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Patent # Description
2017/0298789 GASKET FOR A VALVE OF AN INTERNAL COMBUSTION ENGINE
A gasket for a valve of an internal combustion engine is described. The valve has a guide element defining a through seat, and a stem movable in a sliding...
2017/0298788 VALVE OPENING/CLOSING TIMING CONTROL APPARATUS
A valve opening/closing timing control apparatus includes: a driving side rotating body rotating synchronously with a crankshaft of an internal combustion...
2017/0298787 VALVE GEAR FOR ENGINE AND METHOD OF MANUFACTURING ROCKER ARMS
A valve gear for an engine includes a camshaft including a cam, a rocker shaft, and a first rocker arm which swings when pressed by the cam. The valve gear...
2017/0298786 VARIABLE VALVE DRIVE HAVING A ROCKER LEVER
The present disclosure relates to a variable valve drive for a lifting valve, in particular for a charge-exchange valve of an internal combustion engine, which...
2017/0298785 ROCKER ARM ASSEMBLY AND COMPONENTS THEREFOR
A switching rocker arm system includes a rocker assembly having a first end and a second end, and engaging a lash adjuster an and engine valve. The system...
2017/0298784 VALVE GEAR FOR ENGINE
A valve gear for an engine includes camshaft supports, a camshaft, a rocker housing separate from the cam shaft supports, a rocker shaft, a first rocker arm,...
2017/0298783 METHOD FOR COATING THE NOSE OF THE CAMS OF A CAMSHAFT WITH DLC, CAMSHAFT OBTAINED IN THIS WAY AND FACILITY FOR...
A cam treatment to reduce the friction coefficient thereof relative to a counterpart in an area provided with a hard coating made from amorphous Diamond-Like...
2017/0298782 SYSTEM AND METHOD FOR INCREASING THE RESPONSIVENESS OF A DUCT FIRED, COMBINED CYCLE, POWER GENERATION PLANT
A system and method for increasing the responsiveness of a duct fired, combined cycle power generation plant (12) via operating one or more gas turbine engines...
2017/0298781 Strain Augmented Thermodynamic Power Cycle
Strain augmented power cycle is disclosed. This power cycle is a thermodynamic power cycle that contains a strain energy device to increase the thermodynamic...
2017/0298780 THERMAL ENERGY RECOVERY DEVICE AND OPERATING METHOD OF THE SAME
A thermal energy recovery device includes: a circulation line having an evaporator, an expander, a condenser, and a pump; a power recovery machine; a first...
2017/0298779 Tooling For Partial Disassembly Of A Bypass Turbofan Engine
Tooling for partial disassembly of a bypass turbofan engine wherein the longitudinal axis of the bypass turbofan engine remains generally horizontal during...
2017/0298778 ASSEMBLING AID FOR ASSEMBLING/DE-ASSEMBLING A TURBINE ASSEMBLY
An assembling aid for assembling or de-assembling a turbine assembly having at least two aerofoil assemblies connected to each other by at least two...
2017/0298777 GAS TURBINE ENGINE ASSEMBLIES WITH CERAMIC MATRIX COMPOSITE COMPONENTS HAVING UNDULATED FEATURES
An assembly adapted for use in a gas turbine engine is disclosed herein. The assembly includes a first component including metallic materials and a second...
2017/0298776 BLADE OUTER AIR SEAL HAVING RETENTION SNAP RING
A retention member for a component of a gas turbine engine and methods of using the same are provided. The retention member includes an annular body having a...
2017/0298775 ASSEMBLY OF TWO PARTS COMPRISING A REMOVABLE CENTRING SEAT FOR AN AIRCRAFT TURBINE ENGINE
A turbine engine for an aircraft which includes, in general, at least one assembly made up of a first part wherein a second part is attached with an attachment...
2017/0298774 COUPLING ASSEMBLY FOR COMPONENTS OF CERAMIC MATRIX COMPOSITES FOR A TURBINE CENTER FRAME
A coupling assembly, including a first component and a second component overlapping one another in a join region; a joining device allowing the first component...
2017/0298773 BEARING HAVING INTEGRALLY FORMED COMPONENTS
Embodiments of a stage for a turbomachine have been provided herein. In some embodiments, a stage for a turbomachine may include a bearing having a housing,...
2017/0298772 ROTARY MACHINE WITH GAS BEARINGS
A rotary machine for an aeronautical device includes a thrust generator. The rotary machine additionally includes a rotary component rotatable with the thrust...
2017/0298771 Flow Strakes for Turbocharger Bearing Housing Oil Core
A bearing housing for a turbocharger is disclosed. The bearing housing includes a first end proximate to a turbine wheel of the turbocharger and a second end...
2017/0298770 FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan shaft driving a fan having fan blades, a fan shaft...
2017/0298769 BEARING STRUCTURE OF TURBOCHARGER
An object of the present invention is to provide a bearing structure of a turbocharger that can prevent generation of unusual noise and a decrease in operation...
2017/0298768 FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan shaft driving a fan having fan blades, a fan shaft...
2017/0298767 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 turbine section including a fan drive turbine and a...
2017/0298766 THRUST BEARING
A bearing including a bearing pad and a housing is provided. The bearing pad has a thrust face for supporting a vibration along an axial direction of the...
2017/0298765 FLUID-FILLED DAMPER FOR GAS BEARING ASSEMBLY
The present disclosure is directed to a gas-lubricated bearing assembly for a gas turbine engine and method of damping same. The bearing assembly includes a...
2017/0298764 COMPARTMENTALIZATION OF COOLING AIR FLOW IN A STRUCTURE COMPRISING A CMC COMPONENT
A structure in a gas turbine engine comprises a spar and a CMC component adjoining the spar and separated from the spar by a cavity supplied by cooling air. At...
2017/0298763 MOUNTING ARRANGEMENT FOR MOUNTING A FLUID COOLER TO A GAS TURBINE ENGINE CASE
A mounting arrangement for mounting a fluid cooler to an engine case of a gas turbine engine, the mounting arrangement comprises at least one fixture adapted...
2017/0298762 GAS TURBINE ENGINE TURBINE VANE BAFFLE AND SERPENTINE COOLING PASSAGE
An airfoil for a gas turbine engine includes pressure and suction side walls joined to one another at leading and trailing edges. The pressure and suction side...
2017/0298761 HEAT SHIELD
A heat shield (100) and method for assembling such is disclosed. The heat shield (100) may comprise an outer wall (122) and an inner wall (124). The outer wall...
2017/0298760 Axial Turbine Engine Compressor De-Icing Blade
An aeroplane turbojet low-pressure compressor vane includes a leading edge, a trailing edge, a surface, and an extrados surface which extend from the leading...
2017/0298759 FAILURE DETECTION DEVICE
The failure detection device includes an accumulated data storage unit 30, a unit space generating module 13, a signal space generating module 14 and a...
2017/0298757 GEARED ARCHITECTURE FOR HIGH SPEED AND SMALL VOLUME FAN DRIVE TURBINE
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan shaft driving a fan having fan blades. A fan shaft...
2017/0298756 Stand Alone Hydro Electric Power Supply System
A "Hydro Electric Power Supply System" that comprises an upper water tank and a lower water tank. The tanks are positioned where the said upper water tank is...
2017/0298755 COMPRESSOR SYSTEM
A compressor system (10) includes a motor (3) including a rotor (31) configured to rotate about an axis and a stator (32) disposed on an outer circumference...
2017/0298754 CONTRA-FLOW STRIPS, CONTRA-FLOW SEAL SEGMENTS, AND METHODS FOR INHIBITING LEAKAGE
A contra-flow strip for inhibiting leakage of a fluid between a rotating member and a stationary member includes, for example, a base supportable by the...
2017/0298753 TURBINE SHROUD WITH SEALED BOX SEGMENTS
A turbine shroud adapted to extend around a bladed turbine wheel to block gasses from passing over the bladed turbine wheel is disclosed. In a segmented...
2017/0298752 GAS BEARING SEAL
A turbomachine includes a compressor section, a turbine section, and a rotary component. The rotary component is attached to and rotatable with a portion of at...
2017/0298751 MODULAR TURBINE VANE
An airfoil attachment system (10) for a modular turbine vane (12) of a gas turbine engine (14) including an outer attachment system (10) with forward and aft...
2017/0298750 VANE WITH SPOILER
Relates to a vane for a turbomachine. The vane (12') has a blade (13') and a root (18') to be engaged in an axial groove in a disc of the turbomachine. The...
2017/0298749 MACHINING PROCESS FOR MULTI-VANE NOZZLE
The present invention relates to a method for machine finishing the shape of a blank casting for a multi-vane, in particular bi-vane, nozzle of a turbine...
2017/0298748 GAS TURBINE ENGINE WITH COMPLIANT LAYER FOR TURBINE VANE ASSEMBLIES
A turbine vane assembly for use in a gas turbine engine includes an endwall, a flow path component, and a load-distribution system. The endwall is arranged...
2017/0298747 GAS TURBINE ENGINE TRANSITION DUCT AND TURBINE CENTER FRAME
A transition duct includes fairings with transition duct flow passage and hollow fairing airfoils extending between outer and inner walls of fairings and means...
2017/0298746 TURBINE ENGINE GUIDE VANE
The present invention relates to a turbine engine guide (23) vane (25), with a height (H) extending between a vane root (26) and a vane tip (27) along a radial...
2017/0298745 FIBER REINFORCED AIRFOIL
An airfoil and a method of manufacturing an airfoil may be provided, where the airfoil comprises a core and a shell. The core comprises core ceramic fibers...
2017/0298744 SYSTEM FOR COOLING SEAL RAILS OF TIP SHROUD OF TURBINE BLADE
A turbine blade includes a tip shroud having a seal rail. The seal rail includes a tangential surface extending between tangential ends. The turbine blade...
2017/0298743 COMPONENT FOR A TURBINE ENGINE WITH A FILM-HOLE
An apparatus and method relating to a film-hole of a component of a turbine engine comprising including forming the hole in the component and applying a...
2017/0298742 TURBINE ENGINE AIRFOIL BLEED PUMPING
An apparatus and method of minimizing airfoil boundary layer separation utilizing at least one bleed inlet disposed on the outer wall of the airfoil, such as...
2017/0298741 STATOR OF AN AIRCRAFT TURBINE ENGINE
A stator of an aircraft turbine engine, comprising an annular row of fixed vanes and an annular row of arms, wherein the trailing edges of the fixed vanes are...
2017/0298740 Noise Reduction to the Trailing Edge of Fluid Dynamic Bodies
A fluid dynamic body having a trailing edge with a pattern formed thereon, the pattern can include a plurality of smoothly surfaced adjacent members with...
2017/0298739 Bolt On Seal Ring
A device to route cooling air to a turbine blade is provided. The device includes a seal ring having an L-shaped cross section configured to abut a turbine...
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