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Patent # Description
2016/0177843 AIR SHUTOFF SWING GATE VALVE
An air shutoff valve includes a passage for supplying air, a swing gate, a shaft attached to a reset handle, and a spring to urge the gate toward its closed...
2016/0177842 Method For Operating A Fuel Injection System Of An Internal Combustion Engine
A method for operating a fuel injection system of an internal combustion engine is disclosed. The fuel injection system comprises a high pressure accumulator...
2016/0177841 PLANETARY GEAR SYSTEM FOR TURBOMACHINE
A planetary gear system for a turbomachine includes a forward planetary gear assembly including a plurality of forward planet gears meshed to a forward sun...
2016/0177840 AUXILIARY COMPONENT MOUNTS
A mount for mounting a component to a gas turbine engine is disclosed. The mount may include a central portion that attaches to the component, and a flange...
2016/0177839 METHOD FOR MONITORING A COLD START OF A BRAYTON CYCLE POWER GENERATION SYSTEM
A method for monitoring cold start of Brayton cycle power generation system comprises: measuring an ambient temperature to obtain a Brayton cycle predetermined...
2016/0177838 FUEL CIRCUIT OF AN AIRCRAFT ENGINE WITH A FUEL RECIRCULATING VALVE CONTROLLED BY A PRESSURE DIFFERENTIAL OF A...
A fuel circuit of an aircraft engine including a fuel tank; an engine fuel system including a low-pressure pump and a high-pressure pump, and a fuel...
2016/0177837 FUEL/AIR MIXING SYSTEM FOR FUEL NOZZLE
A fuel nozzle includes an inner wall defining a central passage extending in an axial direction of the fuel nozzle, a hub wall surrounding the inner wall and...
2016/0177836 GAS TURBINE FUEL PIPE COMPRISING A DAMPER
The invention concerns a gas turbine fuel pipe, having a fuel line, the fuel line having a fuel line volume, a fuel line outer wall and an opening in the fuel...
2016/0177835 GAS TURBINE ENGINE WITH ANGULARLY OFFSET TURBINE VANES
A gas turbine engine includes a combustor having a plurality of fuel nozzles arranged circumferentially equidistant from one another about a first center. The...
2016/0177834 FUEL NOZZLE STRUCTURE
A gas turbine engine fuel nozzle apparatus includes: an annular outer body, the outer body extending parallel to a centerline axis, and having a generally...
2016/0177833 ENGINE AND METHOD FOR OPERATING SAID ENGINE
Disclosed is an engine, the engine having a compressor, an expansion machine, and a shaft, the shaft having a direction of rotation. The engine includes a...
2016/0177832 MIXER FOR ADMIXING A DILUTION AIR TO THE HOT GAS FLOW
The invention refers to a combustor arrangement of a gas turbine engine or power plant, having at least one combustion chamber, at least one mixer for admixing...
2016/0177831 COOLING-AIR SUPPLY DEVICE FOR A GAS TURBINE
A cooling-air supply device for a gas turbine, in particular an aircraft gas turbine, including a cooling air chamber, that is disposed about a turbine shaft...
2016/0177830 DIFFUSER CASE MIXING CHAMBER FOR A TURBINE ENGINE
A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication...
2016/0177829 MICROCHANNEL HEAT EXCHANGERS FOR GAS TURBINE INTERCOOLING AND CONDENSING
A gas turbine engine heat exchange system includes a first microchannel heat exchanger (MCHX) configured to transfer heat between a first air stream and a...
2016/0177828 STAGED HEAT EXCHANGERS FOR MULTI-BYPASS STREAM GAS TURBINE ENGINES
A gas turbine bypass flow arrangement comprises an outer housing and an inner housing, an outer bypass duct defined between the outer housing and the inner...
2016/0177827 GAS TURBINE POWER PLANT MADE FLEXIBLE
A gas turbine power plant includes a gas turbine having a compressor, combustion chamber, and expander and is rotationally mechanically coupled to an...
2016/0177826 PROCESS AND CONFIGURATION TO OBTAIN A COMPRESSED GAS
The invention is directed to a process to increase pressure and temperature of a feed gas by means of indirect heat exchange against a fluid having a higher...
2016/0177825 AIRCRAFT ENGINE HAVING A DEVICE FOR SEPARATING OIL
An aircraft engine having at least two shafts, each mounted rotatably about a center axis of the aircraft engine. A first shaft is driven, during operation of...
2016/0177824 GAS TURBINE ENGINE INTAKE DUCT
A gas turbine engine intake duct 30, 80, 100 having an internal duct surface 54 comprising a main region 60, 82 having a particular finish and a secondary...
2016/0177823 SYSTEM AND METHOD WITH INLET PARTICLE SEPARATOR
A turbine engine system includes an inlet particle separator receiving an inlet fluid flow and having a clean outlet for a first flow of substantially clean...
2016/0177822 Hybrid Power Generation System
A system includes a primary, combustion turbine based system that includes one or more power shaft assemblies including a generator or motor/generator, a...
2016/0177821 Generating Power Using an Ion Transport Membrane
In some implementations, a system may include a compressor, a heat exchanger and an ITM. The compressor is configured to receive an air stream and compress the...
2016/0177820 LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM WITH SAFE PYLON TRANSIT
A gas turbine engine includes a fan section delivering air into a compressor section. The compressor section compresses air and delivers air into a combustion...
2016/0177819 SIMPLIFIED ENGINE BLEED SUPPLY WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT
A gas turbine engine assembly for an aircraft includes a fan section delivering air into a main compressor section. The main compressor section includes a...
2016/0177818 INTERNAL COMBUSTION ENGINE AND MANUFACTURING METHOD THEREFOR
In an internal combustion engine in which an anodic oxide film (10) is formed on part or all of a wall surface facing a combustion chamber, the anodic oxide...
2016/0177817 FAILURE DETECTION DEVICE OF INTERNAL COMBUSTION ENGINE
During normal engine operation, a temporary determination mode is executed in which whether or not there is an air-fuel ratio variation among cylinders is...
2016/0177816 TWO-STROKE ENGINE
A two-stroke engine working on the Miller/Atkinson cycle, wherein a space underside the piston crown is divided by a separator into two complimentary sections...
2016/0177815 Exhaust Nozzle Tip Device and System
An exhaust nozzle tip for an exhaust runner conveying a first flow of an exhaust gas includes an inlet, outlet, and nozzle passageway. The inlet receives a...
2016/0177814 Removal of Heat in Exhaust Shielding with Jacket Fluid Cooled Components
An enclosure that encloses turbocharged engines that includes a first and a second turbochargers of the turbocharged engines, the first and second ...
2016/0177813 METHOD AND SYSTEM FOR CHARGE AIR COOLER CONDENSATE CONTROL
Methods and systems are provided for controlling a condensate level in a charge air cooler. In one example, a method may include adjusting an air flow to a...
2016/0177812 METHOD FOR CONTROLLING A TWO-STROKE INTERNAL COMBUSTION ENGINE
A method for controlling a two-stroke internal combustion engine, the control method including: a longitudinal movement of a piston in the direction of the...
2016/0177811 VEHICLE COOLING DEVICE
A vehicle cooling device includes: at least one of a radiator and a condenser; a fan cover including a fan configured to cool the at least one of the radiator...
2016/0177810 HEAT EXCHANGER SYSTEM FOR A VEHICLE
A heat exchanger system for a vehicle includes at least one heat exchanger, a centrifugal fan assembly for improving the flow of air through the at least one...
2016/0177809 ENGINE THERMOSTAT WITH INTEGRATED COOLANT FILTER
A thermostat assembly for use with an engine cooling system includes a thermostat, a frame, a bypass valve and an integrated filter. The frame supports the...
2016/0177808 ENGINE COOLING SYSTEM AND METHOD FOR OPERATING THE SAME
An engine cooling system including a refrigerant circulation flow channel passing through an engine, an electric refrigerant pump, an electromagnetic valve...
2016/0177807 ENGINE COOLING SYSTEM FOR MOTORCYCLE
An engine cooling system for a motorcycle of the present invention includes an engine that includes a crankcase and a cylinder, a water pump to supply cooling...
2016/0177806 Exhaust Outlet Elbow Center Divider Connection
An exhaust outlet elbow includes: a body having an outer wall and an interior wall, the interior wall defining, at least in part, a first interior chamber; a...
2016/0177805 EXHAUST APPARATUS OF OUTBOARD MOTOR
An exhaust apparatus of an outboard motor equipped with a four-stroke engine includes an exhaust pipe having a cylindrical shape and being connected to an...
2016/0177804 DIAGNOSTIC SYSTEM FOR INTERNAL COMBUSTION ENGINE
A diagnostic system for an internal combustion engine is disclosed. The diagnostic system may include an electronic control unit. The electronic control unit...
2016/0177803 METHOD FOR CHECKING THE EFFICACY OF AN EXHAUST GAS AFTER-TREATMENT DEVICE
The invention relates to a method for checking the efficacy of an exhaust gas after-treatment device (9), especially of a caatlyst, for an internal combustion...
2016/0177802 Acoustic Energy Cooling Source
An apparatus includes an exhaust system, a cooling system, and two or more thermoacoustic devices. A first thermoacoustic device is configured to convert heat...
2016/0177801 EXHAUST SYSTEM OF AN INTERNAL COMBUSTION ENGINE WITH MIXER FOR A LIQUID REDUCTANT
An exhaust system for an internal combustion engine includes an injection nozzle for injecting a liquid reductant into exhaust gas streaming through the...
2016/0177800 ENGINE EXHAUST GAS ADDITIVE STORAGE SYSTEM
A system for storing a solution of ammonia precursor for use as an exhaust gas additive, the system including: a tank for storing the solution in a liquid...
2016/0177799 Insulated Reductant Tank
An insulated reductant tank that is arranged so that it has an insulated upper portion and a tapered lower portion, the reductant tank configured to allow...
2016/0177798 EXHAUST PURIFICATION SYSTEM OF INTERNAL COMBUSTION ENGINE
An internal combustion engine in which a hydrocarbon feed valve, exhaust purification catalyst, and NO.sub.X selective reduction catalyst are arranged in an...
2016/0177797 TURBOCHARGER ENGINE EXHAUST SYSTEM MOUNTED WITH GASKET HAVING DIFFERENCE IN CROSS SECTION HEIGHT
A turbocharged engine exhaust system mounted with a gasket having a difference in cross section height includes a turbocharger rotatable by exhaust gasses...
2016/0177796 METHOD FOR OPERATING A DRIVE DEVICE AND CORRESPONDING DRIVE DEVICE
A method for operating a drive device having an internal combustion engine and an exhaust gas purification device for exhaust gas of the internal combustion...
2016/0177795 Exhaust Manifold Assembly and System
An exhaust runner includes an exhaust runner inlet, an exhaust nozzle outlet aperture, and an impingement insulator. The exhaust runner inlet is configured to...
2016/0177794 METHOD FOR REMOVING SOOT FROM EXHAUST GASES
A method for oxidizing soot from diesel exhaust gas from a diesel engine. The method involves providing a diesel particulate filter for receiving the diesel...
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