20210348552 | LONGITUDINALLY ADJUSTABLE CONNECTING ROD WITH MASS-OPTIMIZED CONTROL SLIDE - A longitudinally adjustable connecting rod with a hydraulic control device for effecting a change in the effective length of the connecting rod is provided. The hydraulic control device comprises a hydraulic control valve which comprises a hydraulically actuatable control slide that is preloaded by way of a control slide spring, and two outlet valves which can be actuated by the control slide by way of two control contours arranged at a distance from one another. The control slide comprises a low-pressure section with a low-pressure piston for hydraulically actuating the control slide. For optimizing the control slide for such a longitudinally adjustable connecting rod, the two control contours are arranged together in a high-pressure section of the control slide which is arranged on one side of the low-pressure section and separated therefrom by way of a sealing section disposed therebetween. The control contours each comprise a closure region with control cams and an opening region adjoining the control cams. The closure region has a smaller cross-section than the opening region. The mass of the section of the control slide disposed between the two closure regions corresponds at most to 0.95 times the envelope volume of this section multiplied by the density of steel (7.85 g/mm | 2021-11-11 |
| 20210348553 | METHOD AND SYSTEM FOR HYBRID OPPOSED PISTON INTERNAL COMBUSTION ENGINE WITH VOLUME SCHEDULING AND IGNITION TIMING CONTROLS - A method and system for a hybrid opposed piston engine with dynamic controlling of the combustion volume and power output is provided. The method includes using a control system to control a phasing of opposed pistons for achieving a desired combustion volume during a combustion cycle. The control system can control an activation of an ignition of the hybrid opposed piston engine, such as to activate the ignition when a desired condition is present in the combustion chamber. Various embodiments of the hybrid opposed piston engine are further provided. | 2021-11-11 |
| 20210348554 | Energy Recovery System - An energy storage and retrieval system is disclosed. The system includes a heat generating layer for generating thermal energy based on combusting a combustible substance and a thermal energy storage layer located to receive thermal energy from the heat generating layer. The thermal energy storage layer includes a thermal energy storage material to store thermal energy. The system also includes a thermal energy retrieval layer thermally connectable to the thermal energy storage material and configurable to retrieve thermal energy from the thermal energy storage layer. | 2021-11-11 |
| 20210348555 | HIGH PRESSURE RATIO GAS TURBINE ENGINE - A gas turbine engine ( | 2021-11-11 |
| 20210348556 | GEARED TURBOFAN ENGINE WITH A HIGH RATIO OF THRUST TO TURBINE VOLUME - A gas turbine engine turbine has a high pressure turbine configured to rotate with a high pressure compressor as a high pressure spool in a first direction about a central axis and a low pressure turbine configured to rotate with a low pressure compressor as a low pressure spool in the first direction about the central axis. A power density is greater than or equal to about 1.5 and less than or equal to about 5.5 lbf/cubic inches. A fan is connected to the low pressure spool via a speed changing mechanism and rotates in the first direction. | 2021-11-11 |
| 20210348557 | Gas Turbine Power Generation Systems Using Hydrogen-Containing Fuel Produced By A Wave Reformer And Methods Of Operating Such Systems - An improved power generation system and methods of its operation are provided, wherein the system combines: (i) a wave reformer, (ii) an optional second wave rotor, and (iii) a gas turbine in a flexible range of novel designs. Such a hybrid power generation system can thermally crack or decompose hydrocarbon fuel to produce a high-pressure fuel product, including mainly hydrogen and lead to a higher thermal efficiency than existing engines with low to no direct emission footprint. | 2021-11-11 |
| 20210348558 | HIGH PRESSURE LIQUID AIR POWER AND STORAGE - Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. The process of liquefying the gas may be powered with electric power from the grid, for example, and the heat engine may be used to generate electricity. Hence, in effect these apparatus, systems, and methods may provide for storing electric power from the grid and then subsequently delivering it back to the grid. | 2021-11-11 |
| 20210348559 | METHOD FOR PREPARING A SUPPORT AND FOR ACOUSTIC MANAGEMENT ON A TURBINE ENGINE OR A NACELLE - The invention relates to acoustic management, on an aircraft turbomachine ( | 2021-11-11 |
| 20210348560 | LOW EMISSIONS COMBUSTOR ASSEMBLY FOR GAS TURBINE ENGINE - A combustor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a combustion chamber, and a fuel injector assembly in communication with the combustion chamber that has a swirler body situated about a nozzle to define an injector passage that converges to a throat. The throat is defined at a distance from the combustion chamber. The nozzle includes a primary fuel injector and an array of secondary plain jet fuel injectors. | 2021-11-11 |
| 20210348561 | MODERATE PRESSURE LIQUID HYDROGEN STORAGE FOR HYBRID-ELECTRIC PROPULSION SYSTEM - A turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes, a liquid hydrogen fuel storage tank that is configured to maintain the liquid hydrogen fuel at a pressure greater than an external pressure and less than 20 bar, an electric machine that is in thermal communication with a liquid hydrogen fuel flow from the liquid hydrogen fuel storage tank, the liquid hydrogen fuel flow is configured to maintain at least a component of the electric machine at an operating temperature below an ambient temperature, and a fuel system that is configured to receive gas hydrogen fuel flow and communicate the gas hydrogen fuel flow to a power generation device. | 2021-11-11 |
| 20210348562 | THERMAL BARRIER COATING WITH REDUCED EDGE CRACK INITIATION STRESS AND HIGH INSULATING FACTOR - A thermal barrier coating disposed on a substrate comprising a plurality of surface features formed on the substrate proximate an inner side of the substrate, each of the plurality of surface features comprising a metallic column having a top with rounded edges; a dense layer disposed in a valley located between each of the plurality of surface features, and the dense layer disposed on the top and covering the rounded edges; a thermally insulating topcoat disposed over the plurality of surface features. | 2021-11-11 |
| 20210348563 | SHROUDED AIRCRAFT ENGINE SEAL CARRIER - A seal configuration for an aircraft engine includes a ring shaped sealing component defining an axis. A carrier is disposed radially outward of the ring shaped sealing component and supports the ring shaped sealing component. A housing includes a shroud portion. The shroud portion fully surrounds the carrier and is maintained in a static position relative to the carrier via a bellows spring and a plurality of rotation inhibiting features. Each rotation inhibiting feature in the plurality of rotation inhibiting features includes a tab protruding radially outward from the carrier and received in a slot intruding into the shroud portion. | 2021-11-11 |
| 20210348564 | ENGINE BLEED POWER RECOVERY SYSTEMS AND RELATED METHODS - Engine bleed air power recovery systems and related methods are disclosed. An example power recovery system for an aircraft engine includes a power recovery turbine coupled to aa shaft-driven device. A bleed air valve coupled between the power recovery turbine and a bleed air source. A controller configured to operate the bleed air valve to allow bleed air to flow to the power recovery turbine when the aircraft engine operates in a predetermined mode of operation. | 2021-11-11 |
| 20210348565 | GAS TURBINE ENGINE WITH SPEED SENSOR - A gas turbine engine includes, among other things, a fan, a fan drive gear system that is coupled with the fan and a fan drive input shaft, a compressor section that includes a first compressor and a second compressor, and a turbine section. The turbine section includes a first turbine coupled with a first shaft and a second turbine coupled through a second shaft to the second compressor. A bearing supports the fan drive input shaft. The bearing is located proximal to, and radially spaced from, a forward end of the first shaft. The bearing includes a speed sensor target that is rotatable with the forward end and that defines a rotation path. A speed sensor probe is situated proximal to the rotation path and is operable to read the speed sensor target. | 2021-11-11 |
| 20210348566 | TURBOJET WITH STEP-DOWN MECHANISM - Turbojet engine includes a fan, a compressor, a combustion chamber, and a turbine configured to rotatably drive the fan via a first reduction gear and the compressor via a second reduction gear, in which an outlet of the first reduction gear is rotatably coupled to an inlet of the second reduction gear by a reduction shaft, the reduction shaft being supported by a bearing arranged between the first reduction gear and the second reduction gear. | 2021-11-11 |
| 20210348567 | ADAPTIVE BOOSTING ALGORITHM-BASED TURBOFAN ENGINE DIRECT DATA-DRIVEN CONTROL METHOD - The present invention belongs to the technical field of control of aero-engines, and proposes an adaptive boosting algorithm-based turbofan engine direct data-driven control method. First, a turbofan engine controller is designed based on the Least Squares Support Vector Machine (LSSVM) algorithm, and further, the weight of a training sample is changed by an adaptive boosting algorithm so as to construct a turbofan engine direct data-driven controller combining a plurality of basic learners into strong learners. Compared with the previous solution only adopting LS SVM, the present invention enhances the control precision, improves the generalization ability of the algorithm, and effectively solves the problem of sparsity of samples by the adaptive boosting method. By the adaptive boosting algorithm-based turbofan engine direct data-driven control method designed by the present invention. | 2021-11-11 |
| 20210348568 | GAS TURBINE ENGINE COMPRESSOR PARTICULATE OFFTAKE - In general, techniques are described by which to provide a turbine engine compressor particulate offtake. A gas turbine engine comprising a compressor may perform the techniques. The compressor may comprise a plurality of compressor stages, where each compressor stage comprises a circumferential row of stator vanes and a rotor. The compressor may also include an outer circumferential casing that defines a fluidic opening within or between adjacent compressor stages. The fluidic opening may be configured to receive particulate flowing and air through the compressor and output the particulate and air outside of the gas turbine engine. The gas turbine engine also includes a combustor in series flow downstream of the compressor, and a turbine in series flow downstream of the combustor. | 2021-11-11 |
| 20210348569 | METHOD FOR CONTROLLING A TURBOMACHINE COMPRISING AN ELECTRIC MOTOR - A method for controlling a turbomachine comprising an electric motor forming a torque injection device on a high-pressure rotation shaft, in which method a fuel flow setpoint Q | 2021-11-11 |
| 20210348570 | ENGINE OPERATING DEVICE AND WORKING MACHINE - An engine operating device of a working machine includes a control assembly installed in a body, an operating lever mounted on a handle, and an operating cable. The control assembly includes a base member, a stop switch secured to the base member, and a lever member supported by the base member. The operating cable includes a throttle wire, a stop wire, and a cable tube in which the throttle wire and the stop wire are fitted. As the operating lever is moved to an engine stop position, the lever member moves to a release position, causing an engine to stop. | 2021-11-11 |
| 20210348571 | TURBO-BOOST CONTROL SYSTEM - A system and methods for a turbo-boost control system are disclosed for providing a driver of a vehicle with greater control over vehicle performance. The turbo-boost control system instructs an electronic control unit of the vehicle to increase the manifold pressure to a higher level before releasing the pressure through a waste gate so as to provide a greater power output of the engine. The turbo-boost control system includes a control module, a wiring harness, and a signal adjuster. The wiring harness couples the control module with a turbo inlet pressure sensor, a manifold absolute pressure sensor, and an electronic control unit of the vehicle. The control module sends signals to the electronic control unit based on input readings from the turbo inlet pressure sensor and the manifold absolute pressure sensor. The signal adjuster includes a rheostat that enables manual adjustment of the power output of the engine. | 2021-11-11 |
| 20210348572 | CONTROL DEVICE, ENGINE, AND CONTROL METHOD OF ENGINE - Provided is a control device configured to be able to execute, in an engine which includes a DOC, a DPF, and a temperature increase unit including an exhaust throttle valve, for increasing a temperature of each of the DOC and the DPF, a forced regeneration process of removing PM deposited on the DPF by increasing the temperature of the DPF. The control device includes a flow rate estimation part configured to estimate an intake flow rate of a combustion gas sent into a cylinder of the engine. The flow rate estimation part is configured to estimate a first intake flow rate, which is the intake flow rate in the forced regeneration process, from an opening degree of the exhaust throttle valve and a first state amount which indicates an operation state of the engine including a rotation speed of the engine, based on a first relationship representing a relationship between the first intake flow rate, and the opening degree of the exhaust throttle valve and the first state amount, in the forced regeneration process. | 2021-11-11 |
| 20210348573 | EXHAUST GAS RECIRCULATION FLOW CONTROL FOR REDUCING EMISSIONS WITH VARIABLE DISPLACEMENT INTERNAL COMBUSTION ENGINES - Managing firing fraction transitions of a variable displacement internal combustion engines by (a) avoiding transport delays in an Exhaust Gas Recirculation (EGR) feed by starting movement of an EGR valve position after a decision to transition to a new firing fraction has been made, but prior to the start of the transition and (b) adjusting the EGR valve as needed during the transition so as to maintain an EGR fraction within a predetermined range during the transition. By performing both (a) and (b), spikes of nitrous oxide (NO | 2021-11-11 |
| 20210348574 | METHOD OF CONTROLLING ENGINE COLD RESTART - A method of controlling the fuel air mixture of an internal combustion engine following a cold restart includes determining a control parameter based on the value of current coolant temperature at time of current engine start, the value of coolant temperature at time of the previous engine start, a calibratable reference temperature, the total accumulated fuel mass injected during previous engine run time, the time the engine was off before the restart, and the time the engine was run after previous start. The method also includes controlling the fuel air mixture based on said control parameter. | 2021-11-11 |
| 20210348575 | METHOD AND APPARATUS FOR DIAGNOSING AN EXHAUST GAS SENSOR - A method and a device for performing diagnostics on an exhaust gas sensor includes a series circuit of a Nernst cell and a first other cell. The exhaust gas sensor has a first, a second, and a third connection where a voltage drop can be measured between the first connection and the second connection by the Nernst cell and a voltage drop between the second connection and the third connection can be measured by the first other cell. The diagnostic method has steps for feeding a direct or alternating current into the first, second, and third connections; for directly or indirectly sensing an electrical voltage potential at at least one of the first, second, and third connections; and for evaluating the voltage potential sensed to diagnose a short circuit or an open circuit in the Nernst cell and/or in the first other cell. | 2021-11-11 |
| 20210348576 | ELECTRONIC VALVE CONTROL - A method of controlling an electronically controllable valve of an engine includes receiving, from one or more operation sensors, operation data including sensor data corresponding to a condition of the engine, control inputs indicative of operation of equipment that includes the engine, or a combination thereof. The method includes determining, using a trained valve control model, an operating characteristic of the valve at least partially based on the operation data, and generating a control signal to effect operation of the valve in accordance with the operating characteristic. | 2021-11-11 |
| 20210348577 | CONTROL DEVICE FOR FUEL INJECTION SYSTEM - A control device is included in a fuel injection system. The fuel injection system includes a low pressure pump, a high pressure pump, an accumulator, a fuel injection valve, a relief valve, and a return pipe. The high pressure pump increases a pressure of a fuel discharged from the low pressure pump and discharges high pressure fuel. The accumulator stores the high pressure fuel discharged from the high pressure pump. The relief valve is provided in a high pressure portion provided downstream from the high pressure pump and opens when a high pressure abnormality occurs in the high pressure portion. The return pipe returns the high pressure fuel in the high pressure portion to a low pressure portion provided downstream from the low pressure pump by the relief valve opening. | 2021-11-11 |
| 20210348578 | BANK TO BANK TRIMMING SYSTEM FOR A LOCOMOTIVE ENGINE - A method of bank to bank trimming for a locomotive engine during steady state operation comprises receiving a plurality of operating parameter signals, receiving a fuel quantity signal for each of a standard cylinder bank and a donor cylinder bank, providing a trim map, determining whether the engine is operating in a steady state condition based on the plurality of operating parameter signals, determining a target fuel injection duration for each of the standard cylinder bank and the donor cylinder bank if the engine is operating in a steady state condition, and adjusting an actual fuel injection duration to equal the target fuel injection duration for the standard cylinder bank and the donor cylinder bank. | 2021-11-11 |
| 20210348579 | CYLINDER HEAD AND ENGINE - The cylinder head | 2021-11-11 |
| 20210348580 | CYLINDER HEAD FOR AN INTERNAL COMBUSTION ENGINE AND METHOD FOR THE PRODUCTION THEREOF - The disclosure relates to a cylinder head for covering a combustion chamber of an internal combustion engine. The cylinder head comprises at least one material recess for heat isolation, which is formed in a main body of the cylinder head and is arranged between a fluid-guide channel and a cooling channel. The material recess can be produced e.g. directly during the shaping (e.g. casting or pressing) of the cylinder head and/or thereafter. For example, in the event that exhaust gas is guided through the fluid-guide channel, a significantly lower heat input occurs from the hot exhaust gas into the cooling fluid. In addition, the thermal decoupling via the material recess leads to the hot exhaust gas cooling to a lesser degree in the fluid-guide channel. | 2021-11-11 |
| 20210348581 | AIRCRAFT PROPULSION SYSTEM NOZZLE WITH INTERNAL FLOW PASSAGE - An assembly is provided for an aircraft propulsion system. This assembly includes a nozzle extending axially along and circumferentially about an axial centerline. The nozzle includes a nozzle panel and a nozzle fairing fixedly connected to the nozzle panel at an axial end of the nozzle. The nozzle is configured with an internal flow passage radially between the nozzle panel and the nozzle fairing. The internal flow passage extends axially within the nozzle to an outlet between the nozzle panel and the nozzle fairing at the axial end of the nozzle. | 2021-11-11 |
| 20210348582 | VALVE FOR CONTROLLING A PRESSURE DIFFERENTIAL - A valve, controlling pressure differential by regulating fluid flow between a tank and a canister, includes: a valve opening; a first moving element carrying a first sealing device making a leaktight seal and movable relative to the valve opening between a closed and an opened position allowing a first flow between the tank and the canister, through a first passageway with a first size; a second moving element carrying a second sealing device making a leaktight seal and movable relative to the valve opening between a closed and an opened position allowing a second flow between the tank and the canister, through a second passageway with a second size. The second moving element includes a central hole having a frustoconical surface partly defining the first passageway. The first sealing device has a complementary frustoconical surface cooperating with the frustoconical surface of the central hole of the second moving element. | 2021-11-11 |
| 20210348583 | AIR INTAKE DEVICE WITH A VARIABLE-LENGTH INTAKE DUCT AND A SEPARATE CENTERING DEVICE - An air intake device with a variable-length intake duct, comprising: a base duct component with a base duct, configured for the passage of intake air through the base duct component, an extension duct component with an extension duct, configured for the passage of intake air through the extension duct component, a guidance arrangement which guides the extension duct component and the base duct component to relative movement between a first operating position and a second operating position, wherein in the first operating position the base duct and the extension duct form, in mutually prolonging abutment, a continuous duct section, and wherein in the second operating position the extension duct is arranged at a distance from the base duct, and a first centering arrangement which when the duct components approach the first operating position is configured to decrease a radial distance in relation to a virtual base duct path conceived as passing centrally through the base duct between an end section of the base duct facing towards the extension duct component and an end section of the extension duct facing towards the base duct component, wherein the first centering arrangement is configured as separate from the base duct and from the extension duct. | 2021-11-11 |
| 20210348584 | NOZZLE FOR INJECTING FUEL - The present invention relates to a nozzle for injecting fuel comprising an orifice in the region of a nozzle tip for leading fuel out of the nozzle and a reception hole for receiving a nozzle needle, wherein the reception hole has a seat region for a sealing closing by a nozzle needle to enable a fuel supply to the orifice in dependence on a position of the nozzle needle, characterized in that the longitudinal axis of the orifice is directed toward a region of the reception hole that adjoins the side of the seat region remote from the nozzle tip. | 2021-11-11 |
| 20210348585 | NOZZLE WITH MICROSTRUCTURED THROUGH-HOLES | 2021-11-11 |
| 20210348586 | METHODS AND SYSTEM FOR DETECTING LATENT DEGRADATION OF ENGINE STARTING SYSTEM FEEDBACK - A method and system for operating a vehicle that includes feedback of operating status of an engine starting system is described. In one example, the method inhibits automatic engine pull-down in response to feedback from an engine starting system that does not meet expectations. The system and method may provide diagnostics for the engine starting system. | 2021-11-11 |
| 20210348587 | CONTACTING DEVICE OF A VOLTAGE TRANSMISSION DEVICE OF AN IGNITION DEVICE OF A LARGE ENGINE, SPARK-PLUG, IGNITION DEVICE AND LARGE ENGINE - A contacting device of a voltage transmission device of an ignition device of a large engine, whose cylinders have piston diameters of at least 140 mm having a first spring portion for the electrical contacting of a cable contacting piece of the voltage transmission device and a second spring portion for the electrical contacting of a spark plug connection of a spark-plug of the ignition device. The second spring portion tapers in a direction of its end, which comes to lie against the spark-plug connector of the spark-plug. The spark-plug connector of the spark-plug interacting with the contacting device includes a trough into which the contacting device can be introduced with a spring portion. | 2021-11-11 |
| 20210348588 | SPARK PLUG HEAT UP METHOD VIA TRANSIENT CONTROL OF THE SPARK DISCHARGE CURRENT - A spark plug heat up method via transient control of the spark discharge current. The high temperature plasma channel is used to heat up the central electrode, and the temperature and energy of the plasma channel are realized via transient control of the discharge current. The heating up process takes place before firing the engine, using discharge current to actively heat up the spark plug from inside. By monitoring the discharge current amplitude and discharge duration, the temperature change of the central electrode and the ceramic insulator can be carefully measured and controlled within a proper window. This method can be used to measure the heating range of the spark plug, and to prevent or remove the carbon deposit on the central electrode and the ceramic insulator generated under various engine operation conditions, such as engine cold start, full load operation, and heavy EGR condition, as well as realize self-cleaning. | 2021-11-11 |
| 20210348589 | METHODS AND APPARATUS FOR GENERATING ELECTRICITY FROM MOVING FLUID - In one aspect, a system for generating electricity based on water flow is disclosed. The system comprises a first pipe fitting, a turbine, and a second pipe fitting. The first pipe fitting couples to a pipe that supplies a fluid to a building. The turbine is in fluid communication with the first pipe fitting and rotates in response to a kinetic energy of the fluid supplied by the pipe flowing through the turbine, generates electricity in response to rotation of the turbine, and reduces a pressure of the fluid from a first pressure to a second pressure. The second pipe fitting couples the turbine to an input pipe of the building. The turbine further comprises a conversion circuit that conditions the generated electricity for consumption by the building and conveys the generated electricity to the building via one or more conductors. | 2021-11-11 |
| 20210348590 | POWERED AUGMENTED FLUID TURBINES - A powered augmented fluid turbine for generating electricity from a fluid in motion comprising: a central annular ducted channel extending between an inlet distribution header and an outlet distribution header, the channel comprising a converging section configured to accelerate the fluid received at the inlet distribution header, a turbine assembly for generating electricity, and a diffuser section configured to decelerate the fluid before it exits at the outlet distribution header; a recycle line for transporting the exiting fluid to the inlet distribution header in a closed-loop configuration, the recycle line comprising a recycle line propulsor controllable by a recycle line controller and a recycle line heat exchanger; and a compressed fluid distribution line configured to pressurize the fluid in motion by transporting a compressed fluid from a compressed fluid source to the inlet and outlet distribution headers, the compressed fluid distribution line controllable by at least one pressure controller. | 2021-11-11 |
| 20210348591 | Rotor Blade of a Wind Power Plant with a Particle Damping Device and Method for Producing Same - A rotor blade of a wind turbine with a particle damping device having at least one cavity ( | 2021-11-11 |
| 20210348592 | COMPACT VERTICAL AXIS TURBINE - Disclosed are vertical axis turbines comprising: a turbine shaft; a plurality of helicoidal blades mounted on the turbine shaft, each blade comprising a front face and a rear face; and a plurality of venturis, each venturi comprising a channel extending through each of the plurality of blades from the front face thereof to the rear face thereof. | 2021-11-11 |
| 20210348593 | Vertical Tilting Blade Turbine Wind Mill - The Vertical Tilting Blade Turbine Windmill device is for capturing kinetic energy from the wind and is comprised of a vertical shaft having a central hub connectively attached, the central hub having a plurality of wind capture arms comprising a rotating wind capture blade having a capture surface and a slicing edge that are rotated by a rotating gear and drive gear combination connectively attached to said wind capture blades enabling a rotation of said wind capture blades wherein the wind capture blades are rotated between a blade-mode to capture the wind and a knife-mode to pass with less drag resistance through the air/wind thereby enabling an increase in the ability to capture more of the energy available in an on-coming wind stream. | 2021-11-11 |
| 20210348594 | METHOD OF MANUFACTURING A WIND TURBINE ROTOR BLADE - Provided is a method of manufacturing a wind turbine rotor blade, which method includes the steps of preparing a mold by forming a partial negative leading-edge profile in a first mold half, which partial negative leading-edge profile includes a plurality of first indentations along a leading edge region of the first mold half; forming a partial negative leading-edge profile in a second mold half, which partial negative leading-edge profile includes a complementary plurality of second indentations along a leading edge region of the second mold half; and wherein the combined shape of a first indentation and a complementary second indentation corresponds to the negative shape of a leading-edge fin that will extend radially outward from the body of the rotor. | 2021-11-11 |
| 20210348595 | FLUID TURBINE - A fluid turbine is described herein. The fluid turbine is subject to internal stresses, which can increase the frequency of maintenance or cost of construction, including fixing or replacing one or more components or increasing the amount of material used. One or more support arms of the fluid turbine can be provided in a given manner to generate a force during rotation that opposes one or more other forces, thereby reducing or eliminating the internal stresses exerted on the fluid turbine. For example, the one or more support arms can be provided in a given orientation or with given masses to generate the opposing force. In another example, the one or more support arms can be shaped or angled to generate an aerodynamic force. | 2021-11-11 |
| 20210348596 | A Method for Installing an Offshore Wind Turbine and a Substructure for an Offshore Wind Turbine - A method of installing an offshore wind turbine includes the step of raising a full-length tower for the offshore wind turbine by moving it longitudinally from a container in a substructure, the substructure being a support structure for the wind turbine, wherein the substructure is arranged with a container configured for housing a tower for the wind turbine substantially in its entirety. | 2021-11-11 |
| 20210348597 | PILE FOUNDATION AND CONSTRUCTION METHOD OF PILE FOUNDATION - A pile foundation ( | 2021-11-11 |
| 20210348598 | IRREGULAR SURFACE CLEANING SYSTEM, PROCESS, AND METHOD OF USE - An irregular surface cleaning system, process, and method of use are presented. | 2021-11-11 |
| 20210348599 | Bearing Assembly of a Rotor of a Wind Turbine - A bearing assembly of a rotor of a wind turbine, namely for mounting the rotor in a fixed housing, includes: a plurality of rotor-side axial slide bearing segments, each configured to: engage on the rotor, rotate together with the rotor, and be supported against a sliding surface of the housing; a plurality of housing-side axial slide bearing segments, each configured to: engage on the housing, be fixed together with the housing, and be supported against a first sliding surface of the rotor; and a plurality of housing-side radial slide bearing segments, each configured to: engage on the housing, be fixed together with the housing and be supported against a second sliding surface of the rotor. | 2021-11-11 |
| 20210348600 | SYSTEM FOR RETAINING A VALVE ASSEMBLY IN A CAVITY FORMED IN A CYLINDER BODY OF A COMPRESSOR AND METHOD OF USE THEREOF - A system for retaining a valve assembly in a cavity formed in a cylinder body of a compressor includes a ring having a through-hole positioned adjacent to the cavity and a cover partially inserted inside a through-hole of the ring. The cover and the ring can slide relative to each other. The position of the cover relative to the cylinder body can be adjusted by tightening a cover retainer. The cover applies a downward force on the valve assembly via a cage. The downward force is used to compress a seal located between the valve assembly and the cylinder body. A seal is positioned between the ring and the cover. The seal remains squeezed when the cover and the ring slide relative to each other. The system can be used to convert a jackbolt cage-cover assembly and may not require significant machining of the cavity to provide a surface-finish with a suitable roughness for a sealing surface. | 2021-11-11 |
| 20210348601 | COMPRESSOR DEVICE - Provided is a compressor device, including: a casing in which a motor (armature and movable element) is housed; an output shaft, which projects from the casing, and is configured to be reciprocated by drive of the motor; a piston provided to a projecting end of the output shaft; a cylinder in which the piston is slidably provided to form a compression chamber; and a cylinder head connected to the cylinder. A tubular shield corresponding to a shielding portion configured to cover the cylinder in such a manner as to be separate from the cylinder in a radial direction of the cylinder is provided on an outer periphery side of the cylinder. The cylinder, the cylinder head, and the tubular shield are coupled to be integrated. | 2021-11-11 |
| 20210348602 | ROTOR ASSEMBLY WITH REMOVABLE ROLLERS - A rotor assembly for a peristaltic pump is provided. The rotor assembly includes a hub configured to couple with a drive shaft of a pump. The hub includes at least one receiving slot that extends longitudinally along an outer surface of the hub. The rotor assembly further includes a roller assembly configured to slide longitudinally along the receiving slot to seat the roller assembly onto the hub. | 2021-11-11 |
| 20210348603 | Gas Compressor - An object of the present invention is to realize inexpensive and simple compressor number control of gas compressors. In order to achieve the above object, there is provided a gas compressor set as a master gas compressor that performs compressor number control on N slave gas compressors, the compressor including: a communication I/F that is communicable with the slave gas compressors; and a control unit. When one cycle of communication with the N slave gas compressors in N communication sets is defined as a total compressor number communication cycle, in an initial total compressor number communication cycle, in first to N | 2021-11-11 |
| 20210348604 | GAS LIFT COMPRESSOR SYSTEM AND METHOD FOR SUPPLYING COMPRESSED GAS TO MULTIPLE WELLS - A high pressure gas lift compressor system and method of using the system for supplying compressed gas to multiple wells are provided. The system includes a compressor having multiple compressor cylinders. Each cylinder has its own gas inlet line and dedicated gas outlet line that supplies compressed gas from that cylinder directly to a wellbore to provide artificial gas lift. Each cylinder also has its own control valve upstream of the cylinder to control the suction pressure to the cylinder. A desired gas flow rate to each well may be input, and the control valve is adjusted accordingly to achieve the flow rate. By inputting a flow rate for each separate cylinder, the flow rate to each well may be independently controlled. | 2021-11-11 |
| 20210348605 | COMPACT HIGH PRESSURE, HIGH LIFE INTENSIFIER PUMP SYSTEM - A pumping system pumps material or fluid downhole, for example, to perform a stimulation operation. The pumping system comprises a hydraulic pump coupled to an intensifier. The intensifier comprises a piston which allows for a small footprint as compared to an intensifier with a plunger. The hydraulic cylinder of the intensifier is protected from the corrosive, erosive and abrasive effects of the material or fluid to be pumped by one or more seals. Using the intensifier that includes a piston provides for a greater reliability of the overall pumping system as fewer strokes are required and a compact pumping system as the stroke length of the intensifier with a piston is less than the stroke length required for a plunger. | 2021-11-11 |
| 20210348606 | OIL-INJECTED MULTI-STAGE COMPRESSOR SYSTEM AND PROCEDURE FOR CONTROLLING SUCH A COMPRESSOR SYSTEM - An oil-injected multi-stage compressor system that comprises at least a low-pressure stage compressor element ( | 2021-11-11 |
| 20210348607 | AIR GAP MAGNETIC COUPLING WITH COUNTERBALANCED FORCE - A magnetic coupling assembly includes a first balancing magnet positioned and surrounding drive magnets and, across a gap, a second balancing magnet and surrounding driven magnets. The drive magnets when rotated drive the driven magnets to rotate. The balancing magnets generate a repulsive force, which counterbalances an attractive force generated by the drive magnets and driven magnets. The assembly may be utilized in a pump for contactless coupling of a motor shaft to a pump shaft. The driven side of the assembly may be hermetically sealed, such as with a liquid crystal polymer boundary interposed in the gap. | 2021-11-11 |
| 20210348608 | PROGRESSIVE CAVITY PUMP UNIVERSAL JOINT - A progressive cavity pump includes a torque input disposed on a rotational axis, a resilient stator cylinder, a screw rotor situated within the resilient stator cylinder, and a universal joint. The universal joint rotationally couples the screw rotor to the torque input, and includes a swivel block, a linkage, a universal joint coupler, and a fastener. The swivel block has opposite laterally extending trunnions. The linkage extends parallel to the rotational axis, and laterally captures the laterally extending trunnions. The universal joint coupler is disposed around the swivel block and adjacent the linkage. The fastener connects the universal joint to the swivel block. The fastener and the laterally extending trunnions cooperate to transmit torque about the rotational axis through the linkage, while permitting lateral translation of the universal joint coupler in a plane orthogonal to the rotational axis. | 2021-11-11 |
| 20210348609 | Screw compressor with sliding bearings - A screw compressor with sliding bearings includes a female rotor and a male rotor; a suction end-face of the male rotor and suction and exhaust end-faces of the female rotor are respectively provided with recessed holes, in which radial sliding bearings are arranged and matched with suction and exhaust side projecting shafts embedded; a thrust sliding bearing is arranged on an end-face of the suction side projecting shaft; passages are connected to the recessed holes are provided in the female and male rotors along the axis direction, and radial passages are provided to connect axial passages and rotor chamber. Using sliding bearings inside the rotors can simplify compressor structure and reduce occupied space and cost. Besides, the passages provided inside rotors simplify the liquid return structure of sliding bearings while cool the rotors, reduce the thermal deformation of the rotors, and improve the reliability and performance of the compressor. | 2021-11-11 |
| 20210348610 | PISTON LIMITING STRUCTURE, COMPRESSOR, AND HEAT EXCHANGE APPARATUS - Some embodiments of a disclosure provide a piston limiting structure, a compressor, and a heat exchange apparatus. The piston limiting structure includes: a cylinder, having a piston hole perpendicular to an axial direction of the cylinder and penetrating the cylinder, wherein a projection of the piston hole in a penetrating direction is circular; a piston, disposed in the piston hole and slid in the piston hole, wherein a side wall of the piston is provided with a limiting surface, and the limiting surface does not penetrate two ends of the side wall of the piston along an axial length of the piston; and a limiting member, wherein the cylinder is provided with a limiting hole penetrating from an outer wall of the cylinder to the piston hole, the limiting member is mounted in the limiting hole , and the limiting member abuts against the limiting surface. | 2021-11-11 |
| 20210348611 | DOUBLE SUCTION PUMP - A disclosed submersible pump apparatus includes a three-dimensional frame, a pump housing, a drive shaft, an impeller, and first and second motors. The impeller is mounted on the driveshaft within the pump housing and is driven by one or both of the motors. The first motor is connected to a first end of the drive shaft and the second motor connected a second end of the drive shaft. The first and second motors are hydraulic motors and in a first configuration, the first and second motors are configured to cooperatively rotate the drive shaft with hydraulic fluid supplied to and removed from the first and second motors using a parallel fluidic connection. In a second configuration, only one of the motors has a drive gear and drives the drive shaft while the second motor does not have a drive gear and acts as a frictionless bearing supporting the drive shaft. | 2021-11-11 |
| 20210348612 | ELECTRIC SUBMERSIBLE PUMP WITH DISCHARGE RECYCLE - Included are electric submersible pump assemblies, methods of use, and systems incorporating said electric submersible pump assemblies. An example electric submersible pump assembly comprises an electric submersible pump comprising a pump intake, a storage chamber in fluid communication with the discharge side of the electric submersible pump, and a tubing configured to allow for fluid communication between the pump intake and the storage chamber such that fluid may flow from the storage chamber into the pump intake. | 2021-11-11 |
| 20210348613 | Thrust Runner For Abrasion Resistant Bearing of Centrifugal Pump - A submersible well pump has a rotatable drive shaft extending through pump stages. Each of the stages has a diffuser, an impeller and a bushing fixed for non-rotation in the diffuser. A thrust member has a lower side in sliding rotating engagement with the upward facing surface of the bushing. The bushing and the thrust member are of a harder material than the diffuser and the impeller. A drive member of a softer material than the thrust member is in engagement with the thrust member and has a drive member bore through which the shaft extends. A key extends through the shaft groove, the impeller groove and the drive member groove to cause the impeller and thrust member to rotate with the shaft. | 2021-11-11 |
| 20210348614 | WATER GULPING DETECTION - A method to detect gulping in a pump driven by a motor drive to pump a liquid includes: determining a value of a work indicator corresponding to work performed by a pump pumping a liquid; comparing the value to a first threshold; changing a value of a tracking variable by a first amount if the value of the work indicator is below the threshold; changing the value of the tracking variable by a second amount if the value of the work indicator is above the threshold, wherein the first amount and the second amount have opposite signs; and determining that a gulping event occurred if an absolute value of the tracking variable is larger than an absolute value of a second threshold. | 2021-11-11 |
| 20210348615 | TURBO COMPRESSOR AND TURBO CHILLER INCLUDING THE SAME - A turbo compressor includes a housing with a refrigerant suction hole, through which a refrigerant is introduced, at a front portion thereof, and a motor case defining an accommodation space. The accommodation space includes a rotation shaft extending in a front-rear direction and a motor that is configured to rotate the rotation shaft. A first impeller is coupled to one end of the rotation shaft and a second impeller is coupled to the other end of the rotation shaft. The first impeller is configured to primarily compress the refrigerant introduced into the refrigerant suction hole. A connection passage, that surrounds the motor case extends backward from an outlet of the first impeller. The second impeller is configured to secondarily compress the refrigerant introduced through the connection passage. | 2021-11-11 |
| 20210348616 | FAN MOTOR - A fan motor includes a shroud, a rotating shaft that is disposed inside the shroud and includes a first support portion, a second support portion, and a permanent magnet mounting portion disposed between the first support portion and the second support portion, an impeller disposed at a first end portion of the rotating shaft, an air bearing that is disposed adjacent to the impeller and defines an air gap facing the first support portion, a permanent magnet disposed at the permanent magnet mounting portion between the first end portion and a second end portion of the rotating shaft opposite to the first end portion in the axial direction, and a ball bearing disposed at the second end portion of the rotating shaft and configured to rotatably support the second support portion. | 2021-11-11 |
| 20210348617 | TEMPERATURE DESTRATIFICATION SYSTEMS - A temperature destratification assembly can include an outer housing. An impeller can be positioned within the outer housing between the inlet and outlet of the outer housing. The impeller can have an impeller hub and a plurality of impeller blades extending radially outward from the impeller hub. The assembly can include an impeller motor configured to rotate the impeller blades about an axis of rotation. A stator can be positioned within the outer housing between the impeller and the outlet of the outer housing. The stator can include a plurality of vanes. The stator vanes can include an upstream edge at the upstream end of the stator, a first surface extending from the upstream edge to the downstream edge of the vane, and a second surface opposite the first surface and extending from the upstream edge to the downstream edge of vane. A plurality of the vanes can have a downstream edge at the outlet of the outer housing. | 2021-11-11 |
| 20210348618 | GAS TURBINE COMPRESSOR RADIAL DOOR BLEED VALVE - A bleed system of a gas turbine engine includes a bleed duct having a duct inlet located at a flowpath of a gas turbine engine, and a bleed outlet located outside of the flowpath, and extending circumferentially around a central longitudinal axis. A plurality of bleed doors are located at the bleed outlet and are arrayed along a circumferential length on the bleed duct. Each bleed door includes a first circumferential end, and a second circumferential end. The bleed doors are arrayed such that when the bleed doors are in a closed position the first circumferential end is located at the second circumferential end of an adjacent bleed door of the bleed doors. Each bleed door includes a pivot, such that each bleed door rotates about the pivot from the closed position covering the duct outlet to an opened position allowing a bleed airflow to pass through the duct outlet. | 2021-11-11 |
| 20210348619 | PASSIVE BLEED VALVES WITH ADJUSTABLE PRESSURE THRESHOLD - A bleed valve includes a housing with an inlet coupled to an outlet by a duct, a guide tube with an orifice fixed in the housing between the inlet and the outlet, a piston, and baffle. The piston is slideably supported on the guide tube and is movable between an open and a closed position, the duct fluidly coupling the inlet and outlet in the open position, the duct fluidly separating the inlet and outlet in the closed position. The orifice fluidly couples the inlet and outlet in the open and closed positions to move piston between the open and closed positions according to differential pressure between the bleed valve inlet and outlet. The baffle is slideably supported by the guide tube to set the differential pressure at which the piston moves between the open and closed positions. Gas turbines and differential pressure adjustment methods are also described. | 2021-11-11 |
| 20210348620 | ELECTRIC PUMP - An electric pump provided with a pump unit configured to discharge working oil by being rotationally driven by an electric motor includes: a drive shaft configured to transmit rotational driving force from the electric motor to a rotor of the pump unit; a rotation-detection shaft provided coaxially with the drive shaft, the rotation-detection shaft being configured to be rotated together with the rotor; and a rotation detector unit configured to detect rotation of the rotation-detection shaft. The rotation-detection shaft has: an engagement portion configured to engage with the rotor; and a detection-target portion facing the rotation detector unit, and an outer diameter of the detection-target portion is set so as to be larger than an outer diameter of the engagement portion. | 2021-11-11 |
| 20210348621 | SLIM FAN AND OIL BEARING STRUCTURE OF FAN - An oil bearing structure of a fan includes a shaft seat, a rotating shaft, and an oil bearing. The shaft seat includes a boss. A middle portion of the boss defines a slot. One end of the rotating shaft is inserted into the slot. Another end of the rotating shaft is a free end. The oil bearing is sleeved on an outer periphery of the rotating shaft. An axis of the rotating shaft and an axis of the oil bearing are perpendicular to the shaft seat. An effective length of the oil bearing and the rotating shaft is 50%-70% of a length of the fan. | 2021-11-11 |
| 20210348622 | Centrifugal Compressor and Diffuser - The disclosure relates to a centrifugal compressor and a diffuser; the diffuser includes a pressure drive mechanism, a first diffuser part, a second diffuser part and a movable diffuser part movable diffuser part being connected with the pressure drive mechanism and movably arranged on one of the first diffuser part and the second diffuser part; moreover, the movable diffuser part gets close to or leaves away from the other one of the first diffuser part and the second diffuser parts under the action of a pressure medium in the pressure drive mechanism so as to adjust a width of a pressure diffusion flow channel and prevent adverse phenomena such as gas flow stall and surging. | 2021-11-11 |
| 20210348623 | BLOWER - A blower according to a present embodiment includes a blower unit that has a housing on which a slit is formed to extend vertically, and a support unit that has a support pillar inserted through the slit and pivotally coupled with the blower unit to be swingable vertically. And, by forming a distance between a lower end of the slit and the support pillar in a horizontally directed state in which an airflow direction of the blower unit is in line with a horizontal direction, it is configured to make the blower unit swingable such that the airflow direction of the blower unit is directed toward a lower side below the horizontal direction. | 2021-11-11 |
| 20210348624 | VACUUM MODULATED TWO PHASE COOLING LOOP PERFORMANCE ENHANCEMENT - Embodiments disclosed herein include temperature control systems. In an embodiment, a temperature control system comprises a fluid reservoir for holding a fluid, and a spray chamber fluidically coupled to the fluid reservoir. In an embodiment, a pump is between the spray chamber and the fluid reservoir, where the pump provides the fluid to the spray chamber. In an embodiment, the temperature control system further comprises a vacuum source fluidically coupled to the spray chamber, where the vacuum source controls a pressure within the spray chamber, and where the fluid reservoir is between the vacuum source and the spray chamber. | 2021-11-11 |
| 20210348625 | FLUID PRESSURIZING STRUCTURE AND FAN USING SAME - A fluid pressurizing structure and fan using same are disclosed. The fluid pressurizing structure includes a hub having a plate portion located therearound. The plate portion has a first and a second surface provided with a plurality of first and second hollow protrusions, respectively. Each of the first hollow protrusions has a first fluid inlet and a first fluid outlet, and each of the second hollow protrusions has a second fluid inlet and a second fluid outlet. The first and second fluid outlets extend through the plate portion to communicate the first and second fluid inlets with the second and first surface, respectively. When the fan rotates, fluid drawn thereinto sequentially flows through the first fluid inlets and outlets and the second fluid inlets and outlets in a helical movement in cycles, and is therefore continuously pressurized, which facilitates reduced fan vibration and noise and fan motor power consumption. | 2021-11-11 |
| 20210348626 | PUMP PROPELLER GUARD - An improved guard for a pump propeller is described herein. The guard includes a hub that in use surrounds a drive shaft of a drive motor unit that drives the propeller. The vanes define a propeller receiving area in which the propeller is received allowing the propeller to rotate relative to the vanes, while portions of the vanes radially surround the propeller. The guard is fixed in position about the propeller to protect the propeller from debris and to prevent human contact with the rotating propeller. The guard is designed to shed weeds and other debris, and prevent weeds and other debris from becoming entangled on the guard and with the propeller. | 2021-11-11 |
| 20210348627 | Power Generation System With Rotary Liquid Piston Compressor for Transcritical and Supercritical Compression of Fluids - A system includes a rotary liquid piston compressor configured to exchange pressure between a liquid and a supercritical fluid. The rotary liquid piston compressor includes a rotor configured to exchange pressure between the liquid and the supercritical fluid as the rotor rotates. The rotor defines channels that extend through the rotor. The rotary liquid piston compressor further includes barriers configured to block mixing between the liquid and the supercritical fluid. The barriers rest within the rotor. Each channel of the channels is configured to receive a barrier of the barriers. | 2021-11-11 |
| 20210348628 | SYSTEMS AND METHODS FOR ACTIVE CONTROL OF SURFACE DRAG USING ELECTRODES - A fluid control system includes a dielectric-barrier discharge (DBD) device, and processing circuitry. The processing circuitry is configured to obtain a streamwise length scale of a fluid flowing over a surface. The processing circuitry is also configured to obtain a convective time scale of the fluid flowing over the surface. The processing circuitry is also configured to operate the DBD device, based on the streamwise length scale and the convective time scale, to adjust a flow property of the fluid. | 2021-11-11 |
| 20210348629 | FOLDABLE THREE-SECTION CLAMPING DEVICE - A foldable three-section clamping device is disclosed, comprising a first support unit, provided with a rotatable first pivot member, a first extension member extending from middle of the first pivot member, and the first support unit having a clamp for clamping at a place; a second support unit, provided with a rotatable second pivot member, and a second extension member extending from middle of the second pivot member, the first extension member and the second extension member being mutually docked and both being rotatable along the same axis; a clamping unit being disposed on the second support unit, and the clamping unit further comprising a first clamping arm, an extension member and a second clamping arm, the extension member being disposed on the first clamping arm and adjustable by sliding, the second clamping arm being disposed on the extension member and adjustable by sliding. | 2021-11-11 |
| 20210348630 | SNAP-FIT ASSEMBLY FOR SECURING ELECTRONIC COMPONENTS AT HARD-TO-REACH LOCATIONS - A snap-fit assembly that allows securely attaching and locking components to each other or to wall-like objects. The snap-fit assembly includes an electronic device with a plastic housing designed to have at the same surface a set of oppositely disposed hooks and a tab for defining an area which is shaped and dimensioned to receive a sliding mechanical bracket. The hooks guide the mechanical bracket into place and securely attach the mechanical bracket to the plastic housing, while the tab forms a stop device for the mechanical bracket, while at the same time locking into a locking opening formed at the mechanical tab. | 2021-11-11 |
| 20210348631 | Electronic Control Unit - An object of the invention is to provide an electronic control unit having a structure that suppresses corrosion of plating and completely seals the substrate side under an environment where corrosion occurs. An electronic control unit | 2021-11-11 |
| 20210348632 | Tolerance-Compensating Fastening Arrangement For Fastening A Component To A Structure - A tolerance-compensating fastening arrangement for fastening a component to a structure includes a male fastener having a fastening bolt having a serrated outer profile; and a female fastener having a socket base arranged therewithin movable along a horizontal plane and having a conical funnel to receive the bolt such that horizontal tolerances between the male and female fasteners are compensable by movement of the socket base actuated through contact of the bolt with an inner surface of the funnel; and a socket jaw arranged on the socket base and having several jaw segments arranged circumferentially around a vertical axis to form a central jaw opening configured to receive the bolt through the funnel, the jaw segments configured movable radially with respect to the vertical axis to adjust a size of the jaw opening to retain the bolt along the vertical axis via contact of the serrated inner and outer profiles. | 2021-11-11 |
| 20210348633 | PIN - A pin comprises a metal body extending along a longitudinal insertion axis (Ox) and has a first and a second end along the longitudinal axis (Ox), an upper face and a lower face opposite the upper face. The pin has two convex portions each having an inclined inner wall and an inclined outer wall, the inclined walls of each convex portion forming a ridge and extending along the longitudinal axis. At least one ridge has on its lower face a protruding blade obtained by cutting and folding the metal body along the longitudinal axis. A concave portion of the pin connects the inner walls of each convex portion via a central surface. The pin has at least one blocking member. | 2021-11-11 |
| 20210348634 | Method for Connecting a First Component to a Second Component - A method connects a first component to a second component. The first component is located at a distance to the second component. The method includes: providing a spacer element which has a sleeve-shaped section with a through-opening and an outer thread; screwing the spacer element with the outer thread into a threaded bore which is provided in the second component; screwing the spacer element into a screwed position in which the spacer element protrudes out of the threaded bore such that the spacer element bridges the distance between the first and the second component, wherein the end face of the spacer element rests against the first component side facing the second component; and clamping together the two components and the spacer element by way of a screw which is screwed into the sleeve-shaped section of the spacer element or which passes through the sleeve-shaped section of the spacer element. | 2021-11-11 |
| 20210348635 | Blind Assembly Fastener System - Disclosed are systems and methods for coupling a first panel to a second panel via a fastening system. The fastening system comprises fastener and a doghouse structure. The fastener includes a head assembly coupled to a collar. The collar is configured to pass through and to retain the second panel via an opening formed in the second panel. The doghouse structure defines a chamber that is configured to receive and secure the head assembly. The doghouse structure is positioned on the first panel and is configured to pass at least partially through the opening. | 2021-11-11 |
| 20210348636 | Blind Assembly Fastener System - Disclosed are systems and methods for coupling a first panel to a second panel via a fastening system. The fastening system comprises fastener, a doghouse structure, and a seal assembly. The fastener includes a head assembly coupled to a collar. The head assembly is configured to engage a doghouse structure positioned on the first panel and the collar is configured to pass through and to retain the second panel via an opening formed in the second panel. The seal assembly includes a seal and a seal carrier. The seal carrier is coupled to the fastener via a frangible connection. | 2021-11-11 |
| 20210348637 | Shearable Fastener Bolt And Method For Clamping Electric Wires, And Electrical Connector Comprising A Zero-Protrusion Shearable Fastener - An electric connector comprises a wall surrounding a receptacle that receives a strand of an electric wire and having a threaded hole extending through the wall and opening into the receptacle, and a fastener bolt screwed into the threaded hole and clamping the electric wire. The fastener bolt includes a bolt part having a head section, a thread section and a shearing section connecting the head section and the thread section. The fastener bolt further includes a nut part screwed onto the thread section. The shearing section is adapted to break if a predetermined fastening torque is exceeded. The thread section is hollow and has a predetermined tensile breaking strength. | 2021-11-11 |
| 20210348638 | Nut, Fastener Assembly and Fastening Method - A nut adapted to be connected with a bolt includes a through hole defining a first central axis. A first internal thread is formed on an inner peripheral surface of the through hole at a first side of a first end of the through hole. A second internal thread is formed on an inner peripheral surface of the through hole at a second side, opposite to the first side, of a second end of the through hole. The first internal thread and the second internal thread define a second central axis, distinct from the first central axis. The bolt is capable of being positioned in the through hole in a first posture in which the bolt is parallel to the first central axis, and in a second posture in which the bolt is parallel to the second central axis and engaged with the first and second internal threads. | 2021-11-11 |
| 20210348639 | BOLT PROVIDED WITH OPENINGS - Disclosed herein is a bolt provided with openings. The bolt includes a head part and a threaded part, and is fastened to a structure through the threaded part while being rotated by a tool. The bolt further includes: a coupling recess formed in the head part or the threaded part while forming a recess shape having a cross section corresponding to that of the tool, and configured to allow the tool to be coupled thereto; and one or more openings formed in portions of the coupling recess in hole shapes, and configured to expose at least portions of the tool, coupled to the coupling recess, out of the head part or the threaded part. | 2021-11-11 |
| 20210348640 | FASTENER RETAINING COMPONENT - A fastener retaining component may comprise a first elongated member. A length of the first elongated member may be greater than a diameter of a fastener receiving element of a component. The fastener retaining component may further comprise a second elongated member. A length of the second elongated member may be greater than the diameter of the fastener receiving element. The fastener retaining component may be configured to be press-fit within the fastener receiving element such that press-fitting the fastener retaining component, within the fastener receiving element, increases a tension in the fastener retaining component to cause the first elongated member and the second elongated member to engage with an inner surface of the fastener receiving element and to retain a fastener within the fastener receiving element. | 2021-11-11 |
| 20210348641 | SEALING MATERIAL, ASSEMBLY AND USE OF A SEALING MATERIAL - The invention relates to a sealing material ( | 2021-11-11 |
| 20210348642 | TAPERED FASTENER - A vibration resistant nut is provided for attaching a working surface to a threaded stud, the stud extending through a hole defined through the working surface. The nut includes an annulus for receiving the stud. The annulus includes a cylindrical portion and a tapered terminal end portion for being received in the hole. The tapered terminal end portion extends from the cylindrical portion. The tapered terminal end portion has an outer surface that narrows diametrically from the cylindrical portion. The nut includes a head extending from the cylindrical portion of the annulus opposite the tapered terminal end portion, the head having outer engagement surfaces for engaging a tool for rotation of the nut, the head having a threaded interior for engaging threads of the stud. | 2021-11-11 |
| 20210348643 | ONE-PIECE SELF-LOCKING NUT - A self-locking nut includes a main-nut body and a deformable-nut body. The main-nut body has a recess leading into an interior threaded bore forming x turns of an internal thread therein. The deformable-nut body has an outer flange and an interior threaded nore forming y turns of an internal thread therein. The outer flange of the deformable-nut body is fixed to the main-nut body such that a relief space is formed between the deformable-nut body and the recess. A ratio of x:y is about 2:1. | 2021-11-11 |
| 20210348644 | SLEEVED LUG NUT APPARATUS AND INSTALLATION TOOL - The present invention provides an improved lug nut protection system that includes a keyed lug nut and a specialty tool for installation and removal. According to a preferred embodiment, the present invention includes a protective sleeve which slides over the wheel end of a given lug nut, and which is held in place by a retaining ring or the like. According to a further preferred embodiment, the protective sleeve preferably freely rotates and prevents common tools (i.e., pipe wrenches) from removing the lug nut thus preventing theft of the wheel/tire. According to a further preferred embodiment, the lug nut of the present invention is preferably recessed within the protective sleeve and preferably includes a keyed head which requires a specialty tool to remove the lug nut. Preferably, the specialty tool of the present invention fits inside the sleeve and over the top of the custom lug nut design. | 2021-11-11 |
