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Patent # Description
2017/0234192 EXHAUST SYSTEM AND DEVICE TO INDUCE IMPROVED EXHAUST GAS MIXING PRIOR TO TREATMENT THROUGH A CATALYTIC CONVERTER
An exhaust gas mixer to impart swirl and turbulence in the exhaust stream of an internal combustion engine as well as an exhaust system including such an...
2017/0234191 FLUID LINE
The invention relates to a fluid line (1) having a tube (2) made of a synthetic material. The fluid line (1) should be guided in a flexible manner. To this...
2017/0234190 SCR TANK WITH VENTILATION LINE ATTACHED IN SECTIONS
SCR tank (10) for motor vehicles for storing and dispensing aqueous urea solution, comprising a tank shell (16) enclosing a tank volume (18) having fluid...
2017/0234189 SCR AFTER-TREATMENT OF ENGINE EXHAUST GAS
Reductant is metered into an engine exhaust gas after-treatment system upstream of an SCR catalyst at engine exhaust gas temperatures both less than and...
2017/0234188 SCR AFTER-TREATMENT OF ENGINE EXHAUST GAS
Reductant is metered into an engine exhaust gas after-treatment system upstream of an SCR catalyst at engine exhaust gas temperatures both less than and...
2017/0234187 EXHAUST GAS PURIFICATION APPARATUS FOR INTERNAL COMBUSTION ENGINE
An object is to prevent abrasion inside an addition valve and clogging of the addition valve due to an increase in the particle diameter of precipitates. A...
2017/0234186 EXHAUST GAS CONTROL APPARATUS FOR INTERNAL COMBUSTION ENGINE
An exhaust gas control apparatus for an internal combustion engine includes an addition valve, a tank, a urea water passage, a pump, a nitrogen oxides...
2017/0234185 EXHAUST GAS PURIFICATION CATALYST DEVICE, EXHAUST GAS PURIFICATION SYSTEM, AND METHOD FOR DETECTING...
An object of the present disclosure is to provide an exhaust gas purification catalyst device; an exhaust gas purification system; and a method for detecting...
2017/0234184 SYSTEM AND METHOD FOR EXHAUST TREATMENT
According to various embodiments, an exhaust treatment system includes a catalyst that is in direct contact with an exhaust stream, at least one sensor that...
2017/0234183 SYSTEM AND METHODS FOR REDUCING SOx GASES IN AFTERTREATMENT SYSTEMS
An aftertreatment system comprises a SCR system including a catalyst formulated to decompose constituents of an exhaust gas passing therethrough. A filter is...
2017/0234182 HIGH-END PROCESSING DEVICE FOR PURIFICATION OF EXHAUST OF DIESEL ENGINE
A high-end processing device for purification of exhaust of a diesel engine includes a connection channel, a plurality of catalytic converters, a plurality of...
2017/0234181 PLUGGED HONEYCOMB STRUCTURE, AND MANUFACTURING METHOD OF PLUGGED HONEYCOMB STRUCTURE
A plugged honeycomb structure has a plurality of cells defined by partition walls to become through channels for fluid, one end of each of the predetermined...
2017/0234180 VEHICLE NOISE SUPPRESSION METHOD
Aspects of the present invention relate to noise modification systems of motor vehicles, and controllers and methods of use thereof.
2017/0234179 USE OF ACTIVE NOISE SYSTEM
Aspects of the present invention relate to an active noise system, a controller for an active noise system, a method and a hybrid electric vehicle. The...
2017/0234178 TURBO PCV VALVE
A PCV valve that regulates the flow of gases to a turbocharger. A spring biased plunger member is used to restrict and meter the flow of gases through the PCV...
2017/0234177 TWO-PART STRUCTURAL OIL PAN
An oil pan assembly including a first portion having an inner set of openings configured to receive a first set of fasteners to couple the first portion to an...
2017/0234176 AUTOMOTIVE LUBRICANT PUMPING SYSTEM WITH TWO PIECE RELIEF VALVE
A lubrication pumping system for an oil lubricated engine is provided that includes a pump with an outlet and inlet. A relief valve is included having a...
2017/0234175 HOLLOW ENGINE VALVE AND MANUFACTURING METHOD THEREFOR
The present invention provides a hollow engine valve achieving high durability while suppressing an increase in manufacturing cost, and a manufacturing method...
2017/0234174 VALVE OPENING AND CLOSING TIMING CONTROL APPARATUS
A valve opening and closing timing control apparatus includes a driving-side rotating body, a driven-side rotating body fixed to a camshaft by a bolt, a fluid...
2017/0234173 HYDRAULIC LASH ADJUSTER
A hydraulic lash adjuster assembly constructed in accordance to one example of the present disclosure includes a bucket and a hydraulic lash adjuster. The...
2017/0234172 LOCKING DEVICE FOR A SWITCHABLE VALVE DRIVE COMPONENT
The invention relates to a locking device for a switchable valve drive component, including a first locking body and a second locking body which can be brought...
2017/0234171 COMPRESSED FLUID STORAGE POWER GENERATION DEVICE
A compressed fluid storage power generation device including a compressor and compressor bodies for compressing a working fluid; a pressure accumulation tank...
2017/0234169 Supercritical CO2 Generation System Applying Plural Heat Sources
The present invention relates to a supercritical CO.sub.2 generation system applying plural heat sources. According to the present invention, each heat...
2017/0234168 INSTALLATION SUPPORT STRUCTURE FOR A STEAM CONDENSATION SYSTEM
A support structure for a condensation system is disclosed having a pair of tube bundles connected at its respective upper ends to steam distribution lines for...
2017/0234167 AUXILIARY DRIVE BOWED ROTOR PREVENTION SYSTEM FOR A GAS TURBINE ENGINE THROUGH AN ENGINE ACCESSORY
A bowed rotor prevention system for a gas turbine engine of an aircraft is provided. The bowed rotor prevention system includes a gear train and a bowed rotor...
2017/0234166 BOWED ROTOR PREVENTION SYSTEM USING WASTE HEAT
A bowed rotor prevention system for a gas turbine engine is provided. The bowed rotor prevention system includes a thermoelectric generator system operable to...
2017/0234165 GAS TURBINE ENGINE PACKAGE AND CORRESPONDING METHOD
A gas turbine engine unit (110) for use in a modular power generation system includes an engine package (112) and a mechanical handling system adapted to...
2017/0234164 ROTARY MACHINE UNIT
A rotary machine unit equipped with rotary shaft provided so as to penetrate the respective opposing surfaces of a first casing and a second casing arranged...
2017/0234163 CONNECTION SYSTEM FOR HOUSING ELEMENTS OF A TURBINE INTERMEDIATE CASING
A connection system for a hot gas-conducting annular duct of a turbine intermediate casing of a gas turbine includes a first housing element, a second housing...
2017/0234162 STEAM TURBINE INNER CASING COMPONENT AND REPAIR METHOD THEREFOR
Embodiments of the present invention relate to an inner casing component configured to form part of a steam flow path of a last stage of an axial flow steam...
2017/0234161 Flowpath Contouring
A gas turbine engine includes a compressor section, combustion section, and turbine section. The turbine section includes a turbine component stage, the...
2017/0234160 AIRCRAFT ENGINE WITH AN IMPACT PANEL
A facing sheet for a fan casing comprising a support layer that includes a set of partitioned cavities with open faces and a facing sheet comprising a polymer...
2017/0234159 GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan, a compressor section, and a turbine section...
2017/0234158 BOWED ROTOR START RESPONSE DAMPING SYSTEM
A method of bowed rotor start response damping for a gas turbine engine is provided. A spring rate and a damping characteristic of one or more bearing supports...
2017/0234157 Rotor Support System With Shape Memory Alloy Components For A Gas Turbine Engine
A rotor support system for a gas turbine engine may generally include a bearing assembly and a load reduction member configured to be coupled between the...
2017/0234156 GAS TURBINE HAVING AN ANNULAR PASSAGE SUBDIVIDED INTO ANNULUS SECTORS
A gas turbine having at least one inner and outer housing part, between which two housing parts a ring channel is at least partially arranged, which ring...
2017/0234155 TURBINE FRAME COOLING SYSTEMS AND METHODS OF ASSEMBLY FOR USE IN A GAS TURBINE ENGINE
A turbine frame cooling system for use with a gas turbine engine includes an outer ring defining a cavity and a hub positioned radially inward of the outer...
2017/0234154 Turbine stator vane with closed-loop sequential impingement cooling insert
A turbine stator vane with a closed loop sequential impingement cooling circuit with an impingement cooling insert that includes a three-pass serpentine flow...
2017/0234153 Guide Apparatus for a Turbocharger Including a Vane Lever Integrated Adjustment Ring Axial Travel Stop
A vane lever (46) for a guide apparatus (28) of a turbocharger (10) may include a base (49). The base (49) may include a bore (48) disposed therethrough. An...
2017/0234152 Variable low turbine vane with aft rotation axis
A turbine with a variable inlet guide vane assembly in which the vane airfoils extend between inner and outer buttons, and in which a center of rotation of the...
2017/0234151 AIR SHREDDER INSERT
An engine component assembly includes at least one cavity that is in communication with a source of cooling air. An insert disposed within the cavity includes...
2017/0234150 Thermal Stress Relief Of A Component
A component for a gas turbine engine includes a hot side wall, a plurality of connection walls, and a cold side wall. The hot side wall is exposed to a core...
2017/0234149 NOZZLE BOX ASSEMBLY
A nozzle box assembly includes steam inlets, through which working steam is supplied, a torus part connected to the steam inlets so as to form an annular steam...
2017/0234148 METHOD FOR CARRYING OUT WORK ON A ROTOR AND ASSOCIATED FOIL
In the method for carrying out work, according to the invention, in order to maintain a metal turbine engine motor, such as a drum, in an operational state: ...
2017/0234147 CENTRIFUGAL COMPRESSOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY
A fluid transfer assembly for use in a gas turbine engine includes a rotor shaft, a stationary assembly circumscribing the rotor shaft, and a rotating...
2017/0234146 AIRFOIL HAVING IMPINGEMENT OPENINGS
An airfoil for a turbine engine having a perimeter wall bounding an interior and defining a pressure side and a suction side, a radially extending rib located...
2017/0234145 ACCELERATOR INSERT FOR A GAS TURBINE ENGINE AIRFOIL
An apparatus for a gas turbine engine can include an airfoil having an interior. The interior can be separated into one or more cooling air channels extending...
2017/0234144 COOLING CONCEPT FOR TURBINE BLADES OR VANES
A turbine assembly with a hollow aerofoil having a main cavity with an impingement tube, insertable inside the main cavity for impingement cooling of an inner...
2017/0234143 GAS TURBINE ENGINE COMPONENT HAVING VASCULAR ENGINEERED LATTICE STRUCTURE
A flowpath component for a gas turbine engine includes a first platform including a vascular engineered lattice structure, a body extending from, and supported...
2017/0234142 Rotor Blade Trailing Edge Cooling
The present disclosure is directed to a rotor blade for a gas turbine engine. The rotor blade includes a platform having a radially inner surface and a...
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