EP1151279A1 - Appareil et procede destines a surveiller une structure a l'aide d'un procede de propagation opposee de signaux pour localiser des evenements - Google Patents

Appareil et procede destines a surveiller une structure a l'aide d'un procede de propagation opposee de signaux pour localiser des evenements

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Publication number
EP1151279A1
EP1151279A1 EP99957747A EP99957747A EP1151279A1 EP 1151279 A1 EP1151279 A1 EP 1151279A1 EP 99957747 A EP99957747 A EP 99957747A EP 99957747 A EP99957747 A EP 99957747A EP 1151279 A1 EP1151279 A1 EP 1151279A1
Authority
EP
European Patent Office
Prior art keywords
waveguide
signals
counter
fibre
propagating
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Withdrawn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
EP99957747A
Other languages
German (de)
English (en)
Other versions
EP1151279A4 (fr
Inventor
Edward E. Tapanes
Jason R. Goode
Jim Katsifolis
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.)
Future Fibre Technologies Pty Ltd
Original Assignee
Future Fibre Technologies Pty Ltd
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
Priority claimed from AUPP7808A external-priority patent/AUPP780898A0/en
Application filed by Future Fibre Technologies Pty Ltd filed Critical Future Fibre Technologies Pty Ltd
Priority claimed from PCT/AU1999/001028 external-priority patent/WO2000037925A1/fr
Publication of EP1151279A1 publication Critical patent/EP1151279A1/fr
Publication of EP1151279A4 publication Critical patent/EP1151279A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0025—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of elongated objects, e.g. pipes, masts, towers or railways
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
    • G01M11/08—Testing mechanical properties
    • G01M11/083—Testing mechanical properties by using an optical fiber in contact with the device under test [DUT]
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
    • G01M11/30—Testing of optical devices, constituted by fibre optics or optical waveguides
    • G01M11/31—Testing of optical devices, constituted by fibre optics or optical waveguides with a light emitter and a light receiver being disposed at the same side of a fibre or waveguide end-face, e.g. reflectometers
    • G01M11/3109—Reflectometers detecting the back-scattered light in the time-domain, e.g. OTDR
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
    • G01M11/30—Testing of optical devices, constituted by fibre optics or optical waveguides
    • G01M11/39—Testing of optical devices, constituted by fibre optics or optical waveguides in which light is projected from both sides of the fiber or waveguide end-face
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0091—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by using electromagnetic excitation or detection

Definitions

  • This invention relates to an apparatus and method for monitoring a structure which employs a waveguide transmissive counter-propagating signal method and associated systems for locating events in fibre optic sensing systems.
  • structure used in this specification and in the claims should be understood to mean machines, buildings, infra-structure such as pipe lines and the like to which the apparatus and method may be applied as well as waveguides themselves which act as a communication link for transmission of data from one place to another.
  • Optical devices are commonly used in industry and science and include laser cavities, waveguides, lenses, filters and other optical elements and their combinations. Such optical devices are used in a variety of instruments and installations .
  • Photonics technology has revolutionised the communications and sensor fields. This is mainly due to the rapid development of optical and opto-electronic devices .
  • a wide variety of glass materials, material-dopants and waveguide structures are available and this invention relates to a waveguide transmissive counter-propagating 2 signal method and associated systems for locating events in fibre optic sensing systems.
  • Fibre optic sensors are very promising for these applications because of their dielectric properties, their fine size, their ability to be remotely located and, in the case of intrinsic sensors, rapid response times. They also have particular advantages in hazardous environments. In addition, they have several clear advantages over existing conventional sensing techniques such as bulk optical measurements, potentiometric electrodes, resistive foil gauges and piezo-electric transducers.
  • Engineered structures are usually not monitored in realtime because of the difficulties in incorporating conventional sensors into the sensing environment and because of the limitations of the sensors. Furthermore, conventional sensors are generally point sensing devices, thus requiring a large number of sensors to cover a large area or long length of interest . The subsequent cost and complexity of such a system is most often impractical.
  • Fibre optic sensors overcome many of these difficulties by virtue of their inherent properties.
  • optical sensors and optical processing systems are extremely fast and do not suffer from electro-magnetic interference
  • EMI unlike their electronic counter-parts.
  • the technology is gaining wide acceptance for monitoring applications and is expected to play a major role in the realisation of real-time structural integrity and machine condition monitoring systems, offering an advanced new generation of engineering sensors.
  • Fibre optic sensor technology has progressed at a rapid pace over the last decade. Many different sensing techniques have been developed to monitor specific parameters. Different configurations of fibre sensing devices have been developed for monitoring specific parameters, each differing by the principle of light modulation. Fibre optic sensors may be intrinsic or extrinsic, depending on whether the fibre is the sensing element or the information carrier, respectively. They are designated “point” sensors when the sensing gauge length is localised to discrete regions. If the sensor is capable of sensing a measurand field continuously over its entire length, it is known as a “distributed” sensor; “quasi-distributed” sensors utilise point sensors at various locations along the fibre length.
  • Fibre optic sensors can be transmissive or can be used in a reflective configuration by mirroring the fibre end-face. So, fibre optic sensors are actually a class of sensing device. They are not limited to a single configuration and operation unlike many conventional sensors such as electrical strain gauges and piezoelectric transducers .
  • OTDR optical time domain reflectometry
  • This method is essentially based on an optical radar technique, where a very narrow pulse of light launched into an optical fibre is back-scattered or back-reflected by anomalies in the fibre material or structure along its length (ie., fracture, localised compression, fault, etc.) and the measured ti e-of- flight determines the locations of the anomalies.
  • DTS Fibre Optic Distributed Temperature Sensor
  • Sagnac interferometer loops Physical placement of Sagnac interferometer loops at specific locations or geometric configurations have also been used for distributed fibre disturbance detection and location.
  • a Sagnac interferometer light is launched into opposite ends of a sensing fibre loop such that two beams circulate through the loop in opposite directions and then recombine to i
  • fibre particularly transient events which are too quickly occurring to detect with OTDR techniques.
  • This can be achieved by combining a distributed sensing technique incapable of locating the events with a compatible technique which is capable of locating the events.
  • This would have the further advantage of monitoring any structure or material near the fibre or to which the fibre is attached.
  • Such a capability should enable truly distributed sensing applications such as structural integrity monitoring, pipeline leak detection, ground monitoring, machine condition monitoring and intrusion detection of high security areas.
  • the object of the present invention is to provide a waveguide transmissive counter-propagating signal method and associated systems for locating events in waveguide sensing systems.
  • the present invention provides an apparatus for monitoring a structure and for locating the position of an event including; a light source; a waveguide for receiving light from the light source so that the light is caused to propagate in both directions along the waveguide to thereby provide counter-propagating optical signals in the waveguide, the waveguide being capable of having the counter-propagating optical signals or some characteristic of the signals modified or effected by an external parameter caused by or indicative of the event to provide modified counter- propagating optical signals; and detector means for detecting the modified counter-propagating optical signals effected by the parameter and for determining the time delay or difference i
  • optical signals preferably continuous-wave (C ) optical signals
  • C continuous-wave
  • Pulsing of the optical signal is not necessary, although it may be employed in some arrangements. Any sensed parameter which acts to alter the counter-propagating signals will effect both signals in the same manner, but because the effected counter- propagating signals must each continue travelling the remainder of the waveguide length to their respective photodetectors there is a resultant time delay or time difference between the detected signals.
  • the time delay is directly proportional to the location of the sensed event along the waveguide length. Therefore, if the time delay or difference is detected and measured, the location of the event can be determined. At the same time, if a compatible sensing mechanism is being employed the sensed event can be quantified and/or identified (ie., strain, vibration, acoustic emission, temperature transient, etc.).
  • non-sensitive fibre optic delay lines may be connected to the waveguide at either or both ends in order to add additional delay between the transmissive counter-propagating signals and to provide insensitive lead fibres. This may assist engineering the technique into a practical working system.
  • the invention also has the advantage of operating on virtually any existing type of transmissive distributed fibre optic sensor, enabling dynamic and transient events to be detected, quantified and located anywhere along the length of the optical fibre which forms the waveguide. Furthermore, it operates in a transmissive configuration, thus, delivering substantially the entire optical signal and power back to the detector and not requiring signal averaging, and it determines the location of events via the time delay measurement between counter-propagating optical signals effected by the same disturbance.
  • the waveguide is a silica waveguide.
  • the light from the light source is launched simultaneously into opposite ends of the waveguide.
  • the light source is a single light source.
  • two CW or synchronised light sources could be used for launching light simultaneously into opposite ends of the waveguide.
  • the waveguide is one or more optical fibres which forms an event sensitive optical fibre.
  • the detector means comprises: first and second photodetectors for simultaneously receiving the radiation from the counter- propagating signals in the silica waveguide; and processing means for receiving signals from the first and second photodetectors for determining the time delay or difference between the signals effected from the same disturbance and therefore determining the location of the sensed event.
  • a waveguide coupler or set of couplers is arranged between the light source and photodetectors and the silica waveguide so that the light can be simultaneously transmitted from the light source to both ends of the silica waveguide and the detector means also being connected to the coupler or couplers so that the counter-propagating transmissive radiation can be directed via the coupler or couplers from the silica waveguide to the detector means .
  • the invention also provides a method for monitoring a structure to locate the position of an event, including the steps of; launching light into a waveguide so that the light is caused to propagate in both directions along the waveguide to thereby provide counter-propagating optical signals in the waveguide, the waveguide being capable of having the counter-propagating optical signals or some characteristic of the signals modified or effected by an external parameter caused by the event, to provide counter-propagating optical signals; and detecting the modified counter-propagating optical signals effected by the parameter and for determining the time delay or difference between the modified signals in order to determine the location of the event.
  • the light is launched into both ends of the waveguide to provide the counter-propagating signals.
  • the light is launched into both ends of the waveguide from a single light source.
  • the preferred embodiment provides a waveguide transmissive counter-propagating signal method and associated systems for locating events in optical waveguides, which may include: providing an optical fibre (single or multi moded) formed from a waveguide material designed to simultaneously transmit counter-propagating optical signals; providing a sensor configuration (single or multi moded) , with any appropriate waveguide length, any suitable geometry and compatible with the waveguide transmissive counter-propagating signal method and associated systems for locating events in optical waveguides, designed to optimise the sensor sensitivity and detection capabilities; providing a lead optical fibre (single or multi moded) formed from a waveguide material which acts as an insensitive light guide between the sensing fibre and the sensing and locating system optics and optoelectronics interf ce; providing a lead optical fibre (single or multi moded) formed from a waveguide material which acts as an insensitive light guide between the sensing fibre and the excitation source; fusion splicing, or otherwise connecting, the sensor waveguide and the lead optical fibres so that
  • the time delay or difference between the signals may be measured and utilised to determine the location of the sensed event; and registering any changes in the waveguide sensor optical signals that may be utilised with a compatible sensing technique, such that the sensed parameter may be quantified and/or identified.
  • the preferred embodiment may also be said to reside in a method for producing a waveguide transmissive counter- propagating signal method and associated systems for locating events in optical waveguides, including, but not limited to, the steps of:
  • a waveguide sensor and optical fibre lead by cleaving or polishing their ends so as to establish a flat, smooth surface. After taking necessary precautions to remove any contaminants from the cleaved or polished waveguide sensor and fibre lead end-faces, the waveguide sensor and fibre lead are placed end-to-end in a fusion splicing apparatus and fused together using the appropriate or desired fusion are times and currents. The fusion splicing procedure may be repeated a number of times if necessary.
  • waveguide sensor and fibre lead are not limited and translation stages or V-grooves may be used on the fusion splicing apparatus to centrally align the cores of the waveguide sensor and fibre lead before the fusion splicing procedure. Different combinations of waveguide sensor and fibre lead may require a different or unique set of fusion splicing parameters.
  • Preparing or connectorising the free ends of the fibre leads in any manner which facilitates attaching, connecting, splicing or coupling the fibre leads to the appropriate combination and arrangement of light source, couplers, photodetectors and signal processing electronics which achieves the transmissive counter-propagating signal method for locating events in optical waveguides.
  • the manufactured sensor and/or the exposed fusion spliced region(s) may be protected by encapsulating or coating the desired region in a suitable device or material (ie., heatshrink fusion splice protector, acrylate, enamel, epoxy, polyimide, etc.).
  • the sensor waveguide is a multimode fibre and the lead fibres are singlemode fibres.
  • a plurality of multimode fibres and singlemode fibres are fusion spliced in end-to-end relationship to form several sensitive and insensitive regions along the entire fibre assembly.
  • a plurality of singlemode fibres are fusion spliced to respective multimode fibres and the plurality of singlemode fibres are connected to a coupler which in turn is connected to a further singlemode fibre to form a multiplexed sensor arrangement.
  • the senor fibre may be replaced by two or more suitably configured optical fibres (single or multi moded) and additional couplers may be utilised to connect the plurality of sensor fibres to the fibre optic leads.
  • additional couplers may be utilised to connect the plurality of sensor fibres to the fibre optic leads.
  • a further number of couplers and photodetectors may be required at the instrumentation to facilitate the increased number of sensing and lead fibres.
  • the sensing part is formed by two suitably configured singlemode fibres and the insensitive leads are singlemode fibres.
  • the two sensing fibres are connected to a lead fibre by the use of a singlemode coupler at either or both ends.
  • the present invention is effective on any optical waveguiding distributed sensing technique that may be arranged in a transmissive configuration.
  • the distributed sensing technique is based on a modalmetric technique utilising the fusion splicing of insensitive singlemode fibre to sensitive multimode fibre.
  • the distributed sensing technique is based on a Mach-Zehnder or Michelson interferometer utilising two singlemode fibres as the sensitive region.
  • the waveguide comprises at least one optical fibre and/or at least one optical fibre device.
  • the waveguide may merely i
  • the optical fibre 14 comprise an optical fibre without any additional elements.
  • the optical fibre can include passive or active elements along its length.
  • the optical fibre can include sensing elements along its length and those sensing elements can comprise devices which will respond to a change in the desired parameter in the environment of application and influence the properties and characteristics of the electromagnetic radiation propagating in the waveguide to thereby provide an indication of the change in the parameter.
  • any suitable CW or pulsed single-frequency or multiple wavelength source or plurality of sources may be employed.
  • a CW or pulsed coherent laser diode is utilised to supply the optical signal.
  • multiple light sources of the same or varying wavelengths, may be used to generate the counter-propagating signals.
  • the preferred embodiments of the present invention offer the potential to utilise all-fibre, low-cost optical devices in conjunction with laser diodes, light emitting diodes, photodetectors, couplers, isolators, circulators and filters. Any suitable light source, coupler and photodetector arrangement may be used with the sensor and locating systems.
  • the required optical properties of the light source are such that light may be launched into and propagated in the singlemode waveguide.
  • the light propagated in a singlemode fibre must remain singlemoded during the entire period of travel in the singlemode fibre.
  • the singlemode fibre Once the light is launched into the multimode fibre from the singlemode fibre, several modes may be excited and the multimoded fibre will be sensitive to various parameters.
  • the singlemode fibre Once the light is launched back into the singlemode fibre from the multimode fibre, only a single mode is supported and travels to the optical components of the system.
  • Lead- in/lead-out fibre desensitisation and sensor localisation 15 is achieved in this manner.
  • the singlemode fibre should be made sufficiently long to attenuate all cladding modes in order to improve the signal-to-noise ratio. This preferred embodiment applies for both directions of travel of the transmissive counter- propagating optical signals.
  • electromagnetic radiation is launched into an optical waveguide (single or multi moded) , such as an optical fibre, from a light source, such as a pigtailed laser diode, fibre laser or light emitting diode, and propagates along the optical waveguide.
  • the optical waveguide is connected (temporarily or permanently) to one arm of an optical waveguide light splitter or coupler and when the electromagnetic radiation reaches the light splitter the electromagnetic radiation can branch out into the two output waveguide arms of the light splitter.
  • Each of the output arms of this light splitter are fusion spliced to other couplers, thus the optical radiation from the laser source is simultaneously launched into each of the other two couplers.
  • couplers form the launch and detection ports for the dual-ended, counter- propagating method described above.
  • the optical signal is simultaneously launched to the output waveguide arms of the couplers . Only one output arm is used in each coupler, the other is fractured or otherwise terminated to avoid back-reflections.
  • the output arms of the couplers are either connected (temporarily or permanently) directly to the waveguide sensing element or to a lead optical i
  • any one of the output waveguide arms of the light splitter may be used to deliver the electromagnetic radiation to the sensor waveguide via an optical waveguide lead.
  • a plurality of output waveguide arms may be used to deliver the electromagnetic radiation to a number of individual or multiplexed waveguide sensors.
  • Each of the counter- propagating signals transmitted into the waveguide sensor propagates along the entire length of the waveguide until they reach the opposite ends and are launched back into the latter couplers in the opposite direction to the initial launch signals. The signals are each split in the reverse direction through the latter couplers.
  • the optical signals are simultaneously monitored by the two photodetectors .
  • Appropriate electronics, signal processing schemes and algorithms process the signals from each detector and provide the location of the sensed event by determination of the time delay or difference between the signals effected by the same disturbance.
  • the insensitive fibre optic leads may be very long to provide an additional time delay between the optical signals. This may assist engineering the technique into a practical working system.
  • the sensing section is formed by two or more suitably configured fibres (single or multi moded) and the insensitive leads are singlemode fibres.
  • the plurality of sensing fibres are connected to the lead fibres by the use of additional singlemode couplers at either or both ends of the sensing fibres.
  • the instrument optical and electronic arrangements will utilise noise minimisation techniques.
  • all the optical and electrical components will be located in a single instrument control box, with individual optical fibre input ports.
  • Electro-optic devices may also be utilised in the system.
  • the invention provides an apparatus for monitoring an optic fibre communication link into which data signals are launched and from which the data signals are received, and for locating the position of a disturbance to the link including; a light source for launching light into the link so that the light is caused to propagate in both directions along the link to thereby provide counter- propagating optical signals in the link, the link being capable of having the counter-propagating optical signals or some characteristic of the signals modified or effected by the disturbance to provide modified counter-propagating optical signals; and detector means for detecting the modified counter-propagating optical signals and for determining the time delay or difference between the modified counter- propagating optical signals in order to determine the location of the disturbance.
  • the invention still further provides a method for monitoring an optical fibre communication link into which data signals are launched and from which the data signals are received, to locate the position of a disturbance to the link, including the steps of; launching light into the link so that the light is caused to propagate in both directions along the link J
  • the link being capable of having the counter- propagating optical signals or some characteristic of the signals modified or effected by the disturbance to provide counter-propagating optical signals; and detecting the modified counter-propagating optical signals effected by the disturbance and for determining the time delay or difference between the modified signals in order to determine the location of the disturbanee.
  • Figure 1 is a view showing a general embodiment of the invention
  • Figure 2 is a view showing an embodiment of the invention, utilising a modalmetric sensing technique
  • Figure 3 is a view showing a further embodiment of the invention, utilising a Mach-Zehnder interferometric sensing technique
  • Figure 4 shows an integrated fibre optic sensing and communication system, utilising a modalmetric sensing technique
  • Figure 5 is a view showing yet a further embodiment of the invention.
  • Figure 6 is an oscilloscope plot illustrating the actual response of a system formed by the method of a preferred embodiment of the present invention, as detailed in Figure 5, when a perturbation acts on the fibre of a 14.71 km fibre link;
  • Figure 7 is another oscilloscope plot illustrating the actual response of a system formed by the method of a preferred embodiment of the present invention, J
  • Figure 8 shows a combined fibre optic sensing and communication arrangement, utilising a modalmetric sensing technique and the ability to locate disturbances formed by the method of the preferred embodiments of the present invention
  • Figure 9 is a view of a further embodiment of the invention.
  • Figure 10 is a view of a still further embodiment of the invention.
  • insensitive fibre leads 14a and 14b With reference to Figure 1, a general set-up is illustrated where the distributed sensor 10 may be preceded and succeeded by certain arbitrary lengths of insensitive fibre leads 14a and 14b. It is important to emphasise that neither one or both of the insensitive fibre leads 14a and 14b are required for the methodology; they simply provide additional optical delay lines in order to add additional delay between the transmissive counter-propagating signals, to provide insensitive lead fibres and/or to facilitate specific placement of the sensing region(s) . This may assist engineering the technique into a practical working system.
  • the insensitive leads 14a and 14b may be fusion spliced 17, or otherwise connected, to the sensing fibre 10.
  • the optical fibre link (total distance d * ) is made up of an insensitive section 14a, of length d a , fusion spliced 17 to a sensitive section 10, of length d b , and finally fusion spliced 17 again to a third insensitive section 14b, of length dc.
  • the aim of the set-up is to locate a disturbance 18 (at point C) along the sensitive section of the fibre link 10 (between points B and D) .
  • the fibre link has two counter-propagating i
  • CW coherent laser light is launched into a singlemode optical fibre 15, from a pigtailed laser diode 20 and fibre isolator 22, and propagates along the optical fibre 15.
  • the optical fibre 15 is fusion spliced 41 to one arm of a singlemode fibre optic coupler 24 and when the light reaches the coupler 24 the light can branch out into the two output arms of the coupler 24.
  • Each of the output arms of this coupler 24 are fusion spliced 42a and 42b to other singlemode fibre couplers 26a and 26b, respectively, thus the light from the laser source 20 is simultaneously launched into each of the other two couplers 26a and 26b.
  • These two couplers 26a and 26b form the launch and detection ports for the dual-ended, counter-propagating method utilising a modalmetric sensing technique.
  • the optical signal is J
  • the output arms 27a and 27b of the couplers 26a and 26b are terminated at singlemode fibre optic bulkhead connectors (through adaptors) 28a and 28b.
  • a connectorised singlemode fibre lead 14a is connected to the through adaptor 28a, such that the light from coupler 26a is launched into the fibre link in one direction.
  • a connectorised singlemode fibre lead 14b is connected to the through adaptor 28b, such that the light from coupler 26b is launched into the fibre link in the opposite direction.
  • the singlemode fibre lead 14a is fusion spliced 43 to one end of the multimode sensing fibre 10 and the singlemode fibre lead 14b is fusion spliced 44 to the opposite end of the multimode sensing fibre 10, thus forming the transmissive counter- propagating sensing loop configuration required.
  • Each of the counter-propagating signals transmitted through the fibre sensor 10 propagates along the entire length of the fibre link until they reach the opposite ends and are launched back through leads 14a and 14b and bulkhead through adaptors 28a and 28b into the couplers 26a and 26b, respectively, in the opposite direction to the initial launch signals.
  • the signals are each split in the reverse direction through couplers 26a and 26b. Part of the signals travel back towards the first coupler 24 and laser 20, and the remainder of the signals travel along the arms 16a and 16b of the latter couplers 26a and 26b, respectively, which are terminated at photodetectors 30a and 30b.
  • the fibre isolator 22 is used to reduce the amount of light launched back into the laser diode.
  • the optical signals are simultaneously monitored by the two photodetectors 30a and 30b. Appropriate electronics, signal processing schemes and algorithms process the i
  • the insensitive fibre optic leads 14a and 14b may be very long to provide an additional time delay between the optical signals, if required.
  • CW coherent laser light is launched into a singlemode optical fibre 15, from a pigtailed laser diode 20 and fibre isolator 22, and propagates along the optical fibre 15.
  • the optical fibre 15 is fusion spliced 41 to one arm of a singlemode fibre optic coupler 24 and when the light reaches the coupler 24 the light can branch out into the two output arms of the coupler 24.
  • Each of the output arms of this coupler 24 are fusion spliced 42a and 42b to other singlemode fibre couplers 26a and 26b, respectively, thus the light from the laser source 20 is simultaneously launched into each of the other two couplers 26a and 26b.
  • couplers 26a and 26b form the launch and detection ports for the dual-ended, counter-propagating method utilising a Mach- Zehnder interferometric sensing technique.
  • the optical signal is simultaneously launched to the output arms 27a, 27c and 27b of the couplers 26a and 26b. Only one output arm 27b from coupler 26b is used, all other unused arms of couplers are fractured or otherwise terminated to avoid back-reflections 19.
  • the output arms 27a, 27c and 27b of the couplers 26a and 26b are terminated at singlemode fibre optic bulkhead connectors (through adaptors) 28a, 28c and 28b.
  • Connectorised singlemode sensing fibres 10a and 10c are connected to the through adaptors 28a and 28c, respectively, such that the light from coupler 26a is simultaneously launched into the fibre link in one direction.
  • a further coupler could be used with arms 10a and 10c to replace using arm 27c and adaptor 28c.
  • a connectorised singlemode fibre lead 14 is connected to the 24 through adaptor 28b, such that the light from coupler 26b is launched into the fibre link in the opposite direction.
  • the singlemode sensing fibres 10a and 10c are fusion spliced 45 and 46, respectively, to one end of a singlemode coupler 60 and the singlemode fibre lead 14 is fusion spliced 47 to one arm of the coupler 60 on the opposite side, thus forming the transmissive counter- propagating sensing loop configuration required.
  • the unused arm of coupler 60 is fractured or otherwise terminated to avoid back-reflections 19.
  • Each of the counter-propagating signals transmitted through the fibre arrangement propagates along the entire length of the fibre link until they reach the opposite ends and are launched back through bulkhead connectors 28a, 28c and 28b into the couplers 26a and 26b, respectively, in the opposite direction to the initial launch signals.
  • the signals are each split in the reverse direction through couplers 26a and 26b. Part of the signals travel back towards the first coupler 24 and laser 20, and the remainder of the signals travel along the arms 16a and 16b of the latter couplers 26a and 26b, respectively, which are terminated at photodetectors 30a and 30b.
  • the fibre isolator 22 is used to reduce the amount of light launched back into the laser diode.
  • the optical signals are simultaneously monitored by the two photodetectors 30a and 30b. Appropriate electronics, signal processing schemes and algorithms process the signals from each detector 30a and 30b and provide the location 18 of the sensed event by determination of the time delay or difference between the signals effected by the same disturbance.
  • the insensitive fibre optic lead 14 may be very long to provide an additional time delay between the optical signals, if required.
  • Figure 4 illustrates an integrated fibre optic sensing and communication system, utilising a modalmetric sensing J
  • Figure 5 illustrates a view of an embodiment of the invention used to verify the feasibility of the invention, and is described in detail in the example further below.
  • Figure 6 illustrates an oscilloscope plot illustrating the actual response of a system formed by the method of a preferred embodiment of the present invention, as detailed in Figure 5 and the example further below, when a perturbation acts on the fibre of a 14.71 km fibre link.
  • Figure 7 illustrates another oscilloscope plot illustrating the actual response of a system formed by the method of a preferred embodiment of the present invention, as detailed in Figure 5 and the example further below, when a perturbation acts on the fibre of a 14.71 km fibre link.
  • Figure 8 illustrates a combined fibre optic sensing and communication arrangement, utilising a modalmetric sensing technique and the ability to locate disturbances formed by the method of the preferred embodiments of the present invention.
  • this technique it will usually be desirable for both launch points of the counter-propagating signals to be at the same physical location. This is easily achieved by using a multi-fibre cable which will effectively form a single-ended system.
  • one singlemode fibre is utilised as the communications fibre, whilst two fibres, one singlemode and one multimode, are required to set-up the modalmetric intrusion sensor (event detection and location determination) over the specified region of interest (shaded area) .
  • a perturbation anywhere along the multimode fibre in the shaded region will generate two counter-propagating perturbation signals. Measuring the time difference in their respective time of arrival at the J
  • a communication cable 150 which includes a communications fibre 151.
  • One end of the fibre 151 is connected to a transmitter 152 and the other end to a receiver 153.
  • the transmitter 152 transmits data into the fibre 151 for receipt by the receiver 153.
  • the cable 150 also includes a multimode fibre 155 which is spliced to a single mode fibre 156 at splice point 157.
  • a further single mode fibre 158 is spliced to the multimode fibre 155 at 159.
  • the fibres 155, 156 and 158 are formed in a loop configuration within the cable 150 so that the ends 160 and 161of the continuous fibre formed by the fibres 155, 156 and 158 are adjacent one another.
  • counter-propagating signals are launched into the two ends 160 and 161 of the fibres 155, 156 and 158 and detectors (not shown) are arranged for detecting the two counter-propagating signals which emanate from the two ends 160 and 161.
  • any attempt to break into the cable 150 to physically access fibre 151 will necessarily disturb the multimode fibre 155 which is the sensing fibre and therefore the two counter-propagating perturbation signals will be produced and detected at the ends 160 and 161 in the manner previously described.
  • the location of the attempted break- in can be determined.
  • the modalmetric effect in a multimode fibre can be used to sense and monitor vibrations, disturbances or movement of the fibre itself, or any structure or object the fibre is attached to, by detecting an intensity change in the speckle pattern output of the fibre.
  • Modalmetric sensors can therefore be used as vibration sensors in structural monitoring, condition monitoring of high voltage equipment, intrusion detection of cables or pipelines, and in fence perimeter security.
  • optical fibres were deployed mainly in long- haul and high-speed telecommunication systems.
  • i i
  • optical fibres are now being used as the main carrier in many other communications applications such as, LAN/WAN backbones, and in the private communications networks of many small and large organisations (ie., banks, defence, government, public utilities and multinationals) . Many of these communications networks involve the transfer of sensitive information which has made the security of the communications link a high priority.
  • the modalmetric effect can easily and effectively be employed to guard against any intrusion into or tampering with an optical fibre cable.
  • a typical set-up where the sensing is integrated into a fibre communications system is shown in Figure 4.
  • Both the sensing system 100a (i.e. laser) and 100b (detector and processor) and the communication system 200a (transmitter) and 200b (receiver) are integrated into the same optical fibre 10.
  • the wavelength of the sensing system is chosen so as not to interfere with the communications signal (via wavelength multiplexing) and also such that the fibre link is multimoded for the sensing wavelength.
  • the modalmetric processing unit will detect any perturbation at any point along the fibre link.
  • the sensing fibre 10 (which may be for example 2km long and located between splicing points 105 and 107) may be a dedicated fibre in the fibre cable, or the same fibre as the communications fibre.
  • the fibre 10 is connected to insensitive lead fibres 109 and 111 which form the ends of the waveguide network.
  • the lead fibre 109 is connected to an insensitive fibre 113 of significant length (such as 5km) via splice 115 and the fibre 113 is spliced at 117 to a sensitive multi-mode fibre 119 via splice 117.
  • the fibre 119 is connected to the fibre 10 via splice 107.
  • the fibre 119 may be of significant length such as 8.8km. If a perturbation P is applied to the multimode fibre at the point indicated (point A) , two similar or identical time varying optical signals will be generated consistent with the modalmetric effect, each travelling in the opposite direction.
  • the perturbation signal consistent with Input 1 (PSI) will arrive at Port 2 (Output 1) before the perturbation signal consistent with Input 2 (PS2) arrives at Port 1 (Output 2).
  • PS2 needs to propagate through for example 14.71 km (the difference in distance between A to Port 1 and A to Port 2) more optical fibre than PSI.
  • the error (effectively 300 m) may be a result of the assumption of the value of the effective refractive index of the fibres and by the inaccuracy in the manual measurement of the time delay. These errors could be reduced by knowing the actual effective refractive index of the fibre and by employing digital signal processing means to accurately determine the time delay.
  • Figures 9 and 10 show further embodiments of the invention in which a common waveguide is used for both transmission of data (for example a fibre communication link) and also forms the sensing fibre for determining any attempt to interfere with the fibre. These embodiments has particular application to securing communication links and indicating any attempt to break into the communication link so as to tap off data from the communication link.
  • Figure 10 shows a loop configuration and Figure 9 a configuration without a loop.
  • an optical fibre 200 forms the communication link for transmitting data from one place to another.
  • the fibre 200 is preferably single moded at a wavelength of 1550 nm (which will be the data transmission wavelength) and multimoded at a wavelength of 850 nm (which will be the sensing frequency) .
  • Data is launched into the fibre i
  • a transmitter 210 which may include a pigtailed laser diode with an integrated isolator so that data signals are launched into a single moded fibre 212 at the wavelength of 1550 nm.
  • the fibre 212 is spliced at 213 to fibre 214 which is connected to one arm of a coupler 216.
  • the output of the coupler 216 is spliced at 218 to the fibre 200.
  • the fibre 200 is also spliced at 218 to a coupler 220.
  • One of the arms of the coupler 220 is spliced to a single moded fibre 221 which is spliced at 222 to a further single mode fibre 224.
  • the fibres 221 and 224 are single moded at the wavelength of 1550 nm.
  • the fibre 224 is connected to a detector 226 which is sensitive to the wavelength of 1550 nm.
  • a first counter-propagating sensing system 240 is connected to the other arm of the coupler 216 by a single mode fibre 241 and a multi-mode fibre arm 242 of coupler 216 which are spliced together at splice 243.
  • the fibres 241 and 242 are single moded and multi-moded respectfully at a wavelength of 850 nm which is the sensing wavelength used in the embodiment of Figure 9.
  • the counter- propagating sensing system 240 includes a transmitter such as a pigtailed laser diode for launching the light at the wavelength of 850 nm into the fibre 241, and a detector for detecting light emanating from the fibre 241 in the manner which will be described hereinafter.
  • the system 240 can be identical to the pigtailed laser diode 20 and detector 30a described with reference to Figure 2.
  • the system 240 may include appropriate couplers for enabling light to be launched into the fibre 241 from the pigtailed laser diode and to enable the detector to receive light from the fibre 241.
  • the sensing light signal is launched into the fibre 241 from the counter-propagating system 240 at a wavelength of 850 nm and is coupled with the data transmission signal from the transmitter 210 in the coupler 216. Both the data transmission signal at a i
  • the coupler 220 has a second arm which is connected to multi-mode fibre 249 which is spliced at 250 to a further single mode fibre 251.
  • the fibres 249 and 251 are respectively multi moded and single moded at the wavelength of 850 nm.
  • the fibre 251 is connected to a counter-propagating sensing system 260 which is identical to the system 240.
  • the system 260 both launches and receives sensing light signals at a wavelength of 850 nm or 670 nm into the fibres 251 and 249 for counter propagation in the fibre 200 to the signals which are launched by the system 240.
  • the data signal at a wavelength of 1550 nm which travels along the fibre 200 is coupled into the fibres 221 and 224 by the coupler 220 with some of the 850 nm signal.
  • the detector 226 detects only the signal at the wavelength of 1550 nm and therefore the data which is transmitted from the transmitter 210 and is InGaAs.
  • Retractors in systems 240 and 260 are Si type and only sensitive to the 850 nm or 670 nm wavelengths.
  • the counter-propagating sensing signals which are launched by the systems 240 and 260 travel in opposite directions along the fibre 200 which is multi moded at the wavelengths of 850 nm or 670 nm.
  • the multi moded fibre 200 forms a sensitive fibre along its entire length because it is multi moded at the wavelength of 850 nm or
  • 33 location of the attempted break in can be determined in the manner described in the previous embodiments by determining the time difference between the receipt of the modified signals in the system 240 and the system 260 so that the position along the length of the fibre 200 can be determined.
  • the detectors in the systems 240 and 260 are suitably timed synchronised with one another so that the difference in time between the receipt of the modified signal in the system 240 and receipt of the modified signal in the system 260 can be determined.
  • Figure 10 shows a further embodiment which is similar to the embodiment of Figure 9 except that rather than having two counter-propagating sensing systems 240 and 260 a single system 270 is utilised and a return loop fibre 271 is coupled to the coupler 220 so that the fibre 200 is effectivly looped back to a single system 270 in the same manner as described with reference to Figures 2, 3, 5 and
  • the fibre 271 is single moded at the sensing wavelength so that it is insensitive and therefore any attempt to break into the fibre 200 will cause the modification to the counter-propagating signals launched into the fibre 200 but disturbance of the fibre 271 will not cause any modification to signals in the fibre 271so that the point of attempted break in in the fibre 220 can be detected.
  • the counter-propagating signals are launched from the system 270 into the fibre 241 and also the fibre 271 for counter propagation along the fibre 200 concurrently with the data signal launched from the transmitter 210.
  • the data signal is received by the detector 226 in the same manner as described with reference to Figure 9.
  • This embodiment has the advantage of locating the detectors for detecting the counter- propagating signals at the same place thereby avoiding the need for remote synchronising of detectors which are at different locations as in the embodiment of Figure 9.
  • the modified signals which are detected by the detectors are any parameter of the light signals which is altered by the disturbance to the sensing fibre.
  • the parameter may be the intensity of the signal so that the detectors for detecting the counter-propagating signals effectively look at the intensity of the signal which is received and when the intensity changes this is indicative of the receipt of the modified signal caused by the disturbance to the sensing fibre.
  • Optical devices and systems made by the method of the invention are useful in a wide variety of applications and fields. Not inclusive, but indicatively, the following examples illustrate some potential users of the fibre optic sensing and locating methods described herein:
  • Non-destructive evaluation firms and equipment manufacturers R&D companies and laboratories.
  • the claimed invention overcomes the disadvantages and limitations of many existing fibre optic distributed sensing techniques. Furthermore, it is capable of detecting and locating dynamic and transient events and it is less complex and lower cost than most other fibre optic distributed sensors capable of locating disturbances. Such a system would offer lower cost and increased operational and safety advantages over existing technologies and has the potential for short and long term installation monitoring in plant and ecological environments .

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Abstract

Appareil et procédé destinés à surveiller une structure telle que des machines, des bâtiments, des liaisons de communication par fibres optiques et des infrastructures. Ledit appareil comporte un guide (10) d'ondes et une source (20) de lumière destinée à envoyer de la lumière dans les deux extrémités du guide (10) d'ondes, si bien que des signaux lumineux à propagation opposée sont produits dans le guide (10) d'ondes. Le guide (10) d'ondes se présente sous forme d'une fibre optique ou d'un faisceau de fibres constituées de silice, dans lequel la caractéristique de la lumière est modifiée ou produite par un paramètre extérieur causé par un événement. Un détecteur (30) est destiné à détecter la lumière depuis les deux extrémités du guide (10) d'ondes et à déterminer le retard ou la différence de temps entre les signaux modifiés qui ont été produits par le paramètre afin de localiser l'événement sur la longueur du guide (10) d'ondes.
EP99957747A 1998-12-18 1999-11-19 Appareil et procede destines a surveiller une structure a l'aide d'un procede de propagation opposee de signaux pour localiser des evenements Withdrawn EP1151279A4 (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
AUPP7808A AUPP780898A0 (en) 1998-12-18 1998-12-18 Counter-propagating signal method for locating events in fibre optic sensor systems
AUPP780898 1998-12-18
AUPP012699 1999-05-03
AUPP012699 1999-05-03
PCT/AU1999/001028 WO2000037925A1 (fr) 1998-12-18 1999-11-19 Appareil et procede destines a surveiller une structure a l'aide d'un procede de propagation opposee de signaux pour localiser des evenements

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EP1151279A1 true EP1151279A1 (fr) 2001-11-07
EP1151279A4 EP1151279A4 (fr) 2007-12-05

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2204204A (en) * 1987-01-03 1988-11-02 Plessey Co Plc Deformation location in optical fibres
WO1996008695A1 (fr) * 1994-09-13 1996-03-21 Future Fibre Technologies Pty. Ltd. Capteurs optiques et procede de production de capteurs a detection de mode pour fibres optiques
JPH10160635A (ja) * 1996-12-03 1998-06-19 Nippon Telegr & Teleph Corp <Ntt> 多心光ファイバのスキュー検査方法およびスキュー検査装置

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2204204A (en) * 1987-01-03 1988-11-02 Plessey Co Plc Deformation location in optical fibres
WO1996008695A1 (fr) * 1994-09-13 1996-03-21 Future Fibre Technologies Pty. Ltd. Capteurs optiques et procede de production de capteurs a detection de mode pour fibres optiques
JPH10160635A (ja) * 1996-12-03 1998-06-19 Nippon Telegr & Teleph Corp <Ntt> 多心光ファイバのスキュー検査方法およびスキュー検査装置

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 1998, no. 11, 30 September 1998 (1998-09-30) & JP 10 160635 A (NIPPON TELEGR &TELEPH CORP <NTT>), 19 June 1998 (1998-06-19) *
See also references of WO0037925A1 *

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