JPH01124434A - Optical apparatus - Google Patents

Abstract

PURPOSE: To provide an optical device for inspecting a reaction of eyegrounds by a method wherein first and second diffractions of which the orders are different, of which the intensities are equal, and which are superposed, are generated, and in the superposed region, an interference pattern wherein a contrast is high, and a noise is low, is made, and the interference pattern is projected on a retina from only two point light sources of pupils of eyes. CONSTITUTION: A roof prism 46 is rotated around a vertical axis, and the angle of a stripe orientation in a stripe zone 37A, also rotates around an axis 41B by a double prism rotating angle. The stripe zone is transmitted to an opening wheel 47 by the roof prism 46. An optional opening of the opening wheel 47 is selectively aligned with the axis 41B. An eyepiece 48 receives a light which is transmitted through the selected opening, and forms two point light sources in the pupils of a patient. The stripe zone of the region 37A is transmitted through the pupils, and projected on eyegrounds. During an inspection, the patient makes his pupils 49 locate on the axis 41B in the vicinity of the eyepiece 48, and the two point light sources are shielded from the eyepiece 48. When the eyes of the patient are located at correct locations, the stripe pattern which is projected on his eyegrounds 50, can be sensed and seen.

Description

DETAILED DESCRIPTION OF THE INVENTION (Industrial Field of Application) The present invention relates to the field of optical measurements and testing, and more particularly for creating striped patterns on the retina of the eye. The present invention relates to an optical device.

[Conventional technology and its problems]

There are two basic methods for creating a striped pattern: That is, (11) an interferometry method that utilizes interference phenomena, and (2) a moiré method that utilizes projection and/or pattern multiplication.

There are numerous measurement and testing methods that utilize interference fringe patterns, as well as many methods for creating and controlling interference fringes. Generally, an interference fringe pattern is created when at least two coherent light beams interact. When two coherent beams interact, they interfere destructively to produce a dark spot or curtain, and interfere constructively to produce a bright spot or curtain.

Moiré fringes are created when two similar geometrically regular patterns of well-defined transparent and opaque areas are superimposed and subjected to transillumination. Some examples of geometrically regular patterns used to generate moire fringes include: (1) Ronchi lines, (2) concentric sets, and (3) radial lattices. The generation of moiré fringes can be considered as a projection. That is, the first
Moire fringes are created by projecting the shadow of the pattern onto the second pattern. The mathematical function describing the moiré fringes is obtained by multiplying the intensity transmission or irradiance of superimposed geometrically regular patterns.

The fringes generated by both interferometry and moiré methods are
For example, it is used by ophthalmologists to test fundus reactions. In one device of this type, light from a laser is split into two coherent beams by an optical element consisting of two adjacent Dove prisms. These two
The two beams are focused toward the eye, where they interact to create a fringe pattern on the retina.

In another device used in the optometric field, interference fringes are formed using a laser source and a conventional Ronchi line. A laser source generates a laser beam that is directed toward the Ronchi line. The Ronchi crevice splits the incident beam into multiple coherent beams of widely varying intensities. Selecting only two coherent beams and controlling the spacing of the interference fringes ultimately projected onto the retina requires complex manipulation of many optical and mechanical components.

In yet another optometric device, two Ronchi lines are used. These Ronchi lines create moire fringes that are ultimately imaged onto the retina.

Ophthalmologists use devices such as those described above that perform Moiré or interferometric methods to test and measure fundus reactions. This measurement is done by varying the "fineness" of the stripes projected onto the retina and monitoring the subject's ability to resolve them. A subject's ability to resolve a fringe pattern of a particular "fineness" is a direct measure of fundus response.

In some areas of measurement that are quite different from those mentioned above,
The fringes generated using interferometry or moiré methods are used to precisely position the two elements relative to each other.

In the case of interferometry, the incident light beam is generally split into two parts. One portion is reflected from the reference position and the other portion is reflected from the movable element. The reflected beams are recombined to produce an output fringe pattern.

This output fringe pattern moves as the movable element moves. In one example of the Moiré method, two high contrast Ronchi lines with slightly different spatial frequencies are superimposed and transmitted through illumination.

One Ronchi score line is fixed, while the other Ronchi score line is movable in a predetermined plane. Photodetectors sense changes in the light passing through the gratings and generate signals indicative of its movement.

Devices that utilize interferometry to form fringe backbones in various applications such as optometry and position sensing have certain drawbacks. For example, in this type of device, the two light beams typically follow different optical paths involving different optical elements.

If the optical elements in each optical path are not optically matched, the fringe pattern will be distorted due to aberrations. Aligning the optical elements would eliminate these aberration problems, but doing so would significantly increase the overall cost of the device; It is subject to various external influences such as changes. These external influences can cause the fringe pattern to move or create noise, resulting in inaccurate measurements.

The Moiré method is also subject to many limitations.

When close spacing and high precision are required, the geometrically regular patterns used to generate Moiré fringes can be very difficult and expensive to produce. If one of the score lines is moved adjacent to a fixed score line, the spacing between them must be kept constant, otherwise errors will occur. Furthermore, moire fringes are localized, meaning they exist only in a very narrow spatial region, and additional optical systems are required to image the moire fringes to a desired area. elements are often required.

Recently, one amplitude grating and one spatially coherent quasi-monochromatic light source have been used to create interference fringes. An oscillating grating is a nearly transparent to translucent medium whose opacity varies according to a spatially periodic pattern. An amplitude grating disperses or diffracts an incident light beam into a series of diffraction cones or orders. The intensity or amount of light in each order depends on the exact type of periodic opacity of the amplitude grating. The various diffraction orders have approximately the same intensity, but according to scalar diffraction theory for thin amplitude gratings, the main intensity resides in the zero-order undiffracted light, and the intensities of other diffraction orders may change. Estimated. This estimation has been confirmed in an actual application device.

In one application of this type, light from a light source is passed through an amplitude grating to produce cones of different orders of diffracted light, e.g.
It is proposed to create a cone of order and a cone of first order. To compensate for these different intensities, the diffracted light cone is reflected through a grating. After passing through the grating for the second time in this way, the 0th order cone of the reflection 1st cone and the reflection 0
The secondary cone has the same strength as the primary cone,
are combined to form a high contrast fringe field. This dual bus device closely approximates a common path interferometer and is therefore very stable. In a common path interferometer, the interfering beams follow the same optical path. Therefore, the disturbance effects act on both beams simultaneously and do not distort the output fringe pattern, which corresponds only to the difference between the two optical paths. However, this type of dual-pass system has various problems due to the difficulty in controlling grating substrate aberrations and mirror grating separation.

Further improvements have been made with the advent of holographically formed amplitude gratings. Holographic amplitude gratings are created by exposing a high resolution photographic emulsion to the precise interference pattern of a laser two-beam interferometer. During normal photographic processing, the photosensitive silver halide in the emulsion becomes opaque metallic silver to form an oscillating grating.

In one holographic grating application of this type, a dual-frequency holographic grating creates a so-called "jarring pattern. This grating connects a single photographic emulsion to a first laser interference pattern at a first spatial frequency f1. and then a second laser interference pattern at a second spatial frequency f1 and f2. Adjust the exposure for the pattern.Normally two sequential exposures are the same, but if f
. These exposure adjustments to achieve equal amplitude transmission modulation at f and f2 are typically made by trial and error.

When illuminated with spatially coherent quasi-monochromatic light, this dual frequency grating creates two primary light cones of equal intensity. One light cone is associated with fl and each of the 12 frequencies. These two primary light cones interact to form a very stable high contrast striped pattern. This kind of dual frequency holographic interferometer is also a common path interferometer, which is simple to construct. However, in this interferometer, it is necessary to separate the zero-order cone from the interfering first-order cone. This need for separation places a limit on the F-number of the input light cone and the amount of shift that can be obtained. Moreover, if the diffraction angles of the two primary cones are large, aberrational distortions will occur in the output line field. Furthermore, the ratio of output line field power to input power, or efficiency, is only about 2%.

For many years, people bleached photographic amplitude gratings to obtain "phase gratings." One basic form of such bleaching, known as volumetric bleaching, is the chemical conversion of opaque silver into a transparent high refractive index silver salt in a photographic emulsion.

A second form of bleaching, known as tanning, involves chemically removing developed silver in an emulsion, leaving voids. The tanned phase grating has a corrugated surface. Amplitude gratings selectively absorb light, whereas bleached phase gratings introduce a phase delay across the input light beam. As a result, phase gratings are much better than amplitude gratings, with a higher ratio of primary power to input power.

However, bleached grids generally present considerable problems. They are very noisy and can degrade and physically revert to amplitude gratings with prolonged exposure to light. Bleached gratings also have a lower spatial frequency response than amplitude gratings. Even though volume bleached gratings are nearly noiseless and have a higher spatial frequency response than their tanned counterparts, they are generally inferior and less efficient.

The efficiency of a volumetrically bleached lattice can be increased by increasing its thickness. However, increasing the thickness considerably drastically alters the fundamental diffractive properties of the grating. Any amplitude grating or phase grating can be considered thick if the physical thickness of the emulsion is greater than five times the grating spacing. And if the emulsion thickness is less than half the lattice spacing, the lattice can be considered thin. The properties of thick gratings can be accurately predicted by electromagnetic theory, and the properties of thin gratings can be described by scalar diffraction theory.

For example, the output of a thick phase grating consists of only the zeroth order and one first order diffraction cone. Furthermore, diffraction only occurs for plane wave force at a particular angle to the grating. On the other hand, a thin grating with the same spacing will absorb multiple orders (i.e., 0th order, ±1st order, ±2nd order, ±3rd order, etc.) for spherical or plane wave inputs at any angle to the grating. Occur.

The difference between thin amplitude gratings and thin phase gratings can be accurately predicted by scalar diffraction theory. When a perfect sinusoidal amplitude transmission droop is present in a thin amplitude grating, only the zeroth and ±1st orders of diffraction are present. When a complete sinusoidal phase gradient occurs in a thin phase grating, many orders (eg, 0th order, ±1st order, ±2nd order, ±3rd order) are seen. The strength of the phase grating order is proportional to the normal Bessel function (Jq(m/2))2. However, n is the order (for example, n=Q, ±1, ±2, ・
) and m is the strength or magnitude of the phase droop in radians. As the amplitude grating swell departs from a perfect sinusoidal shape, additional diffraction orders occur. The strength of these additional diffraction orders is directly related to the strength of the Fourier component associated with the lattice filter function.

In a phase grating, the diffraction orders associated with a non-sinusoidal phase droop can be predicted by convolving the individual outputs from each Fourier component of the phase droop.

Such amplitude convolution reveals complex phase relationships between orders related to just one particular Fourier component. Furthermore, when the phase aberration consists of two or more fundamental spatial frequencies, diffraction orders corresponding to the sum of frequencies and the difference between frequencies are generated. For example, one might consider bleaching a tri-frequency holographic grating to improve the inefficiency of the tri-frequency holographic grating described above. Bleaching increases the overall efficiency of such grids, but
The convolutional bleaching grating produces a desired fundamental frequency diffraction cone as well as sum and difference frequency diffraction cones that interact with the desired fundamental frequency diffraction cone.

Then, the diffraction cones of the sum and difference frequencies can destroy the fringe field.

In view of the above, it is an object of the present invention to provide an optical device for examining fundus reactions.

[Means for solving problems]

In view of the above object, the present invention provides an optical device for creating an interference pattern on the retina of an eye, which generates first and second diffraction patterns having different A0 orders, equal intensities, and overlapping each other. B. an interference pattern generator positioned to receive and receive the interference pattern from the interference pattern generator, thereby creating an interference pattern with high contrast and low noise in the overlapping region; An optical device further comprising: a focusing device for projecting onto the retina from only two point sources of light in the pupil.

The invention is particularly pointed out in the claims. The above and other objects and advantages of the present invention will be better understood with reference to the following description with reference to the accompanying drawings.

〔Example〕

A. Holoboot FIG. 1 schematically shows the arrangement of equipment necessary to expose a photographic plate during the generation of a holographic phase grating.

A holographic phase grating generated in accordance with the procedure schematically shown in FIG. 2 in the arrangement of FIG. 1 is the basis for the operation of various embodiments of the invention shown in the other figures. In particular, the device has a laser source 10 that transmits light along an axis 11. 1st
The other device shown separates the light into portions to travel on two separate optical paths and returns the separated beams to expose a photographic plate.

A conventional beam splitter 13 separates the light into two parts. The first part sends the light along an optical path that includes a mirror 14.15 for reflecting the light into the objective and pinhole 16, thereby creating a spherical wave emanating from a point source at the pinhole. The waves appear in cone 17 and are directed along axis 18 towards the photographic plate. beam splinter 13
The second optical path formed by includes a mirror 20 and an objective lens/hinghole 21, and creates a spherical wave cone 23 along the optical axis 23, which emanates from a point light source at a pinhole. The light sources from these two point sources combine to destructively interfere to create dark bands and to constructively interfere to create bright bands on photographic plate 12.

Photographic plate 12 is mounted on a rotating table to position photographic plate 12 and accurately form angle θ between axes 18 and 23. The spatial frequency ξ of the interference fringes at plate 12 is approximated by the following equation.

λ where λ is the laser wavelength. The interference pattern created by plate 12 is slightly hyperbolic and closely approximates a rectangular band, as shown in several figures.

To better approximate the rectangular band, plate 1
2 and each pinhole 16.21 along the axis 18.23.

The apparatus schematically shown in FIG. 1 was used to produce gratings having the desired properties characteristic of the present invention. This device is simple and relatively inexpensive.

For example, laser 0 is TEM. Consists of a mode laser,
Beam splitter 3 is a conventional variable density beam splitter capable of equalizing the intensities of the two beams. Mirrors 14.15.20 are standard plane mirrors. The objective lens is an 11 10x microscope objective, and the pinhole is aligned with the objective lens. The distance 18.23 is approximately 2 m. Using this particular device, the inventor produced 500 lines/n of interference fringes over a 3 inch by 3 inch area with a maximum fringe misalignment error of approximately 0.00254 mm.

Once the apparatus of FIG. 1 is in place, the photographic film emulsion can be exposed to the interference pattern shown in step 1 of FIG. During this exposure step, certain controls must be performed to ensure a good quality holographic grating. For example, exposure should be performed in a vibration-free environment.

Thermal disturbances should be minimized since air flow between beam splinter 13 and photographic plate 12 can distort the resulting interference fringes. In applications where very high concentrations and minimal distortions are required, the distance along axis 18.23 is 5.
m or even 10 m. λ and θ must be determined accurately. Although this basic equipment can be used to create highly accurate holographic gratings, ultimately maximum accuracy depends on the accuracy of the angle measurement equipment, the stability of the single frequency laser, and the atmosphere in which it is performed. It will be determined by thermal control.

In order to create a phase grating with specific properties that allow construction of the various embodiments disclosed herein, it is first necessary to create an amplitude grating. Given the commercially available photographic emulsions and developers, a developer is selected that is chemically compatible with the thin emulsion photographic plate. The method of strongly overexposing and underdeveloping the emulsion reduces the optical thickness of the treated emulsion to a refraction of its original physical thickness. Thus, by using the controls described in steps 1 and 2 of FIG. 2, an amplitude grating is created, which amplitude grating has the following characteristics:

1. It has an optically thin emulsion consistent with scalar diffraction theory.

2. After bleaching, the absorption function has a specific shape so as to transform into a corresponding specific phase transfer function.

3. After bleaching, the absorption function has a specific amplitude or intensity that transforms into a specific peak-to-peak phase modulation.

Specific plate types, exposures, development times and developers are discussed below.

Upon completion of step two development, the photographic plate is washed in step three in an acid development stop solution. This solution contains an acid curing agent. A 2 minute treatment in a hardener bath gives acceptable results.

In step 4, the emulsion on the photographic plate is fixed and hardened. A standard fixing bath and acid hardener was successfully used and the plate was immersed in the bath for approximately 10 minutes.

Next (step 5), the emulsion is prewashed for 30 seconds and hypodisinfected in a hypodisinfection bath for about 20 minutes. In step 6 the emulsion is washed (eg in filtered water for 30 minutes) and then soaked in a methanol bath until all residual sensitizing agent is removed (step 7).

Once the methanol bath is complete, the plate is dried with gentle dry air.

All of the foregoing steps are common photographic processing steps using commercially available chemicals. After completing step 7, an amplitude grid was created. Steps 8 and 9 transform this amplitude grating into a phase grating with the desired properties.

More specifically, after the photographic plate is thoroughly dried in step 7, it is bleached in bromine vapor during step 8 until the plate is clean. Once the bleaching operation is complete, in step 9 the plate is rinsed in a methanol bath to remove any remaining Br,2 and then thoroughly dried with a gentle dry air blow operation.

Certain features of these holographic phase gratings that are particularly desirable are discussed below. First, the exposure time, development time, and emulsion were selected to form a "thin" grid. As a specific example, the processing steps produce Kodak 131 by developing for 15 seconds in standard Kodak D-19 developer at 80@F with an average exposure of 200 ergs/ctl.
A grid of 393.7 dragons/dragon was formed on the -01 plate. Uniform development is achieved by using a large developer tank and by manually agitating the plate rapidly. Second
After being completely processed by the process shown, the resulting thin grating will diffract not only the input plane wave but also the input spherical wave, and as mentioned above, the thick grating will diffract the input spherical wave that is incident on the grating at a specific angle. Only plane waves are diffracted.

As a result of the measurement, the thin phase grating formed by the above process is
It was shown that it has a pure sinusoidal phase transfer function, and that its peak-to-peak phase lag makes the strengths of the zero-order and ±1st-order diffraction equal. By exposure of 200ergs/crl,
An average amplitude transmission of about 0.45 was obtained for the developed, unbleached Kogutsuk 130-1 plate. Experimental data confirm that a pure sinusoidal phase transfer function is maintained when the thin grating has an average amplitude transmission of 0.5 or less in the developed, unbleached state. The intensity of the final phase grating, or peak-to-peak phase lag, is within limits determined by the average amplitude transmission measured after step 7 of FIG.
It is adjusted by controlling step 1) in the figure. A very weak phase grating formed at a low exposure level produces a strong zero-order diffraction light, a weak first-order diffraction light, and a very weak second-order diffraction light. A strong grating formed at a high exposure level exhibits progressively higher power first and second order diffraction light and zero order diffraction light with lower power. Diffraction light having equal intensities in the zeroth order and ±1st order or diffracted light having equal intensities in the zeroth order and ±2nd order is created by trial and error adjustment of the initial exposure. The advantage of this thin diffraction grating that produces two different diffracted lights of equal intensity will be clarified in the following explanation of an interferometer using the diffraction grating.

Referring to FIG. 3 of Ikkage Ichigyoku Shosha, an interference type including a helium neon laser 30 is schematically illustrated, and this laser 30
is directed along axis 31 towards negative lens 32 . This negative lens 32 slightly expands the beam so that it completely fills the microscope objective 33. The microscope objective 33 focuses this light to a focal point FP at a distance Z from the holographic grating 34 configured as described above. The laser 30, the negative lens 32, and the microscope objective lens 33 constitute a light source of quasi-monochromatic divergent spherical waves emitted from the focal point FP. In one embodiment, the cone from focus FP is an f/2 cone.

When a spherical wave from a point source at focal point FP hits grating 34, grating 34 generates a number of diffraction cones. According to scalar diffraction theory, the intensity of the diffracted cone is governed by the Bessel function (Jn(m/2))'', where n is the diffraction order and m is the grating transfer function peak-to-peak phase lag in radians. According to the previously specified exposure and development times, m = 2 in λ = 6328 people.
, 870 values are obtained. The zero-order diffraction cone and the first-order diffraction cone are (JO(1,435)) ” = (J, (
1,435) ) ”, their strengths are equal.

Furthermore, the diffraction angles are such that the zero-order cone overlaps both first-order cones, while the first-order cones are only adjacent to each other. At several points a distance Z2 from the grating 34, an output as shown in FIG. 3 is formed. The zero-order cone appears as a plane circle 35 and consists of two 1
The next cones appear as planar circles 36A and 36B.

Regions 37A and 37B are overlapping regions;

Interference fringes are formed in the area. If the interference fringe at the center of region 37A is a dark band, the corresponding interference fringe in region 37B is a bright band. This bright and dark band does not imply that both bands have the same intensity across the band as shown in the figure. Although the naked eye perceives distinct alternating bands depending on the illumination conditions, in reality the interference fringes change smoothly,
It is proportional to the square of the sine wave function.

Since a pure sinusoidal phase transfer function is associated with grating 34, there is a 180° phase shift between the interference fringes of region 37A and region 37B. If the grating 340 phase transfer function deviates from a pure sine wave, the interference fringes of regions 37A and 37B will have other phase relationships that are not equal to 180@. This 180" phase shift is not an essential problem in forming high-contrast interference fringes, but is important when applying a rectangular electrical signal to position detection generated from a central interference fringe. Controlling the shape is achieved by selecting the appropriate combination of emulsion, developer, exposure time, and development time as described above.

The interferometer shown in FIG. 3 has several characteristics.

As the distance Z changes, the number of interference fringes in the overlapping regions 37A and 37B changes. Specifically, when the distance ZI is reduced, the number of interference fringes appearing in the overlapping region becomes smaller. When the distance Z changes, the area 37A and the area 37B
“flows into” or “flows out” from.
The flow of interference fringes causes the central interference fringe to widen or narrow, but the central interference fringe does not move.The central interference fringe remains located at the center of its respective region.

The importance of the movement of the center interference fringes regarding this change in ZI will be discussed later. If the grating 34 moves in a plane perpendicular to the axis 31 and perpendicular to the direction of the interference fringes, then the area 37A
The interference fringes in region 37B and 37B all appear to slide through that region, but the number of interference fringes in that region remains unchanged. If the distance Z2 changes, the number of interference fringes likewise remains the same, but in this case their magnitude changes; the width of the interference fringes becomes smaller as the distance Z2 becomes smaller. The parameters of the meter are related by the following formula.

(2J T= (Z2+ZI)/ξZ1 where, T
is the interference fringe period of the overlapping regions 37A and 37B, and ξ
is the spatial frequency of the grating 34 determined by equation (1), and 2.
and Z2 is the positive direction distance shown in FIG.

Since the holographic grating interferometer of FIG. 3 is essentially a common path interferometer, it is fairly stable and is not susceptible to fringe distortion due to external influences. Atmospheric changes, i.e. airflow and thermal inconsistencies, do not distort the interference pattern. Furthermore, since the phase grating is substantially transparent and relies entirely on time delays within the grating 34 to form the diffraction cones, the light intensity of each of the diffraction cones is substantially different from the amplitude grating. Much more than what you get all the time. As a result, the overall brightness of the interference fringes increases. Moreover, since the strength of each of the zero-order cone and the first-order cone is equal,
Destructive interference and conducive interference tend to be complete;
Thus, the black band becomes substantially black, while the bright band becomes essentially twice as bright as standard light. This grating thus creates a simple common-path interferometer that produces bright, high-contrast interference fringes.

The above characteristics make bleaching phase gratings applicable to different fields.
This provides the basis for understanding two specific application examples. In one example, the distance Z1 is intentionally varied to vary the number of interference fringes that appear in a given area. A device embodying this feature is particularly suitable for use in a fundus reaction testing device, which is shown in Figures 4 to 7B.
This will be described later with reference to the figures. In another application, the distance ZI
and Z2 are essentially unchanged, but the grating is moved, thereby shifting the interference fringes. Devices embodying this feature are particularly suitable for use in positioning devices. In a third application, an auxiliary optical device is placed in front of the grating to form two spatially coherent light sources with the light transmitted through two three-dimensional transmissions. These two become coherent. In the case of Z2=■, the interference fringes, that is, the contour lines observed at the rear focal plane of the lens placed behind the grating disappear. The phase grating used in this application example is the same as the one described above, except that instead of using light with equal intensities of zero- and first-order diffracted lights, we use light with equal intensities of zero- and second-order diffracted lights. is the same as

C,l Cardiac Test Apparatus The fundus reaction test apparatus of FIG. 4 includes a laser 40, which is a low power TEMO laser.

It may be a mode helium neon cylindrical laser or other similar laser. Light from the laser is sent along axis 41A through filter wheel 42. The filter wheel 42 includes a number of conventional metallized intermediate density filters. These filters control the intensity of light sent to other elements of the fundus response testing device. Similarly, the brightness of the interference fringes finally projected onto the patient's fundus can be controlled.

Negative lens 43 and microscope objective 44 are movable along the axis and focus the light at focal point EP. Negative lens 43 slightly diffuses the beam from the laser so that the aperture of microscope objective 44 is completely occupied with a uniform light distribution.

A double concave lens with a focal length of -4 m is a satisfactory negative lens. The microscope objective 44 is a conventional objective; a 10 XN, A, 0.25 objective is satisfactory.

The grating 45 consists of a holographically recorded single frequency phase grating, which is made as described above. The grating frequency is 400 lines/fi to allow for ideal separation of the zeroth and ±1st orders from the human cone of the N, A, 0.25 objective lens.

Grating 45 is also optically thin and the zeroth and first diffraction orders have equal lengths. As will become clear later, there is no reason to control the phase of the output line from grating 45 when the grating is used in a fundus reaction testing device. Therefore, additional constraints on processing procedures associated with preventing pure sinusoidal phase disturbances are eliminated. A convenient development time is chosen that is compatible with the conditions for producing an optically thin emulsion. The exposure time is adjusted by trial and error until a predetermined intensity of phase modulation is obtained.

In such a case, a modulation is obtained that produces zero and ±1 orders of equal strength. A thin, extremely clean, low-noise 400 line/Tsuru phase grating for fundus reaction testing equipment can be fabricated on a Kogutsuk 120-01 plate with an average exposure of 6328 people and 1000 ergs/-. These plates are developed in a Kodak D-19 developer at a temperature of 68'F for 1000 seconds (steps 1 and 2 in Figure 2). Steps 3 through 9 of FIG. 2 are used to complete the process.

The grating 45 creates a divergent cone of different orders of diffraction. In detail, the zero-order cone indicated by circle 35 and the zero-order cone indicated by circle 3
There is a cone of first order shown by abutting 6A and 36B.

These cones are of equal length, so they produce high contrast fringes as shown in areas 37A and 37B, where the zero and first order cones overlap. In this particular embodiment, axis 41B extends from the center of grid 45 to region 37.
Extend through the center of A. Dowel prism 46 is positioned to receive the striped area and has its longitudinal axis aligned with axis 4
It is placed above 1B. Dowel prism 46 is rotated about its longitudinal axis so that striped area 37A
The angle of the fringe orientation within the axis 41 is also twice the prism rotation angle.
Rotate around B.

The striped area is transmitted via dowel prism 46 to aperture wheel 47 . Any aperture in aperture wheel 47 is selectively aligned with axis 41B by rotating aperture wheel 47. Eyepiece 48 receives light transmitted through the selected aperture. This eyepiece 48 forms two point sources within the patient's pupil. These point light sources correspond to the point light sources formed in FIG. 1 by the objective lens and pinholes 16 and 21. The striped area of region 37A is transmitted through the pupil and projected onto the fundus.

During the examination, the patient positions his pupil 49 close to the eyepiece 48 (and on the axis 41B) to block the two point light sources from the eyepiece 48. With the patient's eyes in the correct position, he will sense and see the fringe pattern projected onto the fundus 50 of the eye.Since the optical capabilities of the cornea and eye lens are negligible in such devices, the effect of the fringe pattern projected onto the fundus is negligible. .

The negative lens 43 and the microscope objective lens 44 are connected to the slider 5
1, the slider 51 can be moved in the axis 41A, thereby repositioning the focal point (EP) with respect to the grating 45.

As slider 51 and focus (FP) are repositioned, the number of fringes within fringe map area 37A changes. The patient's ability to see and discriminate a given number of fringes within the area projected onto the patient's fundus is shown to be directly equivalent to a standard measure of response.

During fundus examination, dowel prism 46 and aperture wheel 47
operates subtly, yet plays an important role. This is because fundus examination is rather subjective. The examiner can control the orientation of the stripes by rotating the dowel prism 46, which determines whether the patient's claim to be able to see the stripes in that orientation is actually valid. To the extent that fundus responses may exhibit orientational changes, the nature of such changes can also be evaluated.

The diameter of the aperture selected by the positioning of the aperture wheel 47 controls the size of the fundus area stimulated by the stripe pattern. Such area control is important in determining the range of patchy regeneration. The fundus area revealed by the various apertures of the aperture wheel 47 consists in the special case of 20°.
The angle ranges from 0.5° to 0.5°. These areas have a diameter of 5
．． It corresponds to a circular area stimulated to the fundus in the range of 0 to 0.15 m.

Figure 5 shows a number of striped patterns, which are
This will be perceived by the patient being examined using the apparatus shown in FIG. When the slider 51 is placed in an intermediate position, the patient can perceive a striped pattern of alternating dark and light bands. Note that this pattern is illustrated as pattern A. If a laser that emits red light is used, the light areas will be red and the dark areas will be black. The patient thus perceives a series of straight red and black lines. As slider 51 moves toward grating 45 along axis 41A in FIG. 4, the number of stripes decreases and the patient perceives pattern B, which includes relatively fewer wide stripes. Similarly, as the slider 51 is moved away from the grid beyond the intermediate position, the number of stripes increases, as shown in pattern C. On the other hand, if slider 51 is in the same position producing pattern A, rotating dowel prism 46 of FIG.

Another embodiment of the fundus reaction testing device is shown in FIG. This fundus reaction testing device differs from the fundus reaction testing device shown in FIG. 4 in that an observation system for the examiner is added. This observation system uses the common path principle in area 37A.
It is applied to the superposition order that produces , so it can be added. A variety of viewing system designs are available. This is because the special component selection eliminates the fringe distortion problem. However, to ensure the best viewing system performance, the viewing system components should be of reasonable quality.

The observation system shown in FIG. 6 includes a beam splitter 52 arranged between an aperture wheel 47 and an eyepiece 48.
has. Beam splitter 52 directs white light through fiber optic guide 53 and through eyepiece 48 to the eye. A standard low power fiber optic illuminator (not shown) can be used as the fiber guided light source. Light reflected from the eye passes through eyepiece 48, beam splitter 52, and an aperture in aperture wheel 47 aligned with axis 41B to another beam splitter 54. usually,
The largest aperture is aligned to provide the largest area of field of view. Beam splitter 54 directs this light onto concave mirror 55, which forms a real image of the surface of the eye in the vicinity of beam splitter 54. Lens 56 transmits a real image of the surface of the eye through polarizer 57 to the focal plane of eyepiece 58 for viewing. Polarizer 57 is dowel prism 46
and another crossed polarizer 59 between the beam splinter 54 and the beam splinter 54 to eliminate that portion of the fringe pattern area that is reflected from the beam splinter 54 towards the eyepiece 58 . Aberrations of the viewing system are reduced by placing the aperture wheel 47 in the center of the curvature of the mirror 55 and by using a 1:1 conjugate symmetrical relay lens 56, which are most commonly encountered in eye exams. One problem, even with the best chinrest, is positioning the patient's eyes. In a properly aligned viewing system of the type shown in FIG. Matched. Thus, when the examiner properly positions the patient's pupil to intercept the two coherent point light sources, the examiner will observe a sharp, centered image of the pupil through the eyepiece 58. Observation systems are particularly useful for examining cataract patients.

This is because the viewing system allows two coherent point sources to be precisely positioned at any aperture present in the cataract.

7A and 7B are two views of a fundus reaction testing device constructed in accordance with the present invention. This special fundus reaction testing device has the elements shown in FIG. For details, please refer to the housing 6 for the fundus reaction testing device.
0, and the housing 60 has a normal laser unit 6
1 is provided and extends from one end 62 of the housing 60. Laser 61 is coupled to a conventional laser power supply 63.

Various elements within housing 60 are supported on substrate 64. The first element has an upright stand 65 that supports the filter wheel 42. The inspector uses filter wheel 4
Rotate a portion around 2. Filter wheel 42 extends through a slot in top plate 67 of housing 60 to position the appropriate filter on the optical axis. Even though the angular position of the filter wheel 42 is maintained by friction, positive positioning means may be incorporated into the detent indexing mechanism to interact between the upright stand 65 and the filter wheel 42.

A negative lens 43 and a microscope objective lens 44 shown in FIG. 4 are attached to a housing 70 supported by a slider 51. The rotating cam 71 has a shaft, which is
It extends through side wall 72 of housing 60 and is supported by stand 72A. This shaft is the positioning protrusion 7
3, supporting the scale 74 and a detent mechanism, not shown. Scale 74 is 20/15 to 2
Calibrated directly in the equivalent Snellen reaction in the range 0/400. When the examiner rotates the protrusion 73, the cam 71 rotates and moves both the slider 51 and the negative lens 43 and microscope objective lens 44 in the vertical direction, thereby moving the focal point FP to the position shown in FIG. change. In this embodiment, slider 51 is constituted by a cam follower, which contacts cam 71 and is supported by slide 75. Slide 75 also includes a spring to force slider 51 against cam 71.

Another upright stand 76 is supported on the base plate 64.

Stand 76 supports grid 45. Thus, when the power supply 63 is activated, the light beam emitted by the laser 61 passes through the filter wheel 42, the negative lens 43, the microscope objective 44 to the grating 45, thereby having zero and equal intensities. And the first polymerized
resulting in an order diffraction cone. In one special arrangement,
The distance between the grating 45 and the focal point is approximately 0.6 to 25 degrees.
Varies across the range of cranes. Depending on the range of distances mentioned above, the device can produce striped patterns corresponding to 20/400 to 20/15 response measurements.

Another stand 77 is placed in a fixed position on the base plate 64. This stand places the longitudinal axis of the dove-shaped prism 46 on the axis 41B shown in FIG.
It is slightly slanted. Stand 77 supports rotatable wheel 80. A portion of the car 80 is located at the top 6
7 through another slot. The wheel 80 supports the dove-shaped prism 46 such that rotation of the wheel 80 by the inspector rotates the dove-shaped prism 46;
The orientation of the fringe is changed as shown in pattern D in FIG.

The next element in the tester is axis 41B in FIG.
The end wall 81 supports the upper window wheel 47 and the eyepiece 48. A portion of window wheel 47 extends through a slot in wall 60 to allow the inspector to center the various windows on axis 41B shown in FIG. Furthermore, the end wall 81 has two cutouts 82 and 83 in the outer part of this wall. These notches are offset on both sides of the eyepiece 48. This allows the patient's nose to be positioned relative to the housing during the examination. For example, the patient may place his nose in the notch 82 during an examination of his right eye.

From the above discussion, it will be apparent that the fundus reaction testing device disclosed in Figures 7A and 7B is simple and easy to construct. All optical elements other than grating 45 are conventional elements that are readily available and relatively inexpensive. Such elements are used because the fundus reaction test device is an example of a common path interferometer and because the fringes are not subject to thermal changes, vibrations, or other environmental perturbations.

D0 Position Encoder According to another aspect of the invention, the interferometer shown in FIG. 3 is adapted to be readily used in position control schemes.

As already pointed out, polymerization zone 37A in FIG.
The stripes at and 37B move through the overlapping area in the direction of movement of the grating. Moreover, if the distance Zl between the focal point FP and the grating remains constant, the number of fringes in the overlapping area remains constant. On the other hand, if the distance Z
2 changes, the number of fringes in the polymerization zone remains the same, but the polymerization zone changes, as expected in a projection-based approach.

A special embodiment of a position encoder used in a wide range of measurement and control functions is disclosed in FIG. 8th
In diagram A, the light rays emanate from a point source of quasi-monochromatic, spatially coherent light. A holographically recorded single oscillating phase grating 101 is supported on a support 102 which moves in the X direction in the XY plane perpendicular to the beam or X axis.

The light beam from the light source 100 is diffracted into zero and first order cones of equal intensity by a grating 101 supported on a support 102. The zero order distribution is represented as a flat circle 103 - at the same time the two first order distributions are represented by flat circles 104 and 105. Polymerization zone 10
The fringes at 6 and 107 are photodetector 110
and 111, these photodetectors generate input signals for position detection circuitry 112, which is well known in the art.

Referring to FIG. 8B, photo detectors 110 and 111
are oriented horizontally to the polymerization zone 106 or to the centerline occurring on the axes 120 and 121, respectively. As previously explained, control of the shape of the grating phase transfer function can cause the fringes in a polymerization zone to be 18 out of phase with the fringes in other polymerization zones.
0" off. As shown in FIG. 8B, photo detector 110 is aligned with the dark band at the centerline position, while photo detector 111 is aligned with the light band at the centerline position. Photo For detection purposes, this special embodiment is particularly simplified when the light source 100 generates a red or near-infrared light beam as a photographic detection cell,
Such photographic diodes are particularly sensitive in areas of the spectrum.

If support 102 moves a little to the right in FIG. 8A along the X-axis, the stripes move with it. After a large movement, the photographic detector 110 in FIG. 8B
The band impinging on and 111 moves to the position shown in FIG. 8C. The bright band impinges on photo detector 110 and the dark band impinges on photo detector 111. Moshi lattice 1
If 01 has a phase pattern of 400 lines per 1n, this twice change represents a movement of approximately 0.0127+n (approximately 0.000050 inches) along the X-axis. Even with this precision, the device is relatively easy to construct because the swath that impinges on the photodetector is relatively wide, e.g., approximately 0,1 inch wide. The band with
Z2 is equal to approximately 2 inches; and 2.
is approximately equal to 0.0254 TIM (0,001 inch). See equation (1), a band of this width facilitates placement of the photodetector. This is because those locations are made with sufficiently loose tolerances.

The device includes a grating 10 along axes 120 and 121.
1 and the photographic detector 110.111 is essentially insensitive to any change in distance between the photographic detector 110.111. As already pointed out, the size of the stripe fields 106 and 107 will change if Z2 changes, but the number of stripes within that field will not change.

Thus, in FIG. 8B, photodetectors 110 and 111 are located at a distance Z along axes 120 and 121.
2 is centered on each centerline, regardless of any variation in the 2.

The point light source 100 shown in FIG. 8A is similar to the laser 4 in FIG.
0. It consists of elements such as a negative lens 43 and a microscope objective lens 44. With a light source of this construction, the laser radiation can fully fill the objective lens, thus creating a well-bounded radiation field that is radially symmetrical, as shown in FIG. 8A.

On the other hand, a single laser diode can also only
Alternatively, it can be used in combination with the microscope objective lens 33. The shape of the laser diode emitting area is approximately rectangular instead of circular. Therefore, when the laser diode is used by itself, the zero and upper order distributions are
In FIG. 8A, the XY When a laser diode and a microscope objective are used in combination, the laser diode radiation can fully fill the microscope objective. Therefore, a large radial A symmetrical and well-bounded radiation field is created.For any light source, a discussion of encoders at various positions can be found in Section 8A.
The ideal representations 103, 104 and 105 of the diagram are unaffected and are completely valid.

While the apparatus of FIG. 8A is used to make measurements in one direction, FIG. 9A discloses a support 122 that moves in both the X and Y directions. Grating 123 is different from grating 101 of FIG. 8A, and the difference can be readily appreciated by referring to FIGS. 1 and 2. When forming the grid 123, the photographic plate 12
In the figure, with reference to step 1, it is exposed as already described. However, the photographic board was rotated 90″,
It is exposed again and then developed. This double exposure
Creates a superimposed horizontal and vertical single frequency interference pattern.

Referring again to FIG. 9A, when grating 123 is illuminated with an arbitrary source of quasi-monochromatic spatially coherent light, the grating
Five diffraction cones are created, generally shown in FIG. 9A and clearly shown by planar projection in FIG. 9B. The vertical phase pattern on the grating is circular 1 as already described.
Create a cone represented by 03 to 105,
These cones create polymerization zones 106A and 107A. However, the horizontally oriented phase pattern creates a pair of first order cones in the vertical direction, indicated at 114 and 115. Four polymerization zones are important. Pointed wedge-shaped areas 106A and 107A correspond to areas 106 and 107 in FIG. 8B, which are not affected by the first order cones 114 and 115.

The pointed wedge-shaped areas 116A and 117A are formed by superimposing the zero order cone 103 and the first order cone 114, 115 and are independent of the influence by the first order cones 104 and 105. The photodetector is aligned in the center for each polymerization zone. Photo detectors 110 and 11 aligned in areas 106A and 107A
1 corresponds to movement along the X-axis, as already discussed.

Photo detectors 120 and 121 are aligned with areas 116A and 117A. These sense vertical movement along the X-axis. These four photo detectors are coupled to position detection circuitry 124, which is responsive to the signals to indicate XY movement or to create inputs to the XY positioning servomechanism.

FIG. 10 schematically shows a device for generating a rectangular signal.

Basically, this device is used by adding light receiving elements 125 and 126 to the device shown in FIG. 8A. The light receiving elements 110 and 111 are shifted upward, but are located above the central interference stripe. Additional photoreceptors 125 and 126 are located one quarter interference fringe to the right of each central interference fringe (i.e., 90° out of phase, or in a rectangular position). As will thus be readily apparent, the signals from these four photodetectors provide a rectangular signal that provides both position and orientation information in an incoherent manner.

In each of the above applications, it is assumed that the distance Z+ between the point source and the grating remains constant.

However, it is clear that such fixed dimensions
difficult to achieve in some practical applications. Figures 11A and 11B disclose a device that is essentially insensitive to changes in dimension Z1 over a reasonable range. The device is also shown in conjunction with a device for detecting movement in the X direction only. The resulting signal is sent to a location device 127 having an up and down counter to count the passage of interference stripes and to provide accurate movement instructions.

More specifically, the laser light source 100 transmits light through the grating 101, creating 0th and 1st order cones 103, 104 and 105 with overlapping regions 106 and 107. As shown in FIG. 11B, the light receiving element 11
0 and 111 provide the first group of signals. Another light source 130 is located below light source 100. This light &(130 is positioned to create a 0th order cone 133 and 1st order cones 134 and 135 located below the diffraction cone created by the light from the light source 100.The horizontal or X position of the light source 130 is , the central interference stripe 9 of the central interference stripe overlapping regions 106 and 107
Adjustments are made to create overlapping regions 136 and 137 that are 0° out of phase. Photodetectors 140 and 141 are aligned with the central interference stripes of overlapping regions 136 and 137.

With this arrangement, a rectangular signal is generated from four central interference stripes whose position does not change with changes in Zl. As Z increases, the width of the central interference stripe decreases, but if the aperture of the photodetector can resolve the central interference stripe, then
A precise rectangular signal is generated.

Single frequency holographic phase gratings previously disclosed in connection with position sensing and fundus response testing applications can be readily used as Fourier plane filters. FIG. 12A shows that the key components are the single frequency holographic phase grating 2.
07 is shown. The overall apparatus of Figure 12A is very well known as an interferometric optical processor. Laser 200 and beam expander/collimator 201 are sources of spatially coherent quasi-monochromatic plane waves 203. Two stereo transparent bodies 204 and 205 are placed in the front focal plane of lens 206 and are transilluminated by plane wave 203. The Fourier transforms of the waves transmitted by both stereo transparent bodies are presented at the holographic phase grating 207.

A grating 207 is arranged along the axis and mounted above the micro-positioner so as to constitute a cosine phase filter for the Fourier-transformed light distribution. Lens 208 then converts the filtered Fourier-transform distribution into plane 20
An output image is formed at 9.

The important output image shown in FIG. 12B is a coherent version of the two real image distributions. The "output images" 210 and 211 are therefore not images in the classical sense. “Output image” 21
An important feature of 0 is the dark interference fringes corresponding to contour contours. The contour line 210 is a line-of-sight contour line that can be seen through the original transparent body 205 and its classic image 205A. "Output image" 211 contains the same contour lines as 210, but in this case the contour lines are different from those of the original transparent body 2.
04 and its classic image 204A. The outline of the "output image" 210 is such that the 0th order cone created by the grating 207 in response to the light from the transparent body 205 and the +2nd order cone created by the grating 207 in response to the light from the transparent body 204. This overlaps with Similarly, the outline of the "output image" 211 is the same as that of the transparent bodies 204 and 2.
Gratings 207 each created in response to light from 05
It is created by the overlap of the 0th and 12th order diffraction cones from . Lens 208 forms a classical real image of the contour in plane 209. Other contour contours can be created by mechanically varying the separation B of the original transparency 204 and 205.

The key component of this device is a grating 2 that produces classical images of different orders that overlap to form contour lines.
It is 07. -Layers In particular, the grating 207 is an optically thin holographically constructed phase grating of 901/w. In this particular application, the peak of the lattice transfer function
The toe-peak phase lag is equal in strength to the 0th order and ±2
This is the value required to create the second order diffraction cone, ie 3.68 radians. Furthermore, the phase transfer function must be a purely sinusoidal function so that the second order diffraction cone can be 180° out of phase with the O order diffraction cone so that complete extinction occurs between the overlapping orders. Classic statues 204A and 2
If 05A is the same, the dimming is complete and a dark contour line or contour interference stripe is created.

A grating 207 can be created on top of the AGFA8E75 emulsion exposed to the 901/n interference fringe created by the optical apparatus of FIG.

Average exposure was 80” by Kodak D-76 developer.
F, development time 45 seconds, 2 at 6328 people
000erg/crM. When creating relatively low vibration gratings, the tanning action of the developer creates undesirable phase disturbances. Therefore, a weak tanning D-76 developer and chemically compatible AGFA8E75 emulsion were chosen to create the 901/+n lattice.

While maintaining the pure sine wave phase disturbance effect, 0 with equal strength
The exposure adjustment method described above is used to obtain the first and second order diffraction cones from the final phase grating. The remaining steps 3 through 9 of FIG. 2 are used to complete the process.

In summary, we have disclosed a basic interferometer structure that utilizes a holographically recorded single-frequency bleached phase grating to create high-contrast, stable interference fringes with high efficiency. Furthermore, three different applications of this interferometer are disclosed: for testing fundus responses, for sensing or controlling the position of mechanical elements, and for creating contour lines. Furthermore, a special example of a fundus reaction tester is disclosed.

It will be apparent, however, from the foregoing description that the particular embodiments of the invention disclosed are merely representative. The basic principles can be used in a wide variety of applications to obtain some or all of the advantages of the invention. It is therefore intended that the appended claims cover all such modifications as come within the true spirit and scope of the invention.

FIG. 1 is a schematic diagram showing an apparatus for producing a holographic grating according to the invention; FIG. 2 is a chart showing the various basic steps for processing a holographic grating according to the invention; FIG. Figure t is a schematic diagram of an interferometer constructed in accordance with an aspect of the present invention for creating interference fringes; Figure 4 is a schematic diagram of an apparatus constructed in accordance with the present invention for measuring fundus responses; 4 shows typical interference fringes produced by the fundus reaction device shown in FIG. 4; FIG. 6 is a schematic diagram of an alternative embodiment of a fundus reaction test device constructed in accordance with the present invention; and FIG. FIG. 7B is a perspective view of the fundus reaction test device shown in FIG. 7A.
8B is a detailed perspective view with the housing partially removed; FIG. 8A is a schematic illustration of one embodiment of a position encoder constructed in accordance with the present invention; FIGS. 8B and 80 are the apparatus shown in FIG. 8A. FIG. 9A is a schematic diagram of an alternative embodiment of a position encoder constructed in accordance with the present invention for sensing motion along orthogonal axes, and FIG. 9B is a schematic illustration of an alternative embodiment of a position encoder constructed in accordance with the present invention. 9A shows a typical interference pattern produced by the apparatus shown in FIG. 10, modified to form a rectangular signal, FIG.
FIG. 11A is a schematic diagram of a position encoder for producing a stable rectangular signal; FIG. 11B shows the interference fringes produced by the position encoder of FIG. 11A; FIG. 12A is a schematic diagram of an apparatus for generating contour lines of equal height from a pair of vertical stereographs, and FIG.
2 is a schematic diagram useful in understanding the operation of the apparatus shown in FIG.

Claims (3)

[Claims] (1) An optical device for creating an interference pattern on the retina of the eye, comprising: A, first interference patterns of different orders, equal intensities, and overlapping;
B. an interference pattern generator positioned to receive the interference pattern from the interference pattern generator; , a focusing device for projecting an interference pattern from only two point sources in the pupil of the eye onto the retina. (2) The interference pattern generator comprises: i) a spatially coherent light source of quasi-monochromatic light; and ii)
Optical device according to claim 1, comprising: a holographically recorded single frequency phase grating device for producing diffraction in response to energy from the light source. (3) C. a second focusing device disposed between the light source and the grating device for focusing light to a focal point that is displaced from the grating device toward the light source; and D. the second focusing device; 2. The optical device according to claim 2, further comprising: a focusing device and a positioning device coupled to the grating device to move the focal point relative to the grating to change interference fringes.