WO2024070714A1 - 空中像表示装置 - Google Patents

空中像表示装置 Download PDF

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Publication number
WO2024070714A1
WO2024070714A1 PCT/JP2023/033452 JP2023033452W WO2024070714A1 WO 2024070714 A1 WO2024070714 A1 WO 2024070714A1 JP 2023033452 W JP2023033452 W JP 2023033452W WO 2024070714 A1 WO2024070714 A1 WO 2024070714A1
Authority
WO
WIPO (PCT)
Prior art keywords
concave mirror
display device
light
aerial image
image
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2023/033452
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
宏悦 河西
諒 忠内
主揮 下瀬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kyocera Corp
Original Assignee
Kyocera Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kyocera Corp filed Critical Kyocera Corp
Priority to JP2024550065A priority Critical patent/JPWO2024070714A1/ja
Priority to CN202380067640.1A priority patent/CN119856101A/zh
Priority to EP23871947.0A priority patent/EP4597207A1/en
Priority to US19/114,165 priority patent/US20260036828A1/en
Publication of WO2024070714A1 publication Critical patent/WO2024070714A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B30/00Optical systems or apparatus for producing three-dimensional [3D] effects, e.g. stereoscopic images
    • G02B30/50Optical systems or apparatus for producing three-dimensional [3D] effects, e.g. stereoscopic images the image being built up from image elements distributed over a three-dimensional [3D] volume, e.g. voxels
    • G02B30/56Optical systems or apparatus for producing three-dimensional [3D] effects, e.g. stereoscopic images the image being built up from image elements distributed over a three-dimensional [3D] volume, e.g. voxels by projecting aerial or floating images
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B5/00Optical elements other than lenses
    • G02B5/08Mirrors
    • G02B5/10Mirrors with curved faces

Definitions

  • This disclosure relates to an aerial image display device.
  • an aerial image display device is known, for example as described in Patent Document 1.
  • the aerial image display device of the present disclosure includes a display device having a display surface, a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a second concave mirror that reflects the image light reflected by the first concave mirror in a direction different from the direction toward the first concave mirror, and forms a real aerial image;
  • the optical system further includes a light-shielding member that is positioned between the display device and the second concave mirror and is not positioned in the optical path of the image light that travels from the display surface, via the first concave mirror and the second concave mirror, to the aerial image.
  • the aerial image display device of the present disclosure includes a display device having a display surface, a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a convex mirror that reflects the image light reflected by the first concave mirror in a direction different from a direction toward the first concave mirror; a second concave mirror that reflects the image light reflected by the convex mirror in a direction different from the direction toward the convex mirror, and forms a real aerial image; a light blocking member that is located between the display device and the second concave mirror and is not located in an optical path of the image light that travels from the display surface through the first concave mirror, the convex mirror, and the second concave mirror to the aerial image, The convex mirror is located between the light blocking member and the second concave mirror.
  • the aerial image display device of the present disclosure includes a display device having a display surface, a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a second concave mirror that reflects the image light reflected by the first concave mirror in a direction different from the direction toward the first concave mirror, and forms a real aerial image;
  • the display device includes a focusing member that is located between the display device and the first concave mirror and that collimates the image light emitted from the display surface.
  • FIG. 1 is a cross-sectional view showing a main configuration of an aerial image display device according to an embodiment of the present disclosure.
  • 2 is a cross-sectional view of a first concave mirror for explaining the curvature of the first concave mirror of the aerial image display device of FIG. 1 .
  • FIG. 13 is a cross-sectional view showing a main configuration of an aerial image display device according to another embodiment of the present disclosure.
  • FIG. 13 is a cross-sectional view showing a main configuration of an aerial image display device according to still another embodiment of the present disclosure.
  • the conventional aerial image display device described in Patent Document 1 uses optical elements such as a beam splitter and a retroreflector to focus the image light emitted by the display device into a real aerial image.
  • the optical elements can cause part of the image light to be directed in an undesired direction or location, resulting in ghost images or virtual images being perceived by the user, reducing the visibility of the aerial image.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • the display device according to an embodiment may include well-known components such as a housing and an optical system support member, which are not shown.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • the display device according to an embodiment may include well-known components such as a housing and an optical system support member, which are not shown.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • the display device according to an embodiment may include well-known components such as a housing and an optical system support member, which are not shown.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • FIG. 1 shows the main components of an aerial image display device according to an embodiment.
  • FIG. 1 shows the display device according to an embodiment.
  • FIG. 1 shows the display device according to an embodiment.
  • FIG. 1 shows the display device according to an
  • FIG. 1 is a cross-sectional view showing the main configuration of an aerial image display device according to one embodiment of the present disclosure
  • FIG. 2 is a cross-sectional view of a first concave mirror for explaining the curvature of the first concave mirror of the aerial image display device of FIG. 1.
  • the aerial image display device 1 of this embodiment includes a display device 2, a first concave mirror 3, a second concave mirror 5, and a light-shielding member 6.
  • the display device 2 has a display surface 2a, and displays an image propagating as image light L on the display surface 2a. That is, the display device 2 emits the image light L from the display surface 2a.
  • the display device 2 may be a transmissive display device.
  • the transmissive display device may be, for example, a liquid crystal display device including a backlight and a liquid crystal panel.
  • the backlight may be a direct-type backlight having a plurality of light sources arranged two-dimensionally on the rear side of the liquid crystal panel.
  • the backlight may be an edge-light type backlight having a plurality of light sources arranged on the outer periphery of the liquid crystal panel.
  • the edge-light type backlight may have a lens array, a light guide plate, a diffusion plate, etc. for uniformly irradiating the liquid crystal panel.
  • the light source of the backlight may be, for example, a light-emitting diode (LED) element, a cold cathode fluorescent lamp, a halogen lamp, a xenon lamp, etc.
  • the liquid crystal panel may be a known liquid crystal panel.
  • the known liquid crystal panel may be, for example, an IPS (In-Plane Switching) type, an FFS (Fringe Field Switching) type, a VA (Vertical Alignment) type, an ECB (Electrically Controlled Birefringence) type, etc. liquid crystal panel.
  • the transmissive display device is not limited to a liquid crystal display device.
  • the transmissive display device may be, for example, a MEMS (Micro Electro Mechanical Systems) shutter display device that includes a backlight and a MEMS shutter.
  • MEMS Micro Electro Mechanical Systems
  • the display device 2 is not limited to a transmissive display device, but may be a self-luminous display device including light-emitting elements such as LED elements, organic electroluminescence (OEL) elements, organic light-emitting diode (OLED) elements, and semiconductor laser (LD) elements.
  • light-emitting elements such as LED elements, organic electroluminescence (OEL) elements, organic light-emitting diode (OLED) elements, and semiconductor laser (LD) elements.
  • the first concave mirror 3 and the second concave mirror 5 constitute a reflective optical system that focuses the image light L emitted from the display device 2 as an aerial image R.
  • the first concave mirror 3 and the second concave mirror 5 may be collectively referred to as the reflective optical system 8.
  • the first concave mirror 3 is located on the optical path of the image light L emitted from the display device 2.
  • the first concave mirror 3 is configured to reflect the image light L emitted from the display device 2 in a direction different from the direction toward the display device 2.
  • the first concave mirror 3 may be provided with an adjustment member that adjusts the relative spatial arrangement with respect to the display device 2 (distance from the display surface 2a, inclination angle with respect to the display surface 2a, etc.).
  • the adjustment member may have, for example, a support member such as a rod installed on the back side of the first concave mirror 3, an axis member installed on the support member for rotating the support member and the first concave mirror 3, a slide mechanism for translating the support member and the first concave mirror 3, etc.
  • the adjustment member may be adjusted manually or electrically by a stepping motor or the like.
  • the second concave mirror 5 is located on the optical path of the image light L reflected by the first concave mirror 3.
  • the second concave mirror 5 is configured to reflect the image light L reflected by the first concave mirror 3 in a direction different from the direction toward the first concave mirror 3, forming a real aerial image R.
  • the second concave mirror 5 may be provided with an adjustment member that adjusts its spatial arrangement relative to the first concave mirror 3 (distance from the first concave mirror 3, inclination angle with respect to the first concave mirror 3, etc.). This adjustment member may be configured similarly to the adjustment member provided on the first concave mirror 3.
  • the first concave mirror 3 and the second concave mirror 5 have a reflecting surface 3a and a reflecting surface 5a, respectively.
  • the first concave mirror 3 and the second concave mirror 5 may be free-form mirrors in which the shape of the reflecting surfaces 3a, 5a is a free-form surface.
  • the first concave mirror 3 and the second concave mirror 5 are free-form mirrors, it is possible to reduce distortion of the aerial image R by appropriately designing the shape of the reflecting surfaces 3a, 5a.
  • the free-form surface defining the reflecting surfaces 3a and 5a may be an XY polynomial surface (also called an SPS XYP surface) defined by the following formulas (1) and (2).
  • the XY polynomial surface is expanded into a polynomial of up to the tenth degree that is added to the reference conic surface. Therefore, in formulas (1) and (2), the sum of m and n is 10 or less.
  • z is the sag of the surface parallel to the z axis (also called the optical axis)
  • c is the vertex curvature
  • k is the conic constant
  • r satisfies r2 x2 + y2
  • Cj is a coefficient of the monomial xmyn .
  • the light blocking member 6 is located between the display device 2 and the second concave mirror 5.
  • the light blocking member 6 is not located in the optical path of the image light L that travels from the display surface 2a to the aerial image R via the first concave mirror 3 and the second concave mirror 5.
  • the light blocking member 6 can block the image light L' that travels directly from the display surface 2a to the second concave mirror 5. Therefore, the aerial image display device 1 can effectively prevent the image light L emitted from the display surface 2a from reaching the second concave mirror 5 without passing through the first concave mirror 3 and being reflected by the second concave mirror 5 in an undesired direction and location.
  • image light L' traveling directly from the display surface 2a to the second concave mirror 5 is more likely to occur in recent years because the viewing angle of the image light L in the display device 2 has become closer to ⁇ 180°.
  • ghost images and virtual images are more likely to occur, but the aerial image display device disclosed herein can reduce or eliminate the effects of such problems.
  • the light blocking member 6 may be located between the display device 2 and the second concave mirror 5, closer to the display device 2. In this case, it is possible to block the image light L' that travels directly from the display surface 2a to the second concave mirror 5 while preventing the light blocking member 6 from becoming too large.
  • the light blocking member 6 may be in contact with the display device 2.
  • the light blocking member 6 may be located along at least a portion of the periphery of the display surface 2a, for example, along a portion of the display surface 2a closer to the second concave mirror 5. If the display surface 2a is rectangular, the light blocking member 6 may be located along one or two edges of the display surface 2a closer to the second concave mirror 5.
  • the light blocking member 6 may also extend from a virtual plane including the display surface 2a along the emission direction of the image light L from the display surface 2a.
  • the light blocking member 6 may extend in a direction perpendicular to the display surface 2a. In this case, the image light L' that travels directly from the display surface 2a to the second concave mirror 5 can be effectively blocked while preventing the light blocking member 6 from becoming too large.
  • the light-shielding member 6 may be made of, for example, a metal material such as aluminum, magnesium, copper, zinc, etc., or an alloy material such as stainless steel, a copper-zinc alloy, or an aluminum-copper alloy.
  • the light-shielding member 6 may have a roughened surface 6a (also called a light-shielding surface) facing the display surface 2a, the light-shielding surface 6a may have a fine uneven structure, and a light-absorbing layer may be formed on the light-shielding surface 6a.
  • the fine uneven structure may have an arithmetic mean roughness of about 1 nm to 100 nm, or about 10 nm to 55 nm (about 1/10 of the central visible light wavelength of 555 nm), but is not limited to these ranges.
  • the light absorbing layer formed on the light shielding surface 6a may be composed of a resin material (e.g., epoxy resin, silicone resin, acrylic resin, etc.) containing a light absorbing material.
  • the light absorbing material may be an inorganic pigment, and the inorganic pigment may be a carbon-based pigment such as carbon black, a nitride-based pigment such as titanium black, or a metal oxide-based pigment such as Cr-Fe-Co, Cu-Co-Mn (manganese), Fe-Co-Mn, or Fe-Co-Ni-Cr.
  • the surface of the light absorbing layer may have a fine uneven structure, so that the image light L that reaches the light shielding surface 6a is more easily absorbed by the light absorbing layer on the light shielding surface 6a.
  • This fine uneven structure may have a surface roughness that includes a surface roughness (arithmetic mean roughness) of about 1/10 (about 55 nm) or less of the central frequency of visible light, about 550 nm, or a surface roughness (arithmetic mean roughness) of about 55 nm or less.
  • the micro-relief structure may have an arithmetic mean roughness of about 1 nm to 100 nm, or about 10 nm to 55 nm, but is not limited to these ranges.
  • the light blocking member 6 may be configured to have an electrically adjustable light transmittance.
  • the light blocking member 6 may be a liquid crystal shutter (also called an LCW (LC window)) using polymer liquid crystal.
  • the voltage applied to the liquid crystal shutter can be made to function as the light blocking member 6 by setting the voltage applied to the liquid crystal shutter to an off voltage (a voltage for blocking light).
  • the light transmittance (light blocking ability) of the light blocking member 6 can be controlled by setting the voltage applied to the liquid crystal shutter to an intermediate voltage between the off voltage and the on voltage.
  • the light transmittance of the light blocking member 6 may be about 0% to about 90%, or about 5% to about 80%, but is not limited to these ranges.
  • the light-shielding member 6 may also be an electrophoretic display (EPD).
  • EPDs are also known as electronic paper. EPDs have the advantages of not requiring a backlight, consuming low power as they retain their state without the need for current, and having a wide operating temperature range of approximately 0°C to 50°C.
  • the operating speed of an EPD is approximately 250 ms (milliseconds), which is slower than an LCD shutter, but this operating speed is not problematic for the light-shielding member 6. In other words, once the light-shielding properties are imparted to the light-shielding member 6, it is essentially necessary to maintain that state.
  • the height of the light blocking member 6 (height from the display surface 2a) is set so as not to overlap with the optical path of the image light L that forms the aerial image R, as shown in FIG. 1. In other words, the height of the light blocking member 6 is set so as not to affect the formation of the aerial image R, or so as not to cause a portion of the aerial image R to be missing.
  • the height of the light blocking member 6 is set so as not to enter the image light propagation space that connects the entire surface of the reflecting surface 3a of the first concave mirror 3 and the entire surface of the reflecting surface 5a of the second concave mirror 5. In the case of the configuration of FIG.
  • the height of the light blocking member 6 is set so as not to enter the image light propagation space that connects the entire surface of the reflecting surface 3a of the first concave mirror 3, the entire surface of the reflecting surface 4a of the convex mirror 4, and the entire surface of the reflecting surface 5a of the second concave mirror 5.
  • the height of the light blocking member 6 may be about 0.1 mm to 30 mm, but is not limited to this range.
  • the light shielding member 6 may also be configured such that the shortest distance between the light path of the image light L is longer than the visible light wavelength (approximately 360 nm to 830 nm, i.e., approximately 0.36 ⁇ m to 0.83 ⁇ m). If the shortest distance between the light shielding member 6 and the light path of the image light L is shorter than the visible light wavelength, the light closest to the light shielding member 6 in the image light L is diffracted and spreads at the end of the light shielding member 6, which is likely to cause inconveniences such as distortion of the edge of the aerial image R and a decrease in brightness at the end of the aerial image R.
  • the light closest to the light shielding member 6 in the image light L is prevented from diffracting and spreading at the end of the light shielding member 6, which can prevent inconveniences such as distortion of the edge of the aerial image R and a decrease in brightness at the end of the aerial image R.
  • the shortest distance between the light shielding member 6 and the light path of the image light L may be approximately 1 ⁇ m or more, and may be more than twice the maximum wavelength of the visible light wavelength (approximately 0.83 ⁇ m).
  • the upper limit of the shortest distance between the light blocking member 6 and the optical path of the image light L may be about 10 mm, about 3 mm, or about 1 mm.
  • the aerial image display device 1 can suppress a decrease in the brightness of the aerial image R because the reflective optical system 8 does not include an optical element (e.g., a beam splitter, a polarizing filter, etc.) that transmits a portion of the image light L.
  • the aerial image display device 1 can reduce the brightness of the image displayed on the display surface 2a while maintaining sufficient brightness of the aerial image R, thereby making it possible to reduce the power consumption of the aerial image display device 1.
  • the aerial image display device 1 includes a control device 9.
  • the control device 9 is connected to each component of the aerial image display device 1 and controls each component.
  • the components controlled by the control device 9 include the display device 2.
  • the control device 9 may have functions such as turning the display device 2 on and off, transmitting an image signal to the display device 2, and adjusting the brightness, chromaticity, frame frequency, etc. of the image.
  • the control device 9 may have a function of adjusting the temperature of the heat dissipation member or the cooling member.
  • the control device 9 may control the adjustment members of the first concave mirror 3 and the second concave mirror 5.
  • the control device 9 may be configured to include one or more processors.
  • the processors may include general-purpose processors configured to load specific programs and execute specific functions, and dedicated processors specialized for specific processing.
  • the dedicated processors may include ASICs (Application Specific Integrated Circuits).
  • the processors may include PLDs (Programmable Logic Devices).
  • the PLDs may include FPGAs (Field-Programmable Gate Arrays).
  • the control device 9 may be a SoC (System-on-a-Chip) or SiP (System In a Package) in which one or more processors are configured to work together.
  • the aerial image display device 1 may be configured such that the inclination angle ⁇ 2 of the virtual plane P including the display surface 2a relative to the second concave mirror 5 is greater than the inclination angle ⁇ 1 of the virtual plane P relative to the first concave mirror 3.
  • the inclination angle ⁇ 2 refers to the angle between the virtual plane P and the tangent plane T2 of the second concave mirror 5.
  • the tangent plane T2 refers to a plane that is tangent to the reflecting surface 5a of the second concave mirror 5 at the vertex O2 of the reflecting surface 5a (also called the origin of the free-form surface).
  • the inclination angle ⁇ 1 refers to the angle between the virtual plane P and the tangent plane T1 of the first concave mirror 3.
  • the tangent plane T1 refers to a plane that is tangent to the reflecting surface 3a of the first concave mirror 3 at the vertex O1 of the reflecting surface 3a.
  • ⁇ 1 may be approximately 30° to 60°
  • ⁇ 2 may be approximately 70° to 110°, but are not limited to these ranges.
  • the aerial image display device 1 may be configured such that the curvature Sa1 of the reflecting surface 3a of the first concave mirror 3 is greater than the curvature Sa2, where Sa1 is the curvature of the reflecting surface 5a of the second concave mirror 5. Since the curvature Sa1 is relatively large, the first concave mirror 3, which reflects the image light L emitted from the display device 2 in a direction different from the direction toward the display device 2, can be arranged close to the display device 2. As a result, the space occupied by the display device 2 and the reflection optical system 8 can be reduced, and the aerial image display device 1 can be made smaller.
  • the aerial image display device 1 can be made smaller, the optical path length of the image light L between the display surface 2a of the display device 2 and the reflecting surface 5a of the second concave mirror 5 can be shortened, and the loss of the image light L due to undesired scattering, interference, etc. can be suppressed. As a result, the display quality of the aerial image display device 1 can be improved.
  • the curvature Sa1 of the first concave mirror 3 is defined by D MAX /H, where 2 ⁇ H is the length of a line segment LS that passes over the center of the reflecting surface 3a and connects both ends in a cross section along the optical axis of the image light L incident on the first concave mirror 3, and D MAX is the maximum value of the length (also called the maximum depth) between a point on the reflecting surface 3a and the line segment LS in the direction along the optical axis OA. If D MAX /H varies depending on how the cross section is taken, the maximum value of D MAX /H when the position of the cross section is changed may be defined as the curvature Sa1.
  • the curvature Sa2 is defined in the same way as the curvature Sa1 .
  • the second concave mirror 5 When the second concave mirror 5 is viewed from its rear side along a direction parallel to the virtual imaging plane of the aerial image R (the up-down direction in FIG. 1), the second concave mirror 5 may overlap the display device 2 and the first concave mirror 3. In this case, the space occupied by the display device 2 and the reflective optical system 8 can be reduced and made smaller, allowing the aerial image display device 1 to be made more compact. As a result, the optical path length of the image light L inside the aerial image display device 1 can be shortened, suppressing loss of the image light L due to undesired scattering, interference, etc. This in turn allows the display quality of the aerial image display device 1 to be improved.
  • FIG. 3 is a diagram showing the configuration of an aerial image display device according to another embodiment of the present disclosure.
  • the aerial image display device 1A of this embodiment differs from the aerial image display device 1 of the above embodiment in the configuration of the reflective optical system, but otherwise has a similar configuration, so a description of the similar configuration will be omitted.
  • the aerial image display device 1A of this embodiment includes a display device 2, a first concave mirror 3, a convex mirror 4, a second concave mirror 5, and a light blocking member 6.
  • the first concave mirror 3, the convex mirror 4, and the second concave mirror 5 constitute a reflective optical system that focuses the image light L emitted from the display device 2 as an aerial image R.
  • the first concave mirror 3, the convex mirror 4, and the second concave mirror 5 may be collectively referred to as the reflective optical system 8A.
  • the first concave mirror 3 is located on the optical path of the image light L emitted from the display device 2.
  • the first concave mirror 3 is configured to reflect the image light L emitted from the display device 2 in a direction different from the direction toward the display device 2.
  • the first concave mirror 3 may be provided with an adjustment member that adjusts the relative spatial arrangement with respect to the display device 2 (distance from the display surface 2a, inclination angle with respect to the display surface 2a, etc.).
  • the adjustment member may have, for example, a support member such as a rod installed on the back side of the first concave mirror 3, an axis member installed on the support member for rotating the support member and the first concave mirror 3, a slide mechanism for translating the support member and the first concave mirror 3, etc.
  • the adjustment member may be adjusted manually or electrically by a stepping motor or the like.
  • the convex mirror 4 is located on the optical path of the image light L reflected by the first concave mirror 3.
  • the convex mirror 4 is located between the display device 2 and the second concave mirror 5.
  • the convex mirror 4 is configured to reflect the image light L reflected by the first concave mirror 3 in a direction different from the direction toward the first concave mirror 3.
  • the convex mirror 4 may be provided with an adjustment member that adjusts the relative spatial arrangement with respect to the first concave mirror 3 (distance from the first concave mirror 3, inclination angle with respect to the first concave mirror 3, etc.). This adjustment member may be configured similarly to the adjustment member provided on the first concave mirror 3.
  • the second concave mirror 5 is located on the optical path of the image light L reflected by the convex mirror 4.
  • the second concave mirror 5 is configured to reflect the image light L reflected by the convex mirror 4 in a direction different from the direction toward the convex mirror 4, forming a real aerial image R.
  • the second concave mirror 5 may be provided with an adjustment member that adjusts its spatial arrangement relative to the convex mirror 4 (distance from the convex mirror 4, inclination angle relative to the convex mirror 4, etc.). This adjustment member may be configured similarly to the adjustment member installed on the first concave mirror 3.
  • the first concave mirror 3, convex mirror 4, and second concave mirror 5 each have a reflecting surface 3a, a reflecting surface 4a, and a reflecting surface 5a.
  • the first concave mirror 3, convex mirror 4, and second concave mirror 5 may be free-form mirrors whose reflecting surfaces 3a, 4a, and 5a have shapes expressed by the above-mentioned formulas (1) and (2). In this case, by appropriately designing the shapes of the reflecting surfaces 3a, 4a, and 5a, it is possible to reduce distortion of the aerial image R.
  • the light blocking member 6 is located between the display device 2 and the second concave mirror 5.
  • the light blocking member 6 is not located in the optical path of the image light L that travels from the display surface 2a through the first concave mirror 3, the convex mirror 4, and the second concave mirror 5 to the aerial image R, i.e., in the optical path of the light that forms the aerial image R. Therefore, since the light blocking member 6 is not located in a position that inhibits the formation of the aerial image R, the light blocking member 6 itself does not deteriorate the visibility of the aerial image R.
  • the light blocking member 6 can block the image light L' that travels directly from the display surface 2a to the second concave mirror 5.
  • the light blocking member 6 of the aerial image display device 1A may have a configuration similar to that of the light blocking member 6 of the aerial image display device 1.
  • the light blocking member 6 can block the image light L' that travels directly from the display surface 2a to the second concave mirror 5. Therefore, the aerial image display device 1A can prevent the image light L emitted from the display surface 2a from reaching the second concave mirror 5 without passing through the first concave mirror 3 and the convex mirror 4, and from being undesirably reflected by the second concave mirror 5. As a result, it is possible to prevent the occurrence of ghost images that are visible to the eyes of the user 10, or the perception of virtual images by the eyes of the user 10, and reduce the decrease in visibility of the aerial image R.
  • the convex mirror 4 can block at least a portion of the image light L'. Therefore, the aerial image display device 1A can more effectively prevent a portion of the image light L emitted from the display surface 2a from reaching the second concave mirror 5 without passing through the first concave mirror 3 and the convex mirror 4 and being reflected by the second concave mirror 5 in an undesired direction and location. As a result, the decrease in visibility of the aerial image R can be more effectively reduced.
  • ⁇ 1 may be approximately 10° to 35°
  • ⁇ 2 may be approximately 30° to 70°, but are not limited to these ranges.
  • the aerial image display device 1A can suppress a decrease in the brightness of the aerial image R because the reflective optical system 8A does not include an optical element (e.g., a beam splitter, a polarizing filter, etc.) that transmits a portion of the image light L.
  • the aerial image display device 1A can reduce the brightness of the image displayed on the display surface 2a while maintaining sufficient brightness of the aerial image R, thereby making it possible to reduce the power consumption of the aerial image display device 1A.
  • the aerial image display device 1A may be configured such that the tilt angle ⁇ 2 of the virtual plane P including the display surface 2a relative to the second concave mirror 5 is greater than the tilt angle ⁇ 1 of the virtual plane P relative to the first concave mirror 3.
  • the tilt angles ⁇ 1 and ⁇ 2 are defined in the same manner as described above.
  • most of the image light L emitted from the display surface 2a heads toward the first concave mirror 3, making it easier for the image light L to enter the first concave mirror 3 and less likely to directly enter the second concave mirror 5.
  • ghost images and virtual images are less likely to occur, and the decrease in visibility of the aerial image R can be effectively reduced.
  • the aerial image display device 1A has a reflective optical system 8A that includes three mirrors, which increases the degree of freedom in the relative spatial arrangement of the display device 2 and the second concave mirror 5.
  • the inclination angle ⁇ 2 of the virtual plane P with respect to the second concave mirror 5 can be set to 90 degrees or an angle close to 90 degrees, which prevents a portion of the image light L emitted from the display surface 2a from propagating directly toward the second concave mirror 5.
  • the aerial image display device 1A may be configured such that, when the curvature of the reflecting surface 3a of the first concave mirror 3 is Sa1, the curvature of the convex mirror 4 is Sb, and the curvature of the reflecting surface 5a of the second concave mirror 5 is Sa2, the curvature Sa1 is greater than the curvature Sa2, and the curvature Sa2 is greater than the curvature Sb.
  • the curvatures Sa1, Sb, and Sa2 are defined in the same manner as described above.
  • the first concave mirror 3 which reflects the image light L emitted from the display device 2 in a direction different from the direction toward the display device 2, can be positioned close to the display device 2.
  • the space occupied by the display device 2 and the reflective optical system 8A can be reduced, and the aerial image display device 1A can be made smaller.
  • the optical path length of the image light L between the display surface 2a of the display device 2 and the reflecting surface 5a of the second concave mirror 5 can be shortened, thereby suppressing loss of the image light L due to undesired scattering, interference, etc.
  • the display quality of the aerial image display device 1A can be improved.
  • the convex mirror 4 tends to increase the spread of the image light L and tends to increase the distortion of the aerial image R.
  • the curvature Sa2 is smaller than the curvature Sa1 and the curvature Sa2, so that the increase in distortion caused in the aerial image R by the convex mirror 4 can be suppressed.
  • the display quality of the aerial image R is improved.
  • the curvature Sb of the convex mirror 4 is relatively small, so that the spread of the image light L reflected by the convex mirror 4 can be suppressed.
  • the second concave mirror 5 that reflects the image light L reflected by the convex mirror 4 can be suppressed from becoming large.
  • the second concave mirror 5 When the second concave mirror 5 is viewed from its rear side along a direction parallel to the virtual imaging plane of the aerial image R (the up-down direction in FIG. 3), the second concave mirror 5 may overlap the display device 2, the first concave mirror 3, and the convex mirror 4. In this case, the space occupied by the display device 2 and the reflective optical system 8A can be reduced and made smaller, allowing the aerial image display device 1A to be made more compact. As a result, the optical path length of the image light L inside the aerial image display device 1A can be shortened, suppressing loss of the image light L due to undesired scattering, interference, etc. This in turn allows the display quality of the aerial image display device 1A to be improved.
  • the light blocking member 6 may be configured to be capable of electrically adjusting the light transmittance.
  • the light blocking member 6 may be a liquid crystal shutter or EPD using the polymer liquid crystal described above.
  • the light shielding member 6 may be configured such that the shortest distance between the light path of the image light L is longer than the visible light wavelength (approximately 360 nm to 830 nm, i.e., approximately 0.36 ⁇ m to 0.83 ⁇ m). If the shortest distance between the light shielding member 6 and the light path of the image light L is shorter than the visible light wavelength, the light closest to the light shielding member 6 in the image light L is diffracted and spreads at the end of the light shielding member 6, which is likely to cause inconveniences such as distortion of the edge of the aerial image R and reduction in brightness at the end of the aerial image R.
  • the light closest to the light shielding member 6 in the image light L is prevented from diffracting and spreading at the end of the light shielding member 6, which can prevent inconveniences such as distortion of the edge of the aerial image R and reduction in brightness at the end of the aerial image R.
  • the shortest distance between the light shielding member 6 and the light path of the image light L may be approximately 1 ⁇ m or more, and may be more than twice the maximum wavelength of the visible light wavelength (approximately 0.83 ⁇ m).
  • the upper limit of the shortest distance between the light blocking member 6 and the optical path of the image light L may be about 10 mm, about 3 mm, or about 1 mm.
  • FIG. 4 is a cross-sectional view showing the essential configuration of an aerial image display device according to yet another embodiment of the present disclosure.
  • the aerial image display device 1B of this embodiment includes a light collecting member compared to the aerial image display device 1 of the above embodiment, and is otherwise configured in a similar manner, so a description of the similar configuration will be omitted.
  • the aerial image display device 1B includes a display device 2, a first concave mirror 3, a second concave mirror 5, and a light collecting member 7.
  • the first concave mirror 3 and the second concave mirror 5 are configured similarly to the first concave mirror 3 and the second concave mirror 5 of the aerial image display device 1, respectively.
  • the light-collecting member 7 is located between the display device 2 and the first concave mirror 3.
  • the light-collecting member 7 may be located outside the display device 2 close to the display surface 2a, or may be provided inside the display device 2.
  • the light-collecting member 7 nearly parallelizes the image light L emitted from the display surface 2a, and propagates the image light L toward the first concave mirror 3.
  • the light collecting member 7 may be, for example, a plano-convex lens, a biconvex lens, a Fresnel lens, etc.
  • the light collecting member 7 can be made thinner, and as a result, the aerial image display device 1B can be made smaller.
  • the display device 2 is a liquid crystal display device including a backlight and a liquid crystal panel
  • the light collecting member 7 may be located between the backlight and the liquid crystal panel.
  • An anti-reflection coating may be formed on the surface of the light collecting member 7 facing the display surface 2a (i.e., the incident surface of the image light L).
  • a Fresnel lens is a lens that has been made thinner by dividing a normal convex lens into concentric regions, and has a saw-like cross-sectional shape. The greater the number of concentric regions, i.e., the number of divisions, the thinner the lens can be.
  • the light collecting member 7 can suppress a portion of the image light L emitted from the display surface 2a from propagating directly toward the second concave mirror 5. Therefore, the aerial image display device 1 can suppress the image light L emitted from the display surface 2a from reaching the second concave mirror 5 without passing through the first concave mirror 3 and being reflected by the second concave mirror 5 in an undesired direction and location. As a result, it is possible to suppress the occurrence of ghost images and their recognition by the eyes of the user 10, or the recognition of virtual images by the eyes of the user 10, and to reduce the deterioration of the visibility of the aerial image R.
  • the aerial image display device 1B can increase the degree of freedom of spatial arrangement of the display device 2 with respect to the reflection optical system 8 composed of the first concave mirror 3 and the second concave mirror 5. As a result, the aerial image display device 1B can be made smaller.
  • the focusing member 7 may be configured to be movable in the direction of the optical axis of the image light L. In this case, the parallelism of the image light L by the focusing member 7 can be adjusted.
  • the moving device for the focusing member 7 may include a stepping motor, a linear motor, an ultrasonic motor, a rail, a slider, etc.
  • the moving device for the focusing member 7 may include an adjustment member such as a knob or a screw, and the focusing member 7 may be moved by manually adjusting the adjustment member.
  • the aerial image display device 1B may be configured such that the inclination angle ⁇ 2 of the virtual plane P including the display surface 2a relative to the second concave mirror 5 is greater than the inclination angle ⁇ 1 of the virtual plane P relative to the first concave mirror 3.
  • the inclination angles ⁇ 1 and ⁇ 2 are defined in the same manner as described above.
  • the inclination angle ⁇ 2 is greater than the inclination angle ⁇ 1, most of the image light L emitted from the display surface 2a is directed toward the first concave mirror 3, making it easier for the image light L to enter the first concave mirror 3 and less likely to directly enter the second concave mirror 5.
  • ⁇ 1 may be approximately 25° to 55°
  • ⁇ 2 may be approximately 70° to 110°, but are not limited to these ranges.
  • the aerial image display device 1B may be provided with a light-shielding member 6. In this case, it is possible to further prevent a portion of the image light L emitted from the display surface 2a from propagating directly toward the second concave mirror 5. This can therefore further prevent a ghost image from being generated and being seen by the user 10's eyes, or a virtual image from being seen by the user 10's eyes, thereby further reducing the decrease in visibility of the aerial image R.
  • the aerial image display device 1B may be configured such that the curvature Sa1 of the reflecting surface 3a of the first concave mirror 3 is greater than the curvature Sa2, where Sa1 is the curvature of the reflecting surface 5a of the second concave mirror 5.
  • the curvatures Sa1 and Sa2 are defined in the same manner as described above. Since the curvature Sa1 is relatively large, the first concave mirror 3, which reflects the image light L emitted from the display device 2 in a direction different from the direction toward the display device 2, can be arranged close to the display device 2. As a result, the space occupied by the display device 2 and the reflection optical system 8 (the first concave mirror 3 and the second concave mirror 5) can be reduced, and the aerial image display device 1B can be made smaller.
  • the aerial image display device 1B can be made smaller, the optical path length of the image light L between the display surface 2a of the display device 2 and the reflecting surface 5a of the second concave mirror 5 can be shortened, and the loss of the image light L due to undesired scattering, interference, etc. can be suppressed. As a result, the display quality of the aerial image display device 1B can be improved.
  • the second concave mirror 5 When the second concave mirror 5 is viewed from its rear side along a direction parallel to the virtual imaging plane of the aerial image R (the up-down direction in FIG. 4), the second concave mirror 5 may overlap the display device 2 and the first concave mirror 3. In this case, the space occupied by the display device 2 and the reflective optical system 8 can be reduced and made smaller, allowing the aerial image display device 1B to be made more compact. As a result, the optical path length of the image light L inside the aerial image display device 1B can be shortened, suppressing loss of the image light L due to undesired scattering, interference, etc. This in turn allows for improved display quality of the aerial image display device 1B.
  • the aerial image display devices 1, 1A, 1B make it possible to operate an aerial image touchlessly, eliminating the need to touch buttons or the like, and as a result can be used in a variety of product fields, including, but not limited to, the following: communication devices for conversation and communication with aerial images, medical interview devices for doctors to interview patients through aerial images, navigation devices and operation control devices for vehicles such as automobiles, order placement and reception devices and cash registers for stores, operation panels for buildings, elevators, etc., learning devices for teaching or taking classes with aerial images, office equipment for business communication and instructions with aerial images, game machines for playing games with aerial images, projection devices for projecting images onto the ground or walls at amusement parks, game centers, etc., simulator devices for conducting simulation experiments with aerial images at universities, medical institutions, etc., large displays for displaying prices at markets, stock exchanges, etc., and video viewing devices for viewing aerial images.
  • This disclosure can be implemented in the following configurations (1) to (13).
  • a display device having a display surface; a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a second concave mirror that reflects the image light reflected by the first concave mirror in a direction different from the direction toward the first concave mirror, and forms a real aerial image;
  • An aerial image display device including: a shading member located between the display device and the second concave mirror, and not located in the optical path of the image light that runs from the display surface, via the first concave mirror and the second concave mirror, to the aerial image.
  • a display device having a display surface; a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a convex mirror that reflects the image light reflected by the first concave mirror in a direction different from a direction toward the first concave mirror; a second concave mirror that reflects the image light reflected by the convex mirror in a direction different from the direction toward the convex mirror, and forms a real aerial image; a light blocking member that is located between the display device and the second concave mirror and is not located in an optical path of the image light that travels from the display surface through the first concave mirror, the convex mirror, and the second concave mirror to the aerial image, An aerial image display device, wherein the convex mirror is positioned between the light blocking member and the second concave mirror.
  • An aerial image display device according to any one of (5) to (7) above, in which the shortest distance between the light blocking member and the optical path of the image light is longer than the wavelength of visible light.
  • a display device having a display surface; a first concave mirror that reflects the image light emitted from the display surface in a direction different from a direction toward the display device; a second concave mirror that reflects the image light reflected by the first concave mirror in a direction different from the direction toward the first concave mirror, and forms a real aerial image; and a focusing member positioned between the display device and the first concave mirror, the focusing member collimating the image light emitted from the display surface.
  • the display device is a liquid crystal display device including a backlight and a liquid crystal panel,
  • the aerial image display device disclosed herein is equipped with a light-shielding member or a light-collecting member, and therefore can prevent ghost images and virtual images from being generated by a portion of the image light being directed in an undesired direction or location. As a result, the decrease in visibility of the aerial image can be reduced.
  • the aerial image display device 1, 1A may include a light collecting member 7. In this case, the decrease in visibility of the aerial image R can be more effectively reduced.

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PCT/JP2023/033452 2022-09-29 2023-09-13 空中像表示装置 Ceased WO2024070714A1 (ja)

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CN202380067640.1A CN119856101A (zh) 2022-09-29 2023-09-13 空中像显示装置
EP23871947.0A EP4597207A1 (en) 2022-09-29 2023-09-13 Aerial image display apparatus
US19/114,165 US20260036828A1 (en) 2022-09-29 2023-09-13 Aerial image display device

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Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5311357A (en) * 1992-01-28 1994-05-10 Image Technology Associates Device for the creation of three-dimensional images
JPH07191274A (ja) * 1993-12-27 1995-07-28 Canon Inc 画像表示装置
JP2002511596A (ja) * 1998-04-15 2002-04-16 オロ − ゴーン、エルエルシー 光学的画像投影装置
JP2002282478A (ja) * 2001-03-22 2002-10-02 Samii Kk 立体画像表示遊技機
JP2003015508A (ja) * 2001-07-04 2003-01-17 Nippon Hoso Kyokai <Nhk> 干渉縞作成装置および立体表示装置
JP2004117780A (ja) * 2002-09-26 2004-04-15 Samii Kk 少なくとも一つは非球面形状であるオン軸反射器を使用する実像投射システムにおける映像画質向上のための装置及び方法
JP2013222025A (ja) * 2012-04-16 2013-10-28 Dainippon Screen Mfg Co Ltd 三次元画像表示装置
JP2015194601A (ja) * 2014-03-31 2015-11-05 ソニー株式会社 空間映像表示装置
WO2018043673A1 (ja) 2016-08-31 2018-03-08 国立大学法人宇都宮大学 表示装置及び空中像の表示方法
JP2019012251A (ja) * 2017-06-29 2019-01-24 ピクシーダストテクノロジーズ株式会社 光学イメージング装置
JP2019139129A (ja) * 2018-02-14 2019-08-22 矢崎総業株式会社 投影表示装置
JP2020046679A (ja) * 2019-12-04 2020-03-26 マクセル株式会社 ヘッドアップディスプレイ装置
CN112835199A (zh) * 2021-03-17 2021-05-25 浙江水晶光电科技股份有限公司 一种无介质投影系统
JP2021117295A (ja) * 2020-01-23 2021-08-10 三星電子株式会社Samsung Electronics Co., Ltd. 立体像表示装置、立体像表示方法及び立体像生成表示システム

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5311357A (en) * 1992-01-28 1994-05-10 Image Technology Associates Device for the creation of three-dimensional images
JPH07191274A (ja) * 1993-12-27 1995-07-28 Canon Inc 画像表示装置
JP2002511596A (ja) * 1998-04-15 2002-04-16 オロ − ゴーン、エルエルシー 光学的画像投影装置
JP2002282478A (ja) * 2001-03-22 2002-10-02 Samii Kk 立体画像表示遊技機
JP2003015508A (ja) * 2001-07-04 2003-01-17 Nippon Hoso Kyokai <Nhk> 干渉縞作成装置および立体表示装置
JP2004117780A (ja) * 2002-09-26 2004-04-15 Samii Kk 少なくとも一つは非球面形状であるオン軸反射器を使用する実像投射システムにおける映像画質向上のための装置及び方法
JP2013222025A (ja) * 2012-04-16 2013-10-28 Dainippon Screen Mfg Co Ltd 三次元画像表示装置
JP2015194601A (ja) * 2014-03-31 2015-11-05 ソニー株式会社 空間映像表示装置
WO2018043673A1 (ja) 2016-08-31 2018-03-08 国立大学法人宇都宮大学 表示装置及び空中像の表示方法
JP2019012251A (ja) * 2017-06-29 2019-01-24 ピクシーダストテクノロジーズ株式会社 光学イメージング装置
JP2019139129A (ja) * 2018-02-14 2019-08-22 矢崎総業株式会社 投影表示装置
JP2020046679A (ja) * 2019-12-04 2020-03-26 マクセル株式会社 ヘッドアップディスプレイ装置
JP2021117295A (ja) * 2020-01-23 2021-08-10 三星電子株式会社Samsung Electronics Co., Ltd. 立体像表示装置、立体像表示方法及び立体像生成表示システム
CN112835199A (zh) * 2021-03-17 2021-05-25 浙江水晶光电科技股份有限公司 一种无介质投影系统

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