Patent application number | Description | Published |
20080227054 | DENTAL INSTRUMENT - An angled dental shaft receptacle is provided for operating rotating instruments with an angled shaft. The angled shaft receptacle has a driver pin, and the driver pin is connected to the angled shaft of the instrument by a planar contact during operation. The rotating instrument is preferably a dental instrument. | 09-18-2008 |
20080257907 | Multi-Compartment Dosing For Small Amounts - An apparatus for dosing small amounts of liquid or pasty media as well as media containing filling material or reactive media having a defined processing time, comprising a housing with an outlet, a dosing unit which is in communication with the outlet and is arranged in or on the housing, and a reservoir, for the medium, which is in communication with the dosing unit and is arranged in or on the housing, said apparatus consisting, in a preferred exemplary embodiment, of a housing | 10-23-2008 |
20080286714 | Impression Tray - Disclosed is an impression tray ( | 11-20-2008 |
20120067138 | METHOD FOR DETECTING TORQUE IN A TRANSMISSION, MEASURING DEVICE AND CONTROL PROGRAM - Torque can be detected in a transmission by using at least one vibration sensor to detect at least one vibration signal which is associated with a tooth engagement frequency of intermeshing transmission toothings, and the phase shift of which is dependent on at least one tooth engagement duration of the intermeshing transmission toothings. The tooth engagement duration is torque-dependent as a result of toothing deformations. A torque acting on the transmission is determined from the phase shift of the detected vibration signal and/or of the at least one tooth engagement duration. | 03-22-2012 |
20120222514 | TOOTHED GEAR WHEEL WITH EXCHANGEABLE TOOTHING - A toothed gear wheel with toothed wheel body and exchangeable teeth is disclosed. One or more teeth are embodied as a component which is able to be detachably connected to the toothed wheel body of the toothed gear wheel. A transmission embodied with the toothed gear wheel is disclosed. A component with suitable for use in a toothed gear wheel with toothed wheel body is also disclosed. | 09-06-2012 |
20130088016 | DRIVE SYSTEM FOR A WIND TURBINE - A drive system has a transmission unit comprising at least one planet wheel stage, which has a hollow wheel, several planet wheels, a planet carrier and a sun wheel. Furthermore, a first shaft associated with the transmission unit is provided, which has a coupling flange that can be connected to a work machine shaft or rotor shaft and is mounted via the planet carrier. The transmission unit and a motor unit or generator unit connected to a second shaft of the transmission unit are enclosed by a gear housing which has a cardanic circumferentially symmetric or partially symmetric suspension for connection to a supporting structural element of the wind turbine. | 04-11-2013 |
20130095972 | DRIVE SYSTEM FOR A WIND TURBINE - A drive system has a transmission unit with planetary gear stage and a first shaft associated with a planetary carrier and having a coupling flange connectable to a machine or rotor shaft. The transmission unit and a motor/generator unit includes a rotor connected with a rotation-lock to a hollow rotor shaft which is connected to a second shaft of the transmission unit and enclosed by a gearbox housing. A coupling is arranged radially between the second shaft and the hollow rotor shaft. A gearbox housing support with a hollow cylindrical extension is arranged between the transmission unit and the motor/generator unit. The cylindrical extension concentrically encloses an end section of the second shaft and forms a bearing seat for a bearing arrangement disposed radially between the second shaft and the cylindrical extension. The hollow cylindrical extension is concentrically enclosed by the rotor and the hollow rotor shaft. | 04-18-2013 |
20130133454 | GEAR UNIT WITH IMPROVED LUBRICANT SUPPLY - In order to implement a reliable supply of lubricant to gear unit components during emergency or spinning operation of a gear unit, level control is provided in a lubricant sump of the gear unit as a function of the operating state by means of a control unit associated with a lubricant pump. During normal operation the level is adjusted to dry sump level. In contrast, the lubricant pump is switched off in emergency or spinning operation, so that a splash lubrication level is automatically achieved in the lubricant sump. | 05-30-2013 |
20130165288 | DRIVE SYSTEM FOR A WIND TURBINE - A drive system has a gear unit with planetary gear stage with a planetary gear carrier. A first shaft associated with the gear unit has a coupling flange connectable to the shaft of a working machine or a rotor and is supported by the planetary gear carrier. The gear unit and a motor/generator unit connected to a second shaft of the gear unit are enclosed by a gearbox. The motor/generator unit additionally includes a rotor connected to a hollow rotor shaft with a rotation lock. An electrically isolating, detachable flange connection is disposed between the rotor shaft and the second shaft, with the gear-side end of the detachable flange connection connected to a hollow gear shaft. A gearbox stub which concentrically encloses a gear-side end section of the gear shaft is disposed between gear unit and motor or generator unit and forms a bearing seat for the second shaft. | 06-27-2013 |
20130172141 | DRIVE SYSTEM FOR A WIND TURBINE - A drive system for a wind turbine includes a transmission unit with a planet wheel stage. A coupling flange on a first shaft of the transmission unit can be connected to a driven machine shaft or rotor shaft which is mounted above a planet carrier. The transmission unit and a motor/generator unit connected with a second shaft of the transmission unit are enclosed by a gear case. A rotor of the motor/generator unit is connected to a hollow rotor shaft which surrounds an end section of the second shaft and is connected to the end section via an interior coupling or clamping connection. A connecting-piece is arranged between the transmission unit and the motor/generator unit, and concentrically surrounds a transmission-side end section of the rotor shaft, forming a bearing seat for the rotor shaft, which also supports the second shaft of the transmission unit. | 07-04-2013 |
20130180319 | METHOD FOR IDENTIFYING DAMAGE ON TRANSMISSIONS - A method for identifying possible damage in a toothed transmission stage having at least one pair of engagement toothed wheels includes measuring with a vibration transducer an oscillation signal corresponding to oscillations produced by a rolling and impact motion when teeth of a pair of the toothed wheels mesh under load during operation of the transmission stage, comparing the oscillation signal with a calibration oscillation signal, determining a torque acting on the transmission stage from a difference between the oscillation signal and the calibration oscillation signal, and evaluating the measured oscillation signal commensurate with the determined torque to identify the possible damage to the transmission stage. | 07-18-2013 |
20140302957 | DRIVE SYSTEM FOR A WIND TURBINE - A drive system having an integrated transmission and motor/generator unit for a wind turbine includes a transmission output shaft designed as a hollow shaft, which receives a sun shaft of an output-side planetary gear stage and is connected thereto. The transmission output shaft comprises a transmission-side end section of an insert shaft which is concentrically arranged within a rotor hollow shaft. The transmission output shaft additionally has a bearing for receiving radial and axial forces. The motor/generator unit has two dedicated bearings. One bearing thereof is a transmission-side bearing. In addition, a rear-side generator bearing is provided. | 10-09-2014 |
20150039248 | METHOD FOR DETERMINING A PARAMETER RELEVANT FOR CAUSING DAMAGE TO A STRUCTURE - A method for determining a parameter relevant for the damage to a structure, such as machines, machine components and individual assemblies that are subject to vibration stresses is disclosed. A method for active or passive vibration damping that makes use of this method, and a structure having a device configured to perform the above methods is also disclosed. | 02-05-2015 |
20150142175 | MACHINE COMPONENT OF A DRIVETRAIN AND A METHOD FOR CONFIGURING AND/OR PUTTING INTO OPERATION AND/OR OPERATING SUCH A DRIVETRAIN - The invention relates to a machine component of a drive train and to a method for configuring and/or putting into operation and/or operating such a drive train ( | 05-21-2015 |
Patent application number | Description | Published |
20080202816 | Torque Converter for Use When Drilling with a Rotating Drill Bit - A torque converter for use in drilling with a rotating drill bit, the purpose of the torque converter being to absorb impacts and bring about an axial movement of the drill bit when the torque exceeds a predetermined value. For this purpose the torque converter is composed of two cylindrical string parts connected through the bearing elements. The string parts are connected to each other through helical elements in such a way that relative rotation of the two cylindrical string parts brings about axial movement, which unloads the drill bit. | 08-28-2008 |
20120228029 | Method and Device for Reducing Friction Between Helical Members of a Downhole Damper - A method for reducing friction between interconnected outer and inner helical members of a downhole damper where the damper includes an outer damper body and an inner damper body, and where the outer and inner damper bodies are telescopically movable relative each other, the outer and inner damper bodies being biased in the extending direction, and where one of the outer and inner damper bodies are connected to a drill bit workable at a borehole face, and where the other of the outer and inner damper bodies is connected to a torque and force transmitting member, and where the outer and inner helical parts are arranged so as to retract the bit from the face when torque applied by the torque and force transmitting member exceeds a preset value, wherein the method includes letting a relative movement between the inner and outer body force lubricant to flow between the helical members. | 09-13-2012 |
20130206482 | PUMP POSITIONED AT A DRILL BIT - An ejector pump or jet pump is for use in the drilling of wells in the underground for the production of oil and gas, for example, in which it is the purpose to prevent the total fluid pressure at the bottom of the borehole from reaching a level which constitutes a risk of cracking the rock or sediment being drilled, thus resulting in leakage and circulation failure. For this purpose, the pump is placed between the drill bit and the drill string by means of standard pipe couplings and formed as an elongated cylindrical element with external, longitudinal pump elements with nozzles directed in such a way that low pressure is established externally at the drill bit. The pump is operated by the drilling fluid which is supplied in the normal way from the drill string. The pressure difference across the pump is used to draw a secondary flow of drilling fluid from the established borehole through internal bores in the pump casing to the ordinary nozzles in the drill bit. This fluid flow provides necessary cleaning of the drill bit and drilling surface but, then, will have a highest possible pressure that is limited upwards to the level established in the borehole and so that possible clogging around the drill bit will not cause an increased risk of drilling fluid leaking into the underground. | 08-15-2013 |
Patent application number | Description | Published |
20100111685 | GAS TURBINE ENGINE COMPONENT, A TURBOJET ENGINE PROVIDED THEREWITH, AND AN AIRCRAFT PROVIDED THEREWITH - A gas turbine engine component is provided including at least one ring element, and a plurality of circumferentially spaced load carrying vanes extending in a radial direction of the ring element. The load carrying vanes have an internal structure with an anisotropic load carrying property, and the internal structure is configured so that a main load carrying direction is in parallel with the extension direction of the load carrying vane. The component includes a stiffening structure bridging the distance between at least two adjacent load carrying vanes in the circumferential direction of the ring element, and the at least two adjacent load carrying vanes are attached to the stiffening structure. | 05-06-2010 |
20120213633 | GAS TURBINE ENGINE COMPONENT - A gas turbine engine component includes a ring element and a plurality of circumferentially spaced load carrying vanes extending in a radial direction of the ring element. At least one of the vanes is made of a composite material. The at least one composite vane is fastened to the ring element. The component further includes first and second wall portions that are fixed in relation to the ring element and arranged on opposite sides of the composite vane. At least a first hole extends through the first wall portion, the composite vane and the second wall portion. The first hole is adapted to receive a first insertion member. The component is arranged such as to, with regard to the first hole, provide a tight fit for the first insertion member in the first wall portion as well as in the composite vane and to provide a loose fit with a radial play in the second wall portion. | 08-23-2012 |
20120213634 | GAS TURBINE ENGINE COMPONENT - In a gas turbine engine at least one vanes is made of a composite material and an end part of the vane is fastened to the ring element by at least a first bracket member arranged in a corner region formed by the vane and a ring element. The first bracket member is fastened to the vane by a first fastening device arranged in association with a first hole extending through the vane. The first bracket member is fastened to the ring element by a second fastening device arranged in association with a second hole extending through the ring element. An opening is arranged in the ring element. A second bracket member at least partly has an angular cross section. The second, angled bracket member is arranged through the opening such as to be positioned on an opposite side of both the vane and the ring element in relation to the first bracket member. The second, angled bracket member is fastened to the first bracket member by the first and second fastening devices. | 08-23-2012 |
20140161605 | GAS TURBINE STRUCTURE - A gas turbine structure includes a guide vane. The gas turbine structure (further includes a first housing and a second housing and the guide vane extends from the first housing to the second housing. The guide vane includes a leading edge and a trailing edge and the guide vane extends from the leading edge to the trailing edge along a mean camber line. The guide vane includes a first attachment structure, a first fastening arrangement and a second fastening arrangement. Moreover, the first attachment structure includes a stiffening member extending over at least a portion of a circumference of the first housing. Furthermore, the stiffening member includes a stiffening member center point as measured along the mean camber line. | 06-12-2014 |
20140294579 | COMPOSITE GUIDE VANE - A composite guide vane for a gas turbine structure is adapted to extend in a guide vane direction from a first housing towards a second housing of the gas turbine structure. The guide vane includes a guide vane length in the guide vane direction and the guide vane includes a first attachment portion with at least one first opening for attachment of the guide vane to the first housing. The first opening extends in a first opening direction which forms an angle with the guide vane direction. The guide vane includes a cover portion including a first material and a core portion which is at least partially enclosed by the cover portion. | 10-02-2014 |