GB2197953A - Acoustic sensor - Google Patents

Acoustic sensor Download PDF

Info

Publication number
GB2197953A
GB2197953A GB08628367A GB8628367A GB2197953A GB 2197953 A GB2197953 A GB 2197953A GB 08628367 A GB08628367 A GB 08628367A GB 8628367 A GB8628367 A GB 8628367A GB 2197953 A GB2197953 A GB 2197953A
Authority
GB
United Kingdom
Prior art keywords
sensor
elements
acoustic
acoustic sensor
optical fibre
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.)
Granted
Application number
GB08628367A
Other versions
GB2197953B (en
GB8628367D0 (en
Inventor
Michael Laurence Henning
Christopher Lamb
David Havard
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.)
Plessey Co Ltd
Original Assignee
Plessey Co 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
Application filed by Plessey Co Ltd filed Critical Plessey Co Ltd
Priority to GB8628367A priority Critical patent/GB2197953B/en
Publication of GB8628367D0 publication Critical patent/GB8628367D0/en
Priority to EP19870907617 priority patent/EP0298090A1/en
Priority to PCT/GB1987/000850 priority patent/WO1988004032A1/en
Priority to AU82384/87A priority patent/AU8238487A/en
Publication of GB2197953A publication Critical patent/GB2197953A/en
Application granted granted Critical
Publication of GB2197953B publication Critical patent/GB2197953B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H9/00Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by using radiation-sensitive means, e.g. optical means
    • G01H9/004Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by using radiation-sensitive means, e.g. optical means using fibre optic sensors
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H17/00Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves, not provided for in the preceding groups
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R33/00Arrangements or instruments for measuring magnetic variables
    • G01R33/02Measuring direction or magnitude of magnetic fields or magnetic flux
    • G01R33/032Measuring direction or magnitude of magnetic fields or magnetic flux using magneto-optic devices, e.g. Faraday or Cotton-Mouton effect
    • G01R33/0327Measuring direction or magnitude of magnetic fields or magnetic flux using magneto-optic devices, e.g. Faraday or Cotton-Mouton effect with application of magnetostriction

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Measuring Fluid Pressure (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Abstract

An acoustic sensor comprising a sensor element (1) and a compensation element (4), the two elements having different sensitivities and being positioned together such that they will both be subject to the same spectrum of disturbing phenomena, outputs from the two elements (1, 4) being applied to suitable circuit means to provide an acoustic output signal in which noise due to unwanted vibration effects is substantially reduced. The sensor element may be an optical fibre core surrounded by a jacket of a plastics material and the compensation element may be a similar core with a rubber jacket. The construction is suitable for a linear or a planar optical fibre sensor array.

Description

ACOUSTIC SENSOR This invention relates to an acoustic sensor. It relates particularly to a sensor construction that can be used to form a linear or a planar arrangement of sensitive pattern and in which the effect of one source of interference with the possible output of the sensor can be reduced.
In many applications of an acoustic sensor, the device is required.to detect acoustic signals in an environment where there is a high ambient level of vibration, for example in the presence of machinery noise.
One example of this is in the construction of a hydrophone which is intended to be towed behind a marine vessel or to be mounted in a planar arrangement as a flank array on a hull surface of the vessel. The output from such a hydrophone will be heavily influenced by vibration from the vessel's own machinery and this will make it difficult for any weaker signals to be detected. Sometimes it has been proposed that the sensing system which receives signals from the hydrophone will have a built-in capability for cancelling out the unwanted noise. The present invention provides an alternative approach in which the sensor itself has an inherent ability to reject the unwanted noise.
According to the invention, there is provided an acoustic sensor comprising a sensor element and a compensation element, the two elements having different sensitivities and being positioned together such that they will both be subject to the same spectrum of disturbing phenomena, outputs from the two elements being applied to suitable circuit means to provide an acoustic output signal in which noise due to unwanted vibration effects is substantially reduced.
Preferably, the elements comprise similar core constructions which are encapsulated in jacket materials having differing sensitivities to mechanical loads, such that one element is sensitive and the other element is insensitive to ambient pressure changes. The two elements may be located together in an interleaved arrangement whereby they will be subjected to similar acoustic and mechanical stresses when in operation.
The elements may be constructed in linear form such as an optical fibre, a length of piezoelectric plastics material or a piezoelectric rubber strip. Where the final sensor shape is required to be in a planar rather than a linear form, the shape nay be formed from a spirally sound or folded arrangement of the linear form.
By way of example, some particular embodiments of the invention will now be described with reference to the acconpanying drawing, in which: Figure 1 shows an acoustic sensor element comprising an optical fibre in a jacket of a plastics material; Figure 2 is a cross-sectional view on an enlarged scale of the element of Figure 1; Figure 3 shows the element interleaved with a similar element and formed into a spiral transducer; Figure 4 shows a different arrangement where the elements are interleaved into a curvilinear transducer; Figure 5 shows a further arrangement where the elements have been positioned one above the other as a stacked transducer; Figure 6 shows sensor elements arranged in a line to forr.. a towable array, and; Figure 7 is a circuit diagram of the optical and electronic circuits of the acoustic sensor.
As shown in Figures 1 and 2, an acoustic sensor element 1 comprises an optical fibre core 2 which is surrounded by a jacket 3 of a plastics material. In this example, the jacket 3 is of a thermoplastic plastics material and this has resulted in the element 1 becoming a hydrostatically pressure-sensitive sensor.
A compensation element 4 may be constructed by taking an identical core 2 and forming the jacket 3 of a rubber composition. This results an the element becoming a hydrostatically pressure-insensitive sensor.
The sensitivity of an optical fibre to mechanical strain depends upon the nature of the strain and the encapsulant in which the fibre is embedded. As a generalisation, an encapsulant with high Young's Modulus will always produce low sensitivity. However, an encapsulant with low Young's Modulus and low Poisson's ratio produces high sensitivity to hydrostatic stress whilst a high Poisson's ratio produces virtually zero sensitivity to hydrostatic pressure. Thus two coils of fibre identical in every respect save the nature of their secondary jackets can be made to have very different sensitivity to various mechanical loads.
The two forms of element may be fastened alongside one another so that in operation they will both be subject to the same spectrum of disturbing phenomena. It is convenient if the two forms of element are joined together by a semi-reflecting splice 6 at one end so that the elements are effectively connected in series. This construction is then capable of being towed behind a marine vessel for use as a hydrophone.
In order to obtain an output signal from the resulting hydrophone, a coherent light pulse or a light pulse pair is launched into the fibre which in the marine environment is being subjected to deforming forces such as acoustic waves. A suitable sensing system for sensing acoustic waves is disclosed in our published United Kingdom Patent Application No. 2126820A. This system thus acts to control the production of the light pulses and it receives an output light signal at an output end of the fibre as well as any small proportion of the original pulse that may be transmitted back to the input end by reflection from the splice located between the two element bodies.The sensing system then is capable p providing an output signal and, by use of the sensing and compensating elements of the present invention, any noise in this signal due to unwanted vibration effects has been substantially reduced.
Figure 3 shows a different construction of acoustic sensor where the twin pair of elements comprising a sensor element 1 and compensation element 4, joined at one end by a semi-reflecting splice 6, have been coiled into a flat spiral. After a suitable encapsulation process to give mechanical protection to the sensors, this construction forms a planar pattern of sensor which could for example be mounted as a flank array on the hull surface of a marine vessel.
Figure 4 shows a different arrangement where the interleaved elements haçe been folded to fonn a curvilinear transducer. This arrangement would be also suitable for mounting on a flat surface such as the hull of a vessel.
Figure 5 is a side view of a stacked transducer where the semi-reflecting splice 6 has been located within the thickness of the two layers of the device and the construction is supported in a body 7 of an encapsulation material.
Figure 6 shows a number of linear optical fibre sensor elements arranged in a line to form a towable array. The sensor elements 1 have references S1, S2, 53, etc. whilst the insensitive vibration compensation elements 4 with references S1', S2', S3' etc. are arranged to be interleaved with the sensor elements 1. A reference sensor 2 is provided to cancel out the effects of system phase noise as disclosed in our copending United Kingdom Patent Application No. 8525924. Semi-reflecting splices rl, r2, r3, etc. are located at the junctions between the sensor and compensation elements.
When the towed array is being used under water, it receives, in operation, acoustic signals al, a2, a3, etc.
which impinge on the sensor elements S1, 52, S3, of the array. Of course, the acoustic signals al, a2, a3, etc.
similarly impinge on the compensation elements S1', S2', S3' etc. but these elements have a built-in lack of sensitivity to hydrostatic pressures and they are not affected.
In this construction, the light pulses enter the array from the left hand end and pass through the first semi-reflecting splice rl, then the reference sensor R and enter the second semi-reflecting splice r2. At each semi-reflecting splice, a small proportion of the signal passing along the fibre is reflected back to the beginning of the fibre whilst the remainder of the signal passes through the splice and enters the next length of the optical fibre in the array.
After the second splice r2, the entering light pulses pass into the first sensor element S1 which is capable of being disturbed by the acoustic signal al that may be present in the aquatic environment where the towable array is being used. At the end of the sensor element S1, the entering light pulses pass through the third splice r3 and enter a further sensor element S1' which is arranged to be in a vibration compensation situation with the sensor element S1 as has been already described.
The light pulses entering the array at the left hand end as shown in Figure 6 are produced by an optical circuit as depicted at the left hand side of Figure 7.
Similarly, the pulses reflected back from the splices in the array are returned to the optical circuit. The optical circuit depicted is similar to that disclosed in our aforementioned copending patent application, where a laser 8 produces light pulses that are directed through a Bragg cell 9 and into a downlead 11 leading to the sensor array.
Light pulses returned from the array pass back along the downlead 11 and into the Bragg cell 9 where they are deflected via a mirror 12 onto a photo detector 13. The photo detector 13 forms part of the electronic circuit depicted at the right hand side of Figure 7.
The electronic circuit shown is similar to that disclosed in the aforementioned copending patent application where the photo detector 13 is connected through an amplifier 14 to demultiplexing means 16. The demultiplexed signals together with a reference signal are fed via band-pass filters 17 to demodulators 18. Phase noise and microphony compensation is provided by difference amplifiers 19 and further difference amplifiers 21 give vibration and acceleration compensation. Finally, electrical output signals al and a2 are produced and these are proportional to the acoustic signals which impinged on the sensor elements of the array as described in connection with Figure 6.
It will be apparent that the arrangement in the towable array of Figure 6 of a sensor element together with a compensation element, arranged such that they will both be subject to the same spectrum of disturbing phenomena, has given the resulting acoustic sensor a built-in ability to reject noise due to unwanted vibration effects since the two elements react differently to hydrostatic pressures. The electronic circuit can of course be used to provide compensation against further disturbances such as microphony and sensitivity to inputs other than acoustic.
The foregoing description of embodiments of the invention has been given by way of example only and a number of modifications may be made without departing from the scope of the invention as defined in the appended claims. For instance, although the principle of the invention has been described in connection with an optical fibre hydrophone, the invention will also be suitable for other types of linear array such as a cable made from a polyvinylidene fluoride plastics material, a piezoelectric ceramic material or a ceramic loaded rubber. Other configurations of sensor such as a planar shape which may be attached to a surface are also possible. Since the principle of the invention relies on the use of different coatings to provide different sensitivities in the two parts of the sensor, the invention may also be applied to other devices such as an optical fibre magnetometer.

Claims (7)

1. An acoustic sensor comprising a sensor element and a compensation element, the two elements having different sensitivities and being positioned together such that they will both be subject to the same spectrum of disturbing phenomena, outputs from the two elements being applied to suitable circuit means to provide an acoustic output signal in which noise due to unwanted vibration effects is substantially reduced.
2. A sensor as claimed in Claim 1, in which the elements comprise similar core constructions which are encapsulated in jacket materials having differing sensitivities to mechanical loads, such that one element is sensitive and the other element is insensitive to ambient pressure changes.
3. A sensor as claimed in Claim 2, in which the two elements are located together in an interleaved arrangement whereby they will be subjected to similar acoustic and mechanical stresses when in operation.
4. A sensor as claimed in any one of Claims 1 to 3, in which the said elements are fibre optic devices.
5. An optical fibre hydrophone or magnetometer comprising an acoustic sensor as claimed in Claim 4.
6. An acoustic sensor substantially as hereinbefore described with reference to the accompanying drawing.
The preceding claims have been superseded by the following claims: CLAIMS 1. An acoustic sensor comprising a sensor element and a compensation element. the two elements having different sensitivities and being positioned together such that they will both be subject to the same spectrum of disturbing phenomena, outputs from the two elements being applied to suitable circuit means to provide an acoustic output signal in which noise due to unwanted vibration effects is substantially reduced. in which the elements comprise similar core constructions which are encapsulated in jacket materials having differing sensitivities to mechanical loads, such that one element is sensitive and the other element is insensitive to ambient pressure changes.
2. A sensor as claimed in Claim 1, in which the two elements are located together in an interleaved arrangement whereby they will be subjected to similar acoustic and mechanical stresses when in operation.
3. A sensor as claimed in Claim 1 or 2 in which the said elements are fibre optic devices.
4. A sensor as claimed in any one of Claims 1 to 3 in which the two elements are shaped so as to form a spirally wound transducer.
5. A sensor as claimed in any one of Claims 1 to 3, in which the elements are shaped in a spirally wound or folded arrangement to give a planar form of transducer.
6. An optical fibre hydrophone or magnetometer comprising an acoustic sensor as claimed in any one of Claims 1 to 5.
7. An acoustic sensor substantially as hereinbefore described with reference to the accompanying drawing.
GB8628367A 1986-11-27 1986-11-27 Acoustic sensor Expired - Fee Related GB2197953B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB8628367A GB2197953B (en) 1986-11-27 1986-11-27 Acoustic sensor
EP19870907617 EP0298090A1 (en) 1986-11-27 1987-11-27 Acoustic sensor
PCT/GB1987/000850 WO1988004032A1 (en) 1986-11-27 1987-11-27 Acoustic sensor
AU82384/87A AU8238487A (en) 1986-11-27 1987-11-27 Acoustic sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8628367A GB2197953B (en) 1986-11-27 1986-11-27 Acoustic sensor

Publications (3)

Publication Number Publication Date
GB8628367D0 GB8628367D0 (en) 1987-07-08
GB2197953A true GB2197953A (en) 1988-06-02
GB2197953B GB2197953B (en) 1990-06-06

Family

ID=10608032

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8628367A Expired - Fee Related GB2197953B (en) 1986-11-27 1986-11-27 Acoustic sensor

Country Status (4)

Country Link
EP (1) EP0298090A1 (en)
AU (1) AU8238487A (en)
GB (1) GB2197953B (en)
WO (1) WO1988004032A1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2250588A (en) * 1990-12-06 1992-06-10 Marconi Gec Ltd Optical fibre coil with self adjusting pressure compensation
FR2748108A1 (en) * 1996-04-26 1997-10-31 Marconi Gec Ltd FIBER OPTIC DETECTION SYSTEM
WO2007023260A1 (en) * 2005-08-23 2007-03-01 Qinetiq Limited Demodulation of phase modulated fibre-optic sensor system signals
WO2012084997A2 (en) 2010-12-21 2012-06-28 Shell Internationale Research Maatschappij B.V. Detecting the direction of acoustic signals with a fiber optical distributed acoustic sensing (das) assembly
US20130208283A1 (en) * 2010-10-14 2013-08-15 Fiber Sensys, Inc. Variable sensitivity interferometer systems
US20130211726A1 (en) * 2009-12-23 2013-08-15 Jeffery Joseph Mestayer Detecting broadside and directional acoustic signals with a fiber optical distributed acoustic sensing (das) assembly
WO2014064460A2 (en) * 2012-10-26 2014-05-01 Optasense Holdings Limited Fibre optic cable for acoustic/seismic sensing
GB2515415A (en) * 2009-05-27 2014-12-24 Silixa Ltd Method and apparatus for optical sensing
GB2515574A (en) * 2013-06-28 2014-12-31 Tgs Geophysical Company Ltd Distributed optical sensing
US9655526B2 (en) 2014-09-30 2017-05-23 Shenzhen Darma Technology Co., Ltd. Vital signs fiber optic sensor systems and methods

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0919902D0 (en) * 2009-11-13 2009-12-30 Qinetiq Ltd Improvements in fibre optic cables for distributed sensing
US9638821B2 (en) 2014-03-20 2017-05-02 Lockheed Martin Corporation Mapping and monitoring of hydraulic fractures using vector magnetometers
US9910104B2 (en) 2015-01-23 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US10241158B2 (en) 2015-02-04 2019-03-26 Lockheed Martin Corporation Apparatus and method for estimating absolute axes' orientations for a magnetic detection system
US10520558B2 (en) 2016-01-21 2019-12-31 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with nitrogen-vacancy center diamond located between dual RF sources
US9910105B2 (en) 2014-03-20 2018-03-06 Lockheed Martin Corporation DNV magnetic field detector
US10088452B2 (en) 2016-01-12 2018-10-02 Lockheed Martin Corporation Method for detecting defects in conductive materials based on differences in magnetic field characteristics measured along the conductive materials
US20170212258A1 (en) * 2016-01-21 2017-07-27 Lockheed Martin Corporation Hydrophone
US10120039B2 (en) 2015-11-20 2018-11-06 Lockheed Martin Corporation Apparatus and method for closed loop processing for a magnetic detection system
US9853837B2 (en) 2014-04-07 2017-12-26 Lockheed Martin Corporation High bit-rate magnetic communication
US9614589B1 (en) 2015-12-01 2017-04-04 Lockheed Martin Corporation Communication via a magnio
US10088336B2 (en) 2016-01-21 2018-10-02 Lockheed Martin Corporation Diamond nitrogen vacancy sensed ferro-fluid hydrophone
US9824597B2 (en) 2015-01-28 2017-11-21 Lockheed Martin Corporation Magnetic navigation methods and systems utilizing power grid and communication network
US10168393B2 (en) 2014-09-25 2019-01-01 Lockheed Martin Corporation Micro-vacancy center device
US10338162B2 (en) 2016-01-21 2019-07-02 Lockheed Martin Corporation AC vector magnetic anomaly detection with diamond nitrogen vacancies
US10006973B2 (en) 2016-01-21 2018-06-26 Lockheed Martin Corporation Magnetometer with a light emitting diode
CA2945016A1 (en) 2014-04-07 2015-10-15 Lockheed Martin Corporation Energy efficient controlled magnetic field generator circuit
EP3248021A4 (en) * 2015-01-23 2018-12-12 Lockheed Martin Corporation Dnv magnetic field detector
WO2016118756A1 (en) 2015-01-23 2016-07-28 Lockheed Martin Corporation Apparatus and method for high sensitivity magnetometry measurement and signal processing in a magnetic detection system
EP3251193A4 (en) 2015-01-28 2018-08-08 Lockheed Martin Corporation In-situ power charging
WO2016126436A1 (en) 2015-02-04 2016-08-11 Lockheed Martin Corporation Apparatus and method for recovery of three dimensional magnetic field from a magnetic detection system
WO2017078766A1 (en) 2015-11-04 2017-05-11 Lockheed Martin Corporation Magnetic band-pass filter
WO2017087014A1 (en) 2015-11-20 2017-05-26 Lockheed Martin Corporation Apparatus and method for hypersensitivity detection of magnetic field
WO2017127081A1 (en) 2016-01-21 2017-07-27 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with circuitry on diamond
GB2562957A (en) 2016-01-21 2018-11-28 Lockheed Corp Magnetometer with light pipe
WO2017127090A1 (en) 2016-01-21 2017-07-27 Lockheed Martin Corporation Higher magnetic sensitivity through fluorescence manipulation by phonon spectrum control
WO2017127095A1 (en) 2016-01-21 2017-07-27 Lockheed Martin Corporation Diamond nitrogen vacancy sensor with common rf and magnetic fields generator
US10345396B2 (en) 2016-05-31 2019-07-09 Lockheed Martin Corporation Selected volume continuous illumination magnetometer
US10571530B2 (en) 2016-05-31 2020-02-25 Lockheed Martin Corporation Buoy array of magnetometers
US10677953B2 (en) 2016-05-31 2020-06-09 Lockheed Martin Corporation Magneto-optical detecting apparatus and methods
US20170343621A1 (en) 2016-05-31 2017-11-30 Lockheed Martin Corporation Magneto-optical defect center magnetometer
US10228429B2 (en) 2017-03-24 2019-03-12 Lockheed Martin Corporation Apparatus and method for resonance magneto-optical defect center material pulsed mode referencing
US10145910B2 (en) 2017-03-24 2018-12-04 Lockheed Martin Corporation Photodetector circuit saturation mitigation for magneto-optical high intensity pulses
US10371765B2 (en) 2016-07-11 2019-08-06 Lockheed Martin Corporation Geolocation of magnetic sources using vector magnetometer sensors
US10317279B2 (en) 2016-05-31 2019-06-11 Lockheed Martin Corporation Optical filtration system for diamond material with nitrogen vacancy centers
US10408890B2 (en) 2017-03-24 2019-09-10 Lockheed Martin Corporation Pulsed RF methods for optimization of CW measurements
US10330744B2 (en) 2017-03-24 2019-06-25 Lockheed Martin Corporation Magnetometer with a waveguide
US10274550B2 (en) 2017-03-24 2019-04-30 Lockheed Martin Corporation High speed sequential cancellation for pulsed mode
US10527746B2 (en) 2016-05-31 2020-01-07 Lockheed Martin Corporation Array of UAVS with magnetometers
US10345395B2 (en) 2016-12-12 2019-07-09 Lockheed Martin Corporation Vector magnetometry localization of subsurface liquids
US10281550B2 (en) 2016-11-14 2019-05-07 Lockheed Martin Corporation Spin relaxometry based molecular sequencing
US10359479B2 (en) 2017-02-20 2019-07-23 Lockheed Martin Corporation Efficient thermal drift compensation in DNV vector magnetometry
US10338163B2 (en) 2016-07-11 2019-07-02 Lockheed Martin Corporation Multi-frequency excitation schemes for high sensitivity magnetometry measurement with drift error compensation
US10371760B2 (en) 2017-03-24 2019-08-06 Lockheed Martin Corporation Standing-wave radio frequency exciter
US10379174B2 (en) 2017-03-24 2019-08-13 Lockheed Martin Corporation Bias magnet array for magnetometer
US10338164B2 (en) 2017-03-24 2019-07-02 Lockheed Martin Corporation Vacancy center material with highly efficient RF excitation
US10459041B2 (en) 2017-03-24 2019-10-29 Lockheed Martin Corporation Magnetic detection system with highly integrated diamond nitrogen vacancy sensor

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1088469A (en) * 1964-02-13 1967-10-25 Charles George Mcburney Method and underwater streamer apparatus for improving the fidelity of recorded seismic signals
GB2184237A (en) * 1985-10-21 1987-06-17 Plessey Co Plc Acoustic wave sensing systems

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4297887A (en) * 1980-02-19 1981-11-03 The United States Of America As Represented By The Secretary Of The Navy High-sensitivity, low-noise, remote optical fiber
US4363114A (en) * 1981-01-21 1982-12-07 The United States Of America As Represented By The Secretary Of The Navy Low noise remote optical fiber sound detector
GB2126820B (en) * 1982-07-17 1986-03-26 Plessey Co Plc An optical sensing system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1088469A (en) * 1964-02-13 1967-10-25 Charles George Mcburney Method and underwater streamer apparatus for improving the fidelity of recorded seismic signals
GB2184237A (en) * 1985-10-21 1987-06-17 Plessey Co Plc Acoustic wave sensing systems

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2250588A (en) * 1990-12-06 1992-06-10 Marconi Gec Ltd Optical fibre coil with self adjusting pressure compensation
US5237632A (en) * 1990-12-06 1993-08-17 Gec-Marconi Limited Optical fibre coil assemblies
GB2250588B (en) * 1990-12-06 1994-06-22 Marconi Gec Ltd Improvements relating to optical fibre coil assemblies
FR2748108A1 (en) * 1996-04-26 1997-10-31 Marconi Gec Ltd FIBER OPTIC DETECTION SYSTEM
WO2007023260A1 (en) * 2005-08-23 2007-03-01 Qinetiq Limited Demodulation of phase modulated fibre-optic sensor system signals
US8023829B2 (en) 2005-08-23 2011-09-20 Qinetiq Limited Demodulation of phase modulated fibre-optic sensor system signals
US9541425B2 (en) 2009-05-27 2017-01-10 Silixa Limited Method and apparatus for optical sensing
GB2515415B (en) * 2009-05-27 2015-04-22 Silixa Ltd Fibre arrangements for optical sensing.
US11802789B2 (en) 2009-05-27 2023-10-31 Silixa Ltd. Method and apparatus for optical sensing
US11079269B2 (en) 2009-05-27 2021-08-03 Silixa Limited Method and apparatus for optical sensing
US9541426B2 (en) 2009-05-27 2017-01-10 Silica Limited Optical sensor and method of use
US9140582B2 (en) 2009-05-27 2015-09-22 Silixa Limited Optical sensor and method of use
GB2515415A (en) * 2009-05-27 2014-12-24 Silixa Ltd Method and apparatus for optical sensing
US9080949B2 (en) * 2009-12-23 2015-07-14 Shell Oil Company Detecting broadside and directional acoustic signals with a fiber optical distributed acoustic sensing (DAS) assembly
US20130211726A1 (en) * 2009-12-23 2013-08-15 Jeffery Joseph Mestayer Detecting broadside and directional acoustic signals with a fiber optical distributed acoustic sensing (das) assembly
US20130208283A1 (en) * 2010-10-14 2013-08-15 Fiber Sensys, Inc. Variable sensitivity interferometer systems
WO2012084997A3 (en) * 2010-12-21 2013-04-04 Shell Internationale Research Maatschappij B.V. Detecting the direction of acoustic signals with a fiber optical distributed acoustic sensing (das) assembly
US9322702B2 (en) 2010-12-21 2016-04-26 Shell Oil Company Detecting the direction of acoustic signals with a fiber optical distributed acoustic sensing (DAS) assembly
WO2012084997A2 (en) 2010-12-21 2012-06-28 Shell Internationale Research Maatschappij B.V. Detecting the direction of acoustic signals with a fiber optical distributed acoustic sensing (das) assembly
WO2014064460A3 (en) * 2012-10-26 2014-06-12 Optasense Holdings Limited Fibre optic cable for acoustic/seismic sensing
WO2014064460A2 (en) * 2012-10-26 2014-05-01 Optasense Holdings Limited Fibre optic cable for acoustic/seismic sensing
US9816853B2 (en) 2012-10-26 2017-11-14 Optasense Holdings Limited Fibre optic cable for acoustic/seismic sensing
GB2515574A (en) * 2013-06-28 2014-12-31 Tgs Geophysical Company Ltd Distributed optical sensing
US9655526B2 (en) 2014-09-30 2017-05-23 Shenzhen Darma Technology Co., Ltd. Vital signs fiber optic sensor systems and methods

Also Published As

Publication number Publication date
WO1988004032A1 (en) 1988-06-02
GB2197953B (en) 1990-06-06
EP0298090A1 (en) 1989-01-11
GB8628367D0 (en) 1987-07-08
AU8238487A (en) 1988-06-16

Similar Documents

Publication Publication Date Title
GB2197953A (en) Acoustic sensor
US5155548A (en) Passive fiber optic sensor with omnidirectional acoustic sensor and accelerometer
US4297887A (en) High-sensitivity, low-noise, remote optical fiber
US5140559A (en) Low flow-noise conformal fiber optic hydrophone
US5218197A (en) Method and apparatus for the non-invasive measurement of pressure inside pipes using a fiber optic interferometer sensor
US6314056B1 (en) Fiber optic sensor system and method
US5475216A (en) Fiber optic sensor having mandrel wound reference and sensing arms
US6959604B2 (en) Apparatus and method having an optical fiber disposed circumferentially around the pipe for measuring unsteady pressure within a pipe
US5363342A (en) High performance extended fiber optic hydrophone
US5155707A (en) Omni-directional hydrophone
US5646401A (en) Fiber optic grating and etalon sensor systems
EP1110066B1 (en) Seismic optical acoustic recursive sensor system
AU665490B2 (en) Fiber optic planar hydrophone
US5140154A (en) Inline fiber optic sensor arrays with delay elements coupled between sensor units
EP0027540A2 (en) Optical sensor and transducer array system
GB2272345A (en) Hydrophones
SE434434B (en) FIBEROPTIC LUMINISCENSORS WITH INTERFERENCE IN THIN LAYER STRUCTURES
US5237632A (en) Optical fibre coil assemblies
US5206923A (en) Method to use an optical fibre as a sensor
US5253222A (en) Omnidirectional fiber optic hydrophone
US5394378A (en) Hydrophone transduction mechanism
US6002646A (en) Portable optical range tracking array
CN216160830U (en) Full optical fiber towed linear array
CN113466871A (en) All-fiber towed linear array
Garrett et al. General purpose fiber optic hydrophone made of castable epoxy

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931127