Abstract: An aircraft turbine engine including a gas generator, a fan, and an electrical machine, the stator of the electrical machine being connected to a power electronic circuit by at least one electrically conductive bar which extends substantially radially relative to the axis inside an IGV which forms part of a bladed angular segment, the bar being configured to be disassembled and removed from the turbine engine by disassembling and removing the segment.

Abstract: A partially luminous fan blade and fan containing same. The fan blade includes a light guide bracket, an annular sleeve, and a plurality of blades. The light guide bracket is formed with a shaft connection portion. The annular sleeve is integrated with the blades. The annular sleeve and the light guide bracket together form a hub portion of the fan blade. The annular sleeve is connected to the light guide bracket. The annular sleeve is provided with a light-shielding skirt. A bottom edge of the light-shielding skirt is lower than that of the light guide bracket.

Abstract: The motor-integrated fan has a suction port and a blowing port, and includes a rotating part rotatably supported on a shaft part; and a peripheral drive motor that rotates the rotating part by applying motive power from a duct provided on an outer peripheral side of the shaft part. The motor includes: a permanent magnet on a rotation support ring connected to the outer peripheral side of a blade of the rotating part; and a coil facing the permanent magnet in the axial direction of a rotational axis. In a cross-section taken on a plane orthogonal to the circumferential direction of the rotational axis, the center of gravity of a free end side portion including at least one of the rotation support ring and the permanent magnet is positioned closer to the suction port in the axial direction than the center of gravity of the thrust applied to the blade.

Abstract: Disclosed is an electrically conductive rigid bar (80) for electrically connecting an electric machine (70) of an aircraft turbine engine, characterised in that it comprises: —an elongate body (80a) made from electrically conductive material having a polygonal cross-section greater than or equal to 50 mm2, and— an electrical insulation sheath (80b) that surrounds the body, at least one of the longitudinal ends (84a) of the body not being covered by the sheath and comprising a through-hole (86) in which a bolt (88) for fastening and electrically connecting this end is mounted.

Abstract: A method for connecting a blade to a hub of a wind turbine, the method including pulling the blade towards the hub using a rope guided through an interior of the hub is provided. Thus, movements between the hub and the blade, in particular due to oscillations or waves, are reduced during the connection process.

Abstract: A motor-integrated fan sucks air from a suction port and blows out the sucked air from a blow-out port. The motor-integrated fan includes a shaft part that is provided at a center of a rotational axis; a rotation part that is rotated about the shaft part; an outer peripheral part that is provided on an outer periphery of the shaft part; a motor that rotates the rotation part; a heat generating part that generates heat due to an operation of the motor; and a cooling unit that cools the heat generating part with cooling air. The cooling unit includes an air intake port that takes the cooling air in, an air discharge port that discharges the cooling air, and a cooling flow channel that leads to the air discharge port from the air intake port via the heat generating part.

Abstract: A fan unit includes a centrifugal fan, an air flow volume detector, and a main body casing housing the centrifugal fan and the air flow volume detector. The centrifugal fan includes a fan casing and a rotor. The air flow volume detector includes main body, and a probe that detects an air flow volume equivalent quantity equivalent to an air flow volume provided by the centrifugal fan. The fan casing includes a bell mouth defining an air inlet and having a convex surface. A distance from the probe to the surface of the bell mouth is larger than 0 and smaller than one third of a radius of the air inlet. A thermal air velocity sensor detects, as the air flow volume equivalent quantity, an air velocity of air flowing through the air inlet not connected to a duct by measuring an amount of heat dissipated from the probe.

Abstract: A gas turbine engine includes a fan drive turbine driving a fan rotor through a main gear reduction. A primary lubricant system supplies lubricant to the main gear reduction. An auxiliary oil pump supplies oil to the main gear reduction. An auxiliary pump epicyclic gear train drives the auxiliary pump when the fan rotor is rotating in either direction. The main gear reduction is separate from the auxiliary pump epicyclic gear train.

Abstract: A water transmission device and a washing machine including the same. The washing machine includes a water transmission device configured to discharge water in a washing tub, wherein the water transmission device includes a filter case which is disposed under the washing tub and accommodates a filter, and into which the water in the washing tub is introduced, a pump case connected to the filter case and accommodating an impeller configured to suction the water in the filter case and discharge, a motor configured to rotate the impeller, a suction hole through which a side portion of the pump case facing a center of the impeller and a side portion of the filter case, and an outlet which is open downward from a lowest end inside the pump case and communicates with a water discharge pipeline.

Abstract: Provided is a wind power installation for converting the kinetic energy of the wind into the mechanical energy of rotation of a rotor for subsequent conversion of the mechanical energy of rotation into the electrical energy. A wind power installation includes a support frame, a shaft disposed on the support frame, and a blade system mounted on the shaft. The shaft is configured to rotate about a vertical axis and is functionally connected to an electric generator. The support frame is configured to be mounted between at least three radially arranged structures. The wind power installation can include additional blade systems disposed one above another on the shaft. Mounting the support frame between three radially arranged structures results in greater rigidity and robustness of the wind power installation, thus enabling the use of blade systems having a larger blade area and the arrangement of several blade systems on the shaft.

Abstract: A therapy seat cushion, method of making the cushion and method of using the cushion. The cushion has a planar array of at least two sets of alternatively inflatable and deflatable cells controlled by an inflation control system, and at least one non-inflatable offloading cushioning cell interspersed amongst the inflatable cells. The non-inflatable offloading cushioning cell configured and arranged to align with a pressure sore or an area prone to development of a pressure sore on an individual.

Abstract: An air moving device according to the present disclosure can include a housing and an installation hub. The housing can be connected to the installation hub via one or more adjustable supports. An impeller can be installed at least partially in the housing and configured to direct air out of the housing. In some embodiments, the adjustable supports can be adjusted to move the housing with respect to the installation hub. For example, the adjustable supports can be configured to modify the tilt of the housing and/or the overall distance between the housing and the installation hub. The installation hub can be installed on a ceiling, wall, or other mounting surface. Adjustment of the adjustable supports can permit vertical alignment of the air moving device housing, even when the installation hub is mounted to a slanted or sloped (e.g., non-horizontal) ceiling or wall.

Abstract: An illumination fan includes a first frame, a second frame, a fan blade, a light guide and a light source. The first frame includes an accommodation space. The second frame is assembled with the first frame, and an inner surface of the second frame is substantially flat. The fan blade is rotatably disposed in the accommodation space. The light source is disposed on either the first frame or the second frame. The light guide is disposed on the first frame and surrounds the fan blade.

Abstract: The present disclosure relations to wind mitigation devices which include a deflector that having an inlet and an outlet. An axial fan is disposed above the outlet of the deflector and includes a shroud. The shroud of the axial fan and the outlet of the deflector are aligned along a common vertical axis. The deflector is adapted to receive an airflow at the inlet and direct the airflow through the outlet in a vertical direction toward the axial fan.

Abstract: The disclosure provides a luminous fan including a main body, a light guide member and at least one light source. The main body includes a fan frame and a propeller, and the propeller is rotatably mounted on the fan frame. The light guide member includes an outer light guide ring and an inner light guide ring, the outer light guide ring and the inner light guide ring are mounted on the fan frame, the inner light guide ring has an air channel, the propeller is located in the air channel, and the outer light guide ring surrounds the inner light guide ring and is exposed from the luminous fan. The at least one light source is disposed between the outer light guide ring and the inner light guide ring.

Abstract: Embodiments of the invention provide an illumination grille assembly comprising a frame and a ventilation grille coupled to the frame, and a plurality of light-emitting diodes coupled with the frame and at least partially covered with a light transparent cover. Some embodiments of the invention provide a lighting and ventilating system including a main housing including an inlet through which air can be received within the main housing and an outlet through which the air can exit the main housing. A blower assembly can be supported in the main housing and it can be operable to generate a flow of air. In some embodiments, an illumination grille assembly can be coupled to the main housing to allow fluid to flow through the illumination grill assembly to the main housing. In some embodiments, the set of illumination devices can be configured and arranged to emit light through the light transparent cover.

Abstract: A system for modifying a location of a water impingement limit on an airfoil of an aircraft includes a flight control computer configured to receive data representative of environmental parameters in an environment of a flight path of an aircraft, determine, based on the environmental parameters, an existence of icing conditions to which the aircraft is currently subjected or is predicted to be subjected, and generate, based on the existence of icing conditions, a command signal for actuating a movable surface of the aircraft. The system further includes a surface actuator configured to receive the command signal from the flight control computer and adjust the movable surface in a manner causing an increase in an angle of attack of the airfoil to thereby modify a water impingement limit on the airfoil.

Abstract: According to one embodiment, a noise reduction apparatus includes a speaker, a generator and a controller. The speaker outputs control sound. The generator generates self-excited sound. The controller controls a phase and an amplitude of the control sound to reduce noise generated from a noise source, based on the control sound and the self-excited sound that is synchronized with the control sound.

Abstract: The invention relates to a guide vane system for a turbomachine with at least one guide vane, which can be rotatably mounted around an adjustment axis and is arranged with a radially inner end region in a corresponding recess of an inner ring, wherein the arrangement of the guide vane on the inner ring is secured by a securing element in a form-fitting manner. For an especially advantageous securing of this arrangement, it is provided that the securing element is designed as an oblong element, which is arranged at least in a recess and/or through-opening of the radially inner end region of the guide vane directed in the peripheral direction of the turbomachine and is arranged at least in a recess and/or through-opening of the inner ring directed in the peripheral direction of the turbomachine. In addition, the invention relates to a turbomachine, in particular an aircraft engine, and to a method for assembling a guide vane system.

Abstract: A pump for transferring molten metal includes an intake tube, a motor, a rotor positioned at least partially within the bottom end of the intake tube, a rotor shaft positioned at least partially in the intake tube, the rotor shaft having a first end attached to the motor and a second end attached to the rotor. An overflow conduit is attached to the intake tube. The pump does not include a pump housing and preferably does not include a superstructure, so it is relatively small, light and portable. In use, the motor drives the rotor shaft and rotor to generate a flow of molten metal upward into the intake tube and into the overflow conduit where it is discharged.

Abstract: A method of removing a wind turbine component includes assembling a transport system having a track, one or more support frames, and a carriage movably coupled to the track, the transport system having a first end positioned inside the tower and a second end positioned outside of the tower such that the track extends through an opening in the tower; raising the wind turbine component off of a platform located within the tower and above the door; moving at least part of the platform to allow the component to pass; lowering the wind turbine component onto the carriage; moving the carriage along the track from inside the tower to outside the tower; and removing the wind turbine component from the carriage. A transport system having a track, one or more support frames, and a carriage is also disclosed.

Abstract: Mattress assemblies are provided that make use of air bladders to provide a level of climate control to the mattress assemblies. The mattress assemblies include a body supporting portion having a first surface and a second surface opposite the first surface, an air bladder positioned adjacent to the second surface of the body supporting portion, a frame portion including a bottom surface and a border defining a well for receiving the air bladder, and an air pump that is operably connected to a climate control system for delivering heated or cooled air into the air bladder. A method of controlling the temperature of a mattress assembly is also provided.

Abstract: An air moving device includes a housing member, a rotary fan assembly, and a nozzle. The air moving device further includes a light source member mounted within the nozzle. The light source member can be placed within a flow of air moving out the end of the nozzle in a generally columnar pattern. The flow of air can be used to cool the light source member. A portion of the nozzle can be transparent, allowing the light from the light source member to emanate radially, as well as longitudinally.

Abstract: A table includes a table top, a support pedestal having a plenum, the support pedestal arranged to support the table top, and a fan arranged to blow air upwardly toward the table top through the plenum. An air deflector may be arranged to deflect the air radially outwardly under the table top in a 360° pattern. A heating element, cooling element, and/or a volatile active delivery system may be included to heat and/or cool the air and/or deliver a volatile active into the air. An ice bucket may be removably received within a bucket holder arranged in a recess in or through the table top.

Abstract: A pump for pumping molten metal includes a refractory base that can be submerged in a bath of molten metal. A refractory shaft sleeve has upper and lower end portions. The base includes an impeller chamber and includes at least one inlet opening and outlet opening. The pump includes a motor. A refractory shaft extends in the shaft sleeve and is connected to a motor. A refractory impeller is connected to the shaft and is rotatable in the impeller chamber. A gas source flows inert gas into the shaft sleeve under pressure. In one aspect the shaft sleeve can be spaced from the base so as to leave a gap between the shaft sleeve and the base. A regulator regulates at least one of flow rate and pressure of the gas so as to avoid cavitation of the pump while the gas is released from the shaft sleeve. Also featured is a method of operating the pump so as to reduce dross formation in the molten metal.

Abstract: The invention pertains to a method for removing ice layers and/or snow layers and/or dirt layers from the rotor blades of axial fans in cooling installations for refrigerating and/or freezing products. At least one cleaning substance jet is directed toward the rotor blades of an axial fan within certain time intervals in such a way that ice layers and/or snow layers and/or dirt layers are at least separated from the surfaces of the rotor blades and transported away, wherein the rotor blades rotate with nominal speed while cleaning jets act upon their surfaces.

Abstract: A charged particle emission and air-blowing device includes a communication port biased toward an end portion in a predetermined direction with respect to an air outlet, and a width expander configured to widen a flow path between an air directing plate of the end portion and a second blowing duct wider than a periphery. Emitted light from a light guide plate is reflected by the air directing plate in the delivery direction of an air flow. An air flow passes from a downward direction to an upward direction along a circuit board in an auxiliary suction path, and an opening portion faces the upper portion of the circuit board.

Abstract: An engine blower includes: an engine; a fan that is rotated by the engine; a volute case that houses the fan therein and includes an air intake port; and a sponge cover with which an exterior of the air intake port of the volute case is covered.

Abstract: An example method of reducing loads on a connection shaft includes disengaging a connection shaft from a motor-generator such that the connection shaft is not rotatably coupled to the motor-generator. The method communicates a fluid away from the motor-generator through a communication path established within the connection shaft. An example turbomachine connection shaft is configured to selectively rotatably couple a turbomachine rotor and a motor-generator. The connection shaft establishes a communication path that selectively vents the motor-generator.

Abstract: The present application thus provides a cleaning system for use with a compressor of a turbine engine. The cleaning system may include a wash nozzle positioned about the compressor and a spheroid injection port to inject a number of spheroids therein.

Abstract: An inlet port 4 and an outlet port 5 which are open in a body housing 2, an air-blowing pathway 20 disposed inside the body housing 2, making the inlet port 4 and the outlet port 5 communicate with each other, and also having a plurality of divisional pathways 22 obtained by division with partition plates 21, an air-blowing fan 7 disposed upstream from the divisional pathways 22 inside the air-blowing pathway 20, a removable inner cover 10 covering the divisional pathways 22 and having an inner surface which forms a side wall of the air-blowing pathway 20, and a removable exterior cover 9 covering the inner cover 10 to form an outer surface of the body housing 2 are provided, and the inner cover 10 has marking portions 11 formed on an outer surface along the partition plates 21.

Abstract: An air disruption system for an enclosure includes an air delivery system, at least one plenum including an inlet fluidically connected to the air delivery system and at least one outlet, and a controller operatively connected to the air delivery system. The controller is configured and disposed to selectively cause one or more discrete amounts of air to pass into the at least one plenum and flow through the outlet creating a localized air disruption.

Abstract: One embodiment of the present disclosure is a unique gas turbine engine. Another embodiment of the present disclosure is a unique machine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and electrical systems.

Abstract: An electric machine is disclosed integrated to rotate with a shaft of a gas turbine engine. In one form the electric machine is integrated with a fan of the gas turbine engine. A rotor of the electric machine can be disposed at the end of the fan blades and the stator integrated into a flow path forming surface of the gas turbine engine. In one form the windings of the electric machine can change configuration permitting some windings to be placed in parallel with one or more other windings, and then connected together in series with remaining windings, if any. The voltage of the electric machine can change as a result of a change in configuration of the windings. A moveable member can also be used to alter a magnetic field produced from the electric machine when operated such that a voltage can be changed as a result of altering the magnetic field.

Abstract: A gas turbine inlet heat exchange coil assembly includes a gas turbine inlet housing formed to include an inlet and an outlet and a flow path therebetween. A plurality of adjacent coils are located in proximity to the inlet, and moveable between a closed operative position where the coils are aligned substantially in a plane so as to maximize resistance to flow along the flow path, and an open inoperative position where said coils are individually rotated substantially 90° such that the coils lie in individual, parallel planes so as to minimize resistance to flow along the flow path.

Abstract: A parallel redundant fan system includes at least first and second fans located adjacent each other. Each fan includes: (i) a fan housing defining a fan chamber in which an impeller is supported for rotation about an axis of rotation; (ii) a first chamber outlet in communication with the fan chamber and defined by an opening in a first wall of the fan housing; (iii) a second chamber outlet in communication with the fan chamber and defined by an opening in a second wall of the fan housing; and, (iii) first and second backflow prevention dampers respectively associated with the first and second chamber outlets. The first and second dampers respectively include first and second damper plates that selectively pivot from their closed positions toward their opened positions against the closing force of respective first and second counterweights in response to exhaust air flow pressure exerted thereon.

Abstract: The invention relates to a wind power station (1) for energy generation with an axial-flow, rotating, vortex-generating wind concentrator (2) pivot-mounted on a shaft (3), covered by a ring-shaped outer jacket (4) which on its outside features flow channels distributed over 360° and which is equipped concentrator blades (7) in a circular arrangement between the shaft (3) and the ring-shaped outer jacket (4). To create favourable conditions, it is proposed to include sawtooth-shaped, curved edge-vortex-generating guide profiles (5) producing a downstream vortex coil across the entire cross-section of the ring-shaped outer jacket (4).

Abstract: A wind turbine system having a street light having an upright support or post on which is mounted a canopy housing any suitable lighting gear, and a wind turbine mounted above the canopy and operable to generate electrical energy with which to power the light, the canopy being adapted to augment the flow of air through the wind turbine.

Abstract: A method of scheduling maintenance on mechanical equipment includes monitoring the mechanical equipment with a sensor and collecting diagnostic information provided by the sensor with a local controller associated with the mechanical equipment. The diagnostic information relates to an operational characteristic of the mechanical equipment. The method also includes generating an alarm with the local controller in response to the collected diagnostic information, transferring the alarm from the local controller to a remote monitoring system, assigning an alarm value to the alarm using one of the local controller and the remote monitoring system, referencing a maintenance schedule for the mechanical equipment to ascertain a scheduled maintenance timeframe, and one of generating a work order and not generating the work order for the mechanical equipment based on the alarm value and the scheduled maintenance timeframe.

Abstract: A direct-drive wind turbine comprises a tower with a nacelle having a direct-drive generator and a rotatable hub carrying turbine blades, wherein the direct-drive generator comprises an outer stator and an inner rotor and has a first side facing the turbine blades and a second side facing away from the turbine blades. A slip ring at the second side transfers power and/or signals from the nacelle to the rotatable hub being mounted coaxially with the centerline of the direct-drive generator. The slip ring mounts on a first arm. An end of a second arm distal to the slip ring can engages the rotor or a shaft. The assembly of the first arm, slip ring and second arm may be at a first position where the slip ring is aligned with the centerline of the direct drive generator and at a second position to provide access to the hub.

Abstract: The present invention relates to a connecting tube (2) for hermetic compressors, which is responsible for connecting the housing (1) of a hermetic compressor to the tube (3)—which may be the process valve tube or evaporation, condensation system—which comprises at least two portions composed of materials that are different from each other, which are associated by means of a suitable joining process—preferably welding, soldering or mechanical fastening. In the preferred embodiment of the invention, the connecting tube (2) comprises a first portion (5) comprising a first material and a second portion (6) composed of a second material, wherein the second portion (6) of the connecting tube (2) can join the first portion of the connecting tube (5) and the system tube (3).

Abstract: Example embodiments are directed to fluid turbines that include a turbine shroud and a rotor assembly disposed within the turbine shroud. The rotor assembly includes a nacelle pivotally engageable with a tower structure and a slip ring disposed within the nacelle. The slip ring electrically connects one or more cables in the nacelle to one or more cables in the tower structure. The slip ring is engaged with the nacelle by a mounting apparatus which allows movement of the slip ring along at least one of an x-axis, a y-axis and a z-axis. Example embodiments are further directed to methods of maintaining untwisted electric cables in a fluid turbine.

Abstract: A ceiling fan system that includes a motor/blade assembly that may include a motor, a main rotor attached to the motor, and a plurality of blades attached to the main rotor. A plurality of hoods may partially enclose the motor/blade assembly. The plurality of hoods may include an intake nozzle hood acting as an air inlet and an outlet surface hood with an aerodynamic surface. The profile of the hoods is designed so that the resulting flow from the blades produces a flow pattern controlled by the aerodynamic shape of the hoods.

Abstract: A wire arrangement mechanism including a guiding slot and an arranging slot is formed on a fan frame. The guiding slot includes a bottom wall and two holding walls extending therefrom. The arranging slot is defined by an outer frame and a confining portion connected thereto. The arranging slot is staggered from and communicated with the guiding slot.

Abstract: A ventilator includes a body casing having an opening formed in its lower portion and an exhaust port formed on one side; a fan that is provided in the body casing, for sucking indoor air from the opening and exhausting the indoor air from the exhaust port; a resin fan casing that has a suction port and forms an air passage of the fan; a protection frame formed outside the air passage to cover a terminal block provided outside the air passage; a resin terminal block cover that watertightly seals a protection frame opening of a lower portion of the protection frame and is opened and closed; a sheet-metal case that is provided in the protection frame and stores the terminal block; and a sheet-metal terminal block cover that opens and closes a lower opening of the sheet-metal case.

Abstract: The Wind Wing Electric Generator is a apparatus for inexpensively converting oscillating rotating mechanical energy into electrical energy.

Abstract: A carbon seal assembly comprises an annular member adapted to be secured to a structure. An annular seal runner is sealingly mounted to a shaft to rotate therewith, with the seal runner being made of a material complementary to that of the annular member for magnetic attraction therebetween. An annular carbon seal element is mounted to the annular seal runner to rotate therewith and positioned in a gap between the annular member and the annular seal runner, the annular carbon seal element having an annular wear surface abutting against a face of the annular member. A cross-sectional area of the annular carbon seal element increases as the axial dimension of the annular seal runner decreases for at least a part of the seal.

Abstract: The present application provides a modular enclosure for use with an equipment platform and a turbo-machine. The modular enclosure may include a first number of walls attached to a number of legs of the equipment platform and a second number of walls attached to the legs of the equipment platform. The first number of walls may include a number of pivotable panels. The second number of walls may include an access aperture therein. The equipment platform may provide a roof for the modular enclosure.

Abstract: The present application thus provides a compressor wash system for use about a bellmouth of a compressor of a gas turbine engine. The compressor wash system may include a bellmouth wash nozzle positioned about the bellmouth of the compressor and a wash door assembly positioned about a lower half of the bellmouth such that the wash door assembly may be closed when the bellmouth wash nozzle is activated.

Abstract: The present invention provides a turbocharger including a compressor housing provided therein with an air flow path in which an impeller is disposed and a bearing housing. The air flow path includes a suction port and a discharge scroll chamber. The compressor housing includes a shroud surface and a diffuser surface. The bearing housing includes a facing surface which is facing to the diffuser surface. A cleaning agent supplying units are provided in the diffuser surface and the facing surface. The cleaning agent supplying units include porous supplying portions for forming at least a portion of the diffuser surface or the facing surface, and a cleaning agent for preventing adhesion of deposits is supplied from the porous supplying portions to the diffuser surface or the facing surface.