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Claims  |
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What is claimed is:
1. Force measuring apparatus, comprising:
(a) a single-mode optical fiber (1) having inlet and outlet end portions,
and a curved intermediate portion contained solely in a given plane, the
curvature of said intermediate portion being such as to produce an
inherent well-defined controlled anisotropy extending along the length of
said intermediate portion, thereby to cause the resultant birefringence
produced by the lateral compression of said intermediate portion to have
the same orientation along the entire length thereof;
(b) force-responsive means for laterally compressing said curved optical
fiber intermediate portion, said force-responsive means including at least
two parallel spaced pressure plates (2,3) having planar adjacent surfaces
on opposite sides of, and in engagement with, said optical fiber curved
portion, respectively;
(c) laser means (4) for introducing coherent light into said optical fiber
inlet end portion, thereby to excite in said optical fiber, due to the
birefringence caused by the inherent optical anisotropy thereof, a pair of
linearly polarized light waves having orthogonally-arranged planes of
oscillation, said optical fiber being so arranged relative to said plates
that said planes of oscillation are parallel with and normal to said
adjacent faces of said pressure plates, respectively, whereby when a
compressive force to be measured (F) is applied in a direction normal to
said pressure plate adjacent faces, a phase shift is produced between said
light waves as a function of the degree of change in the stress-induced
birefringence; and
(d) means including interferometer means (5-8) for measuring the magnitude
of the applied force as a function of the phase shift between said light
waves.
2. Force measuring apparatus, comprising
(a) an anisotropic single-mode optical fiber (1) of well-defined anisotropy
having inlet and outlet ends;
(b) a stack of parallel spaced annular pressure plates (25-29), said
optical fiber having a helical configuration defining turns (21-24)
contained between, and in contiguous relation with, the adjacent faces of
successive pairs of said plates, respectively;
(c) laser means (4) for introducing coherent light into one end of said
optical fiber, thereby exciting in said optical fiber, due to
birefringence caused by the optical anisotropy, a pair of linearly
polarized light waves having orthogonal planes of oscillation, said
optical fiber turns being so arranged relative to said plates that said
planes of oscillation are parallel with and normal to the remote parallel
surfaces of said pressure plate stack, respectively, whereby when a
compressive force to be measured (F) is applied in a direction normal to
one of said remote surfaces, an additional phase shift is produced between
said light waves by stress-induced birefringence; and
(d) means including interferometer means (5-8) for measuring the magnitude
of the applied force as a function of the phase shift between said light
waves.
3. Force measuring apparatus, comprising:
(a) a single-mode optical fiber (1) having inlet and outlet end portions,
and an intermediate portion of non-circular cross-section such as to
produce an inherent well-defined controlled anisotropy extending along the
length of said intermediate portion, thereby to cause the resultant
birefringence produced by the lateral compression of said intermediate
portion to have the same orientation along the entire length thereof;
(b) force-responsive means for laterally compressing said optical fiber
intermediate portion, said force-responsive means including at least two
parallel spaced pressure plates (2,3) having planar adjacent surfaces on
opposite sides of, and in engagement with, said optical fiber intermediate
portion, respectively;
(c) laser means (4) for introducing coherent light into said optical fiber
inlet end portion, thereby exciting in said optical fiber, due to the
birefringence caused by the optical anisotropy, a pair of linearly
polarized light waves having orthogonal planes of oscillation, said
optical fiber being so arranged relative to said plates that said planes
of oscillation are parallel with and normal to the remote parallel
surfaces of pressure plates, respectively, whereby when a compressive
force to be measured (F) is applied in a direction normal to said pressure
plate adjacent faces, a phase shift is produced between said light waves
by the stress-induced birefingence; and
(d) means including interferometer means (5-8) for measuring the magnitude
of the applied force as a function of the phase shift between said light
waves.
4. Apparatus as defined in claim 3, wherein at least a portion of said
optical fiber intermediate portion between said pressure plates is curved
and contained in a given plane for lateral compression by said pressure
plates. |
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Claims  |
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Description  |
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BRIEF DESCRIPTON OF THE PRIOR ART
This invention relates to a method and apparatus for the measurement of
force by the use of stress-induced birefringence in a single-mode optical
fiber.
The measurement of force or pressure by means of stress-induced
birefringence in a single-mode optical fiber is well known in the prior
art. Likewise known are highly sensitive electro-optical methods for
detecting polarization changes resulting from birefringence ("Messung
mechanischer, thermischer und elecktrischer Groessen mit Lichtleitfasern",
by R. Ulrich, LABO, October, 1980, pages 1083-1093; "Birefringence and
Polarization Characteristics of Single-Mode Optical Fibers under Elastic
Deformations",: by J.-I. Sakai, T. Kimura, IEEE Journal of Quantum
Electronics, Vol. QE-17, No. 6, June 6, 1981, pages 1014-1051). Most uses
of fiber-optical pressure sensors, however, relate to acoustic measurement
and not to absolute static force measurement ("Optical Fiber Sensor
Technology", T. G. Giallorenzi et al, IEEE Journal of Quantum Electronics,
Vol. QE-18, No. 4, Apr. 1982, pages 626-664; "Acoustic Sensing with a
Single Coiled Monomode Fiber", by S. C. Rashleigh, Optics Letters, Vol. 5,
No. 9, September 1980, pages 392-394). Moreover, the previously described
measurement methods are not suitable for the achievement of high
measurement accuracy over a broad measurement range (i.e., with a
resolution>10.sup.4). Additional problems arise when the optical fiber is
inherently optically anisotropic, that is to say, it is birefringement
independent of its geometric shape or of the force acting upon it.
R. Ulrich, loc. cit., describes a force measurement instrument in which the
force to be measured acts in a vertical direction laterally upon a
straight single-mode optical fiber arranged between two pressure plates.
The stress generated in the optical fiber by the action of force thereon
produces an optical anisotropy causing the refractive index to be raised
in the horizontal direction and lowered in the vertical direction.
Polarized light is supplied to the optical fiber from a laser. As a result
of the anisotropically-produced birefringence, orthogonal polarization
states arise in the optical fiber in both horizontal and vertical
directions. The resultant polarization state is measured and indicated in
a polarimeter. It was also known elsewhere that one can achieve higher
sensitivity and measurement accuracy by the use of interferometric
measurement means.
Force measurement mechanisms of this kind normally require the use of an
inherently optically isotropic optical fiber. Commercially available
singel-mode optical fibers, however, do not meet this requirement, Owing
to manufacturing tolerances, they are more or less anisotropic, whereby
the orientation of the anisotropy along the optical fiber can vary and
differ from one specimen to the next. A uniform series of force
measurement instruments cannot be achieved on the basis of such undefined
optical conditions.
SUMMARY OF THE INVENTION
The present invention was developed to provide an improved force measuring
apparatus that is substantially independent of the inherent birefringence
properties of the optical fiber, and which provides a high degree of
measurement accuracy, together with the corresponding method.
According to a primary object of the invention, a force measuring apparatus
and method are provided including a single-mode anisotropic optical fiber
arranged for lateral compression between a pair of parallel pressure
plates, means supplying coherent light to one end of the optical fiber to
produce a pair of light waves contained in orthogonally arranged planes
that are parallel with and normal to the remote surfaces of the plates,
respectively, and interferometer means arranged at the other end of the
optical fiber for measuring the phase shift produced by the application of
force to be measured in a compressive direction normal to the remote
surface of one of the plates, thereby to provide an indication of the
magnitude of that force.
According to a more specific object of the invention, a single-mode optical
fiber is provided having an inherent anisotropy whose orientation
corresponds with the direction of force application. The inherent
anisotropy can be obtained through the curvature of the optical fiber
along its length. The resultant anisotropy by far exceeds the inherent
anisotropy of a commercially available, straight single-mode optical fiber
with round core cross-section, which substantially has no influence on the
measurement process. The measuring apparatus of the present invention is
characterized in that at least a portion of the optical fiber runs between
the pressure plates along a curved line, for example, in a round open
loop. The resultant birefringence has the same orientation along the
entire length of the optical fiber with necessarily corresponds with the
direction of force.
According to an alternate embodiment of the invention, the defined
anisotropy can also be generated during the manufacture of the optical
fiber. Of course, in arranging such a optical fiber with inherent
anisotropy in the measurement arrangement, the predetermined orientation
of the anisotropy of the optical fiber must be maintained over the entire
operating range of the force. This can be achieved by providing the
anisotropic optical fiber, during manufacture, with a cross-sectional
configuration that deviates from a circular configuration, for example, an
elliptical cross-sectional configuration, whose orientation agrees with
the optical anisotropy. Known methods for making a birefringence
single-mode optical fiber reside, for example, in the fact that the core
cross-section is given an elliptical configuration or that anisotropic
mechanical stresses are created inside the fiber, especially in the
light-conducting core. In these cases, moreover, the optical fiber
preferably extends along a curved line in the measurement arrangement. In
this way, under certain circumstances a higher difference in the
refraction coefficients can be achieved in both polarization directions.
According to a further object of the invention, the light supplied to the
optical fiber comprises linearly-polarized light having a plane of
oscillation inclined at an angle of 45.degree. with respect to the
direction of the force to be measured so that the orthogonal polarization
states will be excited with the same amplitude. For this purpose, a
correspondingly oriented polarizer is provided between the light source
and the input end of the fiber.
In operation, the degree of phase shift between the light waves travelling
in the two orthogonal polarization states by the application of the force
to be measured in a compressive direction on the plates between which the
optical fiber is arranged is a function of the magnitude of the force to
be measured. The pressure exerted upon the optical fiber (force per unit
of length) is decisive for the degree of phase shift and thus for the
level of measurement sensitivity. This pressure is limited by the
condition that the change in the configuration of the optical fiber, which
is brought about under its influence, must take place within the framework
of Hooke's Law. Under this assumption, the integrated effect along the
optical fiber is proportional to the force to be measured. The length of
the optical fiber arranged between two pressure plates depends--at a given
maximum pressure--only on the maximum force to be measured, that is to
say, it depends on the desired nominal load of the force measurement
arrangement.
According to another object of the invention, increased measurement
sensitivity can be achieved by providing the optical fiber with a helical
configuration to define a plurality of turns that are contained between
pairs of pressure plates, respectively. In this way, the phase shift
produced by the action of the force is multiplied in accordance with the
number of turns of the optical fiber.
The interferometer measuring means includes, in the simplest case, two
photo-electric detectors in front of which is arranged a linear polarizer
that is oriented an an angle of 45.degree. relative to the direction of
application of the force to be measured. Furthermore, optical phase
retardation elements can be provided which cause the electrical detector
signals to be respectively phase-shifted by a fixed amount (for example,
90.degree.); this facilitates the determination of the signal passages and
thus the control of an electronic interference period counter. For phase
measurement, an analog circuit or a microprocessor may be used. In this
way the phase difference can be accurately determined to less than
90.degree. over many interference periods. An improved arrangement with
four detectors permits a considerably more accurate interpolation also in
case of intensity and contrast changes.
BRIEF DESCRIPTION OF THE DRAWING
Other objects and advantages of the invention will become apparent from a
study of the following specification when viewed in the light of the
accompanying drawing, in which:
FIG. 1 is a diagrammatic illustration of a first embodiment of the
measuring apparatus of the present invention;
FIG. 2 is a top plan view of the pressure plate and optical fiber assembly
of FIG. 1;
FIG. 3 is a schematic diagram of a second embodiment of the detector means
of FIG. 1; and
FIG. 4 is a partly sectioned side elevation view of a second embodiment of
the invention wherein the turns of a helical optical fiber extend between
respective pairs of pressure plates arranged in a stack.
DETAILED DESCRIPTION
In the single-layer embodiment of FIGS. 1 and 2, the single-mode
anisotrophic optical fiber 1 has the form of a single circular loop which
is arranged between two parallel planar pressure plates 2 and 3. The force
to be measured F acts orthogonally upon the outer surface of pressure
plate 2 and is thus transmitted to pressure plate 3 solely via optical
fiber 1, whereby the force is imparted laterally upon that portion of the
optical fiber contained between the pressure plates. The optical fiber may
be formed of a suitable material having anisotropic properties, as is
known in the optical fiber art. Since the pressure plates 2 and 3 have no
optical function, they may be formed of either opaque or transparent
materials, such as steel or glass. A continuously operable semiconductor
laser 4 supplies into the optical fiber 1 coherent, linearly-polarized
light having an oscillation plane inclined at an angle of 45.degree.
relative to the direction of the force to be measured F. A linear
polarizer plate P may be provided between the light source and the input
end of the optical fiber, which polarizer has the aforementioned
45.degree. orientation relative to the direction of application of force
F. By virture of the curvature of optical fiber 1, a defined anisotropy is
effected in the optical fiber, thereby producing a birefringence which has
an identical orientation along the optical fiber 1. Specifically, the
birefringence generates two linearlypolarized waves with orthogonal
polarization directions one of which is parallel to the direction of the
measurement force F. Between the orthogonal waves there develops a phase
shift which depends on the degree of anisotropy or of birefringence and
which is determined by the magnitude of force F. During the transition
form an unloaded condition to a loaded condition of the measuring
apparatus, there thus arises a change in the phase shift between the two
waves which is a function of the force F that is to be measured. This
phase change is detemined by conventional interferometer means I.
It is known in the art to provide, for the interferometric determinaion of
a phase shift of two light waves, an optical-electronic interference
measuring means including an interference period counter and a phasemeter.
In the example at hand, two photoelectic detectors 5 and 6 are provided in
front of which there is arranged a linear polarizer 7 that is oriented at
an angle of 45.degree. to the direction of the measuring force F. The two
detectors pick up the light signal components coming from a semicircular
portion of the linear polarizer 7 and convert them into corresponding
electrical signals for the control of the interference period counter and
the phasemeter. Also arranged in front of detector 6 is a quarter-wave
plate 8 having the same orientation as the measuring force F, thereby
causing the two detector signals to be phase-shifted, respectively, by
90.degree.. Various electronic phase detector means for analyzing this
detector signal for the determination of the phase angle .phi. are in
themselves known and are not illustrated here.
To maintain a linear relationship between the phase change and the
measuring force, a commercially available single-mode optical fiber with a
diameter of, for example, 125.mu., can be stressed with about 20N/cm
transversely applied pressure. For a nominal value of the measurement
force F of 1,000N, for example, a optical fiber is required having a
length in the pressure range amounting to about 50 cm. One can show that,
with a comparatively simple interference measurement device, a measurement
accuracy of 0.1N in the range from 0 to 1,000N can be achieved.
The described measurement arrangement furthermore offers the advantage of
being simple in design, self-supporting, and stable.
Referring now to the embodiment of FIG. 3, an improved interference
measurement mechanism is illustrated which facilitates more accurate
interpolation of the measurement value within an interference period. Four
photoelectric detectors 9, 10, 11, and 12 are provided, each of which
scans a quadrant of the linear polarizer 7. Connected in front of the
detectors are partly optical delay elements which cause the four detector
signals to be phase-shifted by 90.degree., respectively. In the
illustrated embodiment, no delay element is arranged in front of the first
detector 9, while a quarter-wave plate 13 is arranged in front of the
second detector 10, a half-wave plate 14 is arranged in front of the third
detector 11, and the one-fourth-wave plate 13 and one-half-wave plate 14
are arranged in front of the fourth detector 12, the arrangements in each
case having the same orientation as the force F to be measured.
The differential values of the signals from the detectors 9, 11, and 10,
12, are formed in each case by differential electronic calculation means
15 and 16, respectively, while the quotient of both differential signals
is formed by quotient electronic calculation means 17. This quotient
represents the tangent of the phase angle .phi., and resultant electronic
calculation means 18 determines from this tangent the phase angle .phi..
The designs of the various electronic calculation means for the
above-mentioned purpose are well known in the art and are therefore not
described in greater detail here.
Referring now to the multi-turn embodiment of FIG. 4, the optical fiber 20
is made in the form of a helix, and in this example the optical fiber
includes four turns 21-24 which are arranged between respective pairs of a
stack of annular pressure plates 25-29. Oblique slits 30 in the pressure
plates facilitate the transition of the optical fiber 20 from one winding
plane to the other. Pressure plates 25-29 are arranged between two
terminal plates 31 and 32, whereby on the lower terminal plate 31 there is
provided a vertical rod 33 for the guidance of the annular pressure
plates, the measuring force F acting upon the upper terminal plate 32.
Each of the individual turns 21-24 of the optical fiber 20 is under the
action of the entire measuring force F and is correspondingly dimensioned
according to the same criteria as the simple optical fiber loop in the
single-layer measurement arrangement according to FIGS. 1 and 2. By virtue
of the multiple (in this example, four-fold) action of the full
measurement force F upon optical fiber 20, the phase change, generated by
the way in which the birefringenece is influenced in terms of force, is
quadrupled. In this way, the measurement sensitivity can be increased
significantly if the optical fiber has the corresponding number of
windings.
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Description  |
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