24th week of 2011 patent applcation highlights part 42 |
Patent application number | Title | Published |
20110142616 | NACELLE FOR WIND TURBINE - A nacelle for a wind turbine comprises a plurality of walls connected with each other to define an internal space of the nacelle. A support beam is disposed at an inner surface of the connecting area of at least one set of contiguous walls of the plurality of walls, and a portion of the support beam contacting the contiguous walls has a shape mating with that of the inner surface of the connecting area. The nacelle for a wind turbine is simple in structure, convenient to transport, easy to assemble and strong in the mechanical connecting strength. | 2011-06-16 |
20110142617 | GEAR SET, WIND TURBINE INCORPORATING SUCH A GEAR SET AND METHOD OF SERVICING A WIND TURBINE - A gear set is disclosed. The gear set includes a bearing including an inner race and an outer race, one of the inner race and the outer race being a ring gear including a plurality of first teeth having a first hardness; and a pinion meshable with the ring gear, and including a plurality of second teeth having a second hardness. The second hardness is no greater than the first hardness. A wind turbine incorporating such a gear set and a method of servicing a wind turbine are also disclosed. | 2011-06-16 |
20110142618 | WIND TURBINE PITCH ASSEMBLY ENCLOSURE SYSTEM - A system for enclosing a portion of a wind turbine with an enclosure system and a method of enclosing a wind turbine with the system are described. An inner seal plate is positioned in an inner interface area between a hub of the wind turbine a pitch assembly. An opening is formed in the inner seal plate and is covered with a first access cover when in a closed position. An outer seal plate is positioned in an outer interface area between a pitch assembly and a rotor blade. An opening is formed in the outer seal plate and is covered with a second access cover when in a closed position. The access covers restricts access to the respective openings formed in the seal plates when in the closed position. | 2011-06-16 |
20110142619 | Wind Turbine, Control System, And Method For Optimizing Wind Turbine Power Production - A wind turbine includes a generator and a control system. The control system is configured to determine whether a predefined amount of turbulence will be induced to the wind turbine by a wake zone created by a wind turbine upstream thereof. The control system is also configured to adjust at least one constraint of the wind turbine to a first setting if the amount of turbulence is greater than the predefined amount, the constraint affecting power produced by the generator, and to adjust the constraint of the wind turbine to a second setting if the amount of turbulence is not greater than the predefined amount. | 2011-06-16 |
20110142620 | APPARATUS AND METHOD FOR OPERATION OF A WIND TURBINE - A method for operating a wind turbine is provided. The wind turbine includes a rotor including at least one rotor blade and a pitch drive system coupled to the at least one rotor blade. The pitch drive system is adapted for pitching the rotor blade. The method includes: determining an actual value of a first variable indicative of an overspeed state of the wind turbine; determining an actual value of a second variable of the wind turbine correlated to the rate of change over time of the first variable; and, estimating an occurrence of an overspeed state of the wind turbine from at least the determined actual values of the first and second variables. The pitch drive system pitches the rotor blade for aerodynamically braking the rotor based on the result of the estimation. | 2011-06-16 |
20110142621 | Method and System For Monitoring Wind Turbine - A monitoring system for a wind turbine includes at least one acoustic sensor configured to measure an acoustic emission generated by at least one component of the wind turbine, and a control system configured to calculate at least one wear characteristic of the component based on the measured acoustic emission. The wear characteristic includes at least one of a current amount of wear on the component, a rate of wear on the component, and a predicted amount of wear on the component. | 2011-06-16 |
20110142622 | WIND TURBINE AND METHOD FOR CONTROLLING A WIND TURBINE - The disclosure relates to a method for controlling a wind turbine including a wind rotor shaft, a rotary encoder for measuring the azimuth angle of the wind rotor shaft, wherein the wind turbine further includes at least one impulse generating device including at least one first part and at least one second part, wherein the at least one first part is rotating with the wind rotor shaft and the least one second part is disposed stationary with respect to the wind rotor shaft such that the at least one first part moves by the at least one second part; wherein the method includes: encoding the azimuth angle of the wind rotor shaft by the rotary encoder into a rotation value; generating an impulse when one of the at least one first part moves by one of the at least one second part of the impulse generating device; comparing the rotation value at the time of a detected impulse with a reference value. | 2011-06-16 |
20110142623 | SYSTEM AND METHOD OF DISTRIBUTING AIR WITHIN A WIND TURBINE - An air distribution system for use with a wind turbine. The wind turbine includes a nacelle that is coupled to a tower and a rotor that is rotatably coupled to the nacelle with a rotor shaft. The rotor includes at least one rotor blade that is coupled to a hub. The air distribution system includes a conduit that is defined within the rotor shaft. The conduit provides flow communication between the nacelle and the rotor. An air-flow control assembly is coupled in flow communication with the conduit. The air-flow control assembly is configured to selectively channel air from the nacelle to the rotor and from the nacelle to ambient air. | 2011-06-16 |
20110142624 | Active Control Of A Wind Turbine Blade - A method and system for increasing power production of a wind turbine including a rotor, at least one rotor blade coupled to the rotor, at least one sensor, and a controller communicatively coupled to the sensor. A flow parameter of the rotor blade is detected, and operation of the wind turbine is controlled to reduce a flow separation at the rotor blade based at least partially on the flow parameter of the rotor blade. | 2011-06-16 |
20110142625 | WATER TURBINE - A turbine for use in extracting energy from within a water flow comprises: an array of turbine blades formed and arranged for rotation, in use, about an axis substantially normal to the direction of water flow; wherein at least one turbine blade of the array is formed to be adjustable, in use, from a first, driving, configuration when moving with the direction of water flow, to a second, return, configuration when moving against the direction of water flow, and wherein the surface area of the turbine blade presented to the direction of water flow is reduced when in the return configuration. | 2011-06-16 |
20110142626 | SERVICEABLE YAW BRAKE DISC SEGMENTS WITHOUT NACELLE REMOVAL - A wind turbine yaw brake apparatus includes a circular rotation support base having an inner and an outer cylinder wall. The circular rotation support base is mounted to a top face of a wind turbine tower and a nacelle such that the nacelle can rotate relative to the wind turbine tower. A plurality of brake lining elements are removably mounted to the circular rotation support base. A disc brake unit acts upon the brake aligning elements. | 2011-06-16 |
20110142627 | TEETER MECHANISM FOR A MULTIPLE-BLADED WIND TURBINE - A teeter mechanism for a multiple-bladed wind turbine includes a rotor shaft operable to rotate about a first axis. A spherical member is rotatable about the first axis along with the rotor shaft. A plurality of turbine blades is mounted to a rotor hub. The rotor hub rotationally drives the rotor shaft, and is operable to teeter about the spherical member such that the rotor hub rotates about the first axis in a first position and rotates about a second axis offset from the first axis in a second, teeter position. | 2011-06-16 |
20110142628 | WIND TURBINE BLADES WITH CONTROLLABLE AERODYNAMIC VORTEX ELEMENTS - A wind turbine blade has a suction side surface and a pressure side surface. A plurality of dynamic vortex elements are formed on at least one of the suction side or the pressure side surfaces. The vortex elements are activatable between a first retracted position that is inwardly recessed relative to a neutral plane of the surface on which they are formed and a second extended position that is outwardly protruding relative to the neutral plane of the surface. | 2011-06-16 |
20110142629 | WIND TURBINE ROTOR BLADE WITH POROUS WINDOW AND CONTROLLABLE COVER MEMBER - A wind turbine blade includes a porous window defined in the suction side of the blade. The porous window is permeable to airflow from within an internal cavity of the blade through the suction side. A deployable cover member is configured with the porous window and is variably positionable from a fully closed position wherein airflow through the porous window is blocked, to a fully open position wherein airflow is established through an entirety of the porous window. An actuating mechanism is disposed within the internal cavity of the blade and is configured with the cover member to move the cover member between the fully closed and fully open positions in response to a control signal. | 2011-06-16 |
20110142630 | WIND TURBINE PITCH-ANGLE CONTROL DEVICE AND METHOD THEREOF - The object is to reduce aerodynamic load when a wind turbine is halted. When a wind turbine halt command is input, pitch angles of wind turbine blades | 2011-06-16 |
20110142631 | WIND TURBINE GENERATOR - Provided is a wind turbine generator including an electric pitch-control device that efficiently utilizes the entire circumferential teeth of a ring gear of a wind turbine blade so as to eliminate the need for work at high elevation using a crane or the like even when the teeth of the ring gear are partly broken. A wind turbine generator having an electric pitch-control device that performs pitch-angle control by using a motor to drive a pinion gear that meshes with a ring gear of a wind turbine blade includes a plurality of pinion-driving-mechanism securing supporters or a fixing/releasing switching part as a meshing-region changing mechanism that changes a pitch-angle-control meshing region of the ring gear that meshes with the pinion gear during the pitch-angle control. | 2011-06-16 |
20110142632 | Piecewise Variable Displacement power transmission - In one embodiment, a hydraulic circuit has an input shaft, at least one positive displacement hydraulic pump, a plurality of positive displacement hydraulic motors, and at least one fluid line operatively connecting the at least one positive displacement hydraulic pump to the positive displacement hydraulic motors. In operation, the at least one positive displacement hydraulic pump is placed in an operative condition. At least one of the positive displacement hydraulic motors is also placed in an operative condition. A flow rate of fluid in the fluid line is measured, and the remaining positive displacement hydraulic motors are switched between an operative condition and a bypass condition according to the measured flow rate of the fluid. | 2011-06-16 |
20110142633 | SYSTEMS AND METHODS FOR ASSEMBLING AN AIR DISTRIBUTION SYSTEM FOR USE IN A ROTOR BLADE OF A WIND TURBINE - A method of assembling an air distribution system for use in a rotor blade of a wind turbine. The rotor blade includes a sidewall at least partially defining a cavity extending from a blade root towards a blade tip. The method includes positioning at least a portion of a manifold within the cavity and coupling the manifold to the sidewall. The manifold extends from the blade root towards the blade tip and has a root end and an opposing tip end. A passage is defined from the root end to the tip end. A flow control device is coupled to the manifold root end and configured to channel air through the manifold. A bypass flow assembly is coupled to the manifold and configured to channel air through the air distribution system with the flow control device in a non-operating configuration. | 2011-06-16 |
20110142634 | OVERSPEED PROTECTION SYSTEM AND METHOD - An overspeed protection system for a wind turbine having a hub and at least one rotor blade mounted to the hub includes a rotation sensor adapted for measuring a rotor speed of said wind turbine; a comparator connected to the rotation sensor and adapted for comparing the measured rotor speed with a predetermined threshold value of the rotor speed wherein the comparator outputs a signal indicative of the comparison; and an auxiliary pitch drive controller connected to the comparator and adapted to receive the signal indicative of the comparison, the auxiliary pitch drive controller being further adapted for controlling a pitch drive unit of the wind turbine independently of a main turbine controller and, if the threshold value is exceeded, to adjust a pitch angle of the rotor blade of the wind turbine so that aerodynamic braking of the wind turbine is effected. | 2011-06-16 |
20110142635 | BLADE EXTENSION FOR ROTOR BLADE IN WIND TURBINE - A rotor blade assembly is disclosed. The rotor blade assembly includes a rotor blade and a blade extension. The rotor blade has a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade further has an aerodynamic profile. The blade extension is mounted to the rotor blade. The blade extension includes a cutaway mounting portion for mounting the blade extension to the rotor blade such that the blade extension is generally flush with at least one of the pressure side or the suction side of the rotor blade. The cutaway mounting portion defines a notch configured to locate the blade extension relative to the rotor blade. | 2011-06-16 |
20110142636 | EXPANSION ASSEMBLY FOR A ROTOR BLADE OF A WIND TURBINE - An expansion assembly for a rotor blade of a wind turbine is disclosed. The expansion assembly may generally include a spacer having a first end configured to be attached to a blade root of the rotor blade and a second end configured to be attached to a hub of the wind turbine. Additionally, the expansion assembly may comprise a wing defining a substantially aerodynamic profile and including a base portion configured on the spacer and an outboard portion extending from the spacer in a generally spanwise direction. The outboard portion of the wing may generally be configured to be disposed adjacent to at least one of a suction side and a pressure side of the rotor blade. | 2011-06-16 |
20110142637 | NOISE REDUCER FOR ROTOR BLADE IN WIND TURBINE - A rotor blade assembly for a wind turbine is disclosed. The rotor blade assembly includes a rotor blade having a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root, the rotor blade further defining a pitch axis. The rotor blade assembly further includes a noise reducer mounted to the rotor blade. The noise reducer includes a base plate defining a base line, a plurality of noise reduction features extending from the base line, and a plurality of apertures defined in the base plate. Each aperture is positioned on an opposite side of the base line from the plurality of noise reduction features such that the aperture is fully defined in the base plate. | 2011-06-16 |
20110142638 | WIND TURBINE ROTOR BLADE WITH ACTUATABLE AIRFOIL PASSAGES - A wind turbine rotor blade includes a pressure side and a suction side. At least one airfoil passage is defined through the blade between the pressure side and suction side. A respective cover is configured over the airfoil passage at each of the pressure and suction sides. The covers are actuatable between a closed position wherein the cover is flush with the respective pressure or suction side and an open position wherein the cover moves to open the airfoil passage. | 2011-06-16 |
20110142639 | MODULAR TURBINE AIRFOIL AND PLATFORM ASSEMBLY WITH INDEPENDENT ROOT TEETH - A turbine airfoil ( | 2011-06-16 |
20110142640 | CYLINDER DRIVING DEVICE - An object is to provide a cylinder driving device of a wind-power generation system capable of appropriately controlling a pitch angle of each rotor blade at a time of power failure with a simple configuration. The present invention achieves the object by including a piston connected to the rotor blade; a cylinder that moves the piston by a hydraulic pressure; an urging member that urges the piston in one direction; an accumulator that is connected to the cylinder, and supplies hydraulic oil urging the piston in an opposite direction to a direction where the piston is urged by the urging member to the cylinder; and an on/off valve that controls opening or closing of a channel between the accumulator and the cylinder. | 2011-06-16 |
20110142641 | Enclosed vertical axis fluid rotor - A enclosed vertical axis fluid rotor used as a wind turbine of two designs having multiple sails that are concave on the inside and convex on the outer side which allows omni-directional wind or other fluids to engage sails to create optimum fluid momentum. These are sectional segmentation of each rotor that can be stacked upon one another at locating lug points to be attached to each rotor to keep radial alignment precise during assembly. The preferred embodiment would be of composite materials or plastics that can be molded to a given design of three or more stages. The advantage of this turbine is using the fluids to their optimum efficiency. These designs have low starting speed, low precession, and low drag. One design has a central axis that turns with bearings with the rotor and the other design is a central static (non-turning) axis shaft that allows the turbine to turn on bearings. | 2011-06-16 |
20110142642 | WIND TURBINE ROTOR BLADE WITH AERODYNAMIC WINGLET - A wind turbine includes a plurality of rotor blades, with each blade having a root portion connected to a rotor hub and an airfoil portion extending radially outward from the rotor hub. The airfoil portion further includes a main foil section and a winglet pivotally connected to the main foil section so as to pivot from an in-line position wherein the rotor blade has a first sweep length to an articulated position wherein the rotor blade has a second sweep length. In the articulated position, the winglet may pivot to not more than 90 degrees relative to a longitudinal axis of the main foil section. A deployable sleeve may be connected to the winglet so as to extend between the winglet and the main foil section in the articulated position of the winglet. The sleeve is stowable within either or both of the main foil section or the winglet in the in-line position of the winglet. | 2011-06-16 |
20110142643 | LIGHTNING PROTECTION FOR WIND TURBINES - A rotor blade for a wind turbine is provided. The rotor blade includes a rotor blade body, at least one receptor adapted to be a location for lightning impact, and at least one down conductor connected to the receptor and located within the rotor blade body. The down conductor includes a first conductor connected to the receptor and a ground connection of the wind turbine, and a second insulated conductor connected to the receptor and a non-grounded location of the wind turbine. A path is formed from the ground connection of the first conductor to the non-grounded location of the second insulated conductor. This path facilitates a continuity test used to evaluate a condition of the lightning protection system. | 2011-06-16 |
20110142644 | WIND TURBINE ROTOR BLADES WITH ENHANCED LIGHTNING PROTECTION SYSTEM - A wind turbine rotor blade includes a plurality of lightning receptors configured along either or both of the pressure side or suction side of the blade. At least one looped lightning conductive circuit is provided, with the lightning receptors configured in communication with a respective lightning conductive circuit. The lightning conductive circuit has terminal ends that extend through the root for connection of each terminal end with a grounding system within the wind turbine. The looped lightning conductive circuit provides a redundant path to each lightning receptor for conducting a lightning strike to ground. | 2011-06-16 |
20110142645 | WIND TURBINE BLADE BEARING AND WIND TURBINE THAT MAKES USE THEREOF - It discloses a wind turbine blade bearing that makes it possible to avoid the collision of the blade with the wind turbine tower by providing a separation thereof via the disposal of the blades at an angle with respect to the wind turbine hub; where said angle is given by the bearing of the blade pitch change system. | 2011-06-16 |
20110142646 | PASSIVE CYCLIC PITCH CONTROL - A blade pitch control mechanism for a propeller assembly ( | 2011-06-16 |
20110142647 | ADJUSTING DEVICE FOR ADJUSTING THE ROTATION ANGLE POSITION OF THE ROTOR OF A WIND ENERGY SYSTEM - An adjusting device for adjusting the rotation angle position of the rotor of a wind energy system should be improved by the invention, whereby a complicated processing of the brake disc previously used for engagement of the drive is no longer necessary, and whereby said brake disc can be flexibly arranged in an area with sufficient construction space. For this purpose, the adjusting device has at least one force transducer wheel and/or a force transducing disc which is mounted or can be mounted on a shaft ( | 2011-06-16 |
20110142648 | ENGINE ARRANGEMENT - An engine arrangement has a gear assembly that drives a first propeller assembly. The gear assembly is driven by a power drive shaft that joins to the gear assembly at a first side. The engine arrangement has a static conduit that extends along a longitudinal internal cavity of the power drive shaft. The conduit penetrates the gear assembly such that a portion of the conduit projects from an opposing second side of the gear assembly. The engine arrangement has one or more first fluid supply lines routed along the static conduit between a hydraulic pressure power source and the first hydraulic actuator. A first hydraulic rotating coupling is mounted to the projecting portion of the static conduit. The first fluid supply lines fluidly communicate with the first hydraulic actuator via the first rotating coupling. | 2011-06-16 |
20110142649 | COMPACT GEARED DRIVE TRAIN - A drive train for a wind turbine is provided. The wind turbine includes a rotor hub and one or more blades. The drive train includes a first stage carrier connected to the rotor hub. The first stage carrier includes one or more first stage planet gears that interact with a fixed first stage ring gear and a rotating first stage sun gear. A second stage planet carrier includes one or more second stage planet gears. The second stage planet carrier is rigidly connected to the first stage sun gear. The second stage planet gears interact with a rotating second stage ring gear and a non-rotating second stage sun gear. A generator includes a generator rotor and a generator stator, and the generator rotor is fixedly connected to the second stage ring gear so that both the generator rotor and the second stage ring gear rotate together. | 2011-06-16 |
20110142650 | Turbine Blade Damping Device with Controlled Loading - A damping structure for a turbomachine rotor. The damping structure includes an elongated snubber element including a first snubber end rigidly attached to a first blade and extending toward an adjacent second blade, and an opposite second snubber end defining a first engagement surface positioned adjacent to a second engagement surface associated with the second blade. The snubber element has a centerline extending radially inwardly in a direction from the first blade toward the second blade along at least a portion of the snubber element between the first and second snubber ends. Rotational movement of the rotor effects relative movement between the first engagement surface and the second engagement surface to position the first engagement surface in frictional engagement with the second engagement surface with a predetermined damping force determined by a centrifugal force on the snubber element. | 2011-06-16 |
20110142651 | Two-Part Shroud or Shroud Section for a Stator Stage with Vanes of an Axial Compressor - A shroud or shroud section for a stator stage with vanes of an axial compressor is made of composite material and is built in two parts, each having a series of notches corresponding to a half of the profile of the vanes, so as to form apertures that follow the shape of the vanes when the two parts are assembled. The two parts also include mutual fastening members or means adapted to ensure their assembly. | 2011-06-16 |
20110142652 | ROTATING BLADE SYSTEM FOR A ROW OF ROTATING BLADES OF A TURBOMACHINE - The invention concerns a moving blade system for a moving blade sequence of a continuous-flow machine, in particular a thermal gas turbine with at least two moving blade segments, of which each moving blade segment encompasses at least two moving blades that are disposed, in reference to a rotation axis of the moving blade sequence, at least primarily radially between a radially interior and a radially exterior shroud band and are coupled to the shroud bands, wherein at least the radially exterior shroud bands of the two moving blade segments encompass contact surfaces that correspond to one another, wherein radial equilibrium axes of neighboring moving blades of the at least two moving blade segments are disposed in a tilted manner by respectively axially an angle (60 | 2011-06-16 |
20110142653 | TWO PIECE IMPELLER - A compressor impeller includes a hub and a plurality of blades. The hub is formed of first forged portion and a second forged portion that are bonded together. The first forged portion is comprised of a first alloy and the second forged portion is comprised of a second alloy that has lower fracture toughness than the first alloy. The blades are integral with and extend from the hub and are formed from the first forged portion. The hub is formed from both the first forged portion and the second forged portion. | 2011-06-16 |
20110142654 | Turbine Blade Damping Device With Controlled Loading - A damping structure for a turbomachine rotor. The damping structure including an elongated snubber element including a first snubber end rigidly attached to a first blade and extending toward an adjacent second blade, and an opposite second snubber end positioned adjacent to a cooperating surface associated with the second blade. The snubber element has a centerline extending radially inwardly in a direction from the first blade toward the second blade along at least a portion of the snubber element between the first and second snubber ends. Rotational movement of the rotor effects relative movement between the second snubber end and the cooperating surface to position the second snubber end in frictional engagement with the cooperating surface with a predetermined damping force determined by a centrifugal force on the snubber element. | 2011-06-16 |
20110142655 | Fan set for wind power generator - A fan set for a wind power generator is disclosed. The fan set has fan blades that are able to rotate between 0 and 90 degrees with respect to a fan hub, so that each of the fan blades has a concentrated position and an expanded position. | 2011-06-16 |
20110142656 | ROTOR BLADE DESIGN FOR A WELLS TURBINE - The invention relates to a Wells turbine, comprising
| 2011-06-16 |
20110142657 | WIND TURBINE BLADE ATTACHMENT CONFIGURATION WITH FLATTENED BOLTS - A wind turbine includes a plurality of turbine blades, with each of the blades having a root flange that attaches to a flange of a rotor hub by a plurality of circumferentially spaced blade bolts. The blade bolts have opposite cylindrical end sections engaged within the rotor hub flange and blade root flange, respectively, and a non-cylindrical shank extending between the cylindrical end sections. At least one flattened side is defined in the shank along a longitudinal axis of the bolt. | 2011-06-16 |
20110142658 | HUB FOR A WIND TURBINE AND METHOD OF MOUNTING A WIND TURBINE - A modular rotor blade hub for a wind turbine rotor includes a plurality of segments, wherein at least one segment includes at least one face abutting against at least one face of at least one adjacent segment, and wherein at least one of said faces extends from an outer periphery of the hub to a central region of the hub. Further, methods for mounting a wind turbine including a modular hub are provided. | 2011-06-16 |
20110142659 | VERTICAL AXIS WIND TURBINE WITH SELF-STARTING CAPABILITIES - A vertical axis wind turbine and vertical axis wind turbine assembly comprising a rotary body and a plurality of blades. A cross section through each blade of the plurality of blades transverse to the rotary axis comprises an inner camber line, an outer camber line, and a chord line. The outer camber line comprises a first portion, a transition portion and a second portion. The second portion is longer, in the lengthwise direction, than a combined length of the first portion and the transition portion. The average second portion thickness is less than half an average first portion thickness. A magnitude of an average rate of change in a transition portion thickness is at least twice a magnitude of an average rate of change in a first portion thickness, and a magnitude of an average rate of change in a second portion thickness. | 2011-06-16 |
20110142660 | WIND TURBINE BLADE WITH INTEGRATED HANDLING MECHANISM ATTACHMENT BORES - A wind turbine blade includes a leading edge, a trailing edge, a suction side, and a pressure side. At least one integrated attachment bore is configured in each of the suction side and pressure side between the leading edge and trailing edge. The attachment bores are structurally configured for receipt of a handling mechanism therein for supporting the blade during a transportation, installation, or maintenance procedure. | 2011-06-16 |
20110142661 | TRAILING EDGE BONDING CAP FOR WIND TURBINE ROTOR BLADES - A trailing edge bonding cap for use with a rotor blade of a wind turbine is disclosed. The trailing edge bonding cap may include a body projecting outwardly from a blade shell of the rotor blade. The body may have a first outer surface and a second outer surface. The first outer surface may intersect the second outer surface to define a trailing edge of the rotor blade. Additionally, the first and second outer surfaces may have a profile configured to correspond to an aerodynamic profile of the blade shell. | 2011-06-16 |
20110142662 | Spar Cap Assembly for a Wind Turbine Rotor Blade - A spar cap assembly for a rotor blade of a wind turbine is disclosed. In general, the spar cap assembly may include a tensile spar cap formed from a composite material and configured to engage an inner surface of the rotor blade. The tensile spar cap may generally have a first thickness and a first cross-sectional area. Additionally, the spar cap assembly may include a compressive spar cap formed from the same composite material and configured to engage an opposing inner surface of the rotor blade. The compressive spar cap may generally have a second thickness and a second cross-sectional area that is greater than the first cross-sectional area. Additionally, the composite material is generally selected so that at least one of a strength and a modulus of elasticity of the composite material differs depending on whether the material is in tension or in compression. | 2011-06-16 |
20110142663 | ASSEMBLY AND METHOD OF PREPARING AN ASSEMBLY - The invention relates to a method of preparing an assembly, comprising providing a first structure; providing a second structure; providing at least one flexible adhesive limiting member extending between said structures; and providing an adhesive between said structures to bind said structures to each other; wherein the adhesive is limited by the flexible adhesive limiting member such that a concave front line surface of the adhesive is defined. The invention also relates to such an assembly as well as to a wind turbine rotor blade, and to a wind turbine, comprising such an assembly. | 2011-06-16 |
20110142664 | VORTEX GENERATOR ASSEMBLY FOR USE WITH A WIND TURBINE ROTOR BLADE AND METHOD FOR ASSEMBLING A WIND TURBINE ROTOR BLADE - A method of manipulating a boundary layer across a wind turbine rotor blade. The method includes coupling at least one vortex generator to the rotor blade. The vortex generator includes at least one sidewall that extends outwardly a radial distance from an outer surface of the rotor blade. The vortex generator is selectively positionable between a first position and a second position. A control system calculates a condition of the boundary layer. The vortex generator is positioned at one of the first position and the second position based on the calculated condition of the boundary layer for moving the vortex generator between the first position and the second position. | 2011-06-16 |
20110142665 | NOISE REDUCER FOR ROTOR BLADE IN WIND TURBINE - A rotor blade assembly for a wind turbine is disclosed. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade assembly further includes a noise reducer configured on a surface of the rotor blade. The noise reducer includes a plurality of reinforcing members and a plurality of noise reduction features. Each of the plurality of reinforcing members extends outwardly with respect to the rotor blade. Each of the plurality of noise reduction features is connected to one of the plurality of reinforcing members and defines a width. Each of the plurality of reinforcing members causes the connected noise reduction feature to have a variable stiffness throughout at least a portion of the width of the connected noise reduction feature. | 2011-06-16 |
20110142666 | NOISE REDUCER FOR ROTOR BLADE IN WIND TURBINE - A rotor blade assembly for a wind turbine is disclosed. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade further includes a noise reducer configured on a surface of the rotor blade, the noise reducer comprising a plurality of serrations, each of the plurality of serrations defining a centerline. The centerline of each of the plurality of serrations defines a individual tailored angle dependent on at least one of span-wise location, local chord, width, length, bend angle, and thickness | 2011-06-16 |
20110142667 | WIND TURBINE ROTOR BLADE ASSEMBLY HAVING AN ACCESS WINDOW AND RELATED METHODS - A rotor blade assembly having an access window and methods for assembling a rotor blade are disclosed. The rotor blade assembly may generally include a first shell component and a second shell component. The first shell component may be secured to the second shell component. Additionally, an access region may be defined in the first shell component and/or the second shell component. The access region may generally be configured such that an access window is defined in the rotor blade assembly. The access window may be configured to provide access to the interior of a portion of the rotor blade assembly. | 2011-06-16 |
20110142668 | WIND TURBINE BLADE WITH IMPROVED TRAILING EDGE BOND - A wind turbine blade includes a leading edge and a trailing edge. The blade has an upper shell member and a lower shell member, with each of the shell members having a forward edge bonded at the leading edge of the blade and a rearward edge. A rigid bond cap is pre-formed into a designed size and shape of the trailing edge of the blade. The bond cap includes oppositely oriented leg members bonded to the respective rearward edges of the shell members so as to be essentially flush with the upper and lower shell members. The rigid bond cap defines at least a portion of the trailing edge of the blade and a primary external bonding bridge between the upper and lower shell members at the rearward edges. | 2011-06-16 |
20110142669 | INTEGRATED SHEAR WEBS FOR WIND TURBINE BLADES - The present invention includes a method for fabricating elongated wind turbine blades and wind turbine blades formed by the method. The method includes providing a first shell reinforcing fiber structure. At least one shear web reinforcing fiber structure is positioned adjacent to the first shell reinforcing fiber structure. The method includes infusing the first shell reinforcing fiber structure and shear web reinforcing fiber structure with a matrix material and curing the matrix material to form a unitary composite first shell component. Thereafter a composite second shell component is attached to the composite first shell component to form an elongated composite airfoil suitable for use as a wind turbine blade. The wind turbine blades formed include unitary components providing reduced number of adhesive joints. | 2011-06-16 |
20110142670 | THERMOPLASTIC ROTOR BLADE - A blade comprises a lightweight core, a composite material disposed on the core, and a skin located on the composite material. The composite material comprises fibers incorporated into a thermoplastic resin matrix in the form of a prepreg sheet or wet layup. The rotor blade may also comprise a front edge member attached along at least a portion of a leading edge of the core, a rear edge member attached along at least a portion of a trailing edge of the core, and a skin located over the core, the front edge member, and the rear edge member. The rotor blade may also comprise a spar extending through the core along a longitudinal axis of the rotor blade, and a skin located over the core and the spar. The edge members and the spars may be fabricated from thermoplastic material. | 2011-06-16 |
20110142671 | WIND TURBINE ROTOR BLADES WITH ENHANCED LIGHTNING PROTECTION SYSTEM - A wind turbine rotor blade includes a plurality of lightning receptors configured along either or both of the pressure side or suction side of the blade. At least one continuity circuit is configured with the blade, with the lightning receptors disposed in series within a respective continuity circuit such that an electrical continuity path defined by the circuit passes through each of the lightning receptors within the continuity circuit. The circuit has terminal ends that extend through the blade root for conducting continuity checks with the circuit. | 2011-06-16 |
20110142672 | WIND TURBINE ROTOR BLADE WITH A SUCTION SIDE WINGLET - A rotor blade for a wind turbine is disclosed. The rotor blade may comprise a root portion, a tip, and a body extending between the root portion and the tip. The body may include a pressure side and a suction side. Additionally, a winglet may be defined by the body. The winglet may terminate at the tip of the rotor blade and extend inwardly in a direction of the suction side of the body. Further, a bend may be defined in the body such that a portion of the body extends outwardly in a direction of the pressure side of the body. | 2011-06-16 |
20110142673 | WIND TURBINE BLADES WITH AERODYNAMIC VORTEX ELEMENTS - A wind turbine blade had a suction side surface and a pressure side surface. A plurality of vortex elements are formed on at least one of the suction side or the pressure side surfaces. The vortex elements have an upwardly inclined wind face and a downwardly inclined slip face, with the wind face and slip face meeting at a generally open-ended U-shaped ridge that defines side horns. The side horns decrease in height from a forward most portion of the ridge to the suction side surface or pressure side surface. | 2011-06-16 |
20110142674 | WIND TURBINE BLADES WITH IMPROVED BOND LINE - A wind turbine blade includes an upper shell member and a lower shell member defining an internal cavity therebetween. The shell members are joined with a bond paste along bond lines at the leading edge and trailing edge of the blade. A seal member is disposed between the upper and lower shell members at a designed width of the bond line along at least one of the trailing or leading edges. The seal member has a configuration such that excess towable bond paste is prevented from migrating past the seal member and into the internal cavity upon mating the upper and lower shell members in assembly of the blade. | 2011-06-16 |
20110142675 | WIND TURBINE ROTOR BLADE JOINT - A blade segment is disclosed for a rotor blade formed from a plurality of blade segments, the blade segment having a span and a chord. The blade segment includes a shell segment having a pressure side and a suction side extending between a leading edge and a trailing edge, the shell segment further having a tip end and a root end. The blade segment further includes at least one joint portion projecting from the shell segment at one of the tip end or the root end and defining a generally span-wise extending joining surface. The joint portion allows the blade segment to be coupled to an adjacent blade segment with a mating joint portion. | 2011-06-16 |
20110142676 | ROTOR BLADE ASSEMBLY HAVING AN AUXILIARY BLADE - A rotor blade assembly for a wind turbine is disclosed. The rotor blade assembly may generally include a primary rotor blade and an auxiliary rotor blade disposed on a suction side of the primary rotor blade. The auxiliary blade may generally include an upstream edge and a downstream edge, with the upstream edge being positioned downstream of a leading edge of the primary rotor blade. | 2011-06-16 |
20110142677 | WINGLET FOR WIND TURBINE ROTOR BLADE - A rotor blade for a wind turbine is disclosed. The rotor blade includes a root, a tip, and a body extending from the root, the body including a pressure side and a suction side extending between a leading edge and a trailing edge. The rotor blade further includes a winglet extending between the body and the tip, the winglet including a pressure side and a suction side extending between a leading edge and a trailing edge. The winglet further includes a transition section and defines a height, a sweep angle, an outboard cant angle, and a twist angle. The sweep angle, the outboard cant angle, and the twist angle change continuously throughout the transition section. | 2011-06-16 |
20110142678 | EROSION PROTECTION COATING FOR ROTOR BLADE OF WIND TURBINE - A rotor blade assembly for a wind turbine is disclosed. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade assembly further includes an erosion protection coating configured on a surface of the rotor blade. The erosion protection coating includes a ceramic layer, the ceramic layer having a thickness of less than approximately 10 millimeters. The ceramic layer is configured to reduce erosion of the rotor blade. | 2011-06-16 |
20110142679 | ROTOR BLADE FOR A WIND TURBINE, METHOD AND MANUFACTURING MOLD FOR THE PRODUCTION THEREOF - A rotor blade and a method and a manufacturing mold for the production of a rotor blade for a wind turbine, which extends longitudinally in the operational state from a blade root area to the connection to a rotor hub of the wind turbine and which is divided into at least two segments for its production, wherein at least one subdivision is provided approximately transverse to its longitudinal extension between the blade root area and the blade tip. The method facilitates and shortens the production of the rotor blade, in particular for a series production and to still provide the completed rotor blade as a familiar uniform rotor blade. In the method, the at least two segments, preferably after they have been at least partially produced or partially produced mainly parallel in time, are interconnected in an integration device. | 2011-06-16 |
20110142680 | OFFSHORE WIND TURBINE GENERATOR - Provided is an offshore wind turbine generator capable of withstanding unevenly distributed stress with a simple and inexpensive structure and of maintaining reliability in terms of strength. An offshore wind turbine generator includes a nacelle that rotatably supports a rotor head, and a tower portion that supports the nacelle and yaws integrally with the nacelle, and a structure portion that bears the strength of the tower portion has a higher strength against a load in a direction included in a plane having a rotation axis of the rotor head and an extending direction of the tower portion than the strength of the structure portion against a load in a direction included in other planes including the extending direction of the tower portion. | 2011-06-16 |
20110142681 | ROTOR BLADE ASSEMBLY - A rotor blade assembly is disclosed. The rotor blade assembly includes a main rotor blade, the main rotor blade including a pressure side and a suction side extending between a leading edge and a trailing edge, and an auxiliary rotor blade associated with the main rotor blade, the auxiliary rotor blade including a pressure side and a suction side extending between a leading edge and a trailing edge. The rotor blade assembly further includes a support member connecting the auxiliary rotor blade to the main rotor blade. The auxiliary rotor blade is configured to modify a lift force associated with the rotor blade assembly. | 2011-06-16 |
20110142682 | ONSHORE WIND TURBINE WITH TOWER SUPPORT SYSTEM - A wind turbine includes a nacelle with any manner of associated power generation equipment. The nacelle is mounted atop a tower having a base end configured for support on a ground level foundation. A tower support system provides support to the tower and includes an axially extending circumferential sleeve mounted around the tower at a location between the base end and the nacelle. A plurality of support legs are disposed around the sleeve, with each support leg having a first end rigidly affixed to the sleeve and an opposite foot end configured for mounting to a ground level footing. The support legs extend from the sleeve with a length and at an acute extension angle relative to a longitudinal axis of the tower so as to provide a designed degree of vertical and lateral support around the circumference of the tower. | 2011-06-16 |
20110142683 | Floating Underwater Support Structure - A floating underwater support structure is disclosed. The underwater support structure includes a joint capable of rotation and angular movement along two or three axes coupled to a truss. The truss is capable of sustaining loads in tension, compression, and bending, and comprises one or more elongate, rigid members. The elongate, rigid members are capable of sustaining loads in at least tension and compression. A buoyant member positioned between or around the members of the truss at a predetermined distance below the water provides a buoyant force that typically exceeds the weight of the entire structure. In deeper water, cross bracing may be provided between the members of the truss, and in particularly deep water, a single tendon may connect between the joint, typically anchored to the floor of the body of water, and the truss. The support structure may be used to support wind turbines and other structures. | 2011-06-16 |
20110142684 | Turbine Engine Airfoil and Platform Assembly - A turbine airfoil ( | 2011-06-16 |
20110142685 | PUMP UNLOADER VALVE AND ENGINE THROTTLE SYSTEM - A pressure washer system includes an engine, a water pump, a sprayer, an unloader, and a link. The engine has a throttle system designed to control the speed of the engine. The water pump includes an inlet, a pumping mechanism, and an outlet. The pumping mechanism is designed to be driven by the engine. The sprayer is attached to the outlet of the water pump. The unloader is designed to direct water toward the inlet of the water pump when the unloader is in a first configuration, and to direct water toward the sprayer when the unloader is in a second configuration. Water pressure generated when the sprayer is not actuated moves the unloader to the first configuration. The link connects the unloader and the throttle system of the engine, where the link is designed to adjust the throttle system to a first engine speed when the unloader is in the first configuration, and to adjust the throttle system to a second engine speed when the unloader is in the second configuration. | 2011-06-16 |
20110142686 | VACUUM PUMP - A differentially pumped mass spectrometer system comprises a mass spectrometer having first and second pressure chambers through which, during use, ions are conveyed along a path. A pump assembly for differentially evacuating the chambers is attached to the mass spectrometer. The pump assembly comprises a housing attached to the mass spectrometer and a cartridge inserted into the housing. The cartridge has a plurality of inlets each for receiving fluid from a respective pressure chamber and a pumping mechanism for differentially pumping fluid from the chambers. The cartridge is inserted into the housing such that the pumping mechanism is inclined relative to the ion path, but with the cartridge protruding into the mass spectrometer to such an extent that at least one of the inlets at least partially protrudes into its respective chamber without crossing the ion path. | 2011-06-16 |
20110142687 | FLOOD WATER REMOVAL SYSTEM - Flood water removal systems including a motor, a vacuum generating device, a discharge pump, and a vacuum tank can be efficiently arranged to be transversely mounted to a vehicle. Certain flood water removal systems can include a supercharger driven by the engine to generate vacuum. The systems can include a valve to prevent collapse of a vacuum tank and maintain a predetermined vacuum pressure without varying the speed of the motor. The systems can also include a two-stage exhaust that blends exhaust from the blower with motor exhaust in a silencer to reduce noise generation for operation in residential or other noise-sensitive settings. The systems can also include a vacuum tank comprising a noise reduction baffle to further reduce noise generation. | 2011-06-16 |
20110142688 | MEMS FLUID PUMP WITH INTEGRATED PRESSURE SENSOR FOR DYSFUNCTION DETECTION - The invention relates to a pumping device including a pump ( | 2011-06-16 |
20110142689 | DIESEL PUMP - A diesel pump having enhanced durability in a high pressure environment, capable of being produced at high productivity, and low in cost. The diesel pump ( | 2011-06-16 |
20110142690 | PUMP APPARATUS, POWER TRANSMISSION APPARATUS, AND VEHICLE - A pump apparatus configured with a first pump for pumping working fluid in accordance with a reciprocation of a piston using a space between a first open/close valve for suction and a second open/close valve for discharge as a pump chamber. The pump apparatus is also configured a first flow passage for supplying the working fluid from a supply source to an operation subject via the first open/close valve, the pump chamber, and the second open/close valve in accordance with an operation of the first pump. A second flow passage supplies the working fluid pumped by a second pump, which is different from the first pump, to the pump chamber. A selector is configured to select either the first flow passage or the second flow passage. | 2011-06-16 |
20110142691 | SPEED-DEPENDENT STABILITY VALVE - A stability valve assembly includes a centrifugal pump and a valve downstream of the centrifugal pump. The valve includes a valve member that is movable along a valve axis within a valve body to control a fluid flow from the centrifugal pump. The valve member has a first orifice connecting a valve input to a valve chamber, and has at least one second orifice connecting a valve outlet to the valve chamber. A reference pressure upstream of the centrifugal pump applies pressure to a stepped portion of the valve member such that an amount of negative feedback provided by the valve assembly is proportional to a rotational speed of the centrifugal pump. | 2011-06-16 |
20110142692 | Air Logic Controller - An air logic controller for increasing the efficiency of an air operated double diaphragm pump. The air logic controller may increase the efficiency of the pump by controlling the supply of compressed fluid to the pump. In one embodiment, the air logic controller may control the supply of compressed fluid to the pump by replacing the continuous, large volume supply of compressed fluid supplied to conventional air operated pumps during a single pumping stroke with a varied supply of compressed fluid. The varied supply of compressed fluid may comprise a supply of compressed fluid that alternates between a large volume supply and a small volume supply of compressed fluid. The air logic controller may vary the supply of compressed fluid to the pump based at least partially on the position of a main air valve spool and the setting on an adjustable pneumatic time delay relay. | 2011-06-16 |
20110142693 | BEARING STRUCTURE AND SCREW PROVIDED WITH A BEARING STRUCTURE OF THIS TYPE - A bearing structure between a rotor ( | 2011-06-16 |
20110142694 | MOTOR, GAS COMPRESSOR AND AGITATION ELEMENT - The present invention refers to a motor having a constructive arrangement capable of cooling the environment in which said motor is disposed. In a preferred embodiment, said electric motor ( | 2011-06-16 |
20110142695 | ELECTRIC COMPRESSOR - The present invention provides an electric compressor in which a lead wire on the motor driving circuit side can be electrically connected positively to a sealed terminal. Because the sealed terminal is formed from a terminal body which is made of a metal having electrical conductivity and whose end is provided with a male threaded portion, and a joining nut made of a metal having electrical conductivity and which is different from the material for the terminal body, and is threadably mounted on the male threaded portion of the terminal body, it is possible to positively join the joining nut of a different material to the terminal body and to positively join the lead wire of the same material as the joining nut to the joining nut by welding, whereby it becomes possible to electrically connect a lead wire on the driving circuit housing chamber side positively to the sealed terminal. | 2011-06-16 |
20110142696 | STATOR, MOTOR, AND COMPRESSOR - A stator includes a stator core, which has a plurality of stacked electromagnetic steel sheets, caulking portions configured to fix the plurality of electromagnetic steel sheets to each other, and a plurality of slot portions open toward an inner circumference side and arrayed along a circumferential direction. A number Q (an integer of 1 or greater) of the caulking portions, a number S of the slot portions and a number P of the poles satisfy Q≦S and Q=P×n/2 (where n is an integer of 1 or greater). The stator is preferably part of a motor for a compressor. | 2011-06-16 |
20110142697 | Containment structure for an actuation unit for immersion pumps, particularly for compact immersion pumps to be immersed in wells - A containment structure for an actuation unit for immersion pumps, particularly for compact immersion pumps for wells, comprising
| 2011-06-16 |
20110142698 | Heat-Dissipating Fan Assembly - A heat-dissipating fan assembly is provided. The heat-dissipating fan includes a base, a axial tube, at least one coil mounted on the base, and an impeller module having an impeller, a plurality of vanes disposed on the circumferential surface of the impeller, a shaft, and a permanent magnet. The axial tube is mounted on the base, and made of a permeability material. The shaft and the permanent magnet are disposed on the same surface of the impeller. The shaft is inserted in conjunction with the axial tube. The at least one coil is used to electrically connect with a power to interact with the permanent magnet, which in turns rotates the impeller module. | 2011-06-16 |
20110142699 | Coupling Arrangement Providing An Axial Space Between A Plunger Of A High Pressure Fluid Pump - A coupling for a pump connects a plunger to a plunger adaptor. The coupling provides a space between an end of the plunger and an end of the adaptor. Upon disconnecting the plunger from the adaptor, the space provides for removal of the plunger from and through a well of the pump. | 2011-06-16 |
20110142700 | DUAL-VENTRICLE PUMP CARTRIDGE, PUMP, AND METHOD OF USE IN A WEARABLE CONTINUOUS RENAL REPLACEMENT THERAPY DEVICE - A dual channel pulsatile pump for use with a completely wearable renal replacement device is provided. | 2011-06-16 |
20110142701 | Pump with a Sculptured Fluid End Housing - This invention relates to a method of fabricating or machining the fluid end of a high pressure pump and a fluid end produced by the method. The method includes sculpturing the front side of the fluid end which results in a non-planar surface. In this manner the internal stresses can be varied at critical points within the fluid end. | 2011-06-16 |
20110142702 | ROTARY ENGINE VANE CONDUITS APPARATUS AND METHOD OF OPERATION THEREFOR - A rotary engine is described including: (1) a rotor located within a housing, the rotor configured with a plurality of rotor vane slots; (2) a vane separating an interior space between the rotor and the housing into at least a trailing chamber and a leading chamber, where the vane slidingly engages a rotor vane slot; (3) a first passage through the vane, the first passage including a first exit port into the rotationally trailing chamber; and (4) a second exit port to the rotationally trailing chamber, where the first exit port and the second exit port connect to any of: (a) the first passage through the vane and (b) the first passage and a second passage through the vane, respectively. Optionally, one or more seals affixed to the vane and/or the rotor valve the first passage, the second passage, a vane wingtip, and/or a conduit through the rotor. | 2011-06-16 |
20110142703 | VARIABLE DISPLACEMENT VANE PUMP - A variable displacement vane pump including a relief valve which includes a valve bore, a spherical valve element in the valve bore, a valve seat fixed onto one axial side of the valve bore and having a through hole and an annular seat surface on which the valve element is seated when the relief valve is in a closed position, a coil spring disposed on the other axial side of the valve bore, and a valve element retainer disposed between the valve element and the coil spring, wherein the seat surface is configured such that when the relief valve is in the closed position, a center of the valve element is located offset from a central axis of one winding seating portion of the coil spring which is disposed on an opposite side of the seat surface, in a radial direction of the valve bore. | 2011-06-16 |
20110142704 | Roller Bearing Assembly - A roller bearing assembly is configured to rotatably support a machine component connected with a shaft in a position relative to a reference component. The roller bearing assembly includes a radial bearing, an axially-displaceable axial bearing and an adjusting device configured to adjust an axial gap between the machine component and the reference component by automated axial displacement of the axial bearing. The adjusting device includes a hydraulic regulating device configured to axially displace the axial bearing. | 2011-06-16 |
20110142705 | ROTARY COMPRESSOR - A rotary compressor is provided. The rotary compressor may include a plurality of cylinders each having a suction port formed such that an intersection of a center line of the suction port and a center line of a vane slot is positioned at a predetermined interval closer to the vane slot than to an intersection between a center of an inner diameter of the cylinder and the center line of the vane slot. A proximal end of the suction port may be formed in the vicinity of the vane slot so as to advance a compression start angle of a compression space and reduce a dead volume between the vane slot and the suction port, thus improving compressor performance. | 2011-06-16 |
20110142706 | NOISELESS PRESSURE BLOWER - The present invention relates to a noiseless pressure blower including a main body having an inlet port and an outlet port; a pressing member which rotates to suck in fluid from the inlet port; a control member which rotates in contact with the pressure member to prevent the sucked in fluid from flowing to the inlet port; and an interlocking means for transmitting rotational force to the pressure member and the control member. The main body has two cylinders that communicate with each other. The pressure member includes a pressure rotating shaft which rotates by the interlocking means, and a spiral pressure plate provided on the pressure rotating shaft. The control member includes a control rotating shaft which rotates by the interlocking means, and a control body provided on the control rotating shaft, and which rotates in linear contact with the pressure plate. | 2011-06-16 |
20110142707 | METHODS OF FORMING EARTH BORING ROTARY DRILL BITS INCLUDING BIT BODIES HAVING BORON CARBIDE PARTICLES IN ALUMINUM OR ALUMINUM BASED ALLOY MATRIX MATERIALS - Methods of manufacturing rotary drill bits for drilling subterranean formations include forming a plurality of boron carbide particles into a body having a shape corresponding to at least a portion of a bit body of a rotary drill bit, infiltrating a plurality of boron carbide particles with a molten aluminum or aluminum-based material, and cooling the molten aluminum or aluminum-based material to form a solid matrix material surrounding the boron carbide particles. In additional methods, a green powder component is provided that includes a plurality of particles each comprising boron carbide and a plurality of particles each comprising aluminum or an aluminum-based alloy material. The green powder component is at least partially sintered to provide a bit body, and a shank is attached to the bit body. | 2011-06-16 |
20110142708 | METHODS FOR PROCESSING NANOSTRUCTURED FERRITIC ALLOYS, AND ARTICLES PRODUCED THEREBY - A formed article comprising a nanostructured ferritic alloy is provided. Advantageously, the article is not formed via extrusion, and thus, cost savings are provided. Methods are also provided for forming the article, and the articles so produced, exhibit sufficient continuous cycle fatigue crack growth resistance and hold time fatigue crack growth resistance to be utilized as turbomachinery components, and in particular, large, hot section components of a gas or steam turbine engines. In other embodiments, a turbomachinery component comprising an NFA is provided, and in some such embodiments, the turbomachinery component may be extruded. | 2011-06-16 |
20110142709 | METHOD OF MANUFACTURING A COMPONENT - A component is manufactured from a powdered material such as a titanium alloy, by performing a first hot isostatic pressing HIP operation on the powdered material | 2011-06-16 |
20110142710 | Ti PARTICLE-DISPERSED MAGNESIUM-BASED COMPOSITE MATERIAL, AND MANUFACTURING METHOD THEREOF - A Ti particle-dispersed magnesium-based composite material is a material having titanium particles uniformly dispersed in a magnesium matrix, and is characterized by having a titanium-aluminum compound layer at an interface between the magnesium alloy matrix and the titanium particles dispersed in the magnesium alloy matrix. | 2011-06-16 |
20110142711 | OXIDE-DISPERSION-STRENGTHENED ALLOY - The present invention provides an oxide dispersion strengthened alloy in which even with aluminum contained, the particle diameter and dispersion spacing of the oxide are decreased, and the strength at high temperature, the high temperature oxidation and the corrosion resistance can be improved. An oxide dispersion strengthened alloy being a nickel-base alloy containing aluminum, hafnium, and yttrium oxide, wherein a complex oxide of the yttrium oxide and hafnium oxide is dispersed in a matrix of the nickel-base alloy, with the aluminum contained. | 2011-06-16 |
20110142712 | Nickel base gamma prime strengthened superalloy - A nickel base gamma prime strengthened superalloy with a unique blend of high hot corrosion resistance, high oxidation resistance, high coating compatibility, good weldability, high phase stability and at least moderate creep resistance is disclosed. The composite includes: Up to | 2011-06-16 |
20110142713 | WELDING MATERIALS FOR Ni-BASED ALLOY - Disclosed is a welding material for a Ni-based alloy, comprising components expressed as follows: C≦0.05 mass %; 8 mass %≦Cr≦25 mass %; Fe≦4.0 mass %; W≦15 mass %; 5 mass %≦Mo+½(W+Re)≦20 mass %; Co≦20 mass %; 0.01 mass %≦Al<2.0 mass %; 0.01 mass %≦Ti<2.0 mass %; Al+½Ti≦3.0 mass %; Nb+½Ta≦1.5 mass %; B≦0.007 mass %; Zr≦0.04 mass %; 0.01 mass %≦Si≦0.5 mass %; Mn≦1.0 mass %; P≦0.010 mass %; S≦0.002 mass %; O≦0.005 mass %; and Ni and unavoidable impurities which constitute the balance. | 2011-06-16 |
20110142714 | Ni-BASED SINGLE CRYSTAL SUPERALLOY AND COMPONENT OBTAINED FROM THE SAME - Provided is an Ni-based single crystal superalloy wherein the ingredients have a composition containing, as ratio by mass, from 5.0% by mass to 7.0% by mass of Al, from 4.0% by mass to 8.0% by mass of Ta, from 0% by mass to 2.0% by mass of Mo, from 3.0% by mass to 8.0% by mass of W, from 3.0% by mass to 8.0% by mass of Re, from 0% by mass to 0.50% by mass of Hf, from 3.0% by mass to 7.0% by mass of Cr, from 0% by mass to 9.9% by mass of Co and from 1.0% by mass to 10.0% by mass of Ru, with the balance of Ni and inevitable impurities. The alloy prevents TCP phase precipitation at high temperatures, therefore having improved strength at high temperatures and having oxidation resistance at high temperatures. | 2011-06-16 |
20110142715 | Brass alloy - The present invention provides an environmental friendly brass alloy, including 0.4 to 0.8 wt % of aluminum; 0.6 to 1.6 wt % of nickel; 0.8 to 2.0 wt % of tin; more than 95.6 wt % of copper and zinc; and less than 0.1 wt % of iron, lead, phosphorous and impurities, wherein the copper is present in an amount ranging from 60 to 68 wt %. | 2011-06-16 |