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Patent # Description
2016/0115840 Construction Machine
An inlet port (17A) of a first exhaust gas purifying device (16) is provided on a side opposite to an engine (8) by sandwiching an axis (O1-O1) of a...
2016/0115839 SYSTEM AND METHOD FOR EMISSIONS CONTROL IN GAS TURBINE SYSTEMS
A system includes an emissions control system. The emissions control system includes a processor programmed to receive one or more selective catalytic...
2016/0115838 SYSTEMS AND METHODS FOR MANAGING DIESEL EXHAUST FLUID STRATIFICATION
A method for an exhaust system is provided, comprising adjusting reductant injection responsive to a reductant concentration, the reductant concentration based...
2016/0115837 Method for operating a device for providing a liquid additive
A method for operating a device for providing a liquid additive, the device having a delivery path running from a tank to an additive dispensing device, at...
2016/0115836 EXHAUST GAS TREATMENT SYSTEM
A method and system for treating exhaust gas from stationary engines used to generate electricity is provided. Substantially all of the exhaust gases from at...
2016/0115835 DIESEL PARTICULATE FILTER AND EXHAUST GAS PURIFICATION DEVICE
Provided is a novel DPF which can prevent PM from accumulating on the surface and interior of a filter substrate, and can suppress an increase in back pressure...
2016/0115834 EXHAUST GAS TREATMENT DEVICE, ESPECIALLY FOR AN EXHAUST GAS FLOW PATH OF AN INTERNAL COMBUSTION ENGINE, AND...
An exhaust gas treatment device for an exhaust gas flow path of an internal combustion engine, includes a tubular carrier body (12) extending along a...
2016/0115833 POLLUTION CONTROL DEVICE STRUCTURE WITH LOWER FRICTION SURFACE AND UNDERLYING HIGHER FRICTION SURFACE
A structure comprising at least one inorganic layer comprising inorganic materials suitable for use in a pollution control device. A friction-inducing material...
2016/0115832 VARIABLE DISPLACEMENT LUBRICANT PUMP
A lubricant pump comprises a shiftable control ring, a pump rotor rotating in the control ring, a pump outlet, and a pressure control system. The pressure...
2016/0115831 LATCH INTERFACE FOR A VALVE ACTUATING DEVICE
A novel latch seat for a switching rocker arm assembly used in variable valve actuation (VVA) systems for internal combustion engines. The seat is formed...
2016/0115830 DETECTION APPARATUS FOR AT LEAST ONE OF TEMPERATURE AND PRESSURE IN A CYLINDER OF AN INTERNAL COMBUSTION ENGINE
An apparatus for measuring at least one of temperature and pressure within a cylinder of an internal combustion engine can include an engine valve and a...
2016/0115829 ELECTRONIC ACTIVE LOCK PIN CONTROL METHOD FOR MIDDLE PHASE TYPE CONTINUOUSLY VARIABLE VALVE TIMING SYSTEM
An electronic active lock pin control method may include checking whether a default position of a lock pin is present, determining whether the checked default...
2016/0115828 CAMSHAFT ADJUSTER
A camshaft adjuster having a drive element, an output element and a spring, wherein the drive element and the output element can rotate relative to each other,...
2016/0115827 HEAT TRANSFER PROCESS
The use of a refrigerant in organic Rankine cycle systems including at least one hydrofluoroolefin, having at least four carbon atoms represented by the...
2016/0115826 COMBINED CYCLE POWER PLANT
The present invention generally relates to a combined cycle power plant. More in particular, the present invention relates to a plant where the temperature of...
2016/0115825 SEAL SUPPORT STRUCTURE FOR A CIRCUMFERENTIAL SEAL OF A GAS TURBINE ENGINE
A seal support structure is provided for a circumferential seal. In one embodiment, the seal support structure includes an engine support structure, a seal...
2016/0115824 ROTARY SYSTEM
An object of the present invention is to provide a rotary system capable of maintaining a distance of separation between two rotary machines and inhibiting...
2016/0115823 TURBINE HOUSING OF AN EXHAUST-GAS TURBOCHARGER
A turbine housing (1) of an exhaust-gas turbocharger (15) having a turbine volute (7) which is delimited by a metallic outer shell (8) and which has an inner...
2016/0115822 Lattice Type Blade Of An Axial Turbine Engine Compressor
The invention relates to a blade of a low-pressure compressor of an axial turbine engine. The blade comprises a vane in which a cavity is formed. The vane has...
2016/0115821 BLADED ROTOR DISK INCLUDING ANTI-VIBRATORY FEATURE
A rotor disk includes a ring shaped rotor body defining a radially inward opening, rims protrude radially outward from the rotor body, and outwardly facing...
2016/0115820 HOLLOW METAL OBJECTS AND METHODS FOR MAKING SAME
A method of making a hollow metal component comprising the steps of providing at least one core comprising a first side and a reverse side; utilizing a first...
2016/0115819 ARTICLE AND METHOD OF MAKING THEREOF
An article including a substrate and a plurality of coatings disposed on the substrate is presented. The plurality of coatings includes a thermal barrier...
2016/0115818 ARTICLE AND METHOD OF MAKING THEREOF
An article including a substrate and a plurality of coatings disposed on the substrate is presented. The plurality of coatings includes a thermal barrier...
2016/0115817 TURBOMACHINE COMPRISING AN ELECTRIC CURRENT GENERATOR ALLOWING OIL INJECTION FROM THE INSIDE OF A ROTOR SHAFT
A turbomachine for an aircraft, comprising a rotor shaft, a turbomachine case, a lubricated bearing chamber, at least one bearing supporting the rotor shaft...
2016/0115816 GAS TURBINE ENGINE WITH SEAL INSPECTION FEATURES
A turbine shroud of a turbine of a gas turbine engine and methods of making the turbine shroud are disclosed. The turbine shroud is configured to direct...
2016/0115815 TURBINE ASSEMBLY
The invention relates to a turbine in which a bypass-passage extends through a base member of a stationary vane to join seal cavities of adjacent rotating...
2016/0115814 SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal...
2016/0115813 DUAL COMPLIANT SEAL
The present disclosure relates generally to a seal between two circumferential components. The seal comprises a first rope seal partially disposed within a...
2016/0115812 SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. At least one of the two components includes a ramped surface on which the...
2016/0115811 CONFORMAL SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an adjacent second seal...
2016/0115810 BIFURCATED SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal...
2016/0115809 BIFURCATED SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal...
2016/0115808 HINGED SEAL
The present disclosure relates generally to a seal between two components. The seal includes a first substantially frustoconical seal section including a first...
2016/0115807 MULTI-PIECE SEAL
The present disclosure relates generally to a seal between two components. The seal includes a plurality of seal sections including convolutions therein that...
2016/0115806 SEGMENTED SEAL
The present disclosure relates generally to a seal between two circumferential components. The seal comprises a plurality of seal segments disposed adjacent...
2016/0115805 FLEXIBLE FILM-RIDING SEAL
A seal apparatus for a rotary machine, including a plurality of sealing assembly segments surrounding a rotor element which is mounted for rotation about a...
2016/0115804 SEAL SUPPORT STRUCTURE
The present disclosure relates to sealing systems for gas turbine engines. In one embodiment, a seal support structure for a gas turbine engine includes a seal...
2016/0115803 PLATFORM COOLING CIRCUIT FOR A GAS TURBINE ENGINE COMPONENT
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform having a first path...
2016/0115802 PULSE ENERGY ENHANCED TURBINE FOR AUTOMOTIVE TURBOCHARGERS
A turbocharger with a turbine (10) having a turbine wheel (12) in a turbine housing (14) with an associated manifold (24) having individual ports (22)...
2016/0115801 MULTI-PIECE TURBINE AIRFOIL
A gas turbine engine includes a compressor, a combustor fluidly connected to the compressor via a flow path, and a turbine fluidly connected to the combustor...
2016/0115800 STATOR ASSEMBLY WITH PAD INTERFACE FOR A GAS TURBINE ENGINE
An inner platform structure of a stator vane for a gas turbine engine includes a male circumferential side opposite a female circumferential side, the male...
2016/0115799 METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS
A method of forming a plurality of turbulators on a turbomachine surface includes depositing a portion of material on the turbomachine surface forming a first...
2016/0115798 ROTOR BLADE WITH REDUCED ACOUSTIC RESPONSE
A turbine engine rotor blade having a trailing edge (20A) with a modified surface state (22, 28) enabling the flow speed passing around the blade to be altered...
2016/0115797 COATED ARTICLE AND METHOD FOR PRODUCING COATING
A coated article and a method for producing a coating are disclosed. The method for producing a coating includes providing an iron-based alloy substrate, and...
2016/0115796 TURBINE BLADE COOLING STRUCTURE
In a structure for internally cooling a turbine blade, a cooling medium passage is provided in the turbine blade. The cooling medium passage has a shape in...
2016/0115795 TURBINE BLADE AIRFOIL AND TIP SHROUD
A turbine blade airfoil (25, 31R, 31M, 31T, 72) comprising an outer surface shape defined by Cartesian coordinates of successive transverse profiles at radial...
2016/0115794 COMPOSITE ANNULUS FILLER
A composite annulus filler adapted to bridge the gap between two adjacent rotor blades attached to a rim of a rotor disc of a gas turbine engine. The annulus...
2016/0115793 Compressor For An Axial Turbine Engine With Double Contra-Rotating Rotors
The invention concerns a compressor of an axial turbine engine comprising two rotors or contra-rotating drums, of which an inner rotor and an outer rotor are...
2016/0115792 Hydrostatic Positive Displacement Machine
A hydrostatic positive displacement machine has a cam ring for adjusting the displacement volume thereof. This cam ring is guided in translation by...
2016/0115791 DISCHARGING OF MATERIAL EXCAVATED IN UNDERGROUND WORKINGS
A device for the conveying of material excavated in underground workings in a mine road stretch including a belt conveyor system which has an endless conveyor...
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