WO1994018596A1 - Head mounted display utilizing diffractive optical elements - Google Patents
Head mounted display utilizing diffractive optical elements Download PDFInfo
- Publication number
- WO1994018596A1 WO1994018596A1 PCT/US1994/001115 US9401115W WO9418596A1 WO 1994018596 A1 WO1994018596 A1 WO 1994018596A1 US 9401115 W US9401115 W US 9401115W WO 9418596 A1 WO9418596 A1 WO 9418596A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- image
- combiner
- diffractive optical
- tilt
- optical means
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/017—Head mounted
- G02B27/0172—Head mounted characterised by optical features
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
- G02B27/0103—Head-up displays characterised by optical features comprising holographic elements
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
- G02B27/0103—Head-up displays characterised by optical features comprising holographic elements
- G02B2027/0105—Holograms with particular structures
- G02B2027/0107—Holograms with particular structures with optical power
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
- G02B2027/011—Head-up displays characterised by optical features comprising device for correcting geometrical aberrations, distortion
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
- G02B2027/0112—Head-up displays characterised by optical features comprising device for genereting colour display
- G02B2027/0116—Head-up displays characterised by optical features comprising device for genereting colour display comprising devices for correcting chromatic aberration
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0149—Head-up displays characterised by mechanical features
- G02B2027/0161—Head-up displays characterised by mechanical features characterised by the relative positioning of the constitutive elements
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/017—Head mounted
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/08—Mirrors
- G02B5/10—Mirrors with curved faces
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/18—Diffraction gratings
Definitions
- This invention relates to a display which has a special utility in connection with a head mounted apparatus and more particularly to an attachment for a helmet worn by an aircraft pilot (helmet mounted display) wherein an image of a desired display, such as information on the face of a cathode ray tube, can be introduced into the field of view being observed by the pilot.
- the present invention is an improvement which utilizes one or more diffractive optical surfaces to provide a system which operates with fewer elements and thus simpler, lighter and easier to align and assemble than prior art systems.
- This system utilizes a rather complex optical arrangement, usable in a rather restricted space, for directing light from a source, such as a cathode ray tube, to a spherical reflector from which the light is then reflected through a tuned optical filter and, as collimated rays, is directed to the eye of the pilot so that he sees the image at infinity combined with his normal field of view through the optical filter and spherical combiner.
- a source such as a cathode ray tube
- the present invention overcomes the problems with the prior art head mounted display by utilizing one or more diffractive surfaces in the optical system.
- These diffractive surfaces are shaped by known techniques to correct not only for chromatic and aspheric aberration, but also to produce the necessary tilt and decenter functions for aberration correction and distortion mapping correction, and thus may be substituted for several optical elements of the Rotier apparatus and thus reduce the number of optical elements and eliminate off-center lenses therein.
- the diffractive surfaces are preferably formed on existing surfaces of the system so as to further prevent an increase the number of components.
- the hybrid system of the present invention contains only simple spherical lenses that are fewer in number and with a spherical combiner, involve no off-axis components and yet which provides all the same corrections as in the prior art.
- the number of lenses can be reduced from eight, some of which are non-spherical and/or non-centered, as seen in the above mentioned Rotier Patent, to seven centered spherical lenses, thus making alignment and assembly of the system much easier. Further reductions in number of components is obtainable by using a non-spherical (e.g. elliptical) combiner which suffers no astigmatism from the combiner and only four lenses are then needed but, although none of the lenses are aspheric, two of the lenses are now decentered.
- a non-spherical e.g. elliptical
- diffractive surfaces are known in the prior art.
- "Head Up Displays” have employed diffractive elements, usually in combination with the combiner therein so as to act as an optical filter and/or focusing and collimating means.
- Diffractive surfaces have also been used in telescopes to correct for chromatic and spherical aberrations but neither head up displays nor telescope systems require the very close tolerances and small available space encountered in head mounted systems and the design concepts cannot normally be interchanged.
- FIG. 1 shows a system utilized in the prior art
- Fig. 2 shows the present invention utilizing a spherical combiner
- Fig. 3 shows the apparatus of the present invention utilizing an elliptical combiner.
- the helmet mounted display of Fig. 1 is like that shown in the above-referred to Rotier Patent 4,859,030.
- an image from a cathode ray tube surface 12 passes through an optical relay system 14 to a spherical combiner surface 16.
- light rays from the optical relay system 14 is reflected from a tuned filter 18, which may be like that of the Rotier patent, and then to the combiner 16 for reflection back through the filter 18 and are focused on the eye of a pilot 20.
- the light rays are shown as three principal rays 21, 22 and 23 passing through the system.
- the rays 21, 22 and 23 emerge from the filter 18 as collimated wavefronts to produce an image of the CRT surface 12 at infinity so as to superimpose this image with the image of the surrounding scene being viewed by the pilot 20 through the combiner 16 and the filter 18.
- the combiner 16 is tilted so that the optical axis of the eye and combiner are not collinear which allows the rays 21, 22 and 23 coming from the relay optics 14 to reflect off of filter 18 at different angles of incidence than the rays from combiner 16 and allow greater amounts of light for both the CRT image and the scene image by tuning the filter 18 as described in the Rotier patent. As explained, however, this produces tilt errors, decentering and distortion mapping which must be corrected.
- the optical relay system 14 consists often optical elements, eight of which are lenses and that several of these lenses are non-spherical and/or off- centered.
- Each of the lenses and combinations of lenses performs a function such as correcting for chromatic operation, correcting for aspheric aberration, producing the required tilt and decentering corrections, and for correcting distortion mapping. It is also seen that the number of elements produces a rather complex system which, it has been found, is difficult to assemble and align, and adds greatly to the weight and cost of the helmet mounted display.
- Fig. 2 shows the present invention utilizing a simplified optical relay system 24 in combination with the spherical combiner 16 and the filter 18 to focus an image from the surface 12 of the CRT on the eye of the pilot 20 as was the case in Fig. 1.
- Fig. 2 only three principal light rays 26, 28, and 30 are shown. Since the combiner 16 is spherical, it must be tilted and the rays 26, 28 and 30 passing from the cathode ray tube 12 to the eye of pilot 20 must be corrected for chromatic aberrations, spherical aberration, decentering, distortion mapping and tilt correction.
- diffraction surfaces shown as dashed lines 40 and 42 are introduced on two surfaces which for example may be the planer surfaces of two of the presently existing lenses.
- Diffraction surfaces 40 and 42 may be made by Binary Optic Microlithography, by diamond turning or any other suitable method and are shaped to counter balance the effects of the aberrations and errors.
- the image formed is, like that of Figure 1, at infinity so that the pilot observes the image along with the image of the scene he sees through the filter 18 and spherical combiner 16. It is seen that the optical system of Fig. 2 has reduced the number of optical elements involved to nine, only seven of which are lenses and all of which are spherical and coaxial.
- Fig. 3 shows a yet simpler system utilizing an elliptical combiner 46, which is somewhat more difficult to fabricate than a spherical combiner.
- the optical system 54 transmits an image from the surface of cathode ray tube 12 along paths such as shown by reference numerals 55, 56 and 57 through three spherical lenses, one prism and one reflecting surface to the filter 18 and then to the elliptical combiner 46 for reflection back through the filter 18 to the eye of pilot 20.
- reference numerals 55, 56 and 57 three spherical lenses, one prism and one reflecting surface to the filter 18 and then to the elliptical combiner 46 for reflection back through the filter 18 to the eye of pilot 20.
- two diffractive surfaces shown as dashed lines 58 and 59 are again used with each being formed on one surface of already existing lens within optical system 54.
- the diffractive surfaces 58 and 59 are again formed to correct for the aberrations and for the tilt, decentering and mapping distortions as was the case in Figure 2.
- three principle light rays 55, 56 and 57 are shown passing from the cathode ray tube surface 12 through the optical system 54 to be reflected from the filter 18 to the elliptical combiner 46 and then back through the filter 18 to be focused on the eye of the pilot 20 as an image at infinity so as to be combined with the view seen by the pilot through the filter 18 and combiner 46.
- the on-axis field point suffers no astigmatism from the combiner. Because the elliptical combiner can have the eye of the pilot 20 at one of the ellipse's foci, the astigmatism caused by tilting the combiner is substantially eliminated thus reducing the number of optical components even without the diffraction surfaces. With the diffraction surfaces 58 and 59. the system is simplified further to one having only three lenses all of which are spherical and centered. Thus the system of Figure 3 although involving a more difficult combiner to fabricate, yields a great weight reduction and, in addition, provides a better performance, a larger exit pupil, and is a very simple centered optical train compared to the conventional design of the prior art.
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6518141A JPH08506429A (en) | 1993-02-01 | 1994-02-01 | Head mounted display device using diffractive optical element |
CA002153503A CA2153503C (en) | 1993-02-01 | 1994-02-01 | Head mounted display utilizing diffractive optical elements |
EP94907384A EP0681710B1 (en) | 1993-02-01 | 1994-02-01 | Head mounted display utilizing diffractive optical elements |
DE69411711T DE69411711T2 (en) | 1993-02-01 | 1994-02-01 | DISPLAY SYSTEM ON THE HEAD WITH DIFFERENTIAL OPTICAL ELEMENTS |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/011,582 US5537253A (en) | 1993-02-01 | 1993-02-01 | Head mounted display utilizing diffractive optical elements |
US08/011,582 | 1993-02-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1994018596A1 true WO1994018596A1 (en) | 1994-08-18 |
Family
ID=21751050
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1994/001115 WO1994018596A1 (en) | 1993-02-01 | 1994-02-01 | Head mounted display utilizing diffractive optical elements |
Country Status (6)
Country | Link |
---|---|
US (1) | US5537253A (en) |
EP (1) | EP0681710B1 (en) |
JP (1) | JPH08506429A (en) |
CA (1) | CA2153503C (en) |
DE (1) | DE69411711T2 (en) |
WO (1) | WO1994018596A1 (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5483307A (en) * | 1994-09-29 | 1996-01-09 | Texas Instruments, Inc. | Wide field of view head-mounted display |
EP0710865A1 (en) * | 1994-10-31 | 1996-05-08 | Kaiser Electro-Optics, Inc. | Optical collimating device |
WO1996036898A2 (en) * | 1995-05-15 | 1996-11-21 | He Holdings, Inc., Doing Business As Hughes Electronics | Low-cost light-weight head-mounted virtual-image projection display with low moments of inertia and low center of gravity |
FR2784201A1 (en) * | 1998-10-06 | 2000-04-07 | Sextant Avionique | OPTICAL DEVICE FOR A HELMET SIGHT COMPRISING A DIFFRACTIVE MIRROR |
WO2000028369A2 (en) * | 1998-11-12 | 2000-05-18 | Digilens, Inc. | Head mounted apparatus for viewing an image |
US6211976B1 (en) | 1998-09-14 | 2001-04-03 | Digilens, Inc. | Holographic projection system |
EP1792225A2 (en) * | 2004-09-01 | 2007-06-06 | Optical Research Associates | Compact head mounted display devices with tilted/decentered lens element |
US9581818B2 (en) | 2012-08-08 | 2017-02-28 | Nikon Corporation | Head-mounted display optical system and head-mounted display |
Families Citing this family (48)
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---|---|---|---|---|
US5539578A (en) * | 1993-03-02 | 1996-07-23 | Olympus Optical Co., Ltd. | Image display apparatus |
GB9304944D0 (en) * | 1993-03-11 | 1993-04-28 | Pilkington Perkin Elmer Ltd | Head-up displays |
NL9401109A (en) * | 1994-07-01 | 1996-02-01 | Optische Ind Oede Oude Delftoe | Display system intended for mounting on the head or on a helmet and a helmet provided with such a display system. |
US5909325A (en) * | 1995-06-26 | 1999-06-01 | Olympus Optical Co., Ltd. | Image display apparatus |
GB2304483B (en) * | 1995-08-18 | 2000-03-29 | London Electricity Plc | System for and method of determining the location of an object in a medium |
US6204974B1 (en) | 1996-10-08 | 2001-03-20 | The Microoptical Corporation | Compact image display system for eyeglasses or other head-borne frames |
US5886822A (en) * | 1996-10-08 | 1999-03-23 | The Microoptical Corporation | Image combining system for eyeglasses and face masks |
US6023372A (en) * | 1997-10-30 | 2000-02-08 | The Microoptical Corporation | Light weight, compact remountable electronic display device for eyeglasses or other head-borne eyewear frames |
US5838490A (en) * | 1996-11-04 | 1998-11-17 | Honeywell Inc. | Head mounted display system using mangin mirror combiner |
US5907416A (en) * | 1997-01-27 | 1999-05-25 | Raytheon Company | Wide FOV simulator heads-up display with selective holographic reflector combined |
US5889625A (en) * | 1997-05-21 | 1999-03-30 | Raytheon Company | Chromatic aberration correction for display systems |
EP1027627B1 (en) * | 1997-10-30 | 2009-02-11 | MYVU Corporation | Eyeglass interface system |
US6008946A (en) * | 1997-11-07 | 1999-12-28 | Honeywell, Inc. | Ambient light display illumination for a head-mounted display |
US20040108971A1 (en) * | 1998-04-09 | 2004-06-10 | Digilens, Inc. | Method of and apparatus for viewing an image |
US6147807A (en) * | 1999-05-04 | 2000-11-14 | Honeywell, Inc. | High brightness see-through head-mounted display |
DE60006535T2 (en) | 1999-06-21 | 2004-09-23 | The Microoptical Corp., Westwood | DISPLAY DEVICE WITH OKULAR, DISPLAY AND LIGHTING DEVICE ON OPTOMECHANICAL CARRIER |
US7158096B1 (en) | 1999-06-21 | 2007-01-02 | The Microoptical Corporation | Compact, head-mountable display device with suspended eyepiece assembly |
US6353503B1 (en) | 1999-06-21 | 2002-03-05 | The Micropitical Corporation | Eyeglass display lens system employing off-axis optical design |
US6724354B1 (en) | 1999-06-21 | 2004-04-20 | The Microoptical Corporation | Illumination systems for eyeglass and facemask display systems |
JP2001027738A (en) | 1999-07-14 | 2001-01-30 | Minolta Co Ltd | Video display device |
US6636356B2 (en) | 2000-08-02 | 2003-10-21 | Olympus Optical Co., Ltd. | Observation optical system |
EP1433160A1 (en) * | 2001-09-07 | 2004-06-30 | The Microoptical Corporation | Light weight, compact, remountable face-supported electronic display |
US7313246B2 (en) * | 2001-10-06 | 2007-12-25 | Stryker Corporation | Information system using eyewear for communication |
JP2003172899A (en) * | 2001-12-05 | 2003-06-20 | Fujitsu Ltd | Display device |
DE10316533A1 (en) * | 2003-04-10 | 2004-11-04 | Carl Zeiss | Head-mounted display, has two sub-lens units including diffractive lens units for compensating for their dispersion errors |
DE10316534B4 (en) * | 2003-04-10 | 2007-06-28 | Carl Zeiss | Hybrid optical HMD device with color aberration correction |
WO2004106982A2 (en) * | 2003-05-22 | 2004-12-09 | Optical Research Associates | Optical combiner designs and head mounted displays |
US7206133B2 (en) * | 2003-05-22 | 2007-04-17 | Optical Research Associates | Light distribution apparatus and methods for illuminating optical systems |
WO2004106983A2 (en) * | 2003-05-22 | 2004-12-09 | Optical Research Associates | Illumination in optical systems |
JP4218553B2 (en) * | 2004-03-08 | 2009-02-04 | ソニー株式会社 | Image display device |
US7450310B2 (en) * | 2005-05-03 | 2008-11-11 | Optical Research Associates | Head mounted display devices |
US9057826B2 (en) | 2013-01-31 | 2015-06-16 | Google Inc. | See-through near-to-eye display with eye prescription |
US9632312B1 (en) | 2013-04-30 | 2017-04-25 | Google Inc. | Optical combiner with curved diffractive optical element |
US9442291B1 (en) | 2013-06-28 | 2016-09-13 | Google Inc. | Segmented diffractive optical elements for a head wearable display |
US9459455B2 (en) | 2013-12-19 | 2016-10-04 | Google Inc. | See-through eyepiece for head wearable display |
US9389422B1 (en) | 2013-12-23 | 2016-07-12 | Google Inc. | Eyepiece for head wearable display using partial and total internal reflections |
US9395544B2 (en) | 2014-03-13 | 2016-07-19 | Google Inc. | Eyepiece with switchable reflector for head wearable display |
US9915823B1 (en) | 2014-05-06 | 2018-03-13 | Google Llc | Lightguide optical combiner for head wearable display |
US9366869B2 (en) | 2014-11-10 | 2016-06-14 | Google Inc. | Thin curved eyepiece for see-through head wearable display |
US10162180B2 (en) | 2015-06-04 | 2018-12-25 | Google Llc | Efficient thin curved eyepiece for see-through head wearable display |
US10146054B2 (en) | 2015-07-06 | 2018-12-04 | Google Llc | Adding prescriptive correction to eyepieces for see-through head wearable displays |
US10429646B2 (en) | 2015-10-28 | 2019-10-01 | Google Llc | Free space optical combiner with prescription integration |
WO2017116952A1 (en) | 2015-12-29 | 2017-07-06 | Dolby Laboratories Licensing Corporation | Viewport independent image coding and rendering |
WO2017127494A1 (en) | 2016-01-22 | 2017-07-27 | Corning Incorporated | Wide field personal display |
US10976551B2 (en) | 2017-08-30 | 2021-04-13 | Corning Incorporated | Wide field personal display device |
JP7205166B2 (en) * | 2018-11-01 | 2023-01-17 | セイコーエプソン株式会社 | Display device |
KR102603552B1 (en) * | 2019-01-31 | 2023-11-17 | 크리얼 에스에이 | Light-field mixed reality system provides viewers with accurate monocular depth cues |
CN114063300B (en) | 2020-07-30 | 2023-12-22 | 精工爱普生株式会社 | virtual image display device |
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GB2186384A (en) * | 1981-08-25 | 1987-08-12 | Secr Defence | Head-up display collimating element |
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EP0526067A2 (en) * | 1991-07-25 | 1993-02-03 | Pilkington P.E. Limited | Improvements in or relating to displays |
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-
1993
- 1993-02-01 US US08/011,582 patent/US5537253A/en not_active Expired - Lifetime
-
1994
- 1994-02-01 DE DE69411711T patent/DE69411711T2/en not_active Expired - Lifetime
- 1994-02-01 JP JP6518141A patent/JPH08506429A/en active Pending
- 1994-02-01 EP EP94907384A patent/EP0681710B1/en not_active Expired - Lifetime
- 1994-02-01 WO PCT/US1994/001115 patent/WO1994018596A1/en active IP Right Grant
- 1994-02-01 CA CA002153503A patent/CA2153503C/en not_active Expired - Fee Related
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Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0704739A3 (en) * | 1994-09-29 | 1996-11-20 | Texas Instruments Inc | Image display systems |
US5483307A (en) * | 1994-09-29 | 1996-01-09 | Texas Instruments, Inc. | Wide field of view head-mounted display |
EP0710865A1 (en) * | 1994-10-31 | 1996-05-08 | Kaiser Electro-Optics, Inc. | Optical collimating device |
WO1996036898A2 (en) * | 1995-05-15 | 1996-11-21 | He Holdings, Inc., Doing Business As Hughes Electronics | Low-cost light-weight head-mounted virtual-image projection display with low moments of inertia and low center of gravity |
WO1996036898A3 (en) * | 1995-05-15 | 1997-02-06 | Hughes Aircraft Co | Low-cost light-weight head-mounted virtual-image projection display with low moments of inertia and low center of gravity |
US5822127A (en) * | 1995-05-15 | 1998-10-13 | Hughes Electronics | Low-cost light-weight head-mounted virtual-image projection display with low moments of inertia and low center of gravity |
US6211976B1 (en) | 1998-09-14 | 2001-04-03 | Digilens, Inc. | Holographic projection system |
FR2784201A1 (en) * | 1998-10-06 | 2000-04-07 | Sextant Avionique | OPTICAL DEVICE FOR A HELMET SIGHT COMPRISING A DIFFRACTIVE MIRROR |
WO2000020913A1 (en) * | 1998-10-06 | 2000-04-13 | Thomson-Csf Sextant | Optical device for helmet visor comprising a diffractive mirror |
US6788442B1 (en) | 1998-10-06 | 2004-09-07 | Thomson-Csf Sexant | Optical device for helmet visor comprising a diffractive mirror |
WO2000028369A2 (en) * | 1998-11-12 | 2000-05-18 | Digilens, Inc. | Head mounted apparatus for viewing an image |
WO2000028369A3 (en) * | 1998-11-12 | 2000-08-10 | Digilens Inc | Head mounted apparatus for viewing an image |
EP1792225A2 (en) * | 2004-09-01 | 2007-06-06 | Optical Research Associates | Compact head mounted display devices with tilted/decentered lens element |
EP1792225A4 (en) * | 2004-09-01 | 2010-07-28 | Optical Res Associates | Compact head mounted display devices with tilted/decentered lens element |
US9581818B2 (en) | 2012-08-08 | 2017-02-28 | Nikon Corporation | Head-mounted display optical system and head-mounted display |
Also Published As
Publication number | Publication date |
---|---|
CA2153503A1 (en) | 1994-08-18 |
EP0681710A1 (en) | 1995-11-15 |
DE69411711D1 (en) | 1998-08-20 |
US5537253A (en) | 1996-07-16 |
DE69411711T2 (en) | 1999-01-21 |
EP0681710B1 (en) | 1998-07-15 |
JPH08506429A (en) | 1996-07-09 |
CA2153503C (en) | 2003-09-23 |
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