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US20140186166 |
Hybrid Continuous Fiber Chopped Fiber Polymer Composite Structure
An engine component having a monolithic composite body, the body having a continuous fiber portion, a chopped fiber portion, a thermoplastic polymer contained in both the continuous fiber portion... |
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US20120067054 |
HIGH EFFICIENCY POWER PRODUCTION METHODS, ASSEMBLIES, AND SYSTEMS
The present disclosure provides methods, assemblies, and systems for power production that can allow for increased efficiency and lower cost components arising from the control, reduction, or... |
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US20160153429 |
BUILDINGS WITH WIND-ENERGY-CONVERSION SYSTEMS
An embodiment of a building may include a wind-energy-conversion system with a duct that may be a substantially vertical converging nozzle. An energy extractor may be fluidly coupled to the duct.... |
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US20130004309 |
PROTECTIVE INTERNAL COATINGS FOR POROUS SUBSTRATES
A material contains open pores in which the channels and pores that are internally coated with at least one layer of phosphorus-containing alumina. Such material is formed by infiltrating a porous... |
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US20090160193 |
BENKATINA HYDROELECTRIC TURBINE
New hydroelectric turbine devices, systems, and methods, based on recirculation of fluid through at least one turbine, offer the potential for less costly and greater energy output in many... |
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US20110052379 |
METHOD FOR MONITORING A MIXTURE OF AT LEAST TWO COMPONENTS
Provided is a method and apparatus for monitoring a mixture of at least two components. Also provided is a rotor blade of a wind power installation, a gondola casing of a wind power installation... |
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US20140255173 |
FAN ASSEMBLY
A nozzle for a fan assembly includes an air inlet, an air outlet, an interior passage for conveying air from the air inlet to the air outlet, an annular inner wall, and an outer wall extending... |
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US20120219408 |
CYLINDRICAL STRUCTURE AND METHOD FOR MANUFACTURING THE SAME
A method for manufacturing a cylindrical structure having an axial direction includes: winding a fabric around a mandrel in a circumferential direction that is perpendicular to the axial... |
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US20090065064 |
COMPRESSOR TIP GAP FLOW CONTROL USING PLASMA ACTUATORS
A plasma generator for delaying the onset of rotation stall by tip gap flow control in, for example, an axial flow compressor is disclosed. The tip gap flow control system includes a housing... |
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US20140271162 |
PUMP CASING WITH PRE-STRESSED LINING
A method is described for forming a lining on an inner surface of a pump casing. The lining can protect the pump casing from corrosive and abrasive fluids. The method disclosed improves the... |
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US20160083102 |
NACELLE
A nacelle is configured to be coupled to an underside of a wing so as to form a clearance space therebetween. The nacelle includes at least a first cowling which at least partially defines an... |
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US20120308369 |
LAMINATE THERMAL INSULATION BLANKET FOR AIRCRAFT APPLICATIONS AND PROCESS THEREFOR
A thermal insulation blanket for an aircraft engine, and processes for producing the thermal insulation blanket to have low thermal conductivity and high temperature capability. The thermal... |
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US20140003923 |
FUNCTIONALLY GRADED COMPOSITE FAN CONTAINMENT CASE
A fan containment case for a gas turbine engine includes a first inner layer and a second layer outside the first inner layer, where the second layer is made of a first material having a first... |
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US20130156555 |
BRAZE MATERIALS, BRAZING PROCESSES, AND COMPONENTS WITH WEAR-RESISTANT COATINGS FORMED THEREBY
Braze materials, brazing processes, and coatings produced therefrom, for example, a wear-resistant coating suitable for protecting surfaces subjected to wear at high temperatures. The braze... |
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US20140086734 |
METHOD AND SYSTEM FOR FABRICATING COMPOSITE CONTAINMENT CASINGS
A system and a method for making a composite containment casing are provided. The method includes providing a mandrel, applying at least one ply of a material about the mandrel to form a first... |
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US20130330180 |
PASSAGE CHANNEL FOR A TURBOMACHINE AND TURBOMACHINE
A transition duct for a turbomachine, in particular an aircraft engine, for forming a flow channel between an upstream flow cross section and a downstream flow cross section, including supporting... |
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US20120288363 |
CEILING-MOUNTED INDOOR UNIT FOR AIR CONDITIONING APPARATUS
A ceiling-mounted indoor unit for an air conditioning apparatus is disposed in a ceiling of an air-conditioned room. The ceiling-mounted indoor unit includes a casing having an air outlet formed... |
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US20120301283 |
TURBINE WITH UNEVENLY LOADED ROTOR BLADES
An unevenly loaded turbine rotor blade is disclosed herein, the blade including a power-extracting region adapted for radially-varied (relative to the axis of rotation) power extraction per mass... |
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US20120301281 |
FAN MODULE
A fan module suitable for an electronic apparatus is provided. The fan module includes a bottom plate, a top cover. a sidewall, a heat-dissipating fan and a housing. The sidewall is assembled... |
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US20130260664 |
ECCENTRIC FAN HOUSING
Embodiments of the present disclosure are directed towards an electrical equipment system including an electrical equipment component, a thermal management system configured to direct air over... |
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US20120045321 |
WIND TURBINE NACELLE
The present invention relates to a nacelle for a wind turbine, the nacelle having a first height in its installed position and a second height in its transported position, the first height being... |
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US20090000296 |
Turbocharger having divided housing with integral valve
A turbocharger is provided having a turbine wheel and a housing configured to at least partially enclose the turbine wheel. The housing may have a first turbine volute including a first inlet and... |
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US20110038721 |
FAN WITH DUST-RESISTANT COATING
A method of making a fan having one or more dust-resistant surfaces comprises the steps of: providing (S50) an open mold for injection-molding purposes, having a cavity (43) corresponding to the... |
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US20110211943 |
PANELLED ASSEMBLY
A panelled assembly has a spacer 26 of cuboid, or rectangular prism, shape located between adjacent first panels 16 in order to maintain separation of the panels 16 at a desired minimum distance... |
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US20080247868 |
FAN AND IMPELLER THEREOF
A fan has an impeller, a motor and a frame. The impeller and the motor are disposed within the frame, and the motor is connected to the impeller and drives the impeller to rotate. The impeller... |
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US20080010986 |
Turbocharger with catalytic coating
A turbo machine having a rotor and a stator is at least partially provided on a flow-guiding part with a catalytic coating. The catalytic coating (7, 7′) comprises at least one oxide of a... |
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US20130318941 |
Supercharged Combined Cycle System With Air Flow Bypass
A system and method for supercharging a combined cycle system includes a forced draft fan providing a variable air flow. At least a first portion of the air flow is directed to a compressor and a... |
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US20100284802 |
INFLATABLE WIND TURBINE
A wind turbine has an impeller surrounded by a shroud. The shroud is formed from inflatable components extending between two rigid structural members. When inflated, the shroud acts to increase... |
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US20160032776 |
REINFORCED COMPOSITE CASE
A composite assembly comprises a first composite wall, a second composite wall spaced radially inward from the first outer wall, and a composite reinforcement ring attached to an outer surface of... |
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US20130004306 |
CHORDAL MOUNTING ARRANGEMENT FOR LOW-DUCTILITY TURBINE SHROUD
A shroud apparatus for a gas turbine engine includes: a shroud segment comprising low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed... |
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US20130004307 |
IMPELLER AND CENTRIFUGAL FAN HAVING THE SAME
An impeller and a centrifugal fan having the same are provided. The impeller includes a lower shroud, an upper shroud, and a plurality of blades which are arranged along a circumference direction... |
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US20120248776 |
WAVE ENERGY EXTRACTION SYSTEM USING AN OSCILLATING WATER COLUMN ATTACHED TO THE COLUMNS OF AN OFFSHORE PLATFORM
An offshore platform includes a support structure for supporting a workstation in a body of water at an offshore location. The support structure has a mounting formation and at least one duct is... |
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US20150226224 |
VENTILATION UNIT
A ventilation unit includes an axial fan having an axis of rotation; an electric motor for driving the axial fan and comprising a casing, a cap coupled to the casing to form a sealed enclosure and... |
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US20140154064 |
THRUST REVERSER DEVICE
A thrust reverser device of a nacelle includes a thrust reversal cowl which moves alternately from a closed position to an open position in which the thrust reversal cowl opens a path within the... |
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US20140056701 |
FAN SHROUD WITH COMPLEMENTARY TWO-SIDED RIBBING
A fan shroud has a panel including a first surface and a second surface substantially opposite the first surface. A first rib extends substantially perpendicularly from the first surface, and the... |
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US20130333350 |
AIRFOIL INCLUDING ADHESIVELY BONDED SHROUD
An airfoil includes an airfoil body that extends between a leading edge and a trailing edge, a suction side and a pressure side, and a first end and a second end. At least one fitting is located... |
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US20160356180 |
NACELLE INLET HAVING AN ANGLE OR CURVED AFT BULKHEAD
A construction of a nacelle inlet aft bulkhead has a curved or angled cross-section configuration between a connection of an outer edge of the aft bulkhead to an outer barrel of the nacelle inlet... |
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US20120099976 |
FAN CONTAINMENT SYSTEMS WITH IMPROVED IMPACT STRUCTURES
Methods and apparatus are provided for a fan containment system for a gas turbine engine having a plurality of fan blades includes a cylindrical casing with an inner surface surrounding the... |
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US20100247301 |
Power converting device
A power converting device includes a main body having a heat producing part housed therein, a fan case having a cooling fan therein for cooling the heat producing part provided in the main body,... |
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US20110268565 |
Tunnel turbine system generates potential energy from dorment kinetic energy
A generator system includes a pipe line which includes a control valve for diverting input gas or liquid into a pair of bypass pipe lines, whose output is coupled with two nozzle venture inlets in... |
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US20090226309 |
ENHANCED AXIAL AIR MOVER SYSTEM WITH ALIGNMENT
Implementations of an enhanced axial air mover system address various issues such as drying performance, transportability, storage, use, and assembly. Some implementations include ergonomic... |
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US20140314553 |
Method for Manufacturing a Plastic Housing and Plastic Housing
In a method for manufacturing a plastic housing, in particular a compressor housing, by joining at least two contact surfaces of at least two plastic components, the contact surfaces are joined... |
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US20130224002 |
COVER HUB WITH SEALING RING
A cover hub for a torque converter includes a radial wall arranged for axial alignment with a cover of the torque converter, a first circumferential surface including an opening for receiving a... |
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US20160101871 |
ASSISTANCE DEVICE FOR OPERATING A COWL AND A NACELLE FOR TURBOJET ENGINE EQUIPPED THEREWITH
An assistance device is provided to maneuver of a cover of a nacelle of a turbojet engine. The assistance device includes a joint collinear with an existing joint or hinge for a fitting of the... |
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US20120256424 |
CONTROLLED, DIFFUSED, AND AUGMENTED WIND ENERGY GENERATION APPARATUS AND SYSTEM
An apparatus and system for increasing power output for wind energy generation through a diffusing mechanism. An apparatus and system for mixing the wake and external flow, thereby permitting... |
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US20120251305 |
IMPACTOR CONTAINMENT
A containment system 20 is described, e.g. for a gas turbine engine. The system 20 includes a containment casing 22 and may also include a face sheet 30 and a backing layer 32. The casing 22... |
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US20160032747 |
SEALING ELEMENT FOR SEALING GAP
A sealing element for sealing a gap between two components, which can thermally move relative to each other and each have two substantially parallel component grooves, wherein the sealing element... |
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US20150330254 |
Compact Nacelle With Contoured Fan Nozzle
A gas turbine engine including a fan, compressor, combustor and a turbine arranged in series and surrounded by a nacelle. An engine core cowl is disposed within the nacelle. Each of these elements... |
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US20110286131 |
DIRECTING WINDAGE ESTABLISHED BY A ROTATING DISC
An apparatus and associated method for directing windage involves a body defining an aperture. A fastener is operably disposed in the aperture and is selectively engageable with a fixed support... |
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US20100050649 |
COMBUSTOR DEVICE AND TRANSITION DUCT ASSEMBLY
A combustor device and transition duct assembly is provided for use in a gas turbine engine. The combustor device comprises combustor structure having an exit portion; spring clips mounted to the... |