16th week of 2018 patent applcation highlights part 27 |
Patent application number | Title | Published |
20180106188 | Apparatus and Method for Reducing Flow Noise in a Commercial Engine Vehicle - An apparatus for reducing flow noise in a commercial engine vehicle includes an actuator into which first compressed air generated according to operation of an accelerator pedal and second pressed air generated from an air tank of a vehicle are selectively introduced. The apparatus also includes a lift plate moving up and down in the actuator by a pressure of the first or second compressed air introduced thereinto. The apparatus also includes a waste gate valve operated by a pressure according to the up and down movement of the lift plate in the actuator, in order to bypass exhaust gas in a turbine when the waste gate valve is opened. | 2018-04-19 |
20180106189 | Water Injection Device of an Internal Combustion Engine, and Method for Operating a Water Injection Device of Said Type - A water injection device of an internal combustion engine is provided. The water injection device includes a water tank for storing water, and a delivery element for delivering the water. The delivery element is connected to the water tank. The water injection device further includes at least one water injector for injecting water. The at least one water injector is connected to the delivery element. The water injection device further includes a pressure sensor, which is arranged in a line region between the delivery element and the water injector, and a control unit, which is designed to determine, on the basis of pressure data of the pressure sensor, a formation of vapour in the aforementioned line region when the water injector is closed and the delivery element is deactivated. | 2018-04-19 |
20180106190 | APPARATUS TO OPTIMIZE COMPRESSION - The apparatus is directed toward improving compression ratios relating to the crank angle positions, generating higher variable compression during the expansion cycle. An internal combustion engine is disclosed. This invention is directed toward retaining the highest compression ratio available during the expansion cycle without increased fuel consumption. The apparatus comprising of three basic components: a conventional and eccentric half of crank pin with radially displaced centerline section, two piston rods and an articulated connecting rod end. The piston is linked to this piston rod assembly. Applied dimensions of said components provide virtual infinite variations of compression curves. | 2018-04-19 |
20180106191 | Light Weight Engine Mounted Trim Part - Engine mounted trim part for a vehicle engine comprising a fibrous carrier layer and at least one mounting system for mounting the trim part to a vehicle engine characterised in that the mounting system is built such that it can form a vibration-coupled connection upon mounting to the engine and the fibrous carrier layer is at least self-damping such that it can dampen the vibrational energy. | 2018-04-19 |
20180106192 | NOVEL MULTILOOP GAS TURBINE AND METHOD OF OPERATION THEREOF - The present disclosure relates to a novel gas turbine having applications, for example, in thermal power generation in an environmentally friendly manner. In various embodiments, the present disclosure provides a multiloop gas turbine with enhanced efficiency close to Ericsson/Carnot Cycle and a method of operating the multiloop gas turbine. | 2018-04-19 |
20180106193 | HIGH OVERALL PRESSURE RATIO GAS TURBINE ENGINE - A gas turbine engine includes a compressor section and turbine section. The gas turbine engine of the present disclosure is a relatively small gas turbine engine, configured to generate less than 2,000 horsepower during peak operations. The compressor section defines an overall compressor ratio of at least 15:1 in order to increase in overall efficiency of the gas turbine engine. | 2018-04-19 |
20180106194 | TIP TURBINE ENGINE COMPOSITE TAILCONE - A non-metallic tailcone in a tip turbine engine includes a tapered wall structure disposed about a central axis. The non-metallic tailcone is fastened to a structural frame in the aft portion of the tip turbine engine. The tip turbine engine produces a first temperature gas stream from a first output source and a second temperature gas stream from a second output source. The second temperature gas stream is a lower temperature than the first temperature gas stream. The second temperature gas stream is discharged at an inner diameter of the tip turbine engine over an outer surface of the tailcone. Discharging the cooler second temperature gas stream at the inner diameter allows a non-metallic to be used to form the tailcone. | 2018-04-19 |
20180106195 | ENERGY STORAGE VIA THERMAL RESERVOIRS AND AIR TURBINES - The present invention relates to a process of storing energy through the conversion of thermal energy and subsequent power generation by means of
| 2018-04-19 |
20180106196 | METHOD AND SYSTEM FOR SUPPLYING CHARGE PULSES TO A CHIP ZAPPER OF A GAS TURBINE ENGINE - An energy generation system for generating energy to be supplied to a chip zapping unit of for example a gas turbine engine comprises an ignition system, e.g. that of the gas turbine engine, the ignition system having an energy output and configured to supply operational energy to the energy output, and the chip zapping unit having an energy input, the energy input coupled to the energy output of the ignition system to receive the operational energy therefrom. Such an energy generation system generates the operational energy needed for the chip zapping unit directly from the ignition system thus avoiding pulse generation circuitry inside an electronic control unit. | 2018-04-19 |
20180106197 | SYSTEMS AND METHODS FOR PREDICTING FUEL CIRCUIT LEAKS - A system includes a combustor assembly which receives a fuel-oxidant mixture. The system includes a control valve which controls a fuel flow into the combustor assembly. The system includes one or more sensors which measure one or more properties. The system includes a controller communicatively coupled to the one or more sensors and the control valve. The controller receives data from the one or more sensors indicative of operating conditions of the combustor assembly. The controller determines a predicted fuel flow for a first fuel line of a plurality of fuel lines based in part on the data received from the one or more sensors. The controller calculates a difference between a commanded fuel flow and the predicted fuel flow. The controller adjusts an operation of the control valve associated with a gas turbine engine when the difference is greater than a threshold. | 2018-04-19 |
20180106198 | VARIABLE VALVE TRAIN FOR ENGINE - A variable valve train for an engine is provided that includes a plurality of electric variable valve mechanisms, a single drive circuit used to drive at least two of the plurality of electric variable valve mechanisms, and a controller provided separately from the drive circuit and configured to control the drive circuit. The drive circuit is integrated with at least one of the at least two electric variable valve mechanisms. | 2018-04-19 |
20180106199 | COMPRESSION RATIO ADJUSTMENT APPARATUS FOR INTERNAL COMBUSTION ENGINE - An object of the present invention is to provide a variable mechanism apparatus for an internal combustion engine capable of preventing a crown surface of a piston and intake and exhaust valves from interfering with each other or sufficiently acquiring an internal EGR effect during an exhaust stroke when a piston position at a compression top dead center is raised to achieve a high mechanical compression ratio. The variable mechanism apparatus is configured to set a piston position at an intake (exhaust) top dead center to a lower position than the piston position at the compression top dead center by a variable compression ratio mechanism. According thereto, the variable mechanism apparatus can prevent the crown surface of the piston and the intake and exhaust valves from interfering with each other or sufficiently acquiring the internal EGR effect during the exhaust stroke by setting the piston position at the exhaust top dead center to the low position when the piston position at the compression top dead center is raised to achieve the high mechanical compression ratio. | 2018-04-19 |
20180106200 | SYSTEM AND METHOD FOR CONTROLLING ENGINE OPERATION - A machine includes an engine and a governor operable to control an operating speed of the engine along a first droop curve such that the operating speed is a function of an operating load of the engine. The first droop curve includes a first region that defines a first slope, a second region that defines a second slope different from the first slope, and a transition point located at an intersection of the first region and the second region. The machine further includes a controller in communication with the governor. The controller is configured to determine an average operating load of the engine over a predetermined time period, adjust the location of the transition point based at least in part on the average operating load to create a second droop curve, and operate the engine based on the second droop curve. | 2018-04-19 |
20180106201 | ENGINE CONTROL IN FUEL AND/OR CYLINDER CUT OFF MODES BASED ON INTAKE MANIFOLD PRESSURE - Methods and arrangements for transitioning an engine between a deceleration cylinder cutoff (DCCO) state and an operational state are described. In one aspect, transitions from DCCO may begin with reactivating cylinders to pump air to reduce the pressure in the intake manifold prior to firing any cylinders. The number of pumping cycles, if any, is based on intake manifold absolute pressure (MAP). | 2018-04-19 |
20180106202 | Method of Determining Air Charging System Deficient State of Health during Part Load Operation - A method to diagnose post air charger compressor icing obstructions without the addition of a post compressor pressure sensor. The method detects when conditions exists for icing to occur and performs at least one icing mitigation strategy when the icing conditions exceed a predetermined icing condition threshold. | 2018-04-19 |
20180106203 | FUEL EVAPORATIVE EMISSION CONTROL DEVICE - A fuel evaporative emission control device including an electronic control unit that, when fuel tank inner pressure exceeds a first predetermined pressure, performs tank purge of closing a bypass valve and opening a sealing valve, discharging fuel evaporative gas inside the fuel tank into an air intake path of an engine in an operated state through a purge pipe and a vapor pipe, and treating the fuel evaporative gas, where, when tank purge is performed, if a first predetermined period of time passes after closing of the bypass valve without the fuel tank inner pressure falling to or below the first predetermined pressure, the sealing valve is closed and tank purge is stopped. | 2018-04-19 |
20180106204 | IN-CYLINDER EGR FOR AIR FUEL RATIO CONTROL - Air to fuel ratio management comprises sensing a power output request for the engine and determining a fuel-efficient air to fuel ratio. A current air to fuel ratio is sensed in one or both of an intake manifold and an exhaust manifold connected to the engine. An air to fuel ratio adjustment is determined based on the fuel-efficient air to fuel ratio and based on the current air to fuel ratio. An in-cylinder exhaust gas recirculation technique is selected. The in-cylinder exhaust gas recirculation technique adjusts an oxygen and particulate content of exhaust gas resulting from combustion. A number of cylinders of the multiple-cylinder engine are selected to implement the in-cylinder exhaust gas recirculation technique. The intake valves and the exhaust valves are controlled to adjust the oxygen and particulate content of the exhaust gas by applying a second compression stroke of the respective reciprocating pistons to the exhaust gas. | 2018-04-19 |
20180106205 | METHOD AND SYSTEM FOR CATALYTIC CONVERSION - Methods and systems are provided for regulating exhaust flow through an exhaust system of an engine. In one example, a method may include directing exhaust from downstream of a catalytic converter to a compressor storage tank in response to an engine air-fuel ratio deviating from stoichiometry. The stored exhaust may be released from the compressor storage tank to recirculate through the catalytic converter to atmosphere after adjusting an air-fuel ratio of the exhaust in the storage tank and when the he catalytic converter is at a target operating temperature. | 2018-04-19 |
20180106206 | HYBRID VEHICLE - In a hybrid vehicle including: an engine having an exhaust system in which a filter that removes particulate matter is provided; a motor configured to generate a driving force for the hybrid vehicle; a power storage device configured to exchange an electric power with the motor; and an electronic control unit configured to control the engine and the motor. When an accumulation amount of the particulate matter of the filter is equal to or more than a predetermined accumulation amount, the electronic control unit is configured to permit fuel cut of the engine when a temperature of the filter is lower than a predetermined temperature, and the electronic control unit is configured to prohibit the fuel cut of the engine when the temperature of the filter is equal to or higher than the predetermined temperature. | 2018-04-19 |
20180106207 | Method for Diagnosing Failure of Power Stage of Electronic Waste Gate Actuator - The present invention relates to a method for diagnosing a failure of a power stage of an electronic waste gate actuator (EWGA). According to the present invention, whether the failure of the power stage of the EWGA occurs is determined by confirming, by an engine control unit (ECU), information on the failure of the power stage transferred from an EWGA driver IC at the time of EWGA position learning, after an engine is turned off. By doing so, even when a turbo-charger is not used for a long time, whether the failure of the power stage of the EWGA occurs may be diagnosed for every driving cycle, such that a failure of the ECU may be prevented in advance and unnecessary replacement of components may be prevented, thereby decreasing maintenance costs for a vehicle. | 2018-04-19 |
20180106208 | METHOD AND DEVICE FOR ASCERTAINING A CORRECTION VALUE FOR A FUEL INJECTION QUANTITY - A method for ascertaining a correction value for a fuel metering of a fuel injector of an internal combustion engine, in which fuel is injected from a high pressure accumulator into a combustion chamber with the aid of the fuel injector, a value which is representative for a static flow rate through the fuel injector being ascertained by way of ascertaining, during at least one injection process of the fuel injector, a ratio of a pressure difference occurring in the high pressure accumulator as a result of the injection process and an associated duration which is characteristic for the injection process, and the correction value being ascertained on the basis of a comparison of the representative value with a comparative value. | 2018-04-19 |
20180106209 | METHOD AND SYSTEM FOR ENGINE STARTING CONTROL - Methods and systems are provided for restarting an engine when a high pressure fuel pump is degraded. In response to an indication of high pressure fuel pump degradation, fuel may be injected during an intake stroke, rather than a compression stroke, for a selected number of combustion events since the engine restart. By shifting to an intake stroke injection, the engine may be started even when sufficient fuel rail pressures are not available. | 2018-04-19 |
20180106210 | Oil Cooled Internal Combustion Engine Cylinder Liner And Method Of Use - An oil cooled cylinder liner, a method for cooling the same, and an opposed piston engine using the oil cooled cylinder liner are described. The cylinder liner includes a liner wall that has an inner face adjacent a piston bore and an outer face including an oil gallery surface. A plurality of grooves are disposed along the oil gallery surface. The grooves run parallel to each other and are spaced apart by bridging portions of the liner wall. At least some of the grooves have at least one fin disposed therein that runs parallel with the grooves. The grooves in combination with the fins increase surface area of the oil gallery to improve heat transfer from the liner wall to oil disposed along the oil gallery surface. | 2018-04-19 |
20180106211 | METHOD FOR MANUFACTURING ENGINE - A method for manufacturing an engine includes: preparing, as a preparing step, a cylinder head having a surface on which a ceiling surface of a combustion chamber is formed; forming, as a film formation step, a thermal insulation film on the ceiling surface; measuring, as a measurement step, a volume of the thermal insulation film; and selecting, as a selection step, from a plurality of ranks set in correspondence with compression heights of pistons, the rank of the piston to be combined with the ceiling surface, the selected rank corresponding to an amount of difference of the measured volume of the thermal insulation film from a design value of the volume of the thermal insulation film. | 2018-04-19 |
20180106212 | MANUFACTURING METHOD FOR ENGINE - A manufacturing method for an engine includes: preparing, as a preparing step, a cylinder head having a surface on which a ceiling surface of a combustion chamber is formed; forming, as a film formation step, a thermal insulation film on the ceiling surface; measuring, as a measurement step, a volume of the thermal insulation film; and selecting, as a selection step, a rank for an engine valve to be used in combination with the ceiling surface so as to correspond to an amount of difference of a measured volume of the thermal insulation film from a designed value of a volume of the thermal insulation film, the rank being selected from a plurality of ranks set in correspondence with thicknesses of umbrella portions of engine valves. | 2018-04-19 |
20180106213 | CYLINDER HEAD FOR AN INTERNAL COMBUSTION ENGINE - The invention relates to a cylinder head ( | 2018-04-19 |
20180106214 | INTAKE VALVE FAIRING FOR A CYLINDER HEAD OF AN ENGINE - An engine has a cylinder head defining an intake port with a roof defining first and second valve guide bores upstream of first and second siamesed intake valve seats for a cylinder. The head has first and second asymmetric fairings extending outwardly from the roof and positioned directly upstream of respective bores. Each fairing has an inner wall intersecting an outer wall along an upstream edge and an inclined planar roof wall extending between the inner and outer walls. A method of forming the cylinder head and engine is also provided by milling the fairings from a roof preform formed with the intake port of the head. | 2018-04-19 |
20180106215 | OPEN-FACED PISTON ASSEMBLY - The present disclosure provides an open-faced piston with a circumferential groove into which a piston ring assembly is arranged. Openings at the bottom of the circumferential groove and between a front land of the open-faced piston and the piston face are provided. The openings are arranged to allow for a combustion reaction to propagate through the volume defined between the bottom of the piston ring assembly and the piston face such that at least a portion of an air and fuel mixture located in that volume is reacted. | 2018-04-19 |
20180106216 | NACELLE OF A TURBOJET ENGINE COMPRISING AN INVERTER FLAP - A nacelle for a ducted fan turbojet engine comprising an engine. The nacelle comprises a fixed cowl, an upstream wall bounding off, with the engine, a working section for a secondary flow, a movable cowl with an interior wall and an exterior wall, and movable in translation between a closing position where the exterior wall adjoins the fixed cowl and the interior wall prolongs the upstream wall, and an opening position where the exterior wall is distant from the fixed cowl so as to open a window and the interior wall is distant from the upstream wall, an inverter flap between the interior wall and the exterior wall mounted to be free in rotation about an axis of rotation situated on the interior wall and a drive mechanism for moving the movable cowl. | 2018-04-19 |
20180106217 | MANDREL ASSEMBLY AND METHOD OF MANUFACTURING SOLID ROCKET PROPELLANT GRAIN USING THE SAME - The present disclosure relates to a dismantleable mandrel assembly and a method of molding solid propellant grains with deep fin cavities whose major transverse dimensions are larger than casing opening dimensions in a monolithic rocket motor. The mandrel assembly comprises a base mandrel, a core mandrel insertable into the base mandrel and a plurality of fin molds attachable onto the base mandrel in a circular pattern about the motor axis. The plurality of longitudinal fin cavities is configured with forward swept leading and trailing edges. The manufacturing technique involves assembling and disassembling the mandrel components before propellant casting and after propellant curing respectively in a specific sequence. With minimum number of components and critical joints the method assures reduced quantum of explosive hazard in propellant grain manufacturing for high performance solid rocket motors. | 2018-04-19 |
20180106218 | INTEGRATED THRUSTER - A thruster has an additively-manufactured housing that includes an integrally-formed nozzle with a burst disk in it. The housing is part of a casing that surrounds and encloses a propellant that is burned to produce pressurized gases that burst the burst disk and produce thrust. The thruster may be placed in a receptacle that defines a recess for receiving the thruster. The receptacle also may be additively manufactured. The thruster and the recess both may be cylindrical, with the housing being closely fit with the cylindrical walls of the receptacle. This may allow some of the structural loads on the housing, such as loads produced by the combustion of the propellant, to be transferred to the adjoining walls of the receptacle. This enables the housing to have less structural strength than if it were to have to contain the pressure from the propellant all on its own. | 2018-04-19 |
20180106219 | PROPULSION SYSTEM - A propulsion system is provided. The propulsion system provides a single or array of low power pulsed lasers used to accelerate water vapor or other molecules to relativistic velocities using the Wakefield effect. The present invention provides a thrust plate having one or more thrust channels operatively associated with the single or array of low power pulsed lasers, wherein the resulting electric field of the Wakefield effect accelerates the water or molecular ions at high speeds out of the thrust plate through the thrust channels. | 2018-04-19 |
20180106220 | FULL-CLOSE ABNORMALITY DIAGNOSIS APPARATUS FOR FLOW CONTROL VALVE - An EGR valve includes a valve seat in a flow passage of a housing, a valve element seatable on the valve seat, a rotary shaft to open or close the valve element, a motor and a speed reducing mechanism, a return spring urging the valve element in a valve closing direction, and an opening-degree sensor to detect an opening degree of the valve element. An electronic control unit (ECU) diagnoses abnormality due to lodging of foreign matter between the valve seat and the valve element during full close. When driving the motor to urge the valve element in the valve closing direction during full close of the valve element, the ECU determines the EGR valve to be abnormal because of lodging of foreign matter if a difference between a value detected by the opening-degree sensor and a predetermined reference value is larger than a first determination value. | 2018-04-19 |
20180106221 | EXHAUST GAS RECIRCULATION COOLER FOR AN INTERNAL COMBUSTION ENGINE - An exhaust gas recirculation cooler may include a housing having a coolant inlet opening into an inlet region and a coolant outlet, and a plurality of cooling tubes arranged in the housing next to one another to form a tube row, each cooling tube connecting an exhaust gas inlet and outlet. At least two tube rows with one arranged on top of another and spaced from each other may form a tube block. Exhaust gas may be flowable through an inside of each cooling tube, and a coolant flow may be able to be circulated outside of the cooling tubes within the housing and flowable through an annular space enclosing the tube block in a circumferential direction. A flow guide arrangement for guiding the coolant in the interior of the tube block may be arranged in the housing lying against at least portions of one of the tube rows. | 2018-04-19 |
20180106222 | DEVICE FOR THE TREATMENT AND ELIMINATION OF BACTERIA IN HYDROCARBON FUELS AND PROCESS FOR ITS MANUFACTURE AND SURFACE ACTIVATION - This invention consists of a device for the treatment and elimination of bacteria in combustible hydrocarbons, whose function is to ensure the purity of said fuels. The elimination of bacteria takes place catalytically thanks to the alloy of which its inner part is composed and the interaction with the casing containing it. This device has the advantage of having a more intense effect of eliminating microbiological contamination than other technologies. It is installed inside the fuel tanks. Its design allows that its presence in the tank does not cause damage to the components that may be inside it. | 2018-04-19 |
20180106223 | System and Method for Improving Fuel Mileage of Internal Combustion Engine - A modification to the air input ducting of an internal combustion engine. The engine can be gasoline, diesel or other fuel and can be located in any type of vehicle including automobiles, trucks, boats, ships, aircraft and any other vehicle. The invention includes mounting layers of very strong permanent magnets with interspersed iron or other metal structures in the air intake of the engine. The magnets are placed so that the intake air must flow between them through the strong magnetic field and at the same time contact the iron or other metal which is generally a surface layer on each magnet. The total amount of airflow is not impeded and is almost the same as when the magnets are not present. Pollution is also greatly reduced. | 2018-04-19 |
20180106224 | AUXILIARY POWER UNIT INLET ASSEMBLY WITH FILTER - An inlet assembly for an auxiliary power unit for an aircraft, including a duct configured to provide fluid communication from an environment of the aircraft to an inlet of an engine of the auxiliary power unit, and a filter received in and extending across the duct. The filter includes a first filter portion permeable to air, positioned across only part of the duct and defining a transverse edge in the duct; a second filter portion permeable to air and extending from the transverse edge to an end downstream of the transverse edge, and a collection member impermeable to water. The collection member extends between the downstream end and a duct wall. The first and second filter portions are non-parallel and the second filter portion and the collection member are non-parallel. An auxiliary power unit assembly and a method of feeding air to an internal combustion engine are also discussed. | 2018-04-19 |
20180106225 | AUXILIARY POWER UNIT INLET ASSEMBLY WITH PARTICLE SEPARATOR - An inlet assembly for an auxiliary power unit for an aircraft, including a particle separator and a plenum having first and second inlets. A first duct configured to deliver air to an engine of the auxiliary power unit is in fluid communication with an outlet of the plenum. A second duct configured to deliver air to a compartment containing the auxiliary power unit is in fluid communication with the outlet of the plenum. The assembly is selectively configurable between a first configuration where the plenum is in fluid communication with the environment of the aircraft through the second inlet and through the particle separator, and a second configuration where the plenum is in fluid communication with the environment of the aircraft through the first inlet independently of the particle separator. An auxiliary power unit assembly and a method of feeding air to an auxiliary power unit assembly are also discussed. | 2018-04-19 |
20180106226 | Fuel Supply System - A fuel supply system having a low pressure region, a pumping device to deliver fuel from the low pressure region to a high pressure region. In the high pressure region between the pumping device and injectors there is a pressure storage system that is permanently under high pressure. The pressure storage system has a plurality of distributor units each with at least three connections connected in series. A respective injector connection of each distributor unit is connected to at least one injector each via a high pressure line that is under high pressure at times dependent on the injection cycle. Each distributor unit of the pressure storage system is assigned an individual leakage detection device. Each distributor unit is assigned a non-return valve, which allows a leakage flow starting out from the respective distributor unit in the direction of the pumping device. | 2018-04-19 |
20180106227 | FUEL INJECTOR MOUNTING SYSTEM FOR MOUNTING AN INJECTOR TO AN ENGINE CYLINDER LINER - Technology is provided for a fuel injector mounting system for mounting an injector to an engine cylinder liner. The system includes an injector adapter having an adapter body including a first end portion threaded for engagement with a cylinder liner and an injector port formed in the adapter body opposite the first end portion. The injector port includes a plurality of concentric bores configured to receive the proximal end portion of an injector. A flange extends transversely from the adapter body and a collar engages a portion of the injector and connects to the flange to retain the injector in the adapter. A transverse passageway extends through a sidewall of the adapter body and intersects the injector port and an annular fitting is disposed on the injector adapter for fluid communication with the transverse passageway. An injector support bracket attaches a distal end portion of the injector to the engine. | 2018-04-19 |
20180106228 | GASKET FOR FUEL INJECTOR - A gasket for a fuel injector includes: an annular tube having an opening, a first surface, and a second surface, in which the second surface is disposed opposite to the first surface of the annular tube; and an inner portion and an outer portion connecting the first surface with the second surface. The inner portion and the outer portion include a flexible material and interact with a fluid filled within the annular tube via the opening of the annular tube. | 2018-04-19 |
20180106229 | FUEL INJECTOR - A fuel injector for delivering fuel to an internal combustion engine includes a nozzle having a valve needle which is movable with respect to a valve needle seat. The valve needle travels through a range of movement between a closed position and an open position to control fuel delivery through at least one nozzle outlet. The valve needle cooperates with a needle sleeve or a control member which is located in a piston guide. The valve needle is movable relative to the needle sleeve or the control member. The needle sleeve or the control member is movable relative to the piston guide. | 2018-04-19 |
20180106230 | System and Method for Starting a Multi-Engine Power System - A power system is provided that includes a plurality of engines and a compressed air source in communication with the plurality of engines and configured to assist in starting the engines. A plurality of engine controllers are provided each associated with a respective one of the plurality of engines. The engine controllers are communicatively linked with each other and upon receipt of a signal to start the plurality of engines are configured to stagger the starts of the plurality of engines according to a predetermined order and to apply an air start system charge delay timer before starting an individual engine when the compressed air source is in a first state in which the compressed air source is unable to assist starting at least one of the plurality of engines. | 2018-04-19 |
20180106231 | Electronic Control for Engine Block Heater Elements - An electronic control for engine block heater elements for heating an engine to an engine ready temperature includes a power input, a power output, and a controller. The controller includes a clock for keeping a time and a temperature sensor for sensing a temperature. The controller is configured for controlling the power from the power input to the power output in at least two modes of operation for heating the engine to the engine ready temperature. The second mode of timed ready is where the power from the power input to the power output is connected at a pre-calculated time interval for the purpose of making ready the subject vehicle for starting at the desired start time as set by the user. The third mode of maintain ready is where the power from the electrical outlet to the engine block heater element is regulated to maintain the engine ready temperature. | 2018-04-19 |
20180106232 | CONTROL DEVICE - The invention, while reducing noise, suppresses a load increase in a processor and a delay in drive control. An engine control unit includes a processor, a driving circuit including a switching element to drive a load such as a fuel injector and an ignition device, and a communication circuit that transmits control signals from the processor to the driving circuit via serial communication. The control signals each include a command frame for controlling the driving circuit and a data frame for driving the load. If a predetermined bits in each of the data frames received from the processor at predetermined time intervals are determined to be the same twice in succession, the engine control unit changes a state of a driving signal ‘Drive’ for driving the load and thereby changes an operating state of the switching element. | 2018-04-19 |
20180106233 | FLOATING POWERHOUSE - Systems and methods related to floating powerhouse for hydropower turbine systems are presented. A turbine system may be coupled to floating powerhouse that can include a floating platform. A pressurized water delivery system can be coupled to the floating powerhouse and can accommodate vertical and/or horizontal movement of the floating power house. The pressurized water delivery system can include a segmented penstock coupling the turbine to an intake, and individual segments of the penstock can be free to rotate about a substantially horizontal axis, such that in response to variations in a tailwater height, the floating platform rising and falling does not disrupt fluid flow from a fluid source. | 2018-04-19 |
20180106234 | Ship Screw, Pump Screw or Turbine Screw - A ship screw, pump screw or turbine screw for use under water or another liquid, comprising a front side and a rear side, wherein water or another liquid is forced from the front side to the rear side in use, and comprising a hub and at least two blades extending from said hub, wherein the blades are substantially helical/spiral shaped, their effective surface area increasing from the front side toward the rear side. | 2018-04-19 |
20180106235 | DAMP-PROOF LAYER FOR CREATING A SEAL FOR A POTENTIAL ENERGY STORE, AND METHOD FOR ASSEMBLING A SEAL FROM DAMP-PROOF LAYERS FOR A POTENTIAL ENERGY STORE - A damp-proof layer is provided for creating a seal for a potential energy store. The damp-proof layer has a supporting structure of wire ropes arranged next to one another or sections of one or more wire ropes arranged next to one another. At least parts of the plane in which the wire ropes lie, or at least parts of a plane running parallel thereto, form a fluid-tight surface or layer, in which the wire ropes, at the ends of the damp-proof layer, are each secured to an anchor piece for anchoring the damp-proof layer or are guided around the anchor piece. Between each two anchor pieces there is in each case arranged an elastic element. A seal is assembled from damp-proof layers on a potential energy store with a hydraulic cylinder, in which there is arranged a piston for storing energy in the form of potential energy of the piston. | 2018-04-19 |
20180106236 | SUBMERSIBLE POWER GENERATION PLATFORM - Discloses herein a submersible power generation platform. The submersible power generation platform a power generation unit ( | 2018-04-19 |
20180106237 | ATTACHMENT METHODS FOR SURFACE FEATURES OF WIND TURBINE ROTOR BLADES - The present disclosure is directed to methods for attaching a plurality of surface features to a rotor blade of a wind turbine. Such methods may include direct molding of the surface features to the rotor blade, bonding arrays of connected components to the rotor blade and subsequently removing connections between components, as well as using a flexible template with or without a tinted adhesive. | 2018-04-19 |
20180106238 | IMPROVED WIND TURBINE SUITABLE FOR MOUNTING WITHOUT A WIND TURBNIE TOWER - This invention discloses an improved wind turbine suitable for mounting without a wind turbine tower. The wind turbine is based on a rotor with appropriately selected blades. A nozzle and diffuser in the wind flow increase the amount of wind energy available to the rotor. The rotor is interruptibly connected with one or more of a plurality of generators which allows generation at a wide range of wind speeds. The rotor is also interruptibly connected with a co-axial flywheel which allows for storage or use of rotational energy as needed by the availability of wind energy. One or more wind turbines can be grouped together in a common housing. Electricity can also be generated by means of stored energy or other motive source. The lack of a wind turbine tower and the general compact design allows the wind turbine to be used in close proximity to or on buildings. | 2018-04-19 |
20180106239 | Wind Warrior - The Wind warrior is a wind turbine that is situated in the wind, horizontally so winds from all directions affect it equally without, the need for a rudder type directional control. The Wind Warrior has several veins, similar to umbrellas, at the ends of arms (trusses) that are connected to a center mandrel that turns with the arms as the wind drive; the veins attached to the outer ends of the arms. The wind acts upon the face side of the veins to spin them, transferring the wind force through the arms to the mandrel but partially closing the veins as they rotate into a position where the wind acts upon their back side. Drag is reduced due to the veins partially closing as they rotate until the face side is again exposed to the force of the wind and is opened and driven thereby to rotate the mandrel. | 2018-04-19 |
20180106240 | System and Method for Monitoring and Controlling Wind Turbines within a Wind Farm - In one aspect, a system for monitoring and controlling the operation of wind turbines located within a wind farm may generally include first and second wind turbines. The first wind turbine may include a first turbine controller configured to monitor an operating parameter(s) associated with the first wind turbine and provide a first control interface for controlling the operation of the first wind turbine. The second wind turbine may include a second turbine controller configured to monitor an operating parameter(s) associated with the second wind turbine and provide a second control interface for controlling the operation of the second wind turbine. The system may also include a secondary computing device coupled to the second turbine controller. The second turbine controller may be configured to provide the secondary computing device access to the first control interface in order to allow the operation of the first wind turbine to be controlled. | 2018-04-19 |
20180106241 | STIRLING ENGINE FOR AN EMISSION-FREE AIRCRAFT - Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes an aircraft thruster structured and arranged to generate thrust force on the aircraft, an aircraft lift device structured and arranged to generate lift on the aircraft, and a heat engine, which is structured and arranged to convert thermal energy into kinetic energy to drive the aircraft thruster, that includes at least one flat-plate Stirling engine drivable by solar thermal radiation. | 2018-04-19 |
20180106242 | SYSTEM AND METHOD FOR CONVERTING HEAT TO KINETIC ENERGY - A system for converting heat to kinetic energy is disclosed. The system may include a heat source, bimetallic bands and wheels that may support the bimetallic bands. The bimetallic bands may be heated by the heat source and may rotate the wheels. The rotation of the wheels may then be used to convert the kinetic energy to power. | 2018-04-19 |
20180106243 | CHARGE SEPARATION MECHANISM - A method of producing a charge separation in a plasma having a low particle density which comprises a plurality of electrons and a plurality of positive ions. The method includes generating a magnetic field and passing the plasma having a low particle density along a first axis through the magnetic field. The magnetic field is generated having a component which is perpendicular to the first axis and is configured so as to deflect the plurality of electrons from the first axis and allow the plurality of positive ions to travel substantially undeflected along the first axis. Also provided is a magnetohydrodynamic generator and a low earth orbit thruster making use of the charge separation mechanism. | 2018-04-19 |
20180106244 | ELECTRIC PUMP - An electric pump includes a rotor ( | 2018-04-19 |
20180106245 | DRIVING SYSTEM FOR PIEZOELECTRIC PUMP - A driving system includes a voltage conversion module, a frequency control module, a voltage switching module and a detecting module. The voltage conversion module is used for converting a first DC voltage into a second DC voltage. The frequency control module searches a resonant working frequency of a piezoelectric actuator through circuit oscillation and generates a switching signal according to the resonant working frequency. According to the switching signal, the voltage switching module converts the second DC voltage into an AC voltage so as to drive the piezoelectric actuator. The detecting module includes a gas pressure sensor and a microcontroller. The gas pressure sensor generates a detected gas pressure value according to a result of detecting a gas pressure of the piezoelectric pump. The microcontroller controls the voltage conversion module to adjust the output voltage. Consequently, the gas pressure of the piezoelectric pump is adjusted. | 2018-04-19 |
20180106246 | PERISTALTIC PUMP - A peristaltic pump having at least first, second, and third stages is provided. The peristaltic pump includes a plunger, inlet and outlet valves, a spring, and an actuator. The plunger actuates toward and away from a tube, the inlet valve is upstream of the plunger, the outlet valve is downstream of the plunger, the spring biases the plunger toward the tube, and the actuator mechanically engages and disengages from the plunger. In the first stage, the inlet valve is opened and the plunger is actuated from the tube, in the second stage, the inlet valve is closed, the plunger is actuated toward the tube, and the actuator is mechanically disengaged from the plunger, and in the third stage, the outlet valve is opened. In the third stage or in a fourth stage, the actuator actuates the plunger toward the tube to discharge fluid downstream past the outlet valve. | 2018-04-19 |
20180106247 | METHOD OF DETERMINING OUTPUT FLOW RATE OF GAS OUTPUT BY FLOW RATE CONTROLLER OF SUBSTRATE PROCESSING APPARATUS - In a method of an embodiment, a pressure sensor is selected from first and second pressure sensors according to a set flow rate. A measurable maximum pressure of the second pressure sensor is higher than a measurable maximum pressure of first pressure sensor. The target pressure of a chamber is determined according to the set flow rate. Until the pressure of the chamber reaches the target pressure after gas is started to be output from the flow rate controller to the chamber at an output flow rate according to the set flow rate and a pressure controller provided between the chamber and an exhaust apparatus is closed, the pressure of the chamber is measured by the selected pressure sensor. The output flow rate of the flow rate controller is determined from a rate of rise of the pressure of the chamber. | 2018-04-19 |
20180106248 | Condensate pump - An improved condensate pump for use with items that exhibit condensation having an audible alarm and concentrating flange. | 2018-04-19 |
20180106249 | CONTROL SYSTEM FOR SUPPLYING FUEL TO ENGINE - A control system for a fuel supply module of an engine is provided. The control system includes a first fuel flow sensor in a fuel supply line which detects a first amount of fuel flowing through the fuel supply line and generates a first signal indicative of the first amount of fuel. The control system includes a second fuel flow sensor in the fuel return line which detects a second amount of fuel flowing through the fuel return line and generates a second signal indicative of the second amount of fuel. A controller receives the first signal and the second signal. The controller calculates a difference between the first signal and the second signal. The controller commands operation of the fuel supply module to supply a fuel flow to the engine independent of the engine speed, based on the difference between the first signal and the second signal. | 2018-04-19 |
20180106250 | COATINGS FOR REDUCING WEAR ON ROD PUMP COMPONENTS - A pump for an oil and gas well includes a barrel with a surface configured to contact oil and gas well fluid. The pump further includes a first coating formed on at least a portion of the barrel surface. The first coating includes a combination of diamond particles and a composition including nickel and phosphorous. The pump also includes a plunger with a surface configured to contact oil and gas well fluid. The pump additionally includes a second coating formed on at least a portion of the plunger surface. The second coating includes a combination of tungsten carbide particles and a composition including cobalt and chromium. | 2018-04-19 |
20180106251 | OIL PUMP - An oil pump is provided with an inner rotor having external teeth, an outer rotor disposed in a loose-fit state within a pump chamber and having internal teeth meshed with the external teeth, a ring-shaped pressure chamber provided adjacent to the pump chamber in a direction of a rotation axis, a discharge opening for connecting the pump chamber and the pressure chamber, and a cylindrical discharge passage having one end connected to the pressure chamber and the other end serving as a connection opening. A portion of the discharge passage is located to open inside of the outer periphery of the pressure chamber when viewed in the rotation axis direction. The one end reaches to a middle of the pressure chamber when viewed in a radial direction of the rotation axis, and the discharge passage and the pressure chamber are in direct communication with each other. | 2018-04-19 |
20180106252 | VANE SPACING FOR A VARIABLE DISPLACEMENT OIL PUMP - A vane fluid pump for a vehicle component has an inner rotor supported within a cam ring. A series of vanes is positioned within a series of slots in an inner rotor to define and separate a series of non-uniformly sized segmented pumping chambers to disrupt harmonics during operation to reduce pressure ripples and associated tonal noise. One chamber has a first sector angle being within a first predetermined range of a nominal value. A portion of the chambers each has a sector angle greater than the first sector angle, with an average sector angle greater than the nominal value by a second predetermined range. A remaining portion of the chambers each has a sector angle less than the first sector angle, with an average sector angle less than the nominal value by the second predetermined range. | 2018-04-19 |
20180106253 | TRIPLE GEAR PUMP AND FLUID SUPPLYING DEVICE - A gear pump is comprised of a driving gear, a first driven gear and second driven gears mutually in mesh; a housing accommodating them and defining a flow path including a first suction port, a second suction port, a first pressure port and a second pressure port; a floating comprising a thrust face bearing a floating force exerted by fluids and first, second and third pressure-receiving faces respectively oriented in a direction opposed to the thrust face; a first pressurizing chamber having fluid connection with the first pressure port or the second pressure port to exert pressure on the first pressure-receiving face; a second pressurizing chamber having fluid connection with the first suction port to exert pressure on the second pressure-receiving face; and a third pressurizing chamber having fluid connection with the second suction port to exert pressure on the third pressure-receiving face. | 2018-04-19 |
20180106254 | Liquid Feeding Type Screw Compressor - There is provided a liquid feeding type screw compressor that can reduce size and weight and improve vibration insulation and sound insulation. A liquid feeding type screw compressor includes as components: a compressor main body; a motor driving the compressor main body; and a gas-liquid separator separating a liquid from a compressed air discharged from the compressor main body. The motor is arranged above the compressor main body. The gas-liquid separator is arranged below the compressor main body. A compressor main body casing constituting an inner cylindrical space forming a compression operation chamber together with the screw rotor and constituting the contour of the compressor main body and a casing constituting the contour of another component consist of an integrally molded single member. | 2018-04-19 |
20180106255 | COMPRESSOR WITH LIQUID INJECTION COOLING - A positive displacement rotary compressor is designed for near isothermal compression, high pressure ratios, high revolutions per minute, high efficiency, mixed gas/liquid compression, a low temperature increase, a low outlet temperature, and/or a high outlet pressure. Liquid injectors provide cooling liquid that cools the working fluid and improves the efficiency of the compressor. A gate moves within the compression chamber to either make contact with or be proximate to the rotor as it turns. | 2018-04-19 |
20180106256 | METHOD OF DETERMINING CIRCULATION STATE OF COOLING WATER - A method of determining a state of cooling water is provided. The method includes operating, by a controller, a driving motor of a cooling water-circulating pump that is configured to circulate cooling water at a fixed current, a fixed torque, or a fixed power. In addition, the controller is configured to calculate an average rotation speed of the driving motor for a preset first period of time during the operation of the driving motor. Whether the circulation state of the cooling water is normal is determined based on an error between the calculated average rotation speed and a preset reference rotation speed. | 2018-04-19 |
20180106257 | PORTABLE DUNNAGE BAG INFLATION SYSTEM - Various embodiments provide a compact, portable dunnage bag inflation system that provides an air source that is easily carried by a user via a wearable container. Generally, the dunnage bag inflation system includes a portable dunnage bag inflator having an air generator that, in operation, expels air through an outlet. One end of a hose is removably connectable to the air generator to fluidly connect the hose and the outlet. An inflator head that includes a button actuatable to operate the portable dunnage bag inflator is connected to an opposing end of the hose. The dunnage bag inflation system also includes a rechargeable battery electrically connectable to the portable dunnage bag inflator to power the inflator and a charging station to charge the battery. This enables dunnage bags to be inflated to desired specifications at point-of-use and eliminates the need for a compressed air supply. | 2018-04-19 |
20180106258 | VACUUM PUMP LUBRICANTS - A vacuum pump may include a rotor and a stator, wherein the rotor is supported by metal bearings (such as steel bearings) to allow relative rotation of the rotor with respect to the stator. A liquid PFPE lubricant compound is provided to lubricate the bearings, wherein the lubricant further comprises a solid lubricant that is in suspension in the liquid lubricant. The solid lubricant can comprise any of graphite, graphene and molybdenum disulphide. In other words, the inventive concept encompasses a lubricated bearing arranged to support a rotating shaft in a body under sub-atmospheric conditions, wherein a lubricant used to lubricate the bearing comprises liquid PFPE lubricant having a low vapour pressure, and a solid lubricant that is held in suspension in the liquid lubricant. The solid lubricant may comprise any of graphite, graphene and molybdenum disulphide. | 2018-04-19 |
20180106259 | FAN STRUCTURE - The present disclosure illustrates a fan structure which includes an outer shell member, a rotating module and a circuit module. The outer shell member has a receiving groove, and an axis part and a fastening part. The fastening part includes winding columns. The rotating module includes the fan, an axis coupling part pivotally connected with the axis part, and a magnetic part disposed on a periphery of the axis coupling part. The circuit module includes a circuit board which has positioning holes formed on and annularly arranged the surface thereof. Position-limiting caps are respectively mounted and fixed on the winding column after the winding columns are inserted through the positioning holes. A conductive wire is wound on the winding columns to form coils, and has two ends welded on the circuit board. Therefore, defect rate and assembly cost of production of fan structure of the present disclosure can be decreased. | 2018-04-19 |
20180106260 | METHOD AND APPARATUS FOR COMPRESSOR SYSTEM PRESSURIZATION - A method of pressurizing a downstream compressor system operatively connected to an upstream compressor system by using a bleeding line connected at a first end to the downstream compressor system and at a second end at least to one bleeding region or tie-out region of the upstream compressor system. | 2018-04-19 |
20180106261 | SYSTEM, METHOD, AND APPARATUS TO MONITOR COMPRESSOR HEALTH - A method, system, and apparatus to monitor health of a compressor are provided. The method, system, and apparatus include detecting whether the compressor has a fault associated using one or more of performance-based modeling and structure-based modeling of physical aspects associated with operation of the compressor; diagnosing any detected fault to determine the cause or causes of the fault; and evaluating each diagnosed fault to assess the significance of the fault. Data pertaining to the cause or causes of the fault and the significance of the fault is used to output health information corresponding to a health state or status of the compressor. The method, system, and apparatus also predict future health-related conditions of the compressor, and data pertaining to the predicted future health-related conditions is used to output health information corresponding to a future health state or status of the compressor. | 2018-04-19 |
20180106262 | SURGE WEAR PREDICTOR FOR A TURBOCHARGER - A turbocharged device subject to a surge event during operation, the turbocharged device including a turbocharger having a controller and a bearing assembly, a first sensor configured to detect the oil pressure provided to the bearing assembly, a second sensor in operable communication with the turbocharger, where the controller is configured to determine the magnitude of the surge event based at least in part on a signal provided by the second sensor in response to the surge event, and where the controller is configured to determine the wear inflicted on the turbocharger during the surge event based at least in part on the magnitude of the surge event and a signal provided by the first sensor in response to the surge event. | 2018-04-19 |
20180106263 | SINGLE PIECE BEARING HOUSING WITH TURBINE END PLATE - A number of variations may include a product comprising a bearing housing comprising a body having an internal cavity defined by an inner surface of the body, wherein a first end of the body includes an end face and a second end of the body opposite of the end face is open, wherein the end face further comprises a through hole defined by an inner surface of the end face; and an end plate constructed and arranged to attach to the second end of the body of the bearing housing, wherein the end plate further comprise a first face and a second face, and an opening defined by an inner surface of the end plate. | 2018-04-19 |
20180106264 | WASTE WATER PUMP - A waste water pump includes an impeller ( | 2018-04-19 |
20180106265 | SEALING STRUCTURE AND TURBOCHARGER - A sealing structure includes: an insertion hole formed in a sealing plate; a sealing ring provided in the insertion hole; a first rotating body provided to the shaft, at least a part of the first rotating body positioned inside the insertion hole; a second rotating body disposed at a position apart from the compressor impeller than the first rotating body and having a maximum outer diameter larger than a minimum inner diameter of the insertion hole; and an annular receiving groove formed by the first rotating body and the second rotating body and receiving an inner circumferential surface side of the sealing ring. | 2018-04-19 |
20180106266 | ENTHALPY EXCHANGER - Disclosed is an enthalpy exchanger for changing the enthalpy of a throughflow medium to cool process water coming from an industrial process by passing air, including: an air inlet; an enthalpy exchanger panel guiding medium so the medium exchanges enthalpy with airflows let through by the air inlet; an air throughflow space connecting to the enthalpy exchanger panel so air can only flow into the air throughflow space via the air inlets and the enthalpy exchanger panels; a fan connecting to the air throughflow space and which draws in and blows out air via the air inlet, the enthalpy exchanger panel and the air throughflow space; and a rotation-symmetrical airflow-guiding element extends both into the air throughflow space and outside the enthalpy exchanger; the airflows in the air throughflow space converge at any position and are substantially free of vortices, turbulences and areas without suction. | 2018-04-19 |
20180106267 | FAN WITH FAN WHEEL AND GUIDE WHEEL - The invention relates to a fan having a fan wheel ( | 2018-04-19 |
20180106268 | BLADE COMPONENT - A blade component has a longitudinal axis and extends between a root end and a tip end. The component comprises a composite laminate structure, the laminate structure comprising a plurality of plies of fibres in a matrix, wherein all the plies are arranged such that the fibres in respective plies are oriented symmetrically relative to the component axis at respective layup angles, the layup angles being in the range of 19° to 25° and −19° to −25° respectively relative to the component axis. | 2018-04-19 |
20180106269 | FAN HOUSING HAVING A HEATING BAND CHANNEL - A fan housing includes a housing body for accommodating fan components and an outer casing which surrounds the housing body in circumferential direction. The housing body has at least two webs extending in a circumferential direction on the radial outer side. The outer casing has at least two ribs extending in the circumferential direction on the radial inner side. The ribs, in the assembled state, between the housing body and the outer casing, form a channel circulating in the circumferential direction for receiving and holding a heating band. The outer casing has at least one guiding rib directed in the radial direction toward a housing body as well as into the channel and extending in the circumferential direction. | 2018-04-19 |
20180106270 | DIFFUSER FOR A FLUID COMPRESSION DEVICE, COMPRISING AT LEAST ONE VANE WITH OPENING - The present disclosure describes a diffuser ( | 2018-04-19 |
20180106271 | AIRFOIL SHAPE FOR SIXTH STAGE COMPRESSOR STATOR VANE - A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances. | 2018-04-19 |
20180106272 | AIRFOIL SHAPE FOR TWELFTH STAGE COMPRESSOR STATOR VANE - A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances. | 2018-04-19 |
20180106273 | APPARATUS AND METHODS TO DEPLOY A FLUID FLOW CHANNEL - Apparatus and methods to deploy a fluid flow channel are disclosed herein. An example apparatus includes a first loop coupled to an outside surface of a vehicle via a first fastener, a second loop coupled to the vehicle and disposed a distance from the first loop, and a flexible material having a first end coupled to the first loop and a second end coupled to the second loop, where the flexible material is to form a fluid flow channel between the first loop and the second loop. | 2018-04-19 |
20180106274 | GAS TURBINE ENGINE - A gas turbine engine includes a fan section having a single-stage fan, a core turbine engine, and a nacelle at least partially surrounding the fan of the fan section and the core turbine engine. The gas turbine engine also includes an outlet guide vane extending between a casing of the core turbine engine and the nacelle. The gas turbine engine is configured to define an acoustic ratio greater than or equal to 2.3, with the acoustic ratio being a ratio of an axial spacing between the trailing edge of the fan blade and the leading edge of the outlet guide vane at a radial location seventy-five percent (75%) along the span of the fan blade to the axial width of the fan blade also at the radial location seventy-five percent (75%) along the span of the fan blade. | 2018-04-19 |
20180106275 | ENERGY STORAGE STRUCTURE - Provided is an energy storage structure, comprising a housing and a piston. An accommodating cavity and a piston cylinder part communicating with each other are arranged within the housing. The piston is slidably and sealingly arranged within the piston cylinder part for transferring impact energy. A self-pressure of an energy storage medium, arranged within the accommodating cavity and the piston cylinder part, acts on the piston, tending to push the piston to move. An energy storage structure provided by the present invention has a simple structure, is convenient for use, and can ensure that a thrust or impact force remains unchanged or slightly changes during operation, to achieve stable release of potential energy. Moreover, the adjustment of the thrust or impact force can be achieved by changing the temperature of the energy storage medium in the accommodating cavity, thereby achieving change in total impact energy of the energy storage structure. | 2018-04-19 |
20180106276 | Robotic Hydraulic System - A control system may receive sensor data indicative of respective fluid levels of two or more hydraulic accumulators configured to operate at respective target fluid levels within a hydraulic system. The control system may determine respective errors of the hydraulic accumulators based on the respective fluid levels and respective target fluid levels of the hydraulic accumulators. The respective errors may correspond to pressure errors, fluid volume errors, or other types of errors of the hydraulic accumulators. Responsive to determining the respective errors, the control system may determine that the error of a given hydraulic accumulator is greater than errors of the other hydraulic accumulators and provide instructions to control a hydraulic valve to supply fluid from a single pump of the hydraulic system to the given hydraulic accumulator | 2018-04-19 |
20180106277 | VALVE DEVICE AND FLUID PRESSURE CONTROL DEVICE - A valve device includes a valve body, a drain chamber wall configured to define a drain chamber, a drain port formed in the drain chamber wall facing the valving element, and a drain passage configured to guide drain fluid from another valve device to the drain chamber, wherein at least one of the drain chamber wall and the valving element includes a communicating passage configured to allow the drain port to communicate with the drain chamber when the movement of the valving element is restricted by the drain chamber wall. | 2018-04-19 |
20180106278 | CONSTRUCTION MACHINE - A hydraulic excavator is equipped with: an arm cylinder driven by a hydraulic working fluid from a hydraulic pump; a meter-out passage through which the hydraulic working fluid discharged from the arm cylinder flows; a control valve controlling the hydraulic fluid flow rate of the meter-out passage; a pressure sensor detecting a load acting on the arm cylinder; a pressure sensor detecting an operation amount of an operation device operating the arm cylinder; and a controller. The controller alternatively selects a normal operation mode in which the opening area of the control valve is controlled based on an actuator load and the operation amount, and a substitution operation mode in which the opening area of the control valve is controlled based on the operation amount. When the substitution operation mode is selected, a delivery flow rate of the hydraulic pump is further increased as compared with the normal operation mode. | 2018-04-19 |
20180106279 | WASTE WATER AIR STOP VALVE - Embodiments provide systems and methods for releasing grey water from an aircraft sink or sump using an improved waste water air stop valve. The valves described herein allow drainage of waste water, without air leakage. Additionally, if drainage in the piping is blocked, the valves are designed to ensure that water cannot flow back into the sinks or sumps. | 2018-04-19 |
20180106280 | ACTUATOR CONTROL ARRANGEMENT - An actuator control arrangement is provided comprising a pair of rotary control valves used in combination to control the operation of an actuator. The rotary control valves are driven synchronously through a hydraulic or mechanical coupling. Each rotary control valve has a by-pass mode which activates in the event of a jam. In addition each rotary control valve has a mechanism for activating the by-pass mode absent any jam. The actuator control arrangement further comprises a circuit coupling a pilot control and/or a flight control computer (FCC) to one or both of the mechanisms for remotely switching the rotary control valve(s) from an active mode to a by-pass mode under control of a pilot or FCC. | 2018-04-19 |
20180106281 | HIGH-CAPACITY RADIAL FIT COUPLING BOLTS - A high capacity radial-fit coupling bolt (or “expanding sleeve bolt”) has a pair of tapered sleeves about a shank of a bolt to which can be applied a tensioning load. An extrudable ring, or a compression ring, is interposed between a head nut or head flange at one end of the shank, and one end of an inner sleeve. A tensioning load is applied to the shank, the inner sleeve causing the outer sleeve to expand diametrically. At a preset load limit, the extrudable ring is extruded through at least one bore in a drive piston between the head nut and the extrudable ring, to allow shank to move relative to the inner sleeve until the tensioning load is fully applied. Alternatively, a drive member is provided between the head nut or head flange and the compression ring, and at a preset limit, the compression ring allows the shank to move relative to inner sleeve until the tensioning load is fully applied. The preset limit will typically correspond to the force required to fully expand the outer sleeve. | 2018-04-19 |
20180106282 | Panel Fastening System - A fastening system for joining a first composite sandwich panel and a second composite sandwich panel comprising a cam assembly and a stud receiving assembly. The cam assembly is configured to be positioned within a first hole extending through a thickness of a first composite sandwich panel. The cam assembly comprises a housing and a cam connector rotatable within the housing. The cam connector is configured to engage a head of a stud. The stud receiving assembly is configured to be positioned within a second hole extending through a thickness of a second composite sandwich panel. The stud receiving assembly has internal retaining channels configured to secure a first end of the stud. | 2018-04-19 |
20180106283 | CONNECTOR FOR CONCRETE BARRIERS - Provided are a connector and a connection system for concrete barriers. The connector is configured to slip-fit into a cross-shaped gap formed between the concrete barriers. The connector includes a saddle member and a fork member. The saddle member includes a base plate and peripheral plates. The peripheral plates extend at angles from the base plate to define open ends of the saddle member. The fork member extends below the base plate of the saddle member. The fork member includes an elongated base, flanges, and legs. The elongated base extends between the peripheral plates. The flanges are transverse to the elongated base forming a cross-shaped structure with the flanges that extend toward the open ends of the saddle member. The legs extend separately from the elongated base. | 2018-04-19 |
20180106284 | SPRING CLIP UPRIGHT CONNECTION FOR RACK SHELVING - A spring clip upright connection for rack shelving includes one upright with tabs and square cutouts and another upright with slots with metal spring clips. As the tabs of one upright are inserted into the slots of the other upright, the uprights are aligned and the spring metal clips open up. When the tabs are fully inserted, the clips latch into the cutouts of the slots of the other upright thereby engaging the upright sections together. This latching prevents one upright from being removed from the other upright while the slots and tabs maintain the appropriate alignment of the uprights. | 2018-04-19 |
20180106285 | FASTENER - A fastener includes a head portion, a leg portion, and an easily deformable portion. The head portion is formed in a cylindrical shape with an oval shape in an axial view. The leg portion has one end portion in an axial direction that is connected to a back surface of the head portion. The leg portion is formed in a hollow cylindrical shape with an oval shape in the axial view whose minor axis direction is the same as a minor axis direction of the oval shape of the head portion. The easily deformable portion is provided to a pair of major-axis leg portions which are portions crossing a major axis in the leg portion. | 2018-04-19 |
20180106286 | Driver/Fastener Inter-engagement System - Embodiments of the present invention provide a screw and driver system comprising a range of screws and a driver for said range. Each screw comprises a head having a driving recess in its surface for engagement by said driver. Each recess has a recess longitudinal axis. The recess of larger screws in the range has a plurality of superimposed recess-tiers of decreasing size with increasing depth from said surface, each recess-tier except the smallest having substantially parallel driving surfaces substantially parallel said recess longitudinal axis. The driving head of the driver has a driver longitudinal axis and a plurality of superimposed drive-tiers of decreasing size towards a tip of the driver, each drive-tier except the smallest having substantially parallel driving surfaces substantially parallel said longitudinal axis. The driver and recess are shaped so that, when the driver is engaged with the recess of any screw in said range, torque applied to the driver is transmitted to the screw through said driving surfaces. The smallest recess-tier of larger screws has a mouth in a floor of an adjacent recess-tier and has recess flanks that are all tapered from the mouth towards the recess longitudinal axis at a recess taper angle between 1.91 and 6.85°. The smallest drive-tier of the driver has a root in a base of an adjacent drive-tier and has drive flanks that are all tapered from the root towards the driver longitudinal axis at a tier taper angle between minus 1.5 and plus 2.5° difference with respect to said recess taper angle. The diameter of the drive-tier at the root and the diameter of the recess-tier at the mouth are such that, on insertion of said driver head in the screw recess, said drive and recess flanks inter-engage to deform and stick together through frictional engagement before said base engages said floor. | 2018-04-19 |
20180106287 | Screw Having Discontinuous Scraping Edges - A screw has a shaft section which extends axially, a screw thread at the shaft section, which screw thread has thread turns that extend radially starting from the shaft section, a screw tip section which connects to the shaft section, at least one first scraping edge at the screw tip section, and at least one second scraping edge in a region of the shaft section adjacent to the screw tip section. The at least one first scraping edge and the at least one second scraping edge are spaced at a distance from each other and extend in an axial direction over different areas of the screw. | 2018-04-19 |