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Patent # Description
2017/0044961 METHOD OF CONTROLLING A PARTICULATE FILTER
A method of controlling a particulate filter of an internal combustion engine is disclosed. A regeneration cycle of the particulate filter is initiated. During...
2017/0044960 METHOD OF PROTECTING A DIESEL PARTICULATE FILTER FROM OVERHEATING
A method for preventing overheating of a diesel particulate filter during regeneration when an engine is idling may include using an electric machine to apply...
2017/0044959 SECONDARY AIR PUMP ASSEMBLY
A secondary air pump assembly for a vehicle includes a housing having an air inlet and an air outlet, a pump disposed within the housing, a position assembly...
2017/0044958 EXHAUST AFTERTREATMENT DEVICE
An exhaust treatment device for treating exhaust includes a main body defining an interior, an inlet, and an outlet; an inlet arrangement disposed at the...
2017/0044957 MIXING STRUCTURE
A lattice board 7 is obliquely arranged in a bent portion 1A (a flow changing portion) halfway in an exhaust pipe 1 where exhaust gas 4 flows curvedly so as to...
2017/0044956 EXHAUST GAS MIXER
Systems are provided for a mixer. In one example, the mixer may include intersecting tubes with a plurality of inlets and/or outlets located along an exhaust...
2017/0044955 EXHAUST GAS HOUSING FOR AN EXHAUST GAS SYSTEM OF AN INTERNAL COMBUSTION ENGINE
An exhaust gas housing for an exhaust gas system of an internal combustion engine, including a rail system which is provided for receiving at least one...
2017/0044954 METHOD FOR INFLUENCING A FLUID FLOW
A method for influencing a fluid flow in a fluid line is provided. The fluid line has a wall and a honeycomb body arranged in the fluid line with a fluid inlet...
2017/0044953 EXHAUST GAS PURIFICATION APPARATUS FOR AN INTERNAL COMBUSTION ENGINE
An amount of ammonia flowing out from an SCR catalyst is reduced at the time of carrying out rich spike control to reduce an amount of NOx stored in an NSR...
2017/0044952 METHOD FOR EXHAUST GAS AFTERTREATMENT AND COMBUSTION SYSTEM
In a method for exhaust gas aftertreatment, in which an exhaust gas to be aftertreated, which is produced during combustion of a fuel, is treated with a...
2017/0044951 METHOD FOR THERMALLY REGULATING AN INJECTOR FOR INJECTING A REDUCING AGENT INTO AN EXHAUST PIPE OF AN INTERNAL...
A computer program, system and method are provided for thermally regulating an injector injecting a reducing agent into an exhaust pipe of an internal...
2017/0044950 EXHAUST PURIFYING SYSTEM
An exhaust purification system can prevent a NH.sub.3 slip caused by an excessive injection of urea water, and includes: an SCR that purifies NOx contained in...
2017/0044949 VIRTUAL REDUCTANT LEVEL SENSOR
An aftertreatment system comprises a reductant storage tank and a SCR system fluidly coupled thereto. A reductant physical level sensor and a tank temperature...
2017/0044948 METHOD AND SYSTEM FOR EXHAUST EMISSIONS CONTROL
A twin charged engine is provided comprising a catalytic converter; a first compressor which, when operated, increases engine load; a second compressor which...
2017/0044947 INTERNAL COMBUSTION ENGINE
An internal combustion engine, wherein a chemical thermal storage device is provided with a first heater including a first element generating heat when...
2017/0044946 METHOD OF OPERATING AN AUTOMOTIVE SYSTEM
A method is disclosed for operating an automotive system having an internal combustion engine equipped with an exhaust gas aftertreatment system including a...
2017/0044945 Low Temperature Method and System for Fuel Gas Purification and Utilization Thereof
A low temperature purification system includes a reactor; a lye tank to store oxygen-rich alkaline absorbent; an exhausted gas supplier to provide vehicle...
2017/0044944 METHOD AND SYSTEM FOR PROCESSING EXHAUST GAS
A method of processing exhaust gas includes receiving incoming exhaust gas and cooling it in at least one heat exchanger to create cooled exhaust gas. The...
2017/0044943 MUFFLER FOR AUTOMOBILE
A muffler for an exhaust system of a gas combustion engine, which comprises a muffler body (14) connected to an exhaust pipe inlet (10a), an exhaust pipe...
2017/0044942 Systems and Methods for Determining a Remaining Life of Fluid Onboard a Machine
Systems and methods for determining the remaining life of a fluid onboard a machine are disclosed. One method includes determining a dielectric constant of a...
2017/0044941 ENGINE
An engine includes a crank shaft inside a crankcase and an oil pan and penetrates the crankcase and the oil pan in an up-down direction. An oil pump and an oil...
2017/0044940 OIL FEED MEMBER AND LUBRICANT FEED MECHANISM FOR ENGINE PROVIDED WITH SAME
There is provided an oil feed member capable of preventing lubricant from being excessively fed from an oil feed member to lubrication portions of valve gears,...
2017/0044939 RELIEF VALVE DEVICE
Provided is a relief valve device including: a housing (1) including a valve chamber (2), an orifice (25), and a relief discharge port (26); a valve body (4)...
2017/0044938 INTERNAL COMBUSTION ENGINE AND OIL TREATMENT APPARATUS FOR USE WITH THE SAME
An internal combustion engine having an improved oil treatment system. The internal combustion engine may be a splash lubrication engine in which oil is flowed...
2017/0044937 HYDRAULIC LASH ADJUSTER
A hydraulic lash adjuster having a reduced number of elements, yet capable of suppressing air from infusing into a high-pressure chamber. A plunger is fitted...
2017/0044936 Roller Type Rocker Arm
A roller-type rocker arm includes a roller shaft. A sliding surface of an outer circumference surface of the roller shaft includes a number of dimples. An...
2017/0044935 STEAM CYCLE, AND METHOD FOR OPERATING A STEAM CYCLE
A steam cycle for a power station, and to a method for operating, in particular for starting, a steam cycle. The steam cycle has a high-pressure turbine, a...
2017/0044933 BEARING STRUCTURE AND TURBOCHARGER
A bearing structure includes a through-hole penetrating through in the axial direction of shaft, a bearing holder accommodated in the through-hole, a...
2017/0044932 IMPINGEMENT STRUCTURE FOR JET ENGINE MID-RUTBINE 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...
2017/0044931 BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE
A gas turbine engine includes a turbine section including a plurality of blade outer air seals (BOAS) disposed therein, the BOAS including a BOAS body...
2017/0044930 HOT DUST RESISTANT ENVIRONMENTAL BARRIER COATINGS
An environmental barrier coating system for a component of a gas turbine includes at least one rare earth disilicate layer and at least one rare earth...
2017/0044929 METHOD OF MONITORING RUBBING BETWEEN A ROTARY PARTY AND A STATIONARY PART IN A ROTATING TURBOMACHINE,...
The arrangement for monitoring rubbing between a rotary part and a stationary part in a rotating turbomachine comprises at least one mechanical oscillations...
2017/0044928 FIVE-DEGREE-OF-FREEDOM ADJUSTMENT AND POSITIONING METHOD AND APPARATUS FOR ASSEMBLY/MEASUREMENT OF ROTOR AND...
A five-degree-of-freedom adjustment and positioning method and apparatus for assembly/measurement of rotor and stator of an aircraft engine; said method...
2017/0044927 LOCK-UP PREVENTION VANE FOR VARIABLE GEOMETRY TURBOCHARGER
A turbocharger includes a variable geometry turbine (1). The turbine includes a turbine wheel (12) disposed in the turbine housing (4) between the volute (10)...
2017/0044926 METHOD FOR PRODUCING A VARIABLE TURBINE GEOMETRY OF AN EXHAUST GAS TURBOCHARGER
A method for producing a variable turbine geometry for an exhaust gas turbocharger may include arranging a first and a second guide vane support ring coaxially...
2017/0044925 TURBOCHARGER TURBINE WITH VARIABLE NOZZLE
An exhaust gas turbocharger (1) includes a turbine section (2) having a turbine housing (11) and a turbine wheel (4) disposed in the turbine housing (11). The...
2017/0044924 SYSTEM FOR THE ACTIVE SETTING OF A RADIAL CLEARANCE SIZE AND AIRCRAFT ENGINE WITH A SYSTEM FOR THE ACTIVE...
A system for the active setting of a radial clearance size between a blade tip of at least one compressor stage and/or at least one turbine stage of an...
2017/0044923 TURBINE SHROUD ASSEMBLY AND METHOD FOR LOADING
A turbine shroud assembly is disclosed including an inner shroud having a surface adjacent to a hot gas path, an outer shroud, and a biasing apparatus. The...
2017/0044922 SYSTEM AND METHOD FOR SUPPORTING A TURBINE SHROUD
In one aspect the present subject matter is directed to a system for supporting a turbine shroud. The system includes a shroud support at least partially...
2017/0044921 FLEXIBLY MOUNTED CERAMIC MATRIX COMPOSITE SEAL SEGMENTS
A segmented turbine shroud for radially encasing a turbine in a gas turbine engine comprises a carrier comprising a flange; a ceramic matrix composite (CMC)...
2017/0044920 TURBINE SHROUD HAVING CERAMIC MATRIX COMPOSITE SEAL SEGMENT
A segmented turbine shroud for radially encasing a rotatable turbine in a gas turbine engine comprising a carrier, a ceramic matrix composite (CMC) seal...
2017/0044919 TURBINE SHROUD SEGMENT SEALING
An integrated shroud structure surrounds a circumferential array of stator vanes and a circumferential array of rotor blades of a gas turbine engine. The...
2017/0044918 SELF CRYSTALLINE ORIENTATION FOR INCREASED COMPLIANCE
Aspects of the disclosure are directed to a seal comprising: a shoe, and at least one beam coupled to the shoe, wherein the seal includes a single crystal...
2017/0044917 SEALING ATTACHMENT FOR A GAS TURBINE ENGINE
A gas turbine including: a wall component having a gas-facing surface bounding the main gas path; a male-female sealing attachment having a male or female part...
2017/0044916 GAS TURBINE MEMBRANE SEAL
A gas turbine membrane seal is disclosed. The gas turbine membrane seal includes a membrane, the membrane configured and arranged to extend from a first gas...
2017/0044915 TURBINE ASSEMBLY AND CORRESPONDING METHOD OF OPERATION
A turbine assembly having a basically hollow aerofoil with at least one cavity spanning the aerofoil in span wise direction of the aerofoil, an outer platform...
2017/0044914 TURBINE COMPONENT SURFACE COOLING SYSTEM WITH PASSIVE FLOW MODULATION
A system according to various embodiments includes: a cooling network within a turbine component, the cooling network including at least one passageway fluidly...
2017/0044913 OVERLAPPING HERRINGBONE FILMHOLE PATTERNED SURFACES
A surface structure having an overlapping herringbone filmhole pattern is disclosed. For instance, the surface structure may have filmholes arranged in...
2017/0044912 DUAL ALLOY GAS TURBINE ENGINE ROTORS AND METHODS FOR THE MANUFACTURE THEREOF
Dual alloy Gas Turbine Engine (GTE) rotors and method for producing GTE rotors are provided. In one embodiment, the method include includes arranging bladed...
2017/0044911 ABRASIVE SHEATHING
An abrasive sheath for application to a component surface is disclosed. The abrasive sheath may comprise a metallic layer and an abrasive layer plated on a...
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