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Patent # Description
2016/0195017 Recuperated Gas Turbine Engine
A gas turbine engine that includes a compressor, a turbine, a heat exchanger, and a combustor. The compressor is mounted on a rotating shaft with at least one...
2016/0195016 OIL BEARING WITH DRAIN SYSTEM, GAS TURBINE COMPRISING SUCH AN OIL BEARING
An oil bearing to support a rotor of a turbine, especially of a gas turbine, wherein the rotor extends along a rotor axis coinciding with a bearing axis, has...
2016/0195015 GAS TURBINE ENGINE NOSECONE ATTACHMENT STRUCTURE
A single piece nosecone with support ring and fastening method providing smooth aerodynamic flow into a gas turbine engine is disclosed. The support ring may...
2016/0195014 Membrane Technology for Use in a Power Generation Process
Disclosed herein is a power generation process in which a portion of the carbon dioxide generated by gaseous fuel combustion is recycled back to the power...
2016/0195013 CRYOGENIC FUEL COMPOSITIONS AND DUAL FUEL AIRCRAFT SYSTEM
Cryogenic fuel compositions including a cryogenic fuel and paraxyelene and a dual fuel aircraft system for an aircraft having at least one turbine engine,...
2016/0195012 TURBOMACHINE PROVIDED WITH AN ASSEMBLY FOR CONTROLLING THE PITCH VARIATION OF A PROPELLER
The assembly (25) links a static housing (24) of the turbomachine, into which supply lines, in particular fluid supply lines (23), arrive, to the blades of the...
2016/0195011 SPLIT GEAR SYSTEM FOR A GAS TURBINE ENGINE
A gas turbine engine includes a fan section, a compressor section aft of the fan section, a combustor fluidly connected to the compressor section, and a...
2016/0195010 VANELESS COUNTERROTATING TURBINE
A gas turbine engine includes a compressor section, a combustor, and a turbine section. The turbine section includes a first turbine portion and a second...
2016/0195009 Internal Combustion Engine Having at Least One Piston
An internal combustion engine has at least one piston which performs stroke movements in a cylinder crankcase. Via two connecting rods, the piston interacts...
2016/0195008 Two-stroke opposed piston Rotary internal combustion engine with no reactive torque
A two-cycle internal-combustion, rear compression, engine with variable valve timing, activated by air pressure and located at about top dead center. This...
2016/0195007 Combustion Pre-Chamber and Method for Operating Same
An engine includes a main combustion chamber; an intake duct configured to provide a lean fuel-oxidizer mixture to the main combustion chamber; a pre-chamber...
2016/0195006 VARIABLE TURBINE GEOMETRY TURBOCHARGER VANE RING ASSEMBLY RETENTION DEVICE
A variable turbine geometry turbine turbocharger (1) includes a vane ring assembly (29) configured to control flow of exhaust gas to a turbine wheel (12), and...
2016/0195005 Valve
A housing, a solenoid, a pin which can be moved by the solenoid, and a piston which is connected to the pin. The piston is pot-shaped and its base has an...
2016/0195004 WATER INJECTOR FOR AVIATION COOLING SYSTEM
A water injector for an aviation cooling system includes a body having a first end, a second end, and an intermediate portion extending therebetween. A conduit...
2016/0195003 Fuel Gas Feed and Ignition Apparatus for A Gas Engine
For a fuel gas feed and Ignition apparatus for a gas engine (1) with a combustion chamber injection nozzle (12) in which a number of injection channels (37)...
2016/0195002 COOLING WATER CONTROL APPARATUS
A cooling water control apparatus is configured to control a cooling apparatus, wherein the cooling apparatus includes: a first pipe in which the cooling water...
2016/0195001 THERMOSTAT VALVE FOR A COOLANT CYCLE
A thermostat valve for a coolant circuit includes a housing with a plurality of coolant connectors, and at least one hollow valve element mounted in the...
2016/0195000 ENGINE COOLING SYSTEM
A cooling system for an engine includes a block-side water jacket divided into a block cooling passage and a bypass passage in the circumferential direction of...
2016/0194999 METHOD FOR ADJUSTING A GRILLE SHUTTER OPENING
Methods and systems are provided for adjusting a grille shutter opening based on an estimated amount of fuel in oil dilution. In one example, a method may...
2016/0194998 SECONDARY-AIR SYSTEM AND METHOD FOR CHECKING THE OPERABILITY OF THE SECONDARY-AIR SYSTEM
A method for checking the operability of a secondary-air system of an internal combustion engine includes measuring a first pressure between a first...
2016/0194997 ENERGY SYSTEM FOR DWELLING SUPPORT
The present disclosure is directed to a system and method of providing energy to a dwelling. An engine is housed within an inner tank, which is in turn housed...
2016/0194996 DIESEL EXHAUST SYSTEM AND METHOD FOR CONTROLLING EXHAUST FLUID DOSING
A method for controlling dosing of a diesel exhaust fluid includes providing a diesel engine and an exhaust system. The exhaust system includes an exhaust...
2016/0194995 FLOW MIXING DEVICE FOR AN EXHAUST AFTER-TREATMENT SYSTEM
A flow mixing device includes a body having a first end, a second end, and an interior volume defined between them. An inlet plate, coupled to the first end of...
2016/0194994 EXHAUST GAS TREATMENT UNIT COMPRISING FLOW DIVIDING AND MIXING GUIDE ELEMENTS
An exhaust-gas treatment unit includes: a supply line, for exhaust gas, having an entry opening and an exit opening, and a first exhaust-gas treatment body...
2016/0194993 EXHAUST GAS AFTERTREATMENT DEVICE FOR A COMBUSTION ENGINE, IN PARTICULAR OF A MOTOR VEHICLE
An exhaust gas aftertreatment device for a combustion engine is disclosed. The device includes an exhaust pipe element having an exhaust duct through which...
2016/0194992 Engine Exhaust Gas Purifier
In an engine exhaust gas purifier having a urea-SCR-catalyst and an injector, the urea-SCR-catalyst is regenerated periodically to remove stack up sulfur...
2016/0194991 EXHAUST AFTERTREATMENT SYSTEM WITH SILICA FILTER
An exhaust system including an upstream portion, a downstream portion, a service access, and a silica filter defines an exhaust gas flow path. The downstream...
2016/0194990 EXHAUST GAS HEAT EXCHANGER AND SEALING DEVICE FOR THE SAME
An exhaust gas heat exchanger including connection points for the exhaust gas flow, for connecting the exhaust gas heat exchanger to an exhaust gas supply line...
2016/0194989 MOWER WITH IMPROVED EXHAUST GAS COMPONENT COOLING
A mower includes: a driver's seat provided to a vehicle frame. A transmission is arranged at least partially below the driver's seat. An engine arranged...
2016/0194988 HOUSING FOR A CRANKCASE VENTILATION SYSTEM
A housing for a crankcase ventilation system of an engine is provided. The housing includes a plurality of walls connected together and having an outer surface...
2016/0194987 MOUNTING ASSEMBLY FOR OIL MIST SEPARATOR
An assembly for mounting an oil mist separator to a valve cover of an engine is provided. The assembly includes a cylindrical housing having two portions and...
2016/0194986 NETWORK DEVICE AND COMMUNICATION CONTROL METHOD
A network device that is used in a mobile communication system that supports cellular communication in which a data path passes through a core network, and D2D...
2016/0194985 CAM SHAFT PHASE SETTER COMPRISING A CONTROL VALVE FOR HYDRAULICALLY ADJUSTING THE PHASE POSITION OF A CAM SHAFT
A cam shaft phase setter for adjusting the rotational angular position of a cam shaft relative to a crankshaft of an internal combustion engine by a hydraulic...
2016/0194984 INTERNAL COMBUSTION ENGINE
An internal combustion engine includes an exhaust valve, a plurality of cams Ca, Cb, and Cc used to drive the exhaust valve, a cam-switching variable valve...
2016/0194983 MULTI-PRESSURE ORGANIC RANKINE CYCLE
The present disclosure relates to a multi-pressure stage, organic Rankine cycle ("ORC") that includes a dry organic working fluid that flows through a high...
2016/0194982 MULTI STAGE STEAM TURBINE FOR POWER GENERATION
The invention relates to a steam turbine having a plurality of stages comprising a plurality of points of admission connected to a plurality of admission...
2016/0194981 DUAL ANTI SURGE AND ANTI ROTATION FEATURE ON FIRST VANE SUPPORT
A gas turbine engine includes a vane and a combustor housing that are supported relative to an engine static structure. A retaining assembly clamps the...
2016/0194980 GAS TURBINE ENGINE COMPONENT PROVIDING PRIORITIZED COOLING
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform having a non-gas path...
2016/0194979 CANTED BOAS INTERSEGMENT GEOMETRY
A blade outer air seal segment has an inner surface and an outer surface. The outer surface is in communication with a cooling air source. The segment also has...
2016/0194978 Turbine stator vane with insert and flexible seal
An air cooled turbine stator vane with an impingement cooling insert secured within a hollow cavity, where seal slots are formed between the cavity and the...
2016/0194977 TURBINE ENGINE SHAFT BREAK DETECTION
A method of detecting a shaft break in a turbine engine is provided. The shaft connects a torque-exerting turbine of the engine to a torque-receiving unit of...
2016/0194976 BORESCOPE PLUG FOR GAS TURBINE ENGINE
A borescope plug includes a threaded section that extends from a head section along an axis, the threaded section including a central passage along said axis....
2016/0194975 ENERGY RECLAMATION FROM FLUID-MOVING SYSTEMS
A system includes a building, a fluid-moving system, and a turbine system. The fluid-moving system includes one or more conduits in or coupled to the data...
2016/0194974 BOAS WITH RADIAL LOAD FEATURE
This disclosure relates to a gas turbine engine including a blade outer air seal (BOAS) having at least one attachment hook adjacent one of a leading edge and...
2016/0194973 FAN PLATFORM WITH LEADING EDGE TAB
A platform for a gas turbine engine has an outer surface and an inner surface. The inner surface is provided with a mount location for mounting the platform to...
2016/0194972 SEAL AND CLIP-ON DAMPER SYSTEM AND DEVICE
A seal and damper system is provided. The system comprises a blade assembly seal with a central portion defining a recess and a depression. The system also...
2016/0194971 SEAL FOR TURBOFAN ENGINE
A seal for sealing a gap between a vane and a liner of an outlet guide vane is comprised of: a joint section for joining with the liner; a flexible fillet...
2016/0194970 ARRANGEMENT FOR SECURING TURBINE BLADES
An arrangement for securing turbine blades in a groove of an inner housing of a steam turbine is provided. A caulking piece which is made of bi-metal is used...
2016/0194969 Turbine Vane With Platform Rib
A vane for use in a gas turbine engine has an airfoil extending between a leading edge and a trailing edge, a radially outer platform and a radially inner...
2016/0194968 HIGH PERFORMANCE CONVERGENT DIVERGENT NOZZLE
A turbofan engine includes a fan section. A core engine section drives the fan section. An outer nacelle surrounds the fan section and defines a radially outer...
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