25th week of 2019 patent applcation highlights part 34 |
Patent application number | Title | Published |
20190186341 | PISTON BOWL FOR IMPROVED COMBUSTION STABILITY - A piston comprises a crown portion with a contoured bowl having a reentrant surface extending from the top squish surface that connects to a lower sidewall surface that connects to a swirl pocket surface disposed adjacent the bottom bowl surface. | 2019-06-20 |
20190186342 | Method for Operating an Internal Combustion Engine, and Internal Combustion Engine - A method for operating an internal combustion engine includes using a 3-front combustion method. When the fuel is injected into the combustion chamber the fuel flows through an injection element with a hydraulic flow of more than 1000 cubic centimeters per 60 seconds and under an injection pressure of 100 bar and 1 liter capacity per cylinder if the internal combustion engine is used in a truck application. The fuel flows through the injection element with a hydraulic flow of more than 1900 cubic centimeters per 60 seconds and under an injection pressure of 100 bar and 1 liter capacity per cylinder if the internal combustion engine is used in a car application. | 2019-06-20 |
20190186343 | INTAKE STRUCTURE OF INTERNAL COMBUSTION ENGINE - In an intake structure of an internal combustion engine, on an intake upstream side from a valve seat of an intake port, a convex portion is provided which protrudes to an inside of the intake port in a place near an outer circumferential portion of a cylinder chamber when viewed from an upper side of the cylinder chamber. The convex portion includes an upstream guide surface extending from an apex of the convex portion to the intake upstream side, and a downstream guide surface extending from the apex to an intake downstream side and including a curved surface recessed inside the convex portion at a middle portion thereof. | 2019-06-20 |
20190186344 | COOLING SYSTEM FOR A WORK VEHICLE - A cooling system includes a charge air cooler system that includes a first stage that receives charge air via a charge air flow path and receives coolant fluid via a first coolant fluid flow path. A second stage receives charge air from the first stage via the charge air flow path, outputs the charge air, and receives the coolant fluid via a second coolant fluid flow path. A third stage receives and outputs the charge air from the second stage via the charge air flow path and receives the coolant fluid via a third coolant fluid flow path. The cooling system includes a low temperature radiator system that includes a low temperature radiator that directs the coolant fluid toward the third stage via the third coolant fluid flow path and includes a high temperature radiator system that directs the coolant fluid toward the first stage and second stage. | 2019-06-20 |
20190186345 | INTEGRATED PASSIVE ONE WAY VALVE IN CHARGE AIR INLET TANK - An inlet tank for a charge cooler comprises a manifold portion, a turbocharger inlet port, and a supercharger inlet port. The turbocharger inlet port is in fluid communication with a compressor wheel of a turbocharger and the manifold portion of the inlet tank. An opening is formed in a sidewall of the turbocharger inlet port. The supercharger inlet port is in fluid communication with an electric supercharger and intersects the turbocharger inlet port. The opening formed in the sidewall of the turbocharger inlet port provides fluid communication between the supercharger inlet port and the turbocharger inlet port. A valve element selectively determines when a flow of air from the supercharger inlet port enters the turbocharger inlet port through the opening based on a pressure differential present between the air exiting the compressor wheel of the turbocharger and the air exiting a compression mechanism of the electric supercharger. | 2019-06-20 |
20190186346 | COOLING SYSTEM FOR A WORK VEHICLE - A cooling system includes a charge air cooler system that includes a first stage and a second stage. The first stage receives charge air via a charge air flow path. The first stage receives coolant fluid via a first coolant fluid flow path. The second stage receives the charge air from the first stage via the charge air flow path, such the second stage of the charge air cooler system outputs the charge air and receives the coolant fluid via a second coolant fluid flow path. The cooling system includes a low temperature radiator system that includes a low-temperature radiator that directs the coolant fluid toward the second coolant fluid flow path and a third coolant fluid flow path. The cooling system includes a high temperature radiator system that directs the coolant fluid toward the first stage via the first coolant fluid flow path. | 2019-06-20 |
20190186347 | INTERCOOLER PROVIDED WITH A THERMOELECTRIC GENERATOR FOR A TURBOCHARGED INTERNAL COMBUSTION HEAT ENGINE - An intercooler for a turbocharged internal combustion heat engine; the intercooler has: a cooling chamber, which is provided with an air inlet opening and an air outlet opening opposite one another; a plurality of exchanger plates, which are stacked on top of one another inside the cooling chamber, are arranged parallel to an air flowing direction from the inlet opening to the outlet opening, are spaced apart from one another so as to define corresponding air passage channels between one another, and are internally hollow; a circulation circuit, which allows a cooling fluid to circulate inside the exchanger plates; and a plurality of thermoelectric cells, each of which is mounted on a corresponding exchanger plate, and has a cold side resting on the exchanger plate and a hot side delimiting a corresponding air passage channel. | 2019-06-20 |
20190186348 | ELECTRICALLY-ASSISTED TURBOCHARGER - A turbocharging system for an internal combustion engine includes a turbocharger having a shaft supported for rotation about an axis. The turbocharger also includes a turbine wheel mounted on the shaft and configured to be rotated about the axis by the exhaust gas, and a compressor assembly mounted on the shaft and configured to pressurize an airflow received from the ambient for delivery to the cylinder. The turbocharging system additionally includes an electric motor configured to generate electric motor torque. The turbocharging system further includes a one-way clutch configured to selectively connect the electric motor to the compressor assembly, such that the electric motor torque assists the turbocharger in generating boost pressure. An internal combustion engine employing such a turbocharging system is also disclosed. | 2019-06-20 |
20190186349 | TURBOCHARGER WASTEGATE ASSEMBLY - A turbocharger includes a housing, a turbine wheel, a bypass channel formed in the housing, a wastegate assembly having a valve and configured to selectively allow a flow of exhaust gas to bypass the turbine wheel via the bypass channel, and a wastegate outer housing having an aperture fluidly coupled to the bypass channel, and an outer valve seating surface, the valve configured to selectively seat against the outer valve seating surface over the aperture. A shroud extends outwardly from the wastegate outer housing and is configured to direct the bypass exhaust gas flow toward a catalytic converter. | 2019-06-20 |
20190186350 | EXTERNALLY POWERED TURBINE FOR AN INTERNAL COMBUSTION ENGINE - Described herein is a turbocharging system comprising a compressor having an air inlet and a compressed air outlet, the compressed air outlet to couple with the intake manifold of the internal combustion engine, a first turbine coupled to the compressor, the compressor driven without using power from the internal combustion engine; and a vacuum compressor coupled directly or indirectly to the first turbine. The first turbine can drive a common drive shaft that includes the compressor and the vacuum compressor or output of the first compressor can drive a second compressor that is coupled with the vacuum compressor. The vacuum compressor can be used to scavenge exhaust from the internal combustion engine. | 2019-06-20 |
20190186351 | AUXILIARY POWER UNIT WITH VARIABLE SPEED RATIO - An auxiliary power unit for an aircraft includes a rotary intermittent internal combustion engine drivingly engaged to an engine shaft, a turbine section having an inlet in fluid communication with an outlet of the engine(s), the turbine section including at least one turbine compounded with the engine shaft, and a compressor having an inlet in fluid communication with an environment of the aircraft and an outlet in fluid communication with a bleed duct for providing bleed air to the aircraft, the compressor having a compressor rotor connected to a compressor shaft, the compressor shaft drivingly engaged to the engine shaft. The driving engagement between the compressor shaft and the engine shaft is configurable to provide at least two alternate speed ratios between the compressor shaft and the engine shaft. | 2019-06-20 |
20190186352 | AUXILIARY POWER UNIT WITH COMBINED COOLING OF GENERATOR - An auxiliary power unit for an aircraft, including an internal combustion engine having a liquid coolant system, a generator drivingly engaged to the internal combustion engine and having a liquid coolant system distinct from the liquid coolant system of the internal combustion engine, a first heat exchanger in fluid communication with the liquid coolant system of the internal combustion engine, a second heat exchanger in fluid communication with the liquid coolant system of the generator, an exhaust duct in fluid communication with air passages of the heat exchangers, and a fan received in the exhaust duct and rotatable by the internal combustion engine for driving a cooling air flow through the air passages. The liquid coolant system of the engine may be distinct from fuel and lubricating systems of the auxiliary power unit. A method of cooling a generator and an internal combustion engine is also discussed. | 2019-06-20 |
20190186353 | CONNECTING ROD FOR INTERNAL COMBUSTION ENGINE WITH ECCENTRICAL ELEMENT ADJUSTMENT ARRANGEMENT FOR ADJUSTING AN EFFECTIVE CONNECTING ROD LENGTH - A connecting rod for an internal combustion engine with an eccentrical element adjustment arrangement for adjusting an effective connecting rod length, the eccentrical element adjustment arrangement including at least one ball joint including a ball head that is arranged at a support rod and supported in a ball head receiver of a piston, wherein the ball head is secured at its outer surface in the ball head receiver by safety devices against sliding out of the ball head receiver, and wherein the safety devices are configured as a one-piece or a multi-piece annular safety element which is arranged in the piston at least partially bonded or form locking. | 2019-06-20 |
20190186354 | Internal Combustion Engine - The disclosure relates to an internal combustion engine ( | 2019-06-20 |
20190186355 | THERMAL BARRIERS FOR ENGINES AND METHODS OF MAKING THE SAME - A thermal barrier for component surfaces of an engine. The thermal barrier includes a plurality of modules, each module includes a shield. An edge of at least one shield in the array is spaced apart from an edge of an adjacent shield in the array. | 2019-06-20 |
20190186356 | SEGMENTED THERMAL BARRIERS FOR INTERNAL COMBUSTION ENGINES AND METHODS OF MAKING THE SAME - A segmented thermal barrier for a combustion chamber surface of an internal combustion engine. The segmented thermal barrier includes a plurality of modules, each module with a support and a shield. The edges of shields of at least two adjacent modules are spaced apart by a distance. | 2019-06-20 |
20190186357 | GAS TURBINE ENGINE WITH FAN TIED COMPRESSOR - A turbofan engine according to an example of the present disclosure includes, among other things, a fan including fan blades, an outer housing that surrounds the fan to define a bypass flow path, a compressor section in fluid communication with the fan, the compressor section including a low pressure compressor section and a high pressure compressor section, a turbine section including a fan drive turbine section driving the fan and the low pressure compressor section and a high pressure turbine section driving the high pressure compressor section. A gear reduction including an epicyclic gear train is between the fan drive turbine section and the low pressure compressor section such that the low pressure compressor section and the fan are rotatable at a common speed and such that the fan is rotatable at a lower speed than the fan drive turbine section. The fan drive turbine section has a first exit area at a first exit point and is rotatable at a first speed, the high pressure turbine section has a second exit area at a second exit point and is rotatable at a second speed, which is higher than the first speed. A first performance quantity is defined as a product of the first speed squared and the first area, a second performance quantity is defined as a product of the second speed squared and the second exit area and a performance ratio of the first performance quantity to the second performance quantity is between 0.2 and 0.8. | 2019-06-20 |
20190186358 | FURNACE WALL, GASIFICATION UNIT AND INTEGRATED GASIFICATION COMBINED CYCLE, AND METHOD OF MANUFACTURING FURNACE WALL - The purpose of the present invention is to provide a furnace wall in which a throat section with a smaller channel diameter than other regions can be formed using all peripheral wall tubes. Provided is a furnace wall comprising: a plurality of peripheral wall tubes ( | 2019-06-20 |
20190186359 | ROTOR BOW MANAGEMENT - A method of reducing rotor bow in a high pressure rotor of a gas turbine engine that has in axial flow a low pressure rotor and a high pressure rotor. The method involves storing bleed air from the gas turbine engine when the engine is running to provide stored pneumatic energy; and using that stored pneumatic energy after the engine has been shut-down to rotate the high pressure rotor at a speed and for a duration that reduces rotor bow. A gas turbine engine wherein rotor bow in the high pressure rotor after engine shut-down has been reduced by carrying out the aforesaid method is also disclosed. | 2019-06-20 |
20190186360 | METHODS, COMPUTER PROGRAMS, NON TRANSITORY COMPUTER READABLE STORAGE MEDIUMS, SIGNALS, AND APPARATUS FOR CONTROLLING ELECTRICAL POWER SUPPLIED TO A COMPONENT OF A VEHICLE - A method of controlling electrical power supplied to a component of a vehicle, the method comprising: receiving a signal comprising information associated with an operating condition of a gas turbine engine; determining whether a parameter exceeds a predetermined threshold value using the information in the received signal; and controlling a reduction in electrical power supplied to a component of a vehicle from a generator of the gas turbine engine if the parameter exceeds the predetermined threshold value. | 2019-06-20 |
20190186361 | RECUPERATOR FOR GAS TURBINE ENGINE - A recuperator includes a monolithic heat exchanger core having a first side proximal to a combustor inlet and a turbine outlet, and a second side that includes an exhaust outlet. A compressed air inlet is located on the second side, and a compressed air outlet is located on the first side. The compressed air outlet supplies air to a combustor. A first plurality of passageways connects the compressed air inlet to the compressed air outlet. A turbine exhaust inlet is located on the first side, and a turbine exhaust outlet is located on the second side. A second plurality of passageways connects the turbine exhaust inlet to the turbine exhaust outlet. The first and second plurality of passageways are defined by parting plates that extend radially outward in a spiral pattern that maintains a substantially equal distance between adjacent parting plates. | 2019-06-20 |
20190186362 | HEAT EXCHANGER DEVICE FOR AN AIRCRAFT ENGINE - A heat-exchanger device for an aircraft engine, having a fuel-oil heat exchanger for exchanging heat between fuel and oil, and a housing with an air inlet and an air outlet, wherein the fuel-oil heat exchanger is arranged at least partially within the housing such that air flowing from the air inlet to the air outlet can flow over or around the fuel-oil heat exchanger. The invention further relates to a method for operating an aircraft engine. | 2019-06-20 |
20190186363 | Turbine Engine Cooling with Substantially Uniform Cooling Air Flow Distribution - Various embodiments of the present disclosure address problems associated with non-uniform flow of cooling air by providing a turbine engine including a cooling air chamber in fluid communication with a cooling air source, a turbine chamber, and multiple conduits fluidly connecting the cooling air chamber and the turbine chamber. The system is configured such that, when cooling air is flowing from a cooling air source the static pressure within the cooling fluid chamber is substantially uniform and such that the mass flow rates of cooling air through the conduits and into the turbine chamber are substantially uniform. | 2019-06-20 |
20190186364 | FUEL INJECTOR SYSTEMS AND SUPPORT STRUCTURES - A turbomachine fuel injector system includes an air distributor configured to be mounted to and contained within a casing and to provide air to mix with a fuel from one or more fuel distribution systems. The system includes a fuel manifold configured to be mounted indirectly to the casing such that the fuel manifold system is contained within the casing but is independent such that fuel manifold does not touch or directly mount to either an interior of the casing or touch the air distributor within the casing to prevent or reduce thermal transfer from the air distributor to the fuel manifold. | 2019-06-20 |
20190186365 | Jet Engine with Fuel Injection Using a Conductor of a Resonator - An example system can include a combustion chamber of a jet engine, a radio-frequency power source, a direct-current power source, a resonator, and a fuel conduit. The resonator can be electromagnetically coupled to the radio-frequency power source and have a resonant wavelength. Further, the resonator can include (i) a first conductor, (ii), a second conductor, and (iii) a dielectric between the first conductor and the second conductor. The resonator can be configured to provide at least one of a plasma corona or electromagnetic waves. The fuel conduit can be configured to couple to a fuel source and have a fuel outlet for expelling fuel into a combustion zone of the combustion chamber. A portion of the fuel conduit is disposed within the first conductor. | 2019-06-20 |
20190186366 | Jet Engine with Fuel Injection Using a Dielectric of a Resonator - An example system can include a combustion chamber of a jet engine, a radio-frequency power source, a resonator, and a fuel conduit. The resonator can be electromagnetically coupled to the radio-frequency power source and have a resonant wavelength. Further, the resonator can include (i) a first conductor, (ii), a second conductor, and (iii) a dielectric between the first conductor and the second conductor. The resonator can be configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter of the resonant wavelength, the resonator provides at least one of a plasma corona or electromagnetic waves. The fuel conduit can be configured to couple to a fuel source and have a fuel outlet for expelling fuel into a combustion zone of the combustion chamber. A portion of the fuel conduit is arranged proximate to the dielectric. | 2019-06-20 |
20190186367 | CONTROLLED EVAPORATION AND HEATING OF FUELS FOR TURBINE ENGINES - Provided are turbine engines and methods of operating thereof by heating and evaporating liquid fuels in a controlled manner prior to burning. Specifically, a fuel is heated and evaporated while avoiding coking. Coking is caused by pyrolysis when the fuel contacts a metal surface within a certain temperature range, which is referred herein to a coking temperature range. In the described methods, the fuel is transferred from one component, maintained below the coking temperature range, to another component, maintained above this range. The fuel is airborne and does not contact any metal surfaces during this transfer, and coking does not occur. In some examples, the fuel is also mixed with hot air during this transfer. The heated fuel, e.g., as an air-fuel mixture, is then supplied into a combustor, where more air is added to reach flammability conditions. | 2019-06-20 |
20190186368 | Method of Starting a Gas Turbine Engine - A method of starting a gas turbine engine is generally provided. The engine includes a rotor assembly including a compressor rotor and a turbine rotor each coupled to a shaft. The rotor assembly is coupled to a bearing assembly within a casing enabling rotation of the rotor assembly. The method includes determining, based on a lubricant parameter, a period of time within which a rotational speed of the rotor assembly is maintained within a bowed rotor mitigation speed range; rotating the rotor assembly for the period of time within the bowed rotor mitigation speed range; and accelerating the rotor assembly to the combustion speed to ignite a fuel-oxidizer mixture for combustion. | 2019-06-20 |
20190186369 | Jet Engine with Plasma-assisted Combustion - An example system and corresponding method can include a combustion chamber of jet engine, a radio-frequency power source, and a resonator. The combustion chamber can include a liner defining a combustion zone, and include a fuel inlet configured to introduce fuel into the combustion zone. The resonator can have a resonant wavelength and include: a first conductor, a second conductor, a dielectric, and an electrode coupled to the first conductor. The resonator can be configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength, the resonator provides a plasma corona in the combustion zone. The controller can be configured to cause the radio-frequency power source to excite the resonator with the signal so as to provide the plasma corona. | 2019-06-20 |
20190186370 | Power-generation Gas Turbine with Plasma-assisted Combustion - An example system and corresponding method can include a combustion chamber of a power-generation gas turbine, a radio-frequency power source, and a resonator. The combustion chamber can include a liner defining a combustion zone, and include a fuel inlet configured to introduce fuel into the combustion zone. The resonator can have a resonant wavelength and include: a first conductor, a second conductor, a dielectric, and an electrode coupled to the first conductor. The resonator can be configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter of the resonant wavelength, the resonator provides a plasma corona in the combustion zone. The controller can be configured to cause the radio-frequency power source to excite the resonator with the signal so as to provide the plasma corona. | 2019-06-20 |
20190186371 | Power-generation Gas Turbine with Fuel Injection Using a Conductor of a Resonator - An example system can include a combustion chamber of a power-generation gas turbine, a radio-frequency power source, a direct-current power source, a resonator, and a fuel conduit. The resonator can be electromagnetically coupled to the radio-frequency power source and have a resonant wavelength. Further, the resonator can include (i) a first conductor, (ii), a second conductor, and (iii) a dielectric between the first conductor and the second conductor. The resonator can be configured to provide at least one of a plasma corona or electromagnetic waves. The fuel conduit can be configured to couple to a fuel source and have a fuel outlet for expelling fuel into a combustion zone of the combustion chamber. A portion of the fuel conduit is disposed within the first conductor. | 2019-06-20 |
20190186372 | Power-generation Gas Turbine with Fuel Injection Using a Dielectric of a Resonator - An example system can include a combustion chamber of a power-generation gas turbine, a radio-frequency power source, a resonator, and a fuel conduit. The resonator can be electromagnetically coupled to the radio-frequency power source and have a resonant wavelength. Further, the resonator can include (i) a first conductor, (ii), a second conductor, and (iii) a dielectric between the first conductor and the second conductor. The resonator can be configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter of the resonant wavelength, the resonator provides at least one of a plasma corona or electromagnetic waves. The fuel conduit can be configured to couple to a fuel source and have a fuel outlet for expelling fuel into a combustion zone of the combustion chamber. A portion of the fuel conduit is arranged proximate to the dielectric. | 2019-06-20 |
20190186373 | Power-generation Gas Turbine with Fuel Injection Using a Conductor of At Least One of Multiple Resonators - An example system can include a combustion chamber of a power-generation gas turbine, one or more radio-frequency power sources, a plurality of resonators, and a fuel conduit. The plurality of resonators can be electromagnetically coupled to the one or more radio-frequency power sources and each have a respective resonant wavelength. Further, each resonator can include (i) a respective first conductor, (ii) a respective second conductor, and (iii) a respective dielectric between the first conductor and the second conductor, and can be configured to provide at least one of a plasma corona or electromagnetic waves. The fuel conduit can be configured to couple to a fuel source and have a fuel outlet for expelling fuel into a combustion zone of the combustion chamber. A portion of the fuel conduit is disposed within the first conductor of a given resonator of the plurality of resonators. | 2019-06-20 |
20190186374 | Jet engine with plasma-assisted afterburner - A system includes a radio-frequency power source, a resonator, a fuel outlet, and an afterburner. The afterburner includes a duct that defines a channel, and can receive gas from a turbine of a jet engine into the channel and output a gas resulting from combusting fuel within the channel. The resonator can be configured to be electromagnetically coupled to the power source and has a resonant wavelength. The resonator includes first and second conductors, a dielectric between the first and second conductors, and an electrode coupled to the first conductor and disposed within the afterburner. The fuel outlet outputs fuel into the channel for mixing with the gas from the turbine. The resonator, when excited by the power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter of the resonant wavelength, provides electromagnetic waves and/or a plasma corona proximate to a concentrator of the electrode. | 2019-06-20 |
20190186375 | Plasma-Distributing Structure and Directed Flame Path in a Jet Engine - An example system can include a combustor of a jet turbine engine, a radio-frequency power source, a plasma-distributing structure, and a resonator having a first concentrator. The combustor can include one or more fins protruding into a combustion zone and can be configured to guide combustion of fuel along a flame path defined by the fin(s). The resonator can be configured to provide a plasma corona when excited by the power source. The plasma-distributing structure can be arranged within the combustor and proximate to the plasma corona, and can include a second concentrator. When the resonator is excited, the plasma corona can be provided proximate to the first concentrator. Further, when the plasma corona is provided proximate to the first concentrator and the plasma-distributing structure is at a predetermined voltage, an additional plasma corona can be established proximate to the second concentrator and at least partly within the flame path. | 2019-06-20 |
20190186376 | Plasma-Distributing Structure and Directed Flame Path in a Power Generation Turbine - An example system can include a combustor of a power-generation turbine, a radio-frequency power source, a plasma-distributing structure, and a resonator having a first concentrator. The combustor can include one or more fins protruding into a combustion zone and can be configured to guide combustion of fuel along a flame path defined by the fin(s). The resonator can be configured to provide a plasma corona when excited by the power source. The plasma-distributing structure can be arranged within the combustor and proximate to the plasma corona, and can include a second concentrator. When the resonator is excited, the plasma corona can be provided proximate to the first concentrator. Further, when the plasma corona is provided proximate to the first concentrator and the plasma-distributing structure is at a predetermined voltage, an additional plasma corona can be established proximate to the second concentrator and at least partly within the flame path. | 2019-06-20 |
20190186377 | Jet Engine with Plasma-assisted Combustion and Directed Flame Path - An example system and corresponding method includes a jet engine combustor and a resonator. The combustor includes (i) a combustion zone, (ii) one or more fuel inlets for introducing fuel into the combustion zone for combustion, and (iii) one or more fins protruding into the combustion zone and configured to guide combustion of the fuel along a flame path. The resonator can have a resonant wavelength and can provide a plasma corona in the combustion zone when excited with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength. A radio-frequency power source can excite the resonator with the signal so as to provide the plasma corona in the combustion zone and cause combustion of the fuel along the flame path. | 2019-06-20 |
20190186378 | Jet Engine with Plasma-assisted Combustion Using Multiple Resonators and a Directed Flame Path - An example system and corresponding method includes a jet engine combustor and a plurality of resonators. The combustor includes (i) a combustion zone, (ii) one or more fuel inlets for introducing fuel into the combustion zone for combustion, and (iii) one or more fins protruding into the combustion zone and configured to guide combustion of the fuel along a flame path. The resonators can each have a respective resonant wavelength and can each provide a respective plasma corona in the combustion zone when excited with a respective signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the respective resonant wavelength. A radio-frequency power source can excite the resonators with the respective signals so as to provide the respective plasma coronas in the combustion zone and cause combustion of the fuel along the flame path. | 2019-06-20 |
20190186379 | Power-generation Gas Turbine with Plasma-assisted Combustion and Directed Flame Path - An example system and corresponding method includes a power-generation turbine combustor and a resonator. The combustor includes (i) a combustion zone, (ii) one or more fuel inlets for introducing fuel into the combustion zone for combustion, and (iii) one or more fins protruding into the combustion zone and configured to guide combustion of the fuel along a flame path. The resonator can have a resonant wavelength and can provide a plasma corona in the combustion zone when excited with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength. A radio-frequency power source can excite the resonator with the signal so as to provide the plasma corona in the combustion zone and cause combustion of the fuel along the flame path. | 2019-06-20 |
20190186380 | FAULT DETECTION ASSEMBLY - A fault detection assembly for an aircraft system according to an example of the present disclosure includes, among other things, a transmitter that communicates an electrical input signal to a first portion of an electrical connector, the first portion moveable between a fully seated position and a fully unseated position relative to a second portion of the electrical connector to define a range of insertion depths, a receiver that senses an electrical output signal relating to the electrical input signal, and a comparison module that determines an insertion depth in the range of insertion depths based on a change in a resonant frequency of the electrical output signal with respect to the electrical input signal. | 2019-06-20 |
20190186381 | INTERGRATED ENVIRONMENTAL CONTROL SYSTEM MANIFOLD - A compressor intermediate case for a gas turbine engine includes a plurality of intermediate case struts joining the compressor intermediate case to an inner engine structure. Each strut of the plurality of intermediate case struts includes a leading edge. A turning scoop is disposed at the leading edge of each strut of the plurality of intermediate case struts. A plurality of diffusers extends radially outwardly from the compressor intermediate case so that each diffuser of the plurality of diffusers engages with a corresponding turning scoop. A substantially annular structural fire wall extends radially outwardly from the compressor intermediate case. An environmental control system manifold is disposed on the compressor intermediate case. The environmental control system manifold includes an exit port. | 2019-06-20 |
20190186382 | AUTOMATED TUNING OF GAS TURBINE COMBUSTION SYSTEMS - The present disclosure provides a tuning system for tuning the operation of a gas turbine. The system comprises operational turbine controls for controlling operational control elements of the turbine, including at least one of turbine fuel distribution or the fuel temperature. The system also has a tuning controller communicating with the turbine controls. The tuning controller is configured to tune the operation of the turbine in accordance with the following steps: receiving operational data about the turbine, providing a hierarchy of tuning issues, determining whether sensed operational data is within predetermined operational limits and producing one or more indicators. If the operational data is not within predetermined operational limits, the tuning controller will rank the one or more indicators to determine dominant tuning concern, and tune the operation of the turbine based on dominant tuning concern. Also provided herein are a method and computer readable medium for tuning. | 2019-06-20 |
20190186383 | Gas Turbine Engine Installed Monitoring and Control to Prevent Standing Wave Dynamic Resonance - A method of preventing standing waves in an installed gas turbine having a fan, having a fan speed, and a compressor, having a compressor speed, includes correcting the fan and compressor speeds for temperature and monitoring the corrected speeds to prevent them from converging, or becoming the same value. In addition, a computer implemented monitoring and adjusting program may monitor a position of an aircraft on a ACTFS plot and make adjustments to avoid intercepting a surge line by changing the speed of the plane, one or both of the fan or compressor speeds or by changing altitude. An aircraft may form a standing wave when crossing or operating on a surge line of an ACTFS plot and this condition should be avoided which may require high data rate monitoring and control logic. | 2019-06-20 |
20190186384 | ENGINE - An engine promoting activation of a catalyst is provided, including an exhaust manifold, an exhaust lead-out path led out from a manifold exit of the exhaust manifold, a catalyst case provided on the exhaust lead-out path, and a catalyst housed in the catalyst case. The exhaust manifold and the catalyst case are extended in the front-back direction of crankshaft extension and disposed side by side orthogonally to the front-back direction. The engine may further include a supercharger attached to the exit of the exhaust manifold, and the catalyst case is attached to a turbine exit of the supercharger. The engine may further include an exhaust relay pipe attached to the exit of the exhaust manifold, and the catalyst case is attached to a relay pipe exit of the exhaust relay pipe. The engine may further include an exhaust throttle device provided on an exhaust downstream side of the catalyst. | 2019-06-20 |
20190186385 | ANGLE DETECTION MECHANISM AND ANGLE DETECTION SYSTEM - An angle detection mechanism to detect a rotation angle of a rotation body includes a first detection unit to cause a first output value to constantly change in response to an angle change of the rotation body in the entire region of a specific rotation range and to set a change quantity of the first output value relative to the angle change in a first rotation region of the specific rotation range to be greater than a change quantity in a non-first rotation region, and a second detection unit to cause a second output value to constantly change in response to an angle change and to set a change quantity of the second output value in a second rotation region including a rotation region different from the first rotation region to be greater than a change quantity in a non-second rotation region. | 2019-06-20 |
20190186386 | ENGINE STOPPING DEVICE - There is provided an engine stopping device including a stopping solenoid, where an operating shaft, interlocked to a control rack of a fuel injection pump, is rotatably supported by an engine case in a pass-through manner. The control rack is forcibly movable to a stopping position by an action of the stopping solenoid on an operation arm provided for a projecting portion of the operating shaft in an integrally rotatable manner. An extending-retracting rod of the stopping solenoid and the operation arm are interlocked by fitting engagement between a pin provided for the extending-retracting rod and a cut-out portion of the operation arm. The cut-out portion is configured in a shape elongated along a direction perpendicular to a movement trajectory of the extending-retracting rod. | 2019-06-20 |
20190186387 | COMBINATION CONTROL ASSEMBLY - A combination control assembly for dual fuel internal combustion engine comprises: a bracket ( | 2019-06-20 |
20190186388 | Exhaust Gas Recirculation Blower And Internal Combustion Engine - An exhaust gas recirculation blower of an internal combustion engine, with a stator and a rotor. Assemblies of the stator and the rotor, which serve for conducting exhaust gas, consist of a material that is corrosion-resistant and erosion-resistant when exposed to an acidic atmosphere. | 2019-06-20 |
20190186389 | ENGINE OPERATING SYSTEM AND METHOD - Methods and systems are provided for estimating maximum in-cylinder pressure for all engine cylinders while reducing the number of individual cylinders required for pressure sensing. Pressure sensing is performed for a single instrumented cylinder. For remaining non-instrumented cylinders, an engine speed-dependent correction factor is applied that compensates for compression pressure variation between cylinders due to intake valve closing differences. | 2019-06-20 |
20190186390 | METHOD AND SYSTEM FOR A BOOSTED ENGINE - Methods and systems are provided for improving transient performance in a boosted engine having staged air compression systems. An electric supercharger compressor is staged downstream of a turbocharger compressor in a bypass, airflow diverted from a main intake passage to the bypass via closure of a bypass valve. During selected conditions when the supercharger compressor is not being spun, the bypass valve may be closed to direct air to the engine after flowing through the supercharger in a stand-by mode, thereby enabling a transient increase in torque demand to be rapidly met. | 2019-06-20 |
20190186391 | DUAL FUEL ENGINE CONTROL STRATEGY FOR LIMITING CYLINDER OVER-PRESSURIZATION - A dual fuel engine control system includes a pressure sensor, and an electronic control unit coupled with the pressure sensor and structured to receive cylinder pressure data indicative of cylinder over-pressurization, and to switch the system to a limited gas-to-liquid substitution mode based on the cylinder pressure data indicative of cylinder over-pressurization. The electronic control unit is further structured to return the system to a normal gas-to-liquid substitution mode, receive cylinder pressure data indicative of cylinder over-pressurization after returning the system to the normal gas-to-liquid substitution mode, and responsively output a gas substitution fault signal. | 2019-06-20 |
20190186392 | SYSTEMS AND METHODS FOR VEHICLE FUEL SYSTEM AND EVAPORATIVE EMISSIONS SYSTEM DIAGNOSTICS - Methods and systems are provided for diagnosing a vehicle fuel system for a presence or absence of undesired evaporative emissions. In one example, a method comprises evacuating the fuel system of a vehicle to a variable vacuum target as a function of a volatility of fuel in a fuel tank positioned in the fuel system and a loading state of a fuel vapor storage canister configured for capturing and storing fuel vapors from the fuel tank. In this way, analysis of a pressure-bleedup portion of the diagnostic may be more reliable and completion rates of the diagnostic may be improved, while conducting the test in an environmentally fashion. | 2019-06-20 |
20190186393 | ACTIVE FUEL VAPOR PURGING SYSTEM AND METHOD USING THE SAME - An active fuel vapor purge system includes: a turbocharger having a turbine and a compressor; a canister collecting fuel vapor; a purge pump pumping the collected fuel vapor; a main purge line connecting the canister and the purge pump; a first purge line branched from the main purge line and joined to an intake manifold at downstream of the compressor; a second purge line branched from the main purge line and jointed to an intake line at upstream of the compressor; purge control solenoid valves respectively disposed in the first purge line and the second purge line; a hydrocarbon sensor measuring an amount of hydrocarbon; a pressure sensor measuring an upstream pressure and a downstream pressure of the purge pump; and a controller controlling operation of the purge pump based on the amount of hydrocarbon and pressures at a front end and at a rear end of the purge pump. | 2019-06-20 |
20190186394 | CONTROL SYSTEM FOR COMPRESSION-IGNITION ENGINE - A control system for a compression-ignition engine is provided, which includes an engine having a combustion chamber formed by a cylinder, a piston and a cylinder head, an injector, a spark plug, an exhaust gas recirculation (EGR) device configured to introduce into the combustion chamber a portion of burned gas generated inside the combustion chamber as EGR gas, an EGR controller to change an EGR ratio, the EGR controller changing the EGR ratio so that a compression start temperature of the combustion chamber rises as an engine speed increases, and a controller connected to the injector and the spark plug to control them. The controller includes a processor configured to execute a combustion controlling module to output an ignition instruction to the spark plug so as to ignite at an ignition timing after the EGR ratio adjustment so that partial compression-ignition combustion is performed. | 2019-06-20 |
20190186395 | CONTROL SYSTEM FOR COMPRESSION-IGNITION ENGINE - A control system for a compression-ignition engine is provided, which includes an engine having a combustion chamber formed by a cylinder, a piston and a cylinder head, an injector, a spark plug, an exhaust gas recirculation (EGR) device configured to introduce into the combustion chamber a portion of burned gas generated inside the combustion chamber as EGR gas, an EGR controller configured to change an EGR ratio, the EGR controller changing the EGR ratio so that a compression start temperature of the combustion chamber rises as an engine load is reduced, and a controller connected to the injector and the spark plug to control them. The controller includes a processor configured to execute a combustion controlling module to output an instruction to the spark plug so as to ignite at an ignition timing after the EGR ratio adjustment so that partial compression-ignition combustion is performed. | 2019-06-20 |
20190186396 | CONTROL SYSTEM FOR COMPRESSION-IGNITION ENGINE - A control system for a compression-ignition engine is provided, which includes an engine having a combustion chamber, an injector, a spark plug, a swirl valve provided to an intake passage of the engine, and a controller connected to the injector, the spark plug, and the swirl valve to control them. The controller includes a processor configured to execute a swirl adjusting module to control an opening of the swirl valve so as to make the opening of the swirl valve smaller as an engine speed decreases and output a control signal to the injector to inject the fuel after the control of the swirl valve, and a combustion controlling module to output an ignition instruction to the spark plug so as to ignite at a given ignition timing after the EGR ratio adjustment, so that partial compression-ignition combustion is performed. | 2019-06-20 |
20190186397 | SYSTEMS AND METHOD FOR A COLD START SYSTEM FOR A GASEOUS FUEL ENGINE - Apparatuses, methods, and systems for starting an internal combustion engine under cold start conditions are disclosed. A combustible mixture is supplied to a plurality of cylinders of the internal combustion engine, where a number of ignition devices are operably connected with less than all of the plurality of cylinders so that at least one of the plurality of cylinders does not include an ignition device. In one form, only one ignition device is included in a bank of cylinders. In response to a cold start condition, a spark by the plurality of ignition devices is generated to cause ignition of the combustible mixture and start the internal combustion engine. In response to a normal or non-cold starting condition, the internal combustion engine is started by compression ignition where none of the ignition devices generate a spark. | 2019-06-20 |
20190186398 | DETERMINATION OF PRESSURIZED FUEL TEMPERATURE - A method and a system for determining a temperature for pressurized fuel included in a high pressure fuel system arranged for providing fuel to an engine are presented. The method includes determining a first temperature for a first fuel volume included in a first section of the high pressure fuel system, where the first section includes a common rail fuel system. The method further includes determining a second temperature for a second fuel volume included in a second section of the high pressure fuel system, where the second section includes at least one fuel injector arranged in a cylinder head of the engine. The method also includes the step of determining the temperature for the pressurized fuel based at least on the first temperature and on the second temperature. | 2019-06-20 |
20190186399 | EXHAUST PIPE TEMPERATURE ESTIMATION DEVICE AND SENSOR HEATER CONTROL APPARATUS FOR EXHAUST GAS SENSOR USING EXHAUST PIPE TEMPERATURE ESTIMATION DEVICE - Provided are a novel exhaust pipe temperature estimation device and a sensor heater control apparatus for an exhaust gas sensor using the same that accurately estimates an estimation exhaust pipe temperature when an internal combustion engine is stopped and restarted in response to a change of an environmental condition of the internal combustion engine and controls an operation of a sensor heater based on the estimated estimation exhaust pipe temperature. Thus, at least first correction information Tz based on a change of an exhaust pipe temperature and an elapsed time at stop, second correction information Ty based on a change of an internal combustion engine temperature at the stop of the internal combustion engine, and third correction information Tz based on a change of a cooling degree due to outdoor air during stop from the stop to restart are obtained, an estimation exhaust pipe temperature at the stop is corrected using at least one or more pieces of the correction information at restart of the internal combustion engine to estimate an estimation exhaust pipe temperature at the restart, and an estimation exhaust pipe temperature during an operation of the internal combustion engine thereafter is obtained using the estimation exhaust pipe temperature as an initial value, and further, a heating operation of a sensor heater is started when the estimation exhaust pipe temperature becomes equal to or higher than a predetermined value. | 2019-06-20 |
20190186400 | FLOW RATE DETECTOR - A flow rate detector includes a detection circuit, which is configured to output as an analog signal a voltage in accordance with a flow rate of air flowing through an intake pipe, and a conversion circuit, which is configured to convert the analog signal input from the detection circuit to a digital signal based on an analog-to-digital conversion characteristic to output the digital signal. The analog signal that corresponds to a forward flow direction and is input to the conversion circuit is set to have a value larger than an input voltage range in which a missing code may occur in the analog-to-digital conversion characteristic. | 2019-06-20 |
20190186401 | VARIABLE DISPLACEMENT ENGINE DIAGNOSTIC METHOD - Methods and systems are provided for diagnosing a variable displacement engine. In one example, a method includes during steady-state vehicle cruising, operating an engine with one or more cylinders of the engine deactivated, commanding the one or more cylinders to reactivate, and indicating cylinder valve actuator degradation responsive to a fuel usage change following the command to reactivate. | 2019-06-20 |
20190186402 | CONTROL SYSTEM FOR COMPRESSION-IGNITION ENGINE - A control system for a compression-ignition engine is provided, which includes an engine having a combustion chamber, an injector configured to supply fuel into the combustion chamber, a spark plug, a swirl valve provided to an intake passage of the engine, and a controller. The controller includes a processor configured to execute a swirl adjusting module to adjust a swirl valve opening to generate a swirl flow inside the combustion chamber, a fuel injection amount controlling module to control fuel injection amounts of pre-injection and post-injection so as to increase a ratio of an injection amount of the post-injection to a total fuel injection amount into the combustion chamber in one cycle as an engine speed increases, and a combustion controlling module to control the spark plug to ignite at a given ignition timing after the swirl generation and fuel injection, so that partial compression-ignition combustion is performed. | 2019-06-20 |
20190186403 | FUEL PUMP CONTROL DEVICE - A fuel pump controller performs a feedback control of an actual fuel pressure of a feed pump to a command fuel pressure which is from an external element. The pump controller changes a gain for the feedback control to a value larger than a minimum value of the gain in response to an acceleration command information which is to accelerate a vehicle by using an internal combustion engine. | 2019-06-20 |
20190186404 | ENGINE WITH MINIMUM HEAT TRANSFERRED STRUCTURE - An engine with a reduced cooling loss, may include a cylinder block and a cylinder head, wherein an entire combustion chamber volume of the cylinder block and the cylinder head is 300 cc-700 cc, a compression ratio is 10.0 or more, and the volume of the cylinder head is 40%-70% of the entire combustion chamber volume. | 2019-06-20 |
20190186405 | CONTROL SYSTEM FOR COMPRESSION-IGNITION ENGINE - A control system for a compression-ignition engine is provided, which includes an engine having a combustion chamber, an injector configured to supply fuel into the combustion chamber, a spark plug, a swirl valve provided to an intake passage of the engine, and a controller connected to the injector, the spark plug and the swirl valve to control them. The controller includes a processor configured to execute a swirl adjusting module to adjust an opening of the swirl valve to generate a swirl flow inside the combustion chamber, a fuel injection timing controlling module to control a fuel injection timing and control the injector to retard the fuel injection timing as an engine speed increases, and a combustion controlling module to control the spark plug to ignite at a given ignition timing after the swirl generation and the fuel injection, so that partial compression-ignition combustion is performed. | 2019-06-20 |
20190186406 | CONTROLLER FOR INTERNAL COMBUSTION ENGINE - A controller includes an injection control unit configured to set an injection start timing of fuel based on an engine speed to start injecting the fuel with a cylinder injection valve during an intake stroke. The injection start timing set by the injection control unit when the engine speed is equal to a specified engine speed is referred to as a specified timing. The injection control unit is configured to set the specified timing as the injection start timing or retard the injection start timing from the specified timing when the engine speed is in a range that is higher than the specified engine speed. | 2019-06-20 |
20190186407 | CYLINDER LINER FOR AN INTERNAL COMBUSTION ENGINE AND METHOD OF FORMING - A method of forming an engine is provided. A liner is cast with an outer surface with a first texture extending circumferentially from a first end to a second end of the liner. A circumferential section of the outer surface of the liner is coated with an insulative, thermoset material with a lower thermal conductivity than the texture. An engine and a cylinder liner for the engine are provided. The liner has first and second ends with an outer surface extending therebetween. An outer surface of the liner has axial sections defining a texture and an insulative thermoset coating to form material interfaces with the block with different thermal conductivities thereacross. | 2019-06-20 |
20190186408 | FLOW CONTROL VALVE AND COOLING CIRCUIT FOR VEHICLES WITH FLOW CONTROL VALVE - A cooling circuit for a vehicle may include a plurality of cylinder heads into which cooling water is continuously introduced from a plurality of cylinder blocks oppositely disposed parallel with each other, wherein a flow control valve may include a head port, through which the cooling water discharged from the plurality of cylinder heads is joined and the joined cooling water is introduced into the flow control valve, and wherein the flow control valve also may include a set of ports including a radiator port, a heat exchanger port, and a heater core port, through which the cooling water introduced into the flow control valve is discharged towards a radiator, an oil heat exchanger, and a heater core, respectively. | 2019-06-20 |
20190186409 | CYLINDER HEAD FOR ONE INTERNAL COMBUSTION ENGINE - A cylinder head for an internal combustion engine is provided, whereby the cylinder head has a cylinder head gasket region for closing a combustion chamber with a diameter. The cylinder head includes the following:
| 2019-06-20 |
20190186410 | HIGH STRENGTH ALUMINUM ALLOY, INTERNAL COMBUSTION ENGINE PISTON COMPRISING SAID ALLOY, AND METHOD FOR MANUFACTURING INTERNAL COMBUSTION ENGINE PISTON - An aluminum alloy having excellent high temperature strength and thermal conductivity; and an internal combustion engine piston including the alloy. The aluminum alloy includes 11.0-13.0% Si, ≤0.3% Fe, 0.3-2.0% Mg, 2.0-5.0% Cu, 3.0-4.0% Ni, 0.2-1.0% Mn, 0.05-0.4% Cr, and 0.05-0.4% V, with the remainder including aluminum and unavoidable impurities. | 2019-06-20 |
20190186411 | CYLINDER SYSTEM WITH RELATIVE MOTION OCCUPYING STRUCTURE - Implementations are disclosed herein that relate to a cylinder occupying structure. An example provides a cylinder system comprising a mechanical cylinder including an internal space in which a fluid is introduced, and a piston configured for reciprocating motion in the internal space, and a cylinder occupying structure including an insertion rod acting as a second piston, wherein the insertion rod is variably inserted into, and retracted from, the internal space of the cylinder in correspondence with the reciprocating motion of the piston and where parts of the insertion rod and the piston may surround the combustion space. | 2019-06-20 |
20190186412 | Rebuildable Engine Casing and Oil Squirter Assembly for Air Cooled Internal Combustion Engines - The present invention is directed to a rebuildable engine casing for an internal combustion engine supporting a plurality of pistons. The engine casing forms and provides a novel oil squirter that can readily be serviced or rebuilt. The engine casing also includes a novel mechanism for separating the case members and a removable service plug for accessing the oil galleries. The present invention also provides for a rebuildable oil squirter. | 2019-06-20 |
20190186413 | LADDER FRAME FOR INTERNAL COMBUSTION ENGINE - A ladder frame for an internal combustion engine includes a first lateral wall and a second lateral wall, crank caps, and first joining portions and second joining portions. Each crank cap includes an arc-shaped center portion, a first lateral portion and a second lateral portion. Each first lateral portion is joined to the first lateral wall via each first joining portion, and each second lateral portion is joined to the second lateral wall via each second joining portion. Each center portion includes a supporting portion that rotatably supports the crankshaft, the center portion including a recess to which the residual portion is joined, on the opposite side to the supporting portion. Respective thicknesses of the first lateral portion and the second lateral portion are the same as that of the center portion. The recess is provided with a projection embedded in the residual portion. | 2019-06-20 |
20190186414 | SOLAR AIR CONDITIONING HEAT PUMP WITH MINIMIZED DEAD VOLUME - A method and apparatus that reduces the dead volume in a heat engine or heat pump, such as a duplex Stirling or Vuilleumier cycle device, by nesting the components of the displacer and regenerator such that nearly all working fluid is purged from the interstices of the regenerator elements and all other working fluid spaces that are not involved in doing useful work at each portion of the cycle. Particularly, a more scalable and efficient method and apparatus for providing solar air conditioning or refrigeration by means of a heated cylinder that alternately pressurizes and depressurizes a separate cooling cylinder by directly transferring thermally induced pressure changes to that cooling cylinder at optimized times in the cycle, under the control of a numerically controlled actuation system that can cycle at a much lower rate than mechanically coupled or harmonically phased systems. | 2019-06-20 |
20190186415 | WASTE HEAT RECOVERY SYSTEM WITH LOW TEMPERATURE HEAT EXCHANGER - Systems and methods are disclosed to recover waste heat from an engine fluid with a heat exchanger subsystem that includes a heat exchanger. The heat exchanger subsystem is thermally coupled to a working fluid and the engine fluid, so the waste heat from the engine fluid is transferred to the working fluid. The engine fluid is bypassed from the heat exchanger in response to a heat exchanger bypass condition. | 2019-06-20 |
20190186416 | AN INTEGRATED TEST METHOD FOR TESTING THE ELECTRICAL OPERATION OF A THRUST REVERSER OF AN AIRCRAFT TURBOJET, AND AN ASSOCIATED SYSTEM - An integrated test method for testing the operation of an electrical power converter powered by an on-board power supply network and using field-oriented control to control a three-phase electric motor for a thrust reverser of a turbojet of an aircraft is provided. The method includes: receiving an order to initiate the integrated test; controlling the converter from a current setpoint defined from a non-zero in-phase component and a zero quadratic component; measuring the currents delivered on each of the three outlet phases of said converter; determining in-phase and quadratic components of the three phase currents previously measured; comparing these components with the in-phase and quadratic components of the current setpoint; and sending a notification concerning the malfunctioning or the functioning of the thrust reverser as a function of the result of the comparison. | 2019-06-20 |
20190186417 | TURBINE MODULE FOR A TURBOMACHINE - The present invention relates to a turbine module for a turbomachine, comprising a first flow bypass structure and a second flow bypass structure, said flow bypass structures being arranged in a hot gas duct, which is bounded by the turbine module and is designed to convey a hot gas and, namely, being arranged in succession in relation to a longitudinal axis of the turbine module in a direction of rotation, wherein, in relation to the bypass flow in the hot gas duct, the flow bypass structures each have a leading edge, and, downstream thereto, a trailing edge, and the second flow bypass structure is provided as a deflecting blade, wherein the second flow bypass structure has a smaller profile thickness than the first flow bypass structure, and wherein the hot gas duct is enclosed by a radial width. | 2019-06-20 |
20190186418 | Multi-Hybrid Aircraft Engine - A multi-hybrid aircraft engine that includes a primary compressor | 2019-06-20 |
20190186419 | Fluid Injector and Needle for a Fluid Injector - Various embodiments include a fluid injector comprising: an injector housing defining a fluid path; a needle within the housing and movable to a closed position and an open position. The needle comprises two axial ends, an end face on the second, and an axial needle section surrounded by the housing. Between the axial section and the surrounding housing, there is a gap comprising at least part of the fluid path. The needle includes a hole extending from the end face and a connecting hole providing fluid connection between the hole and the gap. The valve also includes a plate defining a through-hole. A first valve seat is defined at a surface of the plate facing the end face and adjoining the through-hole and when the needle is in the closed position the through-hole is closed by the end face. | 2019-06-20 |
20190186420 | WATER INJECTOR CONTROL METHOD FOR IMMEDIATE WATER INJECTION AND ENGINE DRIVEN BY METHOD - Disclosed herein are a method of controlling a water injector for immediate water injection and an engine driven by the method. A method of controlling an operation of a water injector for injecting water into the combustion chamber of an engine to which a turbo system for increasing the amount of air by pressing air has been applied includes detecting water pressure applied to a water supply pipe for supplying water to the water injector, stopping an operation of a water supply pump when the detected data reaches a preset reference value, detecting a temperature of water within the water supply pipe for supplying the water to the water injector, and returning the water within the water supply pipe to a water storage tank and driving the water supply pump to supplying new water to the water supply pipe when the detected data deviates from a preset range. | 2019-06-20 |
20190186421 | METHOD OF CONTROLLING WATER INJECTOR FOR PREVENTING DAMAGE TO CATALYST FOR EXHAUST GAS PURIFICATION AND ENGINE DRIVEN BY METHOD - Disclosed are a method of controlling a water injector for preventing damage to a catalyst for exhaust gas purification and an engine driven by the method. A method of controlling the operation of an injector for injecting water into the combustion chamber of an engine to which a turbo system for increasing the amount of air by compressing air has been applied includes a catalyst state determination step of determining the danger condition of a catalyst for exhaust gas purification by detecting the state of the catalyst, a water injection amount calculation step of calculating a water injection flow value F | 2019-06-20 |
20190186422 | SYSTEMS AND METHODS FOR VEHICLE FUEL SYSTEM AND EVAPORATIVE EMISSIONS SYSTEM DIAGNOSTICS - Methods and systems are provided for diagnosing a vehicle fuel system for a presence or absence of undesired evaporative emissions. In one example, a method comprises conducting a test for undesired evaporative emissions stemming from a fuel system of a vehicle via in a first operating mode, evacuating the fuel system to a variable vacuum level through an entirety of a fuel vapor canister configured to capture and store fuel vapors, and in a second operating mode, evacuating the fuel system to the variable vacuum level through a portion of the fuel vapor canister. In this way, the diagnostic may be conducted in an environmentally friendly fashion, where analysis of a bleed-up portion of the test is not impacted by fuel volatility at the time of the diagnostic. | 2019-06-20 |
20190186423 | CANISTER PURGE SYSTEM AND METHOD FOR DIAGNOSING PURGE VALVE THEREOF - A method for diagnosing a purge valve of a canister purge system includes (a) determining whether a purge valve, which is installed on a purge pipe connecting a canister with an intake system of an engine, is open and whether a purge pump is running, wherein the purge pump is configured to pump evaporative emission captured in the canister toward the intake system, and (b) determining whether the purge valve is in a close stuck state, based on upstream pressure and downstream pressure of the purge pump, when the purge valve is open while the purge pump is running. | 2019-06-20 |
20190186424 | PURGE CONTROL SOLENOID VALVE - A purge control solenoid valve may include a middle housing in which an inlet flow path is formed and a middle flow path is formed on a center; a valve housing in which a driving module selectively communicating the inlet flow path and the middle flow path is installed; an upper cover coupled to the upper part of the middle housing and including a upper flow path selectively communicated with the middle flow path on the center; and a membrane provided on the upper cover and selectively communicating the middle flow path and the upper flow path. | 2019-06-20 |
20190186425 | Canister - A canister includes a case having a fluid channel formed therein. In addition, the canister includes an adsorption chamber disposed in the fluid channel and containing an adsorbent. Further, the canister includes a filter disposed within the adsorption chamber and extending across an end portion of the adsorption chamber. The case may include a filter supporting portion facing the outer peripheral edge of the filter. The filter supporting portion may include fused portions to which the peripheral edge of the filter may be fusion-bonded and may also include non-fused portions to which the peripheral edge of the filter may not be fusion-bonded. The fused portions and the non-fused portions both may be disposed in an alternating manner in a lengthwise direction of the filter supporting portion about the filter supporting portion. | 2019-06-20 |
20190186426 | CANISTER - A canister includes a charge port, a purge port, an atmosphere port, a main chamber, a sub chamber, activated carbon, and more activated carbon. The charge port takes in evaporated fuel. The purge port discharges the evaporated fuel. The atmosphere port is open to the atmosphere. The charge port and the purge port are connected to the main chamber. The sub chamber communicates with the main chamber. The atmosphere port is connected to the sub chamber. The activated carbon is stored in a main volume (Vmain) in the main chamber. The more activated carbon is stored in a sub volume (Vsub) in the sub chamber. A ratio of a length L in a gas flow direction to an equivalent diameter D in a section perpendicular to the gas flow direction is 2 or more for the sub chamber. An activated carbon volume ratio (Vmain/Vsub) is 5.5 to 7. | 2019-06-20 |
20190186427 | ENGINE SYSTEM - An engine system includes: an engine having a combustion chamber generating a driving torque by combust of a fuel; a plurality of intake lines through which outside air flows to the combustion chamber; an exhaust manifold connected to the combustion chamber at an exhaust side; at least two electric superchargers disposed on the plurality of intake lines, respectively; and an exhaust gas recirculation (EGR) system including a recirculation line branched from the exhaust manifold and joined to one of the plurality of intake lines and a recirculation valve disposed on the recirculation line. | 2019-06-20 |
20190186428 | COOLER FOR VEHICLE - A cooler for a vehicle includes: a cooler housing; tubes disposed inside the cooler housing; cooling pins arranged inside the tubes in a predetermined pattern; and a cup plate attached to both ends of the cooler housing, including a first core material and a first bonding layer bonded at both outer surfaces of the first core material, and having a plurality of slots penetrating the first bonding layer and the first core material in a thickness direction. Each of the tube has an end part penetrating each of the slots and includes a second core material and a second bonding layer that is in contact with an interior surface of the slots, the second bonding layer is in contact with the first bonding layer and the first core material, and the first bonding layer includes a material having a corrosion potential lower than that of the second bonding layer. | 2019-06-20 |
20190186429 | RECIRCULATION VALVE - A recirculation valve of an exhaust gas recirculation apparatus includes: a valve housing having a gas inlet into which a recirculation gas flows, a gas outlet from which the recirculation gas is discharged, and an intermediate inlet disposed between the gas inlet and the gas outlet; and a valve body selectively opening and closing the gas inlet and the intermediate inlet. | 2019-06-20 |
20190186430 | EXHAUST GAS RECIRCULATION COOLER - An EGR cooler in the disclosure includes: a gas path configured to allow an EGR gas to flow; a refrigerant path configured to perform heat exchange between the EGR gas circulating along the gas path and a refrigerant; an exothermic body containing portion configured such that an exothermic body to generate heat by adsorbing a predetermined working gas is contained within the EGR cooler and at least a part of the exothermic body contacts with a wall surface of the gas path; a working gas tank in which the working gas is stored; and a gas moving apparatus configured to move the working gas stored in the working gas tank, from the working gas tank to the exothermic body containing portion. | 2019-06-20 |
20190186431 | TUBE, IN PARTICULAR A FLAT TUBE FOR AN EXHAUST GAS COOLER AND EXHAUST GAS COOLER | 2019-06-20 |
20190186432 | EGR COOLER FOR VEHICLE - An exhaust gas recirculation (EGR) cooler may include a housing forming the receiving space and in which a coolant inflow hole and a coolant exhaust hole are respectively formed so that a coolant of the cylinder block flows into and out, a cover plate mounted on the housing to close the receiving space and in which an exhaust gas inflow hole and an exhaust gas outflow hole are respectively formed so that an exhaust gas flows into and out, a core including both side caps in which a penetration hole respectively connected to the exhaust gas inflow hole and the exhaust gas outflow hole in the receiving space and a tube through which the exhaust gas communicates while connecting both the side caps to each other, and a connector respectively connecting the penetration hole of the cap to the exhaust gas inflow hole and the exhaust gas outflow hole of the cover plate. | 2019-06-20 |
20190186433 | EXHAUST GAS COOLER AND EXHAUST GAS RECIRCULATION SYSTEM WITH AN EXHAUST GAS COOLER - An exhaust gas cooler ( | 2019-06-20 |
20190186434 | DEVICE FOR HEAT TRANSFER - Device for heat transfer and method for making it, the device having a housing with a heat exchanger disposed within and completely enclosed by the housing having a receiving element and cover element integrated within receiving element. First fluid flows through heat exchanger to be cooled; another fluid flows around heat exchanger. Heat transfer elements are shaped as a plate of a first jacket element and a second jacket element as well as a fin element; each includes a throughflow sector for inflow and outflow of first fluid. Each throughflow sector is developed on a front face of heat transfer element. Fin element has a lesser dimension in a longitudinal direction than jacket elements and is disposed therebetween such that in the proximity of a second front face, located distally to first front face, a free region is developed for deflecting direction of flow of first fluid. | 2019-06-20 |
20190186435 | Fuel Injection Using a Dielectric of a Resonator - An example system can include a radio-frequency power source and a resonator. The resonator can be configured to be electromagnetically coupled to the radio-frequency power source and can have a resonant wavelength. The resonator can include: a first conductor, a second conductor, and a dielectric between the first conductor and the second conductor. The resonator can also be configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter of the resonant wavelength, the resonator provides at least one of a plasma corona or electromagnetic waves. The system can also include a fuel conduit configured to couple to a fuel source and having one or more outlets for expelling fuel, where at least a portion of the fuel conduit is arranged proximate to the dielectric. | 2019-06-20 |
20190186436 | SYSTEM INCLUDING OXYGEN SEPARATION DEVICE - An oxygen separation device includes a substrate and an oxygen ion transport membrane supported on the substrate. The substrate has an air inlet end and a retentate outlet end. An intake air passageway extends through the substrate from the air inlet end to the retentate outlet end. The oxygen ion transport membrane is between the substrate and the intake air passageway and is adapted to separate oxygen atoms from the air in the intake air passageway and to transport the oxygen atoms to the substrate. The oxygen separation device collects the oxygen from the substrate for supply to an internal combustion engine for use as the gas of the gas-fuel mixture. | 2019-06-20 |
20190186437 | Electromagnetic Wave Modification of Fuel in a Jet Engine - Example implementations relate to electromagnetic wave modification of fuel in a jet engine. An example implementation includes a jet engine. The jet engine includes a combustion chamber, a radio-frequency power source, and a fuel conduit configured to provide a fuel to the combustion chamber. In addition, the jet engine includes a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength. The resonator includes a first conductor, a second conductor, and a dielectric between the first conductor and the second conductor. The resonator is configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength, the resonator radiates electromagnetic waves usable to modify (i) the fuel within the fuel conduit or (ii) a fuel mixture, which includes the fuel, within the combustion chamber. | 2019-06-20 |
20190186438 | Electromagnetic Wave Modification of Fuel in a Power-generation Turbine - Example implementations relate to electromagnetic wave modification of fuel in a power-generation turbine. An example implementation includes a power-generation turbine. The power-generation turbine includes a combustion chamber, a radio-frequency power source, and a fuel conduit configured to provide a fuel to the combustion chamber. In addition, the power-generation turbine includes a resonator configured to electromagnetically couple to the radio-frequency power source and having a resonant wavelength. The resonator includes a first conductor, a second conductor, and a dielectric between the first conductor and the second conductor. The resonator is configured such that, when the resonator is excited by the radio-frequency power source with a signal having a wavelength proximate to an odd-integer multiple of one-quarter (¼) of the resonant wavelength, the resonator radiates electromagnetic waves usable to modify (i) the fuel within the fuel conduit or (ii) a fuel mixture, which includes the fuel, within the combustion chamber. | 2019-06-20 |
20190186439 | Gasoline Vaporization System And Methods For An Internal Combustion Engine - The present invention provides a novel apparatus and method for the gasification of liquid petroleum fuel (gasoline), that has been atomized and emulsified with atmospheric air, by implementing a multi-Stage Heat Exchanger System. | 2019-06-20 |
20190186440 | PROPANE FUEL SYSTEM TEMPERATURE CONTROL SYSTEMS AND METHODS - Systems and methods for thermal management of a direct injection propane fuel system are disclosed that include control a temperature of the fuel tank at or below a desired operating temperature to avoid venting of fuel to atmosphere. | 2019-06-20 |