GB2270383A - Electronic wearaway sensor - Google Patents
Electronic wearaway sensor Download PDFInfo
- Publication number
- GB2270383A GB2270383A GB9218430A GB9218430A GB2270383A GB 2270383 A GB2270383 A GB 2270383A GB 9218430 A GB9218430 A GB 9218430A GB 9218430 A GB9218430 A GB 9218430A GB 2270383 A GB2270383 A GB 2270383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sensor
- electronic
- wearaway
- wear
- resistive elements
- 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- Withdrawn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
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
- G01B7/02—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring length, width or thickness
- G01B7/06—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring length, width or thickness for measuring thickness
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
Abstract
An electronic wearaway sensor is incorporated in a solid core of the same material as the rest of the wear surface so as to wear away at the same rate as the surface to be monitored. The sensor shown has a number of parallel resistive elements 4 on a cylindrical core 1. As the given surface wears away, the resistive elements are progressively removed, thus increasing the total resistance value of the sensor. As described the resistive elements are formed by laser cutting an aluminium layer 3 formed over a ceramic insulating layer 2 on the core 1. The resistive bands are both insulated and protected by a outer ceramic layer 6. The device may be self powered 4-20mA and is intrinsically safe. The passive signal produced is small and therefore an electronic amplifier and interface buffer circuit are housed in the chamber 7 at the base of the unit through which the signal exits via the connector 8. The signal produced permits constant electronic readout of percentage wear and a set point alarm signal. <IMAGE>
Description
ELECTRONIC WEARAWAY SENSOR
This invention relates to an embedded wearaway -sensor.
A considerable amount of research has been carried out into the problem of how to measure the life of wear surfaces in an environment which is extremely hostile.
The device or devices must be able to operate reliably over a wide range of temperature and be capable of withstanding high pressures and loadings.
In order to monitor the actual thickness of a given material it is proposed to embed a sensor which can be worn away at the same rate as a given material.
Several methods may be employed to produce a sensor that will provide a change of electrical output as its length is reduced.
Two such methods which can be applied are based on the resistive and capacitive principles.
The following description is indicative of the principle and applied embodiment of a resistive wearaway sensor.
Figure 1. shows a number of resistors connected in parallel Having measured the total resistance across a. and b., it will be found that as each resistive element 1,2,3 is removed by process of wear, the total resistance value will be increased accordingly. On reaching the point that the 99th element is worn away the device indicates that the material has reached the end of its use able life. A number of discreet measurement steps may be produced dependant on the required resolution and length to be measured.
Figure 2. illustrates incorporation of the resistive elements within a solid core 1. of the same material as the rest of the wear surface. The sensor is therefore neither harder nor softer than the surrounding material thus ensuring that it wears at the same rate.
The core is covered in a fine layer of ceramic 2. to act as an insulator.
The next layer is sprayed aluminium 3. which is lazer cut to produce resistive bands or elements 4. connected by two strips 5. The second strip is at 1800 to the first and therefore not illustrated,
The aluminium is both protected and insulated by an outer layer of ceramic or similar 6. The signal produced is passive and very small therefore an electronic amplifier and interface buffer circuit is incorporated in a chamber at the base of the unit 7. The signal exits via a connector 8. fitted into the base.
The above sensor is resistive, however, if two layers of aluminium are employed a capacitive sensor is produced by the same method.
Figure 3. illustrates the build up of the sensor.
The device is self powered, can be operated at 4-20mA and is intrinsically safe.
The size and construction of the sensor is adaptable to a very wide range of applications.
The signal produced permits constant electronic readout of percentage wear and set point alarm signal.
The sensor will operate reliably over a wide temperature range and withstand high pressures and loadings.
Technology now available, enables construction compatible with virtually all sizes of component. The smallest limit, wherein a sensor conforming with the configuration illustrated in figure 2. using a solid core, is likely to be indicated by the structure of the material or as discussed, of a softer material should the area of wear be significantly larger than the sensor diameter. It is envisaged that, if required, the overall length of the sensor could be attained at approximately 27inch. Further reduction in length is possible by producing the sensor in two halves, the chamber 7. and connector 8. being a separate unit which could be externally situated when the sensor is in a stationary component.
The structural potential of the material comprising the core would present the main limiting factor regarding the diameter of the sensor, subject to which a diameter of 30 microns may possibly be achievable.
It is theoretically possible, using technology currently available, to produce a wearaway sensor in wafer form of a thickness down to approximately 0.01 of an inch and successfully in plant the device to monitor a wear surface.
It is possible that the resistive material 3. in figure 2. could be replaced by an alternative conductive layer, should a specific application demand, for instance, operation at very high temperature.
The insulative layer 3. in figure 2. could also, if operating conditions dictate, possibly be replaced by an alternative insulative material of acceptable properties.
Claims (5)
1. An electronic wearaway sensor.
2. An electronic wearaway sensor as claimed in Claim 1. which can be embedded in a solid core of the same material as the wear surface to be monitored.
3. An electronic wearaway sensor as claimed in Claim 1. or Claim 2. which will permit constant electronic readout of percentage wear and set point alarm signal.
4. An electronic wearaway sensor as claimed in Claim 2. or Claim 3. which may be self powered 4-20mA, intrinsically safe and will operate over a wide temperature range at the same time withstanding high pressures and loadings.
5. An electronic wearaway sensor the configuration of which is described herein and with reference to Figures 1-3 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9218430A GB2270383A (en) | 1992-08-29 | 1992-08-29 | Electronic wearaway sensor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9218430A GB2270383A (en) | 1992-08-29 | 1992-08-29 | Electronic wearaway sensor |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9218430D0 GB9218430D0 (en) | 1992-10-14 |
GB2270383A true GB2270383A (en) | 1994-03-09 |
Family
ID=10721176
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9218430A Withdrawn GB2270383A (en) | 1992-08-29 | 1992-08-29 | Electronic wearaway sensor |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2270383A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001006207A1 (en) * | 1999-07-19 | 2001-01-25 | Eskom | Monitoring arrangement for a wear part |
EP1270983A1 (en) * | 2001-06-27 | 2003-01-02 | Federal-Mogul Friction Products GmbH | Brake lining wear sensor |
WO2014187824A1 (en) * | 2013-05-21 | 2014-11-27 | Flsmidth A/S | Methods and apparatus for the continuous monitoring of wear in grinding circuits |
EP3404355A1 (en) * | 2017-05-17 | 2018-11-21 | Southern Cross Trading 5 (Pty) Ltd | A wear gauge |
GB2579671A (en) * | 2018-12-12 | 2020-07-01 | Weston Aerospace Ltd | A probe for monitoring a moving engine element |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1168056A (en) * | 1967-07-21 | 1969-10-22 | Teledyne Ind | Rupture Strip for Indicating Earth Movement |
GB1341814A (en) * | 1971-02-22 | 1973-12-25 | Computas As | Device for detection of wear on machine elements |
GB1518165A (en) * | 1974-09-20 | 1978-07-19 | Burmeister & Wains Mot Mask | Measuring probe for measuring wear |
GB2107807A (en) * | 1981-10-12 | 1983-05-05 | Morganite Elect Carbon | Wear sensor |
US4646001A (en) * | 1983-11-21 | 1987-02-24 | Morganite Electrical Carbon Limited | Resistive wear sensors |
-
1992
- 1992-08-29 GB GB9218430A patent/GB2270383A/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1168056A (en) * | 1967-07-21 | 1969-10-22 | Teledyne Ind | Rupture Strip for Indicating Earth Movement |
GB1341814A (en) * | 1971-02-22 | 1973-12-25 | Computas As | Device for detection of wear on machine elements |
GB1518165A (en) * | 1974-09-20 | 1978-07-19 | Burmeister & Wains Mot Mask | Measuring probe for measuring wear |
GB2107807A (en) * | 1981-10-12 | 1983-05-05 | Morganite Elect Carbon | Wear sensor |
US4646001A (en) * | 1983-11-21 | 1987-02-24 | Morganite Electrical Carbon Limited | Resistive wear sensors |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001006207A1 (en) * | 1999-07-19 | 2001-01-25 | Eskom | Monitoring arrangement for a wear part |
EP1270983A1 (en) * | 2001-06-27 | 2003-01-02 | Federal-Mogul Friction Products GmbH | Brake lining wear sensor |
WO2003002888A1 (en) * | 2001-06-27 | 2003-01-09 | Federal-Mogul Friction Products Gmbh | Braking lining wear system |
WO2014187824A1 (en) * | 2013-05-21 | 2014-11-27 | Flsmidth A/S | Methods and apparatus for the continuous monitoring of wear in grinding circuits |
CN105592927A (en) * | 2013-05-21 | 2016-05-18 | Fl史密斯公司 | Methods and apparatus for continuous monitoring of wear in grinding circuits |
CN105592927B (en) * | 2013-05-21 | 2018-04-27 | Fl史密斯公司 | Method and apparatus for continuing to monitor the abrasion in grinding circuit |
EA032648B1 (en) * | 2013-05-21 | 2019-06-28 | Эф-Эл-Смидт А/С | System and grinding disc for grinding with the continuous monitoring of wear of a grinding element |
EP3404355A1 (en) * | 2017-05-17 | 2018-11-21 | Southern Cross Trading 5 (Pty) Ltd | A wear gauge |
GB2579671A (en) * | 2018-12-12 | 2020-07-01 | Weston Aerospace Ltd | A probe for monitoring a moving engine element |
GB2579671B (en) * | 2018-12-12 | 2022-12-14 | Weston Aerospace Ltd | A probe for monitoring a moving engine element |
Also Published As
Publication number | Publication date |
---|---|
GB9218430D0 (en) | 1992-10-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |