WO2022018891A1

WO2022018891A1 - Light source device

Info

Publication number: WO2022018891A1
Application number: PCT/JP2021/003622
Authority: WO
Inventors: 旭洋山田; 博木田
Original assignee: 三菱電機株式会社
Priority date: 2020-07-21
Filing date: 2021-02-02
Publication date: 2022-01-27
Also published as: JPWO2022018891A1; JP7446432B2; WO2022018819A1

Abstract

A light source device according to the present disclosure comprises: a collimating lens that collimates incident light; a light source group that includes a plurality of light sources disposed apart from one another in a direction separating away from the optical axis of the collimating lens and that overall emits a beam of light having a divergence angle which differs in a first direction and a second direction, the first direction and the second direction being perpendicular to one another and being each parallel to a direction separating away from the optical axis; and a light deflecting element that is disposed between the light source group and the collimating lens in the optical axis direction and that deflects the light emitted from each of the plurality of light sources in a direction separating away from the optical axis to cause the light to be incident on the collimating lens in the first direction, in which the divergence angle of the light source group is smaller from among the first direction and the second direction.

Description

Light source device

This disclosure relates to a light source device, and particularly to a light source device having improved light utilization efficiency.

In solid-state light sources used in projection-type display devices, high output and improvement of coupling efficiency have become issues. For example, Patent Document 1 describes a light source having a plurality of light emitting points, a collimating lens that parallelizes the light emitted from the light source, and a plurality of lenses having different inclination angles with respect to the main surface and for each of the plurality of emitted light. A light source unit composed of an optical element having an incident surface of the above is disclosed. Patent Document 1 discloses, in particular, a configuration in which an optical element has a plurality of mirrors provided with an incident surface in order to realize miniaturization of a light source unit.

International Publication No. 2014/115194

In the configuration using a mirror as in Patent Document 1, if the light amount distribution of the parallelized light rays emitted from the collimating lens becomes non-uniform with respect to the optical axis, the light utilization efficiency on the optical axis decreases. However, Patent Document 1 does not consider the decrease in light utilization efficiency on the optical axis due to the apparent tilt of the light source.

The present disclosure has been made to solve the above problems, and an object of the present disclosure is to provide a light source device having improved light utilization efficiency on the optical axis.

The light source device according to the present disclosure includes a parallelizing lens for parallelizing incident light and a plurality of light sources arranged apart from each other in a direction away from the optical axis of the parallelizing lens, and the light as a whole is orthogonal to each other. A group of light sources that emit light sources having different divergence angles in the first direction and the second direction parallel to the direction away from the axis are arranged between the light source group and the parallelizing lens in the direction of the optical axis. Of the first direction and the second direction, in the first direction in which the divergence angle of the light source group is small, the light emitted from each of the plurality of light sources is deflected in a direction away from the optical axis. It is provided with a light deflection element for incident on the parallelizing lens.

According to the light source device of the present disclosure, it is possible to provide a light source device having high light utilization efficiency on the optical axis.

It is a figure which shows the schematic structure of the light source apparatus of Embodiment 1. It is a figure which shows the schematic structure of the light source apparatus of Embodiment 1. It is a figure which shows the light distribution characteristic of the light source of the light source apparatus of Embodiment 1. FIG. It is a figure which shows an example of the ray tracing of the light source apparatus of Embodiment 1. FIG. It is a figure explaining the operation of the light deflection element of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the schematic structure when the light deflection element of the light source apparatus of Embodiment 2 is replaced with a mirror. It is a figure which shows the ray tracing result of the light source apparatus of Embodiment 2. It is a figure explaining the inclination angle with respect to the optical axis of the light ray emitted from a light source. It is a figure which shows the back light tracking result of the light source apparatus of Embodiment 2. FIG. It is a figure which shows the back light tracking result of the parallelizing lens of the light source apparatus of Embodiment 2. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 2. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 2. It is a figure which shows the back light tracking result of the mirror of the light source apparatus of Embodiment 2. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 2. It is a figure which shows the illuminance distribution of the comparative example of the light source apparatus of

Embodiment

1 and 2. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 2. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 2. It is a figure which shows the schematic structure of the light source apparatus of Embodiment 3. It is a figure explaining the operation of the light deflection element of the light source apparatus of Embodiment 3. FIG. It is a figure which shows the back light tracking result of the light source apparatus of Embodiment 3. FIG. It is a figure which shows the back light tracking result of the parallelizing lens of the light source apparatus of Embodiment 3. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 3. It is a figure for demonstrating the positional relationship between the light source group of the light source apparatus of Embodiment 1 and a parallelizing lens. It is a figure for demonstrating the positional relationship between the light source group of the light source apparatus of Embodiment 3 and a parallelizing lens. It is a figure which shows the back light tracking result in the X-axis direction of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the back light tracking result in the X-axis direction of the light source apparatus of Embodiment 3. FIG. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 3. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 3. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 4. It is a figure which shows the illuminance distribution of the light source apparatus of Embodiment 4. It is a figure which shows the illuminance distribution when the anamorphic aspherical surface is applied to the parallel lens of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the illuminance distribution when the toroidal plane is applied to the parallel lens of the light source apparatus of Embodiment 1. FIG. It is a figure which shows the schematic structure of the light source apparatus of Embodiment 5.

<Embodiment 1>
A schematic configuration of the light source device 100 of the first embodiment will be described with reference to FIGS. 1 and 2. FIG. 1 shows a view of the YZ plane observed from the −X axis side, and FIG. 2 shows a view of the ZX plane observed from the + Y axis direction side. As shown in FIGS. 1 and 2, the light source device 100 includes a light source group 1, a light deflection element 2, and a parallelizing lens 3, and a light deflection element 2 is arranged between the light source group 1 and the parallelizing lens 3. ing. The optical deflection element 2 is provided with

optical planes

21 and 22 for optical deflection on the light emitting side, and the

optical planes

21 and 22 are tilted together toward the optical axis C1 passing through the center of the parallelizing lens 3. ing. The light source group 1 has a light source 1a and a light source 1b arranged in the Y-axis direction as shown in FIG.

<Coordinate setting>
In the present embodiment, in order to facilitate the explanation, it is assumed that the light travels in the + Z axis direction using the XYZ coordinates in the figure shown below. Further, the clockwise rotation at the center of the X axis is + RX, the clockwise rotation at the center of the Y axis is + RY, and the clockwise rotation at the center of the Z axis is + RZ.

<Light source 1a, light source 1b>
The light source 1a and the light source 1b are solid-state light sources having different divergence angles in the X-axis direction and the divergence angle in the Y-axis direction, and are, for example, laser diodes. Here, the XY planes of the light source 1a and the light source 1b are the light emitting surfaces, the side in the Y-axis direction is longer than the side in the X-axis direction, and the divergence angle in the Y-axis direction (the angle in the ± RX direction) is the divergence in the X-axis direction. It shall be smaller than the angle (angle in the ± RY direction). For example, the lengths of the

light sources

1a and 1b in the Y-axis direction are 70 μm, and the length in the X-axis direction is 1 μm. Hereinafter, the Y-axis direction having a small divergence angle is also referred to as a first direction, and the X-axis direction is also referred to as a second direction.

<Light distribution characteristics of light source 1a and light source 1b>
FIG. 3 shows the light distribution characteristics of the light emitted from the light source 1a and the light source 1b. In FIG. 3, the vertical axis indicates the relative light intensity (arbitrary unit), and the horizontal axis indicates the light divergence angle (°). The characteristic 301 shown by the solid line shows the light distribution characteristic of the light diverging in the X-axis direction (± RY direction), and the characteristic 302 shown by the alternate long and short dash line indicates the distribution of the light diverging in the Y-axis direction (± RX direction). It shows the optical characteristics. As described above, the divergence angle in the Y-axis direction is smaller than the divergence angle in the X-axis direction.

The broken line 303 indicates a position where the relative light intensity is 1 / e ² , that is, a position where the relative light intensity is about 0.135. Specifications divergence angle generally laser diode, the relative light intensity to be displayed at an angle position at which the 1 / e ² number, a measure of the light spread. Here, the angle of the position of the characteristic 301 at 1 / e ² is ± about 37 °, and the angle of the position of the characteristic 302 at the ^{position of 1 / e 2} is ± about 5 °. Later, if such a range of divergence angle of the light source 1a and the light source 1b, the relative light intensity denote the angular range based on the location of the 1 / e ^2.

<Spacing between light source 1a and light source 1b>
The light source 1a and the light source 1b emit, for example, red light having a center wavelength of 638 nm. When a plurality of light sources are arranged adjacent to each other to increase the output, the light source is red as compared with the light source that emits blue light having a center wavelength of, for example, 450 nm and the light source that emits green light having a center wavelength of, for example, 525 nm. The light source that emits light is highly sensitive to temperature, and when the temperature rises, the emission efficiency decreases and the wavelength shift occurs. Therefore, in consideration of cooling, it is preferable that the distance between the light sources 1a and the light source 1b, that is, the distance in the arrangement direction, that is, the distance in the Y-axis direction in the present embodiment is wide. However, in general, as the arrangement spacing between the light source 1a and the light source 1b increases, the light utilization efficiency on the optical axis C1 decreases. Therefore, in order to improve the light utilization efficiency, the light source 1a and the light source 1b are of the optical axis C1. It is preferably placed close to each other.

<Relationship between the distance between the light source 1a and the light source 1b and the light utilization efficiency>
When the light deflection element 2 is not arranged, that is, when only the light source group 1 and the parallelizing lens 3 are used, the light emitted from the light source 1a and the light emitted from the light source 1b are refracted by the parallelizing lens 3 and then set on the optical axis C1. Gradually move away from the border. Therefore, when a condenser lens is arranged after the parallelizing lens 3 and the light emitted from the plurality of light source devices 100 is focused on the optical axis C1, the light focused on the optical axis C1 of the condenser lens. Is less efficient.

FIG. 4 is a diagram showing an example of ray tracing. FIG. 4 shows an optical system composed of only the light source group 1 and the parallelizing lens 3, and also shows an enlarged view of the region “A” including the light source group 1 and the parallelizing lens 3.

As shown in FIG. 4, the light ray 401 emitted from the central portion of the light source 1a is shown by a solid line, and the light ray 402 emitted from the central portion of the light source 1b is shown by a alternate long and short dash line. The spread of each light ray in the Y-axis direction was set to ± 5 ° as described with reference to FIG. The ray 401 and the ray 402 emitted from the parallelizing lens 3 gradually move away from the optical axis C1 in the arrangement direction of the light source, more specifically, the ray 401 travels in the −Y axis direction and the ray 402 travels in the + Y axis direction. It can be confirmed that it is. As a result, the light from the light source group 1 is separated from the optical axis C1 in the arrangement direction of the light sources, and the light utilization efficiency on the optical axis C1 is lowered. Here, assuming that the array interval from the optical axis C1 to the emission position of each light source is the image height, the shorter the focal length of the parallelizing lens 3, the higher the image height on the reaching surface, that is, at any position in the Z-axis direction. , The light beam reaches a position away from the optical axis C1. On the other hand, the light beam emitted on the optical axis C1 reaches the vicinity of the optical axis C1 even on the arrival surface. Here, in the vicinity, since the light rays have a width in the ± Y-axis direction due to the influence of the divergence angle of the light source, the light rays parallel to the optical axis C1 also reach the reaching surface, and the width in the ± Y-axis direction is defined. Considering that it has, it was set as "nearby".

<Light deflection element>
FIG. 5 is a conceptual diagram illustrating the operation of the light deflection element 2, and the features of the light deflection element 2 will be described with reference to FIG. By arranging the light deflection element 2 between the light source 1a and the parallelizing lens 3 (FIG. 1), the light ray 501cc emitted from the central portion of the light source 1a due to the deflection action of the light deflection element 2 is + Y with respect to the optical axis C1. It has an angle α1 in the axial direction and can be incident on the parallelizing lens 3. A ray traveling in the + Z-axis direction at an angle α1 is emitted as a ray parallel to the optical axis C1 by the parallelizing lens 3, so that a decrease in light utilization efficiency on the optical axis C1 can be suppressed. The same applies to the light source 1b by making the optical axis C1 line-symmetrical. That is, by arranging the light deflection element 2, the light rays parallel to the optical axis C1 emitted from the central portions of the light source 1a and the light source 1b are deflected in the + Y-axis direction and the −Y-axis direction after refraction, thereby causing the optical axis. It is possible to make the light source arranged apart from C1 in the ± Y-axis direction behave as if it were arranged on the optical axis C1 or at a position moved in parallel with the optical axis C1.

For example, as shown in FIG. 5, the length y1a in the Y-axis direction of the light source 1a is 70 μm, the length y1b in the Y-axis direction of the light source 1b is 70 μm, and the central portion of the light source 1a and the optical axis C1 are in the Y-axis direction. The distance y1ac is 105 μm, the distance y1c between the −Y-axis direction end of the light source 1a and the + Y-axis direction end of the light source 1b is 140 μm, and the distance y1d between the central portion of the light source 1a and the central portion of the light source 1b is 210 μm. .. Further, the distance D1 between the light emitting surface of the light source 1a and the light source 1b and the light incident surface of the light deflection element 2 is 350 μm, and the thickness T1 of the minimum portion of the light deflection element 2 is 280 μm. Further, the intersection of the light beam parallel to the optical axis C1 and the light incident surface of the optical deflection element 2 in the light emitted from the central portion of the light source 1a is P50, and the optical axis C1 of the light emitted from the central portion of the light source 1a is defined as P50. When the intersection of the light beam parallel to the light beam and the light deflecting element 2 on the emission surface side is P51, the distance D2 between P50 and P51 is about 315 μm.

Here, the material of the light deflection element 2 is, for example, BSC7 of HOYA Corporation, and the refractive index at a wavelength of 638 nm is about 1.515.

<Behavior of light rays>
As shown in FIG. 5, the light ray 501cu shows a trajectory of a light ray emitted from the central part of the light source 1a at an angle α2 = −5 °, and the light ray 501cc is a light ray emitted from the central part of the light source 1a at an angle of 0 °, that is. , The trajectory of the light ray parallel to the optical axis C1 is shown, and the light ray 501cd shows the trajectory of the light ray emitted from the central portion of the light source 1a at an angle α5 = + 5 °.

The light ray 501cc emits the central portion of the light source 1a and is incident on the light deflection element 2 at an angle of 0 °. After reaching the emission surface of the light deflection element 2, it is refracted and travels in the + Z axis direction at an angle α1. The angle α1 is calculated by the following mathematical formula (1) using Snell's law. The angle is calculated as an absolute value.

1.515 x sin (| α8 |) = sin (| α1 | + | α8 |) ... (1)
Here, assuming that the inclination angle α8 in the Y-axis direction (+ RX direction) with respect to the XY plane of the emission surface of the light deflection element 2 is + 18.81 °, the angle α1 is calculated by the following mathematical formula (2). The angle is calculated as an absolute value.

1.515 x sin (18.81 °) = sin (| α1 | + 18.81 °) ... (2)
From the above formula (2), | α1 | = 10.43 °, and considering the emission direction, α1 = -10.43 °. Since the refractive index and the angle are calculated as approximate values by rounding off, an error occurs at the calculated angle.

The light ray 501cu emits the central portion of the light source 1a and is incident on the light deflection element 2 at an angle α2 = −5 °. The incident light is refracted to an angle α3 and travels to the emission surface of the light deflection element 2. On the emission surface of the light deflection element 2, after refraction, the light travels in the + Z axis direction at an angle α4.

The angle α3 is calculated by the following formula (3). The angle is calculated as an absolute value.

sin (| α2 |) = 1.515 x sin (| α3 |) ... (3)
From the above formula (3), | α3 | = 3.3 °, and considering the emission direction, α3 = -3.3 °.

The angle α4 is calculated by the following formula (4). The angle is calculated as an absolute value.

1.515 x sin (| α8 | + | α3 |) = sin (| α8 | + | α4 |) ... (4)
Substituting a known angle into equation (4) yields the following equation (5).

1.515 x sin (22.11 °) = sin (18.81 ° + | α4 |) ... (5)
From the formula (5), | α4 | = 15.96 °, and considering the emission direction, α4 = −15.96 °.

The light ray 501cd emits the central portion of the light source 1a and is incident on the light deflection element 2 at an angle α5 = + 5 °. The incident light is refracted to an angle α6 and travels to the emission surface of the light deflection element 2. On the emission surface of the light deflection element 2, after refraction, the light travels in the + Z axis direction at an angle α7.

The angle α6 is calculated by the following formula (6). The angle is calculated as an absolute value.

sin (| α5 |) = 1.515 x sin (| α6 |) ... (6)
From the mathematical formula (6), | α6 | = 3.3 °, and considering the emission direction, α6 = + 3.3 °.

The angle α7 is calculated by the following formula (7). The angle is calculated as an absolute value.

1.515 x sin (| α8 |-| α6 |) = sin (| α8 | + | α7 |) ... (7)
Substituting a known angle into equation (7) yields the following equation (8).

1.515 x sin (15.51 °) = sin (18.81 ° + | α7 |) ... (8)
From the mathematical formula (8), | α7 | = 5.09 °, and considering the emission direction, α7 = −5.09 °.

The light ray 501dd shows a locus of a light ray inclined at an angle α5 = + 5 degrees with the optical axis C1 emitted from the end in the −Y axis direction of the light source 1a. Considering the light utilization efficiency, the light ray 501dd preferably passes in the + Y-axis direction from the intersection P52 between the optical axis C1 and the emission surface of the optical deflection element 2.

The light ray 501dd exits the −Y-axis direction end of the light source 1a at an angle α5 = + 5 °, reaches the light incident surface of the light deflection element 2, and after refraction, in the + Z-axis direction at an angle α6 = + 3.3 °. proceed. Further, it is refracted at the emission surface of the light deflection element 2 and travels in the + Z axis direction at an angle α7 = −5.09 °. From the viewpoint of light utilization efficiency, it is preferable that the intersection P53 of the light ray 501dd and the emission surface side of the light deflection element 2 is located in the + Y axis direction from the point P52. The light ray 501cd and the light ray 501dd are in a parallel relationship. The light from the light source 1b has a line-symmetrical relationship with the light from the light source 1a with respect to the optical axis C1.

As described above, the light deflection element 2 is a light source arranged on the + side of the optical axis C1 in the arrangement direction of the light sources, and in the present embodiment, the light distribution direction + side (in the present embodiment) with respect to the light from the light source 1a. A function that deflects and emits light in the + Y-axis direction, and a light source arranged on the-side of the optical axis C1. It has a function of deflecting in the direction) and emitting light. As a result, the apparent positions of the light source 1a and the light source 1b in the Y-axis direction can be moved in the optical axis C1 direction. As a result, the length of the entire apparent light source in the Y-axis direction can be shortened.

<Apparent position of light source 1a>
From the light rays 501cu, the light rays 501cc, and the light rays 501cd, the angle with respect to the optical axis C1 when the light rays emitted from the central portion of the light source 1a traveled to the parallelizing lens 3 was calculated. That is, with respect to the light rays 501cu, the light rays 501cc and the light rays 501cd traveling on the parallelizing lens 3, the behavior of the light rays in the −Z axis direction when it is assumed that the same light rays are emitted without arranging the light deflection element 2 is shown in the figure. In No. 5, it is represented by a ray 502cu, a ray 502cc and a ray 502cd. That is, with respect to the light rays 501cu, the light rays 501cc, and the light rays 501cd, the behavior of the light rays in the −Z axis direction when the configuration in the −Z axis direction is blackboxed is represented by the light rays 502cu, the light rays 502cc, and the light rays 502cd. By this process, it can be seen that the central portion of the light source 1a behaves in the same manner as when it is moved to the position of P54 in FIG.

Here, the length y1p in the Y-axis direction of the position P54 is 21 μm, and the distance D3 between the light source 1a and the position P54 in the Z-axis direction is 214 μm. Since aberration is generated due to the influence of the light deflection element 2, the position P54 is an approximate position.

That is, while the actual image height of the light source 1a with respect to the optical axis C1 is y1ac = 105 μm, by inserting the light deflection element 2, the virtual image height which is the apparent image height of the light source 1a with respect to the optical axis C1. It is possible to set y1p to 21 μm. That is, the image height after the parallelizing lens 3 is emitted can be reduced to 1/5. By using the light deflection element 2 in this way, it is possible to reduce the apparent image height. This makes it possible to improve the light utilization efficiency in the vicinity of the optical axis C1.

Here, the angle α1 that emits the light deflection element 2 of the light ray 501 cc emitted from the central portion of the light source 1a is preferably as small as possible in consideration of the miniaturization of the parallelizing lens 3 arranged in the subsequent stage. Since the parallelizing lens 3 is circular when observed from the XY plane, it is assumed that when the light beam moves in the Y-axis direction, the divergence angle of the light source 1a in the X-axis direction (± RY direction) is ± 37 °. This is because there is a high possibility that the amount of light incident on the parallelizing lens 3 will decrease.

Further, as described above, the apparent light source position P54 is moved by 214 μm in the + Z axis direction from the actual light source position. Along with this, it becomes necessary to shorten the focal length of the parallelizing lens 3 by 214 μm. Therefore, the light source image at the condensing position becomes slightly larger. For example, when a parallelized lens with a focal length of 6.5 mm becomes a parallelized lens with a focal length of 6.3 mm, when the image height is 21 μm, the image height 2000 mm away from the parallelized lens 3 is an optical deflection element. It becomes 6.67 mm, which is slightly larger than 6.46 mm when there is no 2. That is, it becomes 1.03 times. However, it can be said that the effect of such a magnification (1.03 times) is sufficiently smaller than the effect of lowering the image height, that is, the effect of reducing the image height to 1/5 times. The calculation formula is shown below.

In the case of a focal length of 6.5 mm, the image height = 21 μm × 2000 mm / 6.5 mm ≈ 6.46 mm.

In the case of a focal length of 6.3 mm, the image height = 21 μm × 2000 mm / 6.3 mm ≈ 6.67 mm.

<Other configuration examples>
For example, in the configuration shown in FIG. 5, the distance between the ends of adjacent light sources (distance y1c) is 140 μm, but the same effect can be obtained even if the distance y1c is 70 μm. In that case, the interval D1 can be set from 350 μm to 150 μm.

In this case, the position of the light deflection element 2 so that the light ray traveling in the + Z-axis direction at an angle α5 from the −Y-axis direction end of the light source 1a, that is, the light ray 501dd in FIG. 5 travels in the + Y-axis direction from P52. Can be moved in the + Z axis direction. Similarly, when the length y1a of the light source 1a in the Y-axis direction becomes long, the light beam traveling in the + Z-axis direction at an angle α5 from the end in the −Y-axis direction of the light source 1a travels in the −Y-axis direction from P52. Can move the position of the light deflection element 2 in the −Z axis direction.

It is possible to lengthen the interval D1 by changing the material of the light deflection element 2 to a glass material or the like having a high refractive index. At that time, the angle α8 is changed. For example, when the light deflection element 2 is manufactured by FD60 manufactured by HOYA Corporation, the refractive index at a wavelength of 638 nm is 1.80. In this case, the angle α8 may be set so that the angle α1 is 10.43 °, and specifically, the angle α8 can be set to 12.5 °. Further, the interval D1 can be set to 380 μm in consideration of the change in the back focus length due to the difference in the refractive index. Strictly speaking, when the light deflection element 2 is moved in the + Z-axis direction and the angle α8 is changed, the apparent Y-axis direction and Z-axis direction of the light source position P54 change. It becomes necessary to change the position and focus in the Z-axis direction of. If the distance D1, the thickness T1 of the minimum portion of the light deflection element 2, and the angle α8 are set so that the apparent Y-axis direction and Z-axis direction positions of the light source position P54 do not change, the Z of the parallelizing lens 3 is set. Eliminates the need to change axial position and focus.

<Substitute with a mirror>
Here, for example, the same function as that of the light deflection element 2 can be realized by using two mirrors. In this case, assuming that α1 = 10.43 °, the mirror is tilted by ± 10.43 / 2≈5.22 ° with respect to the optical axis C1. More specifically, it is tilted by −5.22 ° with respect to the light of the light source 1a arranged on the + Y-axis side and by +5.22 ° with respect to the light of the light source 1b arranged on the −Y-axis side.

When the divergence angle of the light source 1a is ± 5 °, a part of the light emitted at −5 ° may reach the parallelizing lens 3 without reaching the mirror. This is because the light source has a length in the Y-axis direction, which is the arrangement direction, so that the width of the mirror, that is, the length in the Z-axis direction must be longer than the distance to the parallelizing lens 3, the end of the light source, For example, if the light source 1a is arranged on the + Y-axis side, the light emitted from the end portion in the + Y-axis direction may not reach the mirror.

<Embodiment 2: An example when a mirror is used>
FIG. 6 shows a schematic configuration in which the light deflection element 2 is replaced by a mirror as the second embodiment. For convenience, only the behavior of the light rays of the light source 1a is shown as in FIG. The length y1a of the light source 1a in the Y-axis direction is 70 μm, and the distance y1ac in the Y-axis direction between the central portion of the light source 1a and the optical axis C1 is 105 μm, which is the same as the example of FIG. The angle α2 and the angle α5 are the same as in the example of FIG. The tilt angle α9 of the mirror M was set to −8 °.

The light ray 503cc emitted from the central portion of the light source 1a in parallel with the optical axis C1 is reflected by the reflection surface of the mirror M, and then travels in the + Z axis direction at an angle α11 = -16 ° with respect to the optical axis C1. The light ray 503cu emitted from the central portion of the light source 1a at an angle α2 = -5 ° reflects the mirror M and then has a + Z axis at an angle α12 = -11 ° (-(16 ° -5 °)) with respect to the optical axis C1. Go in the direction. The light ray 503cd emitted from the central portion of the light source 1a at an angle α5 = + 5 ° reflects the mirror M and then has an angle α10 = -21 ° (-(16 ° + 5 °)) with respect to the optical axis C1 in the + Z-axis direction. proceed.

Further, in FIG. 6, as the behavior of the light ray in the −Z axis direction, a light ray corresponding to the light ray 503 cc parallel to the light axis C1 is emitted from the light ray 504 cc and the central portion of the light source 1a at an angle α2 = −5 °. The ray corresponding to the ray 503cu is indicated by the ray 504cu, and the ray corresponding to the ray 503cd emitted from the central portion of the light source 1a at an angle α5 = + 5 ° is indicated by the ray 504cd. As shown in FIG. 6, in this configuration, it can be confirmed that the light beam is apparently behaving as if it is emitted from the light emitting point at the position P55c. Focusing on the light emitted from the end of the light source 1a in the + Y-axis direction, the light ray 503 uc emitted in parallel with the optical axis C1, the light ray 503 uu emitted at an angle α2 = −5 °, and emitted at an angle α5 = + 5 °. When the light rays in the −Z axis direction are represented by the light rays 504 uc, 504 uu, and 504 ud, it can be confirmed that the light rays 503 ud behave as if they are emitted from the light emitting point at the position P55u.

Similarly, focusing on the light emitted from the end of the light source 1a in the −Y axis direction, the light ray 503dc emitted parallel to the optical axis C1, the ray 503du emitted at an angle α2 = −5 °, and the angle α5 = + 5 °. When the light rays in the −Z axis direction are represented by the light rays 504dc, 504du, and 504dd with respect to the light rays 503dd emitted in, it can be confirmed that they behave as if they are emitted from the light emitting point at the position P55d.

From these, the light source 1a apparently behaves as if the light emitting surface is arranged at an angle α13 = -16 ° with respect to the XY plane. Therefore, when the parallelizing lens 3 is arranged in the subsequent stage to make the light beam parallel to the optical axis C1, the light ray width differs between the −Y axis direction and the + Y axis direction due to the influence of the inclination of the light emitting surface. , Image blurring occurs due to the tilt of the light emitting surface. However, the influence of image blur can be reduced by adjusting the parallelizing lens 3.

By the way, when the light collecting efficiency of the light source 1a is improved by using the mirror M, the light collecting effect is highest when the following formula (9) is satisfied. The following is a conditional expression when the position P55c is on the optical axis C1.

y1ac / D4 = sin (2 × | α9 |) ・・・ (9)
For example, when the distance y1ac = 105 μm and the tilt angle α9 of the mirror M = −8 °, the distance D4 between the central portion of the light source 1a and the reflection surface of the mirror M is about 381 μm. The mounting interval D4 allows, for example, an error of 381 μm ± 10% (38 μm).

As shown in FIG. 6, when the tilt angle α9 of the mirror M is small, it is outward from the + Y-axis direction end of the light source 1a, that is, the end in the direction away from the optical axis C1, that is, in the direction away from the optical axis C1. The light beam 503uu emitted at the angle α2 does not easily reach the mirror M. When the mirror M is used in this way, the effect of lowering the apparent image height and the effect of improving the light utilization efficiency near the optical axis C1 can be obtained, but the angle accuracy of the mirror M is required and the following There are such concerns. That is, it is necessary to increase the angle α11 corresponding to the angle α1 in FIG. 5, and therefore there is a concern that the diameter of the parallelized lens 3 in the subsequent stage may be increased or the efficiency of reaching the parallelized lens 3 may decrease.

However, if the diameter of the parallelizing lens 3 can be increased, the substitution of the optical deflection element 2 by the mirror M is not excluded. By using the mirror M, the traveling direction of light can be changed from the + Z-axis direction to the ± X-axis direction and the like. Therefore, by adjusting the inclination of the mirror M or the distances from the light source 1a and the light source 1b to the parallelized lens, in addition to the effect of suppressing the decrease in the light utilization efficiency on the optical axis, the degree of freedom in component arrangement is improved. can.

However, when the traveling direction of light is changed in the ± X-axis direction, the mirror surface is tilted in two axes, so the tendency of the emitted light rays changes depending on the center of rotation of the mirror. Unlike FIG. 6, after the mirror reflection, the light beam travels in the X-axis direction without maintaining the spread of the light ray before the reflection.

<Parallelized lens applied to Embodiment 1 and Embodiment 2>
In the first embodiment, the parallelizing lens 3 makes the light emitted from the light deflection element 2 parallel to the optical axis C1. The parallelizing lens 3 is formed, for example, in an aspherical shape. The aspherical shape can be a toroidal shape having different shapes in the X-axis direction and the Y-axis direction. Further, the light incident surface may have a convex shape or a concave shape.

In the second embodiment, the parallelizing lens 3 makes the light reflected by the mirror M parallel to the optical axis C1. The parallelizing lens 3 is formed, for example, in an aspherical shape. The aspherical shape can be a toroidal shape having different shapes in the X-axis direction and the Y-axis direction. Further, the light incident surface may have a convex shape or a concave shape.

Further, it is preferable that the light rays are parallel to the optical axis C1 with respect to the light rays emitted from the central portion of the light source 1a and the central portion of the light source 1b. As a result, at the arrival position of the light rays, the light rays emitted from the central portion of the light source 1a and the central portion of the light source 1b reach the vicinity of the optical axis C1, and the reached light source image can be minimized.

<Light ray tracing result of the light deflection element of the first embodiment>
FIG. 7 is a diagram showing a ray tracing result of a ray emitted from the light source 1a in the first embodiment. In FIG. 7, an enlarged view of the region “B” including the light source group 1 and the light deflection element 2 and an enlarged view of the region “C” of the emission surface of the parallelizing lens 3 are shown together. The positional relationship between the light source 1a and the light deflection element 2 is as shown in FIG. Further, the parallelizing lens 3 is arranged on the + Z axis direction side of the light deflection element 2. The focal length of the parallelizing lens is about 6.5 mm.

As shown in the enlarged view of the area "B" in FIG. 7, a light ray having a spread of ± 5 ° is emitted from the light source 1a in the + Z axis direction. The ray tracing results of the ray 601u emitted from the + Y-axis direction end of the light source 1a, the ray 601c emitted from the central portion of the light source 1a, and the ray 601d emitted from the −Y-axis direction end of the light source 1a are shown.

As shown in the enlarged view of the region "C" in FIG. 7, the light rays 601u, the light rays 601c, and the light rays 601d emitted from the parallelizing lens 3 are substantially parallel to the optical axis C1.

<Confirmation of the effects of Embodiment 1 and Embodiment 2>
FIG. 8 is a diagram illustrating an inclination angle of a light ray actually emitted from the light source 1a with respect to the optical axis C1. The parallelizing lens 3 is a virtual thin-walled lens 703, and the focal length F7 is 6.5 mm. It is assumed that the light source 1a is moved so that the central portion of the light source 1a is located on the optical axis C1. FIG. 8 shows the behavior of the light rays 701u emitted from the + Y-axis direction end of the light source 1a and the light rays 701d emitted from the −Y-axis direction end of the light source 1a. The angle βu and the angle −βd of the light ray 701u and the light ray 701d emitted from the thin-walled lens 703 with respect to the optical axis C1 are expressed by the following mathematical formula (10).

βu = -βd = atan ((y1a / 2) / F7)
= Atan (35 μm / 6500 μm)
≒ 0.31 ° ・・・ (10)
From the results of the angle βu and the angle βd, the light rays emitted from the central portion of the light source 1a are at an angle of 0 °, and the light rays 701u emitted from the + Y-axis direction end of the light source 1a and the light rays 701d emitted from the −Y-axis direction ends are obtained. When the parallelizing lens 3 is emitted at an angle of 0.31 °, it can be assumed that the light source 1a is emitted from the optical axis C1.

In order to verify the above assumption, FIG. 9 shows the result of back light tracing using the configuration of FIG. In FIG. 9, an enlarged view of the region “D” including the light source group 1 and the light deflection element 2 and an enlarged view of the region “E” of the emission surface of the parallelizing lens 3 are shown together. Here, the above assumption is confirmed by tracking the back rays of the light rays traveling from the + Z axis direction to the −Z axis direction of the parallelizing lens 3 and confirming the image formation position.

FIG. 9 shows the back ray tracing results of the light rays 801u, the light rays 801c, and the light rays 801d in the first embodiment, and the light rays 801d have an angle of −0.31 ° with respect to the optical axis C1 and are collimated beams. The ray 801c is incident on the optical axis C1 and is incident on the parallelizing lens 3 in parallel with the optical axis C1. It is incident.

When the light rays on the light source 1a are confirmed, the light rays 801u are focused (imaged) on the + Y-axis direction end of the light source 1a, and the light rays 801c are focused (imaged) on the center of the light source 1a, and the light rays 801d. Can be confirmed to be focused (imaging) on the end of the light source 1a in the −Y axis direction. That is, by inserting the light deflection element 2, it can be confirmed that the light source 1a behaves in the same manner as when it is on the optical axis C1. As described above, by using the light deflection element 2, the effect of improving the light utilization efficiency in the vicinity of the optical axis C1 can be obtained.

In the above, the light ray 801c is an example of condensing light on the central portion of the light source 1a in the Y-axis direction, but the parallelizing lens 3 and the optical deflection when parallel light is incident from the + Z-axis direction side of the parallelizing lens 3. The condensing position of the parallel light by the optical system including the element 2 does not have to be exactly located on the light emitting surface of each of the light source 1a and the light source 1b. That is, in the case of the light source 1a, the central portions of the light source 1a and the light source 1b are within ± y1a / 3 from the center in the Y-axis direction and ± 30 μm from the light emitting surface of the light source 1a in the Z-axis direction. It may preferably contain ± 10 μm or less.

Here, as shown in FIG. 5, the position in the Y-axis direction of the position P54 is the image height position of the light source 1a, but in FIG. 9, the behavior of the light ray such that the central portion of the light source 1a is located on the optical axis C1. I am doing. This is because the shape of the parallelizing lens 3 is set so that the light rays are concentrated at the position P54 when the light rays parallel to the optical axis C1 are incident on the parallelizing lens 3 from the + Z axis direction. The focal position of the parallelizing lens 3 is in the −Z axis direction from the position P54, but it is possible to make the optical axis C1 behave as a light ray in which the central portion of the light source 1a is arranged.

<Characteristics of the parallelized lens of the first embodiment>
FIG. 10 is a diagram showing a back light ray tracking result when a light ray parallel to the optical axis C1 is incident from the + Z axis direction of the parallelizing lens 3. In FIG. 10, an enlarged view of the region “F” including the light source group 1 is also shown. As shown in FIG. 10, it can be seen that the focusing point P80 of the parallelizing lens 3 is on the + Z axis direction side from the light source 1a and on the + Y axis direction side from the optical axis C1. Further, it can be seen that the focal position P80f of the parallelizing lens 3 is on the −Z axis direction side from the focusing point P80. The focal position P80f is located on the + Z axis side of the light source 1a because the back focus of the parallelizing lens 3 is shortened due to the influence of the optical deflection element 2 which is an optical element. It is also considered that the angle α1 is affected by the deflection of the light beam. In the example of FIG. 10, the distance between the focusing point P80 and the focal position P80f in the Z-axis direction is about 140 μm.

In FIG. 10, the illuminance distributions on the condensing point P80 and the focal position P80f when the parallel light flux is incident on the + Z axis side of the parallelizing lens 3 in the −Z axis direction are shown in FIGS. 11 and 12, respectively. In FIGS. 11 and 12, the X-axis (mm) is shown on the horizontal axis and the Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

As shown in FIG. 11, it can be seen that a ring-shaped illuminance distribution with a hollow center is formed on the condensing point P80, and the intensity is strong in the vicinity of a region having a radius of 20 μm. Further, as shown in FIG. 12, it can be seen that on the focal position P80f, a concentric illuminance distribution is formed and a small condensing spot is formed to be the focal position.

In this way, by forming a ring-shaped region with strong light intensity on the + Z axis direction side from the focal position, even if the virtual light source position is located on the + Y axis side, it is the same as when emitted from the optical axis C1. It is possible to make the behavior of the light beam of.

In the first embodiment, the

optical surfaces

21 and 22 for light deflection are provided on the light emitting side of the light deflection element 2, but there is also a case where the

optical surfaces

21 and 22 for light deflection are provided on the light incident side. A similar effect can be obtained. It should be noted that the effect of improving the light utilization efficiency on the optical axis C1 can be obtained without forming a ring-shaped region having a strong light intensity. Further, even in the configuration using the mirror M of the second embodiment shown in FIG. 6, a ring-shaped illuminance distribution can be formed.

<Characteristics when the mirror of the second embodiment is used>
FIG. 13 shows the result of back light tracking of the configuration using the mirror M of the second embodiment shown in FIG. In FIG. 13, an enlarged view of the region “G” including the light source group 1 and the mirror M and an enlarged view of the region “F” of the emission surface of the parallelizing lens 3 are shown together.

FIG. 13 shows the back ray tracing result when the ray 1101u, the ray 1101c, and the ray 1101d are incident from the + Z axis direction of the parallelizing lens 3. The ray 1101u is incident on the parallelizing lens 3 at an angle −0.31 ° with respect to the optical axis C1, the ray 1101c is incident on the parallelizing lens 3 parallel to the optical axis C1, and the ray 1101d is emitted. , It is incident on the parallelizing lens 3 at an angle of +0.31 ° with respect to the optical axis C1.

From FIG. 13, the light ray 1101u is focused (imaged) on the + Y-axis end of the light source 1a, the light ray 1101c is focused (imaged) on the center of the light source 1a, and the light ray 1101d is focused on the light source 1a. It can be seen that the light source is focused (imaging) at the end in the Y-axis direction.

Further, it can be seen that the light ray 1101u is focused in the −Z axis direction as compared with the light collecting position of the light ray 1101c. Further, it can be seen that the light ray 1101d is focused in the + Z axis direction as compared with the light collecting position of the light ray 1101c. That is, since the condensing position in the Y-axis direction shifts in the Z-axis direction as compared with the case where the light deflection element 2 is used, in the light beam emitted from the light source 1a, at an arbitrary reaching surface after the parallelizing lens 3 is emitted. It can be seen that the light beam width of is non-uniform in the Y-axis direction.

<Comparison between the light deflection element of the first embodiment and the second embodiment and the mirror>
In FIG. 9 which is the result of performing the back light tracing using the configuration of FIG. 5 of the first embodiment, and FIG. 13 which is the result of performing the back light tracking using the configuration of FIG. 6 of the second embodiment, the light source 1a. 14 to 16 show the illuminance distribution of the light emitted from the light source 1a on the evaluation surface (XY plane) at a distance of 2000 mm from the light source. From FIG. 3, the divergence angle of the light source 1a ^{is ± about 37 ° for 1 / e 2 in} the X-axis direction (RY direction) and ± about 5 ° ^{for 1 / e 2 in} the Y-axis direction (RX direction). .. In FIGS. 14 to 16, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

FIG. 14 shows the illuminance distribution of light in the case of the first embodiment using the light deflection element 2, and FIG. 15 shows the illuminance distribution of the light in the case of the second embodiment using the mirror M. From FIG. 14, when the light axis C1 is 0 mm in the Y-axis direction, the region where the light intensity is 80% (80% when the maximum light intensity is 100%) or more is continuously 8.4 mm to + 10.1 mm ( It can be seen that the light reaches the range of 18.5 mm) uniformly. Further, it can be seen that the region where the light intensity is 20% or more with the maximum light intensity as 100% is in the range of -10.3 mm to + 12.3 mm (22.6 mm). From this, the ratio of the range in the Y-axis direction of the uniform region of 80% or more to the region of light intensity of 20% or more is about 81.9% (18.5 mm / 22.6 mm).

Further, in the configuration shown in FIG. 8, assuming that the focal length F7 is 6.5 mm and the distance from the virtual thin-walled lens 703 (parallelized lens 3) to the evaluation surface is 1993.5 mm, the image height of the light source 1a is as follows. It is expressed by the formula (11).

(Y1a / 2) × (1993.5 mm / 6.5 mm) = 10.7 mm ... (11)
According to the illuminance distribution in FIG. 14, the illuminance range in the Y-axis direction is slightly less than +10.7 mm on the + side from the region of light intensity of 20% or more, but is within -10.7 mm on the-side. Further, the region of light intensity of 80% or more is within ± 10.7 mm, and considering the ratio of the region of light intensity of 80% to the region of light intensity of 20% or more in the Y-axis direction, the optical axis C1 It is considered that almost the same result as the case where the light source 1a is on the top is obtained.

On the other hand, from FIG. 15, it can be seen that the illuminance distribution in the Y-axis direction has a region of light intensity of 80% or more in the range of -9.3 mm to -6.9 mm (2.4 mm) in the Y-axis direction. It can be seen that the region with high light intensity is located at a position away from the optical axis C1. Further, since the range of the light intensity region of 80% or more is narrow, it can be seen that the light having a strong light intensity is concentrated. Further, it can be seen that the light intensity of 20% or more is in the range of -10.2 mm to + 12.8 mm (22.8 mm). Since the light intensity of 40% or more is within the range of ± 10.7 mm, it is considered that the light intensity is generally within ± 10.7 mm. As a result, although the effect of improving the light utilization efficiency near the optical axis C1 can be confirmed, the light intensity on the optical axis C1 is lower than the peak position, and the apparent light source 1a is tilted. Conceivable.

FIG. 16 is a diagram showing an illuminance distribution in the case of the configuration of FIG. 4 in which the light deflection element 2 and the mirror M are not arranged as a comparative example. From FIG. 16, when the light intensity on the optical axis C1 is 0 mm in the Y-axis direction, the light intensity region of 20% or more is almost uniformly in the range of −42.7 mm to -20.7 mm (22.0 mm). You can see that it has arrived. That is, it can be seen that the light beam does not reach on the optical axis C1. From the above, it can be confirmed that the effect of improving the light utilization efficiency on the optical axis C1 can be confirmed by using the light deflection element 2 or the mirror M. That is, the effect of improving the light utilization efficiency on the optical axis C1 of the first embodiment and the second embodiment can be seen.

Further, FIGS. 17 to 19 show the illuminance distribution of the light on the evaluation surface at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIGS. 17 to 19, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

FIG. 17 shows the case of the first embodiment using the light deflection element 2, FIG. 18 shows the case of the second embodiment using the mirror M, and FIG. 19 shows the parallelizing lens 3 using the mirror M of the second embodiment. The illuminance distribution when the focal position is moved by 15 μm in the + Z axis direction is shown.

From FIG. 17, when the optical axis C1 is 0 mm in the Y-axis direction, the region where the light intensity is 80% or more is continuously illuminated uniformly in the range of -8.9 mm to +8.9 mm (17.8 mm). Can be seen that has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -11.5 mm to +11.6 mm (23.1 mm). From this, the ratio of the range in the Y-axis direction of the uniform region of 80% or more to the region of light intensity of 20% or more is about 77.1% (17.8 mm / 23.1 mm). That is, it can be seen that the light intensity is uniformly distributed in the range of about 77.1% without peak peaks.

From FIG. 18, there are two peak positions on the + Y-axis side and the −Y-axis side with respect to the reference position (optical axis C1 position), and the non-uniformity centered on the optical axis C1 is larger than that in FIG. It can be seen that it has been reduced. In the Y-axis direction, there are two regions with a light intensity of 80% or more in the range of -9.4 mm to -5.5 mm (3.9 mm) and the range of +5.6 mm to +9.3 mm (3.7 mm). I understand. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -12.0 mm to + 12.0 mm (24.0 mm).

Further, in FIG. 19, it can be seen that the region where the light intensity is 80% or more is in the range of -2.7 mm to +2.7 mm (5.4 mm). Further, it can be seen that the region where the light intensity is 20% or more is in the range of -10.8 mm to +10.7 mm (21.5 mm). From this, the ratio of the range in the Y-axis direction of the region having a high light intensity of 80% or more to the region having a light intensity of 20% or more is about 25.1% (5.4 mm / 21.5 mm). That is, it can be seen that the region having a light intensity of 80% or more is concentrated in the range of about 25.1%, and the light utilization efficiency on the optical axis C1 is high. In other words, it can be seen that the light intensity on the optical axis C1 is increased, and the light utilization efficiency in the optical axis C1 direction can be improved as compared with the case of FIG. This is because the design of the parallelizing lens 3 is devised so that the light beam 1101u traced by the back light beam is focused near the + Y-axis direction end face of the light source 1a shown in FIG. 13, so that the light utilization efficiency in the optical axis C1 direction is achieved. It means that it is possible to improve. Here, the fact that the light beam 1101u traced by the back ray focuses on the vicinity of the + Y-axis direction end face of the light source 1a means that the focusing position (focus position of the parallelizing lens 3) in FIG. 13 moves in the + Z-axis direction. Means.

Although FIG. 19 is an example in which the focal position of the parallelizing lens 3 is moved by 15 μm in the + Z axis direction using the mirror M, the configuration for the light utilization efficiency on the optical axis C1 corresponding to or higher in FIG. 18 is parallel. The focal position of the modified lens 3 may be moved by 15 μm ± 15 μm in the + Z axis direction.

Further, when the width in the Y-axis direction is confirmed in the region where the light intensity is 80% or more, FIG. 19 is 5.4 mm (± 2.7 mm) and FIG. 17 is 17.8 mm (± 8.9 mm). Therefore, FIG. 19 using the mirror M, which is a reflection type light deflection element, has higher light utilization efficiency on the optical axis C1 than FIG. 17 using the transmission type light deflection element 2. In FIG. 17, since there is no light loss due to the reflectance of the mirror M, the light utilization efficiency is high as a whole, and the light utilization efficiency on the evaluation surface is high.

From the above, by using the light deflection element 2 suitably designed in the first embodiment, the ratio of the range in the Y-axis direction of the region having a high light intensity of 80% or more to the region having a light intensity of 20% or more is 75. % Or more, and uniform light can be collected on the optical axis C1 while increasing the light utilization efficiency on the optical axis C1. As an example, in a light intensity uniform element, for example, a rod lens and a light pipe, the number of reflections in the element can be reduced, so that the size (length) of the optical system can be shortened. Further, by using the optical system including the mirror M suitably designed in the second embodiment, the ratio of the range in the Y-axis direction of the region having a high light intensity of 80% or more to the region having a light intensity of 20% or more can be set. It can be 30% or less, and the light utilization efficiency on the optical axis C1 can be further improved. As an example, when the aperture size of a light intensity uniform element, for example, a rod lens and a light pipe, is small, it can be incorporated into an optical system with high light utilization efficiency.

Here, an example of an optical system including a appropriately designed mirror M includes an optical system in which the focal position of the parallelizing lens 3 is adjusted as described above. Examples of the method for adjusting the focal position of the parallelizing lens 3 include a method of moving the parallelizing lens 3 in the + Z axis direction or a method of moving the light source group in the −Z axis direction.

<Embodiment 3: Example of Inversion Arrangement of Light Deflection Element>
FIG. 20 is a diagram showing a schematic configuration of the light source device 2101 of the third embodiment. Since it is the same as that of the first embodiment except that the configuration of the light deflection element 2 and the position of the parallelizing lens 3 in the Z-axis direction are different from those of the light source device 100 of FIG. 1, the description thereof will be omitted as appropriate. The optical deflection element 212 of the third embodiment is different from the configuration of FIG. 1 in that the optical deflection

optical surfaces

2121 and 2122 for deflecting the incident light are provided on the −Z axis direction side. The

optical surfaces

2121 and 2122 are both tilted toward the optical axis C1 passing through the center of the parallelizing lens 3.

<Light deflection element 212 of the third embodiment>
FIG. 21 shows a conceptual diagram illustrating the operation of the light deflection element 212. Since the light source 1a, the light source 1b, the interval y1d, the interval y1ac, the interval y1c, the length y1a, and the length y1b are the same as those in FIG. 5, the description thereof will be omitted. The thickness T1 of the minimum portion of the light deflection element 212 is 280 μm, which is the same as in FIG. Further, the distance D1a between the light source 1a and the recess of the light deflection element 212 is 520 μm. Here, the material of the light deflection element 212 is, for example, BSC7 of HOYA Corporation, and the refractive index at a wavelength of 638 nm is about 1.515.

Further, in the method of manufacturing the optical deflection element 2 (FIG. 1) and the optical deflection element 212, for example, the + Y-axis direction side may be manufactured by cutting and polishing, and the ZX plane including the optical axis C1 may be bonded as an adhesive interface. .. That is, two elements of trapezoidal square pillars having the same shape may be joined to form one light deflection element 2 or light deflection element 212. The light deflection element 2 or the light deflection element 212 may be manufactured by molding without using bonding.

<Behavior of the light beam of the third embodiment>
The light ray 2101uu shows the trajectory of the light ray emitted from the + Y-axis direction end of the light source 1a at an angle α2 = -5 °, and the light ray 2101uc is the light ray emitted from the + Y-axis direction end of the light source 1a at an angle of 0 °, that is, light. The trajectory of the light ray parallel to the axis C1 is shown, and the light ray 2101ud shows the trajectory of the light ray emitted from the + Y-axis direction end of the light source 1a at an angle α5 = + 5 °.

The light ray 2101cu shows the trajectory of the light ray emitted from the central part of the light source 1a at an angle α2 = -5 °, and the light ray 2101cc is a light ray emitted from the central part of the light source 1a at an angle of 0 °, that is, a light ray parallel to the optical axis C1. The light ray 2101cd shows the locus of the light ray emitted from the central portion of the light source 1a at an angle α5 = + 5 °.

The ray 2101du shows the trajectory of the ray emitted from the end of the light source 1a in the −Y axis direction at an angle α2 = −5 °, and the ray 2101dc is the ray emitted from the end of the light source 1a in the −Y axis direction at an angle of 0 °, that is. , The trajectory of the light ray parallel to the optical axis C1 is shown, and the ray 2101dd shows the trajectory of the light ray emitted from the end portion of the light source 1a in the −Y axis direction at an angle α5 = + 5 °.

<Trajectory of ray 2101cu, ray 2101cc, ray 2101cd>
In the trajectories of the light rays 2101uu and the light rays 2101du, the angle α2a in which the light rays of the light rays 2101cu are incident on the light deflection element 212 and travel is the same, and the angle α2b that is emitted from the light deflection element 212 and travels is the same. Only the trajectory will be described. Further, since the light rays 2101 uc and the light rays 2101 cc have the same angle α1a in which the light rays of the light rays 2101 cc are incident on the light deflection element 212 and travel, and the angles α1b in which the light rays of the light rays 2101 cc are emitted and travel are the same, the trajectory of the light of the light rays 2101 cc. Will be explained only with respect to. Since the light rays 2101ud and the light rays 2101dd have the same angle α5a in which the light rays of the light rays 2101cd are incident on the light deflection element 212 and travel, and the angles α5b that are emitted from the light deflection element 212 and travel are the same, the light of the light rays 2101cd. Only the trajectory will be described.

<Behavior of ray 2101cu>
The light ray 2101cu is emitted from the central portion of the light source 1a at an angle α2 = −5 °, then refracted by the light deflection element 212 and travels in the + Z axis direction at α2a. The angle α2a is calculated by the following mathematical formula (12) using Snell's law. The angle is calculated as an absolute value.

sin (| α8 |-| α2 |) = 1.515 x sin (| α8 |-| α2a |) ... (12)
If α8 is, for example, + 18.81 °, then α2a = −9.74 °. It should be noted that the occurrence of calculation error is the same as in the first embodiment, and the same is true in the following calculation.

The light ray 2101cu that has traveled in the light deflection element 212 is refracted at the emission surface of the light deflection element 212 and travels in the + Z axis direction at an angle α2b. The angle α2b is calculated by the following mathematical formula (13). The angle is calculated as an absolute value.

1.515 x sin (| α2a |) = sin (| α2b |) ... (13)
When calculated as α2a = −9.74 °, α2b = −14.85 °.

<Behavior of ray 2101cc>
The light ray 2101cc is emitted from the central portion of the light source 1a at an angle of 0 °, then refracted by the light deflection element 212, and travels in the + Z axis direction at α1a. α1a is calculated by the following mathematical formula (14). The angle is calculated as an absolute value.

sin (| α8 |) = 1.515 x sin (| α8 |-| α1a |) ... (14)
If α8 is, for example, + 18.81 °, then α1a = −6.52 °.

The light ray 2101cc that has traveled in the light deflection element 212 is refracted at the emission surface of the light deflection element 212, and travels in the + Z axis direction at an angle α1b. The angle α1b is calculated by the following mathematical formula (15). The angle is calculated as an absolute value.

1.515 x sin (| α1a |) = sin (| α1b |) ... (15)
When calculated assuming that α1a = −6.52 °, α1b = −9.91 °.

<Behavior of ray 2101cd>
The light ray 2101cd is emitted from the central portion of the light source 1a at an angle α5 = + 5 °, then refracted by the light deflection element 212 and travels in the + Z axis direction at α5a. α5a is calculated by the following mathematical formula (16). The angle is calculated as an absolute value.

sin (| α8 | + | α5 |) = 1.515 x sin (| α8 |-| α2a |) ... (16)
If α8 is, for example, + 18.81 °, then α5a = -3.36 °.

The light ray 2101cd that has traveled in the light deflection element 212 is refracted at the emission surface of the light deflection element 212 and travels in the + Z axis direction at an angle α5b. The angle α5b is calculated by the following mathematical formula (17). The angle is calculated as an absolute value.

1.515 x sin (| α5a |) = sin (| α5b |) ... (17)
When calculated as α5a = -3.36 °, α5b = −5.09 °.

<Apparent position of light source 1a>
From the light rays 2101cu, the light rays 2101cc, and the light rays 2101cd, the angle with respect to the optical axis C1 when the light rays emitted from the central portion of the light source 1a travel to the parallelizing lens 3 was calculated. Here, regarding the light rays 2101cu, the light rays 2101cc, and the light rays 2101cd traveling on the parallelizing lens 3, the behavior of the light rays in the −Z axis direction when it is assumed that the same light rays are emitted without arranging the light deflection element 212 is shown. In FIG. 21, it is represented by a broken line. That is, with respect to the light rays 2101cu, the light rays 2101cc, and the light rays 2101cd, the behavior of the light rays in the −Z axis direction when the configuration in the −Z axis direction is blackboxed is represented by a broken line. The same applies to the light rays 2101 uu, the light rays 2101 uc, and the light rays 2101 ud emitted from the + Y-axis direction end of the light source 1a. The same applies to the light rays 2101du, the light rays 2101dc, and the light rays 2101dd emitted from the end in the −Y axis direction of the light source 1a. By this process, when the central portion of the light source 1a is moved to the position of P21c in FIG. 21 and the end portion of the light source 1a in the + Y-axis direction is moved to the position of P21u in FIG. It can be seen that when the end portion is moved to the position of P21d in FIG. 21, the behavior of the light source is the same as that of the case where the end portion is moved to the position of P21d.

As described above, the light deflection element 212 of the third embodiment is arranged with respect to the light source arranged on the + side of the optical axis C1 in the arrangement direction of the light sources, that is, the light from the light source 1a, as in FIG. For the function of deflecting and emitting light in the + side (+ Y-axis direction) of the light direction and the light source arranged on the-side of the light axis C1, that is, the light from the light source 1b, the light distribution direction-side (-Y-axis direction). It has a function of deflecting in the direction) and emitting light. As a result, the apparent positions of the light source 1a and the light source 1b in the Y-axis direction can be moved in the optical axis C1 direction. As a result, the length of the entire apparent light source in the Y-axis direction can be shortened.

Further, as can be seen from FIG. 21, it can be seen that the apparent position of the light source 1a is tilted at an angle α21 with respect to the light source 1a. The angle α21 is, for example, 7 °. However, the inclination is small as compared with the case where the mirror of FIG. 6 is used, and the influence of image blurring is limited. From the back light tracking result of FIG. 22, which will be described later, it is assumed that the influence of image blurring is small.

Here, the length y1pa in the Y-axis direction from the optical axis C1 of the position P21c is 17 μm, and the distance D3a in the Z-axis direction between the light source 1a and the position P21c is 97 μm, which is shorter than the distance D3 in FIG. I understand. Since aberrations are generated due to the influence of the light deflection element 212, the positions P21u, the position P21c, and the position P21d are approximate positions.

<Confirmation of light collection position in the Y-axis direction by tracking back light>
FIG. 22 shows the back light tracking result of the light source device 2101 of the third embodiment. In FIG. 22, an enlarged view of the region “I” including the light source group 1 and the light deflection element 212 and an enlarged view of the region “J” of the emission surface of the parallelizing lens 3 are shown together. Here, the back ray tracking of the light beam traveling from the + Z axis direction to the −Z axis direction of the parallelizing lens 3 is performed, and the image formation position is confirmed.

FIG. 22 shows the back ray tracing results of the ray 2301u, the ray 2301c, and the ray 2301d, and the ray 2301d is incident on the collimated beam 3 at an angle of −0.31 ° with respect to the optical axis C1. The light ray 2301c is incident on the parallelizing lens 3 in parallel with the optical axis C1, and the light ray 2301u is incident on the parallelizing lens 3 at an angle of +0.31 ° with respect to the optical axis C1.

When the light rays on the light source 1a are confirmed, the light rays 2301u are focused (imaged) on the + Y-axis end of the light source 1a, and the light rays 2301c are focused (imaged) on the center of the light source 1a, and the light rays 2301d. Can be confirmed to be focused (imaging) on the end of the light source 1a in the −Y axis direction. That is, by inserting the light deflection element 212, it can be confirmed that the light source 1a behaves in the same manner as when it is on the optical axis C1. As described above, by using the light deflection element 212, the effect of improving the light utilization efficiency in the vicinity of the optical axis C1 can be obtained. Further, the inclination α23 of the apparent light source image confirmed in FIG. 21 is about 3 °, and it is assumed that there is almost no influence on the illuminance distribution. It is presumed that this is because the tilt angle is reduced by the aberration of the parallelizing lens 3.

<Relationship between parallelizing lens 3 and optical deflection element 212>
FIG. 23 is a diagram showing a back light ray tracking result when a light ray parallel to the optical axis C1 is incident from the + Z axis direction of the parallelizing lens 3. In FIG. 23, an enlarged view of the region “K” including the light source group 1 is also shown. As shown in FIG. 23, it can be seen that the focal position P240f of the parallelizing lens 3 is on the −Z axis direction side with respect to the light source 1a. On the other hand, it is also different from the first embodiment in that the focal position P80f of the parallelized lens 3 in FIG. 10 is located on the + Z axis side of the light source 1a. As will be described later, this is because the shape of the parallelizing lens 3 is the same as that of the first embodiment, but is moved by 100 μm in the −Z axis direction. The distance D24 between the light emitting surface of the light source 1a in FIG. 23 and the focal position P240f in the Z-axis direction is 33 μm, and the distance between the light emitting surface of the light source 1a in FIG. 10 and the focal position P80f in the Z-axis direction is 67 μm. .. That is, the focal position is moved by 100 μm. The parallelizing lens 3 is moved by 100 μm in the −Z axis direction in order to align the focusing position in the Y-axis direction in the back light tracking shown in FIG. 22 with the vicinity of the light emitting surface of the light source 1a.

<Illuminance distribution of Embodiment 3>
FIG. 24 shows the illuminance distribution of light on the evaluation surface (XY plane) at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on by using the light deflection element 212. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIG. 24, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

In the illuminance distribution in the X-axis direction, when 0 mm is on the optical axis C1, the region where the light intensity is 80% or more is separated around 0 mm in the range of -7.2 mm to +7.2 mm (14.4 mm). You can see that it has been reached. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -11.5 mm to +11.4 mm (22.9 mm). It can be confirmed that the spread of the width in the X-axis direction is wider than that of the illuminance distribution of the first embodiment of FIG.

Further, in the illuminance distribution in the Y-axis direction, when the area on the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is uniformly in the range of -10.5 mm to +10.3 mm (20.8 mm). You can see that the light has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -11.9 mm to + 12.0 mm (23.9 mm).

Compared with FIG. 17, the spread of the illuminance distribution in the Y-axis direction (the region where the light intensity is 20% or more) is a little wider, but the effect of improving the light utilization efficiency on the optical axis C1 can be confirmed. Further, it can be confirmed from FIG. 17 that the illuminance distribution spreads in the X-axis direction. This is because when a light ray parallel to the optical axis C1 is incident from the + Z-axis direction to the -Z-axis direction, the light is focused on the light emitting surface of the light source 1a in the Y-axis direction, whereas the light source 1a emits light in the X-axis direction. It means that the light is not focused on the surface, that is, the light is focused in the −Z axis direction from the light emitting surface. That is, it shows that the light collection positions for the light rays in the X-axis direction and the light rays in the Y-axis direction are different. Therefore, by setting the inclined surface of the light deflection element 212 in the −Z axis direction, a new problem has arisen in which the light collection positions for the light rays in the X-axis direction and the light rays in the Y-axis direction are so different that they affect the illuminance distribution. it is conceivable that. However, for example, when the screen size projected on the screen using the light source device 2101 of the third embodiment is close to a square such as horizontal: vertical = 4: 3, the side of the screen is oriented in the Y-axis direction of the light source device. By making the vertical of the screen correspond to the X-axis direction of the light source device, it is possible to suppress the decrease in efficiency and guide the light to the screen. From 22.9 mm in the region where the light intensity in the X-axis direction is 20% or more and 23.9 mm in the region where the light intensity in the Y-axis direction is 20% or more, X: Y = 1: 1.04, horizontal: vertical = The correspondence with 4: 3 is relatively preferable.

Here, the projection device is generally composed of a light source device, an illumination optical system, and a projection optical system, and the light of the light source device is focused on a light intensity equalizing element that equalizes the light intensity distribution of the light source device. The light homogenized by the light intensity equalizing element is transferred to the display device by the illumination optical system, and the image formed by the display device is magnified and projected onto the screen by the projection optical system.

Since the aspect ratios of the light intensity equalizing element and the display device are almost the same, for example, 4: 3 when the screen resolution is XGA (eXtended Graphics Array) and 16: 9 when the screen resolution is full HD (full high definition). It becomes the aspect ratio. When the aspect ratio is 16: 9, it is preferable that the spread of the illuminance distribution in the X-axis direction is narrower than the illuminance distribution in FIG. 24.

<Explanation that the focusing position differs between the X-axis direction and the Y-axis direction>
The positional relationship between the light source group 1 and the parallelizing lens 3 will be described with reference to FIGS. 25 and 26. FIG. 25 is a diagram similar to FIG. 7 shown in the first embodiment, in which light rays are emitted in the + Z-axis direction with a spread of ± 5 ° from the + Y-axis direction end, the center, and the −Y-axis direction end of the light source 1a. The ray tracing result when it progresses is shown. Further, FIG. 26 shows a ray tracing result when the ray travels in the + Z axis direction with a spread of ± 5 ° from the + Y axis direction end portion, the center, and the −Y axis direction end portion of the light source 1a of the third embodiment. ..

In order to determine the position in the Y-axis direction when tracing the back light of the light ray in the X-axis direction, which will be described later, the height in the Y-axis direction at the time when the parallelizing lens 3 is emitted is confirmed. From FIG. 25, the height at which the light ray emitted at −5 ° emits the parallelized lens 3 and the distance y26t1 between the optical axes C1 are 1.8 mm, and the height and the optical axis at which the light ray emitted at + 5 ° emits the parallelized lens 3. The distance y26b1 of C1 is 0.5 mm. Further, from FIG. 26, the height at which the light beam emitted at −5 ° emits the parallel lens 3 and the distance y26t2 of the optical axis C1 are 1.7 mm, and the height at which the light ray emitted at + 5 ° emits the parallel lens 3. The distance y26b2 of the optical axis C1 is 0.5 mm.

The Z-axis direction distance D261 between the light emitting surface of the light source 1a in FIG. 25 and the parallelized end in the + Z-axis direction is 8.14 mm, and the light emitting surface of the light source 1a in FIG. 26 and the parallelizing lens 3 in the + Z-axis direction. The Z-axis direction spacing D262 at the ends is 8.04 mm, and the positions of the parallelizing lenses 3 differ by 100 μm.

<Backlight tracking in the X-axis direction of the first embodiment>
FIG. 27 shows the back light tracking result in the X-axis direction of the first embodiment. In FIG. 27, as an enlarged view of the region “L” including the light source 1a, a light ray is incident at a height of 0.5 mm in the + Y-axis direction from the optical axis C1 whose position in the Y-axis direction shown in FIG. 25 corresponds to the interval y26b1. The enlarged view shows the case and the case where the light ray is incident at a height of 1.8 mm in the + Y-axis direction from the optical axis C1 whose position in the Y-axis direction corresponds to the interval y26t1. From FIG. 27, in the case of the interval y26b1, the range of the condensing position is Dz1m = 41.9 μm on the −Z axis direction side and Dz1p = 47.3 μm on the + Z axis direction side with respect to the light emitting surface of the light source 1a. That is, it can be seen that the light is focused in the range of -41.9 μm to +47.3 μm. Further, in the case of the interval y26t1, the range of the condensing position is Dz2m = 9.8 μm on the −Z axis direction side and Dz2p = 14.6 μm on the + Z axis direction side with respect to the light emitting surface of the light source 1a, that is, −. It can be seen that the light is focused in the range of 9.8 μm to +14.6 μm. It can be confirmed that the light collection range becomes wider when the position in the Y-axis direction is low. In addition, it can be confirmed that the condensing position is slightly deviated in the + Z axis direction when considered on average.

<Backlight tracking in the X-axis direction of the third embodiment>
FIG. 28 shows the back light tracking result in the X-axis direction of the third embodiment. In FIG. 28, as an enlarged view of the region “M” including the light source 1a, a light ray is incident at a height of 0.5 mm in the + Y-axis direction from the optical axis C1 whose position in the Y-axis direction shown in FIG. 26 corresponds to the interval y26b2. The enlarged view shows the case and the case where the light ray is incident at a height of 1.7 mm in the + Y-axis direction from the optical axis C1 whose position in the Y-axis direction corresponds to the interval y26t2. From FIG. 28, in the case of the interval y26b2, the range of the condensing position is Dz3m = 142μm and Dz3p = 52.8μm on the −Z axis direction side with respect to the light emitting surface of the light source 1a, that is, −142μm to −52. It can be seen that the light is focused within the range of 8 μm. Further, in the case of the interval y26t2, the range of the condensing position is Dz4m = 111.9 μm, Dz4p = 85.7 μm, that is, -111.9 μm to −Z axis direction side with respect to the light emitting surface of the light source 1a. It can be seen that the light is focused within the range of 85.7 μm. It can be confirmed that the light collection range becomes wider when the position in the Y-axis direction is low. Further, it can be seen that the condensing position is moved by about 50 μm or more in the −Z axis direction with respect to the light emitting surface of the light source 1a on average. Since the condensing position is moved by about 98 μm in the −Z axis direction, the light beam emitted from the center of the light source 1a in the X-axis direction has an illuminance from that of the first embodiment after emitting the parallelizing lens 3. That is, it is considered that the light emission with low parallelism is a factor for expanding the illuminance distribution in the X-axis direction as shown in FIG. 24.

<Illuminance distribution when the parallelizing lens 3 and the light deflection element 212 are moved>
29 and 30 show the illuminance distribution of light on the evaluation surface at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b of the third embodiment are turned on. FIG. 29 shows the illuminance distribution when the parallelizing lens 3 and the light deflection element 212 of the third embodiment are moved by 150 μm in the + Z axis direction. FIG. 30 shows the illuminance distribution when the parallelizing lens 3 and the light deflection element 212 of the third embodiment are moved by 100 μm in the + Z axis direction. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIGS. 29 and 30, the horizontal axis indicates the X axis (mm) and the vertical axis indicates the Y axis (mm), and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

Here, in the illuminance distribution in the X-axis direction of the first embodiment shown in FIG. 17, when the optical axis C1 is set to 0 mm, the region where the light intensity is 80% or more is continuously from −0.6 mm to +0. It can be seen that the light reaches uniformly within a range of 6 mm (1.2 mm). Further, it can be seen that the region where the light intensity is 20% or more is in the range of -1.8 mm to +1.8 mm (3.6 mm).

On the other hand, in the illuminance distribution in the X-axis direction of FIG. 30, when the light axis C1 is 0 mm, the region where the light intensity is 80% or more is continuously in the range of −0.8 mm to +0.8 mm (1.6 mm). It can be seen that the light reaches evenly. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -1.9 mm to +1.9 mm (3.8 mm). It can be confirmed that the spread of the width in the X-axis direction is slightly wider than that of the illuminance distribution in FIG. Further, in the illuminance distribution in the Y-axis direction of FIG. 30, when the optical axis C1 is 0 mm, the region where the light intensity is 80% or more continuously is in the range of -10.0 mm to + 10.0 mm (20.0 mm). It can be seen that the light reaches evenly. Further, it can be seen that the region where the light intensity is 20% or more is in the range of −12.3 mm to +12.4 mm (24.7 mm). From this, it can be confirmed that the width in the Y-axis direction is slightly wider than that of the illuminance distribution in FIG.

As can be seen from the illuminance distribution in the X-axis direction in FIG. 30, by moving the parallelizing lens 3 and the light deflection element 212 by 100 μm in the + Z-axis direction, the focal position in the X-axis direction is approximately aligned with the light emitting surface of the light source 1a. In order to match, the spread of the illuminance distribution in the X-axis direction is smaller than that in FIG. 24 in which the focal position in the X-axis direction moves about 100 μm in the −Z-axis direction with respect to the light emitting surface of the light source 1a. Can be confirmed. From this, it is considered preferable to align the focal position in the X-axis direction, where the divergence angle of the light source is large, with the light emitting surface of the light source. That is, in the Y-axis direction where the divergence angle is small, the focal depth is deeper than in the X-axis direction where the divergence angle is large, the sensitivity to the focal position is low, and the influence on the illuminance distribution is small. It is considered preferable to adjust to the focal position.

Further, from FIG. 29, it can be confirmed that when the parallelizing lens 3 and the light deflection element 212 of the third embodiment are further moved by 50 μm in the + Z-axis direction, a region having a light intensity of 20% or more expands in the X-axis direction. It can be seen that it is preferable to give priority to the focal position in the X-axis direction over the focal position in the Y-axis direction.

<Correction of light collection position in X-axis direction and Y-axis direction>
As described above, when the light deflection element 212 having an inclination on the incident surface is used, the back ray tracking that incidents a light ray on the parallelizing lens 3 in the X-axis direction and the Y-axis direction from the + Z-axis direction to the −Z-axis direction. It can be seen that the focal position is different when the above is performed, and the X-axis direction is blurred on the evaluation surface when the focus is adjusted in the Y-axis direction. Regarding the difference between the focal positions in the X-axis direction and the Y-axis direction, the surface of the parallelizing lens 3 on the + Z-axis direction is not an aspherical surface that is rotationally symmetric with respect to the Z-axis, but the curvature of the ZX plane is calculated from the curvature of the YZ plane. By increasing the size, it is possible to move the focal position in the X-axis direction in the + Z-axis direction, and it is assumed that it is possible to approach the focal position in the Y-axis direction. That is, it is considered that the surface of the parallelizing lens 3 on the + Z axis direction side should be an anamorphic aspherical surface. For example, on the surface of the parallelizing lens 3 on the + Z axis direction side, the conic constant and the aspherical coefficient similar to those of the YZ plane may be set in the ZX plane, and only the curvature may be increased. For example, the radius of curvature of the YZ plane may be 4.90 mm, and the radius of curvature of the ZX plane may be 4.81 mm. The incident surface, that is, the surface on the −Z axis direction side may have a shape that is rotationally symmetric with respect to the center of the Z axis. For example, it may be a concave shape of a spherical surface having a radius of curvature of 43.7 mm.

<Embodiment 4: Illuminance distribution when an anamorphic aspherical surface is used>
FIG. 31 shows the illuminance distribution when the surface of the parallelizing lens 3 on the + Z axis direction is an anamorphic aspherical surface as the light source device of the fourth embodiment. That is, in FIG. 31, on the surface of the parallelizing lens 3 in the + Z axis direction, the curvature radius of an anamorphic aspherical surface in which the curvature of the ZX plane is larger than the curvature of the YZ plane, for example, the radius of curvature of the YZ plane is 4.90 mm, and the curvature of the ZX plane. The illuminance distribution of the light on the evaluation plane at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on with the radius set to 4.81 mm is shown. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIG. 31, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

In the illuminance distribution in the X-axis direction of FIG. 31, when the light axis C1 is 0 mm, the region where the light intensity is 80% or more is continuously uniform in the range of −0.4 mm to +0.5 mm (0.9 mm). It can be seen that the light has reached. Further, it can be seen that the region where the light intensity is 20% or more is in the range of −1.5 mm to +1.5 mm (3.0 mm). It can be confirmed that the spread of the width in the X-axis direction is slightly narrower than that of the illuminance distribution in FIG.

Further, in the illuminance distribution in the Y-axis direction, when the area on the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is uniformly in the range of -9.9 mm to +9.9 mm (19.8 mm). You can see that the light has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -12.5 mm to + 12.6 mm (25.1 mm). From this, it can be confirmed that the width in the Y-axis direction is slightly wider than the illuminance distribution in FIG.

From the above, it can be confirmed that an illuminance distribution substantially similar to the illuminance distribution of FIG. 17 of the light source device 100 of the first embodiment using the light deflection element 2 can be obtained. As a result, the effect of the anamorphic aspherical surface was confirmed. Further, when compared with the illuminance distribution in the case of defocusing shown in FIG. 30, it can be confirmed that the spread of the illuminance distribution in the X-axis direction is further suppressed. In the parallelizing lens 3, it is preferable that the ZX plane and the YZ plane have an aspherical shape, and when one of them has a spherical surface, for example, on the toroidal surface, the spread in the X-axis direction is suppressed, but aberrations occur. The effect of the light is large, and the utilization efficiency of the light reaching the vicinity of the optical axis C1 on the evaluation surface is lowered.

The anamorphic aspherical surface described in the fourth embodiment shows a case where the conic constants and the aspherical surface coefficients of the YZ plane and the ZX plane are the same, and only the radius of curvature is different. The conic constants and aspherical coefficients of the YZ plane and the ZX plane may have different shapes, but the shape becomes complicated and there is a concern that the workability may be affected.

Further, although the surface shape on the + Z-axis side of the parallelizing lens 3 has been described, the surface shape on the + Z-axis side is an aspherical shape that is rotationally symmetric with respect to the center of the Z-axis, and is a ZX plane with respect to the surface in the −Z-axis direction. The curvature may be larger than the curvature of the YZ plane. For example, the surface on the + Z-axis side is an aspherical surface rotationally symmetric with respect to the center of the Z-axis with the radius of curvature of the surface shape on the + Z-axis side set to 4.90 mm, and the surface on the -Z-axis side is the surface shape on the -Z-axis side. A concave toroidal surface having a radius of curvature of 43.7 mm on the YZ plane and a radius of curvature of 70 mm on the ZX plane may be used. Since the surface shape on the −Z axis side is concave, that is, has a negative curvature, the curvature is larger in the ZX plane than in the YZ plane. The curvature is the reciprocal of the radius of curvature.

<When the surface in the -Z axis direction is a toroidal surface>
FIG. 32 shows an illuminance distribution when the surface of the parallelizing lens 3 on the −Z axis direction side is a toroidal surface as a modification of the light source device of the fourth embodiment. That is, in FIG. 32, a concave toroidal surface having a radius of curvature of the YZ plane of 43.7 mm and a radius of curvature of the ZX plane of 70 mm on the surface on the −Z axis side of the parallelizing lens 3 is shown on the + Z axis direction side. The surface shape is a rotationally symmetric aspherical surface, and the illuminance distribution of light on the evaluation surface at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on is shown. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIG. 32, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

In the illuminance distribution in the X-axis direction of FIG. 32, when the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is continuously uniform in the range of −0.4 mm to +0.4 mm (0.8 mm). It can be seen that the light has reached. Further, it can be seen that the region where the light intensity is 20% or more is in the range of −1.3 mm to +1.3 mm (2.6 mm). It can be confirmed that the spread of the width in the X-axis direction is slightly narrower than that of the illuminance distribution in FIG.

Further, in the illuminance distribution in the Y-axis direction, when the area on the optical axis C1 is 0 mm, the region where the light intensity is 80% or more continuously is uniformly in the range of -10.1 mm to + 10.0 mm (20.1 mm). You can see that the light has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -12.5 mm to +12.5 mm (25.0 mm). From this, it can be confirmed that the width in the Y-axis direction is slightly wider than that of the illuminance distribution in FIG.

From the above, it can be confirmed that an illuminance distribution substantially similar to the illuminance distribution of FIG. 17 of the light source device 100 of the first embodiment using the light deflection element 2 can be obtained. As a result, the effect of the toroidal surface was confirmed. Further, when compared with the illuminance distribution in the case of defocusing shown in FIG. 30, it can be confirmed that the spread of the illuminance distribution in the X-axis direction is further suppressed.

Here, in the fourth embodiment, the surface of the parallelizing lens 3 on the −Z axis direction side and the surface on the + Z axis direction side show different shapes, but the shape is not limited to this, and the parallelizing lens is not limited to this. In 3, the curvature of the ZX plane may be larger than the curvature of the YZ plane.

The toroidal surface showing the effect in the modified example of the fourth embodiment shows the case where the conic constant = 0 and the aspherical coefficient = 0 in the ZX plane and the YZ plane. Having a conic constant and an aspherical coefficient raises concerns that the shape will be complicated. That is, the ZX plane and the YZ plane are toroidal planes having different curvatures or radii of curvature of the spherical surface. It should be noted that the third embodiment has a greater effect than the first embodiment in that the surface of the parallelizing lens 3 on the + Z axis direction side is an anamorphic aspherical surface or the surface on the −Z axis direction side is a toroidal surface. However, as in the illuminance distribution in FIG. 17, even when the inclined surface of the light deflection element 2 is provided on the + Z-axis direction side, the light beam condensing position on the X-axis direction side and the condensing position on the Y-axis direction side. Is different, and the light distribution width on the evaluation surface in the X-axis direction may be narrowed by making the surface of the parallelizing lens 3 on the + Z-axis direction side an anamorphic aspherical surface. Further, the surface of the parallelizing lens 3 on the −Z axis direction side may be used as a toroidal surface.

<When an anamorphic aspherical surface is applied to the first embodiment>
The parallelizing lens 3 of the light source device 100 of the first embodiment may have a conic constant and an aspherical coefficient similar to those of the YZ plane on the surface on the + Z axis direction side, and may have an anamorphic aspherical surface by increasing only the curvature. .. For example, the radius of curvature of the YZ plane is 4.90 mm, and the radius of curvature of the ZX plane is 4.895 mm. The incident surface, that is, the surface on the −Z axis direction side may have a shape that is rotationally symmetric with respect to the center of the Z axis. For example, it may be a concave shape of a spherical surface having a radius of curvature of 43.7 mm.

FIG. 33 shows the illuminance distribution of light on the evaluation surface at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIG. 33, the horizontal axis shows the X axis (mm) and the vertical axis shows the Y axis (mm), and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

In the illuminance distribution in the X-axis direction of FIG. 33, when the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is continuously uniform in the range of -0.5 mm to +0.5 mm (1.0 mm). It can be seen that the light has reached. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -1.8 mm to +1.8 mm (3.6 mm). Compared with FIG. 17, it can be confirmed that the expansion of the width in the X-axis direction in the region where the light intensity is 80% or more is slightly narrower.

Further, in the illuminance distribution in the Y-axis direction, when the area on the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is uniformly in the range of -8.8 mm to +8.8 mm (17.6 mm). You can see that the light has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -11.5 mm to +11.5 mm (23.0 mm). From this, it can be confirmed that the spread of the width in the Y-axis direction is almost the same as that of the illuminance distribution in FIG.

From the above, when the anamorphic aspherical surface is applied to the parallelized lens 3 of the light source device 100 of the first embodiment, the illuminance in the X-axis direction is compared with the illuminance distribution in FIG. 17 when the anamorphic aspherical surface is not applied. It can be confirmed that the distribution is slightly narrower. As a result, the effect of the anamorphic aspherical surface was confirmed.

The anamorphic aspherical surface applied to the parallelizing lens 3 of the light source device 100 of the first embodiment, which has the same effect as that of the fourth embodiment, has the same cornic constant and aspherical coefficient of the YZ plane and the ZX plane, and has a curvature. The case where only the radius is different is shown.

Further, as described with reference to FIG. 27, in the light source device 100 of the first embodiment, it is assumed that the light condensing position in the X-axis direction is located on the + Z-axis direction side from the light emitting surface of the light source. Considering the intensity distribution (light distribution) of the light source from the result of the illuminance distribution in FIG. 33, it is considered that the light collecting position in the X-axis direction is located on the −Z-axis direction side from the light emitting surface, so that the curvature of the ZX plane is determined. It is considered that the effect was obtained by making it larger than the curvature of the YZ plane.

<When the toroidal surface is applied to the first embodiment>
The parallelizing lens 3 of the light source device 100 of the first embodiment has an aspherical shape whose surface shape on the + Z-axis side is rotationally symmetric with respect to the center of the Z-axis, and the curvature of the ZX plane with respect to the plane in the −Z-axis direction is the YZ plane. It may be made larger than the curvature of and used as a toroidal surface. For example, the surface on the + Z-axis side is an aspherical surface rotationally symmetric with respect to the center of the Z-axis with the radius of curvature of the surface on the + Z-axis side set to 4.90 mm, and the surface on the -Z-axis side is the YZ of the surface on the -Z-axis side. A concave toroidal surface may be used, in which the radius of curvature of the plane is 43.7 mm and the radius of curvature of the ZX plane is 50 mm. Since the surface shape on the −Z axis side is concave, that is, has a negative curvature, the curvature is larger in the ZX plane than in the YZ plane.

FIG. 34 shows the illuminance distribution of light on the evaluation surface at a distance of 2000 mm from the light source 1a and the light source 1b when both the light source 1a and the light source 1b are turned on. Incidentally, the divergence angle of the light source 1a and the light source 1b are both from FIG. 3, 1 / ^{e 2} is approximately ± 37 ° in the X-axis direction (RY direction), 1 / ^{e 2} of the Y-axis direction (RX direction) ± It was set to about 5 °. In FIG. 34, an X-axis (mm) is shown on the horizontal axis and a Y-axis (mm) is shown on the vertical axis, and the light intensity is divided into five gradations. The brightest white color represents 100% intensity.

In the illuminance distribution in the X-axis direction of FIG. 34, when the optical axis C1 is 0 mm, the region where the light intensity is 80% or more is continuously uniform in the range of −0.3 mm to +0.3 mm (0.6 mm). It can be seen that the light has reached. Further, it can be seen that the region where the light intensity is 20% or more is in the range of −1.3 mm to +1.3 mm (2.6 mm). It can be confirmed that the spread of the width in the X-axis direction is narrower than that of the illuminance distribution in FIG.

Further, in the illuminance distribution in the Y-axis direction, when the light axis C1 is 0 mm, the region where the light intensity is 80% or more is uniformly in the range of -9.1 mm to +9.0 mm (18.1 mm). You can see that the light has arrived. Further, it can be seen that the region where the light intensity is 20% or more is in the range of -11.3 mm to +11.3 mm (22.6 mm). From this, it can be confirmed that the spread of the width in the Y-axis direction is almost the same as that of the illuminance distribution in FIG.

From the above, it was confirmed that when the toroidal surface is applied to the parallelized lens 3 of the light source device 100, the illuminance distribution in the X-axis direction becomes narrower than the illuminance distribution in FIG. 17 when the toroidal surface is not applied. can. As a result, the effect of the toroidal surface was confirmed.

The toroidal surface applied to the parallelizing lens 3 of the light source device 100 of the first embodiment, in which the same effect as that of the fourth embodiment is obtained, has a conic constant = 0 and an aspherical coefficient = 0 in the ZX plane and the YZ plane. Shows the case of. Having a conic constant and an aspherical coefficient raises concerns that the shape will be complicated. That is, the ZX plane and the YZ plane are toroidal planes having different curvatures (or radii of curvature) of the spherical surfaces.

Further, as described with reference to FIG. 27, in the light source device 100 of the first embodiment, it is assumed that the light condensing position in the X-axis direction is located on the + Z-axis direction side from the light emitting surface of the light source. Considering the intensity distribution (light distribution) of the light source from the result of the illuminance distribution in FIG. 34, it is considered that the light condensing position in the X-axis direction is located on the −Z-axis direction side from the light emitting surface, so that the curvature of the ZX plane. It is considered that the effect was obtained by making the value larger than the curvature of the YZ plane.

<When the inclined surface of the third embodiment is a curved surface>
When the inclined surface on the −Z axis direction side of the light source device 2121 of the light source device 2101 of the third embodiment shown in FIG. 20 is not a flat surface but a curved surface, for example, the curved surface on the + Y axis direction side from the optical axis C1 is formed. It becomes a spherical surface or an aspherical surface in which the center of curvature is located in the + Y-axis direction from the center of the light source 1a, and the light beam emitted from the light source 1a is deflected in the + Y-axis direction and emitted. At this time, the larger the curvature, the stronger the influence of the deflection. As an example of this measure, in order to make the light ray after the emission of the parallelizing lens 3 parallel to the optical axis C1, for example, in the parallelizing lens 3, the parallelizing lens with respect to the curved surface on the + Y axis direction side from the optical axis C1. By setting the center of curvature of No. 3 in the −Y axis direction, the light ray traveling in the + Y axis direction is deflected in the −Y axis direction, so that the light ray parallel to the optical axis C1 can be obtained.

That is, the parallelizing lens 3 is set to the curved surface on the + Y-axis direction side from the optical axis C1, the center of curvature of the parallelizing lens 3 is set to the -Y-axis direction, and the curved surface on the -Y-axis direction side from the optical axis C1. By setting the center of curvature of the parallelizing lens 3 in the + Y-axis direction and integrating two lenses with different positions of the center of curvature, the apparent length of the light source in the Y-axis direction is shortened as in the illuminance distribution in FIG. It becomes possible to do.

Considering the manufacturing cost of forming the inclined surface of the optical deflection element 212 on the −Z axis direction side into a curved surface and the manufacturing cost of integrating lenses having different centers of curvature, the first embodiment, the third embodiment, or the present embodiment It is considered that the fourth embodiment is preferable.

<Embodiment 5: Example of the number of light sources of 3 or more>
FIG. 35 is a diagram showing a schematic configuration of the light source device 100A according to the fifth embodiment. As shown in FIG. 35, the number of light sources can be three or more. In the example shown in FIG. 35, in addition to the light source 14a (first light source) and the light source 14b (second light source) arranged on the optical axis C1, a light source 14c (third) is further placed on the optical axis C1. Light source) is arranged. When such a light source group 14 is used, the light deflection element 20 as shown in FIG. 35 can be used. The optical deflection element 20 shown in FIG. 35 has a first optical surface 20c having no inclination with respect to a reference plane (XY plane) perpendicular to the optical axis C1 on the optical axis C1, and both sides thereof with respect to a reference plane. It includes a second optical surface 20a and a third optical surface 20b having an inclination. The first optical surface 20c emits light rays emitted from the light source 14c from the optical deflection element 20 at the same angle in the + Z axis direction. The second optical surface 20a emits a light ray emitted from the light source 14a in the + Z-axis direction at an angle in the + Y-axis direction as in the light ray 501cc in FIG. 5, for example. The third optical surface 20b emits a light ray emitted from the light source 14b at an angle in the −Y axis direction in the + Z axis direction. The second optical surface 20a causes the virtual focusing point of the light source 14a to move in the + Z-axis direction, and the third optical surface 20b causes the virtual focusing point of the light source 14b to move in the + Z-axis direction. Moving. Therefore, the following adjustment may be made so as to align the position in the Z-axis direction with the virtual condensing points of both. That is, the first optical surface 20c may be moved in the + Z axis direction to adjust the air conversion length. Further, the light source 14c may be moved in the + Z axis direction.

By adopting such a configuration, it is possible to further improve the light utilization efficiency near the optical axis C1.

Although the example shown in FIG. 35 shows an example in which an optical surface for light deflection is arranged on the light incident side, it is also possible to provide the optical surface on the light emitting side. By adopting such a configuration, it is possible to further improve the light utilization efficiency in the vicinity of the optical axis C1.

It is also possible to substitute the same deflection function by using a mirror. In this case, in the case of substituting the optical deflection element 20 shown in FIG. 35, no mirror is provided in the portion corresponding to the first optical surface 20c having no inclination, and the second optical surface 20a and the third optical surface 20a and the third optical surface 20a are not provided. A mirror will be provided on the portion corresponding to the optical surface 20b of the above. Further, as in the case of FIG. 35, the light source 14c may be moved in the + Z-axis direction so as to match the positions of the virtual condensing points of the light source 14a and the light source 14b in the Z-axis direction. Therefore, in the present disclosure, the "light deflection element" in a broad sense is a member that adjusts the length of the entire apparent light source in the Y-axis direction in the arrangement direction of the light source by deflecting the light by using reflection (this example). Then, the above mirror) is also included. In addition, in order to obtain the effect of the fifth embodiment, a configuration in which the number of light sources is two or more is preferable. Further, by using the parallelized lens 3 of the fourth embodiment, it is possible to obtain the effect of the fourth embodiment.

Although the present disclosure has been described in detail, the above description is exemplary in all aspects and the disclosure is not limited thereto. It is understood that a myriad of variants not illustrated can be envisioned without departing from the scope of the present disclosure.

It should be noted that, within the scope of the disclosure, each embodiment can be freely combined, and each embodiment can be appropriately modified or omitted.

Claims

A parallelizing lens that parallelizes the incident light,
It contains a plurality of light sources arranged apart from each other in a direction away from the optical axis of the parallelized lens, and diverges in a first direction and a second direction parallel to the direction away from the optical axis, which are orthogonal to each other as a whole. A group of light sources that emit light sources with different angles,
It is arranged between the light source group and the parallelizing lens in the direction of the optical axis, and in the first direction in which the divergence angle of the light source group is small among the first direction and the second direction. A light source device including a light deflection element that deflects light emitted from each of the plurality of light sources in a direction away from the optical axis and causes the light to enter the parallelizing lens.
The light deflection element is
The light source device according to claim 1, wherein the light emitted from each of the plurality of light sources is transmitted, refracted, and deflected in a direction away from the optical axis.
The light deflection element is
The light source device according to claim 2, which has an optical surface for light deflection on the light emitting side.
The light deflection element is
The light source device according to claim 2 or 3, further comprising an optical surface for light deflection on the light incident side.
When parallel light is incident on the parallelizing lens from the side opposite to the light source group in the direction along the optical axis, the focusing position of the parallel light by the optical system including the parallelizing lens and the light deflection element. The light source device according to any one of claims 2 to 4, wherein the light source device is located at the center of each of the plurality of light sources in the first direction.
The light deflection element is
The light source device according to claim 1, wherein the light emitted from each of the plurality of light sources is reflected and deflected in a direction away from the optical axis.
The light deflection element has a light reflecting surface and has a light reflecting surface.
The distance between the central portion of one light source among the plurality of light sources and the optical axis is defined as the interval y1ac.
The distance between the central portion of the one light source and the reflecting surface is defined as the distance D4.
When the tilt angle of the reflective surface with respect to the optical axis is α9,
The interval D4 is
It is set based on the relational expression of y1ac / D4 = sin (2 × | α9 |).
The light source device according to claim 6, wherein the interval D4 allows an error of ± 10%.
When parallel light is incident on the parallelizing lens from the side opposite to the light source group in the direction along the optical axis, the focusing position of the parallel light by the optical system including the parallelizing lens and the light deflection element. The light source device according to claim 6 or 7, wherein the light source device is located between the plurality of light sources and the optical deflection element.
The light source device according to claim 1 or 8, which has a ring-shaped illuminance distribution at a position on the parallelizing lens side from a focal position on the plurality of light sources side of the parallelizing lens.
The light source group is
The plurality of light sources arranged apart from the optical axis include a first light source and a second light source, and further include a third light source arranged on the optical axis.
The light deflection element is
Claims 1 to 9 for deflecting light emitted from each of the first and second light sources as the plurality of light sources in the first direction of the light source group in a direction away from the optical axis. The light source device according to any one of the above items.
The parallelized lens is
The light source device according to any one of claims 1 to 5, wherein the curvature in the second direction is different from the curvature in the first direction.
The parallelized lens is
11. The light source device according to claim 11, wherein the emission surface has an anamorphic aspherical surface.
The parallelized lens is
The light source device according to claim 11, wherein the incident surface is a toroidal surface in which the curvature of the spherical surface differs between the second direction and the first direction.
The parallelized lens is
The light source device according to any one of claims 11 to 13, wherein the curvature in the second direction is larger than the curvature in the first direction.