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Patent # Description
2016/0146062 CAMSHAFT ASSEMBLY FOR AN INTERNAL COMBUSTION ENGINE
A camshaft assembly for an internal combustion engine includes a camshaft, a first lobe set, and a second lobe set, extending along, and rotatable about, a cam...
2016/0146061 ELECTROTHERMAL ENERGY STORAGE SYSTEM AND AN ASSOCIATED METHOD THEREOF
An electrothermal energy storage and discharge system is provided including a charging cycle and a discharging cycle. The charging cycle includes a...
2016/0146060 METHOD FOR OPERATING A COMBINED CYCLE POWER PLANT
A method for operating a combined cycle power plant, according to which shortly before the planned start-up of a parked load, the steam turbine is lowered to a...
2016/0146059 METHOD AND DEVICE FOR CONTROLLING THE SPRAYING OF WATER INTO THE FLUE GAS DUCT OF A GAS AND STEAM TURBINE...
A method for operating a gas and steam turbine installation, wherein the heat contained in the expanded flue gas of the gas turbine is used to generate steam...
2016/0146058 Method for Energy Saving
Method for coupling a first heat-requiring industrial process to a second cold-requiring industrial process, whereby a first circuit for energy recovery (1)...
2016/0146057 WATER REMOVAL DEVICE FOR STEAM TURBINE
A hollow portion is formed inside a stator blade. A slit having an inlet opening on a pressure surface of the stator blade facing wet steam flow is formed that...
2016/0146056 DEVICE AND METHOD FOR SEPARATING DIRT PARTICLES FROM THE WORKING MEDIUM OF A TURBINE
The invention relates to a device and a method for separating dirt particles from the working medium of a turbine (10). The turbine (10) comprises at least one...
2016/0146055 LINER HANGER WITH SPHERICAL WASHERS
A liner assembly for a gas turbine engine includes a liner defining an inner surface exposed to exhaust gases and a duct spaced radially outward of the liner....
2016/0146054 CASING SUPPORT STRUCTURE
A support structure suitable for interposing between the engine and the nacelle of an aeroengine and suitable for being fastened on an intermediate casing, the...
2016/0146053 BLADE OUTER AIR SEAL SUPPORT STRUCTURE
A support structure for a gas turbine engine includes an axially extending portion that forms a loop. A radially extending portion extends radially inward from...
2016/0146052 FORGED CAST FORGED OUTER CASE FOR A GAS TURBINE ENGINE
A case for a gas turbine engine includes a cast case section cast case section configured to be welded between a forward case section and an aft case section.
2016/0146051 TURBINE ENGINE CASING HAVING A CUT-OUT FLANGE
The present invention relates to a turbine engine casing (1), in particular a turbojet exhaust casing, including at least one hoop (2) and at least one flange...
2016/0146050 FAN CASE LINER REMOVAL WITH EXTERNAL HEAT MAT
A method of replacing a fan case liner panel in an engine fan case is provided. In one illustrative form, the method may include applying heat to an engine fan...
2016/0146049 SEALING INTERFACE FOR A CASE OF A GAS TURBINE ENGINE
A case assembly for a gas turbine engine, includes a case with an oversized case boss, said oversized case boss including a peripheral wall that defines a...
2016/0146048 LUBRICATION OF JOURNAL BEARING DURING CLOCKWISE AND COUNTER-CLOCKWISE ROTATION
The present disclosure is applicable to all gear trains using a journal bearing as a means of supporting gear shaft rotation. It is related in some embodiments...
2016/0146047 TURBOCHARGER ROLLER SUPPORT SYSTEM
Disclosed is an embodiment of a turbocharger roller support system that utilizes roller-shaft interfaces that are slanted to locate a turbocharger shaft with a...
2016/0146046 RADIALLY STACKED INTERSHAFT BEARING
An exemplary gas turbine engine includes a radially stacked intershaft bearing assembly. The assembly includes an outer stubshaft having outer and inner...
2016/0146045 TURBINE ENGINE ROTOR SHAFT COMPRISING AN IMPROVED HEAT EXCHANGE SURFACE
A turbine engine rotor shaft includes at least one portion having an outer periphery having a determined diameter forming a free surface for heat exchange with...
2016/0146044 INTERNALLY COOLED TURBINE PLATFORM
A turbine flowpath component for a gas turbine engine includes a platform defining at least one internal cooling cavity and a turbine flowpath component cover...
2016/0146043 COOLING APPARATUS FOR TURBOMACHINERY WITH METHOD OF INSTALLATION
Embodiments of the present disclosure provide cooling systems for turbomachinery and methods of installation. In an embodiment, an apparatus of the present...
2016/0146042 GAS TURBINE AND HEAT SHIELD FOR A GAS TURBINE
A gas turbine includes a number of annular rotor blade rows coaxially mounted in a heating gas channel and a number of annular stator blade rows mounted...
2016/0146041 BLADE OR VANE FOR A TURBOMACHINE AND AXIAL TURBOMACHINE
The present invention relates to a blade (100) or vane for a turbomachine, having at least one impulse element housing (1.1, 1.2) with a first impact cavity...
2016/0146040 Alternating Vane Asymmetry
A vane assembly for a gas turbine engine may include a plurality of vanes being arranged in vane groupings symmetrically spaced circumferentially from each...
2016/0146039 ACOUSTIC ATTENUATION WITH ADAPTIVE IMPEDANCE
An acoustic liner may include a core with a plurality of resonator chambers, a perforated top sheet coupled to the core, and a backskin coupled to the core. A...
2016/0146038 TURBOMACHINE INCLUDING A VANE AND METHOD OF ASSEMBLING SUCH TURBOMACHINE
A vane for a turbomachine includes a pressure surface and a suction surface opposite the pressure surface. The pressure surface and the suction surface define...
2016/0146037 VARIABLE TURBINE GEOMETRY VANE WITH SINGLE-AXLE, SELF-CENTERING PIVOT FEATURE
A vane pack assembly (25) for a variable geometry turbocharger (10) including a an upper vane ring (28) and a lower vane ring (30) and a plurality of...
2016/0146036 ENGINE CASING ELEMENT
An engine casing element comprises at least one clearance control cavity, the clearance control cavity being delimited by a clearance control cavity inner wall...
2016/0146035 HYBRID RAM AIR TURBINE
A ram air turbine is provided that utilizes a hybrid design. The ram air turbine includes a hydraulic power conversion device directly coupled to a turbine...
2016/0146034 ABRADABLE COMPOSITION AND SEAL OF AN AXIAL-FLOW TURBOMACHINE COMPRESSOR CASING
The invention relates to a composition for an abradable seal of a turbomachine, the composition comprising an aluminium base, nickel powder, polyester powder....
2016/0146033 GAS TURBINE ENGINE CLEARANCE CONTROL
A gas turbine engine includes first and second structures secured to one another at a bolted flange joint. A seal is supported by a third structure. A cover is...
2016/0146032 Pressure Seal With Non-Metallic Wear Surfaces
A gas turbine engine has a first component and a second component. The first and second components have a high-pressure chamber on one side and a low pressure...
2016/0146031 TURBINE BLADE OR VANE HAVING A STEPPED AND BEVELED PLATFORM EDGE
A turbine blade, including: an airfoil and a platform, which has an upper face on which the airfoil is arranged; and at least one lateral face, the lateral...
2016/0146030 NON-METALLIC ENGINE CASE INLET COMPRESSION SEAL FOR A GAS TURBINE ENGINE
A non-metallic engine case inlet compression seal for a gas turbine engine includes a non-metallic longitudinal leg section that extends from the non-metallic...
2016/0146029 SEALING BUSH CARRIER FOR A STEAM TURBINE AND STEAM TURBINE
A sealing bush carrier for a steam turbine, the steam turbine at least having a turbine rotor and a turbine housing, whereby the sealing bush carrier is...
2016/0146028 HIGH STRENGTH JOINTS IN CERAMIC MATRIX COMPOSITE PREFORMS
A joint between a first preform component and a second preform component that are constructed for ultimate use in a gas turbine engine is disclosed. A...
2016/0146027 GUIDE VANE RING AND TURBOMACHINE
The invention is directed to a guide vane ring for a turbomachine, in which a vane bearing is produced in the inner ring via platform plates of the vanes and...
2016/0146026 TRANSITION DUCT ARRANGEMENT IN A GAS TURBINE ENGINE
An arrangement for a gas turbine engine includes a combustor for producing a working medium by combustion of a mixture of fuel and an oxidant, a turbine...
2016/0146025 VARIABLE PITCH FAN FOR GAS TURBINE ENGINE AND METHOD OF ASSEMBLING THE SAME
A gas turbine engine is provided. The gas turbine engine includes a core and a variable pitch fan arranged in flow communication with the core. The variable...
2016/0146024 HYBRID BONDED TURBINE ROTORS AND METHODS FOR MANUFACTURING THE SAME
Hybrid bonded turbine rotors and methods for manufacturing the same are provided. A hybrid bonded turbine rotor comprises a turbine disk and a plurality of...
2016/0146023 Rotor With Blades Secured by Woven Fiber Attachment System
A propulsive engine rotor configured for operation within a gas turbine includes a plurality of spaced airfoil blades circumferentially affixed to an outer...
2016/0146022 HIGH-MODULUS COATING FOR LOCAL STIFFENING OF AIRFOIL TRAILING EDGES
An airfoil is disclosed. The airfoil may comprise a leading edge, a body portion and a trailing edge formed from a high-modulus plating. The body portion of...
2016/0146021 COMPOSITE BLADES FOR GAS TURBINE ENGINES
A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. Each blade is formed as a composite structure including...
2016/0146020 BRAZING METHOD FOR REINFORCING THE Z-NOTCH OF TiAl BLADES
The present invention relates to a method for arranging a reinforcement (8, 9) on a TiAl component (1) of a turbomachine, the reinforcement being formed by a...
2016/0146019 COOLING CHANNEL FOR AIRFOIL WITH TAPERED POCKET
The present invention includes systems and methods for providing cooling channels located within walls of a turbine airfoil. These cooling channels include...
2016/0146018 TAPERED COOLING CHANNEL FOR AIRFOIL
The present invention includes systems and methods for providing cooling channels located within walls of a turbine airfoil. These cooling channels include...
2016/0146017 LEADING EDGE COOLING CHANNEL FOR AIRFOIL
Methods and systems of cooling airfoils are provided. The present invention provides systems and methods for providing cooling channels located within walls of...
2016/0146016 ROTOR RIM IMPINGEMENT COOLING
A system and method of cooling a radially outer surface of a rotor wheel post of a turbine wheel and a rotor wheel space between a turbine bucket and a rotor...
2016/0146015 FLUIDFOIL
There is disclosed a fluidfoil comprising a selectively fluid chargeable capillary and a flexible body adjacent the capillary, the shape of the flexible body...
2016/0146014 MODIFIED BUCKET PLATFORMS OF TURBINE BUCKETS AND METHODS FOR MODIFYING BUCKET PLATFORMS OF TURBINE BUCKETS
Methods for modifying bucket platforms of turbine buckets include removing a portion of the bucket platform to form a void, wherein the void comprises a...
2016/0146013 TURBINE ARRANGEMENT
The invention relates to a turbine for generating work by a stagewise expansion of a gas, such as steam wherein a downstream stage guide average height is less...
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