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Patent # Description
2016/0281556 OIL PAN PART FOR A MOTOR VEHICLE
An oil pan part for a motor vehicle, in particular a passenger car, with a housing and a balancing shaft arrangement with at least one balancing shaft which is...
2016/0281555 ENGINE LUBRICATING DEVICE
There is provided an engine lubricating device with which passage resistance of an oil strainer can be reduced and a support stay for an oil filter is...
2016/0281554 LUBRICATING DEVICE OF INTERNAL COMBUSTION ENGINE
In a lubricating device of an internal combustion engine having a crank chamber and a transmission chamber, which is arranged in the rear of the crank chamber...
2016/0281553 SLIDING CAM SYSTEM HAVING AN EXTENDED ENGAGEMENT REGION
A sliding cam system, having at least one sliding cam, which is arranged in a rotationally fixed but axially displaceable manner on at least one axially fixed...
2016/0281552 Valve arrangement
A valve arrangement for the measured supply of gaseous fuel in internal combustion engines with a plurality of electromagnetically operable control valves of...
2016/0281551 HYDRAULIC CIRCUIT FOR VALVE DEACTIVATION
Methods and systems are provided for deactivating a valve actuation mechanism. In one example, a system may include first and second hydraulic galleries for...
2016/0281550 SYSTEM FOR LUBRICATING VALVE ASSEMBLY OF ENGINE
A system for lubricating a valve assembly of an engine is disclosed. The system includes a valve bridge having a base portion is disposed on a guide rod. The...
2016/0281549 VALVE OPENING/CLOSING TIMING CONTROL DEVICE
The valve opening/closing timing control device includes: a driving rotating body; a driven rotating body; a fixed shaft portion; a fluid pressure chamber; a...
2016/0281548 CAMSHAFT ADJUSTING DEVICE
A camshaft adjusting device including a stator which is connectable to a crankshaft of an internal combustion engine and a rotor which is connectable to a...
2016/0281547 WASHER MEMBER IN VALVE HOUSING OF ENGINE
A washer member disposed in a valve housing of an engine is disclosed. The washer member resiliently supports an injector push member via an elastic member and...
2016/0281546 VARIABLE VALVE MECHANISM OF INTERNAL COMBUSTION ENGINE
The present invention provides a variable valve mechanism of an internal combustion engine, which includes an input member, an output member, a slider and a...
2016/0281545 Versatile Pinch Point Avoidance Recuperator for Supercritical Carbon Dioxide Power Generation Systems
A supercritical carbon dioxide power generation Brayton cycle system and method that employs an alternate heat recuperation method and apparatus that utilizes...
2016/0281544 METHOD AND SYSTEM FOR PROCESSING ANIMAL WASTE
A method and system of processing animal waste is disclosed. In a particular embodiment, the method includes transferring animal waste to a gasifier to burn...
2016/0281543 COMBINED CYCLE POWER PLANT
The invention relates a combined cycle power plant with a gas turbine, a shaft connecting a compressor to a turbine, and a first generator, a heat recovery...
2016/0281542 HEAT-COLLECTING-TYPE POWER GENERATION SYSTEM
Provided is a heat-collecting-type power generation system capable of maintaining a stable power generation efficiency even if supplied heat varies. The system...
2016/0281541 FLANGE RELIEF FOR SPLIT CASING
A split case for a gas turbine engine includes multiple split case portions defining a turbine engine case section. Each of the split case portions has a first...
2016/0281540 APPPARATUS FOR MANUFACTURING A FLANGED COMPOSITE COMPONENT AND METHODS OF MANUFACTURING THE SAME
A method of manufacturing a flanged composite component is provided. The method includes coupling a composite structure to s first composite material. The...
2016/0281539 INNER FIXED STRUCTURE LEADING EDGE LATCH
Pin latch assemblies and cam latch assemblies are disclosed. A pin latch assembly is provided comprising a pin housing at least partially enclosing a pin, an...
2016/0281538 Process to Remanufacture a Turbine Backplate
A process of remanufacturing a backplate used in turbochargers is provided and includes using a mask or an anti-bonding agent and a thermal metal spray. The...
2016/0281537 OIL SCOOP AND SHAFT WITH AXIALLY-ORIENTED HOLE
Aspects of the disclosure are directed to a system associated with an engine of an aircraft. The system includes a shaft configured with at least one...
2016/0281536 PISTON RING ANTI-ROTATION
A squeeze film damper bearing assembly includes a bearing and a squirrel cage radially outward of and supporting the bearing. The squirrel cage includes a...
2016/0281535 BEARING DEVICE FOR A TURBOCHARGER AND TURBOCHARGER
The invention resides in a bearing device for an exhaust gas turbocharger, comprising a first radial bearing and a second radial bearing configured for the...
2016/0281534 BEARING HOLDER HAVING A AXISYMMETRIC SEALABLE GIMLET
The present invention relates to a bypass engine bearing holder (1) that holds an upstream bearing (6) and defines, with said upstream bearing, an oil chamber...
2016/0281533 MOUNTING ASSEMBLY FOR A BUNDLE OF A COMPRESSOR
A mounting assembly for assembling a bundle of a compressor is provided. The mounting assembly may include a plurality of biasing members and a mechanical...
2016/0281532 HEAT EXCHANGER FOR A GAS TURBINE ENGINE
A heat exchanger apparatus for a gas turbine engine includes: a plurality of heat exchanger pipes, each pipe having first and second ends; wherein the heat...
2016/0281531 DAMPER FOR STATOR ASSEMBLY
A stator assembly for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, at least one stator vane...
2016/0281530 MATERIAL FOR RING ROLLING
The present invention provides a high quality material for ring rolling. The material includes radially outer and inner peripheral surfaces. In the material, a...
2016/0281529 AIRCRAFT POWER OUTTAKE MANAGEMENT
A system and method for controlling the operation of a gas turbine engine supplying power to an aircraft. The engine is controlled according to a reading of an...
2016/0281528 MONITORING A DYNAMIC PARAMETER SUCH AS TORQUE IN A ROTATIONAL SYSTEM
A system is provided for a turbine engine. The system includes a rotor assembly and a monitoring system. The rotor assembly includes a plurality of rotor...
2016/0281527 OIL SCOOP WITH INTEGRATED SENSOR
Aspects of the disclosure are directed to a shaft of an engine of an aircraft, an oil scoop coupled to the shaft, a first portion of a sensor integrated with...
2016/0281526 TURBINE
A low-pressure turbine of a jet engine includes: a turbine case; turbine blades rotatable about an axis of the turbine case; and a shroud including a plurality...
2016/0281525 MOBILE TURBINE BLADE WITH AN IMPROVED DESIGN FOR AN AIRCRAFT TURBOMACHINE
A turbine blade for an aircraft turbomachine including a root, an airfoil and a platform inserted between the airfoil and the root and delimiting a gas...
2016/0281524 CLAMPING SEAL FOR JET ENGINE MID-TURBINE FRAME
A mid-turbine frame (MTF") for a jet engine is disclosed and comprises a duct that extends between a high pressure jet engine turbine ("HPT") and a low...
2016/0281523 HULA SEAL
The invention concerns a conical hula seal wherein an inner part of the conical hula seal is closer to a conical hula seal longitudinal axis than an outer part...
2016/0281522 SEALING ARRANGEMENTS IN GAS TURBINES
The invention concerns a gas turbine having a picture frame, a first vane, and a sealing arrangement to seal a gap between the picture frame and the first...
2016/0281521 FLOWING MATEFACE SEAL
Aspects of the disclosure are directed to a first platform, a second platform, a seal arranged between the first platform and the second platform, a first slot...
2016/0281520 SHAFT SEALING DEVICE, ROTATING MACHINE, AND METHOD FOR MANUFACTURING SHAFT SEALING DEVICE
A shaft sealing device (10) includes a plurality of leaves (20) that is arranged in a periphery of a rotating shaft (50) and divides a space around the...
2016/0281519 NOZZLE ASSEMBLY AND STATIONARY NOZZLE THEREFOR
A nozzle assembly is provided. The nozzle assembly includes at least one stationary nozzle. An outer ring having a predefined shape includes at least one...
2016/0281518 TURBINE INTRUSION LOSS REDUCTION SYSTEM
Systems and devices configured to reduce windage and mixing losses in a turbine by redirecting and/or aligning a direction of a leakage flow with the flowpath...
2016/0281517 CAST NOZZLE WITH SPLIT AIRFOIL
A nozzle segment for a turbine nozzle of a gas turbine engine is disclosed. The nozzle segment includes an upper endwall, a lower endwall spaced apart from the...
2016/0281516 WIRE SEAL
The disclosure concerns a wire seal for sealing a gap between two components of a gas turbine, the wire seal including a first core and a second core spaced...
2016/0281515 METHOD OF ATTACHING A CERAMIC MATRIX COMPOSITE ARTICLE
A rotor of a turbine engine includes a mounting slot for receiving a blade. The example blade is formed from a ceramic material and is received within the...
2016/0281514 ARTICLE HAVING VARIABLE COMPOSITION COATING
A coated article includes a substrate and an MCrAlY coating supported on the substrate. The M includes at least one of nickel, cobalt, and iron, Cr is...
2016/0281513 COMPOSITIONS AND METHODS OF DEPOSITION OF THICK ENVIRONMENTAL BARRIER COATINGS ON CMC BLADE TIPS
Coating systems are provided for use on a CMC substrate, that can include: a bond coat on a surface of the CMC substrate; a first rare earth silicate coating...
2016/0281512 TURBINE BLADE WITH A CENTRAL BLOWOUT AT THE TRAILING EDGE
A turbine blade with aerodynamic aerofoil, which extends from a bottom to a top end and has two aerofoil walls extending between, which transversely thereto...
2016/0281511 MODIFIED SURFACE AROUND A HOLE
A layer system is provided having a substrate, an outermost layer with a surface, at least one hole at least in the outermost layer, wherein in the vicinity...
2016/0281510 TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES
A turbine component includes: a metallic wall having opposed interior and exterior surfaces, the wall configured for directing a combustion gas stream in a gas...
2016/0281509 GAS TURBINE ENGINE AIRFOIL PROFILE
An example airfoil includes an airfoil body with a leading edge and a trailing edge joined by a pressure side and a suction side to provide an external airfoil...
2016/0281508 TURBOMACHINE WITH A COOLED COUPLING GUARD
A coupling guard for a rotating member comprising a shell surrounding the rotating member, a plenum disposed in the shell, at least an injection tube for...
2016/0281507 MULTI-VANE-TYPE FLOW KINETIC ENERGY DEVICE
Disclosed is a multi-vane-type flow kinetic energy device placed in the atmosphere with an air current or in a body of water with a water current, and...
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