# US 7,876,096 B2 · Detecting failures in flexible multistrand steel structures

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- Number: US 7,876,096 B2
- Document ID: US7876096B2
- Status: Granted
- Kind: B2
- Application number: 11/722,710
- Filed: 2005-12-14
- Published: 2009-01-15
- Granted: 2011-01-25
- Earliest claimed: 2004-12-23
- Assignees: Maps Technology Limited
- Inventors: David John Buttle; William Dalzell
- Web page: https://patentgrep.com/patent/US7876096B2

## CPC

- G01N 27/9046: {by analysing electrical signals}
- G01N: INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES (measuring or testing apparatus or processes other than immunoassay, involving enzymes or microorganisms C12M, C12Q)

## Abstract

A flexible elongate structure, such as a flexible riser (10) for connecting oil and gas wells to floating production platforms, comprising at least one layer (20) of steel wires near the surface which extend at least partly along the length of the structure, can be monitored by inducing a magnetic field in the steel wires using an electromagnetic coil, and monitoring the magnetic flux density near the surface of the structure so as to detect if any wires have broken. Measurements are made at two different frequencies, the lower frequency giving an output dependent both on stresses and on the number of adjacent wires in the layer (20), and the higher frequency giving an output primarily dependent on the number of these wires. By comparing these two measurements a corrected output parameter (P) may be obtained that is indicative only of stress. A break in a wire can be expected to change the stress in that and adjacent wires.

## Claims

### Claim 1

A method for monitoring a flexible elongate structure with a generally cylindrical surface, the structure comprising at least one layer of steel ligaments near the cylindrical surface, the steel ligaments extending at least partly along the length of the structure, the method comprising inducing an alternating magnetic field less than saturation in the steel ligaments using an electromagnet with spaced-apart poles adjacent to the cylindrical surface, and monitoring the alternating magnetic flux density near the said cylindrical surface in the vicinity of the said electromagnet, from the detected flux density determining a parameter sensitive to stress in the ligaments, and from any variation of the said parameter as measured adjacent to different ligaments detecting if any ligaments have broken, wherein the alternating magnetic field is induced at least two different frequencies at every measurement location, and the said parameter is determined from the values of flux density detected at those different frequencies.

### Claim 2 (depends on 1)

A method as claimed in claim 1 wherein a lower frequency is selected so as to a provide a skin depth in the steel of the ligaments that is between an eighth of and twice the thickness of a ligament.

### Claim 3 (depends on 2)

A method as claimed in claim 2 wherein the lower frequency provides a skin depth substantially equal to a quarter of the thickness of a ligament.

### Claim 4 (depends on 1)

A method as claimed in claim 1 wherein a higher frequency is at least twice a lower frequency.

### Claim 5 (depends on 4)

A method as claimed in claim 4 wherein the higher frequency is between 3 and 5 times greater than the lower frequency.

### Claim 6 (depends on 1)

A method as claimed in claim 1 wherein the magnetic field is in a direction that is not parallel to the longitudinal axes of the ligaments.

### Claim 7 (depends on 1)

A method as claimed in claim 1 wherein the measurements are made using an electromagnetic probe incorporating an electromagnet coil to induce the alternating magnetic field, the coil being wound onto an electromagnet core, the probe also incorporating one or more sensors to monitor the magnetic flux density near the cylindrical surface.

### Claim 8 (depends on 7)

A method as claimed in claim 7 wherein signals from the sensor that monitors the alternating magnetic flux density are resolved into an in-phase component and a quadrature component, from which the stress-dependent parameter is determined such that the stress-dependent parameter is substantially unaffected by lift-off.

### Claim 9 (depends on 8)

A method as claimed in claim 8 wherein the stress-dependent parameter is calculated by resolving the signals from the sensor in a direction orthogonal to the lift-off line in the impedance plane at each of the frequencies, and comparing the resolved signals.

### Claim 10 (depends on 9)

A method as claimed in claim 9 wherein the resolved signals are normalised, and then the difference between the normalised values is taken as the stress-dependent parameter.

### Claim 11 (depends on 1)

A method as claimed in claim 1, the method using an array of probes in an annular support frame around the circumference of said flexible elongate structure.
