JP2001188012A - Camera and lens with laser and gyro device - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a camera and a lens with a laser and a gyro device capable of detecting a rotation direction. SOLUTION: A ring laser typed gyro comprises a first laser 1200 emitting a first laser beam rounding to one direction as a main mode and a second laser 1202 emitting a second laser beam rounding to one direction as a main mode. The gyro takes an electric signal from at least either the first or the second laser, where a first laser beam 1206 and a second laser beam 1207 have different transmitting frequencies and interfere each other.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a camera and a lens provided with a laser device and a gyro.

[0002]

2. Description of the Related Art Conventionally, as a gyro for detecting an angular velocity of a moving object, a mechanical gyro having a rotor and a vibrator and an optical gyro are known. In particular, optical gyros are being revolutionized in the gyro technical field because they can be activated instantaneously and have a wide dynamic range. The optical gyro includes a ring laser gyro, an optical fiber gyro, a passive ring resonator gyro, and the like.

[0003] Among them, the ring laser type gyro using a gas laser has been developed first, and has already been put to practical use in aircraft and the like.

Recently, a semiconductor laser gyro integrated on a semiconductor substrate has been proposed as a small, high-precision ring laser type gyro.
There is 288556.

According to the above publication, as shown in FIG. 69, a ring-shaped gain waveguide 5711 is formed on a semiconductor substrate 5710 having a pn junction.
Carriers are injected into the electrode 11 from the electrode 5722 to cause laser oscillation. Then, a part of each of the laser light propagating in the clockwise direction and the counterclockwise direction in the gain waveguide 5711 is extracted and made to interfere in the light absorption region 5717, and the intensity of the interference light is extracted as a photocurrent from the electrode 5723. I have. 5716 is CCW light, 5715 is CW
Light, 5719 and 5718 are output lights.

Further, Japanese Patent Application Laid-Open No. 57-43486 (U.S. Pat.
SP4, 431, 308) describes a gyro utilizing the fact that the terminal voltage of the semiconductor laser element changes with rotation without extracting light to the outside of the semiconductor laser element. In FIG. 56, the semiconductor laser element 5792 has electrodes 5790 and 5791 on the upper and lower sides. Reference numeral 5793 denotes a DC blocking capacitor, 5794 denotes an output terminal, and 5795 denotes a resistor.

As shown in FIG. 70, a semiconductor laser element is connected to a driving power supply 5796 as a laser element of a ring laser device, and clockwise and counterclockwise frequencies of light generated when a certain angular velocity is applied to the device. It describes that a difference (beat frequency) is detected as a difference between terminal voltages of the laser elements.

Japanese Patent Application Laid-Open No. 4-174317 discloses that a change in terminal voltage of a laser element caused by rotation is detected.

However, none of the above publications can detect the rotation direction of an object. This is because if the angular velocity is the same even if the rotation direction is different, the beat frequency will be the same.

[0010]

However, in the conventional ring laser type gyro, the rotation direction cannot be detected. For this reason, dither (micro vibration) is applied, and the rotation direction is determined from the correlation between the dither direction and the signal.

In the ring laser type gyro, the oscillation frequency is separated into two with rotation. However, when the rotational speed is small, the difference between the oscillation frequencies becomes small.

In this case, a lock-in phenomenon occurs in which the oscillation frequency is pulled into one mode due to the nonlinearity of the medium.

In order to cancel the lock-in phenomenon, the above-mentioned dither is applied to a ring laser type gyro.

Accordingly, an object of the present invention is to provide a camera and a lens provided with a laser device and a gyro.

In particular, the gyro is a ring laser gyro that can detect the direction of rotation even without a mechanical mechanism such as dither (micro vibration).

[0016]

According to the present invention, there is provided a camera comprising: a first laser which generates a first laser beam circling in one direction as a main mode; A laser device arranged so that the first and second laser beams interfere with a second laser beam having a second laser beam having an oscillation frequency different from that of the first laser beam as a main mode, and A gyro including an electric signal detecting means for extracting an electric signal from at least one of the first and second lasers is provided.

In the lens according to the present invention, the first laser beam that circulates in one direction and has the oscillation frequency different from that of the first laser beam that circulates in one direction is generated. A laser device arranged so that the first and second laser beams interfere with a second laser that generates a second laser beam as a main mode, and at least one of the first and second lasers A gyro including an electric signal detecting means for extracting an electric signal is provided.

The gyro is a first laser which generates a first laser beam circling in one direction as a main mode,
A gyro for generating an electric signal from at least one of the first and second lasers, comprising a second laser that generates a second laser beam circulating in one direction as a main mode. The oscillation frequency of the light is different from the oscillation frequency of the second laser light, and the first laser light and the second laser light interfere with each other.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first optical waveguide and the second optical waveguide are provided. At least a part of the second optical waveguide is disposed close to the second optical waveguide.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least one of the first and second optical waveguides is provided. A third optical waveguide optically coupled to the portion.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least one of the first and second optical waveguides is provided. A third optical waveguide connected to the portion.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least one of the first and second optical waveguides is provided. The units are shared.

Further, the gyro includes the first and second gyros.
The circling directions of the laser beams are opposite to each other.

Further, the gyro includes the first and second gyros.
Are characterized in that the circling directions of the laser beams are the same.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and the first and second optical waveguides are asymmetric. Characterized in that the tapered region is provided.

In the gyro, the tapered region includes a first tapered portion and a second tapered portion,
An angle between one of the first and second tapered portions and the optical waveguide portion having a constant width is 90 degrees.

In the gyro, the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and the first and second optical waveguides respectively have An optical element is provided, and the optical element is characterized in that a transmission loss for laser light circulating in one direction is different from a transmission loss for laser light circulating in another direction.

The first laser is driven at a constant voltage, and the second laser is driven at a constant current.

The gyro is a first laser that generates a first laser beam circling in one direction as a main mode,
And a gyro including a second laser that generates a second laser beam circling in one direction as a main mode,
The first laser has a first optical waveguide, the second laser has a second optical waveguide, respectively, and a third optically coupled to at least a portion of the first and second optical waveguides. Characterized in that the optical waveguide is provided.

The gyro includes a first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circulating in one direction as a main mode. A gyro comprising a laser, wherein the first laser has a first optical waveguide, the second laser has a second optical waveguide, and at least a portion of the first and second optical waveguides. And a third optical waveguide connected to the third optical waveguide.

Further, the gyro includes a first laser that generates a first laser beam orbiting in one direction as a main mode, and a second laser that generates a second laser beam orbiting in one direction as a main mode. Wherein the first laser has a first optical waveguide, the second laser has a second optical waveguide, and the first laser has a first optical waveguide.
And at least part of the second optical waveguide.

The gyro includes a first laser that generates a first laser beam circling in one direction as a main mode,
A gyro having a second laser that circulates in one direction and generates a second laser beam as a main mode, and a gyro having beat signal detection means, wherein the oscillation frequency of the first laser beam and the second laser beam is The first laser light and the second laser light interfere with each other.

The beat signal detecting means converts a voltage signal applied to the first or second laser, a current signal flowing through the first or second laser, or an impedance signal of the first or second laser device. To detect.

The first or second laser has an electric terminal for extracting the beat signal.

[0035] The beat signal detecting means includes a photodetector provided outside the first and second lasers.

The gyro is a first laser that generates a first laser beam circling in one direction as a main mode,
A gyro having a second laser that generates a second laser beam circling in one direction as a main mode, and a photodetector that receives the first and second laser beams; The oscillation frequencies of the laser light and the second laser light are different from each other, and the first laser light and the second laser light interfere with each other.

The above-mentioned laser device comprises a first laser generating a first laser beam circulating in one direction as a main mode, and a second laser generating a second laser beam circulating in one direction as a main mode. Wherein the first laser light and the second laser light have different oscillation frequencies, and the first laser light and the second laser light interfere with each other. .

[0038]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Prior to the description of the embodiments of the present invention, first, the operation principle of a gyro related to the present invention will be described with reference to FIGS.

In the present invention, a laser that generates laser light circulating in one direction as a main mode is a laser that generates only laser light circulating in an optical waveguide in one direction, or a laser that generates only laser light circulating in one direction in an optical waveguide. A laser in which the intensity of the laser light circulating in one direction is much greater than the intensity of the laser light circulating in the other direction.

The SN ratio of a signal detected from the gyro according to the present invention is affected by the intensity ratio between the main mode laser beam circling in one direction and the sub mode laser beam circulating in the other direction. .

Therefore, in the present invention, it is preferable to generate only the main mode laser light.

Of course, if the SN ratio of the signal detected by the gyro can be secured to a sufficient value,
A sub mode laser beam may be generated.

The ring-shaped waveguides 602 and 6 shown in FIG.
Consider a laser with 03.

Now, as shown in FIG. 66, the laser beam 606 as the main mode of the first laser 600 circulates clockwise (CW) and its wavelength is λ ₁ . Also, the second
Light 607 as the main mode of the laser 601
Orbits counterclockwise (CCW) and changes its wavelength to λ ₂ (<
λ ₁ ).

Here, when the laser device 625 itself is rotated clockwise, the first laser beam 60 clockwise is rotated.
The oscillation frequency f ₁ of _No. 6 is reduced by Δf ₁ shown in Expression 1 as compared with the oscillation frequency f ₁₀ at the time of non-rotation.

[0046]

(Equation 1) Here, S ₁ is a closed area surrounded by the optical path of the first laser, L
₁ is the optical path length of the first laser, and Ω is the angular velocity of rotation.

On the other hand, the counterclockwise second laser beam 60
The oscillating frequency f ₂ of No. 7 is increased by Δf ₂ shown in Expression 2 as compared with the oscillating frequency f ₂₀ during non-rotation.

[0048]

(Equation 2) Here, S ₂ is a closed area surrounded by the optical path of the second laser, L
₂ is the optical path length of the second laser.

At this time, if the first laser 600 and the second laser 601 are arranged close to each other, the first laser light 606 propagating in the first laser is coupled to the second laser light 607. I do.

At the same time, the second laser propagating in the second laser
Are coupled to the first laser.

For this reason, both laser beams coexist in each of the first laser 600 and the second laser 601. Therefore, the two laser lights interfere with each other, and a difference between the oscillation frequencies of the first laser light 606 and the second laser light 607, that is, a beat light represented by Expression 3, is generated.

[0052]

(Equation 3) On the other hand, when the laser device 625 rotates counterclockwise, beat light having a frequency represented by Expression 4 is generated.

[0053]

(Equation 4) If there are two or more oscillation modes in the laser, the population inversion shows a time variation corresponding to the difference between the oscillation frequencies of the modes.

This phenomenon is known as a population inversion pulsation. In the case of a laser that flows an electric current, such as a gas laser or a semiconductor laser, there is a one-to-one correspondence between the population inversion and the impedance of the laser.

Then, when light interferes in the laser,
The population inversion changes accordingly, and consequently the impedance between the electrodes of the laser changes.

The state of this change appears as a change in the current flowing through the laser if a constant voltage source is used as the driving power supply. If a constant current source is used, the state of light interference can be extracted as a signal as a change in voltage applied to the laser.

Of course, a change in impedance can be directly measured by an impedance meter.

Therefore, by detecting a change in laser current, voltage or impedance as in the present invention,
A beat signal corresponding to the rotation can be extracted.

Further, according to the present invention, the beat frequency increases or decreases in accordance with the direction of rotation, as shown in equations (3) and (4).

Therefore, the rotation direction can be detected by observing the increase / decrease of the beat frequency from the non-rotation time.

If (f ₂ −f ₁ ) satisfies the expression (5), it is possible to detect not only the rotation direction but also the angular velocity accurately. In other words, if the sign of the beat frequency is always the same (however, in the description, the sign is positive and may be reversed, of course) and its absolute value changes depending on the rotation direction, the rotation direction and the angular velocity can be accurately determined. Detection is possible.

[0062]

(Equation 5) Next, consider a case where the first laser light and the second laser light have the same circling direction (FIG. 67). For example, the first
Light 606 as the main mode of the laser 600 of FIG.
Orbits clockwise, and its wavelength is λ ₁ . Also, the second
Laser light 608 as the main mode of laser 601
Also rotates clockwise, and its wavelength is set to λ ₂ . However,
λ ₁ > λ ₂ . When rotating the laser device 625 itself clockwise, the oscillation frequency f ₁ of the first laser light
It is reduced by the formula (6) in comparison to the oscillation frequency f ₁₀ during non-rotation.

[0063]

(Equation 6) Here, S ₁ is a closed area surrounded by the optical path of the first laser, L
₁ is the optical path length of the first laser, and Ω is the angular velocity of rotation. Further, the oscillation frequency f ₂ of the second laser beam is also decreased by the formula (7) in comparison to the oscillation frequency f ₂₀ during non-rotation.

[0064]

(Equation 7) Here, S ₂ is a closed area surrounded by the optical path of the second laser, L
₂ is the optical path length of the second laser.

At this time, when the first laser 600 and the second laser 601 are arranged close to each other, the first laser light propagating in the first laser is coupled to the second laser. At the same time, a second laser propagating in the second laser
Are coupled to the first laser.

For this reason, the first laser beam and the second laser beam coexist in each of the first laser and the second laser. Therefore, the two laser beams interfere with each other, and the difference between the oscillation frequencies of the two laser beams, that is, equation (8)
The beat light shown in FIG.

[0067]

(Equation 8) On the other hand, when the laser device itself rotates counterclockwise, the oscillation frequency increases, and beat light having the frequency shown in Expression (9) is generated.

[0068]

(Equation 9) Also in this case, the population inversion shows a time variation according to these beat frequencies.

As a result, the impedance between the electrodes of the laser changes.

Further, as shown in equations (8) and (9), the beat frequency increases and decreases in accordance with the rotation direction. Therefore, by observing the increase and decrease of the beat frequency from the time of non-rotation, the rotation direction is detected. can do.

If the oscillation wavelengths of the first laser light and the second laser light are equal, equation (10) holds, and the beat frequency f ₂ -f ₁ takes a positive or negative value.

[0072]

(Equation 10) If the absolute values of the beat frequencies are equal, the same signal is output from the terminal for extracting the voltage signal related to the laser device, so that the rotation direction cannot be detected. In contrast, in the present invention,
The rotation direction can be detected from the change in the absolute value of (f ₂ −f ₁ ). If equation (5) is satisfied, particularly accurate angular velocity,
The direction of rotation can be detected.

Instead of detecting the beat frequency from the voltage applied to the laser, the current flowing through the laser, or a change in the impedance of the laser, the beat frequency may be detected using an externally provided detector.

More specifically, the first laser light and the second laser light are taken out of the laser.

When these laser beams are received by the photodetector at the same time, the first laser beam and the second laser beam interfere with each other in the photodetector, and beats corresponding to the difference between the oscillating frequencies are generated. Light is generated.

As a result, a beat signal can be detected from the electric terminal of the photodetector.

In order for the laser light propagating in one direction in the laser to exist in the main mode, it is necessary to apply a loss to the light propagating in the direction opposite to the one direction. Good.

For example, by providing a tapered portion in a part of the optical waveguide, light incident on the tapered portion can be reduced.
Total reflection condition shifts.

For this reason, a mirror loss occurs for the light incident on the tapered portion. Specifically, since the angle of incidence on the tapered portion varies depending on the direction in which the light circulates, the loss is large for laser light circulating in a certain direction, and the loss is small for light circulating in the opposite direction. Can be. By designing the mirror loss to be sufficiently large, laser oscillation can be suppressed.

In this way, it is possible to realize a laser in which laser light propagating in one direction in a circular manner exists as a main mode.

In the present invention, the tapered portion is formed, for example, as a portion in which the width of the optical waveguide gradually increases along one direction of the propagation direction of the laser light. in this case,
The shape of the tapered portion in a plane parallel to the plane including the propagation path of the circulating laser light has a sawtooth shape.

In place of or together with the provision of the tapered portion in a part of the optical waveguide, an optical element such as an optical isolator may be inserted in the optical path.

An optical isolator transmits light having a certain polarization direction in only one direction. Therefore,
By inserting an optical isolator, a ring laser can be created in which the light that propagates in one direction exists as the main mode when the light that circulates in the opposite direction is the same as a normal laser. Can be. Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

Further, in the optical gyro according to the present invention, the injection currents of the first laser and the second laser are made different so that the oscillation frequencies or wavelengths of the first laser and the second laser are different. You may let it.

In the above structure, the first laser,
Assuming that the optical path lengths of the second laser are L ₁ and L ₂ , respectively, there is a relationship as shown in Expression (11) between the oscillation wavelengths of the first laser and the second laser.

[0086]

[Equation 11] Here, m ₁ and m ₂ are positive integers. Positive integer m ₁ ,
When m ₂ is equal, the oscillation wavelengths of the two lasers can be changed if the optical path lengths are different. Since the oscillation frequency is proportional to the reciprocal of the oscillation wavelength, the oscillation frequency also differs. Since the optical path length is given by the product of the equivalent refractive index and the distance over which the light propagates, by changing the equivalent refractive index or the length of the optical waveguide in the first laser and the second laser, these two are obtained. The difference in the optical path length of the laser can be provided.

As a method of changing the refractive index of the optical waveguide, one method is to change the injection current to these two lasers. In the case of a semiconductor laser, depending on the injection current,
The free carrier plasma effect (free carrier plasma effect) is within a range where the effect of the heat generation can be ignored.
effect), the refractive index decreases.

On the other hand, in a region where heat generation is dominant, the refractive index increases. In any case, the refractive index can be changed by controlling the value of the injection current, and the equivalent refractive index of the optical waveguide changes. As a result, the optical path length changes.

Now, the oscillation frequency f _i and the photon number density S
_i (i = 1, 2), Equation (12) and Equation (1)
It is known that there is a relationship as in 3).

[0090]

(Equation 12)

[0091]

(Equation 13) Here, Φ _i is the phase, Ω _i is the resonance angular frequency, σ _i is a coefficient representing the pull-in of the mode, ρ _i is a coefficient representing the self-extrusion of the mode, and τ _ij is a coefficient representing the mutual extrusion of the mode. Here, i = 1, 2; j = 1, 2; i ≠ j.

Here, if the shape of the optical waveguide is determined, the expression (1)
2) _{(13) Ω i, σ i} , ρ i, τ i j is a constant.

If there is no mode jump during laser oscillation, dΦ _i / dt = 0 is considered.

Therefore, it is derived from the equations (12) and (13) that f ₁ ≠ f ₂ when S ₁ ≠ S ₂ .

Since the photon number density S _i (i = 1, 2) changes according to the injection current value to the laser, the equations (12) and (13) are obtained by making the injection current values to the two lasers different. , A difference can be given to the oscillation frequency. This phenomenon applies not only to semiconductor lasers but also to gas lasers.

To change the equivalent refractive index of the optical waveguide, at least two of the width of the optical waveguide, the size of the medium contributing to the equivalent refractive index, the material of the medium, and the composition of the medium are used in the two lasers. It suffices if one is different.

Further, in the two lasers, if the material of the medium or the composition of the medium is different,
Since the peak wavelengths of the gains are different, the oscillation wavelengths of the two lasers can be changed. This is because there are many resonance modes in the optical resonator, and the wavelength closest to the gain peak is selectively amplified, leading to laser oscillation.

In the present invention, an electric signal oscillating at a beat frequency corresponding to the angular velocity of rotation is observed from a terminal provided on the laser itself or an external photodetector for extracting the electric signal.

Here, when the gyro provided with the first and second lasers is stationary, the obtained electric signal changes to any signal due to clockwise rotation or counterclockwise rotation. (FIG. 1A)
(C)).

In the gyro, the first laser generates a laser beam (CW light) circulating clockwise as a main mode, the wavelength is λ _1, and the second laser circulates counterclockwise. Laser light (CCW light) is generated as a main mode, and its wavelength is set to λ ₂ (<λ ₁ ).

An electric signal (for example, a voltage signal applied to the first laser) obtained when the gyro is stationary is shown in FIG.
It is shown in (A).

The period of the electric signal is assumed to be tA.

The period tA is the reciprocal of the oscillating frequency of the first laser light and the second laser light at rest (formula (3) above).
(F ₂₀ −f ₁₀ ) ⁻¹ ).

Now, when the gyro rotates clockwise,
The beat frequency, that is, (f ₂ −f ₁ ) is calculated by the above equation (3).
, It becomes larger. Therefore, the period tB of the electric signal is
It becomes smaller as shown in FIG.

On the other hand, when the gyro rotates counterclockwise, the beat frequency decreases according to equation (4). Therefore, the period tC of the electric signal increases as shown in FIG.

As described above, the direction of rotation can be determined from the magnitude relationship between the beat frequency when the gyro is stationary and the beat frequency when the gyro is rotated.

Further, the angular velocity can be detected from the difference between the beat frequencies when stationary and when rotating.

The beat frequency is proportional to the rotation angular velocity. Therefore, for example, the voltage value can be converted to an angular velocity by converting the electric signal into a voltage magnitude by a frequency-voltage conversion circuit and obtaining a relationship between the rotation speed and the voltage in advance. The principle of operation of the gyro according to the present invention has been described above.

An embodiment of the present invention will be described below with reference to the drawings.

[First Embodiment] A gyro according to a first embodiment of the present invention is a first laser that generates a first laser beam circulating in one direction as a main mode, and circulates in one direction. A gyro that includes a second laser that generates a second laser beam as a main mode, and extracts an electric signal from at least one of the first and second lasers. An oscillation frequency of the laser light is different from that of the laser light, and the first laser light and the second laser light interfere with each other.

In order to cause the first laser light and the second laser light having different oscillation frequencies to interfere with each other, the first and second lasers respectively include the first and second optical waveguides as follows. Configure.

That is, at least a part of the first and second optical waveguides are arranged close to each other, or the first and second optical waveguides are
A third optical waveguide connecting at least a part of the first optical waveguide, a third optical waveguide optically coupled to the first and second optical waveguides, a first optical waveguide, and a third optical waveguide. The gyro is configured to share at least a part of the optical waveguide.

Next, a method of causing the main mode lights of the first laser and the second laser to interfere with each other will be described.

<1> When the first and second lasers are arranged close to each other (FIGS. 2 and 3) As shown in FIG. 2A, the first optical waveguide 1202 of the first laser 1200 is The second laser 1201 and the second optical waveguide 1203 are arranged close to each other.

In FIG. 2A, reference numerals 1204 and 1205 denote tapered regions for generating main mode light circling in one direction.

Note that 1206 is CCW light, and 1207 is CW light.
5 shows W light.

The close arrangement means that at least a part of the optical waveguides of the first laser and the second laser are brought close to each other. By doing so, the main mode light 1206 circulating in the first laser 1200 is optically coupled to the second optical waveguide 1203, and propagates in the second laser.

On the other hand, the main mode light 1207 circulating in the second laser 1201 is optically coupled to the first optical waveguide 1202 and propagates in the first laser. That is, if the oscillation frequencies of the two main mode lights are different from each other, laser lights having two kinds of oscillation frequencies coexist in one laser.

Note that the close arrangement refers to shortening the distance 1 in FIG. 2 (A).

Specifically, the C of the first laser 1200
CW light 1206 and CW light 12 of second laser 1201
07, at least a part of the optical waveguide of another laser is arranged within the seeping distance of the laser light of at least one laser.

Of course, at least a part of the optical waveguide of the other laser may be arranged within the seeping distance of both laser beams.

Although the optical waveguides of the lasers arranged close to each other are not necessarily parallel, the second laser light 1207 is optically transmitted to the optical waveguide 1202 of the first laser 1200. For efficient coupling, it is preferable that the first and second optical waveguide portions arranged close to each other are parallel to each other.

The proximity method is not limited to FIG. 2A, but the first optical waveguide 12 as shown in FIG. 2B.
A second optical waveguide 1203 may be provided inside 02.
In this case, the directions of the first and second laser beams propagating through the first and second optical waveguides are unified. FIG.
As shown in FIG. 3C and FIG. 3D, even in the case of a gas laser, the first and second lasers 1200 and 1201 are used.
Can be placed in close proximity. In the figure, 1214 and 1215 are mirrors (reflection surfaces), and 1210 and 1211 are anodes. Reference numerals 1216 and 1217 denote terminals for extracting an electric signal generated by the rotation. 1212 and 1213
Is a cathode. 1218 and 1219 are optical elements such as optical isolators. In the drawing, terminals for extracting electric signals are provided for both lasers, but of course only one terminal may be provided. Note that not only the arrangement shown in FIG. 2A but also the first and second lasers 1200 and 1201 may be arranged to be shifted as shown in FIG.

It is preferable that the optical waveguide of the laser has a total reflection surface, and it is particularly preferable that the ring laser is constituted only by the total reflection surface in order to reduce the oscillation threshold.

<2> When providing a third optical waveguide that optically couples at least a part of the first optical waveguide and the second optical waveguide, as shown in FIG. And a third optical waveguide 1320 that is close to a part of the second optical waveguide 1303 of the second laser 1301 and a part of the first optical waveguide 1302 of the second laser 1301, respectively, and is optically connected. The first laser 1300 and the second laser 1301 sandwich the third optical waveguide 1320. In the figure, reference numeral 1306 denotes CCW light oscillating as main mode light,
Reference numeral 7 denotes CW light that oscillates as main mode light.

The CCW light 1306 of the first laser 1300 is optically coupled to the second laser 1301 via the third optical waveguide 1302.

Then, a change in the electric signal accompanying the rotation is extracted from the second laser, and the direction of rotation is detected.

The arrangement shown in FIG. 4B may be used. First
Laser 1300 and the second laser 1301 are the third
On the same side of the optical waveguide 1320. In FIG. 4B, 1
302 is a first waveguide, 1303 is a second waveguide, 13
20 is a third optical waveguide. In this case, it is necessary to make the circling directions of the main mode light coincide with each other.

FIGS. 5C and 5D show the case where a gas laser is used. 1310, 1312, 1313,
And 1311 are an anode or a cathode. Reference numeral 1317 denotes an electric terminal for extracting a change in an electric signal accompanying rotation.

Reference numerals 1318 and 1319 are optical elements such as the above-mentioned optical isolator.

In order to generate the main mode light of the first and second lasers, both lasers have a tapered region (1304, 1305) or an optical element (131).
8, 1319) may be provided.

As a matter of course, a tapered region may be used for one laser, and an optical element may be used for the other laser.

Note that the third optical waveguide 13 shown in FIGS.
20 can be formed by using quartz or by using a lithography technique used in a semiconductor process or the like.

<3> A case where a third optical waveguide for connecting at least a part of the first and second optical waveguides is provided.
14A, reference numeral 1400 denotes a first laser, 1404 denotes a tapered region, 1402 denotes a first optical waveguide, 1406 denotes CCW light which is a main mode, and 1407 denotes CW light which is a main mode.
Light 1420 is a third optical waveguide for connection. First
Laser 1400 and second laser 1401 sandwich third optical waveguide 1420.

By adopting such a configuration, the CCW light 1
406 generates a CW light 140 in the second laser 1401.
Coexists with 7.

Therefore, the direction and the angular velocity can be detected by extracting the change in the electric signal of the bioelectric signal accompanying the rotation from the second laser 1401.

The configuration shown in FIG. 6B can be adopted. First laser 1400 and second laser 1401
Are on the same side of the third optical waveguide 1420.

A gas laser can also be used as shown in FIGS. 1410, 141, 1411, 1
413 is an anode and a cathode. 1414 and 1
415 is a mirror, and 1411 is an electric terminal for extracting an electric signal.

<4> In the case where the gyro is configured to share at least part of the first and second optical waveguides. In FIG.
501 is a second laser, 1504 and 1505 are tapered regions, and 1520 is a common portion of an optical waveguide.

The main mode light 15 of the first laser 1500
06 propagates through the common unit 1520 and couples to the second laser. On the other hand, while the main mode light 1507 of the second laser 1501 propagates through the common unit 1520,
Couple to the first laser. Thus, in the first and second laser devices, laser beams having different oscillation frequencies coexist.

Accordingly, a beat frequency is generated even at rest, and
By reading the change of the electric signal due to the rotation, the rotation direction and the angular velocity can be detected.

Incidentally, one electric signal of the first or second laser may be detected. By using both signals, the accuracy of rotation detection is improved.

As shown in FIG. 8B, the first and second
It is also possible to make the circling direction of the main mode light of the laser beam the same. In this case, the first laser light 1506 and the second laser light 1509 coexist in the common unit 1520.

Of course, in the case of a gas laser as shown in FIGS. 9C and 9D, a part of the optical waveguide is shared so that laser beams having different oscillation frequencies coexist in one laser. Can be.

In the above <1> to <4>, the case where the shape of the laser is a quadrangle has been described. Of course, the shape of the laser is not limited to the quadrangle, but may be triangular, circular, or polygonal. Good.

In the above <1> to <4>, a laser having a ring-shaped optical waveguide has been described. Of course, if it is possible to generate a main mode light propagating in one circular direction, the laser shown in FIG. The waveguide 1202 without such a hollow portion may be used. 1205 is a tapered region, 1
206 is a main mode light.

(Tapered Region) Next, the shape of the tapered region for generating a laser beam circulating in one direction as a main mode will be specifically described.

In FIG. 10, reference numeral 1601 denotes an optical waveguide;
Reference numeral 606 indicates a tapered region.

If there is no tapered region 1606, both CW light 1608 and CCW light 1606 are generated.

However, the provision of the asymmetric tapered region causes a difference in optical loss between CW light and CCW light. The closer one angle β of the tapered portion is to 90 °, the more C
The light intensity of the W light decreases, and the CCW light becomes the main mode. Of course, when α = 90 °, the CW light is in the main mode.

In order to substantially rotate in only one direction, 80 ° ≦ β (or α) ≦ 100 °, preferably 8 °
3 ° ≦ β (or α) ≦ 97 °, more preferably 87 °
≤ β (or α) ≤ 93 °. Optimally, β (or α) = 90 °.

In particular, when β = 90 °, the oscillation mode changes stepwise at the starting point (1630 in the figure) of the tapered region, so that the coupling efficiency between the waveguide mode and the optical waveguide having a constant width decreases. Accordingly, the main mode light is easily generated. Considering the case where α <β, when β is in the above range, 2 ° ≦ α ≦ 10 °, preferably 3 ° ≦ α ≦
It is good to be 6 degrees.

The difference between the oscillation frequencies of the main mode light of the first laser and the main mode light of the second laser is 100 Hz or more, preferably 1 kHz, in order to avoid the lock-in phenomenon.
z or more, more preferably 10 kHz or more.

In order to change the oscillation frequency of the main mode lights, the materials constituting the lasers are changed, the magnitude of the current injected into each laser, the magnitude of the voltage applied to the laser is changed, or the like. Alternatively, it can be realized by changing the width or length of the optical waveguide.

When two laser beams having different oscillation frequencies coexist in one laser device, the two laser beams interfere with each other, and the beat frequency is detected as an electric signal.

The electric signal extracted from the laser device is a voltage signal when the device is driven by a constant current, and is a current signal when the device is driven by a constant voltage.

Further, the impedance signal of the laser device may be extracted.

The frequency of the voltage signal or the like thus extracted corresponds to the above-mentioned beat frequency. Therefore, by detecting the frequency change, it becomes possible to detect the angular velocity and the direction of the rotation received by the laser device.

The case where an electric signal is extracted from the laser device will be described. However, the present invention can be applied to a case where the rotation direction and / or the angular velocity is detected by a signal from a photodetector described in a second embodiment described later.

Hereinafter, means for detecting a change in voltage of the laser device as an electric signal will be described.

As shown in FIG. 11, a constant current source 1902 is prepared, and a semiconductor laser 1900 as a laser device is connected to the power supply via a resistor 1901. Then, an electric signal (a voltage signal in this case) of the semiconductor laser 1900 is read by the voltage detection circuit 1906.

It is preferable to provide a voltage follower circuit 1905 as a protection circuit as necessary as shown in FIG.

The semiconductor laser is described as an example, but the same goes for a gas laser.

In FIG. 12, the laser is driven at a constant current, and the change in the anode potential of the semiconductor laser 2000 is read.
FIG. 3 shows an example of a circuit diagram for performing rotation detection.

The anode of the semiconductor laser 2000 is connected to the output terminal of the operational amplifier 2010 via the protection resistor 2003, and the cathode of the semiconductor laser 2000 is connected to the inverting input terminal of the operational amplifier 2010.

The operational amplifier 2011 outputs a signal Vout in accordance with the input potential Vin from the microcomputer. Since this signal Vout has a beat frequency proportional to the angular velocity, the signal is converted into a voltage by a known frequency-voltage conversion circuit (FV conversion circuit) or the like, and rotation is detected.

FIG. 13 shows a frequency-voltage conversion circuit (F
-V conversion circuit). This circuit is composed of a transistor, a diode, a capacitor, and a resistor, and the output voltage _Vc2 is represented by Expression (14).

[0168]

[Equation 14] Here, Ei is a peak-to-peak value of the input voltage, and f is a beat frequency. _{C 2 >> C 1, R O} C 2 f <
By designing the circuit parameters to be 1, Vc2 as shown in Expression (15) is obtained, and a voltage output proportional to the beat frequency can be obtained.

[0169]

(Equation 15) Next, a case where rotation is detected by a change in current of the laser device will be described.

When a constant voltage source is used as the power supply, the angular velocity of rotation can be measured as a change in the current flowing through the semiconductor laser. As shown in FIGS. 14 and 15, the use of a battery as a constant voltage source leads to a reduction in size and weight of a drive system. In FIG. 14, an electric resistor 2201 is connected in series with the semiconductor laser 2200, and a current flowing through the semiconductor laser is measured as a change in voltage across the electric resistance. 2202 is a battery, (battery) and 2206 is a voltmeter. On the other hand, in FIG.
And an ammeter 2306 is connected in series to directly measure the current flowing through the semiconductor laser. 2301 is an electric resistance.

Next, another circuit configuration for detecting a beat signal will be described.

FIG. 16 shows an example of a circuit diagram in which the semiconductor laser is driven at a constant voltage, the change in the anode potential of the semiconductor laser 2400 is read, and the rotation is detected.

The anode of the semiconductor laser 2400 is connected via a resistor 2403 to the output terminal of an operational amplifier 2410, and the cathode of the laser 2400 is grounded to a reference potential.

When a constant voltage (Vin) is applied to the inverting input terminal of the operational amplifier 2410 from a microcomputer or the like, a constant voltage drive configuration in which the potential is constantly applied to the resistor 2403 and the laser 2400 is provided.

The electric resistance 2403 is connected to an operational amplifier 2411 for a buffer.

The operational amplifier 2411 outputs a signal Vout. Since this signal Vout has a beat frequency proportional to the angular velocity, a known frequency-voltage conversion circuit (F
-V conversion circuit) and the like to detect rotation. Of course, without passing through the operational amplifier 2411, the signal of the equipotential portion with the electric resistance 2403 may be directly input to the FV conversion circuit to detect the rotation. Further, a frequency counter can be used as the beat signal detecting means.

Next, FIG. 17 shows a case where the reference of the signal potential is grounded by using a subtraction circuit 2515 in addition to the configuration of the constant voltage drive circuit shown in FIG.

A constant potential V ₁ is applied to the inverting input terminal of the operational amplifier 2510 from a microcomputer or the like. 2500 is a laser,
2511 and 2512 are voltage followers, 2503,
2516 and 2519 are electric resistances,
17, 2518 and 2519 have the same resistance.

The potentials V ₁ and V at both ends of the electric resistance 2503
₂ is connected to an inverting input terminal and a non-inverting input terminal of the amplifier 2520 through voltage followers 2511 and 2512 and resistors 2516 and 2518. By doing so, the reference potential is grounded and the electric resistance 2
A change in voltage (V ₂ −V ₁ ) = V ₀ applied to 503 can be detected. That is, a change in current flowing through the laser 2500 can be detected.

The rotation of the obtained signal is detected through an FV conversion circuit or the like.

Also, regardless of the type of power supply, the semiconductor laser 2600 is directly measured by the impedance meter 2609.
Can be measured. 26
02 is a power supply. In this case, unlike the case where the terminal voltage or the current flowing through the element is measured, the influence of the noise of the driving power supply is reduced. This example is shown in FIG.

The semiconductor laser has been described above as an example, but the same applies to a gas laser. [Second Embodiment] In the first embodiment, the beat frequency is extracted as an electric signal from the one laser as a change in the voltage applied to the one laser and the change in the current signal flowing in the one laser. On the other hand, in the second embodiment, the change in the beat frequency, that is, the number of rotations and the direction of rotation are detected by using a photodetector in which two types of laser beams having different oscillation frequencies are arranged outside the laser. is there.

<1> A second embodiment will be described with reference to FIGS. 2 and 3 denote the same items.

In FIG. 19A and FIG.
Reference numeral 56 denotes output light of the main mode light 1206 of the first laser 1200. Reference numeral 1257 denotes output light of the main mode light 1207 of the second laser 1201. Reference numeral 1230 denotes a photodetector. Both output lights 1256 and 1257 interfere with each other, and a signal corresponding to the difference between the oscillation frequencies is detected by the photodetector.

In FIG. 20D, reference numeral 1240 denotes a mirror. The output light of the CCW light 1209 is transferred to this mirror 1240
And is incident on the photodetector 1230.

Note that FIGS. 21E and 21F show
Instead of the tapered regions 1204 and 1205 for generating main mode light in FIGS. 20C and 20D,
This is a case where an optical element such as an optical isolator is used. FIG. 19 shows the case of a semiconductor laser, and FIGS. 20 and 21 show the case of a gas laser. As shown in FIGS. 19 to 21, output light 1256 having an oscillation frequency (wavelength) different from each other.
When light 1257 is received by the photodetector 1230, the first
The second lasers (1200, 1201) do not necessarily have to be arranged close to each other. That is, it is not necessary to dispose within the light seeping distance.

<2> The second embodiment will be described with reference to FIGS. 22 and 23. 4 and 5 are denoted by the same reference numerals.

In FIG. 22A, 1356, 135
7 is output light from each of the first and second lasers, and 1330 is a photodetector.

The main mode light 13 of the first and second lasers
Third Optical Waveguide 13 Optically Coupled to 06,1307
From 20, both output lights are received by the photodetector 1330.

Then, according to the signal from the photodetector,
Detect rotation.

FIG. 22 shows the case of a semiconductor laser, and FIG. 23 shows the case of a gas laser.

<3> Further, a second embodiment will be described with reference to FIGS. 6 and 7 are denoted by the same reference numerals.

Reference numeral 1430 denotes a photodetector, 1456, 1457
Is output light of main mode light of the first and second lasers, and is received by the photodetector 1430.

FIG. 24 shows the case of a semiconductor laser, and FIG. 25 shows the case of a gas laser.

<4> Further, a second embodiment will be described with reference to FIGS. 26 and 27. 8 and 9 are denoted by the same reference numerals.

In FIGS. 26 and 27, the first laser and the second laser share a part of the optical waveguide.

Reference numerals 1556 and 1557 denote output lights of main mode light of the first and second lasers.
The light is received at 30.

FIG. 26 shows the case of a semiconductor laser, and FIG. 27 shows the case of a gas laser.

The photodetector referred to here is a device for converting the intensity of light into an electric signal, and specifically includes a phototube and a photomultiplier using photoemission (external photoelectric effect). In addition, there are various devices utilizing the internal photoelectric effect in a semiconductor, that is, a photoconductive cell, a photodiode, a phototransistor, an avalanche photodiode, and a photovoltaic cell using a photovoltaic effect. Further, there are a heat detector by light absorption, that is, a thermocouple detector, a bolometer, a Golay cell, a pyroelectric light detector by a pyroelectric effect, and the like.

Hereinafter, a semiconductor laser having a ring shape which can be used in the present invention will be described.

FIG. 28 is a sectional view of the semiconductor laser shown in FIG.
FIG. 3 schematically shows an example of a cross-sectional view between A ′. 2
800 is a semiconductor laser, 2801 is an active layer, 2802
Is a substrate, 2803 is an anode, 2804 is a cathode, 2
Reference numeral 806 denotes an upper cladding layer, and 2807 denotes a lower cladding layer.

As described above, at least the upper cladding layer 28
06 (Ring shape) with the center region hollowed out
809 makes it difficult for current to flow in the central region of the semiconductor laser. Therefore, since a gain can be generated only in the light that mainly circulates, an ineffective current can be reduced. In particular, when the single transverse mode is realized, the beat frequency becomes very stable.

In FIG. 28, the light guide layer and the cap layer are not particularly shown.
It suffices that at least the central portion of the upper cladding layer 2806 has a hollow structure.

FIG. 29 shows an example. 2921 is a cap layer, 2922 and 2923 are light guide layers, 2901
Denotes an active layer and 2904 denotes a cathode.

Further, it is possible to form the electrode 2903 in a ring shape while keeping the shapes of the upper cladding layer 2906, the cap layer 2921, and the like. Although the anode electrode 2903 is provided on the entire surface of the laser device in the drawing, it is not always necessary to provide the anode electrode 2903 on the entire surface.

As shown in FIG. 30, the active layer 280
It is also preferable that part of the active layer 1 or the active layer itself is formed in a ring shape, or that a part of the lower cladding layer 2807 is also formed in a ring shape as shown in FIG. When a part of the active layer is also formed into a ring shape, the volume of the active layer is reduced, so that the threshold current can be more effectively reduced.

In particular, it is preferable to have a ring shape within the range where the laser light is distributed (for example, 1 in FIG. 31). That is, the active layer is preferably ring-shaped (donut-shaped).

For example, when the thickness of the active layer is 0.1 μm, 1 in FIG. 31 is about 1 μm.

Within the seepage distance in the direction perpendicular to the surface of the active layer, if the structure has a ring shape, the light confinement coefficient for the active layer becomes large, so that low current driving can be suitably performed, and the oscillation frequency can be improved. Is also stable. Of course, as shown in FIG. 32, the entire semiconductor laser 2800 may have a ring shape.

Although FIG. 31 shows that the light exudation distance 1 is located within the cladding layers 2806 and 2807, it is needless to say that depending on the conditions such as the refractive index and the thickness of the cladding layer, Light may seep beyond the layers. In such a case, the portion corresponding to the light exudation distance 1 preferably has a cylindrical shape. In the case where the light guide layer between the active layer and the clad layer or the substrate 2802 is exuded, it is preferable that a part of the optical guide layer and the substrate corresponding to the exudation distance have a ring shape.

When low current or low voltage driving is required to prevent loss of light, a low refractive index layer 2806,
It is desirable to reduce the loss of light at 2807.

FIG. 33 is an enlarged view of the area 2850 in FIG. In the case of driving with low power, the angles θ ₁ and θ ₂ (FIG. 33) formed by the side surface of the low refractive index layer and the surface of the active layer are: 75 ° ≦ θ ₁ , θ ₂ ≦ 105 °, preferably 80 ° ≦ θ ₁ , θ ₂ ≦ 100 ° More preferably, it is desirable to manufacture a laser device so as to satisfy 85 ° ≦ θ ₁ , θ ₂ ≦ 95 °.

By satisfying such conditions, loss of light (evanescent light) seeping into the low refractive index layers 2806 and 2807 can be prevented, so that the semiconductor laser can be driven with lower current (or lower voltage). It becomes possible.

Of course, it is also preferable that the side surface of the semiconductor laser is a total reflection surface. It is preferable that the angle formed by 90% or more of the light exuding region on the total reflection surface with the active layer surface is within the above range.

Further, the side surface over the entire circumference of the low refractive index layer is
It is also preferable that the above conditions of θ ₁ and θ ₂ are satisfied. It is more preferable that the inner side surface of the laser also satisfies the above conditions of θ ₁ and θ ₂ .

The surface accuracy (surface roughness) of the side surface of the low-refractive-index layer sandwiching the active layer 2801 is not more than half of the wavelength in the medium (wavelength in vacuum / equivalent refractive index of the medium) in the active layer. , More preferably less than 1/3. Specifically, in the case of an InP system (wavelength: 1.55 μm, equivalent refractive index of the medium: 3.6), it is about 0.22 μm or less, preferably 0.14 μm or less.

In the case of a GaAs system (wavelength: 0.85 μm, equivalent refractive index of the medium: 3.6), about 0.12 μm or less,
Preferably, it is 0.08 μm or less.

Of course, not only the side surface of the low refractive index layer,
It is desirable that the side surface of the active layer is also in the above range.

Note that at least a part of the ring-shaped portion is
It is also preferable to fill with an insulating material (dielectric thin film). Of course, if the desired characteristics are obtained,
It is not limited to an insulating material, and it is not necessary to completely fill the hollow portion.

The dielectric thin film is not particularly limited as long as its specific resistance is higher than that of the cladding layer, but amorphous Si, SiO ₂ , MgO, and SiN are preferably used. The filler may form a total reflection surface inside the cylindrical shape. As shown in FIG. 34, one type of material 2930
Or a mixture thereof. In addition, as shown in FIG. 35, it is preferable that at least one of the inner side and the outer side surface of the active layer or the like is covered with the thin film 2931. In this case, deterioration of device characteristics due to exposure to an external atmosphere can be prevented, and material can be saved compared to a case where the device is completely filled. In FIG. 25,
Although a single-layer coating film is shown, it goes without saying that a plurality of layers may be used.

When a plurality of dielectric thin films are used, S
It is also preferable to provide several layers of pairs of iO ₂ and Si. Of course, if the desired properties are obtained, it is not necessary to completely fill.

Hereinafter, another example of filling will be described.

In FIG. 36, reference numeral 2930 denotes an insulating film. As described above, it is also preferable to have the insulating film region 2930 in the lower central portion of the anode 2903. The current does not easily flow in the center of the semiconductor laser device, the ineffective current is reduced, and the single transverse mode is easily generated. This is useful when a flat electrode structure is desired.

In the case where the upper cladding layer 2906 is of a P-type, a PNP-type conductive material is filled in place of the insulating film 2930, so that the laser central region becomes P-type.
With the NPN thyristor structure, it is possible to make the current hardly flow.

In FIG. 37, reference numeral 2840 denotes, for example, an Fe-doped high-resistance layer. By using such a high resistance layer, a structure in which a current does not easily flow in the center of the semiconductor laser device can be realized.

Hollow portion 280 of active layer of semiconductor laser
9 (for example, FIG. 31) may be located approximately at the center. A state in which no waveguide mode exists is called a cutoff. In order to stabilize a transverse mode, it is preferable that the waveguide be formed so as to satisfy a cutoff condition for a higher-order mode. It is desirable that the diameter d of the hollow portion (FIG. 28) is also defined so as to satisfy the cutoff condition for the higher-order mode.

By satisfying the cut-off condition for the higher-order mode, the transverse mode becomes only the basic mode and becomes stable.

Further, it is preferable that the shape of the hollow portion also satisfies the cutoff condition of the higher-order mode as much as possible, and that the shape is such that only a single guided mode exists (single transverse mode).

The formation of a laser device having a hollow shape is as follows.
When a semiconductor film to be an active layer, a light guide layer, a clad layer, or the like is deposited on a substrate, the semiconductor film may be deposited in a ring shape using a mask or the like. After the active layer, the light guide layer, the clad layer, and the like are deposited, they may be removed by etching or the like so as to form a ring shape.

The etching method for forming the hollow portion includes wet etching, gas etching, plasma etching, sputter etching, reactive ion etching (RIE), and reactive ion beam etching (R).
IBE) or the like can be used as appropriate.

The material of the active layer applicable to the present invention includes GaAs, InP, ZnSe, AlGaAs, and InGaAs.
GaAsP, InGaAlP, InGaAsP, GaAs
sP, InGaAsSb, AlGaAsSb, InAs
SbP, PbSnTe, GaN, GaAlN, InGa
N, InAlGaN, GaInP, GaInAs, Si
Ge-based, and the like.

As the clad layer, those applicable to the above-mentioned active layer can be used.

As the combination of the active layer and the cladding layer, for example, PbSnTe (active layer) / PbSeTe
(Cladding layer), PbSnSeTe (active layer) / PbS
eTe (cladding layer), PbEuSeTe (active layer) /
PbEuSeTe, PbEuSeTe (active layer) / Pb
Te (cladding layer), InGaAsSb (active layer) / G
aSb (cladding layer), AlInAsSb (active layer) /
GaSb (cladding layer), InGaAsP (active layer) /
InP (cladding layer), AlGaAs (active layer) / Al
GaAs (cladding layer), AlGaInP (active layer) /
AlGaInP (active layer) or the like can be used.

The structure of the semiconductor laser is not limited to the active layer having a bulk structure, but may be a single quantum well structure (SQ).
W) and a multiple quantum well structure (MQW).

When a quantum well laser is used, it is also preferable to adopt a strained quantum well structure. For example, an InGaAsP quantum well 8 having a compression strain of about 1%
The active layer is formed by the layer and the barrier layer of InGaAsP. Of course, an MIS structure can also be used.

The substrate may be any substrate on which a desired material can be grown, and may be a GaAs substrate, InP substrate, GaSb substrate, InAs substrate, PbTe substrate, Ga
A compound semiconductor such as an N substrate, a ZnSe substrate, or a ZnS substrate, a SiC substrate, a 4H-SiC substrate, a 6H-SiC substrate, a sapphire substrate, a silicon substrate, an SOI substrate, or the like can be used.

The active layer and the like of the semiconductor laser are formed by liquid phase epitaxy (LPE method), molecular beam epitaxy (MBE).
Method), metal organic chemical vapor deposition (MOCVD, MOVPE)
Method), atomic layer growth method (ALE method), metalorganic molecular beam epitaxy (MOMBE), chemical beam epitaxy (CB)
E) can be used.

As the anode electrode, Cr / Au, Ti
/ Pt / Au, AuZn / Ti / Pt / Au or the like can be used. AuGe / Ni as the cathode electrode
/ Au and AuSn / Mo / Au can be used.

Of course, the present invention is not limited to these.

The arrangement of the electrodes can be appropriately reversed from that shown in the drawings according to the conductivity of the substrate, the active layer, and the like. The same applies to other embodiments.

It is also preferable to form a cap layer (contact layer) for reducing contact resistance with an electrode on the clad layer and then form the above-mentioned electrode material on the cap layer.

For example, the structure is InGaAsP (active layer) / P-type InP (cladding layer) / P-type InGaAsP (cap layer) / electrode.

Although the drawing shows the cathode electrode below the substrate, the arrangement of the anode and the cathode may be reversed depending on the type of the substrate.

It is also preferable to mount a semiconductor laser chip on a heat radiating material (heat sink) in order to prevent the semiconductor laser from affecting the heat. As a heat sink material, Cu, Si, SiC,
AlN, diamond, or the like can be used. Of course, it is not limited to these. Further, if necessary, a Peltier element can be used for temperature control.

In order to ensure that the semiconductor laser becomes a total reflection surface, or to prevent deterioration, an insulating film (coating film) is provided on the side surface (side surface of the region where light exists) of the semiconductor laser. The formation is also preferable. The coating materials include SiO ₂ , Si
An insulating film such as N, Al ₂ O ₃ , Si ₃ N ₄ or amorphous silicon (α-Si) can be used.

It is also preferable that a portion corresponding to the above-mentioned ring-shaped hollow portion has a high resistance as shown in FIG. 38, and the substantial shape of the optical waveguide is ring-shaped.

FIG. 38 is a schematic diagram showing an example of a sectional view in that case.
Shown in

2801 is an active layer, 2802 is a substrate, 28
Numeral 03 denotes an anode, numeral 2804 denotes a cathode, numeral 2806 denotes an upper cladding layer, numeral 2807 denotes a lower cladding layer, and numeral 2859 denotes a region whose resistance is increased by ion implantation. With such a configuration, the current is less likely to flow in the central region, and a gain can be given mainly to only the circulating light.

In FIG. 38, high resistance region 2
Although the interface at 859 is shown as being clear, in practice there is some spread at the interface. Of course, as shown in FIG. 39, it is also preferable to perform ion implantation so that the projection range at the time of ion implantation mainly comes to the active layer.

In FIG. 38, at least a part of the upper cladding layer is described as having a high resistance. However, if the structure is such that a current does not easily flow in the central region, the active layer region 2801 has a high resistance. The resistance may be partially increased, or at least a part of the lower cladding layer 2807 may be increased in resistance. Of course, the entire central region of the semiconductor laser may have a higher resistance.

In particular, when the central region of the active layer 2801 has a high resistance, the volume of the active layer is substantially reduced, and the drive current can be further reduced.

Of course, it is also possible to perform ion implantation so as to have a projection range at a depth near the active layer, and to increase the resistance around the depth.

In FIG. 38, the anode 280
Although 3 has a structure arranged around the semiconductor laser, it may be arranged on the entire upper surface of the laser, or conversely, may be arranged in a partial area.

As appropriate, a light guide layer, a cap layer and the like can be formed.

Regarding the increase in resistance according to the present invention, the specific resistance in the ion-implanted region is approximately 100 Ω · cm to 10 ⁵ Ω · cm, preferably 5 × 10 ³ Ω · cm, although it depends on the type of the active layer. And 1 × 10 ⁵ Ω · cm.

Examples of the ion-implanted species include proton and boron.

It is also preferable to perform ion implantation so that the projection range Rp of the ion implantation is at the center of the active layer. In this case, the acceleration voltage is set to 10 Ke in consideration of the material and thickness of the cladding layer on the active layer, the optical guide layer, and the like.
It is preferable to perform the treatment appropriately in the range of V to 1 MeV.

The amount of ion implantation is from 1 × 10 ¹³ cm ⁻² to 1
It can be performed within a range of × 10 ¹⁵ cm ^-2 .

The substrate temperature at the time of ion implantation may be room temperature.

The ion implantation region does not need to be strictly at the center of the semiconductor laser, but is preferably implanted substantially at the center so as to satisfy the cut-off condition for higher-order modes.

It is desirable that the diameter d of the implantation region is also defined so as to satisfy the cutoff condition for the higher-order mode.

Further, the shape of the injection region is not necessarily limited to a circle, but satisfies the cut-off condition of a higher-order mode as much as possible, and only a single waveguide mode (single transverse mode) exists. It is preferable to make it into such a shape.

It is also preferable to perform an annealing process after the implantation in order to reduce damage caused during the ion implantation. The annealing temperature is 200
C. to 500.degree. C., preferably 300.degree. C. to 400.degree. As an atmosphere for annealing, an atmosphere containing hydrogen or the like can be used.

Although an example in which ion implantation is used to increase the resistance has been described, the resistance may be increased by selectively oxidizing a portion to be increased in resistance.

The embodiment of the present invention has been described. The gyro according to the present invention includes not only articles that can detect angular velocity and rotation direction, but also articles that detect only angular velocity and articles that detect only rotation direction.

Example 1 FIG. 2A is a drawing that best illustrates the features of the present invention, and a cross-sectional view taken along line AA ′ of FIG.
It is. 1200 is a ring resonator type semiconductor laser, 1
204 is a tapered portion of the optical waveguide, 33 is an anode, 34
Is an electric terminal, 35 is a cap layer, 36 is a cladding layer, 3
7 is a light guide layer, 38 is an active layer, 39 is a light guide layer, 1
201 is a ring resonator type semiconductor laser, 1205 is a tapered portion of an optical waveguide, 43 is an anode, 44 is an electric terminal, 45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, 48 is an active layer, and 49 is light A guide layer, 54 is a semiconductor substrate, 55 is a cathode, 1206 is a counterclockwise laser beam, and 1207 is a clockwise laser beam.

The manufacturing method in the above configuration will be described. First, an n-InP substrate 54 is formed by using a metal organic chemical vapor deposition method.
(Thickness: 350 μm) and undoped In of 1.3 μm composition constituting the ring resonator type semiconductor laser 1200.
1. GaAsP light guide layer 39 (0.15 μm thickness);
Undoped InGaAsP active layer 38 of 55 μm composition
(Thickness 0.1 μm) Undoped In of 1.3 μm composition
GaAsP light guide layer 37 (0.15 μm thickness), p-
InP clad layer 36 (thickness 2 μm), p-InGaAsP cap layer 35 having a composition of 1.4 μm (thickness 0.3 μm)
m) grow.

Further, n-I is formed using metalorganic vapor phase epitaxy.
An undoped InGaAsP light guide layer 49 (having a thickness of 0.15 μm) having a composition of 1.3 μm and constituting a ring resonator type semiconductor laser 1201 on an nP substrate 54 (having a thickness of 350 μm)
μm), 1.55 μm undoped InGaAsP
Active layer 48 (0.1 μm thick), undoped InGaAsP light guide layer 47 having a composition of 1.3 μm (0.15 μm thick)
m), p-InP cladding layer 46 (2 μm thickness),
A p-InGaAsP cap layer 45 (thickness: 0.3 μm) having a composition of 4 μm is grown.

This time, the ring resonator type semiconductor laser 1
Although the common semiconductor layers constituting the semiconductor laser 200 and the ring resonator type semiconductor laser 1201 are grown at the same time, they may be grown separately.

[0270] After the crystal growth, p was applied using a spin coater.
A photoresist AZ-135 on the InP cap layer
0 (made by Hoechst) is applied so that the film thickness becomes 1 μm. After pre-baking at 80 ° C. for 30 minutes, the wafer was exposed with a mask. The width of the optical waveguide after development and rinsing is 5 μm, and the tapered portions 1204 and 1205
Then, the maximum value of the width of the optical waveguide is 8 μm, and the minimum value is 5 μm.
It is. The angle of the tapered portion (β in FIG. 10) is 90
°. The length of one round of the optical waveguide is
It is 600 μm.

After that, the wafer is introduced into a reactive ion beam etching apparatus, and chlorine gas is used.
Etching was performed to a depth of 3 μm. Finally, p
Cr / Au was formed as an anode 33 and 43 on the InGAsP cap layers 35 and 45 by vapor deposition, respectively. Further, as a cathode 55 on an n-InP substrate, A
uGe / Ni / Au was deposited. After that, annealing was performed in a hydrogen atmosphere to make ohmic contact.

In the above structure, since the refractive index of the semiconductor is different from that of air, reflection occurs at the interface. Assuming that the refractive index of the semiconductor is 3.5, total reflection occurs when the angle between the normal to the interface and the laser beam is 16.6 degrees or more. In the mode that receives total reflection, the oscillation threshold gain can be small because the mirror loss is small compared to the other modes, so that oscillation starts at a low injection current level. Moreover, since the gain is concentrated in this oscillation mode, oscillation in other modes is suppressed.

In FIG. 2A, the angle between the laser beam and the normal to the interface is 45 degrees, which satisfies the condition of total reflection. The oscillation threshold current at room temperature is 2 mA. The driving current of the ring resonator type laser 1200 is 3 mA, and the driving current of the ring resonator type laser 1201 is 3.5 mA. When these lasers are stationary, the oscillation wavelengths of the laser light 1206 and the laser light 1207 are almost equal. And the oscillation wavelength λ is 1.55 μm. However, the ring resonator type laser 1200 and the ring resonator type laser 1
Since the drive currents of the lasers 201 are different, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers.

For this reason, the oscillation frequency is slightly different.
Oscillation frequency f of laser light 1206 _ThreeIs the laser light 1
207 oscillation frequency f_Four1 kHz higher. Also,
When total reflection occurs, the evanescent
There is a luminescent light. When the oscillation wavelength is 1.55 μm
In this case, the exudation distance of evanescent light is 0.0735μ
m. Evanescent light intensity decays exponentially
(The exudation distance decreases the electric field amplitude to 1 / e
Distance), ring cavity lasers 1200 and 12
01 separated by 0.07 μm within the exudation distance
Laser light 1206 and laser light
1207 are efficiently coupled. As a result, each
Laser light 1206 and 1 in ring resonator type laser
207 interfere. At this time, the power supply current becomes constant
And adjust the voltage between the electrode terminal 34 and the cathode 55.
Voltage or the voltage between the electrode terminal 44 and the cathode 55
When you monitor, the amplitude is 80mV and 100mV respectively.
A signal with a frequency of 1 kHz is obtained. That is, both rings
When the pendulum lasers 1200 and 1201 are stationary
However, the beat frequency can be detected.

When the ring resonator type lasers 1200 and 1201 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser beam 1206 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser light 1207 decreases by 88.7 Hz. Therefore, the beat frequency is represented by equation (16).

[0276]

(Equation 16) On the other hand, the ring cavity lasers 1200 and 1201 are:
When subject to rotation counterclockwise at a rate of 30 degrees per second, the beat frequency is expressed by equation (17).

[0277]

[Equation 17] Since the absolute value of the increase / decrease of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also the rotation direction and the increase / decrease of the beat frequency correspond one-to-one.
The rotation direction can be detected. The laser device thus obtained is mounted on a car, a camera, a lens, an aircraft, a ship, and used as a gyro.

In this embodiment, constant current driving is used.
Although the change in the terminal voltage was measured, if the driving was performed at a constant voltage, the change in the current flowing through the terminal could be detected.
Further, a change in the impedance of the element may be directly detected using an impedance meter.

[0279] This eliminates the need for a photodetector for detecting beat light, and as a result, there is no return light noise caused by return light from the photodetector.

[0280] Here, InG is used as a semiconductor material.
aAsP type was used, but GaAs type, ZnSe type
Any material system, such as a system, an InGaN system, and an AlGaN system, may be used. The shape of the optical waveguide may be any shape, such as a hexagon, a triangle, or a circle, as well as a square as shown in FIG.

Ring resonator type lasers 1200 and 120
In the present embodiment, the magnitude of the driving current was changed so that the oscillation wavelengths of the first and second lasers differed. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

FIGS. 41 to 4 show another method of producing a laser.
9 will be described. First, an n-GaAs substrate 4402
An active layer 4401 having a multiple quantum well structure composed of three layers of Al _0.3 Ga _0.7 As / GaAs is provided thereon, and an optical guide layer 4422 of Al _0.3 Ga _0.7 As sandwiches this active layer.
Is provided. Further, the cladding layer (4
406 p- Al _0.5 Ga _0.5 As, 4407 is n-
Al _0.5 Ga _0.5 As) is formed. 4415 is n
-A buffer layer made of GaAs. 4440 is p
-A cap layer made of GaAs.

An anode 440 is formed on the cap layer 4440.
Then, cr / Au (or Ti / Pt / Au) to be 3 is formed (FIG. 42).

Then, after applying a photoresist 4460, patterning is performed as shown in FIG.

[0285] Patterned photoresist 446
Dry etching is performed on the anode 4403 using 0 as a mask (FIG. 44).

Next, the semiconductor layer is removed by dry etching (FIG. 45), and the photoresist is stripped (FIG. 46).

Here, the anode is annealed in a hydrogen atmosphere to form an alloy.

Next, after polishing the substrate as necessary, AuGe
A cathode 4404 made of Ni / Au is deposited (FIG. 4).
7).

Thus, a ring laser 4400 can be formed. FIG. 48 is a diagram of the laser 4404 thus formed as viewed from above.

The angle m in FIG. 48 is 45 ° ± 0.
It is desirably in the range of 01 °, preferably 45 ° ± 0.001 °. The same applies to locations corresponding to other corners. This is a condition necessary for the laser beam to return as close to the starting point as possible when making a round in the optical resonator.

Of course, when a semiconductor ring laser is produced by another process, it is desirable that m is within the above range.

FIG. 49 shows a corner 4490 in FIG.
The surface roughness r at the corner is 5
The thickness is less than 0 nm, preferably less than 20 nm. As a result, backscattering can be reduced, and lock-in can hardly occur.

FIG. 50 is a diagram showing an example for detecting a beat using the above-mentioned laser, wherein 1 is an optical gyro, 2 is a turntable, 3 is a current source, 4 is a resistor, and 5 is a frequency minus.
It is a voltage conversion circuit (FV conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two lasers constituting the optical gyro 1 is obtained as a change in the terminal voltage. Furthermore, when the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 2) In FIG.
2 is an optical waveguide; 1204 is a tapered portion of the optical waveguide;
03 is an optical waveguide, 1205 is a tapered portion of the optical waveguide, 1
Reference numeral 208 denotes a laser beam, and 1207 denotes a laser beam.

In the above configuration, both the laser beam 1207 and the laser beam 1208 propagate in the same direction in a circular manner. In this case as well, the rotation direction can be detected as described in the operation, but when the laser light circulates in the same direction, to increase the coupling efficiency between the laser lights 700 and 800,
It is desirable that the propagation directions of the laser beams propagating in adjacent portions of the optical waveguide are equal. To realize this, an optical waveguide 1203 is formed in the optical waveguide 1202.

(Embodiment 3) In FIG.
2 is a quartz tube, 1204 is a tapered portion of an optical waveguide, 121 is
4 is a mirror, 1210 is an anode, 1216 is an electric terminal, 1212 is a cathode, 1203 is a quartz tube, 1205
Is a tapered portion of the optical waveguide, 1215 is a mirror, 1211
Denotes an anode, 1217 denotes an electric terminal, 1213 denotes a cathode, 1206 denotes laser light, and 1207 denotes laser light.

In the above configuration, since the optical waveguide exists within the exudation distance of the laser light, the second laser light is optically and efficiently coupled to the optical waveguide of the first laser. At the same time, the first laser light is efficiently and optically coupled to the optical waveguide of the second laser. For this reason, the interference light component in each laser increases, and the electric signal at the terminal can be further increased. In addition, the light that seeps out in this way is called emissive light.

In the above configuration, a quartz block was cut out using a drill to form quartz tubes 1202 and 1203. Thereafter, mirrors 1214 and 1215 were attached to the quartz tubes 1202 and 1203, respectively. Further, the anodes 1210,
Electrical terminal 1216, cathode 1212, anode 121
1. The electric terminal 1217 and the cathode 1213 were attached. Next, helium gas and neon gas are put into the quartz tubes 1202 and 1203, and when a voltage is applied between the anode and the cathode, discharge starts and current flows.

The quartz tube 12 is formed by the tapered portion of the optical waveguide.
02, only the counterclockwise laser beam 1206 oscillates, and the clockwise laser beam 1206 oscillates in the quartz tube 1203.
Only 207 oscillates. In addition, the angle of the tapered portion (FIG. 1)
Β) of 0 was formed to be 90 °.

When the quartz tubes 12020 and 1203 are stationary, the oscillation frequencies of the laser beams 1206 and 1207 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm. However, the quartz tube 120
By changing the current flowing through 2 and 1203, the Q of the medium
Since the value changes, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1206 is
20 MHz higher than the oscillation frequency f _{2 of}

Also, since the quartz tubes 1202 and 1203 are arranged close to each other, the laser beam 1206 is combined with the laser beam 1207 in the quartz tube 1203.

At the same time, the laser beam 1207 is
2 is combined with the laser beam 1206. As a result, the laser beams 1206 and 1207 interfere in the respective quartz tubes. At this time, the power supply current is adjusted to be constant, and when the voltage between the electrode terminal 1216 and the cathode 1212 is monitored, the amplitude is 100 mV and the frequency is 20 MHz.
The signal of z is obtained. At the same time, when the voltage between the electrode terminal 1217 and the cathode 1213 is monitored, the amplitude is 80 mV.
Thus, a signal having the same frequency of 20 MHz can be obtained.
That is, the beat voltage can be detected even when the quartz tubes 1202 and 1203 are stationary.

Now, the quartz tubes 1202 and 1203 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 100
Oscillation frequency f ₁ of the increases only 248.3kHz.

On the other hand, the oscillation frequency f ₂ of the clockwise laser light 200 decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

[0307]

(Equation 18) On the other hand, when the quartz tubes 1202 and 1203 are rotated counterclockwise at a rate of 180 degrees per second, the beat frequency becomes
9).

[0308]

[Equation 19] Since the absolute value of the increase / decrease of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also the rotation direction and the increase / decrease of the beat frequency correspond one-to-one.
The rotation direction can be detected.

In this embodiment, the change in the terminal voltage is measured with the constant current drive. However, if the drive is performed with the constant voltage, the change in the current flowing through the terminal can be detected. Further, a change in the impedance of the discharge may be directly detected using an impedance meter.

[0310] This eliminates the need for a photodetector for detecting beat light, and as a result, there is no return light noise due to return light from the photodetector.

[0311] Here, helium gas and neon gas are used, but any gas that oscillates laser may be used. Also, the shape of the optical waveguide surrounded by the optical path is shown in FIG.
The shape may be any shape such as a hexagon, a triangle, or a circle, as well as a square as in (C).

(Embodiment 4) In FIG.
Denotes an optical isolator and 1219 denotes an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the third embodiment. This embodiment is different from the third embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, in the third embodiment, a tapered optical waveguide is used, whereas in the fourth embodiment, an optical isolator is used.

When lights of the same polarization enter the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

Embodiment 5 In FIGS. 4A and 51, reference numeral 1300 denotes a ring resonator type semiconductor laser;
4 is a tapered portion of the optical waveguide, 33 is an anode, 35 is a cap layer, 36 is a cladding layer, 37 is a light guide layer, 38
Is an active layer, 39 is a light guide layer, 1301 is a ring resonator type semiconductor laser, 1305 is a tapered portion of an optical waveguide,
43 is an anode, 44 is an electric terminal, 45 is a cap layer,
46 is a cladding layer, 47 is a light guide layer, 48 is an active layer,
49 is a light guide layer, 54 is a semiconductor substrate, 55 is a cathode, 1320 is an optical waveguide, 1306 is a counterclockwise laser beam, and 1307 is a clockwise laser beam. A-
The cross-sectional views cut along A ′ and BB ′ are respectively shown in FIG.
(A) and FIG. 51 (B).

The manufacturing method in the above configuration will be described. First, an n-InP substrate 54 is formed by using a metal organic chemical vapor deposition method.
(Thickness: 350 μm), undoped In of 1.3 μm composition constituting the ring resonator type semiconductor laser 1300
1. GaAsP light guide layer 39 (0.15 μm thickness);
Undoped InGaAsP active layer 38 of 55 μm composition
(Thickness 0.1 μm) Undoped In of 1.3 μm composition
GaAsP light guide layer 37 (0.15 μm thickness), p-
InP clad layer 36 (thickness 2 μm), p-InGaAsP cap layer 35 having a composition of 1.4 μm (thickness 0.3 μm)
m) grow.

[0317] Further, n-I
An undoped InGaAsP light guide layer 49 (having a thickness of 0.15 μm) having a composition of 1.3 μm constituting a ring resonator type semiconductor laser 1301 is formed on an nP substrate 54 (having a thickness of 350 μm).
μm), 1.55 μm undoped InGaAsP
Active layer 48 (0.1 μm thick), undoped InGaAsP light guide layer 47 having a composition of 1.3 μm (0.15 μm thick)
m), p-InP cladding layer 46 (2 μm thickness),
A p-InGaAsP cap layer 45 (thickness: 0.3 μm) having a composition of 4 μm is grown.

This time, the ring resonator type semiconductor laser 1
Although the common semiconductor layers constituting the semiconductor laser 300 and the ring resonator type semiconductor laser 1301 are grown at the same time, they may be grown separately.

After the crystal growth, p was applied using a spin coater.
-Photoresist AZ on InGaAsP cap layer
-1350 (made by Hoechst) is applied so that the film thickness becomes 1 μm.

After prebaking was performed at 80 ° C. for 30 minutes, the wafer was exposed with a mask. The width of the optical waveguide after development and rinsing is 5 μm, and the tapered portion 1304
And 1305, the maximum value of the width of the optical waveguide is 8 μm and the minimum value is 5 μm. The length of one round of the optical waveguide is 600
μm. After that, the wafer is introduced into a reactive ion beam etching device, and chlorine gas is used.
Etching was performed to a depth of 3 μm. Finally, p
Cr / Au was formed as the anodes 33 and 43 on the InP cap layers 35 and 45 by vapor deposition, respectively. AuG is used as a cathode 55 on an n-InP substrate.
e / Ni / Au was deposited. After that, annealing was performed in a hydrogen atmosphere to make ohmic contact.

The configuration of the third optical waveguide 1320 is as follows.

The third optical waveguide 1320 has the same layer structure as the semiconductor laser 1300. Then, a current was injected so that the active layer 38 became transparent and used as a passive optical waveguide.

Further, a current may be further injected into the third optical waveguide to be used as an optical waveguide on the amplification shoulder.

If only the optical waveguide function is realized, the layer structure of the third optical waveguide 1320 may be a structure in which only the active layer 38 is removed from the semiconductor laser 1300. In this case, since the third optical waveguide 1320 is already a passive optical waveguide, there is no need to inject a current into the third optical waveguide.

In FIG. 4A, the angle between the laser beam and the normal to the interface between the semiconductor and air at the corner is 45 degrees, which satisfies the condition of total reflection. The oscillation threshold current at room temperature is 2 mA. The drive current of the ring resonator type laser 1300 is 3 mA, and the drive current of the ring resonator type laser 1303 is 3.5 mA. When these lasers are stationary, the oscillation wavelengths of the laser beam 1306 and the laser beam 1307 are almost equal. And the oscillation wavelength λ is 1.55 μm.

However, the ring resonator type laser 1300
Since the drive currents of the ring resonator type laser 1301 and the ring resonator type laser 1301 are different from each other, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers. Therefore, the oscillation frequencies are slightly different, and the oscillation frequency f ₃ of the laser light 1306 is 1 kHz higher than the oscillation frequency f ₄ of the laser light 1307.

When total reflection occurs, there is evanescent light traveling along the interface. When the oscillation wavelength is 1.55 μm, the exudation distance of the evanescent light is 0.0735 μm. Although the intensity of the evanescent light attenuates exponentially (the exudation distance is the distance at which the electric field amplitude attenuates to 1 / e), the distance between the ring resonator type laser 1300 and the optical waveguide 1320 is within 0.1 mm. 07 μm apart and the laser light 1
306 and the optical waveguide 1320 are efficiently coupled. Then, the ring resonator type laser 1303 and the optical waveguide 132
The laser light is disposed at a distance of 0.07 μm within the oozing distance, and the laser light propagating through the optical waveguide 1320 is efficiently coupled to the ring resonator type laser 1303.

As a result, the ring resonator shoulder laser 130
In 1, the laser beams 1306 and 1307 interfere. Laser light 30 in each ring resonator type laser
0 and 400 interfere. At this time, the power supply current is adjusted so as to be constant, and when the voltage between the electrode terminal 44 and the cathode 55 is monitored, the amplitude is 80 mV and the frequency is 1 kHz.
Is obtained. That is, the beat voltage can be detected even when the ring resonator type lasers 1300 and 1303 are stationary.

Now, when the ring resonator type lasers 1300 and 1301 are rotated clockwise at a rate of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser light 1306 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser light 1307 decreases by 88.7 Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1300 and 1301 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by equation (17).

Since the absolute value of the increase / decrease of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

Ring cavity lasers 1300 and 130
In the present embodiment, the magnitude of the driving current was changed so that the oscillation wavelengths of the first and second lasers differed. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

In FIG. 52, 1 is an optical gyro, 2 is a turntable, 3 is a current source, 4 is a resistor, and 5 is a frequency-voltage conversion circuit (FV conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two lasers constituting the optical gyro 1 is obtained as a change in the terminal voltage. Furthermore, when the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing the beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, when the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is set to zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 6) Referring to FIG.
2 is an optical waveguide, 1304 is a tapered portion of the optical waveguide, 13
03 is the optical waveguide, 1305 is the tapered portion of the optical waveguide, 1
Reference numeral 320 denotes an optical waveguide, 1306 denotes a laser beam, and 1309 denotes a laser beam.

In the above configuration, both the laser beam 1306 and the laser beam 1309 propagate in the same direction. In this case as well, the rotation direction can be detected as described in the operation. However, when the laser light circulates in the same direction, the optical waveguides 1302, 1303, and 1320 are arranged so that the distance between the laser light 1306 and 1309 is increased. Can be increased.

(Embodiment 7) In FIG.
2 is a quartz tube, 1304 is a tapered portion of an optical waveguide, 131
4 is a mirror, 1310 is an anode, 1312 is a cathode, 1303 is a quartz tube, 1305 is a tapered portion of an optical waveguide, 1315 is a mirror, 1311 is an anode, 1317
Denotes an electric terminal, 1313 denotes a cathode, 1320 denotes an optical waveguide, 1306 denotes a laser beam, and 1307 denotes a laser beam. The angle of the tapered portion (β in FIG. 10) is 90 °
And The same applies to other embodiments. However, the angle is not limited to 90 ° as long as a beat signal is appropriately obtained at rest.

In the above structure, a quartz block was cut out using a drill, and quartz tubes 1302 and 1303 and an optical waveguide 1320 were formed. Then, the quartz tubes 1302 and 1
Mirrors 1314 and 1315 were attached to 303, respectively. Further, an anode 1310, a cathode 1312, and an anode 131 are placed in quartz tubes 1302 and 1303, respectively.
1. The electric terminal 1317 and the cathode 1313 were attached.

Next, when helium gas and neon gas are put into the quartz tube 1302 and a voltage is applied between the anode and the cathode, discharge starts and current flows. The quartz tube 130 is formed by the tapered portions 1304 and 1305 of the optical waveguide.
2, only the counterclockwise laser beam 1306 oscillates, and the clockwise laser beam 13
Only 07 oscillates.

When the quartz tubes 1302 and 1303 are stationary, the oscillation frequencies of the laser light 1306 and the laser light 1307 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm.

However, since the Q value of the medium is changed by changing the current flowing through the quartz tubes 1302 and 1303, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser light 1306 is 20MHz greater than the frequency f _2.

Since the quartz tube 1302 is arranged close to the optical waveguide 1320, the laser light 1306 is coupled to the optical waveguide 1320. Since the quartz tube 1303 is arranged close to the optical waveguide 1320,
The laser light that has propagated through the optical waveguide 1320 is
Combine with 3. As a result, the laser beams 1306 and 1307 interfere in the quartz tube 1303.

At this time, the power supply current is adjusted so as to be constant, and the voltage between the electric terminal 1317 and the cathode 1313 is monitored. The amplitude is 80 mV and the frequency is 20 MHz.
The signal of z is obtained. That is, the quartz tubes 1302 and 13
Even when 03 is stationary, the beat voltage can be detected.

Now, the quartz tubes 1302 and 1303 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 130
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.

On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1307 decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1302 and 1303
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one-to-one. The direction can be detected.

(Embodiment 8) In FIG.
8 is an optical isolator and 1319 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the seventh embodiment. This embodiment is different from the seventh embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser.

That is, while the tapered optical waveguide is used in the seventh embodiment, an optical isolator is used in the present embodiment.

When lights of the same polarization enter the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.
(Embodiment 9) In FIGS. 6A and 53, 1402
Is a ring resonator type semiconductor laser, 1404 is a tapered portion of an optical waveguide, 33 is an anode, 35 is a cap layer, 3
6 is a cladding layer, 37 is a light guide layer, 38 is an active layer, 3
9 is an optical guide layer, 1403 is a ring resonator type semiconductor laser, 1405 is a tapered portion of an optical waveguide, 43 is an anode, 44 is an electric terminal, 45 is a cap layer, 46 is a cladding layer, 47 is an optical guide layer, and 48 is An active layer, 49 is a light guide layer, 54 is a semiconductor substrate, 55 is a cathode, 1430 is an optical waveguide, 1406 is a counterclockwise laser beam, 140
Reference numeral 7 denotes a clockwise laser beam. FIG. 53 (A),
FIG. 53B is a cross-sectional view cut along AA ′ and BB ′ in FIG.

A description will be given of a manufacturing method with the above configuration. First, an n-InP substrate 54 is formed by using a metal organic chemical vapor deposition method.
(Thickness: 350 μm) undoped In of 1.3 μm composition that constitutes the ring resonator type semiconductor laser 1402
1. GaAsP light guide layer 39 (0.15 μm thickness);
Undoped InGaAsP active layer 38 of 55 μm composition
(Thickness 0.1 μm) Undoped In of 1.3 μm composition
GaAsP light guide layer 37 (0.15 μm thickness), p-
InP clad layer 36 (thickness 2 μm), p-InGaAsP cap layer 35 having a composition of 1.4 μm (thickness 0.3 μm)
m) grow.

Further, n-I is formed by metalorganic vapor phase epitaxy.
An undoped InGaAsP light guide layer 49 (having a thickness of 0.15 μm) having a composition of 1.3 μm constituting a ring resonator type semiconductor laser 1403 on an nP substrate 54 (having a thickness of 350 μm)
μm), 1.55 μm undoped InGaAsP
Active layer 48 (0.1 μm thick), undoped InGaAsP light guide layer 47 having a composition of 1.3 μm (0.15 μm thick)
m), p-InP cladding layer 46 (2 μm thickness),
A p-InGaAsP cap layer 45 (thickness: 0.3 μm) having a composition of 4 μm is grown.

In this case, the ring resonator type semiconductor laser 1
Although the common semiconductor layers constituting the semiconductor laser 402 and the ring resonator type semiconductor laser 1403 are grown at the same time, they may be grown separately. After the crystal growth, using a spin coater, a photoresist AZ-1350 (made by Hoechst) is applied on the p-InGaAsP cap layer so as to have a thickness of 1 μm. After pre-baking at 80 ° C. for 30 minutes, the wafer was exposed with a mask. The width of the optical waveguide after development and rinsing is 5 μm, and the tapered portion 140
4 and 1405, the maximum value of the width of the optical waveguide is 8 μm, and the minimum value is 5 μm. The length of one circumference of the optical waveguide is 60
0 μm. Thereafter, the wafer was introduced into a reactive ion etching apparatus, and was etched using a chlorine gas to a depth of 3 μm. Finally, p-I
Cr / Au was formed as an anode 33, 43 by vapor deposition on the nGaAsP cap layers 35, 45, respectively. Au is used as a cathode 55 on an n-InP substrate.
Ge / Ni / Au was deposited. After that, annealing was performed in a hydrogen atmosphere to make ohmic contact.

In the above structure, since the refractive index of the semiconductor is different from that of air, reflection occurs at the interface. Assuming that the refractive index of the semiconductor is 3.5, total reflection occurs when the angle between the normal to the interface and the laser beam is 16.6 degrees or more. In the mode that receives total reflection, the oscillation threshold gain becomes smaller by the mirror loss compared to the other modes, so that oscillation starts at a low injection current level. Moreover, since the gain is concentrated in this oscillation mode, oscillation in other modes is suppressed. In FIG. 6A, the angle between the normal to the interface and the laser beam is 45
Degree, and satisfies the condition of total reflection. The oscillation threshold current at room temperature is 2 mA. Ring resonator type laser 140
2 drive current 3 mA, ring resonator type laser 1403
Is 3.5 mA, and when these lasers are stationary, laser light 1406 and laser light 14
07 have substantially the same oscillation wavelength, and the oscillation wavelength λ is 1.55 μm.
m. However, since the drive currents of the ring resonator type laser 1402 and the ring resonator type laser 1403 are different, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers. For this reason, the oscillation frequencies are slightly different, and the oscillation frequency f ₃ of the laser light 1406 is 1 kHz higher than the oscillation frequency f ₄ of the laser light 1407.

Since the ring resonator type laser 1402 and the ring resonator type laser 1403 are connected by the optical waveguide 1430, the laser light 1406 and the laser light 1407 are efficiently coupled. As a result, laser light 1406 and 1
407 interfere.

At this time, if the power supply current is adjusted to be constant and the voltage between the electric terminal 44 and the cathode 55 is monitored, a signal having an amplitude of 100 mV and a frequency of 1 kHz is obtained. That is, the ring resonator type laser 140
The beat voltage can be detected even when 2 and 1403 are stationary.

When the ring resonator type lasers 1402 and 1403 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser light 1406 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser beam 1407 is reduced by 88.7Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1402 and 1403 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by the equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one-to-one. The direction can be detected.

The ring resonator type lasers 1402 and 140
In the present embodiment, the magnitude of the drive current was changed in order to make the oscillation wavelengths of No. 3 different. However, besides this, the length and width of the optical waveguide are changed. The oscillation wavelength can be changed by changing the optical length of the two lasers, for example, by changing the thickness, composition, and material of the semiconductor layer forming the laser.

In FIG. 54, 1 is an optical gyro, 2 is a turntable, 3 is a current source, 4 is a resistor, and 5 is a frequency-voltage conversion circuit (FV conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two lasers constituting the optical gyro 1 is obtained as a change in the terminal voltage. Furthermore, when the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing the beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 10) Referring to FIG.
02 is an optical waveguide, 1404 is a tapered portion of the optical waveguide, 1
403 is an optical waveguide, 1405 is a tapered portion of the optical waveguide,
1430 is an optical waveguide, 1406 is a laser beam, 1409
Is a laser beam.

In the above configuration, both the laser beams 1406 and 1409 are propagated in the same direction in a circular manner. In this case as well, the rotation direction can be detected as described in the operation, but when the laser beam circulates in the same direction, FIG.
By arranging the optical waveguides 1402 and 1403 as in (B), the coupling efficiency between the laser beams 1406 and 1409 can be increased.

(Embodiment 11) Referring to FIG.
02 is a quartz tube, 1404 is a tapered portion of an optical waveguide, 14 is
14 is a mirror, 1410 is an anode, 1412 is a cathode, 1403 is a quartz tube, 1405 is a tapered portion of an optical waveguide, 1415 is a mirror, 1411 is an anode, 1417
Denotes an electric terminal, 1413 denotes a cathode, 1430 denotes an optical waveguide, 1406 denotes laser light, and 1407 denotes laser light.

In the above configuration, a quartz block was cut out using a drill, and quartz tubes 1402 and 1403 and an optical waveguide 1430 were formed. Then, quartz tubes 1402 and 1
Mirrors 1414 and 1415 were attached to 403, respectively. Further, the quartz tubes 1402 and 1403 have an anode 1410, a cathode 1412, and an anode 141, respectively.
1. The electric terminal 1417 and the cathode 1413 were attached.

Next, when helium gas and neon gas are put into the quartz tube 1402 and a voltage is applied between the anode and the cathode, discharge starts and current flows. The quartz tube 140 is formed by the tapered portions 1404 and 1405 of the optical waveguide.
2, only the counterclockwise laser beam 1406 oscillates, and the clockwise laser beam 1414 oscillates in the quartz tube 1403.
Only 07 oscillates.

When the quartz tubes 1402 and 1403 are stationary, the oscillation frequencies of the laser light 1406 and the laser light 1407 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm.

However, since the Q value of the medium changes by changing the current flowing through the quartz tubes 1402 and 1403, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1406 is 20MHz greater than the frequency f _2. Also, quartz tubes 1402 and 1403
Are connected via the optical waveguide 1430, so that the laser light 1406 is coupled to the laser light 1407 in the quartz tube 1403.

At the same time, the laser beam 1407 is
2 is combined with the laser light 1406. As a result, the laser beams 1406 and 1407 interfere in the respective quartz tubes. At this time, the power supply current is adjusted to be constant, and the voltage between the electric terminal 1417 and the cathode 1413 is monitored.
Is obtained. That is, quartz tubes 1402 and 140
Even when 3 is stationary, the beat voltage can be detected.

Now, the quartz tubes 1402 and 1403 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, a counterclockwise laser beam 140 is emitted.
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1407
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1402 and 1403
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond to one to one, The direction can be detected.

In this embodiment, the change in the terminal voltage is measured with the constant current drive. However, if the drive is the constant voltage, the change in the current flowing through the terminal can be detected. Further, a change in the impedance of the discharge may be directly detected using an impedance meter. (Example 12) FIG. 7 (D)
In the figure, 1418 is an optical isolator and 1419 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the eleventh embodiment. The twelfth embodiment is different from the eleventh embodiment in a means for selecting a mode for collecting light in only one direction in a ring laser. That is, while the eleventh embodiment uses a tapered optical waveguide, the present embodiment uses an optical isolator.

When lights of the same polarization enter the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

(Embodiment 13) In FIGS. 8A and 55, reference numeral 1502 denotes a ring resonator type semiconductor laser;
04 is the tapered portion of the optical waveguide, 33 is the anode, 34 is the electric terminal, 35 is the cap layer, 36 is the cladding layer, 37
Is a light guide layer, 38 is an active layer, 39 is a light guide layer, 15
03 is a ring resonator type semiconductor laser, 1505 is a tapered portion of an optical waveguide, 43 is an anode, 44 is an electric terminal,
45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, 48 is an active layer, 49 is a light guide layer, 54 is a semiconductor substrate, 55 is a cathode, 1506 is a counterclockwise laser beam, and 1507 is a clockwise laser beam. It is a laser beam. FIG.
5 is a cross-sectional view cut along AA ′ of FIG.

A description will be given of a manufacturing method in the above configuration. First, an n-InP substrate 54 is formed by using a metal organic chemical vapor deposition method.
(Thickness: 350 μm) undoped In of 1.3 μm composition that constitutes the ring resonator type semiconductor laser 1502
1. GaAsP light guide layer 39 (0.15 μm thickness);
Undoped InGaAsP active layer 38 of 55 μm composition
(Thickness 0.1 μm) Undoped In of 1.3 μm composition
GaAsP light guide layer 37 (0.15 μm thickness), p-
InP clad layer 36 (thickness 2 μm), p-InGaAsP cap layer 35 having a composition of 1.4 μm (thickness 0.3 μm)
m) grow.

Further, n-I is formed by using the metalorganic chemical vapor deposition method.
An undoped InGaAsP light guide layer 49 (having a thickness of 0.15 μm) having a composition of 1.3 μm and constituting a ring resonator type semiconductor laser 1503 on an nP substrate 54 (having a thickness of 350 μm)
μm), 1.55 μm undoped InGaAsP
Active layer 48 (0.1 μm thick), undoped InGaAsP light guide layer 47 having a composition of 1.3 μm (0.15 μm thick)
m), p-InP cladding layer 46 (2 μm thickness),
A p-InGaAsP cap layer 45 (thickness: 0.3 μm) having a composition of 4 μm is grown.

In this case, the ring resonator type semiconductor laser 1
Although the common semiconductor layers constituting the semiconductor laser 502 and the ring resonator type semiconductor laser 1503 are grown at the same time, they may be grown separately. After the crystal growth, using a spin coater, a photoresist AZ-1350 (made by Hoechst) is applied on the p-InGaAsP cap layer so as to have a thickness of 1 μm. After pre-baking at 80 ° C. for 30 minutes, the wafer was exposed with a mask. The width of the optical waveguide after development and rinsing is 5 μm, and the tapered portion 150
4 and 1505, the maximum value of the width of the optical waveguide is 8 μm, and the minimum value is 5 μm. The length of one circumference of the optical waveguide is 60
0 μm. Thereafter, the wafer was introduced into a reactive ion etching apparatus, and was etched using a chlorine gas to a depth of 3 μm. Finally, p-I
Cr / Au was formed as an anode 33, 43 by vapor deposition on the nGaAsP cap layers 35, 45, respectively. Au is used as a cathode 55 on an n-InP substrate.
Ge / Ni / Au was deposited. After that, annealing was performed in a hydrogen atmosphere to make ohmic contact.

In the above structure, the semiconductor and air have different refractive indices, so that reflection occurs at the interface. Assuming that the refractive index of the semiconductor is 3.5, total reflection occurs when the angle between the normal to the interface and the laser beam is 16.6 degrees or more. In the mode that receives total reflection, the oscillation threshold gain becomes smaller by the mirror loss compared to the other modes, so that oscillation starts at a low injection current level. Moreover, since the gain is concentrated in this oscillation mode, oscillation in other modes is suppressed. In FIG. 8A, the angle between the laser beam and the normal to the interface between the semiconductor and air at the ring-shaped corner is 45 degrees, which satisfies the condition of total reflection. The oscillation threshold current at room temperature is 2 mA. The driving current of the ring resonator type laser 1502 is 3 mA, and the driving current of the ring resonator type laser 1503 is 3.5 mA. When these lasers are stationary, the laser beam 1506 and the laser beam 1507 are provided.
Are almost equal, and the oscillation wavelength λ is 1.55 μm.

However, a ring resonator type laser 1502
Since the driving currents of the ring resonator type laser 1503 and the ring resonator type laser 1503 are different from each other, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers. Therefore, the oscillation frequencies are slightly different, and the oscillation frequency f ₃ of the laser beam 1506 is 1 kHz higher than the oscillation frequency f ₄ of the laser beam 1507.

Since the ring resonator type laser 1502 and the ring resonator type laser 1503 share a part of the optical waveguide, the laser light 1506 and the laser light 15
07 is efficiently bonded. As a result, laser light 1506 and 150
7 interfere. At this time, if the power supply current is adjusted to be constant and the voltage between the electric terminal 34 and the cathode 55 is monitored, a signal having an amplitude of 80 mV and a frequency of 1 kHz is obtained. When the voltage between the electric terminal 44 and the cathode 55 is monitored, the amplitude is 100 mV and the frequency is 1 kHz.
Is obtained. That is, the beat voltage can be detected even when the ring resonator type lasers 1502 and 1503 are stationary.

When the ring resonator type lasers 1502 and 1503 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or vehicle vibration, the oscillation frequency f ₃ of the counterclockwise laser light 1506 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser light 1507 decreases by 88.7 Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1502 and 1403 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one-to-one. The direction can be detected.

Ring resonator type lasers 1502 and 150
In the present embodiment, the magnitude of the drive current was changed in order to make the oscillation wavelengths of No. 3 different. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

In FIG. 56, 1 is an optical gyro, 2 is a turntable, 3 is a current source, 4 is a resistor, and 5 is a frequency-voltage conversion circuit (FV conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two lasers constituting the optical gyro 1 is obtained as a change in the terminal voltage. Furthermore, when the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation. Embodiment 14 In FIG. 8B, reference numeral 1502 denotes an optical waveguide;
Reference numeral 1504 denotes a tapered portion of the optical waveguide, 1503 denotes an optical waveguide, 1505 denotes a tapered portion of the optical waveguide, 1506 denotes a laser beam, and 1509 denotes a laser beam.

In the above configuration, both the laser beams 1506 and 1509 propagate in the same direction in a circular manner. Also in this case, the rotation direction can be detected as in the thirteenth embodiment.

(Embodiment 15) Referring to FIG.
02 is a quartz tube, 1504 is a tapered portion of an optical waveguide, 15 is
14 is a mirror, 1510 is an anode, 1516 is an electric terminal, 1512 is a cathode, 1503 is a quartz tube, 1505
Is a tapered portion of the optical waveguide, 1515 is a mirror, 1511
Denotes an anode, 1517 denotes an electric terminal, 1513 denotes a cathode, 1506 denotes a laser beam, and 1508 denotes a laser beam.

In the above structure, a quartz block was cut out using a drill to form quartz tubes 1502 and 1503. Thereafter, mirrors 1514 and 1515 were attached to the quartz tubes 1502 and 1503, respectively. Further, anodes 1510,
Electrical terminal 1516, cathode 1512, anode 151
1. The electric terminal 1517 and the cathode 1513 were attached. Next, helium gas and neon gas are put into the quartz tubes 1502 and 1503, and when a voltage is applied between the anode and the cathode, a discharge starts and a current flows. The quartz tube 15 is formed by the tapered portions 1504 and 1505 of the optical waveguide.
02, only the counterclockwise laser beam 1506 oscillates, and the clockwise laser beam 1
Only 508 oscillates.

When the quartz tubes 1502 and 1503 are stationary, the oscillation frequencies of the laser beam 1506 and the laser beam 1508 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm. However, quartz tube 1502
By keeping changing the current applied to the 1503, the Q value of the medium is changed, slightly different oscillation frequency, the oscillation frequency f ₁ of the laser beam 1506, 20 MHz greater than the oscillation frequency f ₂ of the laser beam 1508. Also, quartz tube 1
Since 502 and 1503 share a part of the optical waveguide, the laser light 1502 is coupled with the laser light 1508 in the quartz tube 1503. At the same time laser light 150
3 couples with the laser light 1506 in the quartz tube 1502. As a result, laser light 15
06 and 1608 interfere. At this time, the power supply current is adjusted so as to be constant, and the voltage between the electric terminal 1516 and the cathode 1512 is monitored.
A signal having a frequency of 20 MHz is obtained. Also, electrical terminals 15
Monitoring the voltage between 17 and cathode 1513,
A signal having an amplitude of 100 mV and a frequency of 20 MHz is obtained.
That is, the beat voltage can be detected even when the quartz tubes 1502 and 1503 are stationary.

Now, the quartz tubes 1502 and 1503 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 150
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1508
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1502 and 1503
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond to one to one, The direction can be detected.

Here, helium gas and neon gas are used, but any gas that oscillates laser may be used. Also, the shape of the optical waveguide that is surrounded by the optical path is not limited to a square as shown in FIG. 1, but may be any shape such as a hexagon, a triangle, or a circle.

(Embodiment 16) In FIG.
18 is an optical isolator and 1519 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as that of the fifteenth embodiment. This embodiment is different from the fifteenth embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, in the fifteenth embodiment, a tapered optical waveguide is used, whereas in the present embodiment, an optical isolator is used.

When light of the same polarization enters the optical isolator from directions opposite to each other, the optical isolator transmits only light that propagates in one direction and does not transmit light that propagates in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

(Embodiment 17) In FIGS. 19A and 57, reference numeral 1200 denotes a ring resonator type semiconductor laser;
04 is the tapered portion of the optical waveguide, 33 is the anode, 35 is the cap layer, 36 is the cladding layer, 37 is the light guide layer, 3
8 is an active layer, 39 is a light guide layer, 1201 is a ring resonator type semiconductor laser, 1205 is a tapered portion of an optical waveguide, 43 is an anode, 45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, and 48 is The active layer, 49 is a light guide layer, 1230 is a photodetector, 54 is a semiconductor substrate, 55 is a cathode, 1206 is a counterclockwise laser beam, 125
6 is a laser beam emitted from the ring resonator type semiconductor laser 1200, 1207 is a clockwise laser beam, 1
Reference numeral 257 denotes a laser beam emitted from the ring resonator type semiconductor laser 1201. FIG. 57 (G) is a cross-sectional view cut along AA ′ of FIG. 19 (A). Lasers 1200 and 1201 were formed in the same manner as in Example 1 described above.

The oscillation threshold current at room temperature is 2 mA. Driving current of ring resonator type laser 1200 3m
A, drive current 3.5 of ring resonator type laser 1201
mA and when these lasers are stationary,
The oscillation wavelengths of the laser beam 1206 and the laser beam 1207 are almost equal, and the oscillation wavelength λ is 1.55 μm. However, since the driving currents of the ring resonator type laser 1200 and the ring resonator type laser 1201 are different, there is a difference in the value of the equivalent refractive index of the optical waveguides constituting these lasers. Therefore, the oscillation frequencies are slightly different, and the oscillation frequency f ₃ of the laser light 1206 is 1 kHz higher than the oscillation frequency f ₄ of the laser light 1207. Laser light 12
56 and the laser beam 1257 are simultaneously received by the photodetector 1320, so that the laser beam 12
56 and 1257 interfere. As a result, the photodetector 123
A signal having an amplitude of 50 mV and a frequency of 1 kHz is obtained from the 0 electrical terminal. That is, the ring resonator type laser 120
Even when 0 and 1201 are stationary, the beat voltage can be detected.

Now, when the ring resonator type lasers 1200 and 1201 are rotated clockwise at a rate of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser light 300 is increased. Increases by 88.7 Hz. On the other hand, the oscillation frequency f ₄ of the clockwise laser beam 400 is reduced by 88.7Hz. Therefore,
The beat frequency is represented by equation (16).

On the other hand, when the ring resonator lasers 1200 and 1201 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by the following equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one-to-one, The direction can be detected.

[0410] Here, InG is used as a semiconductor material.
aAsP type was used, but GaAs type, ZnSe type
Any material system, such as a system, an InGaN system, and an AlGaN system, may be used. Further, the shape of the optical waveguide that is surrounded by the optical path is not limited to a square as shown in FIG. 19A, but may be any shape such as a hexagon, a triangle, or a circle.

The ring resonator type lasers 1202 and 120
In the present embodiment, the magnitude of the drive current was changed in order to make the oscillation wavelengths of No. 3 different. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

In FIG. 58, 1 is an optical gyro, 222
Is a ring laser, 333 is a photodetector, 2 is a turntable, 3
Is a current source, 4 is a resistor, 5 is a frequency-voltage conversion circuit (FV
Conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the ring laser 222 in the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two ring lasers 222 constituting the optical gyro 1 is obtained as a change in the terminal voltage of the photodetector 333. further,
When the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 18) In FIGS. 19B and 59, reference numeral 1240 denotes a mirror, 1209 denotes a counterclockwise laser beam, and 1257 denotes a laser beam reflected by the mirror 1240.

In the above configuration, the difference from the seventeenth embodiment is that the direction of the tapered portion 1205 of the optical waveguide is
As a result, the ring resonator type laser 12
01 is that the laser light 1209 propagating in the O. 01 circulates counterclockwise. In this case, the laser beam 1257 emitted from the ring resonator type laser 1201 is reflected by the mirror 1240 and received by the photodetector 1230 at the same time as the laser beam 1256, whereby a beat signal can be obtained in the same manner as in the seventeenth embodiment. it can.

(Embodiment 19) In FIG.
230 photodetector, 1202 is a quartz tube, 1204 is a tapered portion of an optical waveguide, 1214 is a mirror, 1210 is an anode, 1212 is a cathode, 1203 is a quartz tube, 1205
Is a tapered portion of the optical waveguide, 1215 is a mirror, 1211
Is an anode, 1213 is a cathode, 1206 is a quartz tube 1
A laser beam propagating through the inside 202, 1256 is a laser beam emitted outside, 1207 is a laser beam propagating inside the quartz tube 1203, and 1257 is a laser beam emitted outside.

The laser was manufactured using the method described in Example 3.

When the quartz tubes 1202 and 1203 are stationary, the oscillation frequencies of the laser beam 12060 and the laser beam 1207 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm. However, the quartz tube 120
By changing the current flowing through 2 and 1203, the Q of the medium
Since the value changes, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1206 is
20 MHz higher than the oscillation frequency f _{2 of} By lowering the reflectance of one of the mirrors constituting the laser resonator, laser light can be extracted from the mirror having a low reflectance. Laser light 1256 and 1257 emitted from the laser to the outside are
At the same time, the laser beams 1256 and 1257 interfere in the photodetector. At this time, an electric terminal of the photodetector 1230 has an amplitude of 50 mV and a frequency of 20 MHz.
The signal of z is obtained. That is, quartz tubes 1202 and 12
Even when 03 is stationary, the beat voltage can be detected.

Now, the quartz tubes 1202 and 1203 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 120
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1207
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1202 and 1203
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

Here, helium gas and neon gas are used, but any gas that oscillates laser may be used. Also, the shape of the optical waveguide surrounded by the optical path is shown in FIG.
Not only squares like 0 (C), but also hexagons and triangles,
Alternatively, any shape such as a circle may be used.

(First Example of Embodiment 1) FIG.
In (C), 1230 photodetector, 1202 is a quartz tube, 1204 is a tapered portion of an optical waveguide, 1214 is a mirror, 1210 is an anode, 1212 is a cathode, 120
3 is a quartz tube, 1205 is a tapered portion of an optical waveguide, 121
5 is a mirror, 1211 is an anode, 1213 is a cathode, 1206 is a laser beam propagating in the quartz tube 1202, 1256 is a laser beam emitted outside, 1207
Is a laser beam propagating in the quartz tube 1203;
Is a laser beam emitted outside.

The laser was manufactured by using the method described in Example 3.

When the quartz tubes 1202 and 1203 are stationary, the oscillation frequencies of the laser beam 12060 and the laser beam 1207 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm. However, the quartz tube 120
By changing the current flowing through 2 and 1203, the Q of the medium
Since the value changes, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1206 is
20 MHz higher than the oscillation frequency f _{2 of} By lowering the reflectance of one of the mirrors constituting the laser resonator, laser light can be extracted from the mirror having a low reflectance. Laser light 1256 and 1257 emitted from the laser to the outside are
At the same time, the laser beams 1256 and 1257 interfere in the photodetector. At this time, an electric terminal of the photodetector 1230 has an amplitude of 50 mV and a frequency of 20 MHz.
The signal of z is obtained. That is, quartz tubes 1202 and 12
Even when 03 is stationary, the beat voltage can be detected.

Now, the quartz tubes 1202 and 1203 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 120
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1207
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1202 and 1203
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

Here, helium gas and neon gas are used, but any gas that oscillates laser may be used. Also, the shape of the optical waveguide surrounded by the optical path is shown in FIG.
Not only squares like 0 (C), but also hexagons and triangles,
Alternatively, any shape such as a circle may be used.

(Embodiment 20) Referring to FIG.
240 is a mirror, 1209 is a counterclockwise laser beam,
Reference numeral 1257 denotes a laser beam reflected by the mirror 1240.

In the above configuration, the difference from the nineteenth embodiment is that the direction of the tapered portion 1205 of the optical waveguide is
As a result, the laser light 1209 propagating in the quartz tube 1203 is circling counterclockwise. In this case, the laser beam 1257 emitted from the quartz tube 1203 is reflected by the mirror 1240 and received by the photodetector 1230 at the same time as the laser beam 1256, whereby a beat signal can be obtained as in the nineteenth embodiment.

(Embodiment 21) In FIG.
218 is an optical isolator and 1219 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the nineteenth embodiment. This embodiment is different from the nineteenth embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, in the nineteenth embodiment, a tapered optical waveguide is used, whereas in the present embodiment, an optical isolator is used.

When light of the same polarization enters the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

(Embodiment 22) The configuration of FIG. 21F is different from the embodiment 21 in that an optical isolator 1219 is used.
Of the quartz tube 12 is opposite to that of FIG.
That is, the laser light 1209 propagating in the laser beam 03 rotates counterclockwise. In this case, the laser light 1257 emitted from the quartz tube 1203 is reflected by the mirror 1240, and the laser light 1256 and the photodetector 1230 are simultaneously reflected.
, A beat signal can be obtained as in the twenty-first embodiment.

Embodiment 23 In FIGS. 22A and 60, reference numeral 1300 denotes a ring resonator type semiconductor laser;
04 is the tapered portion of the optical waveguide, 33 is the anode, 35 is the cap layer, 36 is the cladding layer, 37 is the light guide layer, 3
8 is an active layer, 39 is a light guide layer, 1301 is a ring resonator type semiconductor laser, 1305 is a tapered portion of an optical waveguide, 43 is an anode, 45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, and 48 is An active layer, 49 is a light guide layer, 1330 is a photodetector, 54 is a semiconductor substrate, 55 is a cathode, 1320 is an optical waveguide, 1306 is a counterclockwise laser beam, and 1356 is emitted from the ring resonator type semiconductor laser 1300. 1307, a clockwise laser beam, and 1357, a laser beam emitted from the ring resonator type semiconductor laser 1301. Further, FIGS. 60E and 60F show A-
It is sectional drawing cut | disconnected by A 'and BB'.

A ring laser was formed in the same manner as in Example 5.

The oscillation threshold current at room temperature is 2 mA. Drive current of ring resonator type laser 1300 3m
A, drive current 3.5 of ring resonator type laser 1301
mA and when these lasers are stationary,
The oscillation wavelengths of the laser light 1306 and the laser light 1307 are almost equal, and the oscillation wavelength λ is 1.55 μm. However, since the drive currents of the ring resonator type laser 1300 and the ring resonator type laser 1301 are different, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers. Therefore, the oscillation frequency is slightly different, and the oscillation frequency f ₃ of the laser light 1306 is
Is 1 kHz higher than the oscillation frequency f _{4 of} .

When total reflection occurs, there is evanescent light traveling along the interface. When the oscillation wavelength is 1.55 μm, the exudation distance of the evanescent light is 0.0735 μm. The intensity of the evanescent light attenuates exponentially.
/ E). The ring resonator type laser 1300 and the optical waveguide 1320 are arranged at a distance of 0.07 μm within the exudation distance.
306 couples efficiently to the optical waveguide 1320. Then, the ring resonator type laser 1303 and the optical waveguide 132
The laser light 1307 is also efficiently coupled to the optical waveguide 1320 at a distance of 0.07 μm within the exudation distance. When the laser light 1356 and the laser light 1357 emitted from the optical waveguide 1320 are simultaneously received by the photodetector 1330, the laser lights 1356 and 1357 interfere in the photodetector 1330. As a result, an amplitude of 50 mV and a frequency of 1 kHz from the electrical terminal of the photodetector 1330
Is obtained. That is, the beat voltage can be detected even when the ring resonator type lasers 1300 and 1301 are stationary.

Now, when the ring resonator type lasers 1300 and 1301 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser light 300 is increased. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser light 1307 decreases by 88.7 Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1300 and 1301 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond to one to one, The direction can be detected.

The ring cavity lasers 1300 and 130
In the present embodiment, the magnitude of the driving current was changed so that the oscillation wavelengths of the first and second lasers differed. However, besides this, the length and width of the optical waveguide are changed. The oscillation wavelength can be changed by changing the optical length of the two lasers, for example, by changing the thickness, composition, and material of the semiconductor layer forming the laser.

In FIG. 61, 1 is an optical gyro, 222
Is a ring laser, 333 is a photodetector, 2 is a turntable, 3
Is a current source, 4 is a resistor, 5 is a frequency-voltage conversion circuit (FV
Conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the ring laser 222 in the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two ring lasers 222 constituting the optical gyro 1 is obtained as a change in the terminal voltage of the photodetector 333. further,
When the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 24) In FIG.
302 is an optical waveguide, 1304 is a tapered portion of the optical waveguide,
1303 is an optical waveguide, 1305 is a tapered portion of the optical waveguide, 1320 is an optical waveguide, 1306 is a laser beam, 13
56 is a laser beam, 1309 is a laser beam, and 1357 is a laser beam.

In the above configuration, both the laser beam 1306 and the laser beam 1309 propagate in the same direction in a circular manner. In this case as well, the rotation direction can be detected. However, when the laser beam circulates in the same direction, the laser beams 1306 and 1309 can be detected by arranging the optical waveguides 1302, 1303, and 1320 as shown in FIG. Can be increased.

(Embodiment 25) Referring to FIG.
330 is a photodetector, 1302 is a quartz tube, 1304 is a tapered portion of an optical waveguide, 1314 is a mirror, 1310 is an anode, 1312 is a cathode, 1303 is a quartz tube, 130
5 is a tapered portion of the optical waveguide, 1315 is a mirror, 131
1 is an anode, 1313 is a cathode, 1320 is an optical waveguide, 1306 is a laser beam propagating in the quartz tube 1302, 1356 is a laser beam emitted outside, 1307
Is a laser beam propagating in the quartz tube 1303;
Is a laser beam emitted outside.

Using the method described in Example 7, a ring laser was manufactured.

When the quartz tubes 1302 and 1303 are stationary, the oscillation frequencies of the laser beam 1306 and the laser beam 1307 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm.

However, since the Q value of the medium changes by changing the current flowing through the quartz tubes 1302 and 1303, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1306 is Frequency f ₂
20 MHz.

The quartz tubes 1302 and 1303 are the optical waveguides 13
20 and the laser light 1
306 and 1307 couple to optical waveguide 1320. Laser light 1356 emitted outside from optical waveguide 1320
And 1357 are simultaneously received by the photodetector 1330, so that the laser beams 1356 and 1357 interfere in the photodetector.

At this time, a signal having an amplitude of 50 mV and a frequency of 20 MHz is obtained at the electric terminal of the photodetector 1330. That is, the beat voltage can be detected even when the quartz tubes 1302 and 13030 are stationary.

Now, the quartz tubes 1302 and 1303 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 130
The oscillation frequency f1 of No. 6 increases by 248.3 kHz. On the other hand, the oscillation frequency f2 of the clockwise laser light 1307 decreases by 248.3 kHz. Therefore,
The beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1302 and 1303
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

(Embodiment 26) Referring to FIG.
318 is an optical isolator and 1319 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the twenty-fifth embodiment. This embodiment is different from the twenty-fifth embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, in the twenty-fifth embodiment, a tapered optical waveguide is used, whereas in the present embodiment, an optical isolator is used.

When light of the same polarization enters the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.
(Embodiment 27) Referring to FIGS.
0 is a ring resonator type semiconductor laser, 1404 is a tapered portion of an optical waveguide, 33 is an anode, 35 is a cap layer,
36 is a cladding layer, 37 is a light guide layer, 38 is an active layer,
39 is a light guide layer, 1401 is a ring resonator type semiconductor laser, 1405 is a tapered portion of an optical waveguide, 43 is an anode, 45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, 48 is an active layer, and 49 is an active layer. Light guide layer, 1430
Is a photodetector, 54 is a semiconductor substrate, 55 is a cathode, 14
30 is an optical waveguide, 1406 is a counterclockwise laser beam,
Reference numeral 1456 denotes a laser beam emitted from the ring resonator type semiconductor laser 1400, 1407 denotes a clockwise laser beam, and 1457 denotes a ring resonator type semiconductor laser 1403.
Is the laser light emitted from. FIG. 62
(E) and FIG. 62 (F is a cross-sectional view cut along AA ′ and BB ′ in FIG. 24 (A).

The ring laser was manufactured by using the method described in Example 9.

The oscillation threshold current at room temperature is 2 mA. Drive current of ring resonator type laser 1400 3m
A, drive current 3.5 of ring resonator type laser 1401
mA and when these lasers are stationary,
The oscillation wavelengths of the laser light 1406 and the laser light 1407 are substantially equal, and the oscillation wavelength λ is 1.55 μm. However, since the drive currents of the ring resonator type laser 1400 and the ring resonator type laser 1401 are different, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers.

For this reason, the oscillation frequency is slightly different.
Oscillation frequency f of laser light 1406 _ThreeIs the laser light 1
407 oscillation frequency f_Four1 kHz higher. ring
Resonator laser 1400 and ring resonator laser 1
Whether 401 is connected by an optical waveguide 1430
The efficiency of laser light 1406 and laser light 1407
Combine well. Laser emitted from optical waveguide 1430
The light 1456 and the laser light 1457 are
By receiving light at the same time, the laser
-Light 1456 and 1457 interfere.

As a result, a signal having an amplitude of 50 mV and a frequency of 1 kHz is obtained from the electric terminal of the photodetector 1430. That is, the beat voltage can be detected even when the ring resonator type lasers 1402 and 1403 are stationary.

When the ring resonator type lasers 1400 and 1401 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser light 1406 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser beam 1407 is reduced by 88.7Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1400 and 1401 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

The ring resonator type lasers 1400 and 140
In the present embodiment, the magnitude of the driving current was changed so that the oscillation wavelengths of the first and second lasers differed. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

In FIG. 63, 1 is an optical gyro, 222
Is a ring laser, 333 is a photodetector, 2 is a turntable, 3
Is a current source, 4 is a resistor, 5 is a frequency-voltage conversion circuit (FV
Conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the ring laser 222 in the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two ring lasers 222 constituting the optical gyro 1 is obtained as a change in the terminal voltage of the photodetector 333. further,
When the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, when the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is set to zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Embodiment 28) Referring to FIG.
402 is an optical waveguide, 1404 is a tapered portion of the optical waveguide,
1403 is an optical waveguide, 1405 is a tapered portion of the optical waveguide, 1430 is an optical waveguide, 1406 is a laser beam, 14
Reference numeral 56 denotes a laser beam, 1409 denotes a laser beam, and 1457 denotes a laser beam.

In the above configuration, both the laser beams 1406 and 1409 propagate in the same direction in a circular manner. Also in this case, the rotation direction can be detected as described in the operation. When the laser beam circulates in the same direction, FIG.
(B) The optical waveguides 1402, 1403, and 14 as in FIG.
By disposing 30, laser beams 1406 and 1409
Can be increased.

(Embodiment 29) Referring to FIG.
430 is a photodetector, 1402 is a quartz tube, 1404 is a tapered portion of an optical waveguide, 1414 is a mirror, 13 is an anode, 15 is a cathode, 1403 is a quartz tube, 1405 is a tapered portion of an optical waveguide, 1415 is a mirror, and 23 is a mirror. An anode, 25 is a cathode, 1430 is an optical waveguide, 1406 is a laser beam propagating in a quartz tube 1402, 1456 is a laser beam emitted outside, and 1407 is a quartz tube 140
Reference numeral 1457 denotes a laser beam propagating inside the laser beam 3 and a laser beam emitted outside.

The ring laser was manufactured in the same manner as in Example 11.

When the quartz tubes 1402 and 1403 are stationary, the oscillation frequencies of the laser beams 1406 and 1407 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm.

However, since the Q value of the medium changes by changing the current flowing through the quartz tubes 1402 and 1403, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser light 1406 is 20MHz greater than the frequency f _2.

[0479] Quartz tubes 1402, 1403 and optical waveguide 14
The laser light 1406 and 1407 are coupled to the optical waveguide 1430 because the 30 is connected. Optical waveguide 14
Laser light 1456 and 145 emitted outside from 30
7 are simultaneously received by the photodetector 1430, so that the laser beams 1456 and 1457 interfere in the photodetector. At this time, the electric terminal of the photodetector 1430 has an amplitude of 50 mV.
, A signal having a frequency of 20 MHz is obtained. That is, the beat voltage can be detected even when the quartz tubes 1402 and 1403 are stationary.

Now, the quartz tubes 1402 and 1403 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, a counterclockwise laser beam 140 is emitted.
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1407
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1402 and 1403
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one-to-one. The direction can be detected.

(Embodiment 30) Referring to FIG.
418 is an optical isolator and 1419 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as in the twenty-ninth embodiment. This embodiment is different from the twenty-ninth embodiment in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, while the tapered optical waveguide is used in the embodiment 29, the optical isolator is used in the present embodiment.

When light of the same polarization enters the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

(Example 31) In FIGS. 26A and 64, reference numeral 1500 denotes a ring resonator type semiconductor laser;
04 is the tapered portion of the optical waveguide, 33 is the anode, 35 is the cap layer, 36 is the cladding layer, 37 is the light guide layer, 3
8 is an active layer, 39 is a light guide layer, 1503 is a ring resonator type semiconductor laser, 1505 is a tapered portion of an optical waveguide, 43 is an anode, 45 is a cap layer, 46 is a cladding layer, 47 is a light guide layer, and 48 is An active layer, 49 is a light guide layer, 1530 is a photodetector, 54 is a semiconductor substrate, 55 is a cathode, 1506 is a counterclockwise laser beam, 155
6 is a laser beam emitted from the ring resonator type semiconductor laser 1500; 1507 is a clockwise laser beam;
Reference numeral 557 denotes a laser beam emitted from the ring resonator type semiconductor laser 1403. FIG. 64E is a cross-sectional view taken along a line AA ′ in FIG.

The ring laser was manufactured in the same manner as in Example 13.

The oscillation threshold current at room temperature is 2 mA. Driving current of ring resonator type laser 1500 3m
A, drive current 3.5 of ring resonator type laser 1501
mA and when these lasers are stationary,
The oscillation wavelengths of the laser beam 1506 and the laser beam 1507 are almost equal, and the oscillation wavelength λ is 1.55 μm. However, since the drive currents of the ring resonator type laser 1500 and the ring resonator type laser 1501 are different, a difference occurs in the value of the equivalent refractive index of the optical waveguides constituting these lasers. Therefore, the oscillation frequencies are slightly different, and the oscillation frequency f ₃ of the laser beam 1506 is 1 kHz higher than the oscillation frequency f ₄ of the laser beam 1507. Ring cavity laser 1500 and ring cavity laser 1501
However, since a part of the optical waveguide is shared, the laser light 1506 and the laser light 1507 are efficiently coupled. When the laser light 1556 and the laser light 1557 emitted from the shared optical waveguide are simultaneously received by the photodetector 1530, the laser lights 1556 and 1557 interfere with each other in the photodetector 1530. As a result, an amplitude of 50 mV and a frequency of 1 kHz from the electrical terminal of the photodetector 1530
Is obtained. That is, the beat voltage can be detected even when the ring resonator type lasers 1500 and 1501 are stationary.

When the ring resonator type lasers 1500 and 1501 are rotated clockwise at a speed of 30 degrees per second, such as camera shake or automobile vibration, the oscillation frequency f ₃ of the counterclockwise laser beam 1506 is obtained. Is 88.7 Hz
Only increase. On the other hand, the oscillation frequency f ₄ of the clockwise laser light 1507 decreases by 88.7 Hz. Therefore, the beat frequency is represented by equation (16).

On the other hand, when the ring resonator type lasers 1500 and 1501 are rotated counterclockwise at a speed of 30 degrees per second, the beat frequency is expressed by equation (17).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond to one to one, The direction can be detected.

The ring cavity type lasers 1500 and 150
In the present embodiment, the magnitude of the driving current was changed so that the oscillation wavelengths of the first and second lasers differed. However, besides this, the oscillation wavelength is changed by changing the optical length of the two lasers, such as changing the length and width of the optical waveguide, changing the thickness, composition, and material of the semiconductor layer forming the laser. be able to.

In FIG. 65, reference numeral 1 denotes an optical gyro;
2 is a ring laser, 333 is a photodetector, 2 is a turntable,
3 is a current source, 4 is a resistor, 5 is a frequency-voltage conversion circuit (F
V conversion circuit).

In the above configuration, the resistance 4 connected in series
, A current is injected from the current source 3 into the ring laser 222 in the optical gyro 1. Even when the optical gyro 1 is stationary, a beat signal corresponding to the difference between the oscillation frequencies of the two ring lasers 222 constituting the optical gyro 1 is obtained as a change in the terminal voltage of the photodetector 3. Furthermore, when the optical gyro 1 mounted on the turntable 2 is rotated, a beat signal corresponding to the angular velocity of the rotation appears.

By passing this beat signal through a frequency-voltage conversion circuit (FV conversion circuit) 5, the beat frequency can be converted to a voltage value. For example, if the offset is adjusted and the voltage output of the frequency-voltage conversion circuit (FV conversion circuit) 5 when the optical gyro 1 is stationary is zero, the output of the frequency-voltage conversion circuit (FV conversion circuit) 5 The rotation direction can be detected based on the sign of the rotation.

(Example 32) In FIG.
502 is an optical waveguide, 1504 is a tapered portion of the optical waveguide,
1503, an optical waveguide; 1505, a tapered portion of the optical waveguide; 1520, an optical waveguide; 1506, a laser beam;
Reference numeral 56 denotes a laser beam, 1509 denotes a laser beam, and 1557 denotes a laser beam.

In the above configuration, both the laser beams 1506 and 1509 propagate in the same direction in a circular manner. Also in this case, the rotation direction can be detected as described in the operation. (Example 33) In FIG.
Is a photodetector, 1502 is a quartz tube, 1504 is a tapered portion of an optical waveguide, 1514 is a mirror, 1510 is an anode,
1512 is a cathode, 1503 is a quartz tube, 1505 is a tapered portion of an optical waveguide, 1515 is a mirror, 1511 is an anode, 1513 is a cathode, and 1506 is a quartz tube 150.
2, 1556 is a laser beam emitted outside, 1508 is a laser beam propagated inside the quartz tube 1503, and 1557 is a laser beam emitted outside.

A ring laser was produced in the same manner as in Example 15.

When the quartz tubes 1502 and 1503 are stationary, the oscillation frequencies of the laser beam 1506 and the laser beam 1508 are almost equal, 4.73 × 10 ¹⁴ Hz, and the oscillation wavelength λ is 632.8 nm.

However, since the Q value of the medium is changed by changing the current flowing through the quartz tubes 1502 and 1503, the oscillation frequency is slightly different, and the oscillation frequency f ₁ of the laser beam 1506 is 20MHz greater than the frequency f _2. Since the quartz tubes 150 and 1503 share a part of the optical waveguide, the laser beams 1556 and 1556 emitted to the outside through the shared portion of the optical waveguide.
When 557 is received by the photodetector 1530 at the same time, the laser beams 1556 and 1557 interfere in the photodetector 1530. At this time, the electrical terminals of the photodetector 1530
A signal having an amplitude of 50 mV and a frequency of 20 MHz is obtained. That is, the beat voltage can be detected even when the quartz tubes 1502 and 1503 are stationary.

Now, the quartz tubes 1502 and 1503 are set at 1 per second.
When the laser beam is rotated clockwise at a speed of 80 degrees and the length of one side of the resonator is 10 cm, the counterclockwise laser beam 150
The oscillation frequency f1 of _No. 6 increases by 248.3 kHz.
On the other hand, the oscillation frequency f ₂ of the clockwise laser light 1508
Decreases by 248.3 kHz. Therefore, the beat frequency is represented by equation (18).

On the other hand, the quartz tubes 1502 and 1503
When subjected to rotation counterclockwise at a speed of 80 degrees, the beat frequency is expressed by equation (19).

Since the absolute value of the increase / decrease amount of the beat frequency is proportional to the rotation speed, not only can the rotation speed be detected, but also because the rotation direction and the increase / decrease of the beat frequency correspond one to one, The direction can be detected.

(Embodiment 34) Referring to FIG.
518 is an optical isolator and 1519 is an optical isolator.

In this configuration, the rotation direction can be detected based on the same principle as that of the thirty-third embodiment. This embodiment is different from the embodiment 33 in a means for selecting a mode in which the laser circulates in only one direction in the ring laser. That is, while the tapered optical waveguide is used in the embodiment 33, an optical isolator is used in the present embodiment.

When light of the same polarization enters the optical isolator from directions opposite to each other, the optical isolator transmits only light propagating in one direction and does not transmit light propagating in the opposite direction. In a normal ring laser, the polarization of the light circulating in the opposite direction is the same, but by inserting an optical isolator, a ring laser that has only light propagating in one direction in a single direction exists. Can be.
Of course, as long as the optical element has a function of transmitting light only in one direction, not limited to the optical isolator, other optical elements such as an optical circulator may be used.

[0507] As for the gas laser, an example using helium gas and neon gas is shown in the embodiment.
Any gas may be used as long as the gas is a laser-oscillating gas and a desired angular velocity can be detected. For example, there are an argon laser, a carbon dioxide laser, and an excimer laser.

Although the case where a quartz tube is used for producing a gas laser has been described, a polymer can also be used. In this case, it can be formed by a low-temperature process. In addition, as a polymer material, fluorinated polyimide, polysiloxane, PMMA (polymethyl methacrylate),
Epoxy or polycarbonate can be used.

[0509] As the discharge electrode, aluminum, zirconium, tungsten or the like can be used.

[0510]

As described above, according to the present invention,
By detecting the beat frequency at the time of rotation of the laser device and calculating the increase or decrease from the time of non-rotation, along with the angular velocity,
The direction of rotation can be detected.

[Brief description of the drawings]

FIG. 1 is a waveform chart for explaining a change in a beat signal due to rotation.

FIG. 2 is a conceptual diagram in a case where first and second lasers are arranged close to each other.

FIG. 3 is a conceptual diagram of a case where first and second lasers are arranged close to each other.

FIG. 4 is a conceptual diagram in a case where a third optical waveguide is provided.

FIG. 5 is a conceptual diagram when a third optical waveguide is provided.

FIG. 6 is a conceptual diagram in a case where a part of an optical waveguide is connected.

FIG. 7 is a conceptual diagram in a case where a part of an optical waveguide is connected.

FIG. 8 is a conceptual diagram when an optical waveguide is shared.

FIG. 9 is a conceptual diagram when an optical waveguide is shared.

FIG. 10 is a plan view of an optical waveguide for explaining a tapered shape.

FIG. 11 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 12 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 13 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 14 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 15 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 16 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 17 is a circuit diagram of a means for detecting a voltage change of the laser device.

FIG. 18 is a circuit diagram of a unit for detecting a voltage change of the laser device.

FIG. 19 is a conceptual diagram in the case where a photodetector is provided and the first and second lasers are arranged close to each other.

FIG. 20 is a conceptual diagram of a case where a photodetector is provided and first and second lasers are arranged close to each other.

FIG. 21 is a conceptual diagram of a case where a photodetector is provided and first and second lasers are arranged close to each other.

FIG. 22 is a conceptual diagram in the case where a photodetector is provided and a third optical waveguide is provided.

FIG. 23 is a conceptual diagram of a case where a photodetector is provided and a third optical waveguide is provided.

FIG. 24 is a conceptual diagram of a case where a photodetector is provided and a part of an optical waveguide is connected.

FIG. 25 is a conceptual diagram of a case where a photodetector is provided and a part of an optical waveguide is connected.

FIG. 26 is a conceptual diagram of a case where a photodetector is provided and an optical waveguide is shared.

FIG. 27 is a conceptual diagram of a case where a photodetector is provided and an optical waveguide is shared.

FIG. 28 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 29 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 30 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 31 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 32 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 33 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 34 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 35 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 36 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 37 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 38 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 39 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 40 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 41 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 42 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 43 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 44 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 45 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 46 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 47 is a cross-sectional view for explaining a manufacturing process of the semiconductor laser and the optical waveguide.

FIG. 48 is a plan view illustrating a corner portion of the optical waveguide.

FIG. 49 is an enlarged view of a corner of the optical waveguide;

FIG. 50 is a view for explaining an embodiment of the present invention;

FIG. 51 is a view for explaining an embodiment of the present invention;

FIG. 52 is a view for explaining an embodiment of the present invention;

FIG. 53 is a view for explaining an embodiment of the present invention;

FIG. 54 is a view for explaining an embodiment of the present invention;

FIG. 55 is a view for explaining an embodiment of the present invention;

FIG. 56 is a view for explaining an embodiment of the present invention;

FIG. 57 is a view for explaining an embodiment of the present invention;

FIG. 58 is a view for explaining an embodiment of the present invention;

FIG. 59 is a view for explaining an embodiment of the present invention;

FIG. 60 is a view for explaining an embodiment of the present invention;

FIG. 61 is a view for explaining an embodiment of the present invention.

FIG. 62 is a view for explaining an embodiment of the present invention;

FIG. 63 is a view for explaining an embodiment of the present invention;

FIG. 64 is a view for explaining an embodiment of the present invention;

FIG. 65 is a view for explaining an embodiment of the present invention;

FIG. 66 is a view for explaining an embodiment of the present invention;

FIG. 67 is a view for explaining an embodiment of the present invention;

FIG. 68 is a view for explaining an embodiment of the present invention;

FIG. 69 is a view for explaining a conventional technique;

FIG. 70 is a view for explaining a conventional technique;

[Explanation of symbols]

DESCRIPTION OF SYMBOLS 1 Optical gyro 2 Turntable 3 Current source 4 Resistance 5 FV conversion circuit 222 Ring laser 333 Photodetector 1200, 1300, 1400, 1500, 1600
Asymmetric taper portions 1202, 1302, 1402, 1502, 1602
CW light 1203, 1303, 1403, 1503, 1603
CCW light 1204, 1304, 1504, 1604 Mirror 1230, 1330, 1430, 1530 Photodetector 2602 Power supply 2609 Impedance meter 2712 CW light emitted outside 2713 CCW light emitted outside 2730 Photodetector 2801, 2901 Active layer 2802, 2902 Substrate 2803, 2903 Anode 2804, 2904 Cathode 2806, 2906 Upper cladding layer 2807, 2907 Lower cladding layer 4101 Active layer 4103 Anode 4104 Cathode 4121 Cap layer 4122, 4123 Light guide layer 4124 Electric terminal 4300 for extracting a beat signal Gyro 4350 Turntable 4401 Active layer 4402 p-GaAs substrate 4422 Light guide layer 4406, 4407 Cladding layer 44 3 anode 4460 photoresist 4490 corners 5301 quartz tube 5313 anode 5314 electric terminal 5315 cathode 5800,5900 gain waveguide on the tapered region 5711 Ring 5717 light absorbing region 5722 electrodes 5790,5791 electrode 5792 semiconductor laser element

──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. ⁷ Identification symbol FI Theme coat ゛ (Reference) H01S 5/10 H01S 5/10 5/343 5/343

Claims (82)

[Claims] 1. A first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circling in one direction as a main mode.
A gyro for extracting an electric signal from at least one of the first and second lasers, wherein the first laser light and the second laser light have different oscillation frequencies, and the first laser light has a different oscillation frequency. A gyro, wherein a laser beam interferes with the second laser beam. 2. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first optical waveguide and the second optical waveguide are provided. The gyro according to claim 1, wherein at least a part of the wave path is arranged close to the wave path. 3. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is optically coupled. The gyro according to claim 1, further comprising a third optical waveguide coupled to the gyro. 4. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and is connected to at least a part of the first and second optical waveguides. 2. The device according to claim 1, further comprising a third optical waveguide.
The gyro described. 5. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is shared. The gyro according to claim 1, wherein: 6. The gyro according to claim 1, wherein the first and second laser beams have different oscillation wavelengths. 7. The gyro according to claim 1, wherein the first and second laser beams have different oscillation frequencies. 8. The gyro according to claim 7, wherein the difference between the oscillation frequencies of the first and second laser beams is 100 Hz or more. 9. The gyro according to claim 7, wherein an oscillation frequency difference between the first and second laser beams is 1 kHz or more. 10. The gyro according to claim 7, wherein an oscillation frequency difference between the first and second laser beams is 10 kHz or more. 11. The gyro according to claim 1, wherein the circling directions of the first and second laser beams are opposite to each other. 12. The gyro according to claim 1, wherein the circling directions of the first and second laser beams are the same. 13. The gyro according to claim 1, wherein currents injected into the first and second lasers are different from each other. 14. The gyro according to claim 1, wherein voltages applied to the first and second lasers are different from each other. 15. The gyro according to claim 1, wherein the first and second lasers have different optical path lengths. 16. The gyro according to claim 1, wherein the first and second lasers have different optical waveguide lengths. 17. The gyro according to claim 1, wherein constituent materials of the first and second lasers are different from each other. 18. The gyro according to claim 1, wherein the optical waveguides constituting the first and second lasers have a ring shape. 19. The first laser has a first optical waveguide, and the second laser has a second optical waveguide. The first and second optical waveguides each have an asymmetric tapered region. A gyro according to any one of claims 1 to 5, wherein the gyro is provided. 20. The tapered region includes a first tapered portion and a second tapered portion, and an angle between one of the first and second tapered portions and an optical waveguide portion having a constant width is 90. The gyro according to claim 19, wherein the gyro is a degree. 21. The first laser has a first optical waveguide, and the second laser has a second optical waveguide. Each of the first and second optical waveguides has an optical element. 6. The optical element according to claim 1, wherein a transmission loss for a laser beam circulating in one direction is made different from a transmission loss for a laser beam circulating in another direction. Gyro listed on one. 22. The gyro according to claim 1, wherein the first and second lasers are semiconductor lasers. 23. The gyro according to claim 22, wherein said semiconductor laser has a quantum well structure. 24. The gyro according to claim 1, wherein the first and second lasers are gas lasers. 25. The gyro according to claim 1, wherein the first and second lasers are ring resonator type lasers. 26. The gyro according to claim 1, wherein the first and second lasers have a total reflection surface on a side surface of the waveguide. 27. The gyro according to claim 1, wherein the first and second lasers are driven by a constant current. 28. The gyro according to claim 1, wherein the first and second lasers are driven at a constant voltage. 29. The gyro according to claim 1, wherein the first laser is driven at a constant voltage, and the second laser is driven at a constant current. 30. The gyro according to claim 2, wherein at least a part of the first optical waveguide is arranged close to the exudation distance of the second laser light. 31. The gyro according to claim 1, wherein the electric signal is a signal that changes with rotation of the first and second lasers. 32. The gyro according to claim 1, wherein the electric signal is an electric signal of one of the first and second lasers. 33. The gyro according to claim 1, wherein the electric signal is a voltage signal. 34. The electric signal may be a voltage signal applied to at least one of the first and second lasers, a current signal applied to at least one of the first and second lasers, or the first and second lasers. 2. The gyro according to claim 1, wherein the gyro is an impedance signal of at least one of the lasers. 35. The gyro according to claim 1, wherein a beat frequency is detected based on a change in the electronic signal. 36. The gyro according to claim 1, wherein an angular velocity and a rotation direction are detected based on a frequency change of the electric signal. 37. The gyro according to claim 1, wherein at least one of the first and second lasers has an electric terminal for detecting an electric signal. 38. The gyro according to claim 1, wherein the electric signal is obtained by a photodetector disposed outside the first and second lasers. 39. The gyro according to claim 1, further comprising a frequency-voltage conversion circuit. 40. A device according to claim 1, further comprising a protection circuit.
A gyro described in any one of the above. 41. A gyro including a first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circulating in one direction as a main mode. Wherein the first laser has a first optical waveguide, and the second laser has a second optical waveguide, respectively, and at least a part of the first and second optical waveguides is optically coupled. A gyro comprising a third optical waveguide to be coupled. 42. A gyro including a first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circulating in one direction as a main mode. Wherein the first laser has a first optical waveguide, and the second laser has a second optical waveguide, respectively, and is connected to at least a part of the first and second optical waveguides. A gyro comprising the three optical waveguides. 43. A gyro including a first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circulating in one direction as a main mode. Wherein the first laser has a first optical waveguide, and the second laser has a second optical waveguide, and is shared by at least a part of the first and second optical waveguides. A gyro characterized by being. 44. The gyro according to claim 41, wherein the first and second laser beams have different oscillation frequencies. 45. The gyro according to claim 44, wherein an electric signal is detected from at least one of the first and second lasers. 46. A first laser generating a first laser beam circling in one direction as a main mode, a second laser generating a second laser beam circulating in one direction as a main mode, and a beat signal. A gyro having a detecting means, wherein the first laser light and the second laser light have different oscillation frequencies, and the first laser light and the second laser light interfere with each other. Gyro to do. 47. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first optical waveguide and the second optical waveguide are provided. The gyro according to claim 46, wherein at least a part of the wave path is arranged close to the wave path. 48. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is optically coupled. The gyro according to claim 46, further comprising a third optical waveguide coupled to the gyro. 49. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and is connected to at least a part of the first and second optical waveguides. 5. The apparatus according to claim 4, further comprising a third optical waveguide.
6. The gyro according to 6. 50. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is shared. The gyro according to claim 46, wherein: 51. A gyro according to claim 46, wherein said beat signal detecting means is means for detecting a voltage signal. 52. The beat signal detecting means, wherein
Or a voltage signal applied to a second laser, a current signal flowing through the first or second laser, or the first
47. The gyro according to claim 46, wherein the gyro detects an impedance signal of the second laser device. 53. The first or second laser,
The gyro according to claim 46, further comprising an electric terminal for extracting the beat signal. 54. The beat signal detecting means, wherein:
47. The gyro according to claim 46, further comprising a photodetector disposed outside the second laser. 55. The beat signal detecting means, comprising:
The gyro according to claim 46, further comprising a voltage conversion circuit. 56. A gyro according to claim 46, wherein said beat signal detecting means has a subtraction circuit. 57. A gyro according to claim 46, wherein said beat signal detecting means is provided with a protection circuit. 58. A first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circulating in one direction as a main mode, A gyro having a photodetector for receiving the first and second laser lights, wherein the first laser light and the second laser light have different oscillation frequencies, and the first laser light and the second laser light have different oscillation frequencies. A gyro, wherein the gyro interferes with the second laser light. 59. The first laser has a first optical waveguide, and the second laser has a second optical waveguide. At least a part of the first optical waveguide and the second optical waveguide are provided. The gyro according to claim 58, wherein at least a part of the wave path is arranged close to the wave path. 60. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is optically coupled. The gyro according to claim 58, further comprising a third optical waveguide coupled to the gyro. 61. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and is connected to at least a portion of the first and second optical waveguides. 6. The semiconductor device according to claim 5, further comprising a third optical waveguide.
The gyro according to item 8. 62. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and at least a part of the first and second optical waveguides is shared. The gyro according to claim 58, wherein: 63. The light detector, wherein the first and second light detectors are provided.
The gyro according to claim 58, wherein the gyro receives the laser beams simultaneously. 64. The gyro according to claim 58, wherein an electric signal is extracted from the photodetector and a beat signal is detected. 65. The gyro according to claim 58, wherein the first and second laser beams have different oscillation frequencies from each other. 66. The gyro according to claim 65, wherein the difference between the oscillation frequencies of the first and second laser beams is 100 Hz or more. 67. The gyro according to claim 65, wherein the difference between the oscillation frequencies of the first and second laser beams is 1 kHz or more. 68. The gyro according to claim 66, wherein the difference between the oscillation frequencies of the first and second laser beams is 10 kHz or more. 69. The gyro according to claim 62, wherein the circling directions of the first and second laser beams are opposite to each other. 70. The gyro according to claim 62, wherein the first and second laser beams have the same circumferential direction. 71. The gyro according to claim 62, wherein currents injected into the first and second lasers are different from each other. 72. The gyro according to claim 62, wherein voltages applied to the first and second lasers are different from each other. 73. The gyro according to claim 62, wherein the first and second lasers have different optical path lengths. 74. The gyro according to claim 62, wherein the first and second lasers have different optical waveguide lengths from each other. 75. The gyro according to claim 62, wherein the optical waveguides constituting the first and second lasers have a ring shape. 76. The first laser has a first optical waveguide, and the second laser has a second optical waveguide. The first and second optical waveguides each have an asymmetric tapered region. The gyro according to claim 75, provided. 77. The tapered region includes a first tapered portion and a second tapered portion, and an angle between one of the first and second tapered portions and the optical waveguide portion having a constant width is 90. The gyro according to claim 75, wherein the gyro is a degree. 78. The first laser has a first optical waveguide, and the second laser has a second optical waveguide, and the first and second optical waveguides each have an optical element. 66. The optical element according to claim 62, wherein a transmission loss for a laser beam circling in one direction is made different from a transmission loss for a laser beam circulating in another direction. Gyro listed on one. 79. The gyro according to claim 63, wherein at least a part of the first optical waveguide is disposed close to a distance from which the second laser light exudes. 80. A laser having a first laser that generates a first laser beam circling in one direction as a main mode, and a second laser that generates a second laser beam circling in one direction as a main mode. An apparatus, wherein the first laser light and the second laser light have different oscillation frequencies, and the first laser light and the second laser light interfere with each other. 81. A first laser that generates a first laser beam circling in one direction as a main mode, and a second laser beam circulating in one direction and having an oscillation frequency different from that of the first laser beam. A laser device arranged such that the first and second laser beams interfere with a second laser generated as a main mode; and an electric signal for extracting an electric signal from at least one of the first and second lasers A gyro including a detection unit. 82. A first laser generating a first laser beam circling in one direction as a main mode and a second laser beam circulating in one direction and having an oscillation frequency different from that of the first laser beam. A laser device arranged such that the first and second laser beams interfere with a second laser generated as a main mode; and an electric signal for extracting an electric signal from at least one of the first and second lasers A gyro including detection means.