OPTICAL DEVICE CONTAINING A FIBRE-OPTIC COMPONENT

Abstract: An optical device is described, comprising a fibre-optic component, such as a fibre grating, which is associated with a predetermined transfer function, capable of being placed in a plurality of adjacent windings. Furthermore, the optical device is provided with a rigid housing capable of containing the said fibre-optic component, characterized in that it contains at least one separating element for physically separating the windings of the said plurality so as to prevent mutual contact through superposition and an element for fixing the said fibre-optic component capable of holding the said component in a stable position. The solution makes it possible to avoid undesirable changes of the transfer function that can occur during placement of the fibre-optic component in the housing and/or during the life of the device.

Description: OPTICAL DEVICE CONTAINING A FIBRE-OPTIC COMPONENT The present invention relates to optical devices containing fibre-optic components. In particular the present invention relates to the assembling and packaging of fibre-optic components. For the purposes of the present invention, fibre-optic component means one or more optical fibres connected optically in some way, possessing characteristics (for example dimensions, constituent materials or dopants, types of coating, relative position of the fibres, values of the refractive index of the core and of the outer layers, etc.) chosen so as to transmit an input light beam to at least one output light beam according to a predetermined transfer function. Examples of known components in fibre optics are: fibre Bragg gratings (fibre gratings) , active fibres used for amplification of optical signals, fibre couplers, optical fibres in general (for example single-mode and multimode fibres) , polarization-maintaining fibres, dispersion-shifted fibres, dispersion-compensating fibres, fibres used in optical sensors, etc.) as well as components obtained by combining them. Fibre gratings are generally optical fibres that have, in one portion, a refractive index of the core n and/or of the cladding n c permanently modulated along the propagation axis of the fibre. Gratings reflect, according to various transfer functions, optical signals that have different wavelengths . When the refractive index of the core n has a periodic (e.g. sinusoidal) variation with constant amplitude and pitch Λ along the propagation axis of the fibre, the grating is said to be uniform. Apodized gratings have an amplitude of the refractive index of the core n that varies along the propagation axis of the fibre (e.g. according to a Gaussian profile), whereas chirped gratings have a pitch Λ that is variable along the propagation axis of the fibre. In an article "Fiber Grating Spectra", Journal of Light Technology, Vol. 15, No. 8, p. 1277-1294, August 1997, T. Erdogan describes various types of fibre gratings and gives theoretical principles for their design and their possible uses in the area of optical telecommunications. The types of gratings considered by the author include, among others, the aforementioned uniform gratings, apodized gratings and chirped gratings. It is known that in a digital optical transmission system the chromatic dispersion of an optical fibre, i.e. the different speed at which signals of different wavelengths travel, causes a degradation of the quality of transmission, which becomes more and more relevant as the quantity of information transmitted m unit t me (oit rate) ^s increased. Suitable chirpeo gratings, called dispersion- compensating gratings, abbreviated to DCG, are used for compensating chromatic dispersion. A device for compensating chromatic dispersion is oescribed in US patent 4953939. In this document, referring to Fig. 1, the compensator element 1 comprises a chirped grating 5 formed in a fibre and a directional coupler 6 wnich makes it possible to separate tne travelling waves from the reflected waves. The directional coupler 6 can be a circulator, an isolator or a simp e fiseo-fibre coupler. This compensating element produces an optical delay that varies with the wavelength of the transmitted signal so as to compensate the chromatic dispersion. In this connection, the article oy F. Ouellette, "Dispersion cancellation αsing linearly chirped Bragg grating filters m optical waveguides", Optic Letters, Vol. 12, No. 10, October 1987, describes the use of chirpeo gratings for cancelling dispersion in optical fibres. Typically, a fibre grating is obtained by exposing the core of an optical fibre, from which tne coating has been removed, to UV (ultraviolet) radiation that has a defined intensity distribution. The desired variation of the refractive index of the fibre n is ootamed througn the light refraction effect. Following tne operation of inscribing the grating, the coating of the optical fibre is restored (recoatmg) . Typically, the operation of recoatmg leads to an increase in overall diameter of the optical fibre relative to its diameter before the coating was removed. For example, this increase may be about 75 μm. The fibre components and m general the optical devices that contain fibre components, such as devices for chromatic dispersion, are normally housed m units that protect the component and/or the device and limit its overall dimensions, permitting it to be transported. Devices for compensation of chromatic dispersion, of the types comprising an optical circulator and a DCG, are housed in suitable modules such as tnose manufactured oy the applicant and designated CDCM (Chromatic Dispersion Compensation Module) , for example models CDC 0480 and CDC 016160. US patent 5887107 describes an optical device consisting of a container, and an optical fibre containing, m one portion, a Bragg grating. The Bragg grating described is of the uniform type and is stated to be suitable for separating channels in a WDM system. In addition the container is provided with a locking element, which constrains a portion of the fibre, and a mandrel around wnich another portion of tne fibre is wouno. The applicant has observed that, as shown m Fig. 2 of the saio patent, the portion of fibre containing the grating is arranged between the mandrel and the locking element in a rectilinear position. In US patent 5915061 m the name of the same applicant, an organizer rack is illustrated for the nousmg of fibre-optic components, electrical, opto-electπcal and optical components, variously connected. That document describes an optoelectronic apparatus that includes a casing, inside which are arranged an electronic unit and an optical unit, connected electrically to one another; the optical unit comprises an element housing at least one component, rfticn can oe of tne optical type, with optical connection or of the electro-optical type. The said element has a plurality of separate areas, so that each area houses components substantially of just one type. This organizer rack includes, in addition, a holder for surplus fibres, provided with containment fins. Patent application FR 2 561 002 describes a device for the storage of spare lengths of optical fibre, including a box with inlet and outlet holes. Tne interior of tne box consists of a conduit in the form of a coil. Eacn coil communicates with a hole for fibre inlet. The device described permits withdrawal of the fibre inserted m the box by pulling it out, so as to be aole to work on it. US patent 5649035 describes a f ^ bre-optic sensor for the measurement of stresses m structures sucn as towers, bridges, or aircraft parts. This sensor comprises a carrying layer of flexible material, an optical fibre formed into a plurality of loops and arranged on the carrying layer, and two reflecting elements arranged at the ends of the fibre. The optical fibre is embedded in the flexible carrying layer or is glued to it. The flexible carrying layer is applied to the structure that s to be measured. The elongation of the said structure between the two reflecting elements is observed by measuring, with an optical signal passing through the said fibre, the cnanges in the travel time due to the elongation of the optical fibre . The use of fillers or adhesives inside known optical devices is also known. For example, US patent 5727105 describes a device comprising a main container and two side containers, with an optical fibre that is introduced from the side container into the ma n container. The optical fibre is locked in the side container oy means of silicone resin or an epoxy adhesive. In addition, US patent 5960143, which relates to a protective casing of an optical component, descrioes the use of an adhesive product for fixing an optical fibre to a waveguide and for mechanically fixing an optical fibre to a substrate. This patent also describes the use of a water- repellent lubricating product, for example of the so-called mechanical type or silicone-based, for separating the optical component from tne container walls. In the reference book "Silicones - Chemistry and Technology" s.v., published by Vulkan-Ver ag Essen (DE), 1991, p. 45-59, there is a description of the preparation of room temperature vulcanizaoie (RTV) silicone elastomers (or rubbers) . The RTV silicone rubbers are divided in this book into single-component silicone rubbers (RTV-1) and two-component silicone rubbers (RTV-2). The latter, as described in the aforementioned book, can be produceα by a reaction of condensation oetween two silicone compounds (for example between a poiymethyldisiloxane with -OH end groups and tetra-ester of silicic acid) or oy an addition reaction between two silicone compounds (for example by a reaction of hydrosilation of a silicone compound containing ≡SiH groups along the chain with a polydimetnylsiloxane containing vmylic groups, either terminal or pendent along the chain) . For the purposes of the present invention tne term "winding" of a fibre-optic component means a portion of such a component that has a curved shape, i.e. not rectilinear, for a section of its xength and arranged openly, i.e. such a way that there is no contact between different points of the same winding. For the purposes of the present invention, the expression fibre-optic component arranged in a wound configuration means that the fibre-optic component is arranged as a plurality of windings. The applicant has observed tnat fibre-optic components, arranged the known housing units ana possessing a length such that tney are required to de wound around suitable structures, undergo undesirable cnanges of their optical behaviour, occurring either during placing of the component around the said structure or during normal use of the said component. The applicant nas realized that some changes m optical behaviour of the fibre-optic component are connected with contact between different portions of the component itself. Tnis can be explained oy the fact that these contacts can cause, surprisingly, mechanical stressing of the fibre-optic component that is not negligible in its magnitude, i.e. is such as to alter the said behaviour. In particular, the applicant has noticed that contacts through direct superposition between portions of the fibre component cause mechanical stresses of a greater magnitude relative to contacts occurring between tangent portions, i.e. between portions that remain parallel as they come into contact . Furthermore, during its use, the component may be displaced relative to the oosition in which it was initially placed the housing unit, giving rise to mechanical stresses due to contact between the portions of the optical fibre. Consequently, the optical oehaviour of the fibre-optic component changes αuπng the life of the said component. The applicant has developed an optical device, inside which a fibre-optic component is arranged, wound-up so as to give it a stable position that prevents contact through direct superposition, and preferably any <mα of contact, between different portions of the windings. This arrangement of tne optical component makes it possible to avoid undesirable changes of behaviour of the said fibre- optic component. According to a first aspect, the present invention relates to an optical device comprising - a fibre-optic component, whicn is associated * /ιth a predetermined transfer function, capable of oeing arranged a plurality of adjacent windings, - a rigid housing capable of containing the said fibre- optic component, characterized m that the said housing comprises - at least one separating element, capable of pnysically separating the windings of the said plurality so as to avoid contacts through superposition between them, - an element for fixing the said fiore-optic component, capaole of keeping the said component in a stable position. In a preferred embodiment, the said separating element is capable of separating the windings of the said plurality so as to prevent contacts between them. In a particular embodiment, the said optical component comprises a fibre grating in one portion. In a particular embodiment, the said optical component comprises a chirped fibre grating one portion. In an alternative embodiment, tne said optical component comprises a chromatic dispersion compensator. In a particular embodiment, the said optical component comprises an active fibre. Advantageously, the said fibre-optic component has a length between 10 cm and 20 m. Advantageously, the said fibre-optic component has a length between 20 cm and 20 m. In a particular embodiment, the said rigid housing is made of polycarbonate. In a preferred emooαiment, the said rigid housing is made from a material containing an aluminium alloy. In a particular embodiment, the said housing comprises fms for delineating a circuit for housing the said fibre- optic component. In an alternative emboαiment, the said housing comprises grooves. In a preferred embodiment, the said separating element comprises at least one fm interposed between two windings of the said plurality. In an alternative embodiment, the said separating element comprises crosslmkable resins. In a particular embodiment, the said fixing element is a sealing grease. In a preferred embodiment, the said fixing element is a silicone compound. In an alternative embodiment, the said fixing element is a polyurethane resin, In an alternative embodiment, the said fixing element is a cover that is structurally associated to the said base . A second aspect of the invention relates to an optical apparatus comprising a container, inside wnicn the following are arranged: - a fibre-optic component capable of being arranged m a configuration comprising a plurality of adjacent windings, - an optical component capable of being connecteα to the said fibre-optic component, characterized m that the container comprises - a housing for the said fibre-optic component, the said housing comprising - at least one separating element capable of physically separating the windings of the said plurality so as to avoid contact through superposition between them, - an element for fixing the said fibre-optic component capable of holding the said component a stable position. In a particular embodiment, the said optical component comprises a connecting optical fibre. Advantageously, the said container comprises a unit for connecting the said fibre-optic component to the said connecting optical fibre of the optical component. In a preferred embodiment, the fibre-optic component comprises a fibre-optic grating. In a particular embodiment, the said optical component is an optical circulator. In an alternative embodiment, the said fibre-optic component is an active optical fibre. In an alternative embodiment, the said optical component is an optical isolator. In an alternative embodiment, the saio optical component is an optical coupler. A third aspect of the invention relates to a method for assembling an optical device comprising a f ore-optic component, associated with a predetermined transfer function, the said method comprising the steps of - placing tne saio component inside a rigid nousing, m a wound-up configuration so as to avoid superposition oetween the various parts of the component, - locking, by means of a fixing element, the said component a configuration such as to prevent movements inside the housing. Advantageously, the optical component is placed in a configuration that avoids contacts between tne various parts of the component. In a preferred embodiment of the method, the said component is placed m a spiral configuration. Advantageously, the said spiral configuration has a pitch greater than or equal to the maximum diameter of the fibre-optic component. In a particular embodiment, the said spiral configuration has a pitch approximately equal to 1.5 times the maximum diameter of the said fibre-optic component. Advantageously, the said locking step includes a step of inserting a quantity of a protective compound m the said housing. In a particular embodiment, the said transfer function is associated with a predetermined reflectivity spectrum. Advantageously, m the step of placing the said component m the said housing, the said reflectivity spectrum undergoes a change of less than 0.5 dB . Advantageously, m the step of placing the said component in the said housing, the said reflectivity spectrum undergoes a change of less than 0.2 dB . The present invention makes the operation of placing the fibre-optic component in the relevant housing unit less critical . In addition, it makes it possible to obtain reliable optical devices, possessing an effective transfer characteristic that is substantially equal to the nominal cnaracteristic, reducing the operations of characterization and inspection that must be effected on the device during its life. The optical device that is proposed can easily be coupled to other optical and optoelectronic devices and can be used as a discrete component, independently of the components to which it is connected. The characteristics and advantages of the invention will oe illustrated in the following, with reference to embodiments that are represented as non-limitative examples, tne accompanying drawings m whicn: - Fig. I snows a plan view of an optical device according to the invention; - Fig. 2 snows a plan view of an alternative embodiment of an optical device according to the invention; - Figs. 3a and 3b show schematic representations of two chromatic dispersion compensators; - Fig. 4 shows an exploded perspective view of a container made according to the invention, capable of containing two devices for compensation of chromatic dispersion; - Fig. 5a shows a perspective view of the lower rack of the container m Fig. 4; - Fig. 5b shows a perspective view of tne intermediate rack of the container in F g. 4; - Fig. 5c shows the organizer rack of the container m Fig. 4; - Fig. 6 shows a plan view of a container of a chromatic dispersion compensator made according to the known art; - Fig. 7a shows the measured reflectivity spectrum of an extended chirped grating; - Fig. 7b shows a first measured reflectivity spectrum of a chirped grating housed in the container of Fig. 7 ; - Fig. 7c shows a second measured reflectivity spectrum of a chirped grating housed tne container of Fig. 6; - Fig. 8 shows the reflectivity spectra of a chirped grating extended on a test bench, housed m the container in Fig. 6 and housed in the device of the invention; - Fig. 9 shows an FTIR (Fourier transform infrared spectroscopy) analysis of the crosslmkmg of a silicone rubber used in the optical device of Fig. 1. A preferred embodiment, given as a non-limitative example, of the optical device 100 according to the invention comprises a base 101, shown detail in Fig. 1, a fibre-optic component 200, housed base 101, and a cover (not shown) associated to the oase 101. The fibre-optic component 200 comprises an optical fibre that has an initial section 201 followed Oy a central portion m which there is a chirped grating 202 that extends over nearly the whole of its length, and a final section 203. Base 101, of substantially rectangular external shape, perforated in its central part, contains semicircular peripheral notches 102, for joining to external elements, two inlet openings 103 and two optional outlet openings 104 arranged at the corners of base 101. Base 101 supports the fibre-optic component 200 and protects it against external mechanical stresses, therefore it is sufficiently rigid to offer adequate resistance to the action of external mechanical forces that tend to deform it. Advantageously, base 101 is an almost monolithic element made from materials with high dimensional stability, for example polycarbonate, preferably with glass fibres (e.g. to 40%), glass-filled nylon (e.g. nylon 66), or aluminium and aluminium-based (super) light alloys (e.g. Avional, Ergal, Peraluman) . In addition, the base 101 is provided with holes 105 and holes 106 used respectively for the passage of screws for fixing the container to an external surface and as indicators for aligning the cover. Each inlet opening 103 is connected, oy means of a connecting slot 107, to a housing circuit 108 for the fibre-optic component 200, made in base 101. This housing circuit 108 is preferably made by milling the base 101. The connecting slot 107 comprises a notch 110 suitable for holding materials for fixing the initial section 201 of the fibre-optic component 200, such as rubber, plastics or glue . The housing circuit 108 comprises a pathway for the fibre-optic component 200 and is delimited by arc-snapeα fms 109. Fig. 1 shows two groups of opposing arc-shaped fms 109 and two separating zones 114 between these groups. In each of the two groups, the arc-shaped fms 109 are arranged along concentric circumferences with increasing radius . In particular, the housing circuit 108 for the fibre- optic component 200 shown in Fig. 1 is able to noαse the said component following a spiral profile. Preferably, the distance Between adjacent fms 109 is a little greater than the maximum diameter of tne fibre- optic component 200 in order to house it without exerting pressure on its walls and, at the same time, reduce its mobility withm the housing circuit 108. When outlet 104 is provided, oase 101 nas a groove 111 connected to the said outlet. This groove 111 is also connected to tne nousing circuit 108 and, in the part close to the opening 104, is raised relative to the plane of the housing circuit 108. In this terminal part, each groove 111 comprises wells 112, to nold, if necessary, glue or some other conventional material for locking tne end 203 of the fiore-optic component 200 in the case wnen this end goes out of the device, as shown Fig. 2, and raised portions 113 which act as bases for supporting tne cover. The cover, which provides further protection for the fibre-optic component 200, is typically made of a semirigid plastics material, for example polycaroonate , with thickness preferably of 0.7 mm which, oemg easily printed on by the silk-screen process, also serves as a label. It is also possible to use covers made of stair less-steel sheet, typically of 0.3 mm. The said cover can be of the self-adhesive type and adheres to the base 101 in those regions not occupied by the fibre-optic component 200. According to the optical device shown in Fig. 1, the chirpeo grating 202 is of the DCG type (Dispersion Compensating Grating) , used for compensating chromatic dispersion . A cnirped grating of the DCG type is, for example, manufactured by tne applicant. The optical device 100 is suitable for nous g fibre- optic components 200 of any length, preferaoiy between about 10 cm and about 20 m. More preferaoiy, between about 20 cm and aoout 20 m. In particular, a fibre cnirped grating housed in the said device will preferaoiy nave a length greater than 10 cm. More preferably the said length s greater than 20 cm and typically does not exceed 10 m. According to a preferred embodiment, tne length of the chirped grating is about 2 m. In this last case the fibre- optic component 200 has a total length of about 3.4 m with each of tne terminal portions 201 and 203 nav g a length of about 70 cm. The central portion of fibre-optic component 200, which includes the chirpeo grating 202, can m its turn contain several fibres m which a chirped grating is inscribed, connected optically by means of one of the known welding techniques. Preferably, the cylindrical casing (called tuoe) for protecting the weld, wnich has a reduced occupied space, is made by conventional techniques that employ, for example, a heat-shrmkable tube, sucn as tnat marketed oy OPTOTEC S.p.A. (Italy) . The final section 203 of fibre-optic component 200 can be provided with an antireflective termination ootamed by Known techniques sucn as tapering, antireflective coating, and the like. As shown Fig. I, fibre-optic component 200 is placed carefully between fms 109 so as to follow the spiral shape of the housing circuit 108. The initial section 201 is inserted via inlet 103 into the connecting groove 107, while the chirped grating 202 evolves m housing circuit 108, clockwise, as far as the innermost coil where the final section 203 is placed. Tne initial section 201 is fixed to base 101 by means of a material contained in well 110, so as to prevent axial pulling arising from external sections of fibre oemg transmitted to the internal sections of fibre of the fibre-optic component 200. This material s, for example, an elastomeπc material sucn as silicone elastomer which secures tne initial section 201 to tne base 101 and which at the same time exerts a reduced pressure on the fibre in question, without affecting its optical behaviour. Alternatively, for this specific application, it is possible to use commercial products such as LUXTRAK 4047 or 4057 ABLESTIK (Rancho Dommguez, CA90221) . The spiral along whicn tne fibre-optic component 200 evolves, corresponds suostantially to an Arcnimeoes spiral, navmg a centre of evolution that coincides sαostantially with tne point of intersection of the diagonals of base 101. The radius of the innermost coil correponds to a curvature such that the chirped grating 202 is not αamaged and its behaviour is not disturbed. The distance between tne axes of the sections of fibre of fibre-optic component 200 arranged along adjacent coils, i.e. the pitch ΔR of the spiral, is greater than or equal to the maximum diameter of fibre-optic component 200 and is constant for the entire evolution of the spiral. For example, a suitable value of the pitcn ΔR is ΔR = 1.5 d, where d is the diameter of the fibre-optic component 200 including tne recoatmg zone. In addition, base 101 is suitable for nous g a fibre- optic component 200 m which both its ends emerge from device 100 so as to be available for external connections. Fig. 2 shows the case 101, and tne fibre-optic component 200 arranged so that the final section 203 goes out through the appropriate opening 104. This final section 203 is fixed to groove 111 by means of a suitaoie locking material placed in wells 112. As stated previously, the part of groove 111 containing the wells 112 is raised relative to the housing circuit 108. Accordingly, the final section 203 that extends from the innermost con of the nousmg circuit 108 to the groove 111 is inclined relative to the pxane of the base 101. This inclination means that fiore section 203 is not in contact with the portions of the fiore-optic component 200 arranged in the housing Circuit 108. The applicant has observed that the housing circuit 108, descπoed above, prevents the occurrence of contacts between adjacent sections of fibre-optic component 200, these sections being coplanar or sections that are superimposed. More generally, the nousmg circuit 108 makes it possible to avoid contact etween all the various parts of fibre-optic component 200. In the regions of housing circuit 108 that do not have fms, the fibre-optic component 200 is arranged so as not to have surplus fibre that occupies the region and comes into contact with other sections of fibre. The arc-shaped fms 109 give the fiore-optic component 200 a predetermined profile and also separate the fibre sections corresponding to successive coils. The spiral profile is particularly advantageous in that, in addition to the advantages described above, it makes it possible to optimize the overall dimensions of the optical device. In addition to the arc-shaped fms 109, other elements can also oe made or inserted m case 101 for conferring a defined placement profile and/or for separating sections of the fibre-optic component 200, so that they do not come into contact. Other separating elements are, for example, f s of whatever shape, grooves, crosslmkable resins arranged on base 101 with suitable geometry, for example m a spiral, or obtained by photolithographic processes or a combination of these. In addition, the fibre-optic component 200 arranged in the housing circuit 108 is immersed in a protective compound (not shown m the drawings) . This compound can be a silicone or non-silicone sealing grease of a known type, such as a grease used in fibre-optic cables, for example the silicone sealing grease Filler H55-Pιrellι or the silicone grease LA444 marketed by HUBER. In addition, this compound can be a resin tnat is crosslmkable at room temperature, for example a polyurethane resin. Preferably, the saiα protective compound is a silicone composition. A suitable silicone composition is characterized by the fact that when it is subjected to thermal ageing for 15 days at 100°C, it evolves a quantity of nydrogen less than 1 cm 3 per kg of silicone rubber. Preferaoiy, tne quantity is less than aoout 0.5 cm 3 /κg, and even more preferaoiy it is less than about 0.1 cm 3 /kg of crosslinkeα material. Especially advantageous are tnose silicone ruobers according to the invention that evolve a quantity of nydrogen less than about 0.05 cm 3 /kg of material. The said characteristic can be obtained oy properly controlling the stoichiometric proportions of the hydrogen- siloxane and vmyl-siloxane compounds used in tne reaction of hyorosilation to obtain the said rubber, in particular carrying out the reaction with a stoichiometric ratio of 1:1 between the ≡SiH ana vinyl functional groups, or with a stoichiometric deficit of ≡SiH groups. The applicant has observed that if the aforesaid reaction of hyorosilation is carried out m accordance with what is suggested by the state of the art to optimize the physical properties of the resins, i.e. with a stoichiometric excess of 1.5 to 2 times groups relative to the vinyl groups, the presence of the excess of unreacted hydrogen-siloxane compound in the silicone mixture can cause the formation of hydrogen through reaction of the excess hydrogen-siloxane groups with water, according to the reaction scheme: ≡SiH + H 2 0 → ≡SiOH + H 2 . However, substantially complete reaction of the groups makes it possible to obtain a rubber that is substantially free of the said unreacted hydrogen-siloxane compounds, thereby avoiding the harmful possible formation of hydrogen as a result of their decomposition by reacting witn water. Fig. 9 shows the progress of crosslm mg of a silicone rubber wnere the ratio between the ≡SiH groups and vinyl groups of tne polysiloxane reactants is about 1:1 (prepared in accordance with Example 3 described below) . This graph shows FTIR spectroscopic analysis of the various stages of crosslmking of the resm, starting from mixing of the components (line "A"), with particular reference to IR absorption of the 2155 cm "1 band relating to the ≡SiH group. As can be seen from the graph, this band decreases m intensity considerably just one hour after mixing the components (line "B"), becoming practically negligible after about 4 hours (line "C") . The applicant has also observed that for generation of less than 1 cm" of hydrogen per kg of material, t is necessary for the final silicone rubber to contain a residue of unreacted ≡SiH groups less than 0.045 mmol per kg of material. An elastomer according to the present invention can therefore be obtained by an addition-curing reaction of a polysiloxane, preferably a polydimethylsiloxane containing at least two hydrogen-siloxane functional groups of formula >SιH-0- ("hydrogen-siloxane" for short) with a polysiloxane, preferably a polydimethylsiloxane, containing at least two vinyl groups of formula -CH=CH 2 ("vinyl- siloxane" for short) , with the ratio oetween the molar quantity of hydrogen-siloxane groups and the molar quantity of vmyl groups less than or equal to 1:1. In particular, the ratio between the molar quantity of hydrogen-siloxane groups and the molar quantity of vmyl groups is between about 1:1 and about 0.5:1, preferably oetween about 0.9:1 and about 0.7:1, with a ratio of aoout 0.8:1 being especially preferred. As polysiloxane containing hydrogen-siloxane groups, for the purposes of the present invention a compound of formula (I) can be used advantageously (I): where Ri, R 2 , R 3 , R , and R 5 , independently of one another, represent a (Cι-C_) alkyl group, a (C 5 -Cs) cycloalkyl group or a phenyl group, preferably a methyl group, p is an integer between about 30 and aoout 200, and preferably oetween about 50 and about 120, and q is an integer between about 5 and about 40, and preferably between about 10 and about 25. Preferably, the ratio oetween units of type -HSiR^-O- and units of type -Si(R 2 R 3 )- 0- is between about 1:1 and about 1:10, preferaoiy being between about 1:3 and about 1:5. Preferably, the quantity of ≡SiH groups is between about 1 mmol per gram of compound and about 10 mmol per gram of compound of formula (I). Advantageously, a polysiloxane containing hydrogen- siloxane groups according to the present invention, and in particular a compound of formula (I) wnere R- x , R 2 , R 3 , R , and R 5 are methyl, has a kinematic viscosity (at 25°C) oetween about 10 and about 600 mPas, preferably between 20 Pas and 400 mPas, with a viscosity of about 25 and 250 mPas (measured according to standard ASTM 445) being especially preferred. Examples of polysiloxane compounds containing hydrogen-siloxane groups that can be used in the present composition are sold under the trademarks Silopren U130, Silopren U230, Silopren U430, Silopren U930 (Bayer AG) , PS122.5, PS123, PS123.5, PS123.8, PS124.5, PS125, PS125.5, PS129.5 (United Chemical Technologies). Among the vinyl-terminated polysiloxane compounds, for the purposes of the present invention, compounds of formula (II) can be used advantageously: where Ri, R 2 , R 3 , R 4 , and R 5 , independently of one another, represent a (Cι-C ) alkyl group, a (C 5 -C B ) cycloalkyl group or a phenyl group, preferably a methyl group, n is an integer between about 200 and aoout 1200, and preferably between about 300 and about 1000, and m is zero or an integer between 1 and 5, and is preferaoiy 0, 1 or 2. The kinematic viscosity (at 20°C) of a polyv ylsiloxane according to the invention, ana m particular of a compound of formula (II) wnere Ri, R 2 , R 3 , R , and R 5 are methyl, is preferably between about 100 mPas and about 65,000 mPas, and preferably between about 800 and about 12,000 mPas and (ASTM D445). For tne purposes of the present invention, it is possible to use either a single compound with predetermineα viscosity, for example of aoout 5000 mPas, or a mixture of two or more compounds with different viscosities to obtain a viscosity intermediate between those of the different compounds (for example the said viscosity of about 5000 mPas can be obtained by mixing, in suitable amounts, a compound with viscosity of about 1000 mPas and a compound with viscosity of about 10, 000 mPas) . Examples of poiymethylsiloxane compounds containing vmyl-siloxane groups that can be used m the present composition are sold under the trademarks Silopren Ul, Silopren U5, Silopren U10, Silopren U65 (Bayer AG) , PS441, PS441.2, PS442, PS443, PS444, PS445, PS447.6, PS463, PS491, PS493, PS735 (United Chemical Technologies) . The aforementioned aodition-curmg reaction is typically effected m the presence of a metallic catalyst, which is added to the compounds that are to oe cared, preferably in the form of a soluble salt or an organometallic complex. The quantities are about 5-10 ppm of metal relative to the total weight of the composition. The metal is preferably cnosen from among the transition metals, for example rnodium or, more preferably, platinum, preferably as a soluble salt. Examples of catalysts that can be used for the aforementioned reaction are sold oy the company United Chemical Technologies with tne names PC072, PC073, PC074, PC075, PC075.5 and PC076. The silicone composition according to tne present invention can in addition advantageously contain silicone oils, with the aim of modifying either the viscosity of the mixture that is to be cured or the mecnanical properties of the final elastomer. In particular, whereas on the one nand addition of the said oils can alter the viscosity of the mixture to be cured, making its application easier, on the other hand the presence of these oils (which αo not take part in the crosslmkmg reaction) in tne final rubber contributes to control of the final softness of the material, which is to be sucn as not to transmit (or transmit to a negligible extent) αndesiraole mecnanical stresses on optical components embeαded m tne said material. The kinematic viscosity of these oils is preferably between aoout 20 mPas and aoout 2000 mPas at 25°C (ASTM D445), with a viscosity between aoout 100 mPas and about 1000 mPas being mostly preferred. To obtain the desired viscosity of the mixture to be cured and the desired characteristics of softness of the final elastomer, the aforementioned oils can be used either individually or as a mixture of several oils with different viscosities. Typically, the amount of silicone oil in the final composition can vary from about 30% to about 60% by weight, depending on the required viscosity for the mixture to be cured and on the desired softness characteristics of the final resin. Silicone oils that can be used advantageously for the purposes of the present invention are -ω-trimethylsiloxy- polydimethylsiloxanes of general formula: CH, CH, CH, I 3 I 3 CH 3 —Si-O- -Si—0- -Si-O—CH, I I CH, CH, CH, where r is an integer between about 30 and about 500, preferably between about 100 and about 400. Examples of silicone oils that can be used for the present composition are sold under the trademarks Baysilone M100, Baysilone M500, Baysilone M1000 (Bayer AG) , DC 200/20, DC 200/500, DC 200/1000 (Dow Corning), AK100, AK500, AK1000 (Wacker) . A composition according to the present invention can in addition contain silica, typically quantities between about 5% and about 20% by weight. Pyrogenic silica partially silanized in the form of submicroscopic particles (submicroscopic fire-dry fumed silica) with particle size of about 0.007-0.01 μm can be used advantageously. Examples of commercially available silica include silica Cab-O-Sil TS610 (Cabot), silica HDK H15, HDK H20, HDK H30 (Wacker). The presence of silica in the composition has the dual purpose of imparting thickening of the thixotropic type to the liquid mixture during the application stage (decrease in viscosity when the mixture is subjected tc shearing stresses, increase m viscosity when the mixture is at rest) and of endowing the final material with improved mechanical properties. For practical application, the vmylic component of the mixture to be cured is generally kept separate from the hydrogen-siloxane component up to the moment of application. For this purpose it can oe advantageous to prepare two separate mixtures, each containing the aforementioned components, mixed with other suitable additives. The two- component silicone rubber can then oe obtained by mixing, in suitable proportions, a part A and a part B. A typical example of a composition of parts (or components) A and B is as follows: Part A: containing one or more vmyl-siloxane compounds, a catalyst, optionally a silicone oil (or mixture of several silicone oils 1 to achieve the desired viscosity for application and, optionally, a suitable amount of silica; and Part B: containing one or more hydrogen-siloxane curing agents, optionally a silicone oil (or mixture of oils) and optionally, a suitable amount of silica. According to an alternative embodiment, part B can additionally contain a certain amount of vmyl-silicone compound. Part A and part B are then mixed together m suitable proportions at the moment of application of the material. Since it is necessary, for the specific application in optical device 100, that the elastomeric composition snould be able to be inserted in housings with relatively small dimensions, such as the space between the fms 109, it is preferable that the mixture for application (Part A + Part B) should nave a fairly low kinematic viscosity, preferably less than about 2000 mPas at 20°C, and yet sufficiently high, for example greater than about 500 mPas, so as to avoid excessive flow of the said mixture. A viscosity between about 800 mPas and about 1500 mPas is particularly preferred. The two parts of which the silicone rubber according to the invention is composed can preferably each have roughly the desired viscosity for the specific application, or that viscosity can be obtained on mixing the two parts, which will have respectively a higher viscosity and a lower viscosity than that desired, the final application viscosity being achieved when the two parts are mixed according to the predetermined stoichiometric proportions. As stated previously, the desired viscosity of the mixture can be obtained advantageously by adding a sufficient amount of silicone oil of a suitable viscosity to the two parts of the mixture. Once the two components of the silicone rubber have been mixed, the resulting mixture is poured into the appropriate nousmgs, as described below. The working time of the mixture, or the usefu ^ period during whicn tne mixture can be manipulated without appreciable increase m viscosity, varies from about 10 minutes to about 30, and is preferaoiy about 15-20 minutes. This period of time is generally considered sufficient to allow the operative to place the mixture easily into the housings. After that period of time, the viscosity of the mixture, as a result of progress of the curing reaction between the components, gradually increases, and placing of the material m the respective housings can become difficult. From the moment of mixing of the two components, tne material takes aoout 30 minutes to about 2 hours, preferably 1-1.5 hours to reach a hardness similar to the final hardness, for which the curing reaction can be regarded as substantially completed. As stated previously, the rubber will however need to have a somewhat lower hardness so as not to cause excessive mechanical stresses on the fibre-optic component 200 embedded m it. The desired softness of a silicone rubber according to the invention can be obtained either by suitable adjustment of the stoichiometric ratio of the reactants (on reducing the amount of hydrogen-siloxane compound there is a decrease in the degree of crossl kmg of the elastomer and hence its hardness) , or by adding a suitable amount of silicone oils of suitable viscosity to the mixture. Preferably, a silicone rubber according to tne invention nas a needle penetration value, measured according to standard ASTM D1321, between about 300 1/10 mm and about 600 1/10 mm, preferably between aoout 400 1/10 mm and about 500 1/10 mm. Application of the liquid mixture and of tne fibre- optic component 200 inside optical device 100 for the purpose of embedding the said component m tne silicone material can take place according to various metnoos of assembly. In all the cases described in the following, the liquid silicone mixture referred to is to be understood as the mixture of the two vmyl-siloxane and hydrogen-siloxane components, including catalysts and other any additives such as silicone oils or silica. As mentioned previously, the said mixture nas a sufficiently reduced viscosity, i.e. to permit its easy application in the spaces witn reduced dimensions of the optical device 100, thougn without oemg excessively fluid, to avoid excessive flow of the said mixture inside the housings. Typically, the viscosity of the mixture applied is between about 500 mPas and about 2000 mPas, and is preferably between about 800 and 1200 mPas . A first method of assembly of the optical device according to the invention comprises a first step of placement of the fibre-optic component 200 tne housing circuit 108 of base 101, and a next step that comprises pouring of the liquid silicone mixture on tne said component, m a quantity such as to cover tne said component with a layer aoout 1-2 mm thick. Placement of the fibre-optic component 200 is done with particular care so as not to induce stresses in the said component. A spiral profile of placement of the optical component, as shown in Fig. 1, may prove advantageous in that it ensures minimum stress for the fibre-optic component 200. Once the silicone mixture has oeen placed inside housing 108 made m base 101, the optical device 100 is left open at room temperature for about 2 hours so as to reach tne desired degree of cure of the ruboer, after which it is closed. This method offers the advantage of permitting easy recovery of the optical component before applying the silicone mixture, if the component should exhibit problems, for example as a result of incorrect handling of it m the placement stage. A second method of assembly of the optical device according to the invention comprises, as the first step, a first pouring of a minimum amount of silicone composition (for example a thickness of about 0.8 mm) on the oottom of housing 108 of the optical device 100. Next, once this first layer of silicone rubber has hardened, the fibre- optic component 200 is placed m the said housing. Then a second pouring of tne liquid silicone mixture s carried out so that the fibre-optic component 200 is embedded completely. This second layer is then _eft tc cure as described previously for the first method. The presence of the first layer of silicone rubber on the bottom of housing 108 provides slignt adhesion of optical component 200 placed m the said housing, tnus reducing the risk of possible slipping of the said component out of the said housings, as could occur m the first method. A third metnod comprises a first stage m which the silicone mixture is poured into housing 108 of optical device 100. Immediately thereafter, the fibre-optic component is placed m the said housing, taking care to emoed it completely m tne mixture that is still in the liquid state. Also in this third instance, it is possiole to exert better control during the stage of placement of the optical component, preventing tne possibility of accidental slippage out of the housing. Adopting one of the methods described above, the fibre-optic component is placed in the relevant housing with minimum stress, so as not to induce substantial changes of the transfer function of the said component. In any event, possible minimal changes of this transfer function are kept constant over time on account of the locking action of the silicone material on tne optical component, thus ensuring constancy of the optical oehaviour of the component. A person skilled m the art can easily fmo, on the basis of the above description, suitable methods of placement of the fibre-optic component mside the housing circuit, including the use of protective compounds that are αifferent from those explicitly referred to. The protective compound thus introduced into the housing circuit provides a permanently soft contact surface, wnich is thus able to absorb the stresses to which the fibre-optic component is suojecteo αurmg tne placement stage. This compound prevents the fibre-optic component 200 coming into contact with the walls of the housing circuit 108 and m addition is able to nold the fibre-optic component 200 m a position that does not vary significantly during tne life of the αevice, yet without transmitting any narmfui mechanical stresses to tne said component . Referring to the particular solution m Fig. 2, corresponding to the outlet openings 104 the cover adheres to the raised parts 112 and so does not exert pressure on tne underlying final section 203 of the fibre-optic component 200. It is also possible to use other planar profiles for which the fibre-optic component 200 lies above a plane so that no contact occurs only between soecifieo sections of tne component, for example those sect.ons that are more susceptible to changes of the transfer cnaracteristic. Planar profiles with forms different from that shown in Fig. 1 can be, for example, curves of tne spiral type with coils that are not circular and/or are not equispaced. Furthermore, the fibre-optic component 200 can be arranged so as to prevent contact througn αirect superposition between portions of the fibre-optic component 200 but permit some of its parts to be tangents. According to a particular alternative emoodiment of the invention, the fibre-optic component 200 may not be arranged m planar fashion, but can be wound on a mandrel made on base 101 m such a way that superpositions do not occur. Preferaoiy, fibre-optic component 200 is wound nelically. More preferably, it is wound m such a way that there is no contact of any type oetween different portions of the component. The elements delineating the housing circuit 108 are such as not to create changes in the behaviour of fibre- optic component 200, for example they do not contain sharp corners and do not impose excessive curvature on the said component . The optical device 100 described is suitable for housing, m addition to the aforementioned chirped grating 202, any other fibre-optic component. Examples of known fibre-optic components are: fibre gratings, active fibres used for amplification of optical signals, fibre couplers, optιca_ fibres genera^ sucn as monomode fibres, polarization-maintaining fibres, dispersion-shiftea fibres, fibres used in optica± sensors etc.) as well as components obtained by optical connection of these. It is further pointed out that the listed fibre-optic components can also include sections of purely transmissive optical fibre (such as a monomode fibre) arranged at the input and/or output or in intermediate portions of the said component . As already stated, the technical solution is suitaole for all fibre-optic components tnat have a portion of fiore with a corresponding transfer function that is susceptible to changes as a result of mechanical stresses and in which this portion is of a length sucn as to require that it be arranged in a wound configuration. Device 100 ensures tnat fibre-optic component 200 maintains, during tne life of the said device, a stable position, i.e. it ensures that the fibre-optic component, over its entire length or for predetermined sections, does not move significantly from the initial position inside base 101. In the particular case of device 100 described previously, the position of fibre-optic component 200 is kept stable owing tc the fact tnat the housing circuit 108 has dimensions that do not permit significant mobility of the said component, or because of tne action of the protective compound. The protective compound and the housing circuit 108 represent particular fixing elements but otner fixing elements are also suitable, such as other types of adhesives, grooves, containment fms, tubular patns for the fibre, the cover itself, crosslmkable resins used separately or combined, or any other element suitable for the purpose. A particular chromatic dispersion compensator (CDC) , which uses the optical device 100 illustrated above, will now be described. Fig. 3a shows a schematic representation of a chromatic dispersion compensator 300, comprising a three- port optical circulator 301 that has a first port connected to a fibre 302, a second port connected to a fibre-optic component 200, of the type described with reference to Fig. 1, and a third port connected to another fibre 303. The fibre-optic component 200 comprises, for example, two chirped gratings 202' and 202" of DCG type in cascade. Fig. 3b is a schematic representation of another type of chromatic dispersion compensator 300', comprising a four-port circulator 305 connected to fibres 302 and 303 and to a first fibre-optic component 200, and to a second fibre-optic component 200' similar to the first. Each of the fibre-optic components 200 and 200' includes two chirped gratings 202' and 202" cascade. The fibre-optic components 200 and 200' have reflected bands that are partially or completely superposed. The dispersion of compensator 300' is the resultant of the dispersion of components 200 and 200' m the superposition band. As is well known, along a fibre, such as a single-mode fibre, the components of an optical pulse are propagated at different speeds. In a step-index fibre of the type according to standard ITU-T G652, for example, the components with larger wavelength are propagated faster than the components with smaller wavelength. This causes a broadening and hence distortion of the data pulse. The chromatic dispersion compensators described are positioned at the end of a section of fibre to compensate the chromatic dispersion suffered by the pulses, corresponding to various optical signals, that were propagated aldng the said section of fibre. A pulse corresponding to a signal that has a defined optical wavelength, present at fibre 302, is transmitted from the optical circulator 301 to the fibre-optic component 200. Each component of the optical pulse is reflected oy the chirped gratings 202' or 202" at a point for which the known Bragg condition s satisfied. The components with greater wavelength satisfy the said condition after being propagated over a larger section of the chirped grating relative to the components with smaller wavelength. The components with greater wavelength, travelling a longer path, suffer a greater delay whereas those with smaller wavelength travel a shorter path and suffer a smaller delay. The delays introduced by the chirped gratings are of opposite sign to those introduced by the optical fibre because of chromatic dispersion and are such as to compensate them. The pulses corresponding to signals that have different optical wavelengths after compensation of dispersion are thus sent, via circulator 301, to fibre 303. The fibre-optic component 200 is suitable for compensation of chromatic dispersion of pulses corresponding to a predetermined number of optical signals with respective wavelengths, such as the optical signals of a wavelength division multiplexing (WDM) system. Compensator 300' m Fig. 3b operates similarly to compensator 300 m Fig. 3a out ensures that compensation of the chromatic dispersion accumulated by signals with different wavelengths occurs partly m the first fibre- optic component 200 and, after a further passage in the optical circulator 305, is completed in the second fibre- optic component 200'. Fig. 4 shows an exploded perspective view of a particular container 400 able to contain two chromatic dispersion compensators of type 300' described m Fig. 3b. The connecting optical fibres 302 and 303 are not shown in Fig. 4. Container 400 has a lower rack 404 containing a four- port circulator 305 and two superposed optical devices 100. The optical device 100 that rests directly on the lower rack 404 is of the type shown m Fig. 2, i.e. it nas two output fibres and is connected m series to optical device 100 above it. Circulator 305 is laid gently on lower rack 404 m the central part of the ring delimited by the two optical devices 100. Positioned aoove the ^ ower rack tnere is an intermediate rack 405 which in its turn contains a four port circulator 305', similar to circulator 305, and two optical devices 100 superposed and connected m series as indicated previously. Fig. 4 shows optical device 100 in the upper position, and is fitted to intermediate rack 405 by means of suitable cylindrical elements 408. An organizer rack 406 is superposed on intermediate rack 405 and is closed with a cover 407. The circulators 305 and 305' are for example manufactured by JDS (USA), E-TEK CA (USA) and are of parallelepiped shape. The racks and the cover are, for example, made of plastics material of the same type as useo for making the base 101 of optical device 100. Fig. 5a shows a perspective view of the lower rack 404 that is of rectangular shape and has edges 411, cylindrical or semicylmdrical elements 408 for fitting the two optical devices 100, two posts 409 for fitting the circulator 305 and small pillars 410 for the passage of screws or other fastening elements. Fig. 5b shows the intermediate rack 405 comprising, m addition to tne components already described with reference to the bottom rack 404, two posts 409 for securing the circulator 305' and two slits 412 for passage of the optical fibres that come from the two optical devices 100 housed m the bottom rack 404. The intermediate rack is provided with an opening 413 that permits passage of the optical fibres for connection to the circulator 305 housed m the bottom rack 404. Fig. 5c shows the organizer rack 406 comprising openings 412 arranged on four sides of the rack for passage of the optical fibres from all four optical devices 100 present m the lower 404 and intermediate 405 racks, and openings 418 for passage of the fibres connected to the ports of circulators 305 and 305'. On edges 411 of the organizer rack, there are holes 420 of various sizes for passage of elements for locking the cover 407. The organizer rack 406 also has fms 415 which delimit guides for the optical fibres and suitable housings 414 that are able to contain the welded fibre sections. Advantageously, organizer rack 406 is provided witn two sets of housings 416 for circulators of cylindrical type of different sizes. Container 400 for a CDC, described, is especially versatile, in that it permits the use of circulators of parallelepiped shape 305 and 305' but tney can also be replaced with circulators of cylindrical snape . In particular, a pit 417 is made m housings 416, so that circulators of cylindrical shape and having certain dimensions cannot project above the edges 411 of the organizer rack 406. Circulators of cylindrical shape are manufactured, for example, by the aforementioned JDS and E-TEK. The organizer rack 406 has openings 419 for the passage of optical fibres to the outside and pillars 410' which, aligned with pillars 410 of the bottom rack 40 and intermediate rack 405, permit, for example, the passage of screws for joining the three racks and the cover 407. In the two chromatic dispersion compensators, eacn made according to the scheme shown Fig. 3b, and containing in the said container 400, the optical fibres (not shown m Fig. 4) that come from the circulators 305, 305' ano from the four optical devices 100, pass respectively through the appropriate openings 413 and 412 to reach the organizer rack 406. The optical fibres are wound round the fms 415 and are connected together m ways that are obvious to a person skilled in the art from the above description ana from the relevant diagrams. It can be seen that the fibre-optic components 200 and 200' are each arranged m their own casing, comprising the base 101 and the corresponding cover, and are separated structurally oy the optical circulators 305 ano 305' arranged externally to the said casings. The applicant has noted that the optical device 100 makes it possible to use the fibre-optic component noused within it as a discrete component. For example, tne optical device 100 can easily be transferred from one container to another without approaching the fibre-optic component housed therein and so avoiding repetition of the placement operation, which is particularly delicate ana requires subsequent characterization, oy measuring its transfer function. Containers similar to container 400, aole to house optical equipment of a type that is αifferent from the chromatic dispersion compensator illustrated and comprising a fibre-optic component suitaoly connected to an optical device, for example an optical isolator, or an optical coupler in planar optics or of the fused-fibre type, can easily be made by a person skilled in the art on tne basis of the above description. An example of optical equipment, suitable for housing m a container of the type as described with reference to Fig. 4, is a fibre-optic amplifier of a known type. An optical amplifier of this kind comprises, for example, an erbium-doped optical fibre arranged between two optical isolators ana connected to an optical coupler capable of transferring, to the doped optical fibre, the optical power emitted from a suitable pump source. The erbium-doped optical fibre is advantageously arranged, as described previously, m base 101 and the optical isolators and tne optical coupler are arranged inside container 400 in a similar manner to that described witn reference to the optical circulators 305 and 305' in Fig. 4. The optical connections oetween the erbium-doped fibre, the optical coupler and the two optical isolators are effected inside an organizer rack similar to rack 406 described earlier. EXAMPLE 1 Measurements of reflectivity of chirped gratings The Applicant has conducted experiments measuring the reflection spectrum of a fibre chirped grating, oefore and after placement, both in a module according to the known technology and in a casing such as that described with reference to the optical device 100. As already stated, devices for compensating chromatic dispersion are housed, accordance with the known technology, in suitable modules such as those manufactured by the Applicant ano designated with the symbol CDCM (Chromatic Dispersion Compensation Module), for example models CDC 0480, and CDC 016160. Such a module is for example suitable for containing two devices for the compensation of chromatic dispersion, used m a bidirectional optical transmission system. Referring to Fig. 6, the module 600 comprises a metallic base 601 provided with channels 602 for passage of the optical fibres to the outside, a central area 603 capable of containing one or two circulators, arc-shaped fms 604 and housings 605 suitable for accommodating the cylindrical casings for protecting the welds. The module used n the experiment was about 21 cm long and 14 cm wide. EXAMPLE la Measurement of reflectivity of a chirped grating arranged m a rectilinear position The fibre chirped grating in question, manufactured by the applicant, had a total lengtn of about 2 metres, with the grating occupying about 160 cm of that. A preliminary evaluation of the reflectivity of the fibre chirped grating was effected by carefully placing the chirped grating on a bench an almost rectilinear position. One end of the fibre chirped grating was connected to a first port of a conventional coupler. A second port of this coupler was suitably connected to a wide-spectrum optical source while a third port was connected to a spectrum analyser suitable for measuring the spectrum of the signal reflected from the chirped grating. The other end of the optical fibre, in which the chirped grating was inscribed, was cut in such a way that the final surface was suitably inclined relative to the optical axis of the said fibre, typically with an inclination of 7-8°, to prevent reflections. To reduce any residual reflections, the said end was immersed m an optical oil possessing a refractive index n equal to that of the fibre's core (n ≡ 1.46). Fig. 7a shows the spectrum of reflectivity of the chirped grating measured prior to placement in base 601, i.e. it shows the absolute value of the ratio, expressed in decibels, between the reflected power and the transmitted power in relation to the wavelength. The applicant points out that in the graph of reflectivity shown in Fig. 7a and in the graphs in the following figures, the value shown on the ordinate also takes account of the losses introduced by the measurement set-up. These graphs are significant not for the absolute value of reflectivity, but for evaluating its variation with the wavelength. EXAMPLE lb Measurements of reflectivity of a chirped grating housed in a device according to the state of the art Next, the applicant placed the fibre chirped grating in base 601. The fibre chirped grating was then arranged as several windings along paths of the circular type delimited by fms 604 and housings 605. Some housings 605 were occupied by welds in the fibre whereas other housings constituted guides for sections of the fibre component. In one such path, oetween two contiguous fms 604, several portions of different windings were necessarily housed with contact between them and there were also superpositions between various points of the portion of fibre containing the cnirpeo grating. Next, in the manner described aoove, measurement of reflectivity was repeated. The measured spectrum is shown n Fig. 7b. The applicant observed the presence of a sharp drop in reflectivity corresponding to a wavelengtn of about 1544.5 nm. The applicant assumed that this drop m reflectivity was due to mechanical stresses exerted on the fibre component during placement. The applicant believes that the contacts present oetween some sections of the fibre component can constitute mechanical stresses such as to alter the reflectivity spectrum, as found by measurement. In particular, the applicant considers that contacts through superposition can induce mechanical stresses of greater magnitude than those induced by contacts between tangent portions. Then the applicant extracted the test fibre and inserted it again base 601. The reflectivity spectrum was then measured, with the result shown m Fig. 7c. It can be seen m Fig. 7c that there is a drop in reflectivity corresponding to wavelength of about 1540 nm. The drop m reflectivity corresponding to another wavelength value may be due to stresses occurring in a zone of the fibre different from that corresponding to Fig. 7o. A second fibre chirped grating was then considered; this had a length of about 1.5 m and a diameter, including the recoating region, of about 0.4 mm. Fig. 8 shows, with a thin continuous line, the reflectivity spectrum of this second chirpeα grating, extended, i.e. carefully laid on a bench an almost rectilinear position and not subjected to forces. The spectrum occupies a wavelength range between 1538.5 nm and 1545 nm. This second chirped grating was inserted in base 601 made according to the state of the art and its reflectivity spectrum was measured as describee above. The measured reflectivity spectrum of this second cnirped grating housed case 601 is shown Fig. 8 with a dashed line. For some wavelength values, this spectrum diverges from that relating to the extended component by an amount less than 0.5 dB . For other wavelength values, for example corresponding to a wavelength of 1539.5 nm, there is a deviation of about 0.5 dB . For wavelength of 1544.5 nm there is a deviation of about 1 dB . EXAMPLE lc Measurement of reflectivity of a chirpeo grating arranged n a housing according to tne invention The applicant made a base 101 as describee with reference to Fig. 1. Base 101 was made of reinforced polycaroonate with dimensions of 12 cm x 12 cm x 3 mm. The housing circuit 108, with a spiral profile, was obtained by milling inside tne base 101. The cover used had a thickness of 0.7 mm. The arc-shaped fins 109 had a thickness of about 0.5 mm and a height of about 2.5 mm. The distance between two adjacent arc-shaped fins 109 was about 1 mm. Next, the fibre chirped grating was placed, base 101, according to the method described previously with reference to optical αevice 100, which additionally envisages pouring of the protective compound and its curing. The protective compound used was a mixture made according to the next Example 2. This mixture was cured for about 2 hours . The measured reflectivity spectrum of the second chirped grating, of Example lb, placed in base 101, is shown by the thick continuous line m Fig. 8. All the deviations between the points of the spectrum of the chirped grating placed m base 101 and those of the extended chirped grating are less than 0.5 dB, and m particular are less than 0.2 dB . These experiments have shown that optical device 100 makes it possible to protect the fibre-optic component 200, greatly reducing tne changes in transfer function that occur in the placement stage relative to the changes that occur m placement m a conventional type of module. EXAMPLE 2 Preparation of the silicone rubber The Applicant prepared a first silicone rubber by mixing the following parts A and B, with the following compositions : Part A Part B Compound Parts by -Si-H Total - -Si-H weight groups , groups mmol/g (mmol) Silopren U230 1.0 2.3 2.3 Silicone oil MlOO 15 - - Silicone oil M500 26 - - Silica Cab-O-Sil 8.0 - - TS610 The vmyl-siloxane compounds Silopren Ul and Silopren U10, the hydrogen-siloxane curing agent Silopren U230 and the silicone oils MlOO ano M500 are marketed by the company Bayer AG . Silica Cab-O-Sil TS610 is marketed by the Cabot company. The kinematic viscosity of the two parts A and B (and hence of the mixture of the two) is about 1000 mPas at 25°C (ASTM D445) . Parts A and B are mixed in 1:1 ratio, so the molar ratio between vmyl groups and hydrogen-siloxane groups is about 1:0.8, hence with a slight stoichiometric deficit of the last-mentioned reactive groups. The working times of the fluid mixture are about 15-20 minutes. Approximately one hour after mixing the two components, tne composition has the consistency of a rubbery solid, reaching its final hardness in two-three hours. In the needle penetration test according to standard ASTM D1321, the rubber gives a value of about 470 tenths of mm. EXAMPLE 3 Preparation of the silicone rubber The applicant prepared a second silicone rubber following the procedure described in Example 2, with the only difference that the parts by weight of compound Silopren U230 in part B of the mixture were 1.25 msteao of 1.0. In this way, on mixing part A with part B m 1:1 proportions, the stoichiometric ratio between vmyl groups and hydrogen-siloxane groups becomes about 1:1. The rubber so obtained displays characteristics similar to those of Example 2, with a penetration value of about 400 tenths of mm. EXAMPLE 4 Evolution of hydrogen through ageing of the ruober The applicant prepared 10 g specimens of silicone rubber according to Examples 2 and 3, by distributing a thin layer (about 200 μm thick) of liquid mixture on the inside surface of a series of test-tubes (internal volume 150 cm 3 ). 0.1 ml of water (5.5 mmol) was also present in the test-tubes. A first group (Gl) of specimens of 1:0.8 mixture (vmyl groups : hydrogen-siloxane groups) according to Example 2 and a second group (G2) of specimens of 1:1 mixture according to Example 3 were prepared m tnis way. Each of the two groups Gl and G2 was divided into two subgroups, respectively Gla and Gib, and G2a and G2b. The test-tubes of both subgroups Gla and G2a were sealed immediately after distribution of the liquid mixture on the surface of the test-tubes and the mixture was cured with the test-tube sealed. On the other hand, the mixtures in subgroups Gib and G2b were cured with the test-tube open, sealing the test-tubes once curing had ended. On completion of curing, approximately tnree nours after deposition of the liquid mixture, the test-tubes containing the silicone rubber were submitted to an ageing test at 100°C for 15 days m a stove (roughly corresponding to ageing of more than 20 years at a temperature of about 10°C) . At the end of ageing, the test-tubes were recovered and the composition of the gases evolved inside the said test-tubes was analysed by means of a Hewlett-Packard Mod. 5480 gas chromatograph to detect any traces of hydrogen. The results of the ageing test are presented in Table 1. Table 1: Ageing test As can be seen from the data m Table 1, even m the more severe conditions of group G2a, nydrogen evolution remained well below the limits indicated as acceptable of 1 cm 3 /kg and preferably of 0.5 cm 3 /kg. In a similar ageing test on a comparative composition prepared according to Example 3 but with a ratio 1.5:1 of ≡ SiH groups relative to vmyl groups (i.e. 4.32 parts by weight of compound Silopren U230 m the total composition) , the amount of hydrogen evolved (measured m the test-tube sealed after curing) was greater than 100 cmVkg of material .

Claims: ;LAIMS 1) Optical apparatus comprising a container (400), mside which are arranged: - a fibre-optic component (200) capable of being arranged m a configuration comprising a plurality of adjacent windings, - an optical component (305) capable of being connected to the said fibre-optic component, characterized that the said container comprises: - a housing (101) for tne said fibre-optic component, the said housing comprising - at least one separating element (109) capable of physically separating the windings of tne said plurality so as to avoid contacts through superposition oetween them, - an element for fixing the said fiore-optic component, capable of nolding the saio component m a stable position. 2) Optical apparatus according to claim 1, characterized in that the said optical component (305) comprises at least one optical fibre for connection. 3) Optical apparatus according to claim 2, cnaracteπzed m that the said container comprises a unit 406) for connection of the said fibre-optic component (200) to the said at least one optical fibre for connection of the optical component (305). 4) Optical apparatus according to claim 1, m wnich the said fibre-optic component (200) comprises a fibre-optic grating. 5) Optical apparatus according to claim 1, m wnich the said optical component is an optical circulator (305) . 6) Optical apparatus according to claim 1, m which the said fibre-optic component is an active optical fibre. 7) Optical apparatus according to claim 1, in which the said optical component is an optical ^ solator. 8) Optical apparatus according to claim 1, m wnich the said optical component is an optical coupler. 9) An optical device (100) comprising - a fibre-optic component (200), which is associated with a predetermined transfer function, capable of being arrangeα m a plurality of adjacent windings, - a rigid housing ιl01) capable or containing the said fibre-optic component, characterized that the said housing comprises - at least one separating element (109) capaole of physically separating the windings of the plurality so as to avoid contacts through superposition between them, - an element for fixing the said fibre-optic component, capable of holding the said component in a stable position . 10) An optical device according to claim 9, cnaracterized in that the said separating element is capable of separating tne windings of the said plurality so as to avoid contacts oetween them. 11) An optical device according to claim 9, characterized in that tne said optical component (200) comprises a fibre grating (202) in one portion thereof. 12) An optical device according to claim 9, cnaracterized in that the said optical component (200) comprises a fibre cnirpeo grating (202) m one portion thereof. 13) An optical device according to claim 9, characterized in that the said optical component (200) comprises a chromatic dispersion compensator. 14) An optical device according to claim 9, characterized in that the said optical component (200) comprises an active fibre. 15) An optical device according to claim 9, characterized in that the said fibre-optic component (200) nas a length of between 10 cm and 20 m. 16) An optical device according to claim 9, characterized m that the said fibre-optic component (200) nas a length of between 20 cm and 20 m. 17) An optical device according to claim 9, cnaracterized in that the said rigid housing (101) s made of polycarbonate . 18) An optical device according to claim 9, characterized m that the said rigid housing (101) is made of a material comprisig an aluminium alloy. 19) An optical device according to claim 9, characterized in that the said rigid nousmg (101) comprises fms (109) capable of delineating a housing circuit (108) for the said component. 20) An optical device according to claim 1, characterized in that the said housing (101) comprises grooves. 21) An optical device according to claim 9, characterized in that the said separating element comprises at least one fin (109) interposed oetween two windings of the said plurality. 22) An optical device according to claim 9, characterized in that the said separating element comprises crosslmkable resins. 23) An optical device according to claim 9, cnaracterized in that the said fixing element is a sealing grease. 24) An optical device according to claim 9, cnaracterized in that the said fixing element is a silicone compound. 25) An optical device according to claim 9, characterized in that the said fixing element is a polyurethane resm. 26) An optical device according to claim 9, characterized m that the said fixing element is a cover that is structurally linked to the said base. 27) A method of assembling an optical device comprising a fibre-optic component (200) which is associated with a predetermined transfer function, the said method comprising the steps of - placing the said component mside a rigid housing (101) in a wound configuration such as to avoid superpositions between the various parts of the component, - locking by means of a fixing element the said component in the said configuration so as to prevent movements inside the housing. 28) A method of assembling an optical device according to claim 27, characterized in that tne said placement stage comprises a steps of placing the said optical component in a configuration that avoids contacts oetween the various parts of the component. 29) A method of assembling an optical device according to claim 27, which the said step of placing the component inside the housing comprises placing the said component in a spiral configuration. 30) A method of assembling an optical device according to claim 29, in which the said spiral configuration has a pitch greater than or equal to the maximum diameter of the fibre-optic component (200) . 31) A method of assembling an optical device according to claim 29, in which the saio spiral configuration has a pitch approximately equal to 1.5 times the maximum diameter of the said fibre-optic component. 32) A method of assembling an optical device according to claim 27, m which the said locking step comprises a step of inserting a quantity of a protective compound n the said housing. 33) A method of assembling an optical device according to claim 27, in which the said transfer function is associated with a predetermined reflectivity spectrum. 34) A method of assembling an optical device according to claim 33, characterized in that, m the step of placing the saiα component m the said housing, the said reflectivity spectrum undergoes a change of less than 0.5 dB. 35) A method of assembling an optical device according to claim 34, characterized m that, m the step of placing the said component in the said housing, the said reflectivity spectrum undergoes a change of less than 0.2 dB.

Inventors: DE DONNO MARCO, DELROSSO GIOVANNI, SCARANO DANILO, DE DONNO, MARCO, DELROSSO, GIOVANNI, SCARANO, DANILO
Applicants: DELROSSO GIOVANNI, DONNO MARCO DE, OPTICAL TECHNOLOGIES ITALIA S, SCARANO DANILO, DE DONNO, MARCO, DELROSSO, GIOVANNI, OPTICAL TECHNOLOGIES ITALIA S.P.A., SCARANO, DANILO
Application year: 2000
Main classification: H01S3
IPC codes: G02B6, H01S3, H05K7