The present application claims priority to EP08305231.6, filed on Jun. 4, 2008 in France.
The invention is related to a Fiber Optic Interferometric Sensors (FOIS) array.
The invention is also related to an apparatus for multiplexing/demultiplexing a Fiber Optic Interferometric Sensors (FOIS) array, and to a method for multiplexing/demultiplexing a FOIS array.
The invention can be dedicated to seismic sensing applications where the sensor arrays are made of several receiver points located at different places; each receiver point may contain several sensors.
Nevertheless, the invention is not limited to seismic sensing applications and can be dedicated to any sensing applications involving an array of FOISs spread into groups of sensors.
For seismic applications such as <<Deep Ocean Bottom Cable>> (DOBC), the arrays are made of several Receiver Points (RP), called nodes, distinct one from another and geographically spaced by a given distance. Each node comprises four sensors geographically located at the same point: the four sensors, one hydrophone and three geophones, form a Receiver Point or measurement node. The X-talk level required between the four sensors is very low.
Some external perturbations applied on an optical fiber length (pressure variations, temperature variations, vibrations, . . . ) cause the fiber length and index of refraction to change, leading to a change of the time propagation (or phase) of the light field propagating in the fiber. A FOIS is commonly made of two fibers: at its entrance, the light is divided into two optical fields:
A FOIS interrogating system ensures the reading of the phase difference between two optical fields. It is made of an optical source providing the light, a telemetry fiber bringing the light to the FOIS, a return fiber bringing the light from the FOIS to a photo-detector on which the combination of the two optical fields leads to an interferometric signal bearing the information on the phase difference between the two optical fields, and an electronic demodulation system computing the phase difference from the photo-detector output interferometric signal.
In some applications, the sensors involved in an array can be as many as a few thousands. The decision to go for such arrays mainly depends on their cost and reliability.
In a FOIS array, the interrogating system is ideally shared between several FOIS so as to reduce the array cost: the optical source, the telemetry and return fibers, the photo-detector, and the electronic demodulation system can interrogate many FOISs. A FOIS array is thus made of one or more optical sources, of which light is guided to a group of FOISs. Each FOIS locally brings its information on the optical field that goes through it. The return fiber brings the modified optical fields to one or more photo-detectors. The interferometric signals from the different FOISs then need to be separated or demultiplexed. Demultiplexing of the interferometric signals is achieved by:
As an example, the document <<Fiber interferometric sensor arrays with freedom from source phase induced noise>> in <<Optics Letters>>, vol. 11, July 1986, no7, pp. 473-475 (D1) presents a Time Division Multiplexing Technique. Detailed descriptions of the TDM and WDM techniques are, for example, disclosed in the patent application US 2007/0024857 (D1). The U.S. Pat. No. 5,959,294 (D3) discloses a method and apparatus for the interrogation of fiber optic interferometric sensors based on a FDM technique.
The combination of WDM and TDM techniques allows to increase the number of sensors in a network. The document “Remotely pumped and interrogated 96 channel fiber optic hydrophone array, in “Optical Fiber Sensor Conference 16”, pp. 760-763, November 2003” (D2) deals with a WDM-TDM combined technique. One can also mention the patent application US 2007/0024857 (D4), (improvement of the device disclosed in D2) which allows to get rid of the fabrication constraints to add fiber sections of accurate length in between each Fiber Optic Interferometric Sensor (FOIS) to interrogate (whether the sensors are located at the same node or not), and also allows to keep X-talk and reliability performances. Indeed, seismic applications require that the sensors are located at specific places in the array. Also ease of fabrication of the array, reliability and low X-talk between sensors are great benefits.
A WDM/FDM combined is proposed in the U.S. Pat. No. 7,154,082 (D5) patent.
Table 1a here below summarizes the multiplexing performances density of previous art solutions, in terms of:
It would be an important improvement from the prior art to provide a multiplexing technique in order to:
Indeed, the reduction of the number of fiber buses for a given number of sensors multiplexed onto the cable implies cost reduction and enhanced reliability of the apparatus because less fiber connectors are used. And the increase of the number of sensors multiplexed onto a single photo-detector implies cost and size reduction as less photo-detectors and less demodulation chains are required.
Accordingly, the invention aims at providing a new multiplexing technique which enables to achieve these improvements, thanks to an apparatus and a method for multiplexing and demultiplexing Fiber Optic Interferometric Sensors (FOISs).
More precisely, this aim is achieved thanks to an apparatus for multiplexing and demultiplexing Fiber Optic Interferometric Sensors (FOISs), said apparatus comprising:
The apparatus of the invention also comprises at least one of the following features:
This aim is also achieved thanks to a method for multiplexing and demultiplexing Fiber Optic Interferometric Sensors (FOISs), said method comprising the following steps:
The method according to the present invention can also comprise an additional step where, the n optical sources being organized in p groups of n/p optical emitters each, one switches on successively the p groups of n/p emitters to successively determine the absolute time foot prints of the response of the groups of m fiber optic interferometric on the demultiplexing system.
Other characteristics, objectives and advantages of the present invention will become apparent in the following detailed description illustrated by the appended figures, given as non restrictive examples and among which:
a is a representation of the light La in the telemetry fiber at the outlet of the first arm a of the interferometer that is required to interrogate the FOIS; this light is made up of one light pulse Pa, which has a specific frequency v0+Fa, the pulse being periodically generated at a repetition frequency Frep;
b is a representation of the light Lb in the telemetry fiber at the outlet of a second arm b of the interferometer that is required to interrogate the FOIS; this light is made up of one light pulse Pb, which has a specific frequency v0+Fb, where Fb is different from Fa (and more specifically in that case Fb>Fa), the pulse being periodically generated at a repetition frequency Frep;
c is a representation of the light L in the telemetry fiber at the outlet of the interferometer that is required to interrogate the FOIS; this light is made up of light pulses Pa and Pb;
d is a representation of the light Lout formed of 2 couples of light pulses resulting from the couple (Pa, Pb) of light pulses represented at
a is a representation of the light 210 in the telemetry fiber 13 at the outlet of a coupler 3 and composed of n couples of two light pulses 2101, 2102, . . . , 210j, . . . , 210p. The light 210j required to interrogate a node 5j (1≦j≦p) of m FOISs and is made up of a couple (Pja, Pjb) of light pulses, time-delayed one from another by the pulse delay PDj, the first pulse Pja (1≦j≦p) bearing the light of frequency νj+Fja and the second pulse Pjb (1≦j≦p) bearing the light of frequency νj+Fjb, the couple (Pja, Pjb) being also periodically generated at a repetition frequency Frep;
b is a representation of the group 340 of m*2 couples of light pulses resulting from the couple of light pulses (Pja, Pjb) represented in
c is a representation of the group 340 of m*2 couples of light pulses resulting from the couple of light pulses (Pja, Pjb) represented in
d is a representation of the m interference signals I51,m=(I1,11, I1,22, . . . , I1,kk, . . . , I1,mm), I52,m=(I2,11, I2,22, . . . , I2,kk, . . . , I2,mm), . . . , I5p,m=(Ip,11, Ip,22, . . . , Ip,kk, . . . , Ip,mm) on the photo detector 70 resulting respectively from the group 51, 52, . . . , 5p of m sensors as represented on
e is a representation of the 2m interference signals I51,2m=(I1,11, R1,12, I1,22, R1,23, . . . , I1,kk, R1,k(k+1), . . . , I1,mm R1,m(m+1)), I52,2m=(I2,11, R2,12, I2,22, R2,23, . . . , I2,kk, R2,k(k+1), . . . , I2,mm R2,m(m+1)), . . . , I5p,2m=(Ip,11, Rp,12, Ip,22, Rp,23, . . . , Ip,kk, Rp,k(k+1), . . . , Ip,mm Rp,m(m+1)) on the photo detector 70 resulting respectively from the group 51, 52, . . . , 5p of m sensors, as represented on
f is a representation of the gating pulses Gj,11, Gj,22, . . . , Gj,mm recorded during a calibration step and respectively used to properly time demultiplex the interference signals Ij,11, Ij,22, . . . , Ij,mm from the group 5j of sensors illustrated on
a shows a scheme of one possible way of construction for one m FOIS-node 5j (1≦j≦p) of
b shows a scheme of another possible way of construction for one m FOIS-node 5j (1≦j≦p) of
c shows a means 6j which selectively extracts the wavelength λj towards the group 5j of m FOIS.
a is a representation of the light 10j at the outlet of the mean Mj (1≦j≦p), sent in the telemetry fiber 13 by means of a coupler 11, and that is required to interrogate a number of m*n/p FOISs among the m*n FOISs; this light being made up of the two light pulses Pja, Pjb time delayed one from another by the delay PDj; the light pulses Pja and Pjb are made up of n/p light frequencies, respectively (νj1+Fja, νj2+Fja, . . . , νjn/p+Fja) and (νj1+Fjb, νj2+Fjb, . . . , νjn/p+Fjb);
b is a representation of the groups 221, 222, . . . , 22j, . . . , 22p of light pulses coupled on the telemetry fiber 13 through the coupler 11 shown in
c is a representation of the group 34j of m*2 couples of light pulses resulting from the couple of light pulses (Pja, Pjb) represented in
d is a representation of the 2m interference signals I5q1,2m=(Iq1,11, Rq1,12, Iq1,22, Rq1,23, . . . , Iq1,kk, Rq1,k(k+1), . . . , Iq1,mm Rq1,m(m+1)), I5q2,2m=(Iq2,11, Rq2,12, Iq2,22, Rq2,23, . . . , Iq2,kk, Rq2,k(k+1), . . . , Iq2,mm Rq2,m(m+1)), . . . , I5qp,2m=(Iqp,11, Rqp,12, Iqp,22, Rqp,23, . . . , Iqp,kk, Rqp,k(k+1), . . . , Iqp,mm Rqp,m(m+1)) on the photo detector 7q resulting respectively from the group 5q1, 5q2, . . . , 5qj, . . . , 5qp of m sensors;
a to 2d describe the principle for the interrogation of one interferometric sensor.
S0 is a coherent light source (preferentially a DFB fiber laser source) of wavelength λ0 (and frequency v0). The continuous light the source S0 enters the mean M0 that is capable of generating the light L at its output. One mode of realization of M0 consists in using two AOMs of different shift frequencies Fa and Fb and combined with two optical couplers. Each AOM allows to shift the frequency and to pulse the amplitude of the light that goes through it. The mean M0 is thus made up of two arms a and b comprising respectively the AOMs a and b. The AOM a (AOM b respectively) is driven by a carrier frequency fa (fb respectively), which is switched on and off, with a pulse sequence a (pulse sequence b respectively). The light La (Lb respectively) at the output of the AOMa (AOMb respectively) is made up of pulses Pa (Pb respectively) of width PW, repeated at a repetition rate Frep. The frequency of light La (Lb respectively) is shifted by Fa (Fb respectively) due to a known property of Acousto Optic Modulators.
The lights La and Lb are recombined by a fiber optic coupler, to form the light L on the telemetry fiber. The light L is made up of Pulse sequences Pa and Pb (see
The Light L goes through a fiber optic circulator C down to the Differential Interferometric Sensor (sensor). The sensor shown on
The reflection of light L by reflectors R0s and R0l gives rise to the light LOut, back to the circulator C. It is driven to a Photo Detector through the fiber Fout. The light LOut gives rise to light interferences on the photo-detector PD, through the optical pulses Pa reflected by the reflector R0l of the DIS and the pulse Pb reflected by the reflector R0s of the DIS. The interferences are born by the heterodyne carrier frequency F=Fa−Fb.
The system comprises means 1 forming an optical source capable of generating the light 210 made up of p couples of light pulses.
The means 1 comprise a series of emitters 401, 402, . . . , 40j, . . . , 40p emitting a light at a respective frequency v1, v2, . . . , vj, . . . , vp which differ one from another. Each emitter 40j (1≦j≦p) is followed a respective means Mj as the one described in
The respective means M1, . . . , Mj, . . . , Mp merge onto a coupler 3 (coupler of type “p” towards “l”) which send the light pulses Pja (νj), Pjb (νj), for 1≦j≦p into the telemetry fiber 13.
Thus, the light 210 driven by the telemetry fiber 13, as shown in
Following the light path, the system also comprises a fiber optic circulator 4, p groups (nodes) 51, 52, . . . , 5j, . . . , 5p of m FOISs to interrogate, p optical wavelength selective means 61, 62, . . . , 6j, . . . 6p, each disposed at the entry of a respective node, a photo-detector 70 and a demodulator 80.
The light 210 carried by the telemetry fiber goes through the fiber optic circulator 4 to the groups 51, 52, . . . , 5j, . . . , 5p of sensors.
The entry of each group 51, 52, . . . , 5j, . . . , 5p of sensors has an optical wavelength selective means 61, 62, . . . , 6j, . . . , 6p around the frequency ν1, ν2, . . . , νj, . . . νp respectively. As shown in
For ease of understanding, the description which follows only describes what happens for the jth couple of light pulses 210j which goes down to the jth group 5j, and back to the group 5j to the photo-detector 70 (and demodulator 80). The man skilled in the art will understand that a similar description could be done for the other groups 51, 52, . . . , 5(j−1), 5(j+1), . . . , 5p of sensors.
The jth group 5j is shown in details in
It consists of a main fiber FOj extending from the optical wavelength selective means 6j, and comprising m fiber optic couplers Ej,1 Ej,2, . . . , Ej,k, . . . , Ej,m of type <<1 input towards 2 outputs>> disposed in series. For each fiber optic coupler Ej,k (k=1 to m), one output is connected to the next fiber optic coupler Ej,(k+1) on the fiber FOj whereas the second output feeds the FOIS 54j,k.
Each of the m FOIS 54j,1, 54j,2, . . . , 54j,k, 54j,m comprises at its input an optical coupler Fj,1 Fj,2, . . . , Fj,k, . . . , Fj,m of type <<1 input towards 2 outputs>>, followed by two arms: one long arm and one short arm. The long arm forms the long optical path of one FOIS, and the short arm forms the short optical path of the FOIS.
Each of the m FOISs also comprises a compliant body respectively 540j1, 540j2, . . . , 540jk, . . . , 540jm, arranged on the respective long arms.
The ends of the long and short arms of each of the m FOISs respectively comprise a mirror 54j,l1, 54j,l2, . . . , 54j,lm, 54j,s1, 54j,s2, . . . , 54j,sm. The 2m mirrors 54j,l1, 54j,l2, . . . , 54j,lm, 54j,s1, 54j,s2, . . . , 54j,sm can either be selective or not in frequency (wavelength). If the 2m mirrors 54j,l1, 54j,l2, . . . , 54j,lm, 54j,s1, 54j,s2, . . . , 54j,sm are frequency (wavelength) selective, they preferentially are Fiber Bragg Gratings that selectively reflects, respectively, frequency νj.
The round trip imbalance between the long and short mirrors of each of the m FOISs is equal to D′ and corresponds to a time delay t(D′) close to the pulse delay PDj between the pulses Pja(νj) and Pjb(νj). The round trip path imbalance between two successive FOIS 54j,(k−1) and 54j,k (for 1≦k≦m) is equal to D″ and corresponds to a time delay t(D″).
In the mode of realization illustrated in
We will now clear the path taken by the pulses for both modes of realization.
The couple 210j of light pulses Pja(νj), Pjb(νj) entering the group 5j of m FOISs is driven by fiber optic FOj to a fiber optic coupler Ej1. One part of the power is directed to FOIS 54j,1 and the other part feeds another fiber optic coupler Ej,2 that splits the light into one part driven to the second FOIS 54j2, the other part feeding a third fiber optic coupler Ej3 and so on.
At the input of the FOIS 54j,k (1≦k≦m), the light is a power fraction of the couple of light pulses Pja(νj), Pjb(νj). It is sent to the fiber optic coupler Fj,k that divides it into two identical lights of equal power directed towards the short and long mirrors 54j,lk and 54j,sk. The lights reflected by the mirrors 54j,lk and 54j,sk are then recoupled by the couplers Fj,k and Ej,k onto the optical fiber FOj. The reflection of the light onto the short mirror 54j,sk gives rise to the couple of pulses [Pja,sk(νj); Pjb,sk(νj)] whereas its reflection onto the long mirror 54j,lk gives rise to the couple of light pulses [Pja,lk(νj); Pjb,lk(νj)]. The two couples [Pja,sk(νqj); Pjb,sk(νj)] and [Pja,lk(νj); Pjb,lk(νj)] being time delayed one from the other by t(D′), which is close to the pulse delay PDj.
Thus, at the output of the node 5j, the group 340j illustrated of m*2 couples of pulses [Pja,s1(νi), Pjb,s1(νj)], [Pja,l1(νj), Pjb,l1(νj)], . . . , [Pja,sk(νj), Pjb,sk(νj)], [Pja,lk(νj), Pjb,lk(νj)], . . . , [Pja,sm(νj), Pjb,sm(νj)], [Pja,lm(νj), Pjb,lm(νj)], represented by
The combination of the pulses Pjb,sk(νj) and Pja,lk(νj) onto the photo diode 80, gives rise to an interference signal Ij,kk at the Carrier Frequency Fj=Fjb−Fja that carries the sensor 540j,k response to an external excitation. As can be seen in
For example, the redundant interference signal Rj,12 for the sensor 540j,1 results from the interference between the pulses Pjb,l1(νj) and Pja,s2(νj). One can show that the phase information Φmain born by the interference signal Ij11, for the sensor 540j,1 is linked to the common cumulated phase noise Φccpn and the sensor phase signal Φsps by the relationship:
Φmain=Φccpn−Φsps (1)
Where Φsps is the phase generated on the frequency carrier Fj by an external excitation localized on the sensor 540j,1, and Φccpn is the phase noise accumulated on the carrier frequency, phase noise that one aims at getting rid off.
One can also show that the phase information Φredundant born by the redundant interference signal Rj,12 for the sensor 540j,1 is linked to the common cumulated phase noise Φccpn, to the sensor phase signal Φsps and to the cumulated phase modulation Φs+1,s that the carrier might be altered with through the path from Fj1 to Fj2, by the relationship:
Φredundant=Φccpn+Φsps−Φs+1,s (2)
Accordingly, by substracting the relationships (2) and (1), one can obtain the following relationship:
Φredundant−Φmain=2*Φsps+Φs+1,s (3)
Equation 3 shows that one doubled the sensitivity of the sensor 54j,1 (2*Φsps instead of Φsps) and got rid of the unwanted noise term Φccpn. On the other hand, the unwanted term Φs+1,s that corresponds to the cumulated phase modulation that the carrier might be altered with through the path from Fj1 to Fj2, appeared, but can be far reduced by isolating the corresponding fiber.
More generally, each sensor 540j,k (k=1 to m) gives rise to 2 interference signals Ij,kk and Rj,k(k+1) which can be used as previously described.
Thus, the preferred embodiment of the arrangement of the m FOISs (illustrated in
Independently of the mode of implementation of
Similarly, each group 51, 52, . . . , 5p of m sensors represented on
More precisely, when the emitter 40j is on and all the others are off, the photo-detector 70 only receives the group I5j,m (or I5j,2m) of interference signals illustrated in
Accordingly, during the interrogation phase (following the calibration step) that is to say when all the emitters are simultaneously on, pulse gating is achieved for each group 5j of sensors thanks to the absolute time footprints gathered and registered during the calibration step, allowing for a proper time demultiplexing of the interference signals from the m sensors.
This technique allows the optical path to be loosely adjustable between any two groups of sensors (nodes). And this technique makes it possible to increase the number of sensors which response can be read by one single photo detector 70 by one dimension: number of wavelengths nλ×number of frequencies nFDM/λ (when previous art solutions offered density multiplexing on one photo receiver equal to either the number of wavelengths or the number of frequencies, see table 1a).
The means 1 comprise p groups Sj (1≦j≦p where p≦n) each made up of n/p optical sources 41j, 42j, . . . , 4qj, . . . , 4(n/p)j with p≦n and n/p a positive integer, for 1≦j≦p), each optical source 4qj emitting a light at a respective frequency vqj (for 1≦q≦n/p 1≦j≦p) and being different one from another.
The frequencies vqj (1≦q≦n/p, 1≦j≦p) can be written in the form ν11, ν21, . . . , νq1, . . . , ν(n/p)1, ν12, ν22, . . . , νq2, . . . , ν(n/p)2, . . . , ν1j, ν2j, . . . , νqj, . . . , ν(n/p)j, . . . , ν1p, ν2p, . . . , νqp, . . . , ν(n/p)p and chosen such that ν11<ν12< . . . <ν1j< . . . <ν1p<ν21<ν22< . . . <ν2j< . . . <ν2p< . . . <νq1<νq2< . . . <νqj< . . . <νqp< . . . <ν(n/p)1<ν(n/p)2< . . . <ν(n/p)j< . . . <ν(n/p)p.
Each group Sj is followed by a mean 3j (1≦j≦p). 3j can be a fiber optic coupler of type “n/p towards 1”, but is preferentially a wavelength multiplexer.
At the outlet of each mean 3j, the light is then driven to a respective means Mj (1≦j≦p) as the one described in
a describes the light 22j (1≦j≦p) at the outlet of each means Mj (for 1≦j≦p): it is made up of two light pulses Pja (ν1j, ν2j, . . . , νqj, . . . ν(n/p)j) and Pjb (ν1j, ν2j, . . . , νqj, . . . , ν(n/p)j) of frequencies respectively (ν1j+Fja, ν2j+Fja, . . . , ν(n/p)j+Fja) and (ν1j+Fjb, ν2j+Fjb, . . . , ν(n/p)j+Fjb). The two light pulses Pja (ν1j, ν2j, . . . , νqj, . . . , ν(n/p)j) and Pjb(ν1j, ν2j, . . . , νqj, . . . , ν(n/p)j) are time delayed respectively by a pulse delay PDj, and are repeated at a repetition frequency Frep. The light 22j can be seen as the sum of the n/p lights 211j, 212j, . . . , 21qj, . . . , 21(n/p)j of wavelengths respectively ν1j, ν2j, . . . , νqj, . . . , ν(n/p)j.
The output lights 221, 222, . . . , 22j, . . . , 22p from the means M1, . . . , Mj, . . . , Mp merge onto the telemetry fiber 13 through a coupler 11 (coupler of type “p” towards “l”) and are driven to the groups of sensors 100 through the fiber optic circulator 4.
The group of sensors 100 is made up of n groups (nodes) 5qj (for 1≦q≦n/p and 1≦j≦p) of m FOISs each, which can be written in the form 511, 512, . . . , 51j, . . . , 51p, 521, 522, . . . 52j, . . . , 52p, . . . , 5q1, 5q2, . . . , 5qj, . . . 5qp, . . . , 5(n/p)1, 5(n/p)2, . . . , 5(n/p)j, . . . 5(n/p)p. The entry of each group 5qj (for 1≦q≦n/p and 1≦j≦p) has an optical wavelength selective means 6qj which extracts the wavelength νqj from the light at its input and drives it to the group of sensors 5qj, while passing the remaining part of the light.
As can be seen in
For ease of understanding, the description which follows only describes what happens with the light pulses 21qj (1≦q≦n/p and 1≦j≦p) formed by the pulses Pja(vqj) and Pjb(vqj) of frequencies vqj+Fja and vqj+Fjb, which feed the group 5qj of FOISs. The man skilled in the art will understand that a similar description could be done for any other groups of sensors.
One mode of realization of the group 5qj is shown in details in
Accordingly, it consists of a main fiber FOqj extending from the optical wavelength selective means 6qj, and comprising m fiber optic coupler Eqj,1 Eqj,2, . . . , Eqj,k, . . . , Eqj,m of type <<1 input towards 2 outputs>> disposed in series. For each fiber optic coupler Eqj,k (k=1 to m), one output is connected to the next fiber optic coupler Eqj,(k+1) on the fiber FOqj whereas the second output feeds the FOIS 54qj,k.
Each of the m FOIS 54qj,1, 54qj,2, . . . , 54qj,k, . . . , 54qj,m comprises at its input an optical coupler Fqj,1 Fqj,2, . . . , Fqj,k, . . . , Fqj,m of type <<1 input towards 2 outputs>>, followed by two arms: one long arm and one short arm. The long arm forms the long optical path of the FOIS, and the short arm forms the short optical path of the FOIS.
Each of the m FOISs also comprises a compliant body respectively 540qj,1, 540qj,2, . . . , 540qj,k, . . . , 540qj,m, arranged in the long arms.
The ends of the long and short arms of each of the m FOISs respectively comprise a mirror 54qj,l1, 54qj,l2, . . . , 54qj,lk, . . . , 54qj,lm, 54qj,s1, 54qj,s2, . . . , 54qj,lk, . . . , 54qj,sm. The 2m mirrors 54qj,l1, 54qj,l2, . . . , 54qj,lk, . . . , 54qj,lm, 54qj,s1, 54qj,s2, . . . , 54qj,lk, . . . , 54qj,sm can either be selective or not in frequency (wavelength). If they are frequency (wavelength) selective, they preferentially are Fiber Bragg Gratings that reflects frequency νqj.
The round trip imbalance between the long and short mirrors of each of the m FOISs is equal to D′ and corresponds to a time delay t(D′) close to the pulse delay PDj between the pulses Pja(νqj) and Pjb(νqj). The round trip path imbalance between two successive FOIS 54qj,(k−1) and 54qj,k (for 1≦k≦m) of the group 54qj is equal to D″ and corresponds to a time delay t(D″).
In the mode of realization illustrated in
The couple 21qj of light pulses Pja(νqj), Pjb(νqj) entering the group 5qj of m FOISs is driven by the fiber optic FOqj to a fiber optic coupler Eqj,1. One part of the power is directed to FOIS 54qj,1 and the other part feeds another fiber optic coupler Eqj,2 that splits the light into one part driven to the second FOIS 54qj,2, the other part feeding a third fiber optic coupler Eqj,3 and so on.
At the input of the FOIS 54qj,k (1≦k≦m), the light is a power fraction of the couple of light pulses Pja(νqj), Pjb(νqj). It is sent to the fiber optic coupler Fqj,k that divides it into two identical lights of equal power directed towards the short and long mirrors 54qj,lk and 54qj,sk. The lights reflected by the mirrors 54qj,lk and 54qj,sk are then recoupled by the couplers Fqj,k and Eqj,k into the optical fiber FOqj. The reflection of the light onto the short mirror 54qj,sk gives rise to the couple of pulses [Pqja,sk(νqj); Pqjb,sk(νqj)] whereas its reflection onto the long mirror 54qj,lk gives rise to the couple of light pulses [Pqja,lk(νqj); Pqjb,lk(νqj)]. The two couples [Pqja,sk(νqj); Pqjb,sk(νqj)] and [Pqja,lk(νqj); Pqjb,lk(νqj)] being time delayed one from the other by t(D′), which is close to the pulse delay PDj.
Thus, at the output of the node 5qj, the group 34qj of m*2 couples of pulses [Pqja,s1(νqj), Pqjb,s1(νqj)], [Pqja,l1(νqj), Pqjb,l1(νqj)], . . . , [Pqja,sk(νvqj), Pqjb,sk(νqj)], [Pqja,lk(νqj), Pqjb,lk(νqj)], . . . , [Pqja,sm(νqj), Pqjb,sm(νqj)], [Pqja,lm(νqj), Pqjb,lm(νqj)], represented by
In an alternative embodiment, one can have a node where the round trip path imbalance D″ between two successive FOIS is equal to PDj.
The group 34qj of m*2 couples of pulses is thus recoupled back onto the main fiber 32 by means of 6qj, and driven back to the circulator 4 which then directs it to a wavelength demultiplexing system 40 through the fiber 33. The light entering the system 40 is thus made up of n groups 34qj (1≦q≦n/p and 1≦j≦p) of m*2 couples of pulses. The system 40 separates the light at its input onto n/p different outputs 331, 332, . . . , 33q, . . . , 33n/p containing respectively the lights of wavelength bands B1, B2, . . . , Bn/p, where B1 contains the p wavelengths (ν11, ν12, . . . , ν1j, . . . , ν1p), B2 contains the p wavelengths (ν21, ν22, . . . , ν2j, . . . , ν2p), . . . and Bn/p contains the p wavelengths (ν(n/p)1, ν(n/p)2, . . . , ν(n/p)j, . . . , ν(n/p)p). Each fiber 33q (1≦q≦n/p) is followed by a photo-detector 7q and a demodulator scheme 8q.
Accordingly, each photo-detector 7q (1≦q≦n/p) receives the p groups of lights (34q1, 34q2, . . . , 34qj, . . . , 34qp) resulting respectively from the groups 5q1, 5q2, . . . , 5qj, . . . , 5qp (where the sensors are arranged as described below) and giving rise to the interference signals shown by
The means 1 forming the optical source also comprise calibration means. The calibration means allow the groups of emitters Sj for 1≦j≦p to be successively turned on: when the group S1 of emitters is on, the other groups of emitters are off, then, the group of emitter S1 is turned off and the group of emitters S2 is turned on, whereas the other groups of emitters remain off, and so on. This calibration step enables to sequentially take and record the absolute time ‘footprints’ of each group I5qj,2m (1≦j≦p) of interference signals resulting on photodetector 7q from the group 5qj of m sensors when the groups of optical sources S1, S2, . . . , Sj−1, Sj+1, . . . , Sp are turned off. Indeed, the p groups I5q1,2m, . . . , I5qj,2m, . . . I5qp,2m of interference signals are in general not time aligned on the photo detector 7q (if one doesn't take care of the optical path in between two consecutive groups of sensors), and in order to achieve proper time pulse gating on the photo detector 7q (i.e. time demultiplexing) of the 2m interference signals Iqj,11, Rqj,12, Iqj,22, Rqj,23, . . . , Iqj,kk, Rqj,k(k+1), . . . , Iqj,mm Rqj,m(m+1))) for each group 5qj (j=1 to p) of sensors, the mentioned calibration step is required.
More precisely, when the group Sj is on and all the others are off, the photo-detector 7q only receives the group I5qj,2m of interference signals illustrated in
Accordingly, during the interrogation phase (following the calibration step) that is to say when the groups of emitters S1, S2, . . . , Sj, . . . , Sp are simultaneously on, pulse gating is achieved on photo-detector 7q for each group 5qj of sensors thanks to the absolute time footprints gathered and registered during the calibration step, allowing for a proper time demultiplexing of the interference signals from the m sensors.
This technique makes it possible to use less photo-detectors for a given number of groups of sensors to interrogate. This technique also allows for loosely adjustable distance between any two groups of sensors (nodes).
In an alternative embodiment, there is no calibration phase and the groups S1, S2, . . . , Sj, . . . , Sp are successively turned on/off during the interrogation phase of the sensors. Thus, the group S1 of emitters is turned on to interrogate the groups of sensors 511, 521, . . . 5q1, . . . , 5(n/p)1, then S1 is turned off, and S2 is turned on to interrogate the groups of sensors 512, 522, . . . 5q2, . . . , 5(n/p)2 and so on, according to a similar operation to that explained above.
The advantages by the invention can be summarized in the table 1b below.
The interrogation system can be efficiently shared by several sub arrays, each made up n groups of m sensors each.
Each sub-array 91, 92, . . . , 9y, . . . , 9l comprises n groups of m interferometric sensors, in which the m fiber optic sensors of a same node are separated by a specific distance, the n nodes of each of the l sub arrays can be spaced by any fiber length, and the distribution of the l sub arrays of the system can be any, as shown under the reference 100 in
Each sub-array 91, 92, . . . , 9y, . . . , 9l also comprises a demultiplexer similar to 40, n/p photo detectors similar to 70 followed by n/p demodulators, and arranged in a similar manner than the demultiplexer 40, the photo-detectors and the demodulators illustrated in
The advantages of the system shown by
In an alternative embodiment, the l sub-arrays can be interrogated successively by sending the light coming from the means 1 forming optical source towards only one sub-array to interrogate.
The present invention is not limited to the modes of realization described above. More precisely, the fiber optic interferometric sensors can be Michelson interferometers or Fabry Perot interferometers or any interferometric means, selective in wavelength or not and allowing the proposed time multiplexing.
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