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Patent # Description
2016/0258345 INTERNAL COMBUSTION ENGINE
An internal combustion engine where a tumble flow is generated inside a combustion chamber includes: a spark plug; an in-cylinder injection valve that injects...
2016/0258344 BOILING COOLING SYSTEM
Provided is a compact boiling cooling system for an internal combustion engine that can operate in a stable manner. A lower end (4c) of a water jacket (4) of...
2016/0258343 TEMPERATURE CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE
A temperature control device for an internal combustion engine includes a determining drive processor and an abnormality determining processor. The determining...
2016/0258342 THERMAL CONTROL MODULE
An engine assembly includes an engine head defining a block coolant outlet, a head coolant outlet, and a block coolant inlet. The engine assembly further...
2016/0258341 ENGINE COOLING SYSTEM HAVING THERMOSTAT
An engine cooling system having thermostat may include a cylinder head disposed on a cylinder block and forming a combustion chamber with the cylinder block,...
2016/0258340 ELECTROMOTIVE COOLANT PUMP
An electrically motorized coolant pump includes a pump housing, a pump impeller being driven in a pump chamber, two suction-side intake ducts and a...
2016/0258339 Fan Control System and Method
A method for controlling a fan. An ECU estimates the time for an engine to reach a substantially decreased engine load relative to a current engine load. The...
2016/0258338 Fan Control System and Method
A method for controlling a fan. The method includes determining an actual air flow over an engine of a vehicle at a current time, and determining a necessary...
2016/0258337 ENGINE DEVICE FOR WORK VEHICLE
A engine device for a work vehicle, in which an engine, a first case, and a second case can be constituted in the same vibration structure, and exhaust gas...
2016/0258336 HEAT INSULATOR
A heat insulator includes a first covering part and a second covering part. The first covering part is configured to cover a bent part formed in an exhaust...
2016/0258335 Marine Exhaust System With Catalyst
A marine engine exhaust system is provided that utilizes a single catalyst housing through which exhaust gases from multiple heads of an exhaust system flow. A...
2016/0258334 MALFUNCTION DIAGNOSIS DEVICE FOR EXHAUST GAS PURIFICATION DEVICE OF INTERNAL COMBUSTION ENGINE
The invention relates to a malfunction diagnosis device for an exhaust gas purification catalyst of an engine. The device calculates, on the basis of a...
2016/0258333 SYSTEM AND METHOD FOR NITRIDING COMPONENTS OF AFTERTREATMENT SYSTEM
A method for nitriding of at least one component of an aftertreatment system is provided. The method includes passing heated gases through the at least one...
2016/0258332 EXHAUST GAS CONTROL APPARATUS
An exhaust gas control apparatus includes an exhaust passage, a urea water tank, a urea adding valve, a urea pump, a pipe, and an electronic control unit. The...
2016/0258331 METHOD OF EVALUATING A SOOT QUANTITY ACCUMULATED IN A SELECTIVE CATALYTIC REDUCTION WASHCOATED PARTICULATE...
A method is disclosed for evaluating a soot quantity accumulated in a Selective Catalytic Reduction wash-coated particulate filter of an internal combustion...
2016/0258330 CATALYST DEVICE FOR EXHAUST GAS PURIFICATION AND METHOD FOR EXHAUST GAS PURIFICATION
An exhaust gas purification catalytic device 1 contains Pt, Pd, and Rh as catalytic metals. The catalytic metal Pt is loaded on silica-alumina which serves as...
2016/0258329 ACTUATOR FOR VALVES IN INTERNAL COMBUSTION ENGINES
An actuator for a valve in an internal combustion engine includes a housing, an electric drive unit arranged in an interior of the housing, an aeration opening...
2016/0258328 Internal Combustion Engine
An internal combustion engine includes a cylinder head, a crankshaft, intake and exhaust camshafts, first and second chain covers, a chain, and a fastening...
2016/0258327 SYSTEMS AND METHODS FOR TURBINE SYSTEM OPERATION IN LOW AMBIENT TEMPERATURES
A system includes a controller communicatively coupled to a compressor. The controller is configured to sense an exhaust temperature of a gas turbine system...
2016/0258326 Method for Converting Energy with Fuel Regeneration in a Cyclic Process of a Heat Engine
The invention can be used in energy technology. In the method for conversion with recovery of energy carriers in a cyclical process of a thermal engine, a...
2016/0258325 TURBINE HOUSING
Provided is a turbine housing that comprises: a scroll unit; a flat annular cover (6) that is disposed in a state where one end face abuts a flanged portion...
2016/0258324 AUXILIARY OIL PUMP FOR GAS TURBINE ENGINE GEAR REDUCTION
A gas turbine engine has a turbine driving a gear reduction. The gear reduction drives a fan drive shaft assembly to, in turn, drive a fan rotor at a reduced...
2016/0258323 BEARING RACE REMOVAL
A bearing housing may include a main body integrated with a bearing receiving portion. A bearing retention stop may extend from the main body and include a...
2016/0258322 INTEGRATED INNER CASE HEAT SHIELD
A mid-turbine frame for a gas turbine engine according to an example of the present disclosure includes, among other things, a first frame case, a flange...
2016/0258321 GENERATOR TEMPERATURE MANAGEMENT FOR THROTTLE LOSS RECOVERY SYSTEMS
Turbine assemblies, loss recovery systems, and related fabrication methods are provided for managing temperatures associated with an electrical generator. One...
2016/0258320 VANE ASSEMBLY FOR A GAS TURBINE ENGINE
A vane assembly for a gas turbine engine is disclosed herein. The vane assembly includes an inner platform, an outer platform, and a ceramic-containing airfoil...
2016/0258319 COMPRESSED CHOPPED FIBER COMPOSITE INLET GUIDE VANE
The present disclosure relates generally to the field of guide vanes for gas turbine engines. More specifically, the present disclosure relates to a compressed...
2016/0258318 TURBINE ENGINE WASHING SYSTEM
Portable aircraft turbine engine washing systems and methods are provided. One such washing system has a portable base unit, a wash line connectable to the...
2016/0258317 DIAGNOSIS DEVICE AND DIAGNOSIS METHOD FOR TURBOCHARGER
A diagnosis device for a turbocharger, the diagnosis device includes an electronic control unit. The electronic control unit is configured to calculate a...
2016/0258316 VARIABLE GEOMETRY SYSTEM TURBOCHARGER
A variable geometry system turbocharger includes an annular heat shield plate which shields heat from a turbine wheel side. The heat shield plate is integrally...
2016/0258315 HIGH-CYCLE, SHORT RANGE-OF-MOTION LINKAGE APPARATUS FOR GAS TURBINE ENGINE APPLICATIONS
A high-cycle, short range-of-motion linkage apparatus for actuation of a turbofan engine component includes a pivot member having a head portion and a stem,...
2016/0258314 TEMPERATURE MANAGEMENT FOR THROTTLE LOSS RECOVERY SYSTEMS
Systems and methods are provided for managing temperatures associated with a flow control assembly, such as a throttle loss recovery assembly. One exemplary...
2016/0258313 Combined electricity, heat, and chill generation for a Rankine engine
A generator uses a working fluid in a single-cycle Rankine engine for up to three purposes: generation of electricity; generation of hot water from heat...
2016/0258312 TEMPERATURE MANAGEMENT FOR THROTTLE LOSS RECOVERY SYSTEMS
Systems and methods are provided for managing temperatures associated with a throttle loss recovery system. One exemplary system includes a flow control...
2016/0258311 TURBINE SHROUD WITH AXIALLY SEPARATED PRESSURE COMPARTMENTS
A turbine shroud for a gas turbine engine includes an annular metallic carrier and a blade track. One or more cavities are formed between the carrier and blade...
2016/0258310 SEAL ARRANGEMENT
A turbine secondary air system seal arrangement (62). The arrangement comprises a first seal land (70) facing radially inwardly; a second seal land (80) facing...
2016/0258309 SEAL FOR JET ENGINE MID-TURBINE FRAME
A mid-turbine frame (MTF") for a jet engine is disclosed and comprises a duct that extends between a high pressure turbine ("HPT") and a low pressure turbine...
2016/0258308 SLIDING COMPLIANT SEAL
The present disclosure relates generally to a seal between two circumferential components. The seal comprises one or more rope seals retained within the seal...
2016/0258307 FLOATING PANEL FOR A GAS POWERED TURBINE
A foil assembly for a gas powered turbine includes a plurality of floating wall sectors arranged circumferentially about an axis defined by a flowpath. Each of...
2016/0258306 BAFFLE INSERTS
An airfoil includes an airfoil body extending from an inner diameter platform to an opposed outer diameter platform along a longitudinal axis. The airfoil body...
2016/0258305 VANE FOR JET ENGINE MID-TURBINE FRAME
A mid-turbine frame (MTF") for a jet engine is disclosed and comprises a duct that extends between a high pressure turbine ("HPT") and a low pressure turbine...
2016/0258304 TURBINE ASSEMBLY WITH LOAD PADS
A turbine shroud for a gas turbine engine includes a carrier and a blade track segment. The carrier is formed to include an inwardly opening blade track...
2016/0258303 FAN BLADE FOR AN AIRCRAFT ENGINE
A fan blade for an aircraft engine, including a leading edge, a trailing edge, a suction side, a pressure side and a blade tip, is provided. The fan blade has...
2016/0258302 AIRFOIL AND METHOD FOR MANAGING PRESSURE AT TIP OF AIRFOIL
An airfoil includes a squealer tip at an outer radial end of the airfoil. A squealer tip pocket of the squealer tip has a convex side and a concave side, and a...
2016/0258301 TURBINE ROTOR BLADE
A turbine rotor blade includes a tip portion having a pressure tip wall and a suction tip wall, a tip leading edge and a tip trailing edge. Also included is a...
2016/0258300 GAS POWERED TURBINE COMPONENT INCLUDING SERPENTINE COOLING
A flow path component for a gas powered turbine including a flow path component body having cross sectional profile having a leading edge and a trailing edge,...
2016/0258299 FLUIDIC MACHINING METHOD AND SYSTEM
One exemplary embodiment of this disclosure relates to a method of forming an engine component. The method includes forming an engine component having an...
2016/0258298 PROCESS FOR PRODUCING AN ARTICLE
A process of producing an article and an article made are provided. The process includes producing a near-net shape component. The process includes forming a...
2016/0258297 Composite Compressor Blade for an Axial-Flow Turbomachine
The present application relates to a composite airfoil for a low-pressure compressor of an axial-flow turbomachine. The airfoil includes a platform and an...
2016/0258296 AIRFOIL FOR A GAS TURBINE ENGINE
A component for a gas turbine engine includes an airfoil that has a first end. A first platform is located at the first end of the airfoil. A compound fillet...
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