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Patent # Description
2017/0002705 Separation element of liquid separator, separation medium, liquid separator, and method for producing...
Disclosed are: a separation element (20) of a liquid separator (10) for the separation of liquid from an aerosol; a separation medium (38); a liquid separator...
2017/0002704 BREATHER DEVICE FOR INTERNAL COMBUSTION ENGINE
In a breather device for an internal combustion engine for guiding blow-by gas generated in a crank chamber to an intake system, the breather device includes:...
2017/0002703 COMBINED OIL FILTER AND RESTRICTOR ASSEMBLY
A combined oil filter and restrictor assembly is disclosed having an oil flow restrictor interposed between first and second filters so that, irrespective of...
2017/0002702 COMBUSTION ENGINE, VEHICLE COMPRISING THE COMBUSTION ENGINE AND METHOD FOR CONTROLLING THE COMBUSTION ENGINE
A method to control a four-stroke combustion engine, comprising at least one cylinder; a piston arranged in each cylinder; at least one inlet valve arranged in...
2017/0002701 VALVE TIMING CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE
A valve timing control device for an internal combustion engine is provided which is devised to shorten an axial length of a brush retaining portion of a...
2017/0002700 CAMSHAFT ADJUSTING DEVICE, COMBUSTION ENGINE AND ASSEMBLY METHOD
A camshaft adjustment device comprising an electromagnetic actuator (3) having an armature that can be adjusted axially along an adjustment axis (5) for...
2017/0002699 VALVE TIMING CONTROL APPARATUS FOR INTERNAL COMBUSTION ENGINE AND CONTROLLER FOR VALVE TIMING CONTROL APPARATUS
A valve timing control apparatus includes: an urging member to which a set load is provided to act, to the cam shaft, an urging force from one of the most...
2017/0002698 VALVE TRAIN ASSEMBLY
A valve train assembly includes a rocker arm, comprising: a first roller, configured to engage a first rotatable cam surface; and a further roller, configured...
2017/0002697 VALVE OPENING AND CLOSING APPARATUS
A valve opening and closing apparatus is disclosed having one or a plurality of rocker arms in contact with the cam, such that each of the rocker arms causes a...
2017/0002696 ROTOR ASSEMBLY WITH INNER DIAMETER DIVIDER PATTERN
A phaser with a rotor assembly having a pattern on an inner diameter that acts as a sealing land or divider between the advance supply port and the retard...
2017/0002695 ORGANIC RANKINE BINARY CYCLE POWER GENERATION SYSTEM
An organic rankine binary cycle power generation system includes: a superheater heating a working fluid by exchanging heat with discharged heat; a turbine...
2017/0002694 Thermal Power Plant for Recovering Water from Exhaust Gas and a Method for Treating Recovered Water of Thermal...
A thermal power plant for recovering water from exhaust gas comprising: a gas turbine; a heat recovery steam generator for generating steam by supplying...
2017/0002693 SENSORLESS CONDENSER REGULATION FOR POWER OPTIMIZATION FOR ORC SYSTEMS
The invention relates to a method for regulating a condenser in a thermal cycle apparatus, in particular in an ORC apparatus, wherein the thermal cycle...
2017/0002692 METHODS AND APPARATUS TO OPTIMIZE STEAM TURBINE RAMP RATES
Methods and apparatus to optimize turbine ramp rates are disclosed herein. An example method includes predicting a setpoint for a turbine rotor over a...
2017/0002691 THERMAL POWER PLANT WITH HEAT RECOVERY
In an energy conversion method and a thermal power plant for converting heat into mechanical or electric energy using a working medium, a vapor state in the...
2017/0002690 Activation Control Apparatus
An object of the invention is to provide an activation control apparatus by which a steam turbine can be activated safely at a high speed in response to a...
2017/0002689 DEVICE FOR RETAINING DRAINED FLUIDS FOR A PROPULSIVE ASSEMBLY
A device for retaining drained fluids for a propulsive assembly includes a cavity for storing the drained fluids and two walls mounted at the opening of said...
2017/0002688 UNDUCTED PROPELLER TURBOSHAFT ENGINE PROVIDED WITH A REINFORCING SHELL INTEGRATING PIPE SEGMENTS
An airplane unducted propeller turboshaft engine having a gas generator and a receiver including a propulsion assembly carrying least one propeller, the engine...
2017/0002687 FAN-DRIVE GEAR SYSTEM WITH SEPARATE SCAVENGE PUMP
A lubrication circulation system may comprise a first oil pump configured to retrieve oil from a bearing compartment, and a second oil pump located separately...
2017/0002686 SEAL
A hydraulic seal arrangement including first and second rotatable components, the first defining a first annular trough defined by radially inwardly extending...
2017/0002685 GUIDE VANE OF A GAS TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT ENGINE
A guide vane of a gas turbine engine, in particular of an aircraft engine, which has a pressure-side wall, a suction-side wall, a guide vane root, a guide vane...
2017/0002684 NACELLE COMPRESSION RODS
A compression rod may include a plunger and a spring. A proximal end and a distal end of the compression rod may contact engagement features in a core cowl of...
2017/0002683 STEAM TURBINE SHELL DEFLECTION FAULT-TOLERANT CONTROL SYSTEM, COMPUTER PROGRAM PRODUCT AND RELATED METHODS
Various approaches include: obtaining temperature data indicating temperatures of distinct zones in an upper half of a steam turbine shell and a lower half of...
2017/0002682 DETECTION METHOD OF SENSOR IN GAS TURBINE
A detection method of a sensor in a gas turbine includes adopting a pressure sensor to measure a pushing force of a push rod; measuring a first rotational...
2017/0002681 METHOD OF CONTROLLING A POSITION ACTUATION SYSTEM COMPONENT FOR A GAS TURBINE ENGINE
A method for controlling a position actuation system component in a gas turbine engine based on a modified proportional and integral control loop is provided....
2017/0002680 LINEAR MOTION MECHANISM, GOVERNING VALVE DRIVE DEVICE, AND STEAM TURBINE
A linear motion mechanism (27) is provided with: a cylinder rod (312) into which a ball screw (30) can be inserted, said cylinder rod (312) comprising a base...
2017/0002679 ELECTRIC ACTUATOR FOR ENGINE CONTROL
An electric actuator for control of an engine includes an electric motor coupled to a drive shaft that extends to align a gear interface of the electric...
2017/0002678 ROTOR OFF-TAKE ASSEMBLY
According to exemplary embodiments, a rotor off-take assembly is provided by positioning an angled hole or aperture in a stator assembly. This angled hole...
2017/0002677 BREAK-IN SYSTEM FOR GAPPING AND LEAKAGE CONTROL
A blade outer air seal for use in a gas turbine engine having an axis of rotation includes a main body having a mating face configured to face, be positioned...
2017/0002676 TURBINE SHROUD WITH MOVABLE ATTACHMENT FEATURES
A turbine shroud for positioning radially outside of blades of a turbine rotor includes a carrier, a blade track, and a track attachment system. The blade...
2017/0002675 SEAL FOR A GAS TURBINE ENGINE
A gas turbine engine assembly includes a shield that has a first portion and a second portion. The first portion extends radially from an axial end portion of...
2017/0002674 TURBINE SHROUD WITH CLAMPED FLANGE ATTACHMENT
A turbine engine including a turbine shroud for positioning radially outside of blades of the turbine rotor. The turbine shroud includes a carrier, a retention...
2017/0002673 ROTOR BLADE WITH WHEEL SPACE SWIRLERS AND METHOD FOR FORMING A ROTOR BLADE WITH WHEEL SPACE SWIRLERS
The present disclosure is directed to a rotor blade and method for forming the rotor blade. The rotor blade includes a platform having a bottom side radially...
2017/0002672 SEALING STRUCTURE FOR TURBOCHARGER HOUSING
Bolt holes 16 are formed in a joint part 14 of a turbine housing 12, with flanged bolts 40 screwed in the bolt holes 16. A flange part 32 of a bearing housing...
2017/0002671 AXIAL TRANSFER TUBE
What is described is a transfer tube for use with an airfoil of a gas turbine engine coupled to a platform. The transfer tube includes a main body having a...
2017/0002670 BULGED NOZZLE FOR CONTROL OF SECONDARY FLOW AND OPTIMAL DIFFUSER PERFORMANCE
A turbine nozzle disposed in a turbine includes a suction side extending between a leading edge of the nozzle and a trailing edge of the turbine nozzle in an...
2017/0002669 MECHANICAL FASTENING SYSTEM FOR ROTATING OR STATIONARY COMPONENTS
A mechanical fastening system for rotating or stationary components such as turbine or compressor blades on a rotor or a shaft or a casing, respectively, is...
2017/0002668 TURBINE COMPONENT HAVING A LOW RESIDUAL STRESS FERROMAGNETIC DAMPING COATING
A turbine component having a low residual stress ferromagnetic damping coating. The ferromagnetic damping coating may include a ferromagnetic damping material...
2017/0002667 HEAT-RESISTANT TURBINE BLADE MADE FROM OXIDE CERAMIC
This relates to a turbine blade comprising a preformed fibrous fabric of fibres consisting of carbon, silicon carbide or rhenium fixed with a binder resin, and...
2017/0002666 AIRFOIL WITH VARIABLE PROFILE RESPONSIVE TO THERMAL CONDITIONS
An airfoil includes an airfoil body having a first section and a second section that differ in coefficient of thermal expansion by at least 10% and that each...
2017/0002665 GAS TURBINE BLADE
A gas turbine blade includes a blade root and a blade aerofoil, a cooling fluid plenum extending inside the gas turbine blade through the blade root, the blade...
2017/0002664 TURBINE BLADE
A turbine blade includes an airfoil having an internal cooling circuit. The cooling circuit includes a body cooling passage with at least one turn, and a tip...
2017/0002663 GAS TURBINE ENGINE AIRFOIL SQUEALER POCKET COOLING HOLE CONFIGURATION
A gas turbine engine airfoil includes a body that provides an exterior airfoil surface that extends in a radial direction to a tip. The exterior surface has a...
2017/0002662 GAS TURBINE ENGINE AIRFOIL WITH BI-AXIAL SKIN CORE
An airfoil for a gas turbine engine includes a body that extends in a radial direction that provides an exterior airfoil surface. The body includes pressure...
2017/0002661 ROTOR BLADE OR GUIDE VANE ASSEMBLY
The disclosure refers to a method of assembling or disassembling a rotor blade or guide vane assembly, wherein the rotor blade or guide vane includes an...
2017/0002660 RING INSERT FOR A WIND TURBINE ROTOR BLADE
The present disclosure is directed to a rotor blade assembly for a wind turbine. The rotor blade assembly includes a rotor blade having a blade root section...
2017/0002659 TIP SHROUDED HIGH ASPECT RATIO COMPRESSOR STAGE
A gas turbine engine compressor stage includes a rotor. Compressor blades are supported by the rotor. The blades include an inner flow path surface each...
2017/0002658 IN-SITU LEACHING OF ORE DEPOSITS LOCATED IN IMPERMEABLE UNDERGROUND FORMATIONS
A method and system of in-situ leaching of ore deposits located within underground formations comprising non-porous and impermeable rock. The method includes...
2017/0002657 CUTTER HEAD FOR MINING MACHINE
A cutter head includes a first member, a cutting bit, and a second member. The first member includes a first end and a second end and includes a first mass....
2017/0002656 NON-CONCENTRIC PROTRUDING SHAFT FIXED BEARING RECIPROCATING IMPACT PART FOR IMPLEMENTING RECIPROCATING IMPACT...
A reciprocating impact part non-concentric protruding shaft fixed bearing method, comprising: arranging an eccentric shaft section (12) and a power shaft...
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