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Match Document Document Title
US20130189088 TURBINE EXHAUST DIFFUSER SYSTEM MANWAYS  
A turbine exhaust diffuser system includes a plurality of manways. The plurality of manways each extend between an outer wall of the turbine exhaust diffuser system and an interior access tunnel...
US20110097199 SYSTEM AND METHOD TO INSULATE TURBINES AND ASSOCIATED PIPING  
An insulation system includes at least one turbine insulation compartment configured to enclose at least a portion of a turbine; an insulation storage compartment configured to store a supply of...
US20100278629 Vertical Multi-Phased Wind Turbine System  
A rotational axis multi-phased wind turbine power generating system is disclosed. A differential pressure is created by utilizing the prevailing wind, and air from the prevailing wind is directed...
US20110058934 Cooled Turbine Airfoil Fabricated From Sheet Material  
A turbine airfoil (20) fabricated as an assembly of U-channels (22A-E), each U-channel having a closed side formed by a cross wall (25), an open side (26) opposite the cross wall, and two side...
US20110038710 Application of Dense Vertically Cracked and Porous Thermal Barrier Coating to a Gas Turbine Component  
A configuration for coating a turbine component such as a blade or vane with various forms of thermal barrier coating to provide enhanced temperature capability and increased strain tolerance is...
US20110070075 FASTBACK TURBULATOR STRUCTURE AND TURBINE NOZZLE INCORPORATING SAME  
A heat transfer apparatus, includes a member defining a wall exposed to fluid flow in a predetermined direction of flow; and a plurality of turbulators disposed on the wall. Each turbulator...
US20150240723 BORE BASKET FOR A GAS POWERED TURBINE  
A bore basket for a gas turbine engine includes two cylinders that guide a cooling flow through a bore opening. The cylinder's define an axially aligned gap that further directs fluid flow.
US20110038720 FAN AND FAN ASSEMBLY  
An assembly includes a fan and a heat sink for detachably fixing the fan. The fan includes a pair of first and a pair of second sidewalls, with two pair of rims respectively extending from the...
US20150204345 PROPELLER FAN  
Provided is a propeller fan, including: a boss section including a tubular wall; and a plurality of blades extending in a radiate manner from an outer peripheral surface of the tubular wall of the...
US20150240722 SINGLE PHASE MICRO/MINI CHANNEL HEAT EXCHANGERS FOR GAS TURBINE INTERCOOLING  
A gas turbine engine heat exchange system including a first multi-width channel heat exchanger (MWCHX) configured to transfer heat between a first air stream and a heat transfer fluid. The first...
US20130343881 TURBINE HOUSING OF AN EXHAUST TURBOCHARGER  
A turbine housing of the exhaust turbocharger, having an inlet, which is adjoined by a spiral; having an outlet; and having a coolant arrangement; wherein the coolant arrangement has a plurality...
US20150016975 FAN ASSEMBLY  
A fan assembly includes a motor-driven impeller for creating an air flow, a casing including an interior passage for receiving the air flow, and a plurality of air outlets for emitting the air...
US20110079021 APPARATUS AND METHOD FOR REMOVING HEAT FROM A GAS TURBINE  
An apparatus for removing heat from a turbine includes a stator having a cavity and a first plenum and a second plenum inside the cavity. The second plenum is connected to the first plenum and...
US20130230390 LEADING EDGE STRUCTURE, IN PARTICULAR FOR AN AIR INLET OF AN AIRCRAFT ENGINE NACELLE  
A leading edge structure for an air inlet of an aircraft nacelle includes a leading edge and an inner partition defining a longitudinal compartment that is located inside the leading edge and...
US20110206502 TURBINE SHROUD SUPPORT THERMAL SHIELD  
A turbine shroud assembly includes an annular thermal shield around an annular shroud support. A honeycomb layer is attached to the shroud support along an inner side of the honeycomb layer and a...
US20130011246 Gas-Turbine Aircraft Engine With Structural Surface Cooler  
The present invention relates to a gas-turbine aircraft engine with a core engine surrounded by a bypass duct, with a substantially annular cooling element being provided in the area of a radially...
US20110033284 STRUCTURALLY DIVERSE THERMAL BARRIER COATINGS  
A coated article includes an article having at least one surface and a thermal barrier coating system disposed upon the at least one surface. The thermal barrier coating system has at least two...
US20090317238 COMBINED ACOUSTIC ABSORBER AND HEAT EXCHANGING OUTLET GUIDE VANES  
An outlet guide vane assembly for turbomachines is provided. The outlet guide vane assembly comprises one or more outlet guide vanes, wherein each of the one or more outlet guide vanes comprises a...
US20080298957 INLET AIR CONDITIONING SYSTEM  
An embodiment of the present invention provides an air conditioning system located upstream of the inlet system for a gas turbine. The air conditioning system may comprise at least one...
US20130052051 TURBOMACHINE  
A turbomachine that includes a housing and a circuit assembly. The housing includes an inlet for admitting a working airflow and a flange that extends from the inlet. The circuit assembly includes...
US20100316491 THERMAL INSULATION STRUCTURE FOR STRUCTURAL MEMBER, AND SCROLL STRUCTURE  
To provide a thermal insulation structure for a structural member and a scroll structure which can be easily used even in integrally constructed structural members and which can ensure reliability...
US20150110601 COOLANT BRIDGING LINE FOR A GAS TURBINE, WHICH COOLANT BRIDGING LINE CAN BE INSERTED INTO A HOLLOW, COOLED TURBINE BLADE  
A coolant bridging line for a gas turbine having inner and outer sides which are separated by a wall, wherein the coolant bridging line extends from a first component of the gas turbine to a...
US20150086325 PUMP WITH INTEGRATED HEATING ELEMENT  
A pump for a dishwasher is configured as an impeller pump having a central water inflow to a rotating impeller for conveying the water in the radial direction out of the impeller into a pump...
US20120263581 Heating pump  
A heating pump includes an electric motor, a pump housing fixed to the motor, an impeller driven by the motor, and a ring heater with an inner hole for heating fluid in the pump housing. The pump...
US20130343880 TURBINE END INTAKE STRUCTURE FOR TURBOCHARGER, AND TURBOCHARGER COMPRISING THE SAME  
A turbine end intake structure for a turbocharger includes a turbine housing, a turbine having multiple blades and located in a turbine shell, and thermal insulation located between the turbine...
US20130115063 OIL MANAGEMENT SYSTEM FOR A COMPRESSOR  
The invention relates to an oil management system for a compressor in a refrigeration system comprising: an oil temperature sensor; a heater arranged to heat oil in a crank case of the compressor;...
US20110266802 Tunnel power turbine system to generate potential energy from waste kinetic energy  
A system for generating energy from waste includes a generator device and an ejector device integrated in a pipe line unit. The generator device includes nozzle venture inlets. The ejector device...
US20150050131 TURBINE HOUSING  
A turbocharger system may include a turbine housing and a tongue insert. The turbine housing may include an inlet, an outlet, and a gas pathway between the inlet and outlet. The gas pathway may...
US20140205447 PURGE AND COOLING AIR FOR AN EXHAUST SECTION OF A GAS TURBINE ASSEMBLY  
A turbine exhaust casing having an outer casing, an inner casing, an annular exhaust gas path defined between outer and inner flow path walls, and a turbine exhaust casing cavity located radially...
US20090136340 HYDRODYNAMISCHE MASCHINE, INSBESONDERE HYDRODYNAMISCHE KUPPLUNG EINES TURBOCOMPOUNDSYSTEMS  
A hydrodynamic machine, and especially a hydrodynamic coupling, for a turbine compound system includes (a) a bladed primary wheel and a bladed secondary wheel which together form an operating...
US20120063890 WIND TURBINE NACELLE WITH COOLER TOP  
The present invention relates to a wind turbine nacelle having a first face with a longitudinal extension in a wind direction, comprising a cooling device having a cooling area and extending from...
US20130239588 PUMP SYSTEM FOR TMS AOC REDUCTION  
An engine includes a duct containing a flow of cool air and a pump system having an impeller with an inlet for receiving air from the duct and an outlet for discharging air into a discharge...
US20100047063 Use of a Tungsten Bronze Structured Material and Turbine Component with s Thermal Barrier Coating  
A tungsten bronze structured ceramic material as a thermal barrier coating is described wherein the tungsten bronze structured ceramic coating material has the formula AO—BvOw—CyOz where O stands...
US20110116912 ZONED DISCONTINUOUS COATING FOR HIGH PRESSURE TURBINE COMPONENT  
A turbine component has an airfoil extending between a leading edge and a trailing edge, and has an outer surface. A coating includes at least two discontinuous areas that are spaced from each...
US20130323036 HEAT SHIELD FOR A LOW-PRESSURE TURBINE STEAM INLET DUCT  
The present invention relates to an assembly comprising a duct, preferably a turbine duct, and at least one segment formed of at least two rigid shells, each shell comprising at least one fixing...
US20130343882 PUMP  
An impeller radial pump includes a pump chamber with a central suction and with a pump chamber outlet, wherein an impeller is provided in the pump chamber. Radially outside of the impeller, a...
US20140119903 Gas Turbine Engine With Inlet Particle Separator and Thermal Management  
A gas turbine engine includes a nose cone at an inlet end, and spaced radially inwardly of a nacelle. A compressor is downstream of the nose cone. A core inlet delivers air downstream of the nose...
US20150086796 CERAMIC THERMALLY INSULATING LAYER SYSTEM HAVING AN EXTERNAL ALUMINUM-RICH LAYER AND METHOD  
A layer system is provided that has at least: a substrate, a ceramic layer and an outermost layer, which has an aluminum-rich form, in particular directly on the ceramic layer, and optionally a...
US20080138181 THERMALLY CONDUCTIVE PUMP MOTOR MOUNT FOR LIFTGATE SYSTEM  
A conductive heat transfer system may include a heat conductive element to thermally couple the pump motor of a liftgate assembly to an outer surface of a pump motor housing assembly.
US20140193247 IMPELLER PUMP  
An impeller pump has a pump casing including a pump chamber and an inlet and an outlet thereon and an impeller therein, and including a heating device for heating the conveyed medium, which...
US20120107104 COMPRESSION SYSTEM FOR TURBOMACHINE HEAT EXCHANGER  
An example turbomachine cooling arrangement includes a pump configured to pressurize a first turbomachine fluid that is then communicated through a heat exchanger assembly to remove thermal energy...
US20140298771 GAS TURBINE EXHAUST DIFFUSER  
A gas turbine exhaust diffuser includes a frustoconical portion that defines an interior surface and an axial centerline. In particular embodiments, the interior surface may have a slope greater...
US20140154048 HUB COOLING APPARATUS ADAPTED TO WIND-POWER GENERATOR AND METHOD THEREOF  
A hub cooling apparatus adapted to a wind generator has a circulating fan module installed in a nosed end of a hub and a wind guiding module installed in a main shaft of a nacelle; wherein the...
US20150175269 CASING FOR A PROPULSION UNIT  
An aircraft propulsion unit comprising an engine and a nacelle including an axisymmetric casing (16) delimiting an air flow path, wherein this casing has at least two openings closed by removable...
US20150086345 TURBO CHARGER HAVING COOLING STRUCTURE  
A turbocharger having a cooling structure may include a center housing on which a shaft is rotatably fitted, a turbine impeller disposed at one end of the shaft, a compressor impeller disposed at...
US20150096306 GAS TURBINE AIRFOIL WITH COOLING ENHANCEMENT  
A turbine nozzle vane segment includes one or more nozzle vanes extending between radially inner and outer side walls, each nozzle vane having a peripheral edge wall extending between a leading...
US20120171059 Turbocharger with integrated actuator  
A turbocharger having a turbine with a wastegate, and a compressor including a compressor housing, a compressor wheel, and a wastegate actuator. The turbine wheel includes blades defining an...
US20140178184 FAN AND MOTOR BEARING HEAT DISSIPATION STRUCTURE THEREOF  
A motor bearing heat dissipation structure includes a metal base, a heat conducting element connected to the metal base and including a wall portion and an extended portion, and a plastic bearing...
US20140010639 GAS TURBINE ENGINE OIL TANK WITH INTEGRATED PACKAGING CONFIGURATION  
A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft...
US20140064941 FAN MODULE FOR A HEAT EXCHANGER  
A fan module (1) includes a support structure (2), a motor (6), and an impeller (12). The support structure (2) includes an outer frame (3), an inner seat (5), and spokes (4) connecting the outer...

Matches 1 - 50 out of 401 1 2 3 4 5 6 7 8 9 >