JPH11248848A - Seismometer - Google Patents

Abstract

PROBLEM TO BE SOLVED: To improve detection sensitivity and exert a servo function by layering force sensors which has an optical fiber roll reacting to a pressure change set at a rigid plate. SOLUTION: Force sensors 5-12 in each of which a cylindrical optical fiber roll reacting keenly to a pressure change is set at a rigid plate are layered at gaps of a hollow square pillar-like load body 1 and a cylindrical body 2, and the cylindrical body 2 and a solid load body 3 confronting to each other. A phase shift light obtained by adding and averaging output lights of the optical fiber rolls is output. An elastic function of the optical fiber rolls exerts a servo function of stopping a displacement of the load bodies 2, 3 and the rigid plate at a position where a pressuring force due to the displacement of the load bodies 2, 3 and the rigid plate balances.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a force sensor comprising a rigid plate having optical fiber rolls whose light propagation characteristics change in response to a pressure change in a gap between load bodies which are relatively displaced. The present invention relates to a seismometer for detecting acceleration in two horizontal components and acceleration in a vertical direction.

[0002]

2. Description of the Related Art In an electromagnetic accelerometer, an electromagnet is arranged around a pendulum, a coil is wound around the pendulum, and an acceleration component of ground motion obtained from the pendulum is detected as an electric signal.
A servo-type accelerometer that detects the acceleration by feeding the balance current proportional to the displacement of the pendulum position back to the pendulum coil and holding the pendulum near the position during groundless motion is used. In the observation system using the instrument, the pendulum of the seismometer is locked during equipment transportation and installation work to protect the observation sensor from impact etc., and in the observation state, the sensor control mechanism used to make the pendulum free On the other hand, since a control command signal is transmitted from the land, a sensor control mechanism including an optical / electrical converter and a motor is required.

[0003] In order to solve such a problem, Japanese Patent Application No. 9-60153 filed by the present applicant includes the following:
As an example, a seismometer having the following configuration is disclosed. This will be described with reference to FIGS. 17A and 17B. Each of the six faces 101 of the square pillar-shaped load body 100 disposed at the center inside the frame 105 formed in a cubic shape has: For example, a total of four optical fiber rolls 102 each having a meandering (or loop) optical fiber winding 103 are opposed to each other, and a pressure plate 104 is disposed on the back of the optical fiber roll 102. I do. Bolt 1 planted at the center of the back of this pressure plate 104
06 is passed through each surface of the frame 105, and a spiral spring 108 functioning as an apparent servo circuit is interposed between the nut 107 and the frame 105,
By adjusting the degree of screwing of the nut 107, a pressing force S is generated, and an appropriate pressing bias is applied to the optical fiber roll 102. With such a configuration, the load 10
0 itself has 6 optical fiber rolls 102 interposed therebetween.
Since the pressure is held by each of the pressure plates 104, when an impact is applied, the spring
08 and are displaced in the east-west north-south direction and the up-down direction.

With this configuration, the east-west north-south (XY) direction,
Alternatively, when the acceleration is applied from the vertical direction, the load body 100 displaced in the east-west north-south direction or the vertical direction.
Thus, a load is applied to the optical fiber roll 102 to which the bias pressure has been applied, and the acceleration is detected from a change in the light propagation characteristics of the optical fiber roll 102 due to the load.

[0005]

However, in the present invention using an optical fiber roll, the optical fiber rolls are arranged one by one in the east-west north-south direction and in the vertical direction, and the output signals thereof are detected and processed. If the detection sensitivity of the optical fiber roll is inferior, the output signal is low and the detection sensitivity is poor. In addition, a detection error is generated, and arithmetic processing is performed based on the error. Therefore, there is a problem that measurement accuracy is low. Further, there is a problem that a member including a pressing plate, a helical spring, and a nut is required as a servo function member for applying an appropriate pressing bias to the optical fiber roll 102.

SUMMARY OF THE INVENTION The present invention solves the above-mentioned problems, and stacks a force sensor in which an optical fiber roll whose light propagation characteristic is sensitive to a pressure change is provided on a rigid plate in an opposing gap of a load body that is relatively displaced. It is an object of the present invention to provide a two-component seismometer and a three-component seismometer which can be provided to improve the detection sensitivity and exhibit a servo function or a feedback function without assembling a special member.

[0007]

For this purpose, the present invention as defined in claim 1 is characterized in that a gap is provided inside a hollow rectangular columnar load body with a gap interposed between the hollow cylindrical columnar load body and a hollow cylindrical load body. A solid rectangular column-shaped load body is disposed with the four gaps opposed to each other by the hollow load body and the cylindrical load body, and the four gaps are opposed to each other with the cylindrical load body interposed therebetween. ,
The light transmission characteristic is displaced in response to the pressure change due to the relative displacement of the load body due to the acceleration applied to the rigid plate and the four gaps where the cylindrical load body and the solid load body face each other. Further, a force sensor provided with a cylindrical or meandering optical fiber roll having an elastic constant smaller than that of the load body and the rigid plate is disposed in a stack, and the force sensor is arranged in each of four horizontal (XY) directions orthogonal to each other. Is a seismometer that is positioned so as to face the composite phase displacement obtained by averaging the output light of the optical fiber roll of the force sensor in each of the two directions in which the load is relatively displaced at the exit side of the optical fiber roll. It is characterized by including a measurement circuit for obtaining a phase difference output between the light and the reference light, and for obtaining an applied acceleration in a displacement direction of the solid load body based on a difference between the phase difference outputs.

[0008] According to the present invention, a solid rectangular columnar load body is disposed inside a hollow rectangular columnar load body with a gap interposed between the hollow loader and the solid loader. In each of the six opposing gaps, the rigid body plate has a light propagation characteristic in which the light transmission phase is displaced in response to a pressure change due to the relative displacement of the load body based on the application of the acceleration, and, compared to the load body and the rigid body plate. A plurality of force sensors each having a cylindrical or meandering optical fiber roll having a small elastic constant are stacked and arranged so that the force sensors are oriented in the horizontal (XY) four directions and the vertical (Z) two directions of the coordinate system. A seismometer to be positioned and disposed, wherein the output light of the optical fiber roll of the force sensor in each of the two directions in which the load body is relatively displaced, the combined phase displacement light obtained by averaging at the exit side of the optical fiber roll, Outputs the phase difference output from the reference light It is determined, characterized in that it comprises a measuring circuit for determining the acceleration applied in the direction of displacement of the relative displacement to two azimuth actual load body in based on the difference in phase difference output in each direction of.

According to a third aspect of the present invention, there is provided a solid rectangular columnar load in an internal space of a hollow rectangular columnar load of a Z-direction accelerometer arranged to be oriented in two vertical directions in an XYZ orthogonal coordinate system. The body is arranged to be displaceable in the vertical long axis direction, and toward the both end faces in the direction of displacement of the solid load body, the light propagation characteristic is applied to the rigid plate in response to the pressure change due to the relative displacement of the load body due to the application of acceleration. A force sensor comprising a cylindrical or meandering optical fiber roll having a light transmission phase displaced and having an elastic constant smaller than that of the load body and the rigid plate is laminated, and the outer periphery of the Z-direction accelerometer is provided. A pair of X-direction accelerometers for detecting acceleration in the X direction are arranged in the horizontal X direction of the surface, and a pair of Y-direction accelerometers for detecting acceleration in the Y direction are arranged in the horizontal Y direction on the outer peripheral surface. In the interior space of the X-direction accelerometer A solid rectangular column-shaped load body is displaceable in the horizontal major axis direction, and the light propagation characteristics are applied to the rigid plate in the longitudinal direction of both end faces in the displacement direction of the solid load body by applying acceleration to the rigid plate. A force sensor comprising a cylindrical or meandering optical fiber roll having a light transmission phase displaced in response to a pressure change due to a relative displacement of the optical fiber and having a smaller elastic constant than the load body and the rigid plate is provided. A solid rectangular columnar load body is disposed in the Y-direction accelerometer inside the space so as to be displaceable in the horizontal major axis direction, and a rigid body is provided in the longitudinal direction of both end faces in the displacement direction of the solid load body. In the plate, the light transmission characteristic is displaced in response to the pressure change due to the relative displacement of the load body due to the application of acceleration, and the cylindrical or meandering shape has a smaller elastic constant than the load body and the rigid plate. Optical fiber roll The output light of the optical fiber roll of the force sensor attached to one end face of each solid load body of the pair of X-direction accelerometers was averaged at the exit side of the optical fiber roll. Each of the combined phase displacement lights is further averaged, the recombined value and the phase difference output of the reference light, and the output light of the optical fiber roll of the force sensor attached to the other end face of each solid load body are converted to an optical fiber. Each of the combined phase displacement light obtained by averaging on the exit side of the roll is further added and averaged, and a recombined value and a phase difference output of the reference light are obtained,
The applied acceleration in the X direction is measured based on the difference between the phase difference outputs, and the output light of the optical fiber roll of the force sensor installed on one end face of each solid load body of the pair of Y-direction accelerometers is output from the optical fiber roll. Each of the combined phase displacement lights added and averaged on the exit side is further added and averaged, and a recombined value and a phase difference output of the reference light, and a force sensor provided on the other end face of each solid load body. The combined phase displacement light obtained by adding and averaging the output light of the optical fiber roll at the exit side of the optical fiber roll is further added and averaged to obtain a recombined value and a phase difference output of the reference light, respectively. The applied acceleration in the Y direction is measured based on the difference
The phase difference output between the combined phase displacement light obtained by averaging the output light of the optical fiber roll of the force sensor, which is positioned opposite to both end faces of the solid load body of the directional accelerometer at the exit side of the optical fiber roll, and the reference light, respectively. And a measuring circuit for measuring the Z-direction acceleration based on the difference between the phase difference outputs.

The invention according to claim 4 which depends on claim 2 or 3 measures acceleration in four horizontal directions in a storage container disposed on the bottom of a borehole drilled in the ground,
By configuring so that seismometers that measure acceleration in two vertical directions are housed, the effect of temperature fluctuation on the optical fiber roll in the housing is eliminated.

The invention according to claim 5, which is dependent on any one of claims 1 to 3, wherein the meandering optical fiber roll is immersed and disposed inside a bag filled with a viscous liquid,
The pressure applied to the internal optical fiber roll with the bag intervening from the outside, the viscous liquid inside the bag does not apply the dynamic pressure, and the hydrostatic pressure is maintained, and the uniform pressure is applied to the outer peripheral surface of the optical fiber roll. It is characterized in that a normal stress is applied to uniformly reduce the cross-sectional area and the optical fiber roll is converted into a change in the axial length.

The present invention according to claim 6 is dependent on any one of claims 1 to 3, wherein the meandering optical fiber roll is immersed and disposed inside a bag filled with a viscous liquid, The pressure applied to the internal optical fiber roll with the bag intervening from the outside, the viscous liquid inside the bag does not apply the dynamic pressure, and the hydrostatic pressure is maintained, and the uniform pressure is applied to the outer peripheral surface of the optical fiber roll. A normal stress is applied to reduce the cross-sectional area uniformly, and the optical fiber roll is formed so as to be converted into a change in the axial length of the optical fiber roll. The optical fiber roll is housed in a rigid tube to form a reference optical fiber roll, and a measurement optical fiber roll and a reference optical fiber roll are arranged side by side on a rigid plate. It is characterized in.

[0013]

Embodiments of the present invention will be described below with reference to the drawings. FIGS. 1 to 3 show a first embodiment of a seismometer according to the present invention. FIG. 1 shows a hollow rectangular columnar load 1 with a part 4 cut away, separated in the direction of the arrow, and retracted. FIG. 2 is a perspective view showing the internal state, FIG. 2 is a view of the load body 1 of the seismometer in FIG. 1 viewed from the direction of arrow A, and FIG.
Is a perspective view of the force sensor 8 obtained by molding the optical fiber roll 8A, (B) is a side view of the optical fiber roll 8A seen through the mold 8C from the direction of the arrow A 'in (A), and (C) is a plurality of views. (D) is a plan view of another type of force sensor provided with a meandering type optical fiber roll.
FIG. In the internal space of a hollow rectangular columnar load 1 fixed to a support base (not shown), a rectangular cylindrical load 2 surrounding a solid rectangular columnar load 3 with a gap interposed is provided. 1 are arranged with a gap therebetween. Each of the gaps in the two horizontal directions, that is, in the ± X directions, forms a part of an optical fiber cable, and is made of, for example, a plastic fiber. Has a function of displacing the transmission phase of the load, and has an elastic constant smaller than the elastic constants of the load body 1, the cylindrical body 2, the solid body 3, and the rigid plate formed of a metal body such as iron, and The optical fiber rolls 5A, 6A, 7A, and 8A acting as spring members by the elastic function of the optical fiber roll formed in a cylindrical or meandering shape are combined with the rigid plates 5B, 6B, and 7A.
B, 8B, force sensors 5, 6, 7, 8 are provided. Then, in two vertical directions, that is, ± Y directions,
Optical fiber rolls 9A, 10A, 11A, 12 having the same function as each rigid plate 9B, 10B, 11B, 12B.
The force sensors 9, 10, 11, 12 provided with A are provided. Incidentally, the elastic constant of iron is, for example, 1-2 ×
10 ¹¹ N / m ² , and an elastic constant of the optical fiber roll of 10 ⁸ to 10 ¹⁰ N / m ² is used.

The force sensor provided with the above-mentioned cylindrical optical fiber roll is constituted as follows. That is, after winding an optical fiber cable many times around the outer periphery of a cylindrical mold (not shown), the mold is pulled out, and the remaining optical fiber cable is molded as shown in FIG.
As shown in FIG. 3A, a cylindrical optical fiber roll 8A is formed. Then, for example, as shown in FIG. 3C, the end faces of the plurality of cylindrical optical fiber rolls 8A are fixedly installed on the surface of a rigid plate 8B formed of a metal body such as iron, and the optical fiber rolls 8A are connected to each other. The force sensor 8 is configured by being connected, and the light incident from the arrow direction passes through each optical fiber roll 8A and is emitted in the arrow direction.

[0015] The above-mentioned cylindrical optical fiber roll comprises:
Since the fiber line may be broken if bent at a certain radius or less, a force sensor provided with an optical fiber roll having a meandering fiber line with a large radius of curvature may be used. For the purpose of preventing stress from being applied to a specific area of the fiber wire, in other words,
In order to ensure that the fiber wire is evenly stressed,
In some cases, a wiring method that prevents the fiber lines from overlapping each other on the “wiring surface” is adopted. For example, as shown in FIG. 3 (D), this type of force sensor 8 'is formed by arranging optical fibers in a meandering shape on the surface of a rigid plate 8B, and fixed to the rigid plate 8B by a mold (not shown). It is formed.

Further, in the optical fiber rolls 5A to 12A of the sensors 5 to 12, as shown in FIG.
5 are individually transmitted, and at the exit side, pressure components f1 and f1 ′ generated by each force sensor.
, F2, f2 ', f3, f3', and f4, f4 'are added in parallel and averaged, and the averaged combined phase displacement light f
e, fw, fn, fs and the reference light from the reference circuit 16 are input to the component detection circuits (18-1) to (18-4).

(1) Description of Example of Applying Acceleration in X Direction Now, in FIG. 2, when a horizontal acceleration is applied to load body 1 from the direction of arrow F, cylindrical load body 2 and solid load body 3 In the opposite direction to the arrow F direction, that is, in the figure, the load body 1 is suddenly displaced so as to apply pressure to the right side thereof, and the rigid plate is also rapidly displaced due to the inertial force due to its mass.
Thereby, each optical fiber roll 5 of the sensors 5 and 6
A and 6A reliably transmit and apply a large pressure by the cylindrical load body 2, the solid load body 3, and the rigid plates 5B and 6B of the sensors 5 and 6, and generate pressure components f1 and f1 '. Is done. At this time, the elastic function of the optical fiber rolls 5A and 6A, in other words, the spring function is based on the pressing force and the balance by the cylindrical load body 2, the solid load body 3, and the rigid plates 5B and 6B of the sensors 5 and 6. The servo function for stopping the displacement of the cylindrical load member 2 and the solid load member 3 and the rigid plates 5B and 6B of the sensors 5 and 6 is exerted at a position where no special parts are added.

On the other hand, in the figure, the left cylindrical load body 2 and the solid load body 3 are displaced in a direction away from the left side portion of the load body 1, so that the load body 1 and the cylindrical load body are displaced. The pressurizing force previously applied to the sensor 7 interposed between the cylindrical load 2 and the sensor 8 interposed between the cylindrical load body 2 and the solid load body 3 is reduced, and is generated in the sensors 7 and 8. The pressure components f2 and f2 'change in the reverse sense (direction).

Therefore, as shown in FIG. 4, a composite phase displacement light fe obtained by adding and averaging these pressure components f1 and f1 '.
Pressure components Fe and f2, f indicating the phase difference between
By calculating the difference (Fe-Fw) between the pressure component Fw indicating the phase difference between the composite phase displacement light fw obtained by adding and averaging 2 'and the reference light, the acceleration applied from the direction of arrow F is detected.
At that time, since the outputs of the sensors are combined to obtain an average output, even if the sensitivity of a certain sensor is poor, the output is averaged and corrected by the outputs of the other sensors. Acceleration is detected with high sensitivity.

The sensors 9 and 1 existing in the Y direction
0, and the sensors 11 and 12 are displaced in the lateral direction without displacing the solid load body 3 and the rigid plates 9B, 10B, 11B and 12B in the Y direction so as to apply a pressing force to each sensor.
It receives equal pressure changes f3, f3 ', f4, and f4', and therefore, a pressure component Fn and a pressure component f4 indicating a phase difference between the synthetic phase displacement light fn obtained by averaging the pressure changes f3 and f3 'and the reference light. , F4 ′, and the difference (Fn) between the pressure components Fs indicating the phase difference between the composite phase displacement light fs obtained by averaging and the reference light.
By calculating −Fs), both pressure components are cancelled.

(2) Description of Example of Applying Acceleration in Y Direction Next, in FIG. 2, when acceleration in the horizontal plane Y direction is applied from the arrow G direction, the cylindrical load body 2 and the solid load body 3 Along with the rapid displacement in the direction opposite to the direction of the arrow Y, the rigid body plate is also displaced by its inertial force, so that the optical fiber roll 9A of the sensor 9 in the upper part of the solid body 3 in the figure,
A large pressure is reliably transmitted to the optical fiber roll 10A of the sensor 10 by the cylindrical load body 2, the solid load body 3, and the rigid plates 9B, 10B of the sensors 9, 10, and the pressure component f3, f3 'is generated. At this time, the elastic function of the optical fiber rolls 9A and 10A causes the cylindrical load member 2 to be positioned at a position that balances the pressing force of the cylindrical load member 2, the solid load member 3 and the rigid plates of the sensors 9 and 10. ,
Rigid plates 9B, 10B of solid load 3 and sensors 9, 10
Servo function to stop the displacement is exhibited without adding any special parts.

The sensor 11 below the solid load 3
And the pressure components f4 and f4 'applied to the sensor 12 change in the reverse sense (direction). For this reason, the sensors 9, 1
The combined phase displacement Fn indicating the phase difference between the reference light and the combined phase displacement light fn obtained by averaging the pressure components f3 and f3 ′ of 0 and the combined phase displacement obtained by averaging the pressure components f4 and f4 ′ of the sensors 11 and 12 By obtaining the difference (Fn-Fs) between the pressure component Fs indicating the phase difference between the light fs and the reference light, the acceleration component applied from the direction of arrow G can be obtained with high sensitivity.

The sensors 5 to 8 located in the X direction
Since the solid load body 3 and the rigid plate in the X direction are displaced in the lateral direction without being displaced so as to exert a pressing force on the respective sensors, equal pressure components f1, f1 ', f2, f2' are provided. Therefore, the combined phase displacement light fe of the optical fiber roll obtained by averaging f1 and f1 ′ and the pressure component Fe indicating the phase difference between the reference light and the combined phase displacement light fw of the optical fiber roll obtained by averaging f2 and f2 ′ and By obtaining the difference (Fe−Fw) from the pressure component Fw indicating the phase difference of the reference light, both outputs are canceled.

(3) General Description of Measurement of Applied Acceleration in X and Y Directions Now, the sensors 5 and 6 are set to the direction of X, and the sensors 7 and 8 are set to (−).
X), the pressure component f of the sensors 5 and 6
1, an output Fe indicating the phase difference between the combined phase displacement light fe and the reference light obtained by averaging f1 ′, and the positions of the combined phase displacement light fw and the reference light obtained by averaging the pressure components f2 and f2 ′ of the sensors 7 and 8. The difference (Fe-Fw) from Fw indicating the phase difference is obtained,
The applied acceleration in the X direction can be obtained.

Similarly, since the sensors 9 and 10 are oriented in the Y direction and the sensors 11 and 12 are oriented in the (-Y) direction, the combined phase displacement light obtained by averaging the pressure components f3 and f3 'of the sensors 9 and 10 is averaged. From the difference (Fn-Fs) between Fn indicating the phase difference between fn and the reference light, and Fs indicating the phase difference between the combined phase displacement light fs obtained by averaging the pressure components f4 and f4 'of the sensors 11 and 12 and the reference light. The applied acceleration in the Y direction is determined.

Next, the operation of the first embodiment will be described with reference to a measurement circuit for measuring each pressure component shown in FIG. First, in order to accurately match the output characteristics of the sensors 5 and 6 located in the X direction and the sensors 7 and 8 located in the -X direction, a component detection circuit ( In 18-1) to (18-4), the combined phase displacement light of each of the optical fiber rolls 5A to 12A and the reference light are converted into an electric signal, and the phases of the two are matched to be based on the phase difference. It is set so that no output is generated.

The reference circuit 16 to which the light from the light source 15 is incident generates reference light set to a reference phase to refer to the output lights of the optical fiber rolls 5A to 12A. The component detection circuits (18-1) to (18-4)
With reference to the combined phase displacement light fe, fw, fn, fs obtained by averaging the phase displacement light of each of the optical fiber rolls 5A to 12A into which the light transmitted from the light source 15 is divided and incident, and the reference light from the reference circuit 16, By calculating the phase differences Fe, Fw, Fn, and Fs, the pressure change components Fe, Fs, Fw, and Fn are detected. When the acceleration is applied in the X direction, the acceleration calculation section (19-
In 1), the applied acceleration in the X direction is obtained by extracting the difference (Fe-Fw) between the pressure components Fe and Fw. When the acceleration is applied in the Y direction, the applied acceleration in the Y direction is obtained by extracting the difference (Fn-Fs) between the pressure components Fn and Fs in the Y direction acceleration calculation unit (19-2). Of course, as described above, the output in the Y direction is canceled when the applied acceleration in the X direction is detected, and the output in the X direction is canceled when the applied acceleration in the Y direction is detected.

In this embodiment, the hollow load 1 and the cylindrical load 2, the cylindrical load 2 and the solid load 3
Although the example in which a single force sensor is provided in the gap between the first and second embodiments has been described, a configuration in which a large number of force sensors are stacked and arranged for each of the above gaps is also possible.

In consideration of the temperature dependence of the light propagation characteristics of the optical fiber roll, the heat capacity of the container as the load 1 is increased as much as possible. Then, it is necessary to form the container itself from a material having a low thermal conductivity so as not to be affected by the temperature, and to take care that the light propagation characteristic of the optical fiber roll does not fluctuate due to an external temperature change.

Further, in order to accurately measure a change in an optical signal using the above seismometer, it is necessary to remove the influence of temperature as much as possible. Therefore, by arranging the optical fiber cables through which the reference light and the measurement light pass at the same atmospheric position as much as possible, it is possible to accurately obtain the acceleration under the same temperature condition and the same pressure condition. I can do it. At this time, it is necessary to insert and hold the tube in a rigid tube in order to prevent the measurement pressure from being applied to the reference optical fiber and causing a phase displacement.

Next, a description will be given of a second embodiment of the seismometer according to the present invention for measuring accelerations in four directions in two horizontal directions and two directions in a vertical direction. FIG. 5 shows a hollow rectangular columnar load 2
5 is a perspective view of a seismometer showing a part 23 of the seismometer which is cut away and retracted in the direction of the arrow while removing the sensor in the direction Y. FIG. FIG. 7 is a view of the seismometer for detecting acceleration in two directions in the Z direction from the direction of arrow C in FIG. 5.

Inside a hollow rectangular column-shaped load 21 fixed to a support base (not shown), a square solid load 22 is mounted.
Are arranged in the XYZ orthogonal coordinate axis direction with a gap therebetween, and the gap in two directions in the ± X direction is shown in FIG.
As described above, the function of displacing the phase of the transmitted light in response to the pressing force and the elastic function of itself acting as a spring material are provided on the surface of the rigid plate 24B. Cylindrical or meandering optical fiber roll 2 having
4A, and optical fiber rolls 25A similar to the rigid plates 25B.
, And the same number of force sensors 25... Are laminated so as to prevent rattling due to the elastic function of the optical fiber cable. Further, as shown in FIG.
In the gaps in two directions in the Y direction, force sensors 26 having optical fiber rolls 26A... And 27A. , And 27... Are similarly formed by the elastic function of the optical fiber rolls 26 </ b> A and 27 </ b> A.
The same number of them are stacked so as not to cause backlash.

The force sensors stacked and arranged in the gap in the Z (vertical) direction shown in FIG. 7 will be described. The gap between the solid load body 22 and the hollow load body 21 has the same function as described above. Fiber rolls 28A and 29A having
, 29B are respectively provided on the surfaces of the rigid plates 28B, 29B,..., And the force sensors 28, 29 are stacked in the same number so that no play occurs due to the elastic function of the optical fiber rolls 28A, 29A. Is done. And the above-mentioned optical fiber rolls 24A, 25A, 26A, 27A
The optical fiber rolls 28A and 29A have an elastic function and a servo function like the optical fiber rolls of the sensors 5 to 12 described above.

Reference numeral 13 in FIGS. 6 and 7 denotes one of the six end surfaces of the solid body 3 and reference numeral 30 denotes
Are disposed at four corners inside the hollow load body 21 and between each side surface of the force sensors 24, 25, 26, 27, 28, and 29 and the inner side of the hollow load body 21. Are spacers for positioning and setting each sensor so as to be positioned on the solid load body 22. Further, also in the present embodiment, FIG.
As shown in the figure, the split light from the light source 15 is transmitted to each of the optical fiber rolls 24A to 29A in each of the sensors 24 to 29, and the output light of each optical fiber roll is added and averaged at the outlet side. Of course, the combined phase displacement light is formed.

Next, with reference to the measuring circuit shown in FIG. 8, the operation will be described in the order of measuring the acceleration in the XYZ directions. Also in this case, in the component detection circuits (30-1) to (30-6), the phases of the combined output light from each optical fiber roll at the time of no load and the reference light are matched.
Of course, the difference is adjusted so as not to be output.

(4) Description of the Measurement of the Acceleration in the X Direction In FIG.
The seismographs are arranged so that the sensors 26 and 27 face the (Y) and (−Y) directions, and the sensors 28 and 29 face the vertical direction (Z, −Z). Now, when acceleration is applied in the X direction, that is, in the direction of the arrow H, the solid load body 22
Abrupt displacement in the direction opposite to the
Is also rapidly displaced together with the rigid plate 24B, so that each optical fiber roll 24A of the sensor 24 has a solid load 2
2 and the pressing force of each rigid plate 24B are reliably transmitted and applied. At this time, the spring function of the cylindrical optical fiber roll 24A exerts a servo function of stopping the displacement at a position balanced with the pressing force by the load body and the rigid plate. Further, since the solid load body 22 is displaced in the direction opposite to the arrow H direction, the sensor 2
The pressing force previously applied to the fifth optical fiber roll 25A is reduced.

By the way, the sensors 26 and 27 in the Y direction
And the Z-direction sensors 28 and 29 have a solid load 2
2 and rigid plates 26B, 27B, 28B, 2 in the Y and Z directions.
9B is not displaced in the YZ directions exerting a pressing force, but is displaced in the lateral direction with respect to the sensor in the YZ directions, so that the same pressing force is exerted. Optical fiber roll 27A
The output in the Y direction can be canceled by calculating the output difference between the optical fiber roll 28A of the sensor 28 and the optical fiber roll 29A of the sensor 29 in the Z direction.
The output in the Z direction is canceled by calculating the difference from

Therefore, as shown in FIG. 8, the composite phase displacement light fe obtained by averaging the output lights of the optical fiber roll 24A of the X-direction sensor 24 at the exit side and the reference light are supplied to the component detection circuit (30-1). To compare the phase and output the phase difference Fe
(X direction) is obtained. Similarly, the composite phase displacement light f obtained by adding and averaging the optical fiber roll 25A of the X-direction sensor 25
w and the reference light are input to the component detection circuit (30-2), and the phase difference output Fw (-X
Azimuth), these Fe and Fw are input to the measurement arithmetic circuit 32, and the arithmetic unit (32-1) calculates the difference (Fe-F
w) is obtained, and the applied acceleration in the X direction is measured.

As described above, the same pressing force is applied to the optical fiber roll of the sensor in the Y direction. Therefore, the combined phase displacement light fn, fs, fu, fd obtained by averaging on the exit side of the optical fiber rolls 26A to 29A is
The component detection circuits (30-3) to (30-) together with the reference light
Enter the information in 6). The component detection circuit (30-3) obtains the phase difference output Fn between the combined phase displacement light fn of the optical fiber roll 26A of the Y-direction sensor 26 and the reference light, and the component detection circuit (30-4) calculates (-Y ) A phase difference output Fs between the combined phase displacement light fs obtained by averaging the optical fiber roll 27A of the direction sensor 27 and the reference light is obtained, and these phase difference outputs Fn and Fs are sent to the calculation unit (32-2) of the measurement calculation circuit 32. The output in the Y direction is canceled by inputting and calculating the difference (Fn-Fs).

Similarly, the same pressing force is applied to the optical fiber roll of the sensor in the Z direction. Therefore, the combined phase displacement light fu obtained by averaging the optical fiber roll 28A of the Z-direction sensor 28 is added to the component detection circuit (3
0-5), and the combined average phase-shifted light fd of the optical fiber roll 29A of the sensor 29 and the reference light are input to the component detection circuit (30-6). The component detection circuit (30-5) adds and averages the combined phase displacement light fu of the optical fiber roll 28A of the sensor 28 in the Z direction.
Phase difference Fu between the reference light and the reference light is obtained. Component detection circuit (30
In (-6), the phase difference Fd between the averaged combined phase displacement light fd of the optical fiber roll 29A of the (-Z) direction sensor 29 and the reference light is obtained, and these phase differences Fu and Fd are calculated by the measurement calculation circuit 32. The output in the Z direction is canceled by inputting to the section (32-3) and calculating the difference (Fu-Fd).

(5) Description of Acceleration Measurement in Y Direction Next, in FIG. 6, when acceleration is applied in the Y direction, that is, in the direction of arrow J, the solid load body 22 is reversed in the direction of arrow J. The sensor 26 is also rapidly displaced in the direction, that is, upward in the drawing, and the sensor 26 is also rapidly displaced together with the rigid plate 26B. Therefore, the large pressing force of the solid load body 22 and the pressing force of each rigid plate 26B are To the optical fiber roll 26A. At that time, the optical fiber roll 2
Due to the spring function of 6A, a servo function for stopping the displacement at a position balanced with the pressing force by the load body and the rigid plate is exhibited. On the other hand, since the solid load body 22 is displaced in the direction opposite to the direction of the arrow J, the pressure applied to the sensor 27 in advance is reduced. Then, the phase difference Fn between the combined phase displacement light fn obtained by averaging the outputs of the optical fiber roll 26A of the sensor 26 and the reference light, the combined phase displacement light fs obtained by averaging the outputs of the optical fiber roll 27A of the sensor 27, and The phase difference Fs from the reference light is obtained, and the applied acceleration in the Y direction is measured from the difference (Fn-Fs).

The X-direction sensors 24 and 25
And the sensors 28 and 29 in the Z direction, the solid load body 2
2 and rigid plates 24B, 25B, 28B, 2 in the X and Z directions.
9B is displaced in the lateral direction with respect to the sensor without displacing in the direction in which the pressing force is applied, so that the same pressing force is applied.
For this reason, the optical fiber roll 2 of the sensor 24 in the X direction
4A and the optical fiber roll 25 of the sensor 25 in the X direction
The output difference from A is obtained and the output is cancelled.
And the difference between the Z direction and the optical fiber roll 29A of the sensor 29 in the Z direction, thereby canceling the output.

Therefore, when measuring the applied acceleration in the Y direction, the combined phase displaced light fn obtained by displacing and averaging the phase of the optical fiber roll 26A of the sensor 26 in the Y direction is calculated by:
The phase shift of the optical fiber roll 27A of the sensor 27 in the Y-direction and the averaged combined phase-shifted light fs, together with the reference light, are used as component detection circuits (30-3) and (30-4).
(FIG. 8). Component detection circuit (30-
In 3), the phase difference Fn (Y direction) between the combined phase displacement light of each optical fiber roll 26A and the reference light is obtained. In the component detection circuit (30-4), the combined phase displacement light of the optical fiber roll 26A of the sensor 27A is obtained. A phase difference Fs (−Y azimuth) with respect to the reference light is calculated, and the difference (Fn−F) is calculated by the calculation unit (32-2) of the measurement calculation circuit 32.
s) is obtained, and the applied acceleration in the Y direction is measured.

As described above, the same pressure is applied to the optical fiber roll of the sensor in the X direction. Then, the composite phase displacement light fe obtained by averaging the optical fiber roll 24A in the X direction and the reference light are used as a component detection circuit (30).
-1) to obtain the phase difference Fe, and the combined phase displacement light fw obtained by adding and averaging the optical fiber roll 25A in the -X direction and the reference light to the component detection circuit (30-2). The phase difference Fw is obtained. The same pressing force is applied to the optical fiber roll of the sensor in the Z direction. Therefore, the combined phase displacement light fu obtained by averaging the optical fiber roll 28A in the Z direction and the reference light are used as component detection circuits (30
-5) to obtain the phase difference Fu. -Synthesized phase displacement light f obtained by averaging the optical fiber roll 29A in the -Z direction
d and the reference light are input to the component detection circuit (30-6) to determine the phase difference Fd. The phase differences Fe and Fw and similarly the phase differences Fu and Fd are input to the measurement calculation circuit 32, and the calculation units (32-1) and (32-3) output the difference (Fe-F).
w) and (Fu-Fd), respectively, whereby both outputs are canceled.

(6) Description of Acceleration Measurement in Z Direction Next, in FIG. 7, when acceleration is applied in the Z (vertical) direction, that is, in the direction of arrow K, the solid load body 22
In the opposite direction to the direction, that is, while being rapidly displaced upward, the sensor 28 is also rapidly displaced with each rigid plate 28B,
For this reason, the large pressing force of the solid load body 22 and the pressing force of each rigid plate 28B are
8A is reliably transmitted and provided. At this time, the spring function of the optical fiber roll 28A exerts a servo function of stopping the displacement at a position balanced with the pressing force by the load body 22 and the rigid plate 28B. On the other hand, since the solid load body 22 is displaced in the direction opposite to the arrow K direction,
The pressure applied to the optical fiber roll 29A of the sensor 29 in advance is reduced.

Incidentally, since the solid load body 22 and the rigid plates 24B, 25B, 26B, 27B in the X and Y directions are not displaced in the XY directions exerting the pressing force but are displaced in the lateral direction.
The same pressing force is applied to the sensors 24 and 25 in the X direction and the sensors 26 and 27 in the Y direction. Therefore, the phase difference Fe between the added and averaged combined phase displacement light fe of the optical fiber roll 24A of the sensor 24 in the X direction and the reference light, and the combined and averaged combined phase displacement light fw and the reference light of the optical fiber roll 24A of the sensor 25 are calculated. From the phase difference Fw (Fe
By calculating -Fw), the output is canceled. The optical fiber roll 2 of the sensor 26 in the Y direction
6A, the phase difference Fn between the averaged combined phase displacement light fn and the reference light, and the phase difference F between the averaged combined phase displacement light fs of the optical fiber roll 26A of the sensor 27 and the reference light.
By calculating the difference (Fn-Fs) from s, the output is canceled.

Therefore, when measuring the applied acceleration in the Z direction, the combined phase displacement light fu obtained by adding and averaging the optical fiber roll 28A of the Z direction sensor 28 and the added and averaging the phase of the optical fiber roll 29A of the sensor 29 are obtained. The combined phase displacement light fd and the reference light are input to the component detection circuits (30-5) and (30-6), respectively, and the combined phase displacement lights fu and fd obtained by adding and averaging the optical fiber rolls 28A and 29A, and the reference light And the phase differences Fu and Fd. And an operation unit (32-3) of the measurement operation circuit 32
, The difference (Fu−Fd) is obtained, and the applied acceleration in the Z direction is calculated.

As described above, the X direction sensors 24 and 25
The same pressing force is applied to the optical fiber rolls. Therefore, the optical fiber roll 2 of the X-direction sensor 24
The averaged combined phase displacement light fe from 4A and the reference light are input to a component detection circuit (30-1), and the averaged phase displacement light fw of the optical fiber roll 25A of the X-direction sensor 25 and the reference Light and a component detection circuit (30-
2) and outputs Fe and Fw indicating the phase difference from the reference light.
Ask for. The same pressing force is applied to the optical fiber rolls of the Y direction sensors 26 and 27. So, Y
The combined phase displacement light fn obtained by averaging the optical fiber roll 26A of the direction sensor 26 and the reference light are input to the component detection circuit (30-3), and the averaging combined of the optical fiber roll 27A of the Y direction sensor 27 is obtained. The phase displacement light fs and the reference light are input to the component detection circuit (30-4), and phase differences Fn and Fs from the reference light are obtained. These outputs Fe, Fw and Fn, Fs are measured
The two outputs are canceled by inputting them to the two calculation units (32-1) and (32-2) and calculating the output differences (Fe-Fw) and (Fn-Fs).

Next, a description will be given of a third embodiment of the seismometer of the present invention for detecting applied accelerations in two horizontal directions and a vertical direction. FIG. 9 is a perspective view of a seismometer in which horizontal (XY) two-directional accelerometers 40 and 50 are assembled in a girder shape around a vertical (Z) direction accelerometer 60, and FIG.
A and 41B are removed, and a perspective view of the X-direction accelerometer 40 showing an internal state, FIG.
FIGS. 12A and 12B are perspective views of the Y-direction accelerometer 50 showing the internal state with A and 51B removed, and FIG. 12 is a perspective view of the Z-direction accelerometer 60 showing the internal state with two side walls 61A and 61B removed.

In FIG. 9, the outer peripheral surface below the accelerometer 60 for detecting acceleration in two directions in the vertical (Z) direction having a rectangular cross section fixed to a support base (not shown) includes
A pair of accelerometers 40 and 40A for detecting acceleration in two horizontal directions, that is, ± X azimuth, are disposed opposite to each other, and a pair of accelerometers 50 and 50A for detecting acceleration in ± Y azimuth are also disposed opposite to each other. At the same time, it is fixed to the support base in a girder shape.

(7) Description of the structure of the accelerometer in the XYZ directions The outer wall surfaces 41A and 41B are removed and the X-axis accelerometer 40
Referring to FIG. 10 showing the inside of a hollow body 42, a solid load body 43 having a rectangular cross section is disposed at the center of the inside of a hollow body 42 having a rectangular cross section so as to be displaceable in the longitudinal direction. A force sensor 44 is provided on each end surface of the longitudinal direction 43 of the rigid plate 44B... Provided with a cylindrical or meandering optical fiber roll 44A.
And the same number of force sensors 45... Provided with cylindrical optical fiber rolls 45 A... Having the same function on the rigid plates 45 B. ing.

Next, referring to FIG. 11, which shows the inside of the Y-direction accelerometer 50 by removing the outer wall surfaces 51A and 51B,
Similarly, a solid load body 53 having a rectangular cross section is disposed at the center of the inside of the hollow body 52 having a rectangular cross section so as to be movable in the longitudinal direction. A force sensor 5 provided with a cylindrical optical fiber roll 55A... On a rigid plate 55B.
, And similarly, a force sensor 56 provided with a cylindrical optical fiber roll 56A on a rigid plate 56B.
Are stacked in the same number without any mutual play.

Since the X-direction accelerometer 40A and the Y-direction accelerometer 50A are formed of exactly the same components as the X-direction accelerometer 40 and the Y-direction accelerometer 50, the description thereof will be omitted. Omitted. Therefore, when citing and describing the components of the X-direction accelerometer 40A and the Y-direction accelerometer 50A, reference numerals such as the optical fiber roll of the X-direction accelerometer 40 and the Y-direction accelerometer 50 and the force sensor are used. And a dash.

Further, referring to FIG. 12, which shows the inside of the Z-direction accelerometer 60 by removing the outer wall surfaces 61A and 61B, a solid load body having a rectangular cross section is provided at the center of the hollow body 62 having a rectangular cross section. 63 is disposed movably in the long axis direction, and both end surfaces of the load body 63 in the long axis direction are
Along the long axis direction, a force sensor 64 provided with a cylindrical optical fiber roll 64A provided on a rigid plate 64B.
And a cylindrical optical fiber roll 65A on the rigid plate 65B.
Are arranged in the same number without any backlash.

The cylindrical optical fiber rolls 44A and 44A 'and 45A and 45A'
, 55A, 55A ', 56A, 56A', and the optical fiber rolls 64A, 65A have the light propagation characteristics when pressure is applied similarly to the optical fiber rolls 5A to 12A of the sensors 5 to 12 described above. It has a variable characteristic, has an elastic function acting as a spring, and exhibits a servo function.

As is apparent from FIG. 13 showing the measuring circuit, the optical fiber roll 4 of the X-direction accelerometer 40
A combined phase displacement light fe ′ averaged on the exit side of 4A,
The combined phase displacement light fe ″ added and averaged at the exit side of the optical fiber roll 44A ′ of the X-direction accelerometer 40A is further added, and the averaged recombined value fe is input to the component detection circuit (70-1) together with the reference light. The combined phase displacement light fw ′ averaged at the exit side of the optical fiber roll 45A of the X-direction accelerometer 40 and the combined phase displacement light fw ″ averaged at the exit side of the optical fiber roll 45A ′ of the X-direction accelerometer 40A. Are further added and averaged and the recombined value fw is input to the component detection circuit (70-2) together with the reference light.

The combined phase displacement light f averaged and added at the exit side of the optical fiber roll 55A of the Y-direction accelerometer 50.
n ′ and the optical fiber roll 5 of the Y-direction accelerometer 50A
The combined phase displacement light fn ″ averaged and added on the exit side of 5A ′ is further added and added, and the recombined value fn is input to the component detection circuit (70-3) together with the reference light. The combined phase displacement light fs ′ averaged at the exit side of the 50 optical fiber roll 56A and the combined phase displacement light fs ″ averaged at the exit side of the optical fiber roll 56A ′ of the Y-directional accelerometer 50A are further added in parallel. ,
The averaged recombined value fs is input to the component detection circuit (70-4) together with the reference light.

Further, from the optical fiber rolls 64A and 65A of the Z-direction accelerometer 60, the combined phase displacement lights fu and fd obtained by adding and averaging at the exit side are output, and the component detection circuit (70- 5), (7
0-6). It goes without saying that the split light of the light source 15 is individually input for each optical fiber roll of the force sensor in the XYZ directions.

Next, referring to FIG. 13, the operation of the accelerometer in the XYZ directions will be described in the order of measuring the acceleration in the X, Y, and Z directions. In this case, the component detection circuit (70-
In 1) to (70-6), of course, when no acceleration is applied, the phase is adjusted so that the phase difference between the combined output light of each optical fiber roll and the reference light does not occur.

(8) Description of the Measurement of the Acceleration in the X Direction The accelerometers 40, 40 for detecting the acceleration in the X direction will now be described.
Accelerometers 50, 50A for detecting acceleration in A and Y directions
Are arranged in the XY directions as shown in FIG. Then, a pair of accelerometers 40 and 40A for X-direction acceleration detection are provided.
10, when the acceleration is applied from the direction of the arrow X as shown in FIG. The load bodies 43, 4 having large mass
A large pressing force due to the displacement of 3 ′ and the rigid plates 44B, 4B
The pressing force by 4B 'is reliably transmitted to the optical fiber rolls 44A, 44A' of the sensors 44, 44 '.
At that time, the servo function of stopping the displacement at a position balanced with the pressing force by the load and the rigid plate is exerted by the spring function of the optical fiber rolls 44A and 44A '. On the other hand, the load bodies 43 and 43 '
Since the displacement is made in the opposite direction, the pressing force previously applied to the optical fiber rolls 45 and 45A 'of the sensors 45 and 45' is reduced.

By the way, the accelerometers 50 and 50A in the Y direction
The load bodies 53, 53 'and the rigid plates 56B, 56B' in the Y direction are applied to the optical fiber rolls 55A, 55A 'and the optical fiber rolls 56A, 56A' in the directions in which the pressing force is applied. Is not displaced, so that the same pressing force is applied to each optical fiber roll described above. Similarly, the optical fiber roll 64A of the accelerometer 60 in the Z direction and the optical fiber roll 65A are similarly displaced in the direction in which the load 63 and the rigid plates 64B, 65B in the Z direction exert a pressing force. The same pressure is applied to the roll.

Therefore, a pair of X direction sensors 40, 40A
Optical fiber rolls 44A located in the X direction within
4A 'and the combined phase displacement light f obtained by adding and averaging the output light
e ′ and fe ″ are further added, and the averaged recombined value fe is
It is input to the component detection circuit (70-1) together with the reference light.
In the component detection circuit (70-1), the phase difference Fe between the recombined value obtained by averaging the combined displacement light fe of the optical fiber rolls 44A and 44A 'located in the X direction and the reference light is obtained.

Also, the combined phase displacement lights fw ′ and fw ″ obtained by adding and averaging the output lights of the optical fiber rolls 45A and 45A ′ located in the (−X) direction are further added and averaged to obtain a recombined value. fw is input to the component detection circuit (70-2) together with the reference light.
Then, the optical fiber roll 45A located at (−X),
A phase difference Fw between a recombined value fw obtained by adding and averaging the respective combined phase displacement lights of 45A 'and the reference light is obtained. Then, the phase differences Fe and Fw are input to the calculation unit (71-1) of the measurement calculation circuit 71, and the difference (Fe-Fw) is obtained to measure the applied acceleration in the X direction.

On the other hand, as described above, when the acceleration is applied in the X direction, the load bodies 53, 53 'in the accelerometers 50, 50A in the Y direction and the rigid plates 55B, 55B in the Y direction are applied.
', 56B, 56B' are not displaced in the direction in which the pressing force is applied, and the load body 63 of the Z-direction accelerometer 60 and the rigid plates 64B, 65B in the Z direction are not displaced in the direction in which the pressing force is applied. , Sensors 55 and 55 ', sensors 56 and 56', and sensors 64 and 65 are subjected to the same pressing force.

For this reason, the component detection circuit (70-3)
In (70-4), the combined phase displacement lights fn ′ and fn of the optical fiber rolls 55A and 55A ′ located in the Y direction
The re-combined value fn obtained by adding n ″ and averaged and the re-combined value obtained by adding and averaging the combined phase displacement light fs ′ and fs ″ of the optical fiber rolls 56A and 56A ′ located in the (−Y) direction. fs is input together with the reference light. Then, in the component detection circuit (70-3), the averaged recombined value f of the optical fiber rolls 55A and 55A 'is obtained.
The phase difference output Fn between n and the reference light is obtained. In the component detection circuit (70-4), the optical fiber roll 56A,
The recombined value fs of 56A 'and the reference light are input, and the phase difference output Fs between the averaged recombined value fs and the reference light is obtained. Then, these outputs Fn and Fs are measured by the measurement arithmetic circuit 7.
1 is input to the arithmetic unit 71-2, and the difference in (Fn-Fs) is obtained, thereby canceling the output in the Y direction.

Similarly, in the component detection circuit (70-5),
The phase difference Fu between the combined phase displacement light fu of the optical fiber roll 64A and the reference light is obtained, and a component detection circuit (70-
In 6), the phase difference Fd between the combined phase displacement light fd of the optical fiber roll 65A and the reference light is obtained. Then, the phase difference outputs Fu and Fd are input to the calculation unit (71-3) of the measurement calculation circuit 71, and the difference (Fu−Fd) is obtained, whereby the output in the Z direction is canceled.

(9) Description of Measurement of Acceleration in Y Direction Next, the detection of acceleration applied in the direction of arrow Y shown in FIGS. 9 and 11 will be described. When acceleration is applied to the Y-direction acceleration detecting accelerometers 50 and 50A from the arrow Y direction as shown in FIG. 11, the load bodies 53 and 53 'are rapidly displaced in a direction opposite to the arrow Y direction. , Sensor 55,
55 'is also rapidly displaced, so that a large pressing force due to the displacement of the load bodies 53, 53' having a large mass and each rigid plate 5
The pressing force by 5B and 55B 'is reliably transmitted and applied to the optical fiber roll 55A of the sensor 55 and the optical fiber roll 55A' of the sensor 55 '. At this time, the spring function of the optical fiber rolls 55A and 55A 'stops the displacement at a position balanced with the pressing force by the load body and the rigid body plate, and the servo function or the feedback function is exhibited. On the other hand, the load bodies 53 and 53 'are indicated by arrows Y.
Since the displacement is made in a direction opposite to the direction, the pressing force previously applied to the optical fiber roll 56A of the sensor 56 and the optical fiber roll 56A 'of the sensor 56' is reduced.

By the way, the accelerometers 40 and 40A in the X direction
, The load bodies 43, 43 'of the X-direction accelerometers 40, 40A and the rigid plates 44B, 44B of the X-direction.
, 45B, 45B ′ do not displace in the direction in which the pressing force is exerted, and the sensors 64, 65 of the accelerometer 60 in the Z direction
In contrast, the load 63 of the accelerometer 60 in the Z direction and the rigid plates 64B and 65B in the Z direction do not displace in the direction in which the pressing force is applied.

Therefore, the same pressing force is applied to the optical fiber rolls 44A and 44A 'and the optical fiber rolls 45A and 45A' in the X-direction accelerometers 40 and 40A. A total of 60 optical fiber rolls 64A,
The same pressing force is applied to the optical fiber roll 65A.

Therefore, when measuring the Y-direction acceleration, the combined phase displacement light fn ′ of the optical fiber roll 55A of the Y-direction accelerometer 50A and the combined phase displacement light fn ″ of the optical fiber roll 55A ′ of the Y-direction accelerometer 50A are used. , The combined phase displacement light fs 'of the optical fiber roll 56A of the Y-direction accelerometer 50, and the combined phase of the optical fiber roll 56A' of the Y-direction accelerometer 50A. Displacement light fs ″ at its output,
A re-synthesized value fs obtained by re-addition and averaging is obtained, and these are obtained together with the reference light by the component detection circuits (70-3) and (7-3).
Input to 0-4).

In the component detection circuit (70-3), a recombined value fn obtained by averaging the combined phase displacement light fn 'of the optical fiber roll 55A and the combined phase displacement light fn "of the optical fiber roll 55A', and the reference light Phase difference Fn of Y direction
Ask for. In the component detection circuit (70-4), the re-combined value fs obtained by averaging the combined phase displacement light fs 'of the optical fiber roll 56A and the combined phase displacement light fs "of the optical fiber roll 56A' and the reference light ( -Y) The phase difference output Fs of the azimuth is obtained, and the phase difference outputs Fn and Fs are input to the measurement calculation circuit 71, and the calculation unit (71-
In 2), the difference (Fn-Fs) is obtained, and the acceleration applied in the Y direction is obtained.

On the other hand, as described above, the sensors 44 and 44 'in the X-direction accelerometers 40 and 40A, and the sensors 45 and 44'
Since the same pressure is applied to 5 ′ and the Z-direction sensors 64 and 65, a pair of X-direction accelerometers 40 and 65
The recombined value fe obtained by averaging the combined phase displacement lights fe 'and fe "of the 40A optical fiber rolls 44A and 44A'.
And a re-combined value fw obtained by averaging the combined phase displacement lights fw ', fw "of the optical fiber rolls 45A, 45A' together with the reference light, and a component detection circuit (70-1), (70
-2), and obtain their phase differences Fe and Fw. Similarly, the combined phase displacement light fu of the optical fiber roll 64A of the Z (vertical) direction accelerometer and the combined phase displacement light fd of the optical fiber roll 65A together with the reference light are used as component detection circuits (70-5) and (70-6). ), And obtain the phase differences Fu and Fd. Then, these phase difference outputs Fe, Fw, Fu, and Fd are input to the operation units (71-1) and (71-3) of the measurement operation circuit 71, and the differences (Fe-Fw), (Fu-Fd) ), X
Output in the direction and Z direction is canceled.

(10) Description of the Action of Measuring the Acceleration in the Z Direction Next, the action of detecting the acceleration applied in the Z direction shown in FIG. 9 will be described with reference to FIG. When acceleration is applied to the Z-direction acceleration detecting accelerometer 60 in the direction of the arrow Z as shown in FIG. 12, the load body 63 is rapidly displaced in the direction opposite to the direction of the arrow Z, and the sensor 64 is also rapidly changed. Therefore, a large pressing force due to the displacement of the load body 63 having a large mass and a pressing force by each rigid plate 64B are reliably transmitted and applied to the optical fiber roll 64A of the sensor 64. At this time, the spring function of the optical fiber roll 64A exerts a servo function of stopping the displacement at a position balanced with the pressing force by the load body 63 and the rigid plate 64B. On the other hand, since the load body 63 is displaced in the direction opposite to the arrow Z direction, the pressing force previously applied to the optical fiber roll 65A of the sensor 65 is reduced.

Then, the combined phase displacement light fu of the optical fiber roll 64A and the combined phase displacement light fd of the optical fiber roll 65A in the Z-direction accelerometer 60 together with the reference light are used as component detection circuits (70-5) and (70-
Input to 6). Then, a phase difference Fu between the combined phase displacement light fu of the optical fiber roll 64A and the reference light and a phase difference Fd between the combined phase displacement light fd of the optical fiber roll 65A and the reference light are obtained. Then, the difference (Fu−Fd) is input to the calculation unit (71-3) of the measurement calculation circuit 71, and the acceleration applied in the Z direction is calculated.

By the way, when the acceleration is applied in the Z direction, each load body 4 in the X direction accelerometers 40 and 40A
3, 43 ′, and rigid plates 44B, 44B ′ in the X direction,
5B, 45B ', the load bodies 53, 53' in the Y-direction accelerometers 50, 50A, and the rigid plates 55B, 55 in the Y-direction.
B ', 56B, 55B' are not displaced in the direction in which the pressing force is applied. , 50A, the same pressing force is applied to the optical fiber rolls 55A, 56A and the optical fiber rolls 55A ′, 56A ′. The component detection circuit (70-1) includes optical fiber rolls 44A of the X-direction accelerometers 40 and 40A,
Further, the combined phase-shifted lights fe ′ and fe ″ of 44 </ b> A ′ are re-synthesized and added and averaged, and a re-combined value fe and a reference light are input, and the phase difference Fe is calculated. (70-2) includes optical fiber rolls 45A,
Further, a recombined value fw obtained by recombining and adding and averaging the combined phase displacement lights fw ′ and fw ″ of 5A ′ and a reference light are input, and a phase difference Fw thereof is calculated.

On the other hand, in the component detection circuit (70-3), Y
Optical fiber roll 55 of directional accelerometer 50, 50A
A recombined value fn of each of the combined phase displacement lights fn ′ and fn ″ of A and 55A ′ and the reference light are input, and the phase difference Fn is calculated. , 56A ′, the combined phase displacement light fs ′,
fs ″ is input with the recombined value fs and the reference light, and the phase difference Fs is calculated.

Then, the phase differences Fe and Fw are input to the calculation unit (71-1) of the measurement calculation circuit 71, and the difference, that is,
By calculating (Fe-Fw), the output in the X direction is canceled. Further, in (71-2), the output in the Y direction is canceled by obtaining the difference (Fn-Fs) of the phase difference.

Further, as shown in FIG. 14, a cylindrical storage container 82 is fixed on the bottom 81 of a borehole 80 drilled at an underground depth of about 30 m or less where temperature change hardly occurs. In this container 82, a three-component seismometer as shown in FIGS. 5 to 7 described above is fixedly arranged, or a horizontal two-component seismometer and a seismometer capable of measuring a vertical component are fixed. It is also possible to arrange and transmit the data collected by the seismometer to a ground-based observation device via the signal line 83 for seismic observation. Here, the phase data of the optical signal of the seismometer is converted into three-component ground motion data in the hole by, for example, a “data processing transmission device” 84 provided directly above the seismometer, and then transmitted to the ground. It is desirable to do.
In this case, since the optical fiber roll installed in the storage container 82 can measure the acceleration without being affected by the fluctuation of the ambient temperature, accurate observation information can be transmitted to the ground station.

When a cylindrical or meandering optical fiber roll is provided on the rigid plate of the force sensor applied to the first to third embodiments of the present invention, the hardness is slightly smaller than the hardness of the optical fiber roll. By using a synthetic resin having high hardness (for example, (hard) plastic or glass material) or the like, noise can be reduced and the SN ratio can be improved.

For example, a force sensor in which a meandering optical fiber roll is immersed and disposed in a viscous liquid filled in a rectangular bag will be described below with reference to the drawings instead of the above-described method in which the optical fiber roll is installed by molding. I do.
FIG. 15A is a plan view of the force sensor 8 ″ seen through the bag body 90 and the inside thereof is seen. FIG. FIG. 2C is a perspective view of the force sensor 8 ″, which is a simplified view of the optical fiber roll, and FIG. 2C is an optical fiber 9 when a cross section cut along a cutting line MM shown in FIG.
FIG. 3 is a diagram showing a state where stress is applied from the normal direction of the outer peripheral surface of FIG.

Referring to FIG. 15A, when an external pressure is applied to the bag 90 in the rectangular bag 90 formed of vinyl or the like, dynamic pressure is not applied to the internal optical fiber roll 91. So that a viscous liquid 9 such as silicon having a volume substantially equal to the inner volume of the bag
2 are filled. An optical fiber roll 91 which is coated with a coating material and solidified so as to maintain a meandering shape is immersed in the bag body 90.

As shown in FIG. 15B in which the shape of the meandering optical fiber cable inside is simplified in a sawtooth shape, a load member or a rigid plate Are arranged. Then, as shown in FIG. 15C, when the load or the rigid plate is displaced and external pressure is uniformly applied to the front and back surfaces in the direction of arrow R, the viscous liquid 92 inside hardly flows. , Does not generate dynamic pressure. For this reason, the hydrostatic pressure state is given to the optical fiber roll 91 without giving a dynamic pressure. Therefore, the stress is uniformly applied to the entire outer peripheral surface of the optical fiber roll 91 from the normal direction as shown by the arrow V. Thereby, the optical fiber roll 91
Is uniformly reduced from the dotted line to the solid line position. Therefore, a change in pressure from the outside can be converted into a change in the length of the optical fiber cable in the axial direction, so that the external pressure can be measured based on a change in the light propagation characteristics. As described above, since the cross section of the optical fiber cable can be changed uniformly and converted into a change in the length direction, all pressure changes in the optical fiber roll are converted into changes in the axial length of the optical fiber roll,
For this reason, the phase change can be measured smoothly,
Measurement resolution and accuracy are improved.

Next, a description will be given of an embodiment in which a measurement optical fiber roll and a reference optical fiber roll are arranged side by side on the same rigid plate, and the two optical fiber rolls are placed in the same atmosphere to improve the measurement accuracy. As shown in FIG. 16, for example, the reference light emitted from the reference circuit 16 shown in FIG. 4 is branched into a number equal to the number of rigid plates to form a reference optical fiber roll 8F. The optical fiber roll 8F is paired with the optical fiber roll 8D for measurement, and is disposed close to each of the rigid plates 8B shown as a representative example in FIG.

That is, the measurement optical fiber roll 8D and the reference optical fiber roll 8F to which light having the same shape and the same length and the same light intensity is transmitted are mounted on the rigid plate 8B of the force sensor 8 '. Are arranged in close proximity. Then, as described with reference to FIGS. 15A to 15C, the measuring optical fiber roll 8D fills the bag 90 ′ having a circular cross section with a sufficient amount so as not to be deformed even when an external pressure is applied. When immersed in the viscous liquid and applied with an external pressure, a hydrostatic pressure is applied without applying a dynamic pressure, whereby the diameter of the optical fiber roll 8D in the diameter direction is reduced, and the length in the longitudinal direction is reduced. The dimensions elongate. On the other hand, the reference optical fiber roll 8F has the same diameter as that of the bag body 90 'and is housed in a rigid tube body 8G so as not to be deformed even when pressure is applied.

As described above, the measurement optical fiber roll 8D and the reference optical fiber roll 8F are arranged close to the rigid plate 8B, and the two fiber rolls are placed under the same atmosphere, whereby the measurement accuracy can be improved. .

The XY accelerometer of the seismometer is not necessarily arranged in the north, south, east and west directions, but is arranged at an arbitrary angle. Can be detected. In addition, this seismometer can be used not only on the ground surface but also on the sea floor, lake bottom, celestial body surface, etc., and also for rockets, satellites, gyros, etc. It can be mounted and used.

Further, according to the present invention, not only the above-described phase change data but also the change data of the forward scattered light, the back scattered light, and the transmitted light intensity are used, and the applied acceleration is obtained by performing the same data processing. I can do it. In this case, needless to say, the phase comparison processing with the reference light used in the phase change data processing is unnecessary. Further, since the acceleration data can be integrated to obtain velocity data and displacement data, the present invention can be called a seismometer in this sense.

[0088]

As described above, according to the first and second aspects of the present invention, the rigid body plate has a light propagation characteristic in response to the pressure change in the gap formed between the relatively displaced load bodies. In addition to the function of displacing the phase, a force sensor comprising a cylindrical or meandering optical fiber roll having a smaller elastic constant than the load body and the rigid body plate is laminated and arranged, and the load body that opposes the relative displacement It is configured to output the composite phase displacement light obtained by averaging the phase displacement light from the optical fiber roll of the force sensor in each of the two directions at the exit side, so that the detection sensitivity is included in the stacked force sensors. Even if inferior sensors exist, they are averaged by the detection outputs of many other healthy force sensors,
The deterioration of the detection sensitivity is corrected, the detection sensitivity can be improved, and the measurement accuracy can be improved.In addition to the load, each rigid plate is also rapidly displaced by the application of acceleration,
Thereby, since the pressing force by the load body and the pressing force by each rigid plate are applied to the laminated cylindrical optical fiber rolls, it is possible to reliably transmit and apply the applied acceleration to each optical fiber roll, Thereby, the acceleration signal can be reliably generated from each force sensor.

Further, since the optical fiber roll has an elastic function and is formed in a cylindrical shape, the optical fiber roll itself is located between the load of the seismometer and the rigid plate.
It functions in the same way as a spring member, so that the displacement between the load body and the rigid plate can be stopped at a position that balances the pressing force due to the displacement of the load body and the rigid plate. It can function as a member having a servo function, and this function can be realized without adding a special component.

Further, since the cylindrical optical fiber roll has an elastic function as described above, the cylindrical optical fiber roll itself can behave as an elastic material between the load body and the rigid plate, and a force is applied to the load body and the rigid plate. The sensors can be arranged without rattling with each other.

Further, according to the three-component seismometer according to the third aspect of the present invention, in addition to the same effects as those of the first and second aspects of the present invention, the combined phase displacement of the optical fiber roll in the pair of X-direction accelerometers is provided. In addition to the configuration in which the light is further added in parallel to obtain a recombined value that is averaged, and the combined phase displacement light of the optical fiber rolls in the pair of Y-direction accelerometers is further added in parallel and the recombined value that is averaged is obtained. The output of the optical fiber roll when obtaining the applied acceleration in the X or Y direction is further averaged because it is configured to obtain the acceleration.

According to the fourth aspect of the present invention, a three-component seismometer using an optical fiber sensor is installed in a borehole drilled in the ground, thereby controlling the ambient temperature of the optical fiber roll in the storage container. By keeping the temperature constant, it is possible to prevent the occurrence of measurement errors due to temperature fluctuations.

Further, according to the fifth aspect of the present invention, when an external pressure is applied, a dynamic pressure is not applied to the optical fiber cable, but a meandering shape is formed inside the bag body filled with the viscous liquid so as to apply the hydrostatic pressure. An optical fiber roll is immersed and arranged so that stress is applied uniformly to the outer peripheral surface from the normal direction to reduce and change the cross-sectional area uniformly, and to convert the change into the change in the length direction. Therefore, it is possible to measure the phase change smoothly.

According to the sixth aspect of the present invention, since the optical fiber roll for measurement and the optical fiber roll for reference are arranged side by side on the same rigid plate, both optical fiber rolls are placed in the same atmosphere. As a result, measurement accuracy can be improved.

[Brief description of the drawings]

FIG. 1 is a view showing a first embodiment of a seismometer for measuring acceleration in two horizontal directions according to the present invention, in which a part 4 of a load body 1 formed of a rectangular hollow body is cut out, and Separation,
FIG. 4 is an overall perspective view showing the internal state of the device when it is retracted.

FIG. 2 is a view of the load body 1 of the seismometer in FIG. 1 viewed from the direction of arrow A.

FIG. 3A is an optical fiber roll 8A shown in FIG.
FIG. 3B is a side view of the optical fiber roll 8A viewed from the direction of the arrow A ′ while the mold of the optical fiber sensor shown in FIG. 3A is seen through from the direction of the arrow A ′, and FIG. 4A is a plan view of a force sensor 8 in which a plurality of cylindrical optical fiber rolls 8A are arranged on a rigid plate 8B, and FIG. FIG.

FIG. 4 is a measurement circuit diagram for measuring two horizontal components shown in FIG.

FIG. 5 shows a second embodiment of a seismometer according to the present invention for measuring acceleration in XYZ three directions.
FIG. 1 is an overall perspective view of a seismometer showing a part 23 of one of the seismometers cut away and retracted in the direction of an arrow while removing a sensor in a Y direction.

6 is a diagram in which a sensor in a Z direction is removed from an arrow B direction in FIG. 5 and a seismograph that measures acceleration in the XY directions is viewed.

FIG. 7 is a view of a seismometer that detects acceleration in the Z direction from the direction of arrow C in FIG. 5;

8 is a measurement circuit diagram used in a second embodiment of the seismometer of the present invention shown in FIG.

FIG. 9 shows a third embodiment of the seismometer of the present invention for measuring acceleration in XYZ three directions, in which two horizontal (XY) directions are arranged around a vertical (Z) direction accelerometer 60 in a grid pattern. 1 is an overall perspective view of a seismometer 40 to which the accelerometers 40, 40A, 50, 50A of FIG.

10 is a perspective view of the X-direction accelerometer 40 showing the internal state of the seismometer shown in FIG. 9 by removing two side walls 51A and 51B.

FIG. 11 shows a second example of the seismometer shown in FIG.
It is the perspective view of the Y direction accelerometer 50 which removes side wall surfaces 51A and 51B and shows the internal state.

FIG. 12 shows the seismograph shown in FIG.
It is the perspective view of the Z direction accelerometer 60 which removes side wall surfaces 61A: 61B and shows the internal state.

FIG. 13 is a measurement circuit diagram used for the seismometer shown in FIG.

FIG. 14 is a configuration diagram of an earthquake observation system in which the seismometer of the present invention is installed in a borehole drilled in the ground.

FIG. 15 (A) is a plan view of a force sensor in which a meandering optical fiber cable is disposed inside a bag-like body in which a viscous liquid is sealed, and FIG. 15 (B) is a view showing the force sensor shown in the above (A). (C) is a cross-sectional view of the cross-section cut along the cutting line MM shown in (A) and seen through the bag from the direction of arrow P, in which the shape of the meandering optical fiber cable is simplified. is there.

FIG. 16 is a plan view in which a measurement optical fiber roll and a reference light optical fiber roll are arranged on the same rigid plate and placed under the same atmosphere in order to improve measurement accuracy.

FIG. 17 is a diagram showing a conventional three-way seismometer, and FIG.
Fig. 4B is a view of the accelerometer having the pressing members and the like in four horizontal directions viewed from above, from which the pressing members and the like in the vertical direction have been removed. A fiber optic roll on its remaining surface,
FIG. 3 is an exploded perspective view in which a pressing plate is omitted.

[Explanation of symbols]

1, 21 ... square hollow load body, 2 ... square tubular load body, 3, 22 ... square solid load body, 5A to 12A ...
Optical fiber roll, 5 to 12: Force sensor, 13: End face of solid load bodies 3 and 22, 21A to 29A: Optical fiber roll, 21 to 29: Force sensor, 40, 40A ...
X-direction accelerometer, 50, 50A... Y-direction accelerometer, 60
... vertical accelerometer.

Claims (6)

[Claims] 1. A solid rectangular column-shaped load body is disposed inside a hollow cylindrical column-shaped load body with a gap interposed between the hollow rectangular column-shaped load bodies, and further with a gap interposed therebetween. Four gaps where the hollow load body and the cylindrical load body face each other, and face the four gaps with the cylindrical load body interposed therebetween, and the cylindrical load body and the solid load body face each other. And the four gaps to the rigid plate, the light propagation characteristics are displaced in light transmission phase in response to the pressure change due to the relative displacement of the load body based on the application of acceleration, and more than the load body and the rigid plate A plurality of force sensors each having a cylindrical or meandering optical fiber roll having a small elastic constant are stacked and arranged, and the force sensors are arranged so as to face each of four orthogonal horizontal (XY) directions. A seismometer, in which the load body is displaced relative to two directions In each direction, the output light of the optical fiber roll of the force sensor in each direction, the combined phase displacement light obtained by adding and averaging at the exit side of the optical fiber roll, and the phase difference output between the reference light, respectively, based on the difference of the phase difference output A seismometer for two-component measurement, further comprising a measurement circuit for determining an applied acceleration in a displacement direction of the solid load body. 2. A solid rectangular columnar load body is disposed inside a hollow rectangular columnar load body with a gap interposed therebetween, and each of six opposed gaps between the hollow loader and the solid loader is provided. In addition, the rigid plate has a light propagation characteristic in which the light transmission phase is displaced in response to a pressure change due to the relative displacement of the load based on acceleration application, and has a smaller elastic constant than the load and the rigid plate. A plurality of force sensors each having a cylindrical or meandering optical fiber roll are disposed in a stack, and the force sensors are arranged so as to face the horizontal (XY) four directions and the vertical (Z) two directions of the coordinate system. A combined phase displacement light obtained by averaging output light from the optical fiber roll of the force sensor in each of two directions in which the load body is relatively displaced at an exit side of the optical fiber roll, and a reference. Phase difference output with light A measuring circuit for calculating an applied acceleration in a displacement direction of the solid load body based on a difference in phase difference output in each of the two relative displacement directions. Total. 3. In an XYZ rectangular coordinate system, a solid rectangular columnar load is placed in a vertical long axis direction in an inner space of a hollow rectangular columnar load of a Z-direction accelerometer disposed so as to face two vertical directions. Displaceably disposed, the light transmission characteristics of the rigid plate toward the both end surfaces in the displacement direction of the solid load body react with pressure changes due to the relative displacement of the load body due to the application of acceleration. Displaced, and a stack of force sensors provided with a cylindrical or meandering optical fiber roll having an elastic constant smaller than that of the load body and the rigid plate, and a horizontal arrangement of the outer peripheral surface of the Z-direction accelerometer. In the X direction,
A pair of X-direction accelerometers for detecting acceleration in the X direction are provided, and a pair of Y-direction accelerometers for detecting acceleration in the Y direction are provided toward the horizontal Y direction of the outer peripheral surface. In the internal space of the meter, a solid rectangular column-shaped load body is disposed so as to be displaceable in the horizontal long axis direction, and light is transmitted to the rigid plate in the long axis direction of both end faces in the displacement direction of the solid load body. Cylindrical or meandering optical fiber rolls whose characteristics are such that the transmission phase of light is displaced in response to a pressure change due to the relative displacement of the load due to the application of acceleration, and has a smaller elastic constant than the load and the rigid plate. A solid rectangular columnar load body is disposed in the Y-direction accelerometer inside the space so as to be displaceable in the horizontal long axis direction, and the displacement of the solid load body is provided. The light propagation characteristics of the rigid plate The transmission phase of light is displaced in response to the pressure change due to the relative displacement of the load body due to speed application, and a cylindrical or meandering optical fiber roll having an elastic constant smaller than that of the load body and the rigid plate is provided. A force sensor disposed on one end face of each of the solid load bodies of the pair of X-direction accelerometers, the output light of the optical fiber roll of the force sensor being provided at an exit of the optical fiber roll. Each of the combined phase displacement light obtained by averaging on the side, the recombined value obtained by further averaging and the phase difference output of the reference light, and the output of the force sensor provided on the other end face of each solid load body. Each of the combined phase displacement lights obtained by adding and averaging the output light of the optical fiber roll at the exit side of the optical fiber roll is further added and averaged, and the recombined value and the phase difference output of the reference light are respectively obtained. The applied acceleration in the X direction is measured based on the difference between the phase difference outputs, and the output light of the optical fiber roll of the force sensor installed on one end face of each solid load body of the pair of Y direction accelerometers. Each of the combined phase displacement light obtained by averaging at the outlet side of the optical fiber roll is further added and averaged, and the re-combined value and the phase difference output of the reference light are output to the other end face of each of the solid load bodies. Each of the combined phase displacement lights obtained by adding and averaging the output light of the optical fiber roll of the opposed force sensor at the exit side of the optical fiber roll is further added and averaged, and the recombined value and the phase difference output of the reference light are calculated. Each of them is obtained and the applied acceleration in the Y direction is measured based on the difference between the phase difference outputs. The output of the optical fiber rolls of the force sensors respectively opposed to both end faces of the solid load body of the Z direction accelerometer is obtained. A measuring circuit is provided for calculating a phase difference output between the combined phase displacement light obtained by adding and averaging the light at the exit side of the optical fiber roll and the reference light, and measuring the Z-direction acceleration based on the difference between the phase difference outputs. A seismometer for three-component measurement characterized by the following. 4. A storage container arranged on the bottom of a borehole drilled in the ground to store seismometers for measuring acceleration in four horizontal directions and acceleration in two vertical directions. The seismometer according to claim 2 or 3, wherein the effect of temperature fluctuation on the optical fiber roll in the storage container is eliminated. 5. The meandering optical fiber roll is immersed and disposed inside a bag filled with a viscous liquid, and the pressure applied from the outside to the internal optical fiber roll with the bag interposed therebetween is: The viscous liquid inside the bag body does not apply a dynamic pressure, and while maintaining the hydrostatic pressure, applies a uniform normal stress to the outer peripheral surface of the optical fiber roll to uniformly reduce the cross-sectional area thereof. The seismometer according to any one of claims 1 to 3, wherein the seismometer converts the change into an axial length change of the optical fiber roll. 6. The meandering optical fiber roll is immersed and disposed inside a bag filled with a viscous liquid, and the pressure applied to the internal optical fiber roll through the bag from the outside is: The viscous liquid inside the bag body does not apply a dynamic pressure, and while maintaining the hydrostatic pressure, applies a uniform normal stress to the outer peripheral surface of the optical fiber roll to uniformly reduce the cross-sectional area thereof. The optical fiber roll is formed so as to convert to a change in the axial length of the optical fiber roll, and the optical fiber roll is used as a measurement optical fiber roll. 4. The method according to claim 1, wherein the measurement optical fiber roll and the reference optical fiber roll are arranged side by side on the rigid plate. Seismometer according to one.