Method and an arrangement in condition monitoring of an elevator rope
US-2015362450-A1 · Dec 17, 2015 · US
US10261037B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10261037-B2 |
| Application number | US-201515536760-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 2, 2015 |
| Priority date | Dec 23, 2014 |
| Publication date | Apr 16, 2019 |
| Grant date | Apr 16, 2019 |
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A structure to be monitored for damage and a method of monitoring the structure for damage are provided. The structure has a coating thereon, the coating defining a surface having characteristics which vary in a predetermined manner with damage to the structure. The surface has a series of conductive tracks applied thereto and in intimate contact therewith such that the said predetermined variation of the surface characteristics will vary the resistance of the series of conductive tracks in a predetermined manner in order to determine both location and extent of damage.
Opening claim text (preview).
What is claimed is: 1. A structure to be monitored for damage, the structure having a coating thereon, the coating defining a surface having specific failure characteristics tailored to the structure which vary in a predetermined manner with damage to the structure, the surface having a series of conductive tracks applied thereto and in intimate contact therewith such that the said predetermined variation of the surface characteristics will vary the resistance of the series of conductive tracks in a predetermined manner, wherein the coating comprises crack initiators. 2. The structure according to claim 1 , in which the variation in surface characteristics comprises cracking of the surface to an extent dependent upon the degree and/or type of damage to the structure. 3. The structure according to claim 1 , in which the coating is a glassy polymer. 4. The structure according to claim 1 , in which the coating is a thermoset polymer. 5. The structure according to claim 1 , in which the coating is a mixture of polymers and fillers. 6. The structure according to claim 1 , in which the coating is a cementitious ceramic. 7. The structure according to claim 1 , in which the characteristics of the surface of the coating vary with damage to the structure which includes impact damage, damage due to compressive or tensile loading above a certain threshold or damage due to repeated loading below the said threshold. 8. The structure according to claim 1 , in which a said conductive track is formed on the surface of the coating by a direct write process. 9. The structure according to claim 1 , comprising a protective helmet in which the coating is applied to an interior surface of the helmet. 10. The structure according to claim 1 , comprising an aircraft structural component. 11. The structure according to claim 1 , in which the crack initiation means comprises particulates in the coating. 12. The structure according to claim 1 , in which the crack initiation means comprises voids in the coating. 13. The structure according to claim 1 , in which the crack initiation means comprises micro-cracking in the coating. 14. The structure according to claim 1 , in which the coating is calibrated whereby to display the said variation in characteristics in response to a defined state of damage. 15. The structure according to claim 1 , in which the series of conductive tracks comprises a grid array disposed across the structure. 16. The structure according to claim 15 , including a series of electrical connections positioned around a periphery of the grid array and monitoring means connected via said connections to the grid array, the monitoring means being adapted to interrogate the grid array whereby to determine a location on the structure of any said damage. 17. The structure according to claim 16 , in which the monitoring means is arranged to interrogate the grid array during use of the structure. 18. A method of testing a structure for damage, the method including the steps of providing the structure with a coating defining a surface and having a series of conductive tracks applied to the surface in intimate contact therewith, the surface having specific failure characteristics tailored to the structure which vary in a predetermined manner with damage to the structure and the resistance of the series of conductive tracks being made variable in known relationship with the variation in surface characteristics of the surface, including measuring an electrical parameter of the series of tracks and comparing the measured parameter with the same parameter of the tracks when measured for the undamaged structure, wherein the coating comprises crack initiators. 19. The method according to claim 18 in which the parameter measured is resistance. 20. The method according to claim 18 , in which the series of conductive tracks comprises a grid array having a series of electrical connections positioned around a periphery of the grid array and the method includes the step of operating monitoring means connected via said connections to the grid array to interrogate different combinations of connections whereby to determine a said electrical parameter for each combination followed by analysis of said parameters to determine a location on the structure of any said damage. 21. The method according to claim 20 , in which determination of the location on the structure of any damage by analysis of the parameters includes making reference to results of previous calibration data for the structure.
Investigating the presence of flaws · CPC title
by determining damage, crack or wear · CPC title
by measuring variation of impedance, e.g. resistance, capacitance, induction · CPC title
by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids (of piezo-resistive materials G01L1/18); by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress · CPC title
with damage indication means · CPC title
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