EP2989329A1 - Method for assessing a wear state of a module of a turbomachine, module, and turbomachine - Google Patents
Method for assessing a wear state of a module of a turbomachine, module, and turbomachineInfo
- Publication number
- EP2989329A1 EP2989329A1 EP14721302.9A EP14721302A EP2989329A1 EP 2989329 A1 EP2989329 A1 EP 2989329A1 EP 14721302 A EP14721302 A EP 14721302A EP 2989329 A1 EP2989329 A1 EP 2989329A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- signal
- assembly
- sensor
- bearing
- wear
- Prior art date
- Legal status (The legal status 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 status listed.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 title claims abstract description 28
- 230000004044 response Effects 0.000 claims abstract description 29
- 230000008859 change Effects 0.000 claims description 10
- 239000013078 crystal Substances 0.000 claims description 7
- 238000011156 evaluation Methods 0.000 claims description 6
- 239000012530 fluid Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 6
- 230000002123 temporal effect Effects 0.000 claims description 3
- 238000009826 distribution Methods 0.000 claims description 2
- 230000001105 regulatory effect Effects 0.000 claims description 2
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 9
- 230000006378 damage Effects 0.000 description 7
- 230000000712 assembly Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 5
- 239000000314 lubricant Substances 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 5
- 238000012544 monitoring process Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 3
- 230000010287 polarization Effects 0.000 description 3
- 230000008439 repair process Effects 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000005684 electric field Effects 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 238000010897 surface acoustic wave method Methods 0.000 description 2
- 238000009529 body temperature measurement Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003449 preventive effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000013024 troubleshooting Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M13/00—Testing of machine parts
- G01M13/04—Bearings
- G01M13/045—Acoustic or vibration analysis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D15/00—Control, e.g. regulation, of pumps, pumping installations or systems
- F04D15/0088—Testing machines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D15/00—Control, e.g. regulation, of pumps, pumping installations or systems
- F04D15/02—Stopping of pumps, or operating valves, on occurrence of unwanted conditions
- F04D15/0245—Stopping of pumps, or operating valves, on occurrence of unwanted conditions responsive to a condition of the pump
- F04D15/0272—Stopping of pumps, or operating valves, on occurrence of unwanted conditions responsive to a condition of the pump the condition being wear or a position
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L1/00—Measuring force or stress, in general
- G01L1/16—Measuring force or stress, in general using properties of piezoelectric devices
- G01L1/162—Measuring force or stress, in general using properties of piezoelectric devices using piezoelectric resonators
- G01L1/165—Measuring force or stress, in general using properties of piezoelectric devices using piezoelectric resonators with acoustic surface waves
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/16—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring several components of force
- G01L5/167—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring several components of force using piezoelectric means
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/02—Details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/06—Sliding-contact bearings for exclusively rotary movement for axial load only with tiltably-supported segments, e.g. Michell bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2233/00—Monitoring condition, e.g. temperature, load, vibration
Definitions
- the invention relates to a method for assessing a state of wear of an assembly of a turbomachine, in particular a bearing assembly of a pump or turbine, an assembly of a turbomachine, and a turbomachine, in particular pump or turbine according to the preamble of the independent claims 1, 11, and 15.
- Bearings are used wherever forces acting in certain directions have to be compensated or movements of an object in undesired directions have to be prevented.
- Turbomachines such as pumps or turbines, are used in assemblies with rotating components essentially two types of bearings, namely so-called radial and thrust bearings.
- the bearings commonly used in turbomachines are, depending on the specific application, very often extremely complex assemblies subcomponents in operation
- Bearing segments are arranged in the form of an annular array on a mostly metallic carrier body about a bearing axis and are flooded in the operating state with a circulating fluid as a lubricant.
- the bearing segments as such consist, depending on the application, of a metal, plastic, etc. and often have the shape of a trapezoidal cuboid, on whose side facing the carrier body there is a tilting element on which the bearing segment is mounted.
- On the side facing away from the carrier body of the bearing segments is a track disc, with which the axial forces of the shaft are transmitted to the bearing, whereby corresponding pressure loads on the
- the bearing segments are loosely and discreetly mounted with respect to the carrier body to avoid misalignment and to adapt the tilting of the bearing segments, which is caused by the formation of the hydrodynamic lubricant film, to the rotating shaft.
- the loose mount is in principle limited by the fact that the bearing segments are to be held within the assembly when the shaft is not rotating, so for example by the bearing segments are connected to each other by a flexible network or fastened by means of a fastener in a groove on the support body are.
- fluids with a low viscosity are used, for example a water-based lubricant or an oil mixture.
- the wear of the bearing segments is not a continuous process, but it comes at high pressure loads often within seconds to damage or destruction of the bearing segments.
- Such bearings, as well as the radial bearings are always subject to constant wear and tear, which, without sudden catastrophic effects, ultimately leads to the bearing or parts thereof having to be repaired or replaced.
- the rotating components, or those components which are in contact with rotating parts are wear parts which sooner or later fail. In order for such a failure does not occur completely surprising and thus possibly even worse damage to other components of the corresponding machine caused, it is important even before the final failure of such Verschleissteils information about the
- Turbomachines for example, bearings or bearing seals or bearing shafts of pumps or turbines, or axial
- thermocouples or with electrical resistance thermometers reasonably reliable and allows in principle a good monitoring and assessment of a
- Temperature sensors generated measurement signals are connected via electrical lines with appropriate measuring and Ausnceinstrumenten, so that the use of the aforementioned temperature sensor for use under normal operating conditions in the area prohibits in most cases, as the skilled person is immediately clear.
- the object of the invention is therefore to provide a reliable method for
- turbomachine which avoids the problems known from the prior art and is particularly suitable for use under ordinary operating conditions in the field or in the field, including outside the laboratory for everyday use. Moreover, it is an object of the invention to propose a correspondingly modified assembly of a turbomachine, as well as a
- Turbomachine in particular pump or turbine, with such a modified assembly.
- the invention is intended to provide a method and apparatus such that even under extreme operating conditions, such as e.g. at a pump that is deep below the
- the invention relates to a method for assessing a state of wear of an assembly of a turbomachine, in particular bearing arrangement of a pump or turbine, wherein for determining a Verschleisskenngrosse by means of a signal generator, a mechanical interrogation signal is generated with a predetermined waveform, and with a standing in contact with the module sensor generated from the query signal
- the response signal is changed according to a variation of a physical operating variable of the assembly according to a characteristic pattern, from
- the state of wear of the assembly is not reduced, as known in the art, e.g. with a conventional temperature sensor, such as a thermocouple or a
- thermometer assessed. Rather, a signal generator is used, which generates a mechanical interrogation signal from the one
- SAW sensor surface acoustic wave sensor
- German-language abbreviation SAW sensor surface wave sensor
- Such sensors are preferably made on the basis of a piezoelectric or piezoresistive material, which, as is well known to the skilled person, when exposed to mechanical stresses, such as elongation, compression, pressure, force, torque, etc. due to its special crystalline structure
- piezoelectric materials are also suitable for temperature measurement or for a suitable calibration
- SAW sensors which are constructed of piezoelectric materials, is, inter alia, that they can be made relatively small, often in dimensions of a few millimeters or even smaller. Since the piezoelectric effect is ultimately due to polarization phenomena in the crystal lattice, such a sensor module can be operated and read out with the application of minimal electrical energy, since the main effect, namely the change in polarization or
- Components can be installed.
- the sensor modules can also be wired in special cases.
- such sensor modules are robust, extremely durable and hardly prone to error, and are also commercially available at very favorable prices from a large number of manufacturers.
- Turbomachine in particular for assessing the state of wear of a bearing assembly or for assessing the state of wear of components or subcomponents, such as, inter alia, seals on bearing assemblies, the monitoring of the temperature or the temporal change in temperature in the operating state has to be particularly reliable and easy to handle Measured variable exposed.
- the temperature preferably monitored as a function of time at appropriate locations in the assembly, on the one hand slowly developing damage, for example, on a bearing or on a seal of the bearing or other component or
- Subcomponent of the camp are detected and monitored very early. If such temperature profiles are suitably calibrated to the relevant parameters, for example, a repair or replacement of the bearing can be carried out very early, before the corresponding component finally fails. But also very spontaneous, possibly catastrophic
- Damage can be detected almost immediately in its occurrence, so that a corresponding machine, for example, immediately shut down or can be reduced in their performance before worse and more damage to the corresponding machine can occur.
- the skilled person readily understands that automatic readout of the sensor units used, the monitoring can be automated especially easily, so that, for example, a corresponding message can be triggered when maintenance or repair is necessary or in the worst case, of course, an emergency shutdown or to be initiated automatically.
- Sensor units at different locations on or in the assembly also different components or subcomponents of the assembly
- the signal transmitter and the sensor are integrated in a sensor module, as a result of which the entire space occupied by the sensor
- Signaling device and the sensor together occupy particularly good can be minimized, so that the entire sensor module is particularly space-saving and also very easy to install on the module to be monitored.
- the signal generator additionally, i. at the same time also used as a sensor for detecting the response signal, which allows a further miniaturization of the sensor module.
- the interrogation signal is particularly preferably transmitted to the signal generator wirelessly from a suitable signal source, e.g. transmitted by radio on a suitable carrier frequency, of course, the response signal can be transmitted according wirelessly to an evaluation unit for evaluation and determination of the wear condition.
- the signal transmitter and / or the sensor and / or the sensor module are made at least partially from a suitable piezoelectric or piezoresistive material, in particular from a piezoelectric or piezoresistive single crystal.
- the physical operating variable which is monitored by the sensor module and from which finally the wear characteristic variable is derived, from which the wear state can be detected, can be any suitable physical variable that corresponds to the wear state in
- a pressure, a force, a torque, a rotational speed, a flow of a fluid medium very particularly preferably a temperature and / or a spatial or temporal distribution of these quantities.
- the module to be monitored is a component or a sub-component of a bearing
- the signal transmitter and / or the sensor and / or the sensor can be used
- Sensor module are particularly advantageously provided in a rotating component or sub-component of the module and / or on a stationary component or sub-component of the module.
- the inventive method is basically suitable for assessing the state of wear of any assembly of a turbomachine, but is in practice very particularly advantageous for assessing a wear condition of a bearing assembly of a
- the bearing assembly particularly preferably a mechanical shaft bearing comprising a in a
- stationary bearing saddle arranged rotatable shaft is, or else an axial Kippsegmentlager comprising a in a carrier body
- arranged tilting element may be with a plurality of segmental bodies.
- the inventive method for assessing the state of wear in a bearing assembly comprising a
- temperature peaks may occur, which are detected almost immediately in their emergence, so that a corresponding machine, for example, immediately shut down or can be reduced in their performance before worse and possibly additional damage to the corresponding machine may occur.
- Such temperature peaks usually do not occur, for example when using rolling bearings.
- the monitoring and evaluation of the state of wear can also be fully or partially automated, so that the turbomachine can be controlled and / or regulated in accordance with the response signal.
- the present invention further relates to an assembly of a
- Turbomachine in particular a bearing assembly of a pump or a turbine, with which assembly can perform the method of the invention.
- a signal generator for generating a mechanical
- Interrogation signal and a standing in contact with the module sensor for detecting a response signal generated from the interrogation signal
- Abrasion characteristic is determinable, and the state of wear can be assessed using the Verschleisskenngrösse.
- the signal transmitter and / or the sensor and / or the sensor module is provided in a rotating and / or stationary subcomponent of the assembly, wherein in practice the assembly often has a
- Bearing arrangement in the form of a mechanical shaft bearing comprising a arranged in a stationary bearing saddle rotatable shaft, wherein the signal generator and / or the sensor and / or the sensor module
- the assembly is a bearing arrangement in the form of an axial tilting pad bearing comprising a bearing segment arranged in a carrier body, wherein the signal transmitter and / or the sensor and / or the sensor module on the carrier body and / or on the tilting element and / or on a segment body of Tilting element is provided.
- the assembly comprises a bearing assembly with a
- the invention also relates to a turbomachine
- FIG. 1 a a simple schematic embodiment of a
- Fig. 1b an embodiment of a wireless coupled
- FIG. 2 shows a mechanical shaft bearing according to the invention
- FIG. 3a shows an axial tilting pad bearing according to the invention
- FIG. 3b shows a carrier body of the tilting pad bearing of FIG. 3a.
- FIGS. 1 a and 1 b a simple one is intended to illustrate the functional principle of a sensor module suitable for the invention
- inventive method are as such from the prior art, for example, under the keyword SAW sensors (Surface Acoustic Wave Sensor) or under the German name SAW sensors (Surface wave sensors) known per se and as such not directly the subject of the present invention.
- SAW sensors Surface Acoustic Wave Sensor
- German name SAW sensors Surface wave sensors
- the sensor module S according to the very simple and highly schematically illustrated embodiment according to FIG. 1a comprises a piezoelectric based signal generator 2, which in the operating state, a mechanical interrogation signal 21 in the form of a mechanical
- the piezoelectric signal generator 2 is fed by the signal source 200 with a corresponding electrical or electromagnetic signal.
- the interrogation signal 21 runs as a mechanical surface wave on the surface F of the sensor module S to the sensor 3. For example, due to a change in temperature, which has acted on the sensor module S, because, for example due to wear, the friction in a bearing assembly 1 1, 1 1 1, 1 12 has increased, to which the sensor module S is attached, the sensor module S undergoes a small change in length due to thermal expansion.
- the sensor module S is mechanically no longer resonantly tuned to the surface wave of the interrogation signal, whereby the response signal 31 generated by the sensor 3 via the piezoelectric effect or inverse piezoelectric effect with respect to the interrogation signal 21 follows a characteristic pattern depends on the type and degree of mechanical detuning, is changed.
- the response signal 31 is from the sensor 3 a
- Evaluation unit 300 is supplied, with which then from the change of the response signal 31, possibly with the aid of previously
- Abrasion characteristic can be assessed.
- FIG. 1 b shows an exemplary embodiment of a sensor module S in which the signal generator 2 simultaneously operates as a sensor 3.
- the interrogation signal 21 is fed wirelessly via a radio link in the form of an oscillating electromagnetic wave into an antenna T of the sensor module S and fed to the piezoelectric signal generator 2.
- the piezoelectric signal generator 2 generates via the piezoelectric effect or the inverse piezoelectric effect, a mechanical surface wave that passes over the surface F of the sensor module S, at least partially reflected at the reflection centers RZ and is mirrored back to the signal generator 2, the signal generator now taking advantage of the piezoelectric effect or the inverse
- piezoelectric effect as a sensor 3 operates and feeds the response signal 31 again in the antenna T, which transmits the characteristically modified response signal 31 wirelessly to an evaluation unit, in turn, the wear condition can be determined or assessed.
- Fig. 2 shows a highly schematic representation of a known per se
- inventive mechanical shaft bearing 1 1 1 is executed, and in the example, two sensor modules S are provided.
- two sensor modules S are provided.
- Sensor module S is provided in the static, non-rotating bearing saddle 1 1 1 1, while a second sensor module S in the operating state about the shaft axis A rotating shaft 1 1 12 is placed.
- FIG. 3a finally shows an inventive axial
- Kippsegmentlager 1 12 a turbomachine, which is here in particular a pump.
- the tilting pad bearing 1 12 differs from the axial tilting pad bearings known from the prior art substantially in that in the tilting pad bearing 1 12 shown here on static and rotating components of the tilting pad bearing 1 12 sensor modules S are provided.
- the axial tilting pad bearing 1 12 of FIG. 3 a comprises a carrier body 1 122 with tilting elements 1 121. On the pump shaft 1 1 12, in the
- Carrier body 1 122 so concentrically about the pump shaft 1 1 12th
- Tilting elements 1 121 provided segment body 1 123 of the two
- Carrier body 1 122 opposite. Between the two carrier bodies 1 122, a track disc SP is arranged, which transmits the axial pressure load in a conventional manner to the segment body 1 123.
- Fig. 3b shows for clarity one of the two support body 1 122 of the axial tilting pad bearing 1 12 of FIG. 3a in more detail in detail.
- the segment bodies 1 123 are fastened by means of a fastening means B,
- the carrier body 1 122 movably supported.
- the sensor modules S are preferred, but not necessary, in the corresponding component
- suitable combinations of the described embodiments includes, as well as simple developments of the invention, which also give the expert without further inventive step also informal.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Acoustics & Sound (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Health & Medical Sciences (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP14721302.9A EP2989329A1 (en) | 2013-04-26 | 2014-04-25 | Method for assessing a wear state of a module of a turbomachine, module, and turbomachine |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13165609 | 2013-04-26 | ||
EP14721302.9A EP2989329A1 (en) | 2013-04-26 | 2014-04-25 | Method for assessing a wear state of a module of a turbomachine, module, and turbomachine |
PCT/EP2014/058498 WO2014174097A1 (en) | 2013-04-26 | 2014-04-25 | Method for assessing a wear state of a module of a turbomachine, module, and turbomachine |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2989329A1 true EP2989329A1 (en) | 2016-03-02 |
Family
ID=48190285
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14721302.9A Withdrawn EP2989329A1 (en) | 2013-04-26 | 2014-04-25 | Method for assessing a wear state of a module of a turbomachine, module, and turbomachine |
Country Status (11)
Country | Link |
---|---|
US (1) | US10444118B2 (en) |
EP (1) | EP2989329A1 (en) |
KR (1) | KR20160002686A (en) |
CN (1) | CN105283671B (en) |
AU (1) | AU2014259373B2 (en) |
BR (1) | BR112015024263A2 (en) |
CA (1) | CA2899842C (en) |
MX (1) | MX361171B (en) |
RU (1) | RU2673968C2 (en) |
SG (1) | SG11201505880PA (en) |
WO (1) | WO2014174097A1 (en) |
Families Citing this family (12)
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US9157474B2 (en) * | 2013-09-30 | 2015-10-13 | Bell Helicopter Textron Inc. | System and method of monitoring wear in a bearing |
ES2733606T3 (en) * | 2015-02-26 | 2019-12-02 | Flender Gmbh | Layout with FOFW system |
WO2016153503A1 (en) | 2015-03-25 | 2016-09-29 | Ge Oil & Gas Esp, Inc. | System and method for real-time condition monitoring of an electric submersible pumping system |
AU2017223691B2 (en) | 2016-02-23 | 2020-06-25 | John Crane Uk Ltd. | Systems and methods for predictive diagnostics for mechanical systems |
EP3330493B1 (en) * | 2016-12-02 | 2019-05-01 | Rolls-Royce Deutschland Ltd & Co KG | Control system and method for a gas turbine engine |
DE102017126829B4 (en) * | 2017-11-15 | 2019-10-10 | Voith Patent Gmbh | Axial bearing for a shaft, in particular for the shaft of a hydraulic machine |
DE102017223418B4 (en) * | 2017-12-20 | 2023-05-25 | Zf Friedrichshafen Ag | Model-based method and system for condition monitoring of a plain bearing, especially for wind turbines |
JP6718926B2 (en) | 2018-07-12 | 2020-07-08 | 大同メタル工業株式会社 | Bearing system, bearing system control method, and computer program for controlling bearing system |
WO2020076825A1 (en) | 2018-10-08 | 2020-04-16 | John Crane Uk Limited | Mechanical seal with sensor |
IT201800020677A1 (en) * | 2018-12-21 | 2020-06-21 | Nuovo Pignone Tecnologie Srl | TURBOMACHINES WITH SAW AND BAW DEVICES, MEASUREMENT ARRANGEMENTS AND INSTALLATION METHODS |
US11041404B2 (en) | 2019-11-04 | 2021-06-22 | Raytheon Technologies Corporation | In-situ wireless monitoring of engine bearings |
WO2023224774A1 (en) * | 2022-05-17 | 2023-11-23 | Grant Prideco, Inc. | Predictive wear modeling for actively controlled sealing element |
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US6360610B1 (en) * | 1999-11-02 | 2002-03-26 | Jacek Jarzynski | Condition monitoring system and method for an interface |
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2014
- 2014-04-25 BR BR112015024263A patent/BR112015024263A2/en active Search and Examination
- 2014-04-25 WO PCT/EP2014/058498 patent/WO2014174097A1/en active Application Filing
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- 2014-04-25 MX MX2015014435A patent/MX361171B/en active IP Right Grant
- 2014-04-25 RU RU2015147851A patent/RU2673968C2/en not_active IP Right Cessation
- 2014-04-25 EP EP14721302.9A patent/EP2989329A1/en not_active Withdrawn
- 2014-04-25 CA CA2899842A patent/CA2899842C/en not_active Expired - Fee Related
- 2014-04-25 AU AU2014259373A patent/AU2014259373B2/en not_active Ceased
- 2014-04-25 SG SG11201505880PA patent/SG11201505880PA/en unknown
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CN105283671B (en) | 2017-09-26 |
AU2014259373B2 (en) | 2017-06-08 |
RU2015147851A (en) | 2017-06-02 |
CA2899842C (en) | 2021-10-12 |
BR112015024263A2 (en) | 2017-07-18 |
RU2673968C2 (en) | 2018-12-03 |
SG11201505880PA (en) | 2015-11-27 |
US10444118B2 (en) | 2019-10-15 |
CN105283671A (en) | 2016-01-27 |
AU2014259373A1 (en) | 2015-10-01 |
MX361171B (en) | 2018-11-29 |
CA2899842A1 (en) | 2014-10-30 |
US20160084734A1 (en) | 2016-03-24 |
WO2014174097A1 (en) | 2014-10-30 |
KR20160002686A (en) | 2016-01-08 |
MX2015014435A (en) | 2016-02-03 |
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