WO2007085259A1 - A wind turbine comprising at least one gearbox and an epicyclic gearbox - Google Patents
A wind turbine comprising at least one gearbox and an epicyclic gearbox Download PDFInfo
- Publication number
- WO2007085259A1 WO2007085259A1 PCT/DK2007/000035 DK2007000035W WO2007085259A1 WO 2007085259 A1 WO2007085259 A1 WO 2007085259A1 DK 2007000035 W DK2007000035 W DK 2007000035W WO 2007085259 A1 WO2007085259 A1 WO 2007085259A1
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- WO
- WIPO (PCT)
- Prior art keywords
- sensors
- gearbox
- data
- wind turbine
- epicyclic gearbox
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D15/00—Transmission of mechanical power
- F03D15/10—Transmission of mechanical power using gearing not limited to rotary motion, e.g. with oscillating or reciprocating members
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D15/00—Transmission of mechanical power
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D17/00—Monitoring or testing of wind motors, e.g. diagnostics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
- F03D80/70—Bearing or lubricating arrangements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/40—Transmission of power
- F05B2260/403—Transmission of power through the shape of the drive components
- F05B2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
- F05B2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclic, planetary or differential type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/80—Diagnostics
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2270/00—Control
- F05B2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
- F05B2270/807—Accelerometers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2270/00—Control
- F05B2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
- F05B2270/81—Microphones
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/01—Monitoring wear or stress of gearing elements, e.g. for triggering maintenance
- F16H2057/012—Monitoring wear or stress of gearing elements, e.g. for triggering maintenance of gearings
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Definitions
- the invention relates to a wind turbine comprising at least one gearbox according to the preamble of claim 1 and an epicyclic gearbox according to the preamble of claim 25.
- Epicyclic gears are properly the "most compact embodiment of a gearbox, and in applications, such as wind turbines, where minimum size and weight are important, the use of epicyclic gearboxes is very widespread. But epicyclic gears have the major downside that smithereens from small initial damage may be torn through the gear contacts and bearings and thereby cause severe secondary damage.
- smithereens may cause the entire gearbox to seize, causing heavy damage not only to the gearbox itself but also to the equipment providing the input and the equipment receiving, the output from the gearbox.
- An object of the invention is therefore to provide for a technique for improving the detection of both initial and secondary damage in wind turbine gearboxes.
- the invention provides for a wind turbine comprising at least one gearbox.
- the gearbox comprises one or jnbre sensors for measuring condition values of the wind turbine, and is characterized in that the one or more sensors are mounted on one or more rotating parts of the gearbox.
- the sensors on the rotating parts of the gearbox is advantageous, in that the sensors then are positioned closer to or on the gearbox parts, such as gears, shafts, bearings - either the inner or the outer bearing ring - gear carrier etc., which provides the condition values, that can be used to predict or detect a defect in the gearbox or other rotating or moving wind turbine parts.
- said at least one gearbox is an epicyclic gearbox comprising at least two planet gears each including a planet gear shaft, said epicyclic gearbox further comprising at least one planet carrier connecting said planet gears.
- Epicyclic gearboxes comprises several rotating parts mounted on other rotating parts, hereby making it difficult to identify or pick up vibrations originating for possible defects - especially defects originating from the double rotating parts. It is therefore particularly advantageous to place the sensors on the rotating parts in an epicyclic gearbox.
- said one or more sensors are mounted on or in close proximity of one or more of said at least two planet gear shafts.
- said one or more sensors are mounted on said at least one planet carrier.
- the planet carrier is in most epicyclic gearboxes easily accessible and is not directly exposed to the gear oil, which is advantageous in that, the risk of the gear oil interfering with the sensors measurements or damaging the sensors is hereby reduced.
- the planet carrier is connected to all the planet gears, which is advantageous, in that a good transmission path for structure- born vibrations from all the critical parts of the gearbox is hereby provided.
- each of said at least one planet carrier comprise only one sensor.
- Providing the planet carrier with only one sensor is advantageous, in that it provides for a cost efficient way of detecting defects.
- said one or more sensors comprise means for measuring vibrations and/or acoustic emission.
- Monitoring the vibrations and/or the acoustic emission from e.g. a gearbox is a well- proven and efficient way of detecting 'defects at an early stage. It is therefore advantageous to provide the sensors with means for measuring vibrations and/or acoustic emission.
- said one or more sensors are one or more accelerometers and/or one or more microphones.
- accelerometers and/or microphones is a well-proven and efficient way of detecting defects on moving or rotating parts at an early stage. It is therefore advantageous if the sensors are accelerometers and/or microphones.
- an accelerometer refers to a sensor that measures acceleration or more specifically a device used to measure the rate of change in velocity over a specific period of time.
- An accelerometer can measure the acceleration in one direction, it can measure the acceleration in several directions such as two or three directions e.g. perpendicular to each other or it can comprise several accelerometers built together to ; form a single accelerometer capable of measuring acceleration in several directions.
- said one or more sensors are connected to one or more data transmitters for transmitting data to an external data receiver.
- Connecting the sensors to data transmitters for transmitting the condition values - picked up by the sensors - to an external data receiver is advantageous in that, it hereby is possible to reduce the amount of electrical equipment placed inside the gearbox, hereby enabling that e.g. the data can be analyzed outside the gearbox by equipment placed in a more friendly and controlled environment. ; . ⁇ ⁇
- connection is made wirelessly.
- Connecting the sensors to the data transmitter wirelessly is advantageous in that it among other things provides for a more simple and inexpensive installation procedure. , , ,
- said one or more data transmitters are mounted on said one or more rotating parts of said gearbox.
- more than one of said one or more sensors are connected to the same data transmitter. Connecting more sensors to the same data transmitter provides for a simple and cost- efficient way of transmitting the sensors measurements.
- said one or more data transmitters comprise means for transmitting data continuously during operation of said gearbox.
- Transmitting data continuously is advantageous, in that it hereby is possible to monitor the gearbox and other wind turbine components continuously, hereby enabling that a possible defect is detected more or less as soon as possible.
- said one or more data transmitters comprise means for transmitting data upon receiving a request from an externally positioned request emitter.
- the request emitter could e.g. be a surveillance unit monitoring the condition of several or all components of the wind turbine. When the unit by other means detects that there could be a problem in the gearbox or in other connected wind turbine components, it could emit a signal to the data transmitter, requesting data from the sensors to confirm or support the suspicion of a problem.
- said one or more data transmitters are hard wired to said external data receiver e.g. through a slip ring or brush connection.
- Hard wiring provides for a safei and reliable connection technique which is advantageous in connection with establishing electrical communication between the data transmitter and the external data receiver. Furthermore, it should be emphasised that "slip ring or brush connection" is only two of a number of different ways of transmitting electrical signals from a rotation shaft to a stationary part without doing it wirelessly.
- said one or more data transmitters comprise means for transmitting said sensors measurements wirelessly.
- Connecting fixed parts with rotating parts by means of wires or cables can be very complex and especially if the rotating part is mounted on another rotating part. It is therefore advantageous to provide the data transmitters with means for transmitting data wirelessly.
- said one or more data transmitters comprise a transponder.
- transponder Using a transponder is advantageous, in that the data transmitters and sensors do not need a permanent power supply. Wirelessly the transponder is fed an electromagnetic impulse from the outside of the gearbox, making it generate power enough for the sensors to measure the condition values and transmit them back to an external data receiver.
- said one or more data transmitters and said one or more sensors are formed integrally as one unit.
- Forming the sensors and data transmitters as one unit is advantageous, in that the total production and mounting costs hereby can be reduced.
- said one or more sensors are connected to one or more data processing units.
- Connecting sensors to a data processing unit is advantageous, in that it hereby is possible to filter, compress, analyse or in other way process the data from sensors and thereby enable a faster detection of defects or damage to the gearbox or other wind turbine equipment.
- said one or more data processing units are mounted on said one or more rotating parts of said gearbox.
- more than one of said one or more sensors are connected to the same data processing unit.
- Connecting several sensors to the same data processing unit is advantageous, in that the cost of the equipment and the mounting costs hereby are reduced.
- said one or more data processing units comprise means for detecting defects in said gearbox based on the measurements of said one or more sensors.
- Making the data processing units comprise means for detecting defects in the gearbox is advantageous, in that it hereby is possible to avoid continuous data transmission to the outside,, The, relatively large amount of raw data from the sensors could be processed and analyzed inside the gearbox, where after the data processing unit would only have to emit (or remove) a simple signal in the case, that a defect was detected.
- said one or more data processing units comprise means for generating an alarm signal when detecting a defect in said gearbox.
- said one or more data processing units comprise means for filtering said one or more sensors measurements.
- the signals from the sensors could include a large amount of undesired information such as short-term fluctuations or static noise. It is therefore advantageous to filter the sensors measurements before they are analysed to simplify and speed up the analyse process and to reduce the amount of data, hereby making a possible data transmission more simple and reliable.
- said one or more data processing units comprise means for compressing the data of said One or more sensors measurements.
- said one or more data processing units and said one or more data transmitters are formed integrally as one unit.
- Forming the data processing units and the data transmitters as one unit is t advantageous, in that the total production and mounting costs hereby can be reduced.
- said one or more data processing units and said one or more sensors are formed integrally as one unit.
- Forming the data processing units and the sensors as one unit is advantageous, in that the total production and mounting costs hereby can be reduced.
- said one or more sensors are mounted in one or more of said at least two planet gear shafts.
- Mounting the sensors in the shafts e.g. inside holes, recesses or other types of cavities in the shafts provides for a more controlled and protected environment for the sensors hereby reducing the risk of damage or malfunction of the sensors.
- the invention further relates to an epicyclic gearbox comprising a gearbox housing, one or more gearbox parts rotating in relation to the housing, and one or more sensors for measuring condition values of the gearbox.
- the epicyclic gearbox is characterized in that, the one or more sensors are mounted on one or more of the rotating parts of the gearbox.
- epicyclic gearboxes are characterised in that they comprise a large number of rotating parts and in that they comprise rotating parts mounted on other rotating parts. It is therefore particularly advantageous to mount the sensors measuring the gearboxes condition on the rotating parts of an epicyclic gearbox, in that a more direct path between the source and the sensor is hereby created.
- said one or more sensors are mounted on or in close proximity of one or more planet gear shafts of said epicyclic gearbox.
- said one or more sensors are mounted on at least one planet carrier of said epicyclic gearbox.
- each of said at least one planet carrier comprise only one sensor.
- said one or more sensors comprise means for measuring vibrations and/or acoustic emission.
- said one or more sensors are one or more accelerometers and/or one or more microphones.
- said one or more sensors are connected to one or more data transmitters for transmitting data to an external data receiver.
- said one or more data transmitters are mounted on said one or more rotating parts of said epicyclic gearbox.
- more than one of said one or more sensors are connected to the same data transmitter.
- said one or more data transmitters comprise means for transmitting data continuously during operation of said epicyclic gearbox.
- said one or more data transmitters comprise means for transmitting data upon receiving a request from an externally positioned request emitter.
- said one or more data transmitters comprise means for transmitting said sensors measurements wirelessly.
- said one or more data transmitters comprise a transponder.
- said one or more data transmitters and said one or more sensors are formed integrally as one unit. > •
- said one or more sensors are connected to one or more data processing units.
- said one or more data processing units are mounted on said one or more rotating parts of said gearbox.
- more than one of said one or more sensors are connected to the same data processing unit.
- said one or more data processing units comprise means for detecting defects in said epicyclic gearbox based on the measurements of said one or more sensors.
- said one or more data processing units comprise means for generating an alarm signal when detecting a defect in said epicyclic gearbox.
- said one or more data processing units comprise means for filtering said one or more sensors measurements.
- said one or more data processing units comprise means for compressing the data of said one or more sensors measurements.
- said one or more data processing units and said one or more data transmitters are formed integrally as one unit.
- said one or more data processing units and said one or more sensors are formed integrally as one unit.
- said one or more sensors are mounted in one or more planet gear shafts of said epicyclic gearbox.
- fig. 1. illustrates a large modern wind turbine known in the art, as seen from the front
- fig. 2 illustrates an embodiment of a wind turbine nacelle, as seen from the side
- fig. 3 illustrates an embodiment of a epicyclic gearbox, as seen from the front
- % 4 illustrates an embodiment of an epicyclic gearbox comprising a planet carrier, as seen from the front,
- fig. 5 illustrates a part of a cross section of an embodiment of an epicyclic gearbox, as seen from the side
- fig. 6 illustrates an embodiment of a vibration monitoring system for an epicyclic gearbox, as seen from the front, and
- fig. 7 illustrates another embodiment of a vibration monitoring system for an epicyclic gearbox, as seen from the front.
- Fig. 1 illustrates a modern wind turbine 1, comprising a tower 2 and a wind turbine nacelle 3 positioned on top of the tower 2.
- the wind turbine rotor 4 comprising three wind turbine blades 5, is connected to the nacelle 3 through the low speed shaft 6 which extends out of the nacelle 3 front.
- Fig. 2 illustrates an embodiment of a wind turbine nacelle 3, as seen from the side.
- the drive train in a traditional wind turbine 1 known in the art usually comprises a rotor 4 connected to a gearbox 7 by means of a low speed shaft 6.
- the rotor 4 comprise only two blades 5 connected to the low speed shaft 6 by means of a teeter mechanism 8, but in another embodiment the rotor 4 could comprise another number of blades 5, such as three blades 5, which is the most common number of blades 5 on modern wind turbines 1.
- the rotor 4 could also be connected directly to the gearbox 7.
- the gearbox 7 is then connected to the generator 9 by means of a high speed shaft 10.
- gearbox 7 type in most modern wind turbines 1 is an epicyclic gearbox 11, but other gearbox 7 types are also feasible, such as one or more spur gearboxes, worm gearboxes, helical gearboxes or a combination of different transmission and gearbox 7 types.
- Fig. 3 illustrates an embodiment of an epicyclic gearbox 11 as seen from the front.
- the planet gears 12 mesh with and rotate around a sun gear 13 in the middle and they mesh with an outer annulus gear.14.
- the arrows indicate that the planet gears 12 all rotate in the same direction and that the sun gear 13 rotates in the opposite direction.
- the epicyclic gearbox comprise three planet gears 12, but in another embodiment it could also comprise another number such as two, four or five planet gears 12.
- Each planet gear 12 is provided with one or more planet gear bearings 17 and each of the planet gears 12 with bearings are mounted on a planet gear shaft 16.
- Fig. 4 illustrates an embodiment of an epicyclic gearbox 11 comprising a planet carrier 15, as seen from the front.
- the planet carrier 15 connects the planet gears 12 by fixating the planet gear shafts 16, making it rotate as the planet gears 12 travel around the sun gear 13.
- the annulus gear 14 is connected to a carrying frame, to the gearbox housing or is in other ways .fixed, but in some epicyclic gearbox 11 types the annulus gear 14 could also rotate.
- the illustrated gears show only one stage of a gearbox 11.
- the entire gearbox could comprise a number of stages as the one shown to increase the gearing, or it could comprise a number of different stages e.g.
- gearbox 11 designs are also feasible often depending on what the gearbox 11 is to be used for.
- the gearbox 11 could be designed to carry the entire load of the rotor 4, which means that the gearbox 11 has to be designed to handle this massive load on the input side of the gearbox 11, whereas the load on the output side of the gearbox would be significantly smaller.
- Epicyclic gearboxes 11 used in different wind turbines 1 or gearboxes 11 used in other applications could therefore be designed differently to meet different needs.
- the planet carrier 15 is formed as a simple plate connecting the three planet gears 12, but in another embodiment the planet carrier 15 could comprise a bearing for guiding and stabilizing the carrier 15. This would e.g. be the case if the carrier 15 was connected to a wind turbine rotor 4, and the planet carrier 15 also had to transfer the entire load of the rotor 4. The inner ring of a large diameter bearing could then e.g.
- FIG. 5 illustrates a part of a cross section of an embodiment of an epicyclic gearbox 11, as seen from the side.
- the planet gears 12 are each provided with two juxtaposed bearings 17 but in another embodiment the planet gears 12 could be provided with another number of bearings 17 or the bearings 17 could be placed in the planet carrier 15, where the shaft 16 then would be rigidly connected to the planet gears 12.
- the planet carrier 15 is provided with an input shaft 18, which could be the low speed shaft 6 of a wind turbine 1, but in another embodiment the carrier 15 could be directly coupled to the input generating equipment such as the hub of a wind turbine rotor 4.
- the planet gears 12 mesh with the annulus gear 14, which in this embodiment is rigidly connected the gearbox housing 20, and with the sun gear 13, which is provided with an output shaft 19 e.g. connected to another gear stage or connected to a wind turbine generator 9. ⁇
- the planet carrier 15 is provided with a number of vibration sensors 21, most likely in form of accelerometers, but it could also be microphones measuring the acoustic emissions which the vibrations generates.
- the sensors 21 measuring condition values could also be e.g. strain-gauges, thermometers or other types of sensors 21 providing information of the conditions of the equipment on which they are mounted or any related equipment.
- the carrier 15 is in this embodiment provided with one sensor 21 at the end of each planet gear shaft 16, which in this case would provide the carrier with three sensors
- the gearbox 11 could be provided with another number of sensors 21 and the sensors 21 could be placed elsewhere, such as a different location on the carrier 15, directly on the planet gear shafts 16, in the planet gear shafts 16 (e.g. in a hole, in a recess or in another form of cavity in the shafts 16), on the planet gears 12, on the sun gear 13, on the input shaft 18, on the output shaft 19, on the inner ring of the bearings 17, on the outer ring of the bearings 17, on another revolving member of the gearbox 11 or a combination of different locations.
- the sensors 21 could measure vibration from the different moving or rotating parts of the gearbox 11 but it is also feasible, that the sensors 21 could pick up defect vibrations originating from other parts of the wind turbine 1, such as bearings outside the gearbox 11, the rotor 4 or the generator 9.
- Fig. 6 illustrates an embodiment of a vibration monitoring system for an epicyclic gearbox 11, as seen from the front. • . ' ⁇ ⁇ : .
- a sensor 21 is placed more or less centrally on the planet carrier 15.
- the sensor 21 is connected to a data transmitter 22, which can transmit the sensor signal wirelessly to an external data receiver 23.
- the senor 21 is connected to a data transmitter 22 through hard wiring but in another embodiment 'signals and/or electrical power could be transmitted to and/or from the sensors 21 to and/or from the data transmitter 22 wirelessly.
- the data transmitter 22 could communicate with external data receiver 23 wirelessly.
- the data transmitter 22 could communicate the unprocessed sensor signal continuously or it could transmit the unprocessed sensor signal in certain time intervals or upon receiving a signal from an externally placed request emitter 25 requesting the sensor signal or signals.
- the data transmitter 22 could be battery powered or it could function as a transponder, where the external data receiver 23 or another external source emits an electromagnetic impulse large enough for the data transmitter 22 to produce power enough to feed the sensor 21 and transmit the sensor signal back to the external data receiver 23.
- a transponder solution would render an internal power supply in the data transmitter 22 unnecessary.
- the data transmitter 22 or the sensor 21 or sensors 21 could be connected to the external data receiver 23 directly by means of cables e.g. acting as data conductors and/or supplying the data transmitter 22 or sensors 21 with power.
- This hard wiring would have to pass at least one rotating joint between a rotating shaft and the external data receiver' 23 placed stationary e.g. in the nacelle 3.
- the transmitting of signals, electrical power or other though this rotating joint could e.g. be done by means of a slip ring, a brush connection, a collector or other means for transferring power and/or signals to and from a rotating shaft.
- Fig. 7 illustrates another embodiment of a vibration monitoring system for an epicyclic gearbox 11, as seen from the front.
- the planet carrier 15 is provided with three sensors 21 placed on or in close proximity of the planet gear shafts 16.
- the three sensors 21 are connected to the same data processing unit 24.
- the data processing unit 24 could act as a filter removing noise or undesired short-term fluctuations from the sensor signals or it could compress the sensor signals before they are transmitted to the external data receiver 23.
- the data' processing unit 24 could also analyze the sensor signals and then transmit an alarm signal to the external data receiver 23 if it detects abnormalities e.g. in form of defect frequencies. • i ' . . . , .
- the data processing unit 24 could transmit the filtered or compressed sensor signal or the conclusion of a data analysis continuously, in certain time intervals or upon receiving a signal from an externally placed request emitter 25.
- sensors 21, the data processing unit 24 and the data transmitter 22 are shown as separate individual components connected by conductors but in another embodiment the different components 21, 22, 24 could be integrated in one unit or e.g. the data processing unit 24 and the data transmitter 22 could be integrated in one unit.
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- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2007209631A AU2007209631B2 (en) | 2006-01-25 | 2007-01-25 | A wind turbine comprising at least one gearbox and an epicyclic gearbox |
NZ569819A NZ569819A (en) | 2006-01-25 | 2007-01-25 | A wind turbine comprising at least one gearbox and an epicyclic gearbox |
EP07700169.1A EP1977108B2 (en) | 2006-01-25 | 2007-01-25 | An epicyclic gearbox and a wind turbine comprising at least one epicyclic gearbox |
JP2008551650A JP5094734B2 (en) | 2006-01-25 | 2007-01-25 | Wind turbine comprising at least one gearbox and a planetary gearbox |
ES07700169T ES2676624T5 (en) | 2006-01-25 | 2007-01-25 | An epicyclic gearbox and a wind turbine comprising at least one epicyclic gearbox |
US12/179,061 US8393993B2 (en) | 2006-01-25 | 2008-07-24 | Wind turbine comprising at least one gearbox and an epicyclic gearbox |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DKPA200600114 | 2006-01-25 | ||
DKPA200600114 | 2006-01-25 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/179,061 Continuation US8393993B2 (en) | 2006-01-25 | 2008-07-24 | Wind turbine comprising at least one gearbox and an epicyclic gearbox |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007085259A1 true WO2007085259A1 (en) | 2007-08-02 |
Family
ID=37964360
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DK2007/000035 WO2007085259A1 (en) | 2006-01-25 | 2007-01-25 | A wind turbine comprising at least one gearbox and an epicyclic gearbox |
Country Status (8)
Country | Link |
---|---|
US (1) | US8393993B2 (en) |
EP (1) | EP1977108B2 (en) |
JP (1) | JP5094734B2 (en) |
CN (1) | CN101375053A (en) |
AU (1) | AU2007209631B2 (en) |
ES (1) | ES2676624T5 (en) |
NZ (1) | NZ569819A (en) |
WO (1) | WO2007085259A1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2366989A1 (en) | 2010-03-19 | 2011-09-21 | Eurocopter | Mechanical assembly with means for monitoring structural anomaly, gearbox provided with such mechanical assembly and method for monitoring structural anomaly |
US8043054B2 (en) | 2010-08-25 | 2011-10-25 | General Electric Company | Method and system for monitoring wind turbine |
WO2012126485A1 (en) | 2011-03-22 | 2012-09-27 | Aktiebolaget Skf | Gear with vibration sensor |
WO2014145511A1 (en) * | 2013-03-15 | 2014-09-18 | Digital Wind Systems. Inc. | Method and apparatus for monitoring wind turbine blades during operation |
DK201400518A1 (en) * | 2014-09-11 | 2015-08-24 | Wind Solutions As Kk | Wind turbine blade sensor device |
US9330449B2 (en) | 2013-03-15 | 2016-05-03 | Digital Wind Systems, Inc. | System and method for ground based inspection of wind turbine blades |
US9395337B2 (en) | 2013-03-15 | 2016-07-19 | Digital Wind Systems, Inc. | Nondestructive acoustic doppler testing of wind turbine blades from the ground during operation |
US9453500B2 (en) | 2013-03-15 | 2016-09-27 | Digital Wind Systems, Inc. | Method and apparatus for remote feature measurement in distorted images |
WO2017005238A1 (en) * | 2015-07-07 | 2017-01-12 | Brit Hacke | Device for condition monitoring |
WO2017137586A1 (en) * | 2016-02-12 | 2017-08-17 | Bestsens Ag | Toothing arrangement and method for determining characteristics of a toothing arrangement |
EP3081831B1 (en) | 2015-04-17 | 2017-11-01 | Siemens Aktiengesellschaft | Planetary gear unit |
GB2559808A (en) * | 2017-02-21 | 2018-08-22 | Skf Ab | Instrumented shaft for condition monitoring |
WO2019007601A1 (en) * | 2017-07-04 | 2019-01-10 | Zf Friedrichshafen Ag | Pivotable transmission |
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Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2736236A1 (en) * | 2008-09-06 | 2010-03-11 | Lord Corporation | Motion control system with digital processing link |
US20100097220A1 (en) * | 2008-10-17 | 2010-04-22 | Ge Wind Energy Gmbh | Wireless information system for wind turbine components |
US8742608B2 (en) * | 2009-03-05 | 2014-06-03 | Tarfin Micu | Drive system for use with flowing fluids |
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JP5618319B2 (en) * | 2010-03-16 | 2014-11-05 | Ntn株式会社 | Wind farm monitoring system |
DE102010034749A1 (en) * | 2010-08-19 | 2012-02-23 | Schaeffler Technologies Gmbh & Co. Kg | Device for monitoring a rotating machine part |
US8568099B2 (en) * | 2010-12-17 | 2013-10-29 | Vestas Wind Systems A/S | Apparatus for harvesting energy from a gearbox to power an electrical device and related methods |
CH704874A2 (en) * | 2011-04-26 | 2012-10-31 | Sinell Ag | Transmission for converting rotary movements, gear for such a transmission and use of such gear. |
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EP2696071A1 (en) * | 2012-08-09 | 2014-02-12 | IMO Holding GmbH | Method and device for recognising and monitoring the conditions of modules and components, in particular in wind energy assemblies |
KR101543220B1 (en) | 2014-01-16 | 2015-08-10 | 두산중공업 주식회사 | Power plant operation controlling system amd method using ae sensor |
DE102014206977A1 (en) * | 2014-04-11 | 2015-10-15 | Schaeffler Technologies AG & Co. KG | Weight-optimized planet carrier |
US10309516B2 (en) * | 2015-03-03 | 2019-06-04 | Flender Gmbh | Measuring system and measuring method for detecting variables on planetary carriers of a planetary gear train |
CN104976037A (en) * | 2015-04-23 | 2015-10-14 | 李德生 | Vortex barrier-free intermediate tooth groove power generation device |
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ES2632217B1 (en) * | 2016-03-11 | 2018-07-30 | Wind Power Inside S.L. | Procedure for conducting endoscopy inspection windows executed inside the wind turbine on the closing cover of the planetary stage of wind multipliers |
DE102016204736A1 (en) * | 2016-03-22 | 2017-09-28 | Zf Friedrichshafen Ag | Device for condition monitoring |
US10788394B2 (en) * | 2017-09-12 | 2020-09-29 | General Electric Company | Gearbox sensor arrangement |
US11519820B2 (en) * | 2018-09-19 | 2022-12-06 | Rolls-Royce Deutschland Ltd & Co Kg | Method and device for monitoring a journal bearing |
WO2020258075A1 (en) * | 2019-06-26 | 2020-12-30 | 舍弗勒技术股份两合公司 | Planetary gearbox and bearing clearance monitoring system |
US11780610B2 (en) * | 2019-11-07 | 2023-10-10 | Ge Aviation Systems Limited | Monitoring of a revolving component employing time-synchronized multiple detectors |
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CN114110099A (en) * | 2021-11-30 | 2022-03-01 | 三和技研股份有限公司 | Planetary reducer |
WO2023169783A1 (en) | 2022-03-07 | 2023-09-14 | Sew-Eurodrive Gmbh & Co. Kg | Drive system with planetary gearing |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4239977A (en) * | 1978-09-27 | 1980-12-16 | Lisa Strutman | Surge-accepting accumulator transmission for windmills and the like |
AU672166B3 (en) * | 1994-12-22 | 1996-09-19 | Commonwealth Of Australia, The | Method and apparatus for performing selective signal averaging |
DE19954164A1 (en) * | 1999-11-10 | 2001-06-13 | Fraunhofer Ges Forschung | Sensor for measuring actual condition parameters on surfaces of mechanical components involves using an amorphous carbon layer with piezo-resistive properties |
EP1184567A2 (en) * | 2000-09-01 | 2002-03-06 | Renk Aktiengesellschaft | Gearbox for wind turbines |
EP1612458A2 (en) * | 2004-06-28 | 2006-01-04 | General Electric Company | System and method for monitoring the condition of a drive train |
Family Cites Families (58)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4291233A (en) | 1980-01-29 | 1981-09-22 | Westinghouse Electric Corp. | Wind turbine-generator |
JPS56168520A (en) * | 1980-05-31 | 1981-12-24 | Hitachi Zosen Corp | Detecting method for damage of planetary gear |
JPS5718838A (en) * | 1980-07-09 | 1982-01-30 | Sumitomo Metal Ind Ltd | Measuring uniform load distribution of planetary gear |
GB9122760D0 (en) * | 1991-10-26 | 1991-12-11 | Westland Helicopters | Condition monitoring systems |
JP2957331B2 (en) * | 1991-10-29 | 1999-10-04 | アイシン・エィ・ダブリュ株式会社 | Input rotation detection device for automatic transmission |
ES2166832T5 (en) | 1994-10-07 | 2008-02-16 | Windtec Consulting Gmbh | PLANETARY GEAR FOR A WIND TURBINE. |
US5663600A (en) | 1995-03-03 | 1997-09-02 | General Electric Company | Variable speed wind turbine with radially oriented gear drive |
DE29609794U1 (en) | 1996-06-03 | 1996-08-22 | aerodyn GmbH, 24768 Rendsburg | Gear-generator combination |
IT1293412B1 (en) * | 1997-07-04 | 1999-03-01 | Finmeccanica Spa | Method of surveillance of a planetary unit in a vehicle equipped with accelerometric sensors, in particular in a helicopter. |
JPH1137893A (en) * | 1997-07-18 | 1999-02-12 | Mitsubishi Heavy Ind Ltd | Vibrator for testing torsional vibration |
JP3262046B2 (en) * | 1997-09-17 | 2002-03-04 | トヨタ自動車株式会社 | Method for reducing gear rattle in gear mechanism, power output device, and hybrid vehicle equipped with this power output device |
FR2769396B1 (en) * | 1997-10-02 | 2000-11-10 | Eurocopter France | DEVICE FOR REDUCING THE NOISE OF RAIES INSIDE A ROTATING-SAIL AIRCRAFT, IN PARTICULAR A HELICOPTER |
US6507790B1 (en) * | 1998-07-15 | 2003-01-14 | Horton, Inc. | Acoustic monitor |
US6298725B1 (en) * | 1998-10-02 | 2001-10-09 | Aeronautical And Maritime Research Laboratory, Defence Science And Technology Organisation | Method for the separation of epicyclic planet gear vibration signatures |
DE19916453A1 (en) | 1999-04-12 | 2000-10-19 | Flender A F & Co | Wind turbine |
US6304002B1 (en) | 2000-04-19 | 2001-10-16 | Dehlsen Associates, L.L.C. | Distributed powertrain for high torque, low electric power generator |
DE10023961B4 (en) | 2000-05-16 | 2006-10-19 | Sew-Eurodrive Gmbh & Co. Kg | System for measuring physical quantities on an axle or rotatable shaft |
DE10064815A1 (en) | 2000-12-22 | 2002-07-11 | Zahnradfabrik Friedrichshafen | planetary gear |
WO2002069316A2 (en) * | 2001-02-27 | 2002-09-06 | Sikorsky Aircraft Corporation | System for computationally efficient active control of tonal sound or vibration |
DE10114609A1 (en) | 2001-03-23 | 2002-09-26 | Enron Wind Gmbh | Torque transmission device for a wind turbine |
JP2002303254A (en) | 2001-04-05 | 2002-10-18 | Mitsubishi Heavy Ind Ltd | Wind power generator |
WO2002095633A2 (en) | 2001-05-24 | 2002-11-28 | Simmonds Precision Products, Inc. | Method and apparatus for determining the health of a component using condition indicators |
DE10134245A1 (en) | 2001-07-18 | 2003-02-06 | Winergy Ag | Gearbox with power distribution |
GB2382117B (en) | 2001-10-05 | 2005-07-20 | Hansen Transmissions Int | Wind turbine gear unit lubrication |
DE10159973A1 (en) | 2001-12-06 | 2003-06-18 | Winergy Ag | Gearbox for a wind turbine |
US6731017B2 (en) | 2002-06-03 | 2004-05-04 | Clipper Windpower Technology, Inc. | Distributed powertrain that increases electric power generator density |
DE10242707B3 (en) | 2002-09-13 | 2004-04-15 | Aerodyn Engineering Gmbh | Wind turbine with concentric gear / generator arrangement |
DE10250382A1 (en) | 2002-10-29 | 2004-05-19 | Siemens Ag | Three-phase asynchronous |
DE10254527A1 (en) | 2002-11-22 | 2004-06-09 | Multibrid Entwicklungsges. Mbh | Process for low-loss torque transmission in planetary gears |
EP1588138A1 (en) * | 2003-01-24 | 2005-10-26 | The Commonwealth of Australia as represented by the Defence Science and Technology Organisation of the Department of Defence | Synchronous averaging of epicyclic sun gear vibration |
DE10318945B3 (en) | 2003-04-26 | 2004-10-28 | Aerodyn Gmbh | Planetary gearing, for a wind energy generator, has a bearing structure where the load from the external rotor is minimized on the bearings and gear components to increase their life |
US7042110B2 (en) | 2003-05-07 | 2006-05-09 | Clipper Windpower Technology, Inc. | Variable speed distributed drive train wind turbine system |
US7069802B2 (en) | 2003-05-31 | 2006-07-04 | Clipper Windpower Technology, Inc. | Distributed power train (DGD) with multiple power paths |
DE10325667A1 (en) | 2003-06-06 | 2005-03-03 | Fag Kugelfischer Ag & Co. Ohg | Roller bearing rotating component sensor system uses SAW and BAW sensor with responses transmitted through shared antenna as frequency separated narrow band signals |
JP2005189058A (en) * | 2003-12-25 | 2005-07-14 | Nsk Ltd | Impact sensor unit |
DE102004005543A1 (en) | 2004-02-04 | 2005-09-01 | Siemens Ag | Wind turbine |
US7140994B2 (en) | 2004-06-18 | 2006-11-28 | Paccar Inc | Gearbox torsional load sensor |
US7154191B2 (en) | 2004-06-30 | 2006-12-26 | General Electric Company | Electrical machine with double-sided rotor |
DE102004046563B4 (en) | 2004-09-24 | 2008-01-03 | Aerodyn Energiesysteme Gmbh | Wind energy plant with fully integrated machine set |
US7822560B2 (en) * | 2004-12-23 | 2010-10-26 | General Electric Company | Methods and apparatuses for wind turbine fatigue load measurement and assessment |
US20060265175A1 (en) * | 2005-05-09 | 2006-11-23 | Manuchehr Shimohamadi | Low-cost multi-span conductor temperature measurement system |
ES2274696B1 (en) | 2005-06-13 | 2008-05-01 | GAMESA INNOVATION & TECHNOLOGY, S.L. | WIND TURBINE. |
JP4849880B2 (en) * | 2005-12-07 | 2012-01-11 | 株式会社ハーモニック・ドライブ・システムズ | Method for assembling detection mechanism of planetary gear device |
KR100765087B1 (en) * | 2006-12-01 | 2007-10-09 | 현대모비스 주식회사 | Steering angle sensor assembly in vehicle |
DE102006057055B3 (en) | 2006-12-04 | 2008-06-19 | Lohmann & Stolterfoht Gmbh | Power-split wind turbine gearbox |
EP2108082B1 (en) | 2007-01-31 | 2016-07-20 | Vestas Wind Systems A/S | A wind turbine with a drive train |
DE102007012408A1 (en) | 2007-03-15 | 2008-09-18 | Aerodyn Engineering Gmbh | Wind turbines with load-transmitting components |
US7854591B2 (en) | 2007-05-07 | 2010-12-21 | Siemens Energy, Inc. | Airfoil for a turbine of a gas turbine engine |
US7538446B2 (en) | 2007-06-21 | 2009-05-26 | General Electric Company | Gear integrated generator for wind turbine |
US7935020B2 (en) | 2007-08-27 | 2011-05-03 | General Electric Company | Integrated medium-speed geared drive train |
DE102007049599A1 (en) | 2007-10-15 | 2009-05-07 | Innovative Windpower Ag | Temperature control of coupled gearbox and generator in a wind turbine |
ES2341373T3 (en) | 2007-12-19 | 2010-06-18 | GAMESA INNOVATION & TECHNOLOGY, S.L. | MULTIPLYING UNIT OF PLANETARY TYPE THAT INCLUDES A PORTASATELITES WITH A PLANETARY BOGIE PLATE. |
ATE555332T1 (en) | 2007-12-19 | 2012-05-15 | Gamesa Innovation & Tech Sl | PLANETARY CARRIER FOR A PLANETARY STAGE WITH TURNING PLATE. |
DK2075466T3 (en) | 2007-12-28 | 2012-05-29 | Zf Wind Power Antwerpen Nv | Method of connecting a low-speed main shaft of a wind turbine to an input shaft of the wind turbine transmission gearbox and a connection obtained by this method |
DE102008049530A1 (en) * | 2008-09-29 | 2010-04-01 | Prüftechnik Dieter Busch AG | A method of monitoring a powertrain component of a wind turbine |
US7970556B2 (en) * | 2009-01-30 | 2011-06-28 | General Electric | System and method for monitoring the condition of a gear assembly |
DE102010009634B4 (en) * | 2010-02-27 | 2018-07-12 | Schaeffler Technologies AG & Co. KG | A method for setting and measuring a bias of a radially arranged between a planetary gear and a planet carrier bearing assembly |
FR2957668B1 (en) * | 2010-03-19 | 2012-10-19 | Eurocopter France | MECHANICAL ASSEMBLY HAVING STRUCTURAL ANOMALY MONITORING MONITOR, TRANSMISSION BOX PROVIDED WITH SUCH A MECHANICAL ASSEMBLY, AND METHOD FOR MONITORING STRUCTURAL ANOMALY |
-
2007
- 2007-01-25 CN CNA2007800035545A patent/CN101375053A/en active Pending
- 2007-01-25 WO PCT/DK2007/000035 patent/WO2007085259A1/en active Application Filing
- 2007-01-25 NZ NZ569819A patent/NZ569819A/en unknown
- 2007-01-25 ES ES07700169T patent/ES2676624T5/en active Active
- 2007-01-25 AU AU2007209631A patent/AU2007209631B2/en not_active Ceased
- 2007-01-25 JP JP2008551650A patent/JP5094734B2/en active Active
- 2007-01-25 EP EP07700169.1A patent/EP1977108B2/en active Active
-
2008
- 2008-07-24 US US12/179,061 patent/US8393993B2/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4239977A (en) * | 1978-09-27 | 1980-12-16 | Lisa Strutman | Surge-accepting accumulator transmission for windmills and the like |
AU672166B3 (en) * | 1994-12-22 | 1996-09-19 | Commonwealth Of Australia, The | Method and apparatus for performing selective signal averaging |
DE19954164A1 (en) * | 1999-11-10 | 2001-06-13 | Fraunhofer Ges Forschung | Sensor for measuring actual condition parameters on surfaces of mechanical components involves using an amorphous carbon layer with piezo-resistive properties |
EP1184567A2 (en) * | 2000-09-01 | 2002-03-06 | Renk Aktiengesellschaft | Gearbox for wind turbines |
EP1612458A2 (en) * | 2004-06-28 | 2006-01-04 | General Electric Company | System and method for monitoring the condition of a drive train |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2957668A1 (en) * | 2010-03-19 | 2011-09-23 | Eurocopter France | MECHANICAL ASSEMBLY HAVING STRUCTURAL ANOMALY MONITORING MONITOR, TRANSMISSION BOX PROVIDED WITH SUCH A MECHANICAL ASSEMBLY, AND METHOD FOR MONITORING STRUCTURAL ANOMALY |
US8777800B2 (en) | 2010-03-19 | 2014-07-15 | Airbus Helicopters | Mechanical assembly provided with means for monitoring for a structural anomaly, a gearbox provided with such a mechanical assembly, and a method of monitoring for a structural anomaly |
EP2366989A1 (en) | 2010-03-19 | 2011-09-21 | Eurocopter | Mechanical assembly with means for monitoring structural anomaly, gearbox provided with such mechanical assembly and method for monitoring structural anomaly |
US8043054B2 (en) | 2010-08-25 | 2011-10-25 | General Electric Company | Method and system for monitoring wind turbine |
DE102011052894B4 (en) | 2010-08-25 | 2022-03-03 | General Electric Company | System for monitoring a wind turbine |
WO2012126485A1 (en) | 2011-03-22 | 2012-09-27 | Aktiebolaget Skf | Gear with vibration sensor |
US9652839B2 (en) | 2013-03-15 | 2017-05-16 | Digital Wind Systems, Inc. | System and method for ground based inspection of wind turbine blades |
WO2014145511A1 (en) * | 2013-03-15 | 2014-09-18 | Digital Wind Systems. Inc. | Method and apparatus for monitoring wind turbine blades during operation |
US9194843B2 (en) | 2013-03-15 | 2015-11-24 | Digital Wind Systems, Inc. | Method and apparatus for monitoring wind turbine blades during operation |
US9330449B2 (en) | 2013-03-15 | 2016-05-03 | Digital Wind Systems, Inc. | System and method for ground based inspection of wind turbine blades |
US9395337B2 (en) | 2013-03-15 | 2016-07-19 | Digital Wind Systems, Inc. | Nondestructive acoustic doppler testing of wind turbine blades from the ground during operation |
US9453500B2 (en) | 2013-03-15 | 2016-09-27 | Digital Wind Systems, Inc. | Method and apparatus for remote feature measurement in distorted images |
DK201400518A1 (en) * | 2014-09-11 | 2015-08-24 | Wind Solutions As Kk | Wind turbine blade sensor device |
EP3081831B1 (en) | 2015-04-17 | 2017-11-01 | Siemens Aktiengesellschaft | Planetary gear unit |
US10400880B2 (en) | 2015-04-17 | 2019-09-03 | Flender Gmbh | Planetary transmission |
EP3268635B1 (en) * | 2015-04-17 | 2020-11-11 | Flender GmbH | Planetary gear unit |
WO2017005238A1 (en) * | 2015-07-07 | 2017-01-12 | Brit Hacke | Device for condition monitoring |
WO2017137586A1 (en) * | 2016-02-12 | 2017-08-17 | Bestsens Ag | Toothing arrangement and method for determining characteristics of a toothing arrangement |
US20190033168A1 (en) * | 2016-02-12 | 2019-01-31 | Bestsens Ag | Toothing arrangement and method for determining characteristics of a toothing arrangement |
EP3404778A4 (en) * | 2016-12-08 | 2019-03-20 | Beijing Goldwind Science & Creation Windpower Equipment Co., Ltd. | Conductive ring assembly, conductive device and wind turbine |
AU2017370496B2 (en) * | 2016-12-08 | 2019-09-26 | Beijing Goldwind Science & Creation Windpower Equipment Co., Ltd. | Conductive ring assembly, conductive device and wind turbine |
US11236731B2 (en) | 2016-12-08 | 2022-02-01 | Beijing Goldwind Science & Creation Windpower Equipment Co., Ltd. | Conductive ring assembly, conductive device and wind turbine |
GB2559808A (en) * | 2017-02-21 | 2018-08-22 | Skf Ab | Instrumented shaft for condition monitoring |
WO2019007601A1 (en) * | 2017-07-04 | 2019-01-10 | Zf Friedrichshafen Ag | Pivotable transmission |
CN110869643A (en) * | 2017-07-04 | 2020-03-06 | Zf 腓德烈斯哈芬股份公司 | Pivotable transmission |
Also Published As
Publication number | Publication date |
---|---|
AU2007209631B2 (en) | 2010-03-18 |
NZ569819A (en) | 2010-07-30 |
ES2676624T5 (en) | 2022-07-06 |
ES2676624T3 (en) | 2018-07-23 |
EP1977108A1 (en) | 2008-10-08 |
US8393993B2 (en) | 2013-03-12 |
AU2007209631A1 (en) | 2007-08-02 |
EP1977108B1 (en) | 2018-06-13 |
JP2009524760A (en) | 2009-07-02 |
US20080279686A1 (en) | 2008-11-13 |
EP1977108B2 (en) | 2022-05-18 |
JP5094734B2 (en) | 2012-12-12 |
CN101375053A (en) | 2009-02-25 |
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