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 PDF

Info

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
Authority
WO
WIPO (PCT)
Prior art keywords
sensors
gearbox
data
wind turbine
epicyclic gearbox
Prior art date
Application number
PCT/DK2007/000035
Other languages
French (fr)
Inventor
Jens DEMTRÖDER
Original Assignee
Vestas Wind Systems A/S
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=37964360&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2007085259(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Vestas Wind Systems A/S filed Critical Vestas Wind Systems A/S
Priority to AU2007209631A priority Critical patent/AU2007209631B2/en
Priority to NZ569819A priority patent/NZ569819A/en
Priority to EP07700169.1A priority patent/EP1977108B2/en
Priority to JP2008551650A priority patent/JP5094734B2/en
Priority to ES07700169T priority patent/ES2676624T5/en
Publication of WO2007085259A1 publication Critical patent/WO2007085259A1/en
Priority to US12/179,061 priority patent/US8393993B2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D15/00Transmission of mechanical power
    • F03D15/10Transmission of mechanical power using gearing not limited to rotary motion, e.g. with oscillating or reciprocating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D15/00Transmission of mechanical power
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D17/00Monitoring or testing of wind motors, e.g. diagnostics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D80/00Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/70Bearing or lubricating arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/40Transmission of power
    • F05B2260/403Transmission of power through the shape of the drive components
    • F05B2260/4031Transmission of power through the shape of the drive components as in toothed gearing
    • F05B2260/40311Transmission of power through the shape of the drive components as in toothed gearing of the epicyclic, planetary or differential type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/80Diagnostics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00Control
    • F05B2270/80Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05B2270/807Accelerometers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00Control
    • F05B2270/80Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05B2270/81Microphones
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/01Monitoring wear or stress of gearing elements, e.g. for triggering maintenance
    • F16H2057/012Monitoring wear or stress of gearing elements, e.g. for triggering maintenance of gearings
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind 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.

Landscapes

  • 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

The invention relates to a wind turbine (1) comprising at least one gearbox (7). The gearbox (7) comprises one or more sensors (21) for measuring condition values of the wind turbine (1) and is characterized in that the one or more sensors (21) are mounted on one or more rotating parts of the gearbox (7). The invention further relates to an epicyclic gearbox (11) comprising a gearbox housing (20), one or more gearbox parts rotating in relation to the housing (20), and one or more sensors (21) for measuring condition values of the gearbox (11). The epicyclic gearbox (11) is characterized in that, the one or more sensors (21) are mounted on one or more of the rotating parts of the gearbox (11).

Description

A WIND TURBINE COMPRISING AT LEAST ONE GEARBOX AND AN EPICYCLIC GEARBOX
Background of the invention
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.
Description of the Related Art
Monitoring the condition of gearboxes, motors, transmissions and other electrical and/or mechanical components comprising parts which rotates during use are well known. Particularly wind turbine gearboxes used in remote installations, such as in an off-shore wind turbine operating without permanent supervision, vibration monitoring techniques have proven very efficient for detecting problems at an early stage, hereby making it possible to initiate preventive maintenance or repair before any major damage occurs.
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.
In worst case, 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.
It is therefore known to provide the gearbox housing with one or more accelerometers or microphones for monitoring the condition of the gears and bearings. The output from these sensors is then filtered, using more or less complex methods, in order to be able to' identify damage or potentially destructive conditions.
But in gearboxes such as epicyclic gearboxes; where rotating parts rotate on other rotating parts, the relatively small vibrations amplitudes of initial damage can easily be modulated e.g. by heavy gear impacts, hereby making it very difficult to pick up or identify the significant frequencies.
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.
Furthermore, it is an object of the invention to provide for a technique for improving the detection of both initial and secondary damage in epicyclic gearboxes.
The invention ' ;
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.
Placing 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.
Furthermore, positioning the sensors on the rotating parts of the gearbox creates a more direct transmission path for structure-born noise or vibrations generated by a possible defect, hereby enabling that small initial damage is detected before it causes any major damage. Additionally; the earlier a possible defect is detected the higher the chances are that there is time to initiate preventive maintenance, without having to shut down the entire wind turbine.
In an aspect of the invention, 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.
In an aspect of the invention, said one or more sensors are mounted on or in close proximity of one or more of said at least two planet gear shafts.
It is advantageous to place the sensors on or in close proximity of the planet gear shafts, in that the shafts in most epicyclic gearboxes are easily accessible and in that at least parts of the planet gear shafts are hot exposed to gear oil.
Furthermore, the planet gears mounted on the shafts at some point gets in contact with most of the other gears in the epicyclic gearbox, hereby ensuring that a defect is detected early. • ■ ' ' '' ■
In an aspect of the invention, 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.
Furthermore, through the planet gear shafts, 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.
In an aspect of the invention, 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.
In an aspect of the invention, 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.
In an aspect of the invention, said one or more sensors are one or more accelerometers and/or one or more microphones.
Using 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. i
It should be emphasized that the term "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.
In an aspect of the invention, 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. ; . ■ ■
In an aspect of the invention, said 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. , , ,
In an aspect of the invention, said one or more data transmitters are mounted on said one or more rotating parts of said gearbox.
Placing the data transmitters on a rotating part in gearbox is advantageous, in that the data transmitters then is positioned in close proximity of the sensors.
In an aspect of the invention, 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.
In an aspect of the invention, 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.
In an aspect of the invention, said one or more data transmitters comprise means for transmitting data upon receiving a request from an externally positioned request emitter.
Making the data transmitter transmit data only when receiving a request from an externally positioned request emitter is advantageous, in that by this is possible to reduce the data transmission and by this reducing the power consumption of the sensors and transmitters inside the gearbox. 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.
In an aspect of the invention, 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.
In an aspect of the invention, 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.
In an aspect of the invention, said one or more data transmitters comprise a 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.
In an aspect of the invention, 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.
In an aspect of the invention, 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.
In an aspect of the invention, said one or more data processing units are mounted on said one or more rotating parts of said gearbox.
Placing the data processing unit on the rotating parts in the gearbox is advantageous, in that it hereby is easy to connect the sensors and/or data transmitters to the data processing unit, without having to provide; cables over rotating joints.
Furthermore it would be quit difficult to, transmit all the raw data from the sensors to an externally placed data processing unit. First of all because the shear amount of data would require a large bandwidth and require relatively much power to be transmitted, secondly because' of the risk of loss or signal noise could reduce the data quality. If the data are process in the gearbox e.g. only an on-off alarm signal would need to be transmitted in case of a problem being detected. . -• ■ ■ , . . , • ■ ■ ■ • ;
In an aspect of the invention, 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.
In an aspect of the invention, 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. ' • : . . - . '■ ■ : i 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.
In an aspect of the invention, said one or more data processing units comprise means for generating an alarm signal when detecting a defect in said gearbox.
Making the data processing unit generate an alarm signal when detecting a defect is advantageous, in that this signal could be much simpler than e.g. a constant sensor signal, hereby reducing the risk of data being lost and thereby increasing the reliability of the system. ■ . . ;. . - .
In an aspect of the invention,;' 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.
In an aspect of the invention, said one or more data processing units comprise means for compressing the data of said One or more sensors measurements.
It is advantageous to compress the data, in that because of the reduced amount of data, a possible data transmission can be made more simple and reliable. ■ ■ ; ' . . • • ■ ■ ■ In an aspect of the invention, 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.
In an aspect of the invention, 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.
In an aspect of the invention, 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.
Compared to other gearbox types, 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.
There is a relatively large risk of defect vibrations, originating from a rotating or a "double" rotating gear, being lost if the sensors are placed on a fixed member an epicyclic gearbox. Placing the sensors on one or more rotating parts of an epicyclic therefore creates a more direct transmission path for structure-born vibrations originating from possible defects, hereby increasing the sensors functionality and reliability.
In an aspect of the invention, said one or more sensors are mounted on or in close proximity of one or more planet gear shafts of said epicyclic gearbox.
In an aspect of the invention, said one or more sensors are mounted on at least one planet carrier of said epicyclic gearbox.
In an aspect of the invention, each of said at least one planet carrier comprise only one sensor.
In an aspect of the invention, said one or more sensors comprise means for measuring vibrations and/or acoustic emission.
In an aspect of the invention, said one or more sensors are one or more accelerometers and/or one or more microphones.
In an aspect of the invention, said one or more sensors are connected to one or more data transmitters for transmitting data to an external data receiver.
In an aspect of the invention, said one or more data transmitters are mounted on said one or more rotating parts of said epicyclic gearbox. In an aspect of the invention, more than one of said one or more sensors are connected to the same data transmitter.
In an aspect of the invention, said one or more data transmitters comprise means for transmitting data continuously during operation of said epicyclic gearbox.
In an aspect of the invention, said one or more data transmitters comprise means for transmitting data upon receiving a request from an externally positioned request emitter.
In an aspect of the invention, said one or more data transmitters comprise means for transmitting said sensors measurements wirelessly.
In an aspect of the invention, said one or more data transmitters comprise a transponder.
In an aspect of the invention, said one or more data transmitters and said one or more sensors are formed integrally as one unit. >
In an aspect of the invention, said one or more sensors are connected to one or more data processing units. •
In an aspect of the invention, said one or more data processing units are mounted on said one or more rotating parts of said gearbox.
In an aspect of the invention, more than one of said one or more sensors are connected to the same data processing unit. In an aspect of the invention, 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.
In an aspect of the invention, said one or more data processing units comprise means for generating an alarm signal when detecting a defect in said epicyclic gearbox.
In an aspect of the invention, said one or more data processing units comprise means for filtering said one or more sensors measurements.
In an aspect of the invention, said one or more data processing units comprise means for compressing the data of said one or more sensors measurements.
In an aspect of the invention, said one or more data processing units and said one or more data transmitters are formed integrally as one unit.
In an aspect of the invention, said one or more data processing units and said one or more sensors are formed integrally as one unit.
In an aspect of the invention, said one or more sensors are mounted in one or more planet gear shafts of said epicyclic gearbox.
Figures
The invention will be described in the following with reference to the figures in which
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.
Detailed description
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. In this embodiment 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. In another embodiment 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.
Because of the limited space in the nacelle 3 and to minimize the weight of the nacelle 3 the preferred 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.
In this embodiment 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. Typically 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. Furthermore., 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. a first stage where the sun gear 13 is missing and the input shaft 18 rotates the annulus gear 14, which mesh with a number of planet gears 12. The planet gears 12 of the first stages is then connected to planet gears 12 of a larger size in a second stage, which mesh with a sun gear 13, which is connected to the output shaft 19 of the gearbox 11. Other gearbox 11 designs are also feasible often depending on what the gearbox 11 is to be used for. In wind turbines 1 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.
In this embodiment of the invention 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. be mounted on the outside of the annulus gear 4 and the outer ring of the bearing could be connected to the planet carrier 15, which then would extend beyond the annulus gear 14, or a more or less circular planet carrier 15 could be provided with a bearing' around its outer perimeter, where the outer ring of the bearing was connected to the:annulus gear 14, the gearbox housing 20 or in other ways fixed. . . . . ■ ! . . Fig. 5 illustrates a part of a cross section of an embodiment of an epicyclic gearbox 11, as seen from the side. In this, embodiment of a epicyclic gearbox 11 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.
In this embodiment of the invention 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.
In another embodiment of the invention 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
21, but in another embodiment of the invention 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. . ' ■ ■ : .
In this embodiment of the invention 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.
In this embodiment the sensor 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.
In this embodiment of the invention 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.
In another embodiment of the invention 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.
In this embodiment of the invention 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.
In this embodiment of the invention the, 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.
The invention has been exemplified above with reference to specific examples of vibration sensors 21 mounted on the rotating parts of gearboxes 7, 11. However, it should be understood that the invention is not limited to the particular examples described above but may be designed and altered in a multitude of varieties within the scope of the invention as specified in the claims.
List
1. Wind turbine
2. Tower
3. Nacelle
4. Rotor
5. Blade
6. Low speed shaft
7. Gearbox
8. Teeter mechanism
9. Generator
10. High speed shaft
11. Epicyclic gearbox
12. Planet gear
13. Sun gear
14. Annulus gear
15. Planet carrier
16. Planet gear shaft
17. Planet gear bearing
18. Input shaft
19. Output shaft
20. Gearbox housing
21. Sensor
22. Data transmitter
23. External data receiver
24. Data processing unit
25. Request emitter

Claims

Claims
1. A wind turbine (1) comprising at least one gearbox (7), said gearbox (7) comprising
one or more sensors (21) for measuring condition values of the wind turbine (1),
characterized in that
said one or more sensors (21) are mounted on one or more rotating parts of said gearbox (7).
2. A wind turbine (1) according to claim 1, wherein said at least one gearbox (7) is an epicyclic gearbox (11) comprising at least two planet gears (12) each including a planet gear shaft (16), said epicyclic gearbox (11) further comprising at least one planet carrier (15) connecting said planet gears (12).
3. A wind turbine (1) according to claim 2, wherein said one or more sensors (21) are mounted on or in close proximity of one or more' of said at least two planet gear shafts (16).
4. A wind turbine (1) according to claim 2 or 3, wherein said one or more sensors (21) are mounted on said at least one planet carrier (15).
5. A wind turbine (1) according to claim 4, wherein each of said at least one planet carrier (15) comprise only one sensor (21).
6. A wind turbine (1) according to any of the preceding claims, wherein said one or more sensors (21) comprise means for measuring vibrations and/or acoustic emission.
7. A wind turbine (1) according to any of the preceding claims, wherein said one or more sensors (21) are one or more accelerometers and/or one or more microphones.
8. A wind turbine (1) according to any of the preceding claims, wherein said one or more sensors (21) are connected to one or more data transmitters (22) for transmitting data to an external data receiver (23).
9. A wind turbine (1) according to claim 8, wherein said connection is made wirelessly.
10. A wind turbine (1) according to claim 8 or 9, wherein said one or more data transmitters (22) are mounted on said one or more rotating parts of said gearbox (7).
11. A wind turbine ( 1 ) according to claim 8 to 10, wherein more than one of said one or more sensors (21) are connected to the same data transmitter (22).
12. A wind turbine (1) according to any of claims 8 to 11, wherein said one or more data transmitters (22) comprise means for transmitting data continuously during operation of said gearbox (7).
13. A wind turbine (1) according. to any of claims 8 to 11, wherein said one or more data transmitters (22) comprise means for transmitting data upon receiving a request from an externally positioned request emitter (25).
14. A wind turbine (1) according to any of claims 8 to 13, wherein said one or more data transmitters (22) are hard wired to said external data receiver (23) e.g. through a slip ring or brush connection.
15. A wind turbine (1) according to any of claims 8 to 13, wherein said one or more data transmitters (22) comprise means for transmitting said sensors (21) measurements wirelessly.
16. A wind turbine (1) according to any of claims 8 to 15, wherein said one or more data transmitters (22) comprise a transponder.
17. A wind turbine (1) according to any of claims 8 to 16, wherein said one or more data transmitters (22) and said one or more sensors (21) are formed integrally as one unit.
18. A wind turbine (1) according to any of the preceding claims, wherein said one or more sensors (21) are connected to one or more data processing units (24).
19. A wind turbine (1) according to claim 18, wherein said one or more data processing units (24) are mounted on said one or more rotating parts of said gearbox (7).
20. A wind turbine (1) according to claim 18 or 19, wherein more than one of said one or more sensors (21) are connected to the same data processing unit (24).
21. A wind turbine (1) according to any of claims 18 to 20, wherein said one or more data processing units (24) comprise means for detecting defects in said gearbox (7) based on the measurements of said one or more sensors (21).
22. A wind turbine (1) according to claim 21, wherein said one or more data processing units (24) comprise means for generating an alarm signal when detecting a defect in said gearbox (7).
23. A wind turbine (1) according to any of claims 18 to 22, wherein said one or more data processing units (24) comprise means for filtering said one or more sensors (21) measurements.
24. A wind turbine (1) according to any of claims 18 to 23, wherein said one or more data processing units (24) comprise means for compressing the data of said one or more sensors (21) measurements.
25. A wind turbine (1) according to any of claims 18 to 24, wherein said one or more data processing units (24) and said one or more data transmitters (22) are formed integrally as one unit.
26. A wind turbine (1) according to any of claims 18 to 25, wherein said one or more data processing units (24) and said one or more sensors (21) are formed integrally as one unit.
27. A wind turbine (1) according to claim 2, wherein said one or more sensors (21) are mounted in one or more of said at least two planet gear shafts (16).
28. An epicyclic gearbox (11) comprising
a gearbox housing (20),
one or more gearbox parts rotating in relation to said housing (20), and
one or more sensors (21) for measuring condition values of said gearbox (11),
characterized in that said one or more sensors (21) are mounted on one or more of said rotating parts of said gearbox (11).
29. An epicyclic gearbox (11) according to claim 28, wherein said one or more sensors (21) are mounted on or in close proximity of one or more planet gear shafts
(16) of said epicyclic gearbox (11).
30. An epicyclic gearbox (11) according to claim 28 or 29, wherein said one or more sensors (21) are mounted on at least one planet carrier (15) of said epicyclic gearbox (11).
31. An epicyclic gearbox (11) according to claim 30, wherein each of said at least one planet carrier (15) comprise only one sensor (21).
32. An epicyclic gearbox (11) according to any of claims 28 to 31, wherein said one or more sensors (21) comprise means for measuring vibrations and/or acoustic emission.
33. An epicyclic gearbox (11) according to any of claims 28 to 32, wherein said one or more sensors (21) are one or more accelerometers and/or one or more microphones.
34. An epicyclic gearbox (11) according to any of claims 28 to 33, wherein said one or more sensors (21) are connected to one or more data transmitters (22) for transmitting data to an external data receiver (23).
35. An epicyclic gearbox (11) according to claim 34, wherein said connection is made wirelessly.
36. An epicyclic gearbox (11) according to claim 34 or 35, wherein said one or more data transmitters (22) are mounted on said one or more rotating parts of said epicyclic gearbox (11).
37. An epicyclic gearbox (11) according to any of claims 34 to 36, wherein more than one of said one or more sensors (21) are connected to the same data transmitter (22).
38. An epicyclic gearbox (11) according to any of claims 34 to 37, wherein said one or more data transmitters (22) comprise means for transmitting data continuously during operation of said epicyclic gearbox (11).
39. An epicyclic gearbox (11) according to any of claims 34 to 37, wherein said one or more data transmitters (22) comprise means for transmitting data upon receiving a request from an externally positioned request emitter (25).
40. An epicyclic gearbox (11) according to any of claims 34 to 39, wherein said one or more data transmitters (22) are 'hard wired to said external data receiver (23) e.g. through a slip ring or brush connection.
41. An epicyclic gearbox (11) according to any of claims 34 to 39, wherein said one or more data transmitters (22) comprise means for transmitting said sensors (21) measurements wirelessly.
42. An epicyclic gearbox (11) according to any of claims 34 to 41, wherein said one or more data transmitters (22) comprise a transponder.
43. An epicyclic gearbox (11) according to any of claims 34 to 42, wherein said one or more data transmitters (22) and said one or more sensors (21) are formed integrally as one unit. •
44. An epicyclic gearbox (11) according to any of claims 28 to 43, wherein said one or more sensors (21) are connected to one or more data processing units (24).
45. An epicyclic gearbox (11) according to claim 44, wherein said one or more data processing units (24) are mounted on said one or more rotating parts of said gearbox (11).
46. An epicyclic gearbox (11) according to claim 44 or 45, wherein more than one of said one or more sensors (21) are connected to the same data processing unit (24).
47. An epicyclic gearbox (11) according to any of claims 44 to 46, wherein said one or more data processing units (24) comprise means for detecting defects in said epicyclic gearbox (11) based on the measurements of said one or more sensors (21).
48. An epicyclic gearbox (11) according to claim 47, wherein said one or more data processing units (24) comprise means for generating an alarm signal when detecting a defect in said epicyclic gearbox (11).
49. An epicyclic gearbox (11) according to any of claims 44 to 48, wherein said one or more data processing units (24) comprise means for filtering said one or more sensors (21) measurements.
50. An epicyclic gearbox (11) according to any of claims 44 to 49, wherein said one or more data processing units (24) comprise means for compressing the data of said one or more sensors (21) measurements.
51. An epicyclic gearbox (11) according to any of claims 44 to 50, wherein said one or more data processing units (24) and said one or more data transmitters (22) are formed integrally as one unit.
52. An epicyclic gearbox (11) according to any of claims 44 to 51, wherein said one or more data processing units (24) and said one or more sensors (21) are formed integrally as one unit.
53. An epicyclic gearbox (11) according to claim 28, wherein said one or more sensors (21) are mounted in one or more planet gear shafts (16) of said epicyclic gearbox (11).
PCT/DK2007/000035 2006-01-25 2007-01-25 A wind turbine comprising at least one gearbox and an epicyclic gearbox WO2007085259A1 (en)

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)

* Cited by examiner, † Cited by third party
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
EP3404778A4 (en) * 2016-12-08 2019-03-20 Beijing Goldwind Science & Creation Windpower Equipment Co., Ltd. Conductive ring assembly, conductive device and wind turbine

Families Citing this family (31)

* Cited by examiner, † Cited by third party
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
GB0904913D0 (en) * 2009-03-24 2009-05-06 Rolls Royce Plc A mechanical arrangement
US20120299747A1 (en) * 2009-11-13 2012-11-29 Schaeffler Technologies AG & Co. KG Remote condition monitoring system and method
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.
ES2836803T3 (en) * 2011-08-05 2021-06-28 Zf Wind Power Antwerpen Nv Platform multiplier box for wind turbines
US20130043683A1 (en) 2011-08-17 2013-02-21 Vincent Genovese Fluid driven energy conversion apparatus and method
US8851839B2 (en) * 2011-08-23 2014-10-07 Charles Franklin ECKART Wide blade multiple generator wind turbine
JP5680526B2 (en) * 2011-12-28 2015-03-04 三菱重工業株式会社 Impact load monitoring system and impact load monitoring method for wind turbine for wind power generation
KR101275702B1 (en) 2012-02-15 2013-06-17 목포대학교산학협력단 Method and apparatus for fault diagnosis and fault detection of gearbox using vibration signal
DK2657519T3 (en) * 2012-04-26 2015-09-07 Siemens Ag Windmill
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
CN104976038A (en) * 2015-04-23 2015-10-14 李德生 Vortex barrier-free intermediate tooth spiral ring power generation device
CN105545610B (en) * 2016-03-11 2017-12-05 李勇强 Total power speed-increasing type impeller and architecture system
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
CN111734815A (en) * 2020-07-27 2020-10-02 江苏恒减传动设备有限公司 Double-horizontal-shaft stirring speed reducer
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
EP1977108B1 (en) An epicyclic gearbox and a wind turbine comprising at least one epicyclic gearbox
CN102713554B (en) The apparatus for diagnosis of abnormality of rolling bearing, wind power generation plant and abnormity diagnostic system
US20150177100A1 (en) Method and apparatus for detecting and monitoring states
JP6250345B2 (en) Monitoring system and monitoring method
CN107429818B (en) Measuring system and measuring method for detecting a variable on a planet carrier of a planetary gear
EP1182442A2 (en) Bearing vibration diagnostic apparatuses and methods of detecting vibration of bearings
US10487805B2 (en) Instrumented shaft for condition monitoring
CN203673317U (en) Fan condition monitoring system
CN111594396A (en) Wind turbine generator system state monitoring system
US20140318226A1 (en) Method and calculator unit for determining total damage to at least one rotating component of a drive train
CN115371992A (en) System and method for monitoring component failure in a gear train based system
EP3444576B1 (en) Systems and methods for detecting damage in rotary machines
JP6577394B2 (en) Abnormality diagnosis equipment for wind power generation facilities
Anslow et al. Choosing the Best Vibration Sensor for Wind Turbine Condition Monitoring
CN112444287B (en) Sensor unit and transmission having at least one such sensor unit
CN211230718U (en) Fan running state on-line monitoring device
CN220378407U (en) Wind turbine generator system driving chain fault detection device based on displacement, bending moment and torque
CN203117743U (en) Wind driven generator monitoring system
CN214377058U (en) Teaching instrument for judging bearing fault
CN116792265A (en) Online state monitoring system for wind driven generator blade
JP6561720B2 (en) Bearing evaluation device
JP2015045584A (en) Vibration signal acquisition device and vibration monitoring system
CN112483333A (en) Unit driving chain displacement monitoring warning system based on Internet of things platform
Jung et al. A Wireless Accelerometer for in situ Gearbox Condition Monitoring of Rotating Components
JP2017040610A (en) State monitoring device for rotary machine

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application
DPE1 Request for preliminary examination filed after expiration of 19th month from priority date (pct application filed from 20040101)
WWE Wipo information: entry into national phase

Ref document number: 2007700169

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2797/KOLNP/2008

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2007209631

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 569819

Country of ref document: NZ

WWE Wipo information: entry into national phase

Ref document number: 200780003554.5

Country of ref document: CN

Ref document number: 2008551650

Country of ref document: JP

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2007209631

Country of ref document: AU

Date of ref document: 20070125

Kind code of ref document: A

WWP Wipo information: published in national office

Ref document number: 2007209631

Country of ref document: AU