EP3084489A1 - Verfahren zur herstellung einer behandelten glasfaser für einen strahlungsbeständigen temperatursensor - Google Patents

Verfahren zur herstellung einer behandelten glasfaser für einen strahlungsbeständigen temperatursensor

Info

Publication number
EP3084489A1
EP3084489A1 EP14823950.2A EP14823950A EP3084489A1 EP 3084489 A1 EP3084489 A1 EP 3084489A1 EP 14823950 A EP14823950 A EP 14823950A EP 3084489 A1 EP3084489 A1 EP 3084489A1
Authority
EP
European Patent Office
Prior art keywords
optical fiber
fiber
annealing
temperature
bragg grating
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Withdrawn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
EP14823950.2A
Other languages
English (en)
French (fr)
Inventor
Jocelyn Perisse
Adriana MORANA
Emmanuel Marin
Jean-Reynald MACÉ
Sylvain Girard
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.)
Centre National de la Recherche Scientifique CNRS
Universite Jean Monnet Saint Etienne
Areva SA
Original Assignee
Centre National de la Recherche Scientifique CNRS
Universite Jean Monnet Saint Etienne
Areva SA
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 Centre National de la Recherche Scientifique CNRS, Universite Jean Monnet Saint Etienne, Areva SA filed Critical Centre National de la Recherche Scientifique CNRS
Publication of EP3084489A1 publication Critical patent/EP3084489A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02057Optical fibres with cladding with or without a coating comprising gratings
    • G02B6/02076Refractive index modulation gratings, e.g. Bragg gratings
    • G02B6/02123Refractive index modulation gratings, e.g. Bragg gratings characterised by the method of manufacture of the grating
    • G02B6/02128Internal inscription, i.e. grating written by light propagating within the fibre, e.g. "self-induced"
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/02Optical fibres with cladding with or without a coating
    • G02B6/02057Optical fibres with cladding with or without a coating comprising gratings
    • G02B6/02076Refractive index modulation gratings, e.g. Bragg gratings
    • G02B6/02171Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes
    • G02B6/02176Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes due to temperature fluctuations
    • G02B6/02185Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes due to temperature fluctuations based on treating the fibre, e.g. post-manufacture treatment, thermal aging, annealing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/0006Working by laser beam, e.g. welding, cutting or boring taking account of the properties of the material involved
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B25/00Annealing glass products
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C25/00Surface treatment of fibres or filaments made from glass, minerals or slags
    • C03C25/62Surface treatment of fibres or filaments made from glass, minerals or slags by application of electric or wave energy; by particle radiation or ion implantation
    • C03C25/6206Electromagnetic waves
    • C03C25/6208Laser
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/50Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
    • B23K2103/54Glass

Definitions

  • the present invention relates to a method of manufacturing a processed optical fiber for a temperature sensor, in which at least one Bragg grating is inscribed in the fiber with the aid of a laser, the Bragg grating extending longitudinally in a portion of the fiber and being adapted to reflect light waves propagating along the inscribed optical fiber.
  • the invention also relates to the use of such an optical fiber processed in a temperature sensor.
  • optical fibers comprising a Bragg grating (or FBG in English, for Fiber Bragg Grating) for measuring a temperature.
  • the Bragg grating is constituted by a periodic disturbance of the refractive index of the fiber core along the axis of the fiber.
  • the light propagating in the heart of the broadband spectrum fiber is reflected by the grating around a certain wavelength, called the "Bragg wavelength", which is a function of the pitch of the grating.
  • the Bragg wavelength varies depending on the temperature at which the Bragg grating is located, with a sensitivity of for example about 10 pm / ° C.
  • Bragg grating fiber optic sensors do not require local power supply, are insensitive to electromagnetic interference. They allow a long range offset between a measurement point and a measurement processing point, as well as the multiplexing of a large number of measurement points on the same fiber. They are also not very intrusive, and have a zero intrinsic drift.
  • the fiber optic sensors of the state of the art show their limits in severe environments in temperature and radiation. For high temperatures, for example above 300 ° C., and for radiation doses exceeding a few tens of kilogray, there is a gradual loss of the measurement by erasure of the Bragg grating, and or an offset of the Bragg wavelength inducing a drift of the measurement, and / or a loss of transmission of the optical fiber.
  • An object of the invention is therefore to provide a method for manufacturing a processed optical fiber for a temperature sensor, the fiber being able to withstand higher temperatures and higher radiation doses.
  • the subject of the invention is a method for manufacturing a processed optical fiber for a temperature sensor, comprising at least the following steps:
  • the method comprises one or more of the following characteristics, taken separately or in any technically possible combination:
  • step b) of inscription using the laser has a duration greater than or equal to
  • the optical fiber obtained is a monomode fiber
  • the optical fiber obtained is an optical fiber with a pure silica core or doped with one or more element (s) taken from fluorine and nitrogen;
  • the laser emits pulses, each pulse having a width less than or equal to 150 femtoseconds;
  • the optical fiber obtained comprises a core with a diameter of between 2 micrometers and 20 microns;
  • step b) during the inscription, the optical fiber is tensioned by a weight of 4 grams to 300 grams fixed on the optical fiber;
  • the inscribed fiber is heated to an annealing temperature greater than or equal to 500 ° C. for at least 15 minutes;
  • the method further comprises a step of determining a maximum temperature of use of the optical fiber treated as a component of a temperature sensor, and during the annealing step (140), the fiber inscribed (135) is brought to an annealing temperature, the difference between the annealing temperature and the maximum use temperature being between 100 ° C and 200 ° C.
  • the invention also relates to a use of at least one processed optical fiber obtained by a method as described above in a temperature sensor.
  • FIG. 1 is a schematic view of a temperature sensor according to the invention, comprising a treated optical fiber obtained by a method according to the invention
  • FIG. 2 is a graph illustrating the evolution of the Bragg wavelength of the Bragg grating of the treated optical fiber represented in FIG. 1 as a function of the revolution of the temperature to which the Bragg grating is subjected
  • FIG. 3 is a diagram showing the main steps of a method according to the invention adapted to manufacture the treated optical fiber represented in FIG. 1;
  • FIG. 4 is a graph illustrating the effect of different annealing temperatures on the Bragg peak of the Bragg grating of an optical fiber similar to that shown in FIG. 1;
  • FIG. 5 is a graph illustrating an offset of the Bragg wavelength of the Bragg grating of an optical fiber similar to that represented in FIG. 1 during two successive phases of irradiation,
  • FIG. 6 is a graph illustrating the effect of the treatment annealing step illustrated in FIG. 3 on the amplitude of the Bragg peak of a grating in a reference optical fiber obtained by a method different from FIG. that of the invention, and
  • FIG. 7 is a graph illustrating the effect of two successive irradiations on a fiber obtained by a process similar to that according to the invention, but whose annealing temperature differs from that of the invention.
  • the temperature sensor 1 comprises a treated optical fiber 5.
  • the temperature sensor 1 is for example intended to be placed in a nuclear reactor (not shown).
  • the sensor 1 is used to measure the temperature of a heat transfer fluid, such as the water of the primary cooling circuit of a pressurized water reactor, or the liquid sodium of a fast neutron reactor, or an installation of manufacture or storage of high-level nuclear waste.
  • the processed optical fiber 5 comprises a core 15, a peripheral portion 20, sometimes called an optical sheath, surrounding the core 15 around the axis D, and a Bragg grating 25 located in the core 15.
  • the processed optical fiber 5 comprises a plurality of Bragg gratings similar to the Bragg grating 25.
  • the treated optical fiber 5 is for example a pure silica fiber or a doped fiber, for example by fluorine and / or nitrogen.
  • the processed optical fiber 5 is single-mode at the Bragg wavelength of the Bragg grating 25.
  • element-doped is meant that the core or sheath of the doped fiber comprises at least 10 ppm of this element.
  • the core 15 has a DC diameter for example between 2 ⁇ and 20 ⁇ .
  • the Bragg grating 25 comprises an alternation of portions 27 and portions 29 along the axis D, the portions 29 having for example a refractive index higher than the refractive index of the portions 27.
  • the portions 29 having for example a refractive index higher than the refractive index of the portions 27.
  • a light signal 30 is sent into the treated optical fiber 5.
  • the light signal 30 comprises, for example, a symbolized wavelength range. by the curve 35.
  • the light signal 30 travels along the processed optical fiber 5 to the Bragg grating 25 which transmits a transmitted light signal 40, and reflects a reflected light signal 45.
  • the reflected light signal 45 has a wavelength range 50 in the shape of a peak, called a "Bragg peak".
  • the Bragg peak is centered on a wavelength ⁇ called “Bragg wavelength” of the Bragg grating 25.
  • the transmitted light signal 40 comprises a wavelength range 55 corresponding to the wavelength range minus the wavelength range 50.
  • FIG. 2 is a graph 100 comprising a curve C0 giving the evolution of the wavelength of Bragg ⁇ , in nanometer, as a function of the temperature T, in degrees Celsius, seen by the Bragg grating 25 of the optical fiber treated 5 shown in Figure 1.
  • the method 1 10 makes it possible to manufacture the treated optical fiber 5 represented in FIG. 1, adapted for the temperature sensor 1.
  • the method 1 comprises a step 120 of obtaining an optical fiber 125, a step 130 of writing a Bragg grating in the optical fiber 125 to obtain a listed fiber 135 comprising the Bragg grating 25, and a step 140 of annealing at least a portion of the inscribed fiber 135, to obtain the treated optical fiber 5.
  • step 130 several Bragg gratings are inscribed in the optical fiber 125.
  • the optical fiber 125 obtained is for example a monomode fiber, pure silica or advantageously doped with one or more elements selected from fluorine and / or nitrogen.
  • the method 1 further comprises a step 150 of determining a maximum operating temperature of the processed optical fiber as a component of the temperature sensor 1.
  • step 130 the longitudinal portion of the fiber 125 obtained in which the Bragg grating 25 is inscribed is denuded.
  • the inscription is made using a femtosecond laser, for example using the conventional mask technique. phase.
  • the focusing of the femtosecond laser is done with a cylindrical lens of short focal length, for example from twelve to nineteen millimeters.
  • femtosecond laser is meant a laser that produces pulses whose duration is of the order of a few femtoseconds to a few hundred femtoseconds.
  • the laser advantageously has an average power greater than or equal to 450 mW.
  • the laser emits pulses, each pulse having a width less than or equal to 150 femtoseconds.
  • the laser has for example a wavelength of 800 nm.
  • the optical fiber 125 is advantageously tensioned by a weight of 6 to 8 grams (not shown) attached to the optical fiber.
  • the inscribed fiber 135 is for example brought to an annealing temperature greater than or equal to 500 ° C, for at least fifteen minutes.
  • the inscribed fiber 135 is brought to an annealing temperature, the difference between the annealing temperature and the maximum use temperature determined in step 150 being between 100 ° C. C and 200 ° C.
  • the maximum temperature of use is 600 ° C and the annealing temperature is 750 ° C.
  • the Bragg grating 25 of the inscribed optical fiber 135 is then more or less erased by the annealing step 140.
  • Exposure parameters are determined to have stable Bragg gratings at the temperature of use of the treated optical fiber 5 and having interesting performance in terms of radiation resistance.
  • the radiation resistance of the Bragg grating increases with the annealing temperature.
  • the annealing temperature is 750 ° C
  • the Bragg grating has an offset (BWS) of its Bragg wavelength under irradiation less than the offset obtained when the annealing temperature is 350 ° C.
  • BWS offset of its Bragg wavelength under irradiation
  • no erasure phenomenon of the Bragg grating is observed under irradiation.
  • Fig. 4 is a graph 200 illustrating the effect of the annealing temperature on the Bragg peak.
  • Graph 200 includes four curves C1, C2, C3 and C4.
  • Curve C1 represents the Bragg peak of the Bragg grating 25 in the absence of annealing step 140.
  • Curves C2, C3 and C4 respectively represent the Bragg peak of the Bragg grating obtained for annealing temperatures of 300 ° C, 550 ° C and 750 ° C, respectively.
  • the Bragg grating is obtained from a fluorine-doped silica core fiber inscribed using a femtosecond laser with an average power of 500 mW and a wavelength of 800. nm.
  • Each curve C1 to C4 gives the evolution of the intensity of the reflected light signal 45, in decibels, as a function of the wavelength in nanometers.
  • Each curve C1 to C4 is analogous to the range of wavelengths 50 shown in FIG.
  • the gradual rise in the annealing temperature causes an attenuation of the Bragg peak, as well as a shift of the Bragg wavelength ⁇ towards the shorter wavelengths.
  • FIG. 5 is a graph 300 illustrating the radiation resistance of the Bragg grating 25 of a processed optical fiber obtained by the same method as for graph 200, with an annealing temperature of 750 ° C.
  • the graph 300 comprises a curve C5 illustrating the evolution, as a function of the time t in seconds, on the one hand of the shift ⁇ of the Bragg wavelength in nanometers, and on the other hand of the AND error, in degree Celsius, committed on the measured temperature.
  • the offset ⁇ is read on the left y-axis of graph 300, while the AND error is read on the right y-axis of graph 300.
  • the Bragg grating 25 of the treated optical fiber 5 is irradiated at a constant dose rate.
  • the dose received at the end of the first phase A is 1.5 MGy (megagray).
  • a third phase C of a duration of approximately 30,000 seconds again the Bragg grating 25 is irradiated under the same conditions as in the first phase A, that is to say that it receives again a dose equal to 1, 5 MGy.
  • the wavelength of Bragg begins to decrease by four pm (picometers), and then goes up about twelve pm gradually during the first phase A. This drift of the wavelength of Bragg corresponds to a error ET1 (FIG. 5) on the temperature measured by the sensor 1 of approximately 0.4 ° C.
  • the Bragg wavelength decreases sharply to stabilize at about twelve microns below the initial value.
  • the Bragg wavelength rises sharply substantially to the value it had at the end of the first phase A and remains relatively stable throughout the third phase C.
  • the drift of the wavelength of Bragg during the third phase C corresponds to an error ET2 on the measured temperature of the order of 0.4 ° C.
  • FIGs 6 and 7 illustrate the result of parametric studies conducted to determine the impact of non-compliance with one of the process steps 1 10.
  • FIG. 6 is a graph 400 having a curve C6 illustrating the effect of the annealing temperature T in degrees Celsius (on the abscissa) on the normalized amplitude AN (ordinate) of the Bragg peak of the Bragg grating 25 when the Step 130 of inscription was carried out using a femtosecond laser with a power of 400 mW, instead of 500 mW as in Figure 4.
  • the curve C6 comprises a first point 410 giving the amplitude of the Bragg peak in the absence of annealing step.
  • the amplitude is then 16 dB and corresponds to the maximum of the curve C1 in FIG. 4. This amplitude of 16 dB is normalized to 1.0 on the graph 400 of FIG. 6.
  • curve C6 shows the progressive reduction of the normalized amplitude AN of the Bragg peak when the annealing temperature T is respectively 300 ° C., 550 ° C. and 750 ° C.
  • the curve C6 ' also shows the progressive reduction of the normalized amplitude AN of the Bragg peak when the annealing temperature T is respectively 300 ° C., 550 ° C. and 750 ° C., when the inscription step 130 is performed using a femtosecond laser with a power of 500 mW.
  • the Bragg grating 25 is considered annealing resistant if the normalized amplitude AN remains above a threshold of, for example, 0.2, ie, the attenuation of the amplitude of the Bragg peak is less than 7 dB in the example shown in FIG. 6.
  • FIG. 7 represents a graph 500 similar to graph 300 shown in FIG. 5.
  • Graph 500 comprises a curve C7 illustrating the radiation resistance of a Bragg grating obtained after an inscription step 130, wherein the laser power is 500 mW, and an annealing step 140 at a temperature below 500 ° C.
  • the phases A, B1 and C of the graph 500 are similar to the phases A, B and C of the graph 300.
  • the graph 500 comprises an additional phase B2 corresponding to a stop of the irradiation after the phase C.
  • the Bragg wavelength ⁇ of the Bragg grating 25 is much more sensitive to the two irradiation phases A and C than under the conditions of graph 300 of FIG. at the end of the third phase C corresponding to a second irradiation, the shift in the Bragg wavelength due to the irradiation is -60 pm. This corresponds to an error ET3 on the measured temperature equal to approximately 4.5 ° C.
  • the manufacturing method 1 makes it possible to obtain a treated optical fiber comprising a Bragg grating capable of better withstanding radiation doses greater than 1 MGy, and thus withstanding more radiation doses. strong as the optical fibers of the state of the art.
  • the optional feature that the inscribed fiber 135 is brought to an annealing temperature of 500 ° C or higher for at least fifteen minutes provides a Bragg grating capable of supporting a temperature of use of up to about 550 ° C.
  • the optional feature according to which, during the annealing step 140, the inscribed fiber 135 is brought to an annealing temperature makes it possible to obtain a Bragg grating 25 capable of withstanding a temperature of use equal to the annealing temperature minus a value of between 100 ° C and 200 ° C.
  • the power of the laser is expressed by a formula independent of the size of the beam and the length of the Bragg grating 25.
  • - E is laser pulse energy (in J) which is deduced from the power of the laser (in W) by dividing by the frequency of the pulses (in Hz),
  • A is a parameter related to the position of the fiber relative to the phase mask
  • p is the first order energy fraction (equal to 73%)

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Optics & Photonics (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Geochemistry & Mineralogy (AREA)
  • General Chemical & Material Sciences (AREA)
  • Electromagnetism (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
EP14823950.2A 2013-12-16 2014-12-16 Verfahren zur herstellung einer behandelten glasfaser für einen strahlungsbeständigen temperatursensor Withdrawn EP3084489A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1362691A FR3014866A1 (fr) 2013-12-16 2013-12-16 Procede de fabrication d'une fibre optique traitee pour capteur de temperature resistant aux radiations
PCT/EP2014/077987 WO2015091502A1 (fr) 2013-12-16 2014-12-16 Procédé de fabrication d'une fibre optique traitée pour capteur de température résistant aux radiations

Publications (1)

Publication Number Publication Date
EP3084489A1 true EP3084489A1 (de) 2016-10-26

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ID=50639641

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EP14823950.2A Withdrawn EP3084489A1 (de) 2013-12-16 2014-12-16 Verfahren zur herstellung einer behandelten glasfaser für einen strahlungsbeständigen temperatursensor

Country Status (6)

Country Link
US (1) US20160320558A1 (de)
EP (1) EP3084489A1 (de)
JP (1) JP2017507345A (de)
CN (1) CN106062598A (de)
FR (1) FR3014866A1 (de)
WO (1) WO2015091502A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108332878B (zh) * 2018-01-31 2020-09-18 北京航天控制仪器研究所 一种光纤光栅温度传感器及制备方法

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6665483B2 (en) * 2001-03-13 2003-12-16 3M Innovative Properties Company Apparatus and method for filament tensioning
US7336862B1 (en) * 2007-03-22 2008-02-26 General Electric Company Fiber optic sensor for detecting multiple parameters in a harsh environment
US7835605B1 (en) * 2009-05-21 2010-11-16 Hong Kong Polytechnic University High temperature sustainable fiber bragg gratings
CN102576125B (zh) * 2009-07-29 2014-12-10 拉瓦勒大学 使用短波长超快脉冲写入耐大功率的布拉格光栅的方法
CN102073095A (zh) * 2010-12-15 2011-05-25 华中科技大学 一种窄线宽光纤布拉格光栅的制作方法

Also Published As

Publication number Publication date
FR3014866A1 (fr) 2015-06-19
CN106062598A (zh) 2016-10-26
US20160320558A1 (en) 2016-11-03
WO2015091502A1 (fr) 2015-06-25
JP2017507345A (ja) 2017-03-16

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