Fluid reaction surfaces (i.e., impellers) inventions 08/06

20060193725 - Device for locking a structure for securing a blade to the hub of a rotorcraft rotor: A device for locking a holding structure for securing a foldable blade of a rotorcraft rotor to the hub of the rotor. The holding structure is hinged in pitch and in drag relative to the hub and the rotor includes, for the purpose of folding the blade, elements for locking...

20060193726 - Torque-tuned, integrally-covered bucket and related method: A turbine bucket includes a shank portion, an adjacent and radially inner dovetail mounting portion, an adjacent and radial outer airfoil portion, with a platform at a radially inner end of said airfoil portion adjacent the shank portion, and an integral cover at a radially outer tip of the airfoil...

20060193727 - Drilling element for a bearingless rotor: A twist element for a bearingless rotor is made mostly of composite fiber material and has a cross section with a substantially symmetric, flattened shape that has approximately the contour of a horizontal, central section of a double cone. In addition, a bearingless rotor having at least one such twist...

20060188371 - Wind turbine, hydraulic system, air bleed system and method of controlling at least two wind turbine blades: The invention relates to a wind turbine having rotating means including at least two wind turbine blades which are turnable around the longitudinal axis of said blades, and a wind turbine hub connecting said at least two wind turbine blades with at least one shaft. Further, the wind turbine includes...

20060188372 - Turning gear drive system: A clutch assembly for a turning gear includes an overspeed clutch, an output shaft, and a centrifugal clutch. The overspeed clutch is disposed at the input shaft. The output shaft is in mechanical communication with the input shaft via the overspeed clutch. The centrifugal clutch is disposed at a portion...

20060188373 - Axially separate rotor end piece: A rotor end piece (1) for a rotor of a thermal turbomachine, having at least one circumferential slot (3) in which press blades, intermediate pieces and two end blades (4), between which a residual gap is formed, are fitted, the rotor end piece (1) having two end piece halves (9,...

20060188374 - Methods and apparatus for assembling rotatable machines: A method and apparatus for assembling a rotatable machine is provided. The machine includes a first set of blades that extend radially outwardly from a rotor assembly and wherein a second set of blades is available for installation on the rotor assembly. The method includes determining at least one of...

20060188376 - Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine: A rotor of a turbine-type machine, in particular a gas turbine rotor, is disclosed. The rotor has a rotor base body, where the rotor base body has a groove extending in the circumferential direction of the rotor base body, and has multiple rotor blades or rotor blade segments. The rotor...

20060188375 - Rotor for a turbomachine: A rotor for a turbomachine. The rotor comprises a hub including a peripheral surface, a first side surface, and a second side surface. The hub defines a plurality of cavities, each one of the cavities extending inwardly from the peripheral surface. The hub also defines a plurality of openings, each...

20060188377 - Lock plate arrangement: In gas turbine engines it is found that leaked coolant flow through the lock plates 28, 29, 50, 60 can be used to insulate the rotor surfaces 33, 34 from the effects of hot gas ingestion. In order to enhance this effect chutes 39, 59, 69 are provided to guide...

20060188378 - Method for manufacturing a wind turbine blade, a wind turbine blade manufacturing facility, wind turbine blades and uses hereof: The invention relates to a method for manufacturing a wind turbine blade or a section of a wind turbine blade. The method includes, establishing a first part having a first wind turbine blade part in a first fixating unit, establishing a second part having a second wind turbine blade part...

20060188379 - Apparatus and method of balancing a shaft: An apparatus for balancing a shaft of an aircraft engine preferably includes a nose cone and the use of standard fasteners. The nose cone is adapted to cooperate with at least one standard fastener to retain the standard fastener to the nose cone to rotationally balance the shaft....

20060182631 - Lifting stage: A lifting stage includes a carrier frame, an object plate configured to carry an object, a cross-member, and a parallel articulation arrangement configured to articulate the object plate to the carrier frame so that the object plate is capable of being raised or lowered relative to the carrier frame without...

20060182632 - Windmill rotor comprising multiple separate wind channels: Round honeycomb rotor for wind generators and most propellers has bent tubular trapezoids, two or more concentric tubular cylinders and a variable number of round bent tubular trapezoids. Both cylinders and trapezoids form modular trapezoidal tubes, which have large wind contact surfaces. The concentric tubular cylinders of the round panel...

20060182633 - Turbine blade: A turbine blade 29 for a gas turbine engine 10 having an axis 20, the turbine blade 29 comprising: an aerofoil 30 including a high pressure surface 36, a low pressure surface 34, a root portion 38 and a tip surface 40 extending transverse from the high and low pressure...

20060182634 - Wind power plant: A wind power plant comprises an outside ring, an inside ring and roll bodies arranged between an inside jacket of the outside ring and an outside jacket of the inside ring for permitting twisting or rotation of the bearing rings against one another. One of the rings on the jacket...

20060177307 - Ceiling fan with fragrance dispensing blade: A fan blade is provided with a recess for mounting an air freshener insert therein. The air freshener insert, after being mounted in the recess provided in the blade, releases a fragrance which is dispersed in the air when the fan blade is in rotary motion due to airflow over...

20060177308 - Hydrokinetic speed governor: A method for governing the speed of a fluid turbine by establishing a circulating flow and a rotational flow with a rotor, and interrupting the rotational flow with an opposing stator. A related braking apparatus includes a housing, a rotatable shaft, a rotor configured to rotatingly engage the shaft and...

20060177309 - Airfoil locator rib and method of positioning an insert in an airfoil: An airfoil for a gas turbine engine, the airfoil comprising a locator rib provided at a bottom of a cavity in the airfoil core, the locator rib having an inclined surface to be engaged by a leading end of the insert during installation thereof in the cavity....

20060177310 - Cooled blade or vane for a gas turbine: A cooled blade or vane for a gas turbine has a main blade or vane part which starts from a blade or vane root and a blade or vane shank and has a leading edge and a trailing edge, as well as, inside the main blade or vane part, a...

20060177311 - Wind power generator: A wind power generator has a base, a wind driving wheel, a transmission unit and a power storage unit. The wind driving wheel has a spindle at a center of the wind driving wheel. The spindle is positioned to the lateral frame. A plurality of connecting frames are extended from...

20060177312 - Rotating blade body: A rotating blade body is provided that can restrain vibrations of rotating blades effectively. The rotating blade body comprises rotor disc, a plurality of rotating blades being assembled so as to extend from the outer circumference of the rotor disc in a radial pattern, and sealing pins extending along the...

20060177313 - Install blade bracket for a ceiling suspended fan: A install blade bracket for a ceiling suspended fan comprises: a discal seat is disposed at a bottom of the rotary assembly, the discal seat is formed with a recess, in the recess are defined a plurality of locking cavities and a plurality of receiving cavities, a plurality of positioning...

20060177314 - Turbine rotor blade and turbine: A set of turbine rotor blades is arranged on a rotor disk. Each rotor disk has blade profile, root parts which is fitted axially in an axial disk groove formed circumferenctially in the rotor disk, and an integral cover formed at the outer edge of the blade profile part. A...

20060177315 - Closure system, method of use, and devices including closure system: A closure system and various exemplary embodiments for devices including the closure system are disclosed. The closure system may include a base, a sideplate configured to rotate with respect to the base, and a retaining mechanism carried by the sideplate and configured to pivot with respect to the sideplate substantially...

20060177316 - Shrink-fit stress coupling for a shaft of differing materials: A shrink-fit coupling includes a discontinuous ring between a ceramic stub shaft of a turbine rotor and an inner diameter r2 of a metallic shaft which typically supports a compressor rotor. If the materials for the ceramic stub shaft and the discontinuous ring are pre-determined and the radius of the...

20060171805 - Device for interacting with a fluid moving relative to the deivce and vehicle including such a device: A device (10) for interacting with a fluid (12) moving relative to the device. The device comprises a body with an axis of rotation (22) and a periphery (24). The body is rotatable about the axis of rotation. The device also comprises a plurality of vanes (16i) associated with the...

20060171806 - Turbine blade for monitoring torsional blade vibration: The claimed invention provides a blade vibration measuring system comprising a blade, a transmitter, a target with parallel edges located on the blade shroud and a receiver. The present invention also provides a blade adapted for measuring torsional blade vibration. Furthermore, the claimed invention provides a method for monitoring torsional...

20060171809 - Cooling fluid preheating system for an airfoil in a turbine engine: A platform cooling system usable in a turbine engine together with an airfoil for preheating cooling fluids before the cooling fluids enter a cooling system in the airfoil in a turbine engine. The platform cooling system includes cooling channels in either the ID or OD platforms, or both, of the...

20060171807 - High efficiency fan cooling holes for turbine airfoil: A turbine airfoil includes a leading edge and an axially spaced-part trailing edge, the leading edge having an axially-extending external surface curvature. A cooling circuit in the airfoil includes cooling holes formed in the leading edge along the span axis of the airfoil. The cooling holes have a diffuser section...

20060171808 - Vortex dissipation device for a cooling system within a turbine blade of a turbine engine: A turbine blade for a turbine engine having a cooling system in the turbine blade formed from at least one cooling channel. The cooling system may include one or more protrusions positioned in the cooling channel and including one or more vortex breakers along the length of the protrusion. The...

20060171811 - Efficient windmill: The present invention is directed to a horizontal windmill system. The system has a windfoil system that rotates 360 degrees about a conventional vertical energy shaft to obtain a greater efficiency than other windmill systems....

20060171810 - Wind generator of the type with automatic power regulation: The invention relates to a wind generator of the type with automatic power regulation, comprising at least one propeller having at least two blades (21), whereby the efficiency of one propeller varies inversely to a variation in the wind energy, from a lower wind speed limit. The torque/speed characteristics of...

20060171812 - Support system for a composite airfoil in a turbine engine: A turbine airfoil support system for coupling together a turbine airfoil formed from two or more components, wherein the support system is particularly suited for use with a composite airfoil. In at least one embodiment, the turbine airfoil support system may be configured to attach shrouds to both ends of...

20060171813 - Turbine blade tip and shroud clearance control coating system: A turbine blade tip and shroud clearance control coating system comprising a dense abrasive blade tip layer and an abradable shroud layer are provided. The dense abrasive coating may comprise cubic zirconia, hafnia or mixtures thereof and the abradable layer may be a nanolaminate thermal barrier coating that is softer...