GB2116708A - Method of and apparatus for determining the radial refractive index profile of an optical specimen - Google Patents

Method of and apparatus for determining the radial refractive index profile of an optical specimen Download PDF

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GB2116708A
GB2116708A GB08307578A GB8307578A GB2116708A GB 2116708 A GB2116708 A GB 2116708A GB 08307578 A GB08307578 A GB 08307578A GB 8307578 A GB8307578 A GB 8307578A GB 2116708 A GB2116708 A GB 2116708A
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refractive index
light
axis
endface
angle
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Robert James Mansfield
David Neil Payne
Issei Sasaki
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National Research Development Corp UK
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/17Systems in which incident light is modified in accordance with the properties of the material investigated
    • G01N21/41Refractivity; Phase-affecting properties, e.g. optical path length
    • G01N21/412Index profiling of optical fibres

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  • Investigating Or Analysing Materials By Optical Means (AREA)

Abstract

To determine the radial profile of the refractive index of a substantially cylindrical optical specimen such as an optical fibre or optical fibre preform 20, the specimen is illuminated with a collimated beam of light 28 incident at an angle to the axis of the specimen differing substantially from 90 degrees and the refraction angle at which the light beam leaves a substantially plane end face 22 of the specimen as a function of its radial position on the end face is measured. <IMAGE>

Description

SPECIFICATION Method of and apparatus for determining the refractive index profile of an optical specimen This invention relates to the measurement of radial refractive index profile in an approximately cylindrical object which is essentially invariant (or slowly varying) along its length.
The specification of our co-pending UK Patent Application No. 81 07603 describes the measurement of the optical deflection function and/or the radial refractive index profile of an essentially cylindrical object such as an optical fibre or an optical fibre preform.
The cylindrical object is illuminated by a collimated beam perpendicular to the cylindrial axis. Light transmitted through the curved sides is refracted by the radial variation in refractive index, is then focussed and modulated so that the deflection function can be derived, and from that function the refractive index profile can be obtained by a mathematical transformation.
The present invention relates to a further method of sensing the refractive index profile, usually of an optical fibre preform, but possible also of a single optical fibre, in which the profile is obtainable without use of a mathematical transformation.
According to the invention there is provided a method of measuring radial variations in the refractive index of an approximately cylindrical, translucent object having a substantially plane end face and a substantially invariant refractive index in a direction parallel to its axis, comprising illuminating the end face by means of a collimated beam of light incident at an angle to the cylindrical axis which differs substantially from 90 degrees and measuring at a plurality of radial positions the refractive angle at which light leaves the end face.
There is also provided apparatus for measuring radial variations of refractive index as claimed in Claim 5 having modulating means positioned in the path of said light beam between said focussing means and said sensing means.
Usually the end face will be perpendicular to the cylindrical axis, and usually the light will pass first through the curved surface and then to the endface so that the angle of exit of light from the object is measured, but it is also possible for the light to be directly incident on the endface, with measurement of the angle at which light passes from the endface into the object. The measurement is practicable when the illuminating beam makes an angle of up to 60 with the plane of the endface; at greater angles the length of travel in the preform is so great that accuracy is lost. Usually the light will pass into and out of the object though an index-matching liquid which has an index approximately equal to that of the cylinder outer surface.
The refraction angle at which light leaves the endface may be measured as a function of position on the endface by probing the object with a thin pencil of light, such as from a laser, and directly measuring the beam deflection. Alternatively, the measurement can be made by illuminating all or part of the endface with a broad light beam, focussing said light with a lens so that in the focal plane of said lens the distance of transmitted light from the optical axis in a direction coplanar with the endface of the object is approximately linearly proportional to the angle through which light has been deviated by the object; optically modulating the focused light so that a property of the light varies as a function of said distance; and receiving the modulated light in an image plane, whereby the refractive index profile of the preform can be derived.
The optical modulation may be such that either a spatial or a temporal property of the light varies in the required direction.
In the accompanying drawings, Figure 1 illustrates the optical path through a cylindrical object during measurement according to the prior art method decribed in UKPA 81 07603. The invention will be described with reference to the other Figures in which: Figure 2 illustrates schematically the general optical arrangement according to the invention; Figure 3 shows the endface and an input and output ray of light; Figure 4 illustrates modulation by a neutral density filter; Figures 5 and 6 illustrate modulation buy a knife edge in two different axial positions and Figure 7 illustrates a shadowgraph image; Figure 8 illustrates use of a grating plate or a multicolour grating plate and Figures 9 and 10 show two possible images;; Figure 11 illustrates use of a cylindrical lens, and Figures 12by), (b) and (c) show three possible images; Figure 13 illustrates use of a cylindrical lens plus a grating, and Figures 14(a), (b) and (c) show three possible images; Figure 15 illustrates temporal modulation; and Figure 16 shows a possible measured refractive index profile in the form of a two-dimensional graphic plot.
In the prior art arrangement of Figure 1, an object 10 such as an optical fibre or an optical fibre preform is illuminated over part or the whole of its diameter by a collimated beam of light 12 incident at right angles to the cylindrical axis 14 of the object. The passage of a single light raythrought the object is shown, and the change of direction through angle is related to the refractive index profile in the shaded plane (x,y) perpendicular to the axis. It can be seen that light enters and leaves through the curved walls of the object.
Various optical arrangements can be used to determine the profile and are described ih UKPA 81 07603; some arrangements can be applied to the present invention.
The general arrangement according to the present invention is shown in Figure 2 in highly schematic form.
A generally cylindrical optical fibre preform 20 has a flat endface 22 perpendicular, or at a known angle, to the cylindrical axis of the preform. The preform is immersed in a bath 24 of index-matching liquid 26 and a beam of collimated light 28 (indicated by is central ray) from a source 30 is incident on the preform adjacent the endwall at an angle of 45 to the preform cylindrical axis, light entering the preform through its curved surface, and exiting through the endface 22. Transmitted light passes through a spherical lens 32 to a sensing system 34, which senses, as a function of position on the endface 22, the angle at which light leaves the preform 20. The sensing system can take many forms which will be described below.An alternative position of the preform 20 is shown dotted; light then enters the endface and leaves through the curved walls, and measurement of angle is made through the curved walls.
Figure 3 shows the endface 22 and adjacent curved walls of the preform 20; the preform cylindrical axis is indicated at A. The refractive index of the index-matching fluid 26 is n,, and the refractive index n(u,v) ofthe preform 20 varies over the endface 22 as a function of position, (u,v), where the axes u and v in the plane of the endface 22 are shown.
The illuminated beam is incident on the preform 20 at an angle ato the plane of the endface 22. The passage of one light ray indicated by the double arrow, is shown; the ray is incident on the curved wall at point B, passes through the preform as indicated by the dotted line, and exits from the preform through the endface 22 at point C. The ray has been deviated from its original direction, shown chain-dotted, by an angle #.
We have discovered that this refraction angle I is related and is nearly proportional to the refractive index of the preform at the point on the endface at which the ray leaves the preform. Our inventive method and apparatus are based on this discovery. Thus measurement of angle as a function of position on the endface gives a measure of the refractive index profile of the preform without the need for numerical transformation.
Not only can measurement be made directly, but the index profile of a non-circular preform can be determined easily; considered now theoretically it can be shown that: cos2(ap) = n2(u,v) - sin2a (1) nl2 When, as is usually the case, the preform is immersed in an index-matching liquid, the ray at refraction angle ,0 experiences a further refraction on emerging into air, given by Qla = nile, which must be taken into consideration. Here Çla is the refraction angle in air.Equation (1) holds, provided it is taken that cos# #1, sin # # # (2) and 2n (u,v) = n2 (u,v)-n,2 QL2 n(u,v) (3) n21 n1 If the relative index differences A between different parts of the endface are small, then there is a simple relationship:- A (u,v) Q,Qia sin 12ce 1 / (4) 2n1 A plot of n(u,v) as a function of angle 0 for various values of angle a (not illustrated) shows that for A n(u,v) up to 0.02, the approximation of Equation (4) is valid, so that the measurement of refraction angle is linearly related to the refractive index at the exit point on the endface.
!t is believed that it has not previously been realised that this simple relationship exists. Thus a method and apparatus according to the invention rely on the measurement of angle as a function of position to determine the refractive index profile.
Preferably by provision of the spherical lens 32 (Figure 2) the angular deviation in air Çla of a ray is converted in the focal plane of the lens to a linear position along an axis win that plane, where the axis lies in the plane containing the preform axis A. The usual lens transfer equation applies, i.e.
w = ftan()a (5) where fis the focal length of the lens. The relationship is illustrated in Figure 4.
From Equation (5) it can be seen that when fla is small, w is almost linearly related to pal and therefore to the refractive index of the corresponding point on the endface 22. Therefore by modulation of the light passing through the lens 32, the light distribution in the focal plane of the lens, and hence the local refraction angle, can be determined. The modulation can be spatial or temporal, and can either produce a direct display of a pattern related to index profile, or can produce measureable data which can be converted into a graphic display.
Some of the many forms of the sensing system 34 by which the refraction angle pl as a function of endface position (u,v) can be measured will now be described, by the following examples are by no means exhaustive.
Figure 4 illustrates a first method of applying spatial modulation. In the focal plane of the lens 32 is a neutral density filter 36 having a linear (or other known) attenuation in the w direction. The intensity in the image is an image plane 38 is therefore related to the local refractive index in the endface 22.
Let To be the transmission of the filter 36 at w=o, and T be the transmission elsewhere, then if a is a constant, we can define the transmission T of the filter as: T = aw+T0where1T;'0 (6) The intensity I of the modulation image in the image plane u', v' at a distance qfrom the filter 36 is then: 2af = An(u,v) l(u',v') = lc{ sin 2a )+To} (7) where 1o is the uniform intensity of the image in the absence of the filter. The endface co-ordinates u, v are related to the image co-ordinates u', v' by the usual lens formulae: u' = -qusina (8) f v' = -qv (9) f Thus the density-graded image in the plane u', v', gives a picture of the refractive index distribution on the endface 22.To measure the index profile, a small photodiode 40 of diameter D is scanned across the image plane 38 by a stepping device 42 controlled by a control unit 44. Alternatively, the preform can be translated and the photodiode kept stationary. The intensity sensed by the photodiode 40 is supplied to the control unit which supplies to a visual display unit 46 a two dimensional display of the refractive index profile in the endface 22.
Figure 5 illustrates the use of a straight knife edge 48 arranged in the focal plane of the lens 32 and parallel to the u and u' axes. The knife edge can be stepped across the focal plane in the w direction by a micromanipulator 50. The movement progressively removes light rays in accordance with their angle of refraction 0. At any position wc of the knife edge all areas of the image in the image plane (u', v') with < wc, i.e. with n < nc, will be dark due to the knife edge shadow, where nc is the index at the shadow edge in the preform endface image, and from Equation (4) is given by:: Nc = n1 + w sin 2a (10) 2f Thus a reading of w, from the micromanipulator dial allows the determination of the index at the shadow boundary. The image will in general be an illuminated oval centre with a dark annular outer ring indicating the extinguished rays. As the knife edge approaches the optical axis of the apparatus is progressively removes the more highly deflected rays and the areas of low index are gradually extinguished. Thus the dark area increases, and when the knife edge is on the axis all light from the background index-matching fluid is intercepted, leaving illuminated only those areas of the preform with index higher than the fluid.
Measurement of the corresponding knife edge position w, and the position of the dark area boundary relates refractive index to position in the endface An automatic measurement can be made using a photdiode (not shown) scanned across the image plane.
Figure 6 illustrates a modification of Figure 5 in which the knife edge 48 is positioned out of the focal plane at a distance (fas) from the lends 32; a slightly different shadow pattern is observable in the image plane u', v'; the shadow boundary co-ordinate y' is given by: v' = w'q+w(1-q) = w'q+Av' (1) 5 5 where w' is the distance of the knife edge from the optic axis. Since w = ftan fa Qfn10 = 2 n(u,v) (12) sin 1 2a 1 the co-ordinate A v' is directly proportional to local refractive index difference A n(u, v,), and the shadow pattern therefore shows the refractive index profile.A typical shadow pattern is shown in Figure 7; the shaded area is the shadow cast onto a screen in the plane u', v', and its correspondence to the preform structure 20 is indicated - the preform has a core 20A and a cladding layer 20B of markedly different refractive index. The slight radial variations in the index of the cladding can be seen. It is an advantage of the Figure 6 arrangement that very large preforms can be examined because selected small areas of the endface can be displayed and analysed individually.
Figure 8 illustrates the use of the transmission grating 52 having alternate opaque and transparent areas parallel to the u' axis i.e. orthogonal to the waxis. The grating pitch is dand the grating is positioned at a distance 6 beyond the focal plane of the lens 32. In the image plane u', v', a fringe pattern resembling an interference fringe pattern will be seen, as illustrated in Figure 9. The relationship between the variable is: v' = w'q+w(1-q) (13) o where w' is the co-ordinate in the plane of the grating 52 parallel to the w direction. The first term of Equation (13) determines the spacing dq/S of the dark lines in the plane u', v', and the second term indicates the fringe shifts. The fringe shifts is dependent on distance o, and can be indicated as S'(u, v).Then the index difference An(u, v) on the endface 22 is given by: An(u,v) = - 1 S' (u,v) sin 1 2a 1 (14) 2 f(1 - q) S Equation (14) does not include the grating pitch d, but the pitch gives the tringe spacing so it determines the resolution.
For the special case b = o, i.e. with grating 52 in the focal plane of the lens 32, the fringe pattern in the image plane u', v' takes the form of contour lines of constant refractive index, as illustrated in Figure 10. The contours are spaced at intervals corresponding to an index increment of nE, where: = = dsini2ol1 (15) 2f The fringe spacing in the image is proportional to the gradient of the index profile. An attractive modification of this technique is to replace the grating 52 by a multicolour filter having bands of different colours running orthogonal to the wdirection. In this case, with white light illumination, the contour lines illustrated in Figures 9 and 10 become coloured which allows the differences in index to be more clearly seen.
The apparatus arrangements of Figures 4, 5, 6 and 8 give outputs which, while directly related to refractive index profile without the need to apply a mathematial transformation, still need considerably interpretive effort, either by mathematical calculation or by reading by an experienced human eye. It is also possible to give a more easily interpreted two-dimensional visual display of the index distribution in the preform endface. One such arrangement is illustrated in Figure 11 in which a cylindrical lens 54 is placed in the focal plane of the lens 32, the axis of lens 54 being parallel to the u and u' axes. The cylindrical lens 54 further refracts the rays arriving in the focal plane by an amount which is proportional to their distance wfrom the optical axis, i.e. in proportion to their refraction angle PI at the endface 22. If p is fthe secondary refraction angle, then :- tan ss = fB -tan7tana-w) (16) where f' is the focal length of the cylinderical lens 54. If f' > > tan fa (f' tana), then tanp - f (17) f The secondary refraction displaces a ray by a distance m in the axial direction of the preform 20, where m depends on the local refractive index n(u,v), and: m q [tan (ss + p") - tan p"] (18) where ,0" is the angle of the ray to the optical axis when the cylindrical lens 54 is absent.If tan p tan 0 < < 1, then: m = q tan B Substitution of equation (17) into equation (19) gives: w m = -qf (20) By using equations (2) and (5), equation (20) can be rewritten as: m = - qf2An(u,v) (21) f'sin 2a1 Thus the ray shift introduced by the cylindrical lens 54 produces a two dimensional display of the refractive index distribution in the preform endface, since it is in proportionto the local index difference n(u,v) at the point in the endface 22 from which the ray emerged. If the core has a higher index than the preform cladding, the image of the endface is bowed inwards with a coresponding shape.
If the cylindrical lens 54 is moved a distance 6 beyond the focal plane of the lens 32 as indicated by the broken line, the ray shift m is then given by: m = v'p - ftan pa(q - 6)2 = V'p - 2 n(u,v) f(q - 5)2 (22) qf qf' qf qf' sin ) 2a where p = 62 - Sq + qf' (23) and v' is the ray arrival point in the image plane u', v' when the cylindrical lens 54 is absent.The index profile image then depends on the value of the parameterp; for p > o, the profile of n > n1 appears inside the preform, as shown in Figure 12(a) for a typical graded-index preform; for p=o the image becomes a line with only the index profile visible, as shown in Figure 12(b); and for p < o, the profile of n > n1 appears to protrude from the preform as in Figure 12(c).
It is often convenient to display the type of image given by the Figure 11 arrangement with superimposed contour lines. A suitable arrangement is shown in Figure 13 which is a multipurpose diagram indicating two possible arrangements. In addition to the components shown in Figure 11, with the cylindrical lens displaed from the image plane, a grating plate 56 can be placed between the illuminating beam 28 and the preform 20.
The shadows of the grating lines will appear in the image plane u', v', with distortions due to the ray shafts m given by equation (19). The shadows assist in viewing the profile, as can be seen from Figure 14(a). If the parallel line grating 56 is replaced by a mesh (not illustrated) which is angled with respect to the axis A of the preform 20, the result would be as shown in Figure 14(b). If the parallel line grating plate 56 is put in an alternative position, shown dotted, between the lens 32 and the cylindrical lens 54, the image is as shown in Figure 14(c). The arrangement of Figure 13 is especially useful for observing the very small index differences typically found in the core of a single-mode optical fibre preform. The use of a colour banded plate instead of grating 56 gives essentially the same displays, but with coloured regions replacing the dark lines.
The modulation systems described with reference to Figures 4 to 14 have all relied on spatial modulation of the lens-transformed light. It is also possible to apply a temporal modulation and suitable apparatus is illustrated schematicaly in Figure 15. In the focal plane of the spherical lens 32 is a constant-speed rotary light chopper consisting of two blades having straight edges which are radial from the centre of rotation R, i.e. the mark-space ratio as a function of radius in constant. The centre is offset from the optical axis in a direction parallel to the u' axis. A reference photodiode 60 at a known angular position Ho around the blade periphery is connected to a time interval counter 62, and a detecting photodiode 64 is stepped along the u' axis by a control unit 66.
As the light chopper blades rotate at an angular speed p, the edge of each blade sweeps the focal plane in the w direction; for each value of w, the blade first allows illuminating the detector photodiode 64, then as the next blade edge passes, the illumination is cut off, so that the diode output is a series of square pulses.
The moment in time at which a light ray is cut on or off depends on its distance in the w direction, and hence on its refraction angle p from the endface of the preform 20. The reference diode 60 gives a reference or START signal to the counter from its known position who', and the diode 64 gives a STOP signal. The variations in time between these two signals detected by the counter 62 as the detector 64 is scanned along the u' axis gives a measure of the angle 0, and hence of the local refractive index. The counter output is fed to a computation unit 68 such as a computer and the scan control unit 66 supplies a position signal. The unit 68 applies the calculation given by equation (4), then provides a signal of appropriate form indicating the refractive index function.Note that since the deflection angle gi gives the index n(u, v) at any point u, v in the endface the photodetector can be scanned in any direction, or, for example, in a circle. Note also that either the preform or the photodiode can be moved.
Since the blades 58 describe an arc, and since angle 0 to be measured may be large, a tangent correction may be necessary by using: = = fRtan (pt - 6o) Usually the preform 20 in its bath of index-matching fluid will be supported on a scanning table driven by a stepper motor in the direction indicated by the arrows 70 i.e. the v direction. At each position of the preform, the detector 64 is scanned along the u' axis so that a series of signals is provided. A typical output is illustrated in Figure 16 for a graded-index preform.
The Figure 15 arrangement is the peferred form of apparatus used, because the output is most easily linked to computing means.
It is an advantage of any of the methods of determining refractive index profile described above that the profile is obtainable without a mathematical transformation, so that a profile is obtainable very rapidly. The optical arrangements are all simple, alignment is not critical, and the possibility of direct displays of profile, such as in Figures 7,9, 12 and 14 allows a rapid check of preform quality.
Some arrangements, such as Figues 4 to 15, allow high resolution - this is mainly determined by the size of the detector and the image magnification. As previously stated, large preforms and non-circular preforms can be measured.
While end-preparation is required, it can be rapid and no high accuracy is needed; the use of index-matching fluid allows direct use of diamond-sawn ends, although polishing may give slighly less noisy images.
The method depends on the assumption that the refractive index profile is substantially invariant along the axial section which is illuminated during test; usually a length equal to the preform diameter is illuminated.
The invention has been described with reference to a preform having a flat endface perpendicular to its axis A and with the incident beam coplanar with the axis A. If the incident beam and the axis are not coplanar, the angle is measured as the angle of deviation of the ray when projected into the plane containing the preform axis A and optic in the taxis 7.

Claims (14)

1. A method of measuring radial variations in the refractive index of an approximately cylindrical, translucent object having a substantially plane end face and a substantially invariant refractive index in a direction parallel to its axis, comprising illuminating the end face by means of a collimated beam of light incident at an angle to the cylindrical axis which differs substantially from 90 degrees and measuring at a plurality of radial positions the refractive angle at which light leaves the end face.
2. A method of measuring radial variations in refractive index as claimed in Claim 1 comprising illiiminating the endface with a broad light beam, focussing light emergent from the endface so that the distance from the axis of the focused beam is approximately proportional to the distance from the optical axis in direction coplanar with the endface of the object and optically modulating the focused light in dependence on said distance from the optical axis.
3. A method of measuring radial variations in refractive index as claimed in Claim 2 wherein the focused light is optically modulated temporily.
4. A method of measuring radial variations in refractive index as claimed in Claim 2 wherein the focused light is modulated spatially.
5. Apparatus for measuring radial variations in the refractive index of an aproximately cylindrical, translucent object having substantially plane endface and substantially invariant refracrive index in a direction parallel to its axis comprising an illumination source positioned to direct a collimated beam of light on the said enface at an angle to the axis of said object which differs substantially from 90 degrees, focussing means positioned to receive and focus said beam of light on emergence from said end face and sensing means to determine the angle of emergence of said light beam from said endface as a function of the position of emergence of said light beam.
6. Apparatus for measuring radial variations of refractive index as claimed in Claim 5 having modulating means positioned in the path of said light beam between said focussing means and said sensing means.
7. Apparatus as claimed in Claim 6 wherein said modulating means is adapted to modulate the intensity of said light beam as a function of the distance of said light beam from the optical axis of said focussing and measuring system.
8. Apparatus as claimed in Claim 7 wherein said modulating means comprises a filter having a graded attenuation.
9. Apparatus as claimed in Claim 7 wherein said modulating means comprises a shutter movable in a direction normal to said optical axis.
10. Apparatus as claimed in Claim 7 wherein said modulating means comprises a grating having alternate opaque and transparent regions orthogonal to said axis.
11. Apparatus as claimed in Claim 7 wherein said modulating means comprises a cylindrical lens.
12. Apparatus as claimed in Claim 6 wherein said modulating means is adapted to modulate temporily the intensity of said light beam.
13. Apparatus as claimed in Claim 11 wherein said modulating means comprises a shutter means rotatable about an axis parallel to the optical axis of said focussing and measuring means and positioned apart therefrom.
14. Apparatus for measuring radial variations in the refractive index of an approximately cylindrical, translucent object having a substantially plane endface and a substantially invariant refractive index in a direction parallel to its axis substantially as herein described with reference to Figures 2 to 15 of the accompanying drawings.
GB08307578A 1982-03-18 1983-03-18 Method of and apparatus for determining the radial refractive index profile of an optical specimen Expired GB2116708B (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990005904A1 (en) * 1988-11-15 1990-05-31 York Technology Limited Apparatus and method for measuring refractive index
EP0509848A2 (en) * 1991-04-19 1992-10-21 Kabushiki Kaisha TOPCON Measuring the cross-sectional distribution of the refractive index of an optical waveguide
US5365329A (en) * 1988-11-15 1994-11-15 York Technology Limited Apparatus and method for measuring refractive index
EP0733896A2 (en) * 1995-03-22 1996-09-25 SIP SOCIETA ITALIANA PER l'ESERCIZIO DELLE TELECOMUNICAZIONI P.A. Method of and device for determining the polymerisation profile of a polymeric layer

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990005904A1 (en) * 1988-11-15 1990-05-31 York Technology Limited Apparatus and method for measuring refractive index
US5365329A (en) * 1988-11-15 1994-11-15 York Technology Limited Apparatus and method for measuring refractive index
EP0509848A2 (en) * 1991-04-19 1992-10-21 Kabushiki Kaisha TOPCON Measuring the cross-sectional distribution of the refractive index of an optical waveguide
EP0509848A3 (en) * 1991-04-19 1993-07-28 Kabushiki Kaisha Topcon Measuring the cross-sectional distribution of the refractive index of an optical waveguide
EP0733896A2 (en) * 1995-03-22 1996-09-25 SIP SOCIETA ITALIANA PER l'ESERCIZIO DELLE TELECOMUNICAZIONI P.A. Method of and device for determining the polymerisation profile of a polymeric layer
EP0733896A3 (en) * 1995-03-22 1997-11-19 SIP SOCIETA ITALIANA PER l'ESERCIZIO DELLE TELECOMUNICAZIONI P.A. Method of and device for determining the polymerisation profile of a polymeric layer

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