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Patent # Description
2018/0328250 REAGENT INJECTOR FREEZE PROTECTION
An injector for injecting a reagent includes a first injector body and a second injector body. The first injector body includes an outlet opening. The second...
2018/0328249 REAGENT INJECTOR
An injector for injecting a reagent includes a first injector body defining a first end and a second end. The first injector body further includes an outlet...
2018/0328248 DOSING AND MIXING ARRANGEMENT FOR USE IN EXHAUST AFTERTREATMENT
A dosing and mixing arrangement including an exhaust conduit defining a central axis; a mixing conduit positioned within the exhaust conduit; a dispersing...
2018/0328247 COOLING DEVICE FOR REDUCTANT SPRAY MODULE, AND SELECTIVE ENGINE COOLING SYTEM HAVING SAME
A cooling device for a reducing agent injection module, includes a reducing agent injection module installed in an exhaust pipe to inject a reducing agent into...
2018/0328246 EXHAUST GAS PURIFICATION SYSTEM FOR AN INTERNAL COMBUSTION ENGINE
An exhaust gas purification system comprise a first fuel supply unit to supply fuel to exhaust gas flowing in an exhaust passage by a supply valve arranged in...
2018/0328245 MULTIPURPOSE AIR POLLUTION & HEAT REDUCING DEVICE
A multipurpose pollution reducing-device is shown. The device comprises a tank 1 adapted to be secured with a stand 2 and to store pollution reducing liquid 3...
2018/0328244 OIL FILTER CARTRIDGE AND HOUSING FOR AN OIL FILTER CARTRIDGE
A filter cartridge includes a filter element (forming a fluid channel with a first longitudinal axis) with a front side to which a front end cap is sealingly...
2018/0328243 INTERNAL COMBUSTION ENGINE
An internal combustion engine includes: a case; an oil pan disposed below the case; an oil filter into which oil inside the oil pan flows; and a guide that...
2018/0328242 INTERNAL COMBUSTION ENGINE
An internal combustion engine includes: a case; an oil pan disposed below the case; an oil filter into which oil inside the oil pan flows; and a guide that...
2018/0328241 DRIVE SYSTEM AND ASSOCIATED MOTOR VEHICLE
This drive system for a motor vehicle includes a top end and a bottom end that are coupled together, a kinematic drive chain, a compressor, a main lubrication...
2018/0328240 Hydraulic Early Engine Exhaust Valve Opening System
An early exhaust valve opening (EEVO) module increases a no-load engine speed so an engine can smoothly transition to driving a load when necessary. The EEVO...
2018/0328239 INTERNAL-COMBUSTION ENGINE VALVE TIMING CONTROL DEVICE
A communicating hole, which communicates between a clearance space and the outside of a cover member, is formed in the cover member, and a seal cap is fitted...
2018/0328238 Pushrod for a Valve Gear of an Internal Combustion Engine
The invention concerns a pushrod for a valve gear of an internal combustion engine. The invention furthermore concerns a valve gear and a motor vehicle, in...
2018/0328237 COOLING MODULE, SUPERCRITICAL FLUID POWER GENERATION SYSTEM INCLUDING THE SAME, AND SUPERCRITICAL FLUID SUPPLY...
A cooling module is included in a supercritical fluid power generation system and is used in supercritical fluid supply method. The cooling module includes a...
2018/0328236 FUEL VAPORIZATION USING DATA CENTER WASTE HEAT
Systems and methods are provided for data center cooling by vaporizing fuel using data center waste heat. The systems include, for instance, an ...
2018/0328235 EXPLOITING COMPRESSION HEAT IN HEAT ENGINES
A dual-cycle heat engine employing a first cycling working fluid and a second cycling working fluid whose cycles overlap when fused into a combined working...
2018/0328234 POWER COGENERATION SYSTEM
A power cogeneration system employing a steam turbine in association with conventional engines.
2018/0328233 EXPANSION APPARATUS FOR RECOVERING WASTE HEAT AND WASTE HEAT RECOVERY SYSTEM INCLUDING THE SAME
An expansion apparatus for recovering waste heat may include two or more turbines and a distribution valve distributing working fluid supplied from the boiler...
2018/0328232 Control Of A Thermal Cyclic Process
The invention relates to a method for controlling a thermal cyclic process, in particular an Organic Rankine Cycle (ORC), which is operated with a working...
2018/0328231 THERMAL POWER GENERATION SYSTEM AND CONTROL METHOD FOR SAME
A thermal power generation system includes: a boiler; at least one steam turbine; a generator; a condenser; at least one low-pressure feed water; a...
2018/0328230 EXHAUST DIFFUSER
An exhaust diffuser includes: an internal cylinder; an external cylinder that forms an exhaust passage between the internal cylinder and the external cylinder,...
2018/0328229 EXHAUST DIFFUSER
An exhaust diffuser includes: a plurality of struts, each of which penetrates an internal cylinder and an external cylinder and couples a bearing support and a...
2018/0328228 TURBINE VANE WITH INNER CIRCUMFERENTIAL ANTI-ROTATION FEATURES
A vane assembly includes an outer platform, an inner platform, and a vane. The inner platform has an inner flange that includes a first face, a second face...
2018/0328227 EXHAUST LINER CABLE FASTENER
A hanger for mounting an exhaust liner to an exhaust duct is provided. The hanger includes at least one cable, a cable flange, and a J-shaped flange. The at...
2018/0328226 TURBINE HOUSING
In a turbine housing that includes a scroll portion constituting a spiral exhaust gas passage between an exhaust inlet side flange constituting an inlet for...
2018/0328225 FLUID DAMPING STRUCTURE RING AND METHOD OF FLUID DAMPING
A fluid damping structure is provided that includes a damper ring. The damper ring includes an annular body a plurality of fluid check valves, and at least one...
2018/0328224 IMPINGEMENT INSERT
An airfoil including a leading edge, a trailing edge, a pressure side, a suction side, and an internal impingement cavity. An impingement insert is located...
2018/0328223 Turbine Overspeed Trip Test System
A turbine overspeed trip test data system is a portable system by which an operator can electronically gather and log data during a turbine overspeed test. A...
2018/0328222 Turbine Overspeed Trip Test System
A turbine overspeed trip test data system is a portable system by which an operator can electronically gather and log data during a turbine overspeed test. A...
2018/0328221 SYSTEM AND METHOD FOR PLANNING ENGINE BORESCOPE INSPECTIONS BASED ON FOD PROBABILITY ESTIMATION
A system for identifying timeframes for borescope inspections for a gas turbine engine, having: monitoring systems monitor engine conditions, derive engine...
2018/0328220 METHOD AND SYSTEM FOR SETTING AN ACCELERATION SCHEDULE FOR ENGINE START
Herein provided are methods and systems for setting an acceleration schedule for engine start of a gas turbine engine. A rotational acceleration measurement of...
2018/0328219 VARIABLE STATOR BLADE OPERATING DEVICE
A variable stator blade operating device is a variable stator blade operating device that manipulates the mounting angle of a stator blade of an axial...
2018/0328218 Turbocharger Comprising a Slider for Fluid Connection
A turbocharger, in particular a turbocharger for a motor vehicle, is provided. The turbocharger includes a turbine to which exhaust gases can be supplied by...
2018/0328217 EXHAUST GAS GUIDE SECTION FOR AN EXHAUST GAS TURBOCHARGER AND METHOD FOR OPERATING AN EXHAUST GAS TURBOCHARGER
The invention relates to an exhaust gas guide section for an exhaust gas turbocharger, with a first spiral channel (4) and a second spiral channel (5) for the...
2018/0328215 METHOD AND DEVICE FOR CONTROLLING BLADE OUTER AIR SEALS
A device and methods are provided for controlling blade outer air seal of a gas turbine engine. In one embodiment, a method includes receivg blade outer air...
2018/0328214 ALTERNATIVE W-SEAL GROOVE ARRANGEMENT
A blade outer air seal (BOAS) assembly includes a rotor blade configured to rotate about an axis. The BOAS assembly also includes a BOAS positioned radially...
2018/0328213 SHROUD CARTRIDGE HAVING A CERAMIC MATRIX COMPOSITE SEAL SEGMENT
A shroud for radially encasing a turbine in a gas turbine engine is provided. The shroud comprises a carrier which defines a pin-receiving carrier bore, and a...
2018/0328212 Systems Including Rotor Blade Tips and Circumferentially Grooved Shrouds
A system for a turbomachine includes a rotor blade configured to rotate along a circumferential direction within a casing of the turbomachine and a shroud...
2018/0328211 Dry Gas Seal And Turbomachine Having A Dry Gas Seal
A dry gas seal of a turbomachine, more particularly of a turbocompressor, for sealing a rotor-side component of the turbomachine with respect to a stator-side...
2018/0328210 Super-Critical C02 Expander
An expander may include a longitudinal axis, an inner casing split horizontally along the longitudinal axis, an outer casing split horizontally along the...
2018/0328209 COMPLIANT SEAL ASSEMBLY AND METHOD OF OPERATING
A compliant seal assembly that may be for an MTF of a gas turbine engine includes a housing orientated about an axis with a circumferentially extending groove...
2018/0328208 TURBINE SHROUD SEGMENT WITH FLANGE-FACING PERIMETER SEAL
A turbine shroud adapted for use in a gas turbine engine includes a plurality of metallic carrier segments and a plurality of blade track segments mounted to...
2018/0328207 GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a static structure that extends...
2018/0328206 OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328205 OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328204 OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328203 OPTIMIZED AERODYNAMIC PROFILE FOR AN ARM OF A STRUCTURAL CASING OF A TURBINE, AND STRUCTURAL CASING HAVING SUCH...
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328202 OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328201 OPTIMIZED AERODYNAMIC PROFILE FOR AN ARM OF A STRUCTURAL CASING OF A TURBINE, AND STRUCTURAL CASING HAVING SUCH...
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
2018/0328200 OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF A TURBINE
When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,...
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