OPTICAL FIBER SENSOR

Abstract: An optical fiber sensor for detecting a change of an external subject (50, 88, 90), based on measuring and reference beams. The sensor includes an optical fiber (24) or fibers (328, 334) for optically coupling a light transmitter/receiving portion (100, 100′, 100″) and a sensor head portion (102, 102′, 102″). Where the measuring and reference beams are transmitted through the single optical fiber (24) to the sensor head portion (100) in respective two transmission modes having mutually perpendicular polarization planes, the sensor head portion may include a Faraday effect element (44) for rotating the polarization planes of the measuring and reference beams, in order to switch the two transmission modes when the beams are returned through the fiber to the transmitter/receiver portion. Where the measuring and reference beams are transmitted to the sensor head portion by the respective first and second fibers (238, 334), the sensor head portion (100″) may employ a device (354, 360) for directing the two beams so that the measuring and reference beams are returned to the transmitter/receiver portion (100″) through the second and first fibers.

Description: The present invention relates to an optical fiber sensor which includes a light transmitter/receiver portion, an optical sensor head remote from the transmitter/receiver portion, and an optical fiber optically coupling the transmitter/receiver portion and the sensor head. As a method of measuring a physical quantity, it is proposed to use an optical fiber sensor which includes: a light transmitter/receiver portion having a light source for producing a reference beam of light and a measuring beam of light, and a photosensor which receives the reference beam, and the measuring beam influenced by a subject, for determining the physical quantity associated with the subject; an optical sensor head which changes a transmission parameter of the measuring beam in relation to the external conditions; and an optical fiber for transmitting the reference and measuring beams between the light transmitter/receiver portion and the optical sensor head. An example of an optical fiber sensor of an optical homodyning type is shown in Fig. 13, wherein a light beam 122 which is generated by a light source 120 is polarized in the "y" direction. The light beam 122 passes a polarizing beam splitter 124, which transmits the y-polarized beam 122 and reflects an x-polarized beam. The y-polarized beam 122 is then focused by a converging lens 126, on the end face of an optical fiber 128. This optical fiber 128 is capable of transmitting a polarized light beam while maintaining the same plane of polarization. Namely, the polarization plane of the beam 122 is not changed while it is transmitted through the optical fiber 128. This type of optical fiber is hereinafter referred to as "fixed-polarization-plane optical fiber". The optical fiber 128 is adapted to transmit the incident beam 122 to the sensor head in one of two transmission modes HE₁₁ x and HE₁₁ y whose planes of polarization are perpendicular to each other, for example HE₁₁ y . In this example, the optical sensor head is constituted by a pressure-sensitive, fixed-polarization-plane optical fiber 132 wherein a light beam being transmitted therethrough is phase-modulated according to a variation in the sound pressure. This pressure-sensitive optical fiber 132 is optically coupled to the transmission optical fiber 128 such that the two fibers 128, 134 are rotated about the optical axes by 45 degrees relative to each other. That is, there exists a polarization plane deviation of 45 o between the two fibers 128, 132. Therefore, the incoming light beam transmitted through the optical fiber 128 in one of the two transmission modes is transmitted through the pressure-sensitive optical fiber 132 in the two transmission modes. These two modes are reflected by a reflector film 134 on the end face of the optical fiber 132, and each of the reflected two modes is distributed as the two transmission modes HE₁₁ x , HE₁₁ y of the transmission optical fiber 128, when the reflected two modes are incident upon the optical fiber 128. Consequently, the reflected two modes transmitted through the pressure-sensitive optical fiber 132 combine and interfere with each other. In this instance, therefore, the optical fiber 132 functions as a polarizer. Although either one of the two transmission modes HE₁₁ x , HE₁₁ y from the optical fiber 128 may be received by the polarizing beam splitter 124, the mode HE₁₁ x is utilized in this specific example of Fig. 13, as an optical signal from the beam splitter 124, so that the optical signal is converted into a corresponding electric signal by a photosensor 136. This electric output of the photosensor 136 represents a change in a selected transmission parameter of the measuring beam, for example, a change in the phase of the beam which is caused by the sound pressure to which the optical fiber 132 is exposed. In the optical homodyning type of optical fiber sensor discussed above, an automatic adjustment of the initial optical phase of the sensor is necessary in order to provide the sensor with maximum detecting or sensing accuracy. To this end, a mechanical stress is applied to the pressure-sensitive optical fiber 132, so as to establish an initial phase difference or angle of π/2 between the two modes HE₁₁ x and HE₁₁ y , in the example of Fig. 13. For instance, this stressing of the optical fiber 132 may be achieved by providing the fiber 132 with a piezoelectric element. In this case, however, the piezoelectric element increases the size of the optical fiber 132, and requires means for applying electric power thereto. Alternatively, the initial phase difference of π/2 may be established by controlling the wavelength of the beam produced by the light source. However, this alternative method is comparatively technically difficult to practice. An optical fiber sensor of an optical heterodyning type is illustrated in Fig. 14, wherein a light source 140 such as a horizontal He-Ne Zeeman laser is adapted to produce two polarized beams whose polarization planes are perpendicular to each other, i.e., a measuring beam having a frequency f1 and a reference beam having a frequency f2 which is slightly different from the frequency f1. These beams are transmitted through a fixed-polarization-plane optical fiber 142, and incident upon a beam splitter 144, so that a part of the incident beams is transmitted through the beam splitter 144 while the other part of the beams is reflected by the beam splitter 144. The reflected beams are received by a photosensor 150 through a polarizing plate 146 and a reception optical fiber 148. The photosensor 150 is adapted to detect a reference beam beat frequency f2 - f1. Of the two beams which are transmitted through the beam splitter 144, the beam having the frequency f2 is reflected by a polarizing beam splitter 152, passed through a 1/4 wave plate 154, reflected by a mirror 156 and again passed through the 1/4 wave plate, whereby the plane of polarization of the beam is rotated so that the beam is transmitted through the polarizing beam splitter 152 and is received by a photosensor 158 through a polarizing plate 157 and a reception optical fiber 164. The other beam having the frequency f1 which is transmitted through the beam splitter 144 is passed through the polarizing beam splitter 152 and a 1/4 wave plate 160 and reflected by a surface of a subject 162. The reflected beam is again passed through the 1/4 wave plate 160, with the polarization plane being rotated. The beam is then reflected by the polarizing beam splitter 152 and received by the photosensor 158 through the polarizing plate 157 and optical fiber 164. The beam received by the photosensor 158 has a frequency f1±Δf1. This frequency shift is caused by a displacement of the subject 162. Thus, the photosensor 158 receives the beam having the frequency f2 which has not been influenced by the subject 162, and the beam having the frequency f1±Δf1 which has been influenced by the subject 162. The photosensor 158 is adapted to detect a measuring beam beat frequency f2 - f1 ± Δ f1. Outputs of the photosensors 150 and 158 are applied to a phase difference detecting circuit 166, so that a phase difference Δf1 between the reference and measuring beam beat frequencies is detected. This phase difference represents information carried by the received reference and measuring beams, that is, an amount of displacement of the subject 162. Unlike the optical fibre sensor of the optical homodyning, the optical fibre sensor of the optical heterodyning does not require automatic adjustment of the phase. However, the divided parts of each of the reference and measuring beams having the respective beat frequencies are transmitted from the optical sensor head to the photosensors 150, 158 through the two different optical fibres 148, 164. Patent Abstracts of Japan Volume 11, No 22 discloses a measuring system in which a probe beam and a reference beam are propagated from a source along an optical fibre to the point where the measurement is to be taken and then returned along the optical fibre to a detector. The sensor head comprises a converging lens, a polarising beam splitter, a reference mirror and a mirror mounted on the object to be detected. GB-A-2,144,215 discloses an interferometric detector with a fibre optic sensor in which the measuring and reference beams are transmitted from the source to the sensor along a fibre optic cable. At the sensor they are separated by a splitter of undefined form and returned along the fibre optic cable to a detector adjacent the source. WO 87/01438 discloses a common optical path interferometric gauge in which a beam is split into two and recombined after an optical path length greater than the coherence length of the source has been introduced to one part. The combined beam is propagated along an optical fibre to a sensor head where it is split into reference and measurement beams. The measurement beam is reflected off a moving surface and the beams are recombined after a further path difference to re-establish coherence has been added. The present invention was developed in the light of the drawbacks encountered in the prior art as described above. It is therefore an object of the present invention to provide a comparatively small-sized, inexpensive optical fibre sensor which uses an optical fibre or fibres for optically coupling a light transmitter/receiver portion and a sensor head portion for transmitting a reference beam and a measuring beam therebetween, and which is capable of highly accurately detecting a change in a transmission parameter of the measuring beam influenced at the sensor head portion, based on the reference and measuring beams received at the transmitter/receiver portion. According to the present invention, there is provided an optical fiber sensor for detecting a change in a transmission parameter of a measuring beam, based on the measuring beam and a reference beam, comprising: a single optical fiber capable of transmitting a light beam in two transmission modes having mutually perpendicular polarization planes, such that the polarization planes of said two transmission modes are maintained; a light transmitter/receiver portion for generating said light beam for producing said measuring and reference beams and directing said light beam to said optical fiber so that said light beam is transmitted through said optical fiber in one of said two transmission modes in a first direction from a proximal end of the optical fiber to a distal end thereof, said light transmitter/receiver portion being operable to detect said change in said transmission parameter of said measuring beam, based on said measuring and reference beams which have been returned through said optical fiber in said two transmission modes in a second direction from said distal end toward said proximal end, and a sensor head portion operable to receive said light beam transmitted through said optical fiber in said first direction, and splitting said light beam into said measuring and reference beams, said sensor head portion causing said transmission parameter of at least said measuring beam to be influenced by a change of an external subject, and returning said measuring and reference beams to said light transmitter/receiver portion through said optical fiber in said second direction; characterised in that: said sensor head portion includes adjusting means for adjusting said measuring and reference beams prior to incidence upon said distal end of said optical fiber, so that the measuring and reference beams are returned through said optical fiber in said second direction in said two transmission modes, as two linearly polarized beams having mutually perpendicular polarization planes and a phase difference of 90 o . In the optical fiber sensor constructed as described above, the light beam generated by the light transmitter/receiver portion to produce the measuring and reference beams is transmitted through the optical fiber in the first direction in one of the two transmission modes. The measuring and reference beams obtained at the sensor head portion by splitting the light beam transmitted through the optical fiber in the first direction are adjusted by the adjusting means, as two linearly polarized beams having mutually perpendicular polarization planes and a phase difference of 90 o , so that the measuring and reference beams are returned through said optical fiber in said second direction in the respective two transmission modes. Consequently, both the measuring beam and the reference beam returned through the optical fiber in the second direction experience the same influence of the parameters of the optical fiber such as temperature, vibration and strain. In other words, the influence of the optical fiber on the measuring beam is counterbalanced by the influence of the same on the reference beam. Accordingly, a change in the transmission parameter of the measuring beam, which is given to the measuring beam at the sensor head portion due to a change of the external subject can be accurately detected by the instant optical fiber sensor, based on the measuring and reference beams which have been returned from the sensor head portion to the light transmitter/receiver portion and which have the phase difference of 90 o . The use of the single optical fiber optically connecting the transmitter/receiver portion and the sensor head portion results in reduction in size and cost of the optical fiber sensor as a whole. The above and optional objects, features and advantages of the present invention will be better understood by reading the following detailed description of presently preferred embodiments of the invention, when considered in connection with the accompanying drawings, in which: Fig. 1 is a schematic perspective view depicting an embodiment of the present invention; Figs. 2, 3, 4 and 5 are views explaining the operation of the sensor of Fig. 2; Figs. 6, 7 and 8 are views explaining applications of the optical fibre sensor of Fig. 1, showing measurement of straightness, displacement and length, respectively; Figs. 9, 10, 11 and 12 are views showing optical sensing heads of embodiments of the invention, respectively; Figs. 13 and 14 are views illustrating conventional optical fibre sensors. Referring to Fig. 1, there is illustrated an embodiment of the invention in the form of an optical fiber sensor of the optical homodyning type. In Fig. 1, a monochrome laser beam produced by a laser source 210 such as a He-Ne laser is passed through a polarizing beam splitter 212 rotated 45 o about the optical axis, a Faraday effect element 214 and a polarizing beam splitter 216, and is converged by a converging lens 218 on the end face of a fixed-polarization plane optical fiber 220. The polarizing beam splitter 212, Faraday effect element 214,and polarizing beam splitter 216 serve as an optical isolator for protecting the laser source 210 from the reflected beams. The polarizing beam splitter 216 also functions to split the incident beam into two components whose polarization planes are perpendicular to each other. The light beam reflected by the beam splitter 216 is received by a first photosensor 224 via a converging lens 222. The light beam which is once transmitted through the beam splitter 216 in one direction toward the optical fiber 220 is returned as the reflected beam through the beam splitter 216 in the opposite direction, and incident upon the Faraday effect element 214 whereby the polarization plane of the reflected beam is rotated by 45 o about the optical axis. Therefore, a component of the reflected beam is reflected by the polarizing beam splitter 212 and received by a second photosensor 228 via a converging lens 226. In the present embodiment, the elements (except the optical fiber 220) which have been described constitute light transmitter/receiver portion 100 of the optical fiber sensor. One end of the optical fiber 220 is fixed to a housing of the transmitter/receiver portion 100. The fixed-polarization-plane optical fiber 220 consists of a core 230, a pair of stressing portions 232, 232 sandwiching the core 230, and a clad 234 which covers the core and stressing portions 230, 232. The optical fiber 220 is capable of transmitting a polarized beam such that the polarization planes of the two modes HE₁₁ x and HE₁₁ y that are perpendicular to each other are maintained. Since the linearly polarized beam which has been transmitted through the beam splitter 216 is incident upon the proximal end face of the optical fiber 220, the incident beam is transmitted through the optical fiber 220, as one of the two transmission modes HE₁₁ x , HE₁₁ y . The distal end of the optical fiber 220 is attached to a frame of an optical sensor head portion 102. The linearly polarized beam transmitted through the optical fiber 220 as one of the two modes HE₁₁ x and HE₁₁ y is emitted from the distal end face of the fiber 220, and converted into parallel rays. The parallel rays are splitted by a non-polarizing beam splitter 238 into a reference beam and a measuring beam. The measuring beam transmitted through the non-polarizing beam splitter 238 is transmitted through a 1/4 wave plate 240. This 1/4 wave plate 240 is capable of rotating the polarization plane of a linearly polarized beam by 45 o after the beam is transmitted through the plate 240 two times in the opposite directions. The measuring beam transmitted through the 1/4 wave plate 240 falls upon one of the first and second corner cube prisms 52, 54 on the subject 50, in this case, upon the second prism 54. The reference beam reflected by the non-polarizing beam splitter 238 is transmitted through a 1/8 wave plate 248 and reflected by a mirror 250 toward the other of the first and second prisms 52, 54, in this case, toward the first prism 52, in parallel to the direction of propagation of the measuring beam from the beam splitter 238 to the second prism 54. The 1/8 wave plate 248 is capable of converting a linearly polarized light beam into a circularly polarized light beam after the linearly polarized beam is transmitted two times in the opposite directions. The first and second corner cube prisms 52, 54 are coated with a metallic layer, so that the polarization characteristics of the beams reflected by the prisms 52, 54 are not changed. In the embodiment of Fig. 1, the non-polarizing beam splitter 238 and mirror 250 constitute a major part of the sensor head portion 102, and the 1/4 wave plate 240 and 1/8 wave plate 248 constitute means provided at the sensor head portion 102, for adjusting the polarization planes and phases of the reference and measuring beams so that these beams are transmitted through the optical fiber 220 back toward the transmitter/receiver portion 101, as the two transmission modes whose phases are shifted from each other by 90 o and whose polarization planes are perpendicular to each other. An operation of the instant optical fiber sensor of Fig. 1 will be described by reference to Figs. 2 through 5. As shown in Fig. 2, the linearly polarized laser beam emitted from the laser source 210 is passed through the polarizing beam splitter 212. A short arrow in Fig. 29 that extends perpendicularly to the direction of propagation of the laser beam indicates the plane of polarization of the laser beam. The linearly polarized laser beam is then passed through the Faraday effect element 214, whereby the polarization plane of the beam is rotated 45 o in the clockwise direction. The linearly polarized beam is transmitted through the polarizing beam splitter 216, and converged by the converging lens 218 so that the converged beam enters the core 230 of the optical fiber 220. The incident linearly polarized beam is transmitted through the optical fiber 220 as one of the two transmission modes HE₁₁ x , HE₁₁ y . As shown in detail in Fig. 3, the laser beam emitted from the distal end of the optical fiber 220 is converted into parallel rays by the converging lens 236, and is split by the non-polarizing beam splitter 238 into two parts. This beam splitter 238 is required to divide the incident beam into two parts which not only have equal amounts of optical energy but also exhibit properties of a linearly polarized beam. Commercially available non-polarizing beam splitters generally satisfy these requirements. In the instant embodiment, the linearly polarized beam transmitted through the beam splitter 238 is used as a measuring beam denoted by reference characters 1e, while the linearly polarized beam reflected by the beam splitter 238 is used as a reference beam denoted by reference numeral 1c. The measuring beam 1e is elliptically polarized by the 1/4 wave plate 240 whose crystal axis is inclined 22.5 o with respect to the direction of polarization. The elliptically polarized measuring beam 1e is directed to the second corner cube prism 54. The reference beam 1c is elliptically polarized by the 1/8 wave plate 248, and reflected by the mirror 250 toward the first corner cube prism 52. As shown in Fig. 4, the elliptically polarized measuring beam 1e reflected by the second corner cube prism 54 is again transmitted through the 1/4 wave plate 240 and is thus linearly polarized. The polarization plane of this linearly polarized beam is inclined 45 o with respect to that of the linearly polarized beam prior to the transmission through the 1/4 wave plate 240 in the direction toward the prism 54. The elliptically polarized reference beam 1c reflected by the first corner cube prism 52 is circularly polarized as a result of transmission through the 1/8 wave plate 248. The above conversion of the circularly polarized measuring and reference beams into the linearly polarized beams is effected, since the axes of the 1/4 wave plate 240 and 1/8 wave plate 248 are inclined 22.5 o and 45 o , with respect to the polarization planes of the measuring and reference beams 1e, 1c during transmission in the direction toward the prisms 54, 52, respectively. The linearly polarized measuring and reference beams from the wave plates 240, 248 are combined with each other at the beam splitter 238, into mutually interfering beams 1a, 1b whose polarization planes are perpendicular to each other and whose phases are shifted by 90 o from each other, as indicated in Fig. 4. These interfering beams 1a, 1b are transmitted through the optical fiber 220 as the two modes HE₁₁ x and HE₁₁ y , toward the transmitter/receiver portion 100. The beams 1a, 1b emitted from the proximal end of the optical fiber 220 are converted by the converging lens 218 into parallel rays, and separated from each other by the polarizing beam splitter 216. The linearly polarized beam 1b of the interfering beams 1a, 1b transmitted through the optical fiber 220 is reflected by the beam splitter 216 and is received by the first photosensor 224, which produces a corresponding electric signal. The linearly polarized beam 1a is transmitted through the beam splitter 216, transmitted through the Faraday effect element 214 and polarizing beam splitter 212, and received by the second photosensor 228, which produces a corresponding electric signal. Since the linearly polarized beams 1a, 1b have a phase difference of 90 o as indicated above, the electric signals produced by the first and second photosensors 224, 228 as sine and cosine waves which are counted at 90 o intervals by a pulse counter provided in a phase difference detecting circuit 260. If the subject 50 is rotated in a plane parallel to the planes which include the beams incident upon or reflected by the first and second prisms 52, 54, the rotating angle of the subject 50 may be accurately detected as a change in the phase difference which is represented by the count of the pulse counter. When the two prisms 52, 54 are provided on each of two spaced-apart subjects 50, 50 placed on the surface plate 58, as shown in Fig. 6, the straightness of the surface of the surface plate 58 may be accurately represented by the output of the detecting circuit 260. When the first prism 52 is secured on the sensor head portion 102' while the second prism 54 is secured on the movable table 60, as indicated in Fig. 7, the amount of a displacement of the movable table 60 relative to the sensor head portion 102' can be detected by the detecting circuit 260. When the second prism 54 is fixed to a movable member of a contact type measuring device such as a slide caliper or micrometer, as indicated in Fig. 8, lengths of desired subjects may be accurately detected by the detecting circuit 260. In the present embodiment, the linearly polarized beam for producing the reference and measuring beams is transmitted through the optical fiber 220 toward the sensor head portion 102 as one of the two transmission modes, and the reference and measuring beams 1e, 1c are transmitted backward through the optical fiber 220 as the two transmission modes whose polarization planes are perpendicular to each other. Consequently, the instant embodiment eliminates an influence of temperature, strain, vibration and other external factors associated with the optical fiber 220, on a change in the transmission parameter, i.e., on a change in the phase difference between the reference and measuring beams. That is, the detected change in the phase difference represents only the amount of relative displacement of the first and second prisms 52, 54. Thus, the rotating angle of the subject 50, the straightness of the surface plate 58 and the distance of movement of the movable table 60 can be measured with high accuracy. Where a He-Ne laser is used as the laser source 210 and the counting of the pulse counter is effected at 90 o intervals, the instant sensor provides detecting resolution of 0.1 micron. Further, since the transmitter/receiver portion 100' and the sensor head portion 102 are optically coupled by the single optical fiber 220, the sensor may be designed compact and small-sized. In addition, the measuring accuracy and reliability are not influenced or deteriorated by air streams surrounding the optical path. The above embodiment of Fig. 1 may be modified as needed. In the embodiment of Fig. 1, the sensor head portion 102 is adapted to irradiate the first and second corner cube prisms 52, 54 fixed on the subject 50. While the 1/4 wave plate 240 and the 1/8 wave plate 248 function as means for changing the phases and polarization planes of the reference and measuring beams, these wave plates may be replaced by other optical components capable of changing the phases of the beams. The present optical fiber sensor may be used to detect the straightness of a surface plate 58, by using a movable subject 50 having the first and second corner cube prisms 52, 54. In this case, the subject 50 is moved from left side to right side of Fig. 6, while the reference and measuring beams 1a, 1b are incident upon and reflected by the prisms 52, 54. In this case, the output of the phase difference detecting circuit 56 represents a phase difference indicative of the out-of-straightness of the surface of the surface plate 58. The instant optical fiber sensor may be modified to detect an amount of linear movement of a subject. For instance, if the first corner cube prism 52 is secured on the sensor head portion 102 while the second corner cube prism 54 is fixed on a surface of a movable table 60, as indicated in Fig. 7, the amount of linear displacement of the table 60 can be accurately detected based on an amount of change in the phase difference represented by the output signal of the phase difference detecting circuit 56. Further, the distance between the sensor head portion 102 and the second corner cube prism 54 on the table 60 can be measured by providing the transmitter/receiver portion 100 with a directly-modulatable semi-conductor laser, and measuring the frequency of interference fringes formed by triangular-wave modulation of the laser beam produced by the semi-conductor laser. If the second corner cube prism 54 is fixed on a movable member of a length measuring device of the contact type such as a slide caliper or micrometer, as illustrated in Fig. 8, lengths can be measured based on the phase difference detected by the detecting circuit 56. While the polarizing beam splitter 12, Faraday effect element 14 and polarizing beam splitter 16 function as an optical isolator as described above, the polarizing beam splitter 12 and the Faraday effect element 14 may be eliminated if the light source 10 employs a light-emitting diode (LED) or a super-luminescent diode (SLD) which is less likely to be influenced by a reflected light beam. Where a He-Ne laser is used together with a ultrasonic modulator whose frequency is 2 GHz, the optical isolator indicated above may be eliminated, since the frequency of the reflected beam falls outside the gain band of the He-Ne laser. When a semi-conductor laser or other directly modulatable light source is used, the optical isolator may be eliminated by switching off the light source while the reflected beam is incident upon the light source, by utilizing a propagation time delay of the optical fiber 24. In the arrangement of Fig. 9, the reference and measuring beams as the two different transmission modes emitted from the optical fiber 24 are converted into parallel rays of light by the converging lens 42, and the polarization planes of the beams are rotated by the Faraday effect element 44 by 45 o . Then, the reference and measuring beams are separated from each other by the polarizing beam splitter 46, so that the reference beam is incident upon the first corner cube prism 52 secured on the sensor head portion 102, while the measuring beam is converged on a surface of the subject 50. Since the phase difference between the reference and measuring beams is changed depending upon the surface roughness of the subject 50, the surface roughtness can be measured based on the detected change in the phase difference. In the arrangement of Fig. 10, the subject 50 of Fig. 9 is replaced by a stream of fluid 88. Namely, the velocity of a flow of the fluid 88 is measured based on the fact that the phase difference between the measuring and reference beams is changed in relation to the velocity of the fluid flow. In the arrangement of Fig. 11, the reference and measuring beams are propagated through a subject 90 whose refractive index is changed. In the arrangement of Fig. 12, the reference beam is reflected by the first corner cube prism 52, while the measuring beam is transmitted through the subject 90 and is reflected by the second corner cube prism 54 so that the reflected measuring beam is returned through the subject 90. That is, only the measuring beam is transmitted throught the subject 90 in the opposite directions. In these two arrangements, the phase difference of the measuring beam with respect to the reference beam is changed in relation to the refractive index of the subject 90, whereby a change in the refractive index of the subject 90 may be measured. These arrangements may be utilized for measuring various parameters of desired subjects, other than the refractive index. If the subject 90 consists of a Pockel cell or Pockels effect crystal such as LiNbO₃ or LiTaO₃ capable of changing the refractive index in relation to an electric field or voltage applied thereto, the electric field strength or voltage may be measured. If the subject 90 consists of a substance such as LiNbO₃ whose index of double refractive is changed with temperature, the temperature of the subject 90 may be measured. If the subject 90 consists of a substance such as Pyrex glass or quartz glass which exhibits a photoelastic effect, the pressure, vibration or acceleration of the subject may be measured. If the subject 90 consists of a transparent container containing a gas, the concentration of the gas may be measured. In this case, the beam incident upon the subject 90 does not undergo double refraction, and therefore the sensor head portion 102 shown in Fig. 12 may be suitably employed.

Claims: An optical fiber sensor for detecting a change in a transmission parameter of a measuring beam, based on the measuring beam and a reference beam, comprising: a single optical fiber (220) capable of transmitting a light beam in two transmission modes having mutually perpendicular polarization planes, such that the polarization planes of said two transmission modes are maintained; a light transmitter/receiver portion (100) for generating said light beam for producing said measuring and reference beams and directing said light beam to said optical fiber (220) so that said light beam is transmitted through said optical fiber in one of said two transmission modes in a first direction from a proximal end of the optical fiber to a distal end thereof, said light transmitter/receiver portion being operable to detect said change in said transmission parameter of said measuring beam, based on said measuring and reference beams which have been returned through said optical fiber in said two transmission modes in a second direction from said distal end toward said proximal end; and a sensor head portion (102) operable to receive said light beam transmitted through said optical fiber in said first direction, and splitting said light beam into said measuring and reference beams, said sensor head portion causing said transmission parameter of at least said measuring beam to be influenced by a change of an external subject (50, 88, 90), and returning said measuring and reference beams to said light transmitter/receiver portion through said optical fiber in said second direction; characterised in that: said sensor head portion (102') includes polarisation and phase adjusting means (240, 248) for adjusting the polarisation and phases of said measuring and reference beams prior to incidence upon said distal end of said optical fiber, so that the measuring and reference beams are returned through said optical fiber in said second direction in said two transmission modes, as two linearly polarized beams having mutually perpendicular polarization planes and a phase difference of 90 o . An optical fiber sensor according to claim 1, wherein said light transmitter/receiver portion (100') includes a laser source (210) for producing a linearly polarized laser beam, a pair of photosensors (224, 228) for receiving said measuring and reference beams which have been returned through said optical fiber in said second direction in said two transmission modes, and a detecting circuit (260) receiving outputs of said pair of photosensors and producing an output indicative of a phase difference between the returned measuring and reference beams. An optical fibre sensor according to claim 1 or 2, wherein said adjusting means (240, 248) includes a 1/4 wave plate (240) which transmits one of said measuring and reference beams therethrough, and 1/8 wave plate (248) which transmits the other of said measuring and reference beams therethrough.

Inventors: KONDO, MICHIO BROTHER KOGYO K.K.
Applicants: BROTHER KOGYO KABUSHIKI KAISHA
Application year: 1988
Main classification: G01B9
IPC codes: G01D5