ACTUATOR SYSTEM
Technical field
The present invention relates to a set-up for sending longitudinal displacement pulses along a length of optical fibre between a first reflection point and a sec- ond reflection point, and to a method for repeatedly sending longitudinal displacement pulses through a length of optical fibre.
Technical background , It is known in the prior art to alter the reflectivity of fibre Bragg gratings in optical fibres by means of longitudinal acoustic waves, i.e. longitudinal displacement waves .
One way of coupling an acoustic wave into an optical fibre is presented in the article "100% efficient narrowband acoustooptic tunable reflector using fiber Bragg grating", Liu et al . , Journal of Lightwave Technology, Vol. 16, No. 11, November 1998. According to said journal article, an acoustic wave was coupled into an optical fi- bre by a tapered horn made from fused silica. The horn was tapered in diameter from 3 mm at a first end to 125 μm at a second end, over a length of 12 cm. A planar piezo-electric transducer was bonded to the first end surface of the silica horn, in order to launch an acous- tic wave into the horn. The second end of the horn was fusion-spliced to an end of the optical fibre. Consequently, a longitudinal displacement excited by the piezo-electric transducer was transferred into the optical fibre through said silica horn. However, the optical fibre must be terminated at the transducer. Consequently, the above-described arrangement does not allow light to propagate from one side of the transducer to the other side.
In many cases, it is desirable to launch acoustic waves into an optical fibre without terminating the light propagation path. This, however, not being allowed by the arrangement described above. Thus, there is a need for new and improved arrangements for sending longitudinal acoustic waves, or longitudinal displacement waves or pulses, into an optical fibre.
Summary of the invention It is an object of the present invention to provide a new and improved arrangement for sending longitudinal displacement waves, or pulses, into an optical fibre and the like, by which arrangement at least the above- identified problem of the prior art is eliminated. This ob ect is achieved by an arrangement according to the accompanying claims .
The present invention has several further advantageous features, which will be apparent from the detailed description of some preferred embodiments presented be- low.
Surprisingly, it has been found that a longitudinal displacement pulse, or wave, can be excited in an optical fibre by quickly moving the fibre at one point even when the fibre is not pre-strained. The inertia of the fibre itself is sufficient for a displacement pulse to be excited by said quick movement of the fibre.
By longitudinal displacement wave, it is meant a compression/elongation propagating along the fibre. Sometimes, such a wave or pulse is referred to as a longitu- dinal acoustic pulse.
According to the present invention, an actuator arrangement for exciting a longitudinal displacement wave, or pulse, in an optical fibre is employed. The arrangement comprises a washer element, or a collar, with which the optical fibre is engaged. Furthermore, the arrangement comprises a piezo member, which is responsive to an applied voltage to displace said washer element with re-
spect to a (comparatively heavy) bracket. By virtue of the fibre being engaged with said washer element, said displacement is transferred to the engaged portion of the fibre and propagated along the fibre. Also according to the present invention, a sensor arrangement for sensing longitudinal displacements in an optical fibre is employed.
In some embodiments of the actuator or sensor arrangement above, the washer element is not present. In- stead of using a washer element, the fibre rests directly onto the piezo member. In such a case, it is preferred to have the fibre pre-strained towards the piezo member by a pulling force.
The present invention provides an arrangement, or a set-up, for sending a longitudinal displacement pulse through a length of optical fibre. In said length of optical fibre, the longitudinal displacement pulse is repeatedly reflected back and forth between two reflection points. The arrangement comprises an actuator arrangement and a sensor arrangement. The actuator arrangement is adapted to actuate and amplify the longitudinal displacement pulse, and the sensor arrangement is adapted to directly or indirectly measure the timing of said pulse in order to provide actuation of the actuator arrangement resonantly with the pulse reflected back and forth between said reflection points. One advantage of the inventive set-up is that a longitudinal displacement pulse can be repeatedly sent along a length of optical fibre without terminating the light guiding path in the fibre. In a preferred mode of operation of the above- described set-up, the sensor arrangement is operative to provide an output signal indicative of the amplitude of the displacement pulse propagating between the two reflection points. Feedback is provided from the sensor ar- rangement to the actuator arrangement, and actuation of said actuator is adjusted so that the amplitude of the longitudinal displacement pulse, as detected by the sen-
sor arrangement, is maximised. Maximum amplitude of the displacement pulse is obtained when the actuator is operated resonantly with the displacement pulse, i.e. when the actuator arrangement is actuated at the same instant as the longitudinal pulse passes said actuator. Therefore, maximising of the pulse amplitude is a sufficient means for operating the actuator resonantly with the longitudinal displacement pulse.
In another mode of operation, the timing of the dis- placement pulses is measured, and the time of passage between the two reflection points is determined. Feedback is then provided to the actuator arrangement in order to actuate said actuator arrangement at the time when the displacement pulse passes said actuator. Furthermore, the present invention provides a method for repeatedly sending longitudinal displacement waves, or pulses, along a length of optical fibre between a first reflection point and a second reflection point. It is envisioned that the present invention will have its primary field of use in connection with systems in which the reflective properties of fibre Bragg gratings are altered by means of longitudinal displacement waves, or pulses. Such a system is disclosed in the Swedish patent application number 0002415-8, which is incor- porated herein by reference.
Brief description of the drawings
In the detailed description presented below of some preferred embodiments of the present invention, reference is made to the accompanying drawings, on which:
Fig. 1 schematically shows a first embodiment of an actuator/sensor for use in a set-up according to the present invention;
Fig. 2 schematically shows a piezo member comprised of two semi-circular parts;
Fig. 3 schematically shows a second embodiment of an actuator/sensor for use in a set-up according to the pre-
sent invention;
Fig. 4 schematically shows a third embodiment of an actuator/sensor for use in a set-up according to the present invention; and Fig. 5 schematically shows a set-up for sending longitudinal displacement pulses, or waves, into a length of optical fibre according to the present invention.
On the drawings, like parts are indicated by like reference numerals.
Detailed description of preferred embodiments
A first preferred embodiment of an actuator arrangement according to the present invention is schematically shown in figure 1. In figure 1, a cross-section of an actuator arrangement 10 is shown. As will be explained below, the same structural arrangement can also operate as a sensor. The arrangement comprises a bracket 11, or support, which is comparatively heavy with respect to other parts of the arrangement. Further, the arrangement comprises a washer element 12 and a piezo member 13. The piezo member 13 is arranged between the bracket 11 and the washer element 12, and is operative, responsive to an applied voltage, to displace said washer element 12 with respect to the bracket 11, i.e. to change the separation of the washer from the bracket. A predefined portion of an optical fibre 14 is engaged with the washer element 12 in such a way that said portion of the optical fibre follows any movement of the washer element. In the embodiment illus- trated in figure 1, the fibre 14 is engaged with the washer element 12 by means of a girdle 15, or bulb, on the fibre, said girdle being jammed to a passage in the washer element. However, it is to be understood that the fibre can be attached to or engaged with the washer in any suitable way, as long as the requirement that the engaged portion of the fibre follows the movement of the washer is fulfilled.
The bracket 11, the piezo member 13 and the washer element 12 each have a through passage that allows introduction of the fibre 14 therein. The fibre 14 is engaged with the washer element 12 and extends, in its longitudi- nal direction, through said passage. Consequently, any movement of the washer 12 will cause a longitudinal displacement of the portion of the fibre that is engaged therewith.
In the shown embodiment, the piezo member is com- prised of two separate parts 13a, 13b, each of which has a generally semi-circular shape. It has been found that by having a piezo member comprised of two parts, internal stress and other deteriorating circumstances can be avoided, thereby facilitating excitation of a "clean" and well-defined longitudinal displacement pulse in the fibre. A section through the piezo member comprised of two parts 13a and 13b, with the fibre 14 there between, is schematically shown in figure 2.
In the preferred embodiment, both the bracket 11 (or support) and the washer element 12 is made from brass. The piezo member 13 is preferably made from PZT (Lead Zirconate Titanate) , which is a commercially available piezo-electric ceramic material . The optical fibre 14 engaged with the washer element 12 has a typical outer di- ameter of 125 μm, and the bulb 15 formed thereon has a typical outer diameter of about 160 μm. The outer diameter of the washer element 12 and of the piezo member 13 transverse to the longitudinal direction of the fibre 14 is about 1 mm. The washer element 12 has a thickness, in the longitudinal direction of the optical fibre 14, of about 0.3 mm, and the piezo member 13 (each of the semicircular discs 13a, 13b) has a thickness in the same direction of about 0.51 mm.
In order to provide further stability of the actua- tor arrangement 10, a sleeve 16 could be fitted between the bracket 11 and the piezo member 13, as schematically shown in figure 3.
Although it is preferred to have a washer element resting on the piezo member, and to have the fibre engaged with the washer element, it is conceivable to have the fibre itself resting directly on the piezo member. In case the washer element is omitted, it is preferred to have the fibre pre-strained against the piezo member, as will be further described in connection with figure 4. Having described the basic structural features of the actuator arrangement according to the present inven- tion, the operation thereof will now be described in more detail .
It is well known to the man skilled in the art that a piezo-electric material can alter its dimensions responsive to an applied voltage. Likewise, it is well known that a change of the dimensions of a piezo-electric material can produce an output voltage if electrical connections are applied appropriately. Hence, the piezo member of the actuator arrangement is electrically connected to an external voltage supply. By applying a voltage to the piezo member, its dimensions parallel to the longitudinal dimension of the fibre can be altered. Consequently, the separation between the bracket and the washer element can be altered. It is to be understood that, due to the relatively large inertia of the bracket 11, a sudden change of the separation between the bracket 11 and the washer element 12 caused by the piezo member 13, causes a displacement only of the washer element 12 and of the portion of the fibre engaged therewith. Furthermore, the bracket 11 may be firmly attached to an ex- ternal housing.
If the change in separation between the bracket and the washer is sufficiently quick, the inertia of the optical fibre will, at least to some extent, counteract the displacement . This lead to a longitudinal displacement pulse being excited in the fibre.
The structural arrangement described above can also operate as a sensor for sensing longitudinal displace-
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is filled with a protective gas, e.g. nitrogen. In order to provide further protection of the fibre inside the housing, particularly during transport or in case of mechanical impact, cushions 57 can be provided that support the fibre. One preferred material for such cushions is so-called airglass. An important purpose of the protective housing is to provide temperature stability, although general mechanical protection is certainly important . Inside the housing, the length of fibre 52 between the actuator arrangement 50 and the sensor arrangement 51 is preferably bent in a semi-circle. The radius of curvature of said bend should be large enough for light in the optical fibre not to leak out. However, such a bend can have favourable effects on the longitudinal displacement wave propagating along the fibre, as will be further elucidated below.
A preferred mode of operation of the above set-up will now be described. The sensor arrangement 51 to which the fibre is connected does not have the only function of a sensor, but also acts as a reflection point for longitudinal displacement pulses in the fibre. Thus, whenever a longitudinal displacement pulse reaches the sensor 51, said pulse will, at least to some extent, be reflected back through the fibre towards the actuator arrangement 50. Likewise, the actuator arrangement 50 acts as another reflection point. Consequently, once a longitudinal displacement pulse (an acoustic pulse) has been excited in the fibre, it will be reflected back and forth between the sensor 51 and the actuator 50 through the length of fibre 52 comprising the Bragg grating. In other words, multiple passes of the displacement pulse through the Bragg grating will be provided. However, at each reflection point (i.e. at the sensor 51 and at the actuator 50) , some amplitude of said pulse is lost. The pulse will therefore gradually fade
away unless it is amplified at some point. To this end, it is preferred that the longitudinal displacement pulse is given some additional energy, i.e. increased amplitude, every time said pulse is reflected at the actuator 50. By sensing the pulse at the sensor 51, feedback can be provided in order to drive the actuator 50 in resonance with the propagating displacement pulse.
Alternatively, the sensor can be interchanged with a passive reflector. In that case, the mode of operation of the actuator arrangement is intermittently switched from an actuating mode to a sensing mode. When the actuator is in sensing mode, the timing of the displacement pulses is measured, and feedback and calibration is thereby provided for subsequent operation in the actuating mode. Two different ways of utilising the output signal from the sensor arrangement will now be briefly described.
In a first mode of operation, the sensor arrangement provides timing information regarding the displacement pulses propagating between the two reflection points.
From said timing information, a time of passage between the two reflection points can be determined. Feedback is then provided to the actuator arrangement, in order to actuate said actuator at the time when the longitudinal displacement pulse reaches the actuator after reflection. In a second mode of operation, regarded as the currently best known mode of operation, the sensor arrangement detects the amplitude of the longitudinal displacement pulse propagating between the reflection points. The amplitude is monitored, and the timing of the pulses sent into the length of fibre from the actuator arrangement is adjusted in fine steps until the measured amplitude is maximised. When maximum amplitude is obtained, pulses are excited by the actuator in concert with the propagating displacement pulse between the reflectors. Any other timing of the actuator would give the displacement pulse lower amplitude. Thus, by tuning the actuation of the ac-
tuator arrangement so that the pulse amplitude, as detected by the sensor arrangement, is maximised, said actuation will be in resonance with the displacement pulse. Preferably, the amplitude of the longitudinal displace- ment pulse is monitored continuously during operation, and the output of the monitoring is utilised for adjusting the actuator so that the actuator is actuated at a rate that gives maximum amplitude of the displacement pulse propagating in the length of fibre, i.e. at a rate that is in concert with the roundtrip rate of the displacement pulse between the two reflectors.
As mentioned above, favourable effects may be achieved by providing the fibre with a bend between the two reflection points (i.e. between the actuator and the sensor) . If the fibre is straight between the reflection points, there is a risk of standing waves building up therein. By providing the fibre with a bend between the reflection points, the risk of standing waves evolving is reduced. However, the propagation of a longitudinal dis- placement pulse along the length of fibre is virtually unaffected by said bend. Consequently, by providing the length of optical fibre between the actuator 50 and the sensor 51 with a bend, noise due to build-up of standing waves is reduced. The curvature of the bend should, of course, be sufficiently large in order for light not to leak out from the fibre core.
The invention has been described above by means of some preferred embodiments, schematically shown on the accompanying drawings. However, it is to be understood that various alterations and modifications are conceivable within the scope of the invention, as defined in the appended claims.