GB2270383A - Electronic wearaway sensor - Google Patents

Electronic wearaway sensor Download PDF

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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
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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Withdrawn
Application number
GB9218430A
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GB9218430D0 (en
Inventor
Martin Robin Bowman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Priority to GB9218430A priority Critical patent/GB2270383A/en
Publication of GB9218430D0 publication Critical patent/GB9218430D0/en
Publication of GB2270383A publication Critical patent/GB2270383A/en
Withdrawn legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/02Measuring arrangements characterised by the use of electric or magnetic techniques for measuring length, width or thickness
    • G01B7/06Measuring arrangements characterised by the use of electric or magnetic techniques for measuring length, width or thickness for measuring thickness

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  • 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.
GB9218430A 1992-08-29 1992-08-29 Electronic wearaway sensor Withdrawn GB2270383A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)