Method and apparatus for monitoring vibration using fiber optic sensors
US-9200508-B2 · Dec 1, 2015 · US
US2016265905A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016265905-A1 |
| Application number | US-201615019052-A |
| Country | US |
| Kind code | A1 |
| Filing date | Feb 9, 2016 |
| Priority date | Mar 9, 2015 |
| Publication date | Sep 15, 2016 |
| Grant date | — |
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An apparatus for monitoring strain on a downhole component includes a fiber optic sensor having a length thereof in operable relationship with a downhole component and configured to deform in response to deformation of the downhole component. The fiber optic sensor defines a continuous, distributed sensor. An interrogation assembly is configured to transmit an electromagnetic interrogation signal into the fiber optic sensor and is configured to receive reflected signals therefrom. A processing unit is configured to receive information from the interrogation assembly and is configured to determine a strain on the downhole component during running of the downhole component to depth in a borehole.
Opening claim text (preview).
What is claimed is: 1 . An apparatus for monitoring strain on a downhole component, the apparatus comprising: a fiber optic sensor having a length thereof in an operable relationship with a downhole component and configured to deform in response to deformation of the downhole component, the fiber optic sensor defining a continuous, distributed sensor; an interrogation assembly configured to transmit an electromagnetic interrogation signal into the fiber optic sensor and configured to receive reflected signals therefrom; and a processing unit configured to receive information from the interrogation assembly and configured to determine a strain on the downhole component during running of the downhole component to depth in a borehole. 2 . The apparatus of claim 1 , further comprising a communication line operatively connecting the fiber optic sensor and the interrogation assembly. 3 . The apparatus of claim 2 , wherein the communication line is a fiber optic cable. 4 . The apparatus of claim 1 , wherein the fiber optic sensor is an optical fiber sensor. 5 . The apparatus of claim 4 , wherein the fiber optic sensor is a distributed fiber optic strain monitoring cable. 6 . The apparatus of claim 1 , wherein the interrogation assembly is configured as part of the downhole component. 7 . The apparatus of claim 6 , further comprising a data logger configured to record data from at least one of the interrogation assembly and the processing unit. 8 . The apparatus of claim 1 , wherein the downhole component is a housing configured to mimic the physical properties of a downhole tool. 9 . The apparatus of claim 1 , wherein the downhole component is operatively connected to a production string. 10 . The apparatus of claim 1 , wherein the interrogation assembly is on a ground surface and in operative communication with the fiber optic sensor. 11 . The apparatus of claim 1 , wherein the fiber optic sensor is disposed along a central axis of the downhole component. 12 . The apparatus of claim 1 , wherein the processing unit is configured to continuously determine a strain on the downhole component during running of the downhole component to depth. 13 . The apparatus of claim 1 , wherein the processing unit is configured to periodically determine a strain on the downhole component during running of the downhole component to depth. 14 . The apparatus of claim 1 , wherein the processing unit is configured to determine a strain on the downhole component at a potential landing site. 15 . The apparatus of claim 1 , wherein the downhole component is an electrical submersible pump. 16 . A method of monitoring strain on a downhole component, the method comprising: disposing a length of an fiber optic sensor in a fixed relationship relative to a downhole component, the fiber optic sensor configured to deform in response to deformation of the downhole component, the fiber optic sensor defining a continuous distributed sensor; running the downhole component into a borehole to a potential landing site; transmitting an electromagnetic interrogation signal into the fiber optic sensor during running of the downhole component; receiving reflected signals from the fiber optic sensor during running of the downhole component; and determining a strain on the downhole component from the received reflected signal during the running of the downhole component. 17 . The method of claim 16 , further comprising recording the received reflected signals. 18 . The method of claim 16 , wherein the determining step occurs in situ. 19 . The method of claim 16 , wherein the fiber optic sensor is disposed along a central axis of the downhole tool. 20 . The method of claim 16 , further comprising determining a strain on the downhole component at the potential landing site of the downhole component. 21 . The method of claim 16 , further comprising transmitting at least one of the received reflected signal and the determined strain to a surface component. 22 . The method of claim 16 , wherein the determining step occurs continuously during the running of the downhole component. 23 . The method of claim 16 , wherein the determining step occurs periodically during the running of the downhole component.
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