Patent Application
20180374266
The present disclosure relates to virtual reality, augmented reality, and mixed reality imaging and visualization systems.
Modern computing and display technologies have facilitated the development of “mixed reality” (MR) systems for so called “virtual reality” (VR) or “augmented reality” (AR) experiences, wherein digitally reproduced images or portions thereof are presented to a user in a manner wherein they seem to be, or may be perceived as, real. A VR scenario typically involves presentation of digital or virtual image information without transparency to actual real-world visual input. An AR scenario typically involves presentation of digital or virtual image information as an augmentation to visualization of the real world around the user (i.e., transparency to real-world visual input). Accordingly, AR scenarios involve presentation of digital or virtual image information with transparency to the real-world visual input.
MR systems typically generate and display color data, which increases the realism of MR scenarios. Many of these MR systems display color data by sequentially projecting sub-images in different (e.g., primary) colors or “fields” (e.g., Red, Green, and Blue) corresponding to a color image in rapid succession. Projecting color sub-images at sufficiently high rates (e.g., 60 Hz, 120 Hz, etc.) may deliver a smooth color MR scenarios in a user's mind.
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Some head-worn VR/AR/MR systems employ a display screen in the field of view of the end user and an image projection assembly that projects images onto the display screen. As one example, the image projection assembly may take the form of an optical fiber scan-based image projection assembly, and the display screen may take the form of a optical waveguide-based display into which scanned and collimated light beams from the image projection assembly are injected via an in-coupling (IC) element, which the exit the surface of the optical waveguide-based display towards the user's eyes, thereby producing, e.g., images at single optical viewing distance closer than infinity (e.g., arm's length), images at multiple, discrete optical viewing distances or focal planes, and/or image layers stacked at multiple viewing distances or focal planes to represent volumetric 3D objects.
In a head-worn VR/AR/MR system, it is important that the entrance pupil of the user's eye (i.e., the image of the anatomical pupil as seen through the cornea) be aligned with and be of a similar size to the exit pupil of the display screen (i.e., the width of the cone of light that is available to the eye of the user) in order to properly couple the instrument to the eye (in the case of a monocular arrangement) or eyes (in the case of a binocular arrangement) of the user, given a fixed eye relief (i.e., the distance from the last surface of the display screen and the user's eye or eyes). An exit pupil of the display screen that is smaller than the entrance pupil of the user' eye will often result in a vignette or clipped image, whereas an exit pupil of the display screen that is larger than the entrance pupil of the user's eye wastes some light, but allows for movement of the eye without vignetting or clipping of the image.
In order to increase the wearability and comfort of a head-worn VR/AR/MR system, it is desirable to miniaturize the image source, and in some cases, the image projection assembly, as much as possible. Such an image projection assembly will, without intervention, result in an exit pupil that is much smaller than the entrance pupil of some eyes, assuming a reasonable eye relief between the eye and the display screen. As such, optics are incorporated into the display subsystem to effectively expand the exit pupil of the display screen to match the entrance pupil of the user's eye. That is, the exit pupil of the display screen should create an “eye box” that is slightly larger (e.g., 10 mm) than the entrance pupil of the user's eye (e.g., 5-7 mm) to allow movement of the eye within that eye box to maintain a full view of the image presented by the display screen.
Besides matching the exit pupil of the display screen with the entrance pupil of the user's eye(s), it is desirable to maximize the angular resolution, minimize the depth of field, and maximize the density of the wavefront density of the display screen in a VR/AR/MR system. Maximizing the angular resolution results in a clearer and more vivid virtual image, maximizing the wavefront density alleviates image artifacts (such as the “screen door” effect (grid-like pattern and non-uniformity), and minimizing the depth of the field allows the user to more easily accommodate to virtual content on which the user is currently focused. That is, the smaller the depth of field, the easier it is for an eye to accommodate to the virtual content, providing for a more natural visual real-world experience, whereas the greater the depth of field, the more difficult it is for the eye to accommodate to the virtual content, resulting in a less natural, and perhaps a nauseating, visual experience.
There, thus, remains a need to provide a display screen of a VR/AR/MR system that is capable of producing a highly-saturated light beamlet array exit pupil that matches the entrance pupil of the user's eye(s), without diminishing the wearability of the VR/AR/MR system.
The visualization center of the brain gains valuable perception information from the motion of both eyes and components thereof relative to each other. Vergence movements (i.e., rolling movements of the pupils toward or away from each other to converge the lines of sight of the eyes to fixate upon an object) of the two eyes relative to each other are closely associated with focusing (or “accommodation”) of the lenses of the eyes. Under normal conditions, changing the focus of the lenses of the eyes, or accommodating the eyes, to focus upon an object at a different distance will automatically cause a matching change in vergence to the same distance, under a relationship known as the “accommodation-vergence reflex.” Likewise, a change in vergence will trigger a matching change in accommodation, under normal conditions. Working against this reflex, as do most conventional stereoscopic VR/AR/MR configurations, is known to produce eye fatigue, headaches, or other forms of discomfort in users.
Stereoscopic wearable glasses generally feature two displays for the left and right eyes that are configured to display images with slightly different element presentation such that a three-dimensional perspective is perceived by the human visual system. Such configurations have been found to be uncomfortable for many users due to a mismatch between vergence and accommodation (“vergence-accommodation conflict”) which must be overcome to perceive the images in three dimensions. Indeed, some VR/AR/MR users are not able to tolerate stereoscopic configurations. Accordingly, most conventional VR/AR/MR systems are not optimally suited for presenting a rich, binocular, three-dimensional experience/scenario in a manner that will be comfortable and maximally useful to the user, in part because prior systems fail to address some of the fundamental aspects of the human perception system, including the vergence-accommodation conflict.
One possible approach to address these problems (including the vergence-accommodation conflict) is to project images at multiple depth planes. To implement this type of system, one approach is to use a plurality of light guiding optical elements to direct light at the eyes of a user such that the light appears to originate from multiple depth planes. The light guiding optical elements are designed to in-couple virtual light corresponding to digital or virtual objects and propagate it by total internal reflection (“TIR”), then to out-couple the virtual light to display the digital or virtual objects to the user's eyes. In AR/MR systems, the light guiding optical elements are also designed to be transparent to light from (e.g., reflecting off of) actual real-world objects. Therefore, portions of the light guiding optical elements are designed to reflect virtual light for propagation via TIR while being transparent to real-world light from real-world objects.
Various optical systems generate images at various depths for displaying VR/AR/MR scenarios. Some such optical systems are described in U.S. Utility patent application Ser. No. 14/555,585, the contents of which have been previously incorporated by reference. Some VR/AR/MR systems employ wearable display devices (e.g., head-worn displays, helmet-mounted displays, or smart glasses) that are at least loosely coupled to a user's head, and thus move when the user's head moves.
Some three-dimensional (“3-D”) optical systems, such as those in VR/AR/MR systems, optically render virtual objects. Objects are “virtual” in that they are not real physical objects located in respective positions in 3-D space. Instead, virtual objects only exist in the brains (e.g., the optical centers) of viewers and/or listeners when stimulated by light beams directed to the eyes of audience members.
VR/AR/MR systems must also be capable of displaying virtual digital content at various perceived positions and distances relative to the user. The design of VR/AR/MR systems presents numerous other challenges, including the speed of the system in delivering virtual digital content, quality of virtual digital content, eye relief of the user (addressing the vergence-accommodation conflict), size and portability of the system, and other system and optical challenges.
Further, VR/AR/MR systems must be capable of displaying virtual digital content in sharp focus to generate photo-realistic imagery required for a believable, immersive, enjoyable VR/AR/MR experience/scenario. The lens of an eye must change shape (i.e., accommodate) to bring images or portions thereof into better focus.
Size restrictions of head-worn displays also result in image resolution limitations. Head-worn VR/AR/MR display systems, such as those described in U.S. Utility patent application Ser. No. 14/555,585, the contents of which have been previously incorporated by reference, display images to users with light beams transmitted by TIR through light guiding optical elements which conserve light beam angles. Light beam diameters remain essentially the same through light guiding optical elements. Size limitations of head-worn displays limited the size of various optical components (e.g., light sources, light guiding optical elements, lenses, etc.), which limits the diameters of light beams generated by the head-worn displays. These light beam diameter limitations result in resolution and FOV limitations described above.
The systems and methods described herein are configured to address these challenges.
In accordance with a first aspect of the present disclosure, a virtual image generation system comprises a planar optical waveguide (which may be a single unitary substrate) having opposing first and second faces, and an in-coupling (IC) element configured for optically coupling a collimated light beam from an image projection assembly into the planar optical waveguide as an in-coupled light beam. The image projection assembly may comprise a scanning device configured for scanning the collimated light beam.
The virtual image generation system further comprises a first orthogonal pupil expansion (OPE) element associated with the first face of the planar optical waveguide for splitting the in-coupled light beam into a first set of orthogonal light beamlets, and a second orthogonal pupil expansion (OPE) element associated with the second face of the planar optical waveguide for splitting the in-coupled light beam into a second set of orthogonal light beamlets. In some embodiments, the first OPE element is disposed on the first face of the planar optical waveguide, and the second OPE element is disposed on the second face of the planar optical waveguide. The IC element may be configured for optically coupling the collimated light beam from the image projection assembly as the in-coupled light beam for propagation within the planar optical waveguide via total internal reflection (TIR) along a first optical path that alternately intersects the first OPE element and the second OPE element, such that portions of the in-coupled light beam are deflected as the respective first set of orthogonal light beamlets and the second set of orthogonal light beamlets that propagate within the planar optical waveguide via TIR along second parallel optical paths. In this case, the second parallel optical paths may be orthogonal to the first optical path.
The virtual image generation system further comprises an exit pupil expansion (EPE) element associated with the planar optical waveguide for splitting the first and second sets of orthogonal light beamlets into an array of out-coupled light beamlets (e.g., a two-dimensional out-coupled light beamlet array) that exit the planar optical waveguide. The collimated light beam may define an entrance pupil, and the out-coupled light beamlet array may define an exit pupil larger than the entrance pupil, e.g., at least ten times larger than the entrance pupil, or even at least one hundred times larger than the entrance pupil.
In some embodiments, the EPE element is disposed on one of the first and second surfaces of the planar optical waveguide. The first set of orthogonal light beamlets and the second set of orthogonal light beamlets may intersect the EPE element, such that portions of the first set of orthogonal light beamlets and the second set of orthogonal light beamlets are deflected as the out-coupled light beamlet array out of the planar optical waveguide. In some embodiments, the EPE element is configured for imparting a convex wavefront profile on the out-coupled light beamlet array exiting the planar optical waveguide. In this case, the convex wavefront profile may have a center of radius at a focal point to produce an image at a given focal plane. In another embodiment, each of the IC element, OPE element, and EPE element is diffractive.
In accordance with a second aspect of the present disclosure, a virtual image generation system comprises a planar optical waveguide comprising a plurality of substrates including a primary substrate having a first thickness, at least two secondary substrates having second thicknesses, and at least two semi-reflective interfaces respectively disposed between the substrates.
In some embodiments, each of the second thicknesses is less than the first thickness. For example, the first thickness may be at least twice each of the second thicknesses. In another embodiment, the second thicknesses are substantially equal to each other. In an alternative embodiment, two or more of the secondary substrate(s) have second thicknesses that are not equal to each other. In this case, at least two of the unequal second thicknesses may be non-multiples of each other. In still another embodiment, the first thickness is a non-multiple of at least one of the second thicknesses, and may be a non-multiple of each of the second thicknesses. In yet another embodiment, at least two of the plurality of secondary substrates have second thicknesses that are not substantially equal to each other.
In yet another embodiment, each of the semi-reflective interfaces comprises a semi-reflective coating, which may be, e.g., respectively disposed between the substrates via one of physical vapor deposition (PVD), ion-assisted deposition (IAD), and ion beam sputtering (IBS). Each of the coatings may, e.g., be composed of one or more of a metal (Au, Al, Ag, Ni—Cr, Cr and so on), dielectric (Oxides, Fluorides and Sulfides), and semiconductors (Si, Ge). In yet another embodiment, adjacent ones of the substrates are composed of materials having different indices of refraction.
The virtual image generation system further comprises an in-coupling (IC) element configured for optically coupling a collimated light beam from an image projection assembly for propagation as an in-coupled light beam within the planar optical waveguide. The image projection assembly may comprise a scanning device configured for scanning the collimated light beam. The semi-reflective interfaces are configured for splitting the in-coupled light beam into a plurality of primary light beamlets that propagate within the primary substrate.
The virtual image generation system further comprises one or more diffractive optical elements (DOEs) associated with the planar optical waveguide for further splitting the plurality of primary light beamlets into an array of out-coupled light beamlets (e.g., a two-dimensional out-coupled beamlet array) that exit a face of the planar optical waveguide. The collimated light beam may define an entrance pupil, and the out-coupled light beamlet array may define an exit pupil larger than the entrance pupil, e.g., at least ten times larger than the entrance pupil, or even at least one hundred times larger than the entrance pupil. In some embodiments, the first thickness of the primary substrate and the second thicknesses of the secondary substrates are selected, such that spacings between centers of at least two adjacent ones of the out-coupled light beamlets are equal to or less than a width of the collimated light beam. In another embodiment, the first thickness and the second thicknesses are selected, such that no gap resides between edges of greater than half of adjacent ones of the out-coupled light beamlets.
In some embodiments, the semi-reflective interfaces are configured for splitting the in-coupled light beam into at least two in-coupled light beamlets. In this case, the DOE(s) comprises an orthogonal pupil expansion (OPE) element configured for respectively splitting the at least two in-coupled light beamlets into at least two sets of orthogonal light beamlets, the semi-reflective interfaces are further configured for splitting the at least two sets of orthogonal light beamlets into at least four sets of orthogonal light beamlets, and the DOE(s) comprises an exit pupil expansion (EPE) element configured for splitting the at least four sets of orthogonal light beamlets into the set of out-coupled light beamlets. The OPE element and EPE element may be disposed on a face of the optical planar waveguide.
The at least two in-coupled light beamlets may propagate within the planar optical waveguide via total internal reflection (TIR) along a first optical path that intersects the OPE element, such that portions of the at least two in-coupled light beamlets are diffracted as the at least two sets of orthogonal light beamlets that propagate within the planar optical waveguide via TIR along second parallel optical paths. The second parallel optical paths may be orthogonal to the first optical path. The at least two sets of orthogonal light beamlets may intersect the EPE element, such that portions of the at least two sets of orthogonal light beamlets are diffracted as the out-coupled set of light beamlets out of the face of the planar optical waveguide. In some embodiments, the EPE element may be configured for imparting a convex wavefront profile on the out-coupled light beamlet array exiting the planar optical waveguide. In this case, the convex wavefront profile may have a center of radius at a focal point to produce an image at a given focal plane.
In accordance with a third aspect of the present disclosure, a virtual image generation system comprises a planar optical waveguide comprising a plurality of substrates including a primary substrate having a first thickness, at least one secondary substrate respectively having at least one second thicknesses, and at least one semi-reflective interface respectively disposed between the substrates.
The first thickness is at least twice each of the at least one second thickness. In some embodiments, the first thickness is a non-multiple of each of the second thickness(es). In another embodiment, the secondary substrate(s) comprises a plurality of secondary substrates. In this case, the second thicknesses may be equal to each other or two or more of the secondary substrate(s) may have second thicknesses that are not equal to each other. The first thickness may be a non-multiple of at least one of the second thicknesses. At least two of the unequal second thicknesses may be non-multiples of each other.
In some embodiments, each of the semi-reflective interface(s) comprises a semi-reflective coating, which may be, e.g., respectively disposed between the substrates via one of physical vapor deposition (PVD), ion-assisted deposition (IAD), and ion beam sputtering (IBS). Each of the coatings may, e.g., be composed of one or more of a metal (Au, Al, Ag, Ni—Cr, Cr and so on), dielectric (Oxides, Fluorides and Sulfides), and semiconductors (Si, Ge). In yet another embodiment, adjacent ones of the substrates are composed of materials having different indices of refraction.
The virtual image generation system further comprises an in-coupling (IC) element configured for optically coupling a collimated light beam from an image projection assembly for propagation as an in-coupled light beam within the planar optical waveguide. The image projection assembly may comprise a scanning device configured for scanning the collimated light beam. The semi-reflective interface(s) are configured for splitting the in-coupled light beam into a plurality of primary light beamlets that propagate within the primary substrate.
The virtual image generation system further comprises one or more diffractive optical elements (DOEs) associated with the planar optical waveguide for further splitting the plurality of primary light beamlets into an array of out-coupled light beamlets (e.g., a two-dimensional out-coupled beamlet array) that exit a face of the planar optical waveguide. The collimated light beam may define an entrance pupil, and the out-coupled light beamlet array may define an exit pupil larger than the entrance pupil, e.g., at least ten times larger than the entrance pupil, or even at least one hundred times larger than the entrance pupil. In some embodiments, the first thickness of the primary substrate and the second thickness(es) of the secondary substrate(s) are selected, such that spacings between centers of at least two adjacent ones of the out-coupled light beamlets are equal to or less than a width of the collimated light beam. In another embodiment, the first thickness and the second thickness(es) are selected, such that no gap resides between edges of greater than half of adjacent ones of the out-coupled light beamlets.
In some embodiments, the semi-reflective interface(s) are configured for splitting the in-coupled light beam into at least two in-coupled light beamlets. In this case, the DOE(s) comprises an orthogonal pupil expansion (OPE) element configured for respectively splitting the at least two in-coupled light beamlets into at least two sets of orthogonal light beamlets, the semi-reflective interface(s) are further configured for splitting the at least two sets of orthogonal light beamlets into at least four sets of orthogonal light beamlets, and the DOE(s) comprises an exit pupil expansion (EPE) element configured for splitting the at least four sets of orthogonal light beamlets into the set of out-coupled light beamlets. The OPE element and EPE element may be disposed on a face of the optical planar waveguide.
The at least two in-coupled light beamlets may propagate within the planar optical waveguide via total internal reflection (TIR) along a first optical path that intersects the OPE element, such that portions of the at least two in-coupled light beamlets are diffracted as the at least two sets of orthogonal light beamlets that propagate within the planar optical waveguide via TIR along second parallel optical paths. The second parallel optical paths may be orthogonal to the first optical path. The at least two sets of orthogonal light beamlets may intersect the EPE element, such that portions of the at least two sets of orthogonal light beamlets are diffracted as the out-coupled set of light beamlets out of the face of the planar optical waveguide. In some embodiments, the EPE element may be configured for imparting a convex wavefront profile on the out-coupled light beamlet array exiting the planar optical waveguide. In this case, the convex wavefront profile may have a center of radius at a focal point to produce an image at a given focal plane.
In accordance with a fourth aspect of the present disclosure, a virtual image generation system comprises a pre-pupil expansion (PPE) element configured for receiving a collimated light beam from an imaging element and splitting the collimated light beam into a set of initial out-coupled light beamlets. The virtual image generations system further comprises a planar optical waveguide, an in-coupling (IC) element configured for optically coupling the set of initial out-coupled light beamlets into the planar optical waveguide as a set of in-coupled light beamlets, and one or more diffractive elements associated with the planar optical waveguide for splitting the set of in-coupled light beamlets into a set of final out-coupled light beamlets that exit a face of the planar optical waveguide. The diffractive element(s) may comprises an orthogonal pupil expansion (OPE) element associated with the planar optical waveguide for further splitting the set of in-coupled light beamlets into a set of orthogonal light beamlets, and an exit pupil expansion (EPE) element associated with the planar optical waveguide for splitting the set of orthogonal light beamlets into the set of final out-coupled light beamlets.
In some embodiments, the collimated light beam defines an entrance pupil, the set of initial out-coupled light beamlets define a pre-expanded pupil larger than the entrance pupil, and the set of final out-coupled light beamlets define an exit pupil larger than the pre-expanded pupil. In one example, the pre-expanded pupil is at least ten times larger than the entrance pupil, and the exit pupil is at least ten times larger than the pre-expanded pupil. In some embodiments, the set of initial out-coupled light beamlets is optically coupled into the planar optical waveguide as a two-dimensional light beamlet array, and the set of final out-coupled light beamlets exits the face of the planar optical waveguide as a two-dimensional light beamlet array. In another embodiment, the set of initial out-coupled light beamlets is optically coupled into the planar optical waveguide as a one-dimensional light beamlet array, and the set of final out-coupled set of light beamlets exits the face of the planar optical waveguide as a two-dimensional light beamlet array.
In some embodiments, the PPE element comprises a mini-planar optical waveguide, a mini-OPE element associated with the mini-planar optical waveguide for splitting the collimated light beam into a set of initial orthogonal light beamlets, and a mini-EPE element associated with the mini-planar optical waveguide for splitting the set of initial orthogonal light beamlets into the set of initial out-coupled light beamlets that exit a face of the mini-planar optical waveguide. The PPE may further comprise a mini-IC element configured for optically coupling the collimated light beam into the planar optical waveguide.
In another embodiment, the PPE element comprises a diffractive beam splitter (e.g., a 1×N beam splitter or a M×N beam splitter) configured for splitting the collimated light beam into an initial set of diverging light beamlets, and a lens (e.g., a diffractive lens) configured for re-collimating the initial set of diverging light beamlets into the set of initial out-coupled light beamlets.
In still another embodiment, the PPE element comprises a prism (e.g., a solid prism or a cavity prism) configured for splitting the collimated light beam into the set of in-coupled light beamlets. The prism may comprise a semi-reflective prism plane configured for splitting the collimated light beam into the set of in-coupled light beamlets. The prism may comprise a plurality of parallel prism planes configured for splitting the collimated light beam into the set of in-coupled light beamlets. In this case, the parallel prism planes may comprise the semi-reflective prism plane. The plurality of parallel prism planes may comprise a completely reflective prism plane, in which case, a portion of the collimated light beam may be reflected by the at least one semi-reflective prism in a first direction, and a portion of the collimated light beam may be transmitted to the completely reflective prism plane for reflection in the first direction. The prism may comprise a first set of parallel prism planes configured for splitting the collimated light beam into a set of initial orthogonal light beamlets that are reflected in a first direction, and a second set of parallel prism planes configured for splitting the initial orthogonal light beamlets into the set of in-coupled light beamlets that are reflected in a second direction different from the first direction. The first and second directional may be orthogonal to each other.
In yet another embodiment, the PPE element comprises a first planar optical waveguide assembly configured for splitting the collimated light beam into a two-dimensional array of out-coupled light beamlets (e.g., an N×N light beamlet array) that exits a face of the first planar optical waveguide assembly, and a second planar optical waveguide assembly configured for splitting the two-dimensional out-coupled light beamlet array into multiple two-dimensional arrays of out-out-coupled light beamlets that exit a face of the second planar optical waveguide assembly as the set of in-coupled light beamlets. The first and second planar optical waveguide assemblies may respectively have unequal thicknesses.
The two-dimensional out-coupled light beamlet array has an inter-beamlet spacing, and the multiple two-dimensional out-coupled light beamlet arrays are spatially offset from each other by an inter-array spacing different from the inter-beamlet spacing of the two-dimensional out-coupled light beamlet array. In some embodiments, the inter-array spacing of the multiple two-dimensional out-coupled light beamlet arrays and the inter-beamlet spacing of the two-dimensional out-coupled light beamlet array are non-multiples of each other. The inter-array spacing of the multiple two-dimensional out-coupled light beamlet arrays may be greater than the inter-beamlet spacing of the two-dimensional out-coupled light beamlet array.
In some embodiments, the first planar optical waveguide assembly comprises a first planar optical waveguide having opposing first and second faces, a first in-coupling (IC) element configured for optically coupling the collimated light beam for propagation within the first planar optical waveguide via total internal reflection (TIR) along a first optical path, a first exit pupil expander (EPE) element associated with the first planar optical waveguide for splitting the collimated light beam into a one-dimensional light beamlet array that exit the second face of the first planar optical waveguide, a second planar optical waveguide having opposing first and second faces, a second IC element configured for optically coupling the one-dimensional light beamlet array for propagation within the second planar optical waveguide via TIR along respective second optical paths that are perpendicular to the first optical path, and a second exit pupil expander (EPE) element associated with the second planar optical waveguide for splitting the one-dimensional light beamlet array into the two-dimensional light beamlet array that exit the second face of the second planar optical waveguide. In this case, the first face of the second planar optical waveguide may be affixed to the second face of the first planar optical waveguide. The first and second planar optical waveguides may respectively have substantially equal thicknesses.
The second planar optical waveguide assembly may comprise a third planar optical waveguide having opposing first and second faces, a third IC element configured for optically coupling the first two-dimensional light beamlet array for propagation within the third planar optical waveguide via TIR along respective third optical paths, a third EPE element associated with the third planar optical waveguide for splitting the two-dimensional light beamlet array into a plurality of two-dimensional light beamlet arrays that exit the second face of the third planar optical waveguide, a fourth planar optical waveguide having opposing first and second faces, a fourth IC element configured for optically coupling the plurality of two-dimensional light beamlet arrays for propagation within the fourth planar optical waveguide via TIR along respective fourth optical paths that are perpendicular to the third optical paths, and a fourth EPE element associated with the fourth planar optical waveguide for splitting the plurality of two-dimensional light beamlet arrays into the multiple two-dimensional light beamlet arrays that exit the second face of the fourth planar optical waveguide as the input set of light beamlets. In this case, the first face of the fourth planar optical waveguide may be affixed to the second face of the third planar optical waveguide, and first face of the third planar optical waveguide may be affixed to the second face of the second planar optical waveguide. The first and second planar optical waveguides may respectively have substantially equal thicknesses, and the third and fourth planar optical waveguides may respectively have substantially equal thicknesses. In this case, the substantially equal thicknesses of the first and second planar optical waveguides may be different from the substantially equal thicknesses of the third and fourth planar optical waveguides. The equal thicknesses of the third and fourth planar optical waveguides may be greater than the equal thicknesses of the first and second planar optical waveguides.
In some embodiments, a mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an exit portion, a first light guiding optical sub-element, and a second light guiding optical sub-element. The first light guiding optical sub-element has a first thickness, and the second light guiding optical sub-element has a second thickness different from the first thickness.
In one or more embodiments, the light source and the light guiding optical element are configured such that the virtual light beam enters the light guiding optical element through the entry portion, propagates through the light guiding optical element by substantially total internal reflection, and divides into a plurality of virtual light beamlets. At least some of the plurality of virtual light beamlets may exit the light guiding optical element through the exit portion. The light guiding optical element may be transparent to a real-world light beam.
In one or more embodiments, neither a first quotient of the first and second thicknesses nor a second quotient of the second and first thicknesses are integers. The entry portion may include an in-coupling grating on the first light guiding optical sub-element. The exit portion may include an exit pupil expander on the first light guiding optical sub-element. The second light guiding optical sub-element may not overlay the exit pupil expander on the first light guiding optical sub-element.
In one or more embodiments, the second thickness of the second light guiding optical sub-element facilitates substantially total internal reflection of light having a predetermined wavelength. The predetermined wavelength may be from 515 nm to 540 nm. The predetermined wavelength may be 520 nm or 532 nm. The predetermined wavelength may be 475 nm or 650 nm. The second thickness of the second light guiding optical sub-element may facilitate substantially total internal reflection of light beams substantially parallel to an optical axis of the system to a greater degree than light beams oblique to the optical axis.
In one or more embodiments, the second light guiding optical sub-element overlays substantially all of the first light guiding optical sub-element. The second thickness may be substantially equal to a whole number multiple of a wavelength of the virtual light beam. The second thickness may be a whole number multiple of 475 nm, 520 nm, or 650 nm.
In one or more embodiments, each of the first and second light guiding optical sub-elements includes respective substantially flat sheets, such that the light guiding optical element includes a stack of substantially flat sheets. The light guiding optical element may also have a refractive index gap between the first and second light guiding optical sub-elements. The refractive index gap may be an air layer.
In one or more embodiments, the second light guiding optical sub-element includes two reflective surfaces that reflect light in substantially the same direction. The second light guiding optical sub-element may include two reflective surfaces that reflect light in substantially opposite directions. The system may also include a third light guiding optical sub-element.
In another embodiment, a mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an exit portion, a first light guiding optical sub-element, and a second light guiding optical sub-element. The first light guiding optical sub-element has a first diffractive index. The second light guiding optical sub-element has a second diffractive index different from the first diffractive index.
In one or more embodiments, the light source and the light guiding optical element are configured such that the virtual light beam enters the light guiding optical element through the entry portion, propagates through the light guiding optical element by substantially total internal reflection, and divides into a plurality of virtual light beamlets. At least some of the plurality of virtual light beamlets exit the light guiding optical element through the exit portion. The light guiding optical element may be transparent to a real-world light beam.
In one or more embodiments, neither a first quotient of the first and second diffractive indices nor a second quotient of the second and first diffractive indices are integers. The entry portion may include an in-coupling grating on the first light guiding optical sub-element. The exit portion may include an exit pupil expander on the first light guiding optical sub-element. The second light guiding optical sub-element may not overlay the exit pupil expander on the first light guiding optical sub-element.
In one or more embodiments, the second diffractive index of the second light guiding optical sub-element facilitates substantially total internal reflection of light have a predetermined wavelength. The predetermined wavelength may be from 515 nm to 540 nm. The predetermined wavelength may be 520 nm or 532 nm. The predetermined wavelength may be 475 nm or 650 nm.
In one or more embodiments, the second diffractive index of the second light guiding optical sub-element facilitates substantially total internal reflection of light beams substantially parallel to an optical axis of the system to a greater degree than light beams oblique to the optical axis. The second light guiding optical sub-element may overlay substantially all of the first light guiding optical sub-element.
In one or more embodiments, each of the first and second light guiding optical sub-elements includes respective substantially flat sheets, such that the light guiding optical element includes a stack of substantially flat sheets. The light guiding optical element may also have a refractive index gap between the first and second light guiding optical sub-elements. The refractive index gap may be an air layer.
In one or more embodiments, the second light guiding optical sub-element includes two reflective surfaces that reflect light in substantially the same direction. The second light guiding optical sub-element may include two reflective surfaces that reflect light in substantially opposite directions. The system may also include a third light guiding optical sub-element.
In still another embodiment, a mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an orthogonal pupil expander and a plurality of exit pupil expanders. The light source and the light guiding optical element are configured such that the virtual light beam enters the light guiding optical element through the entry portion, propagates through the light guiding optical element by substantially total internal reflection, divides into a plurality of first virtual light beamlets by interacting with the orthogonal pupil expander, the plurality of first virtual light beamlets entering respective ones of the plurality of exit pupil expanders, and divides into a plurality of second virtual light beamlets by interacting with the plurality of exit pupil expanders. At least some of the plurality of second virtual light beamlets exit the light guiding optical element through the exit pupil expander.
In one or more embodiments, the light guiding optical element is transparent to a real-world light beam. Each of the plurality of exit pupil expanders may include a substantially flat sheet, such that the plurality of exit pupil expanders includes a stack of substantially flat sheets.
In one or more embodiments, the orthogonal pupil expander facilitates substantially total internal reflection of light have a predetermined wavelength. The predetermined wavelength may be from 515 nm to 540 nm. The predetermined wavelength may be 520 nm or 532 nm. The predetermined wavelength may be 475 nm or 650 nm.
In one or more embodiments, the system also includes a plurality of light blockers to selectively block light to the plurality of exit pupil expanders. The plurality of light blockers may include LC shutters or PDLC out-coupling gratings. At least one of the plurality of light blockers may be disposed adjacent an edge of the orthogonal pupil expander. At least one of the plurality of light blockers may be disposed adjacent a central portion of the orthogonal pupil expander.
In yet another embodiment, a mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an orthogonal pupil expander and an exit portion. The light source and the light guiding optical element are configured such that the virtual light beam enters the light guiding optical element through the entry portion, propagates through the light guiding optical element by substantially total internal reflection, and divides into a plurality of virtual light beamlets by interacting with the orthogonal pupil expander. At least some of the plurality of virtual light beamlets exit the light guiding optical element through the exit portion.
In one or more embodiments, the orthogonal pupil expander includes a first orthogonal pupil sub-expander and a second orthogonal pupil sub-expander. Each of the first and second orthogonal pupil sub-expanders divides light beams entering the respective first and second orthogonal pupil sub-expanders. Each of the first and second orthogonal pupil sub-expanders may be a respective flat sheet. The first and second orthogonal pupil sub-expanders may be stacked on top of each other.
In one or more embodiments, the first orthogonal pupil sub-expander includes a first exit edge to direct beamlets into the second orthogonal pupil sub-expander. The first exit edge may include a mirror. The first orthogonal pupil sub-expander may include a second exit edge to direct beamlets into the second orthogonal pupil sub-expander. The first and second exit edges may each include a respective mirror.
In one or more embodiments, the orthogonal pupil expander includes first and second reflective edges. The first and second reflective edges may be orthogonal to each other. The orthogonal pupil expander may also include a third reflective edge.
In one or more embodiments, the orthogonal pupil expander includes an in-coupling grating and a region of high diffraction disposed opposite of the in-coupling grating. The orthogonal pupil expander may include a first light modifier configured to absorb light in a first wavelength range. The orthogonal pupil expander may also include a second light modifier configured to absorb light in a second wavelength range. The first and second light modifiers may be orthogonal to each other.
In one or more embodiments, the orthogonal pupil expander also includes a third light modifier configured to absorb light in a third wavelength range. The orthogonal pupil expander may include diffractive optical elements forming a “V” shape. The orthogonal pupil expander may include a plurality of PDLC swatches.
In still another embodiment, a mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an exit portion, a first light guiding optical sub-element, and a second light guiding optical sub-element. The first light guiding optical sub-element has a first light modifying characteristic. The second light guiding optical sub-element has a second light modifying characteristic different from the first light modifying characteristic.
A virtual image generation system comprises a planar optical waveguide comprising a plurality of substrates including a primary substrate having a first thickness and at least two secondary substrates having second thicknesses, and at least two semi-reflective interfaces respectively disposed between the substrates. The first thickness may be at least twice each of the second thicknesses. The system further comprises an in-coupling (IC) element configured for optically coupling a collimated light beam for propagation as an in-coupled light beam within the planar optical waveguide. The semi-reflective interfaces are configured for splitting the in-coupled light beam into a plurality of primary light beamlets that propagate within the primary substrate. The system further comprises one or more diffractive optical elements (DOEs) associated with the planar optical waveguide for further splitting the plurality of primary light beamlets into an array of out-coupled light beamlets that exit a face of the planar optical waveguide.
A virtual image generation system comprises a pre-pupil expansion (PPE) element configured for receiving a collimated light beam from an imaging element and splitting the collimated light beam into a set of initial out-coupled light beamlets, a planar optical waveguide, an in-coupling (IC) element configured for optically coupling the set of initial out-coupled light beamlets into the planar optical waveguide as a set of in-coupled light beamlets, and one or more diffractive elements associated with the planar optical waveguide for splitting the set of in-coupled light beamlets into a set of final out-coupled light beamlets that exit a face of the planar optical waveguide.
A mixed reality system includes a light source configured to generate a virtual light beam. The system also includes a light guiding optical element having an entry portion, an exit portion, a first light guiding optical sub-element, and a second light guiding optical sub-element. The first light guiding optical sub-element has a first thickness, and the second light guiding optical sub-element has a second thickness different from the first thickness.
Additional and other objects, features, and advantages of the disclosure are described in the detail description, figures and claims.
The drawings illustrate the design and utility of preferred embodiments of the present disclosure, in which similar elements are referred to by common reference numerals. In order to better appreciate how the above-recited and other advantages and objects of the present disclosure are obtained, a more particular description of the present disclosure briefly described above will be rendered by reference to specific embodiments thereof, which are illustrated in the accompanying drawings. Understanding that these drawings depict only typical embodiments of the disclosure and are not therefore to be considered limiting of its scope, the disclosure will be described and explained with additional specificity and detail through the use of the accompanying drawings in which:
The description that follows relates to display subsystems and methods to be used in an augmented reality system. However, it is to be understood that while the disclosure lends itself well to applications in augmented reality systems, the disclosure, in its broadest aspects, may not be so limited, and may be applied to any waveguide-based imaging system. For example, the disclosure can be applied to virtual reality systems. Thus, while often described herein in terms of an augmented reality system, the teachings should not be limited to such systems of such uses.
Various embodiments of the disclosure are directed to systems, methods, and articles of manufacture for implementing optical systems in a single embodiment or in multiple embodiments. Other objects, features, and advantages of the disclosure are described in the detailed description, figures, and claims.
Various embodiments will now be described in detail with reference to the drawings, which are provided as illustrative examples of the disclosure so as to enable those skilled in the art to practice the disclosure. Notably, the figures and the examples below are not meant to limit the scope of the present disclosure. Where certain elements of the present disclosure may be partially or fully implemented using known components (or methods or processes), only those portions of such known components (or methods or processes) that are necessary for an understanding of the present disclosure will be described, and the detailed descriptions of other portions of such known components (or methods or processes) will be omitted so as not to obscure the disclosure. Further, various embodiments encompass present and future known equivalents to the components referred to herein by way of illustration.
The optical systems may be implemented independently of AR/MR systems, but many embodiments below are described in relation to AR/MR systems for illustrative purposes only.
Referring to
The virtual image generation system 100, and the various techniques taught herein, may be employed in applications other than augmented reality and virtual reality subsystems. For example, various techniques may be applied to any projection or display subsystem, or may be applied to pico projectors where movement may be made by an end user's hand rather than the head. Thus, while often described herein in terms of an augmented reality subsystem or virtual reality subsystem, the teachings should not be limited to such subsystems of such uses.
At least for augmented reality applications, it may be desirable to spatially position various virtual objects relative to respective physical objects in a field of view of the end user 50. Virtual objects, also referred to herein as virtual tags or tag or call outs, may take any of a large variety of forms, basically any variety of data, information, concept, or logical construct capable of being represented as an image. Non-limiting examples of virtual objects may include: a virtual text object, a virtual numeric object, a virtual alphanumeric object, a virtual tag object, a virtual field object, a virtual chart object, a virtual map object, a virtual instrumentation object, or a virtual visual representation of a physical object.
The virtual image generation system 100 comprises a frame structure 102 worn by an end user 50, a display subsystem 104 carried by the frame structure 102, such that the display subsystem 104 is positioned in front of the eyes 52 of the end user 50, and a speaker 106 carried by the frame structure 102, such that the speaker 106 is positioned adjacent the ear canal of the end user 50 (optionally, another speaker (not shown) is positioned adjacent the other ear canal of the end user 50 to provide for stereo/shapeable sound control). The display subsystem 104 is designed to present the eyes 52 of the end user 50 with photo-based radiation patterns that can be comfortably perceived as augmentations to physical reality, with high-levels of image quality and three-dimensional perception, as well as being capable of presenting two-dimensional content. The display subsystem 104 presents a sequence of frames at high frequency that provides the perception of a single coherent scene.
In the illustrated embodiment, the display subsystem 104 employs “optical see-through” display through which the user can directly view light from real objects via transparent (or semi-transparent) elements. The transparent element, often referred to as a “combiner,” superimposes light from the display over the user's view of the real world. To this end, the display subsystem 104 comprises a projection subsystem 108 and a partially transparent display screen 110 on which the projection subsystem 108 projects images. The display screen 110 is positioned in the end user's 50 field of view between the eyes 52 of the end user 50 and an ambient environment, such that direct light from the ambient environment is transmitted through the display screen 110 to the eyes 52 of the end user 50.
In the illustrated embodiment, the image projection assembly 108 provides a scanned light to the partially transparent display screen 110, thereby combining with the direct light from the ambient environment, and being transmitted from the display screen 110 to the eyes 52 of the user 50. In the illustrated embodiment, the projection subsystem 108 takes the form of an optical fiber scan-based projection device, and the display screen 110 takes the form of a waveguide-based display into which the scanned light from the projection subsystem 108 is injected to produce, e.g., images at a single optical viewing distance closer than infinity (e.g., arm's length), images at multiple, discrete optical viewing distances or focal planes, and/or image layers stacked at multiple viewing distances or focal planes to represent volumetric 3D objects. These layers in the light field may be stacked closely enough together to appear continuous to the human visual subsystem (i.e., one layer is within the cone of confusion of an adjacent layer). Additionally or alternatively, picture elements may be blended across two or more layers to increase perceived continuity of transition between layers in the light field, even if those layers are more sparsely stacked (i.e., one layer is outside the cone of confusion of an adjacent layer). The display subsystem 104 may be monocular or binocular.
The virtual image generation system 100 further comprises one or more sensors (not shown) mounted to the frame structure 102 for detecting the position and movement of the head 54 of the end user 50 and/or the eye position and inter-ocular distance of the end user 50. Such sensor(s) may include image capture devices (such as cameras), microphones, inertial measurement units, accelerometers, compasses, GPS units, radio devices, and/or gyros).
The virtual image generation system 100 further comprises a user orientation detection module 112. The user orientation module 112 detects the instantaneous position of the head 54 of the end user 50 and may predict the position of the head 54 of the end user 50 based on position data received from the sensor(s). Detecting the instantaneous position of the head 54 of the end user 50 facilitates determination of the specific actual object that the end user 50 is looking at, thereby providing an indication of the specific textual message to be generated for that actual object and further providing an indication of the textual region in which the textual message is to be streamed. The user orientation module 112 also tracks the eyes 52 of the end user 50 based on the tracking data received from the sensor(s).
The virtual image generation system 100 further comprises a control subsystem that may take any of a large variety of forms. The control subsystem includes a number of controllers, for instance one or more microcontrollers, microprocessors or central processing units (CPUs), digital signal processors, graphics processing units (GPUs), other integrated circuit controllers, such as application specific integrated circuits (ASICs), programmable gate arrays (PGAs), for instance field PGAs (FPGAs), and/or programmable logic controllers (PLUs).
The control subsystem of virtual image generation system 100 comprises a central processing unit (CPU) 114, a graphics processing unit (GPU) 116, one or more frame buffers 118, and three-dimensional data base 120 for storing three-dimensional scene data. The CPU 114 controls overall operation, while the GPU 116 renders frames (i.e., translating a three-dimensional scene into a two-dimensional image) from the three-dimensional data stored in the three-dimensional data base 120 and stores these frames in the frame buffer(s) 116. While not illustrated, one or more additional integrated circuits may control the reading into and/or reading out of frames from the frame buffer(s) 116 and operation of the image projection assembly 108 of the display subsystem 104.
The various processing components of the virtual image generation system 100 may be physically contained in a distributed subsystem. For example, as illustrated in
130 may be mounted in a variety of configurations, such as fixedly attached to the frame structure 102 (
The local processing and data module 130 may comprise a power-efficient processor or controller, as well as digital memory, such as flash memory, both of which may be utilized to assist in the processing, caching, and storage of data captured from the sensors and/or acquired and/or processed using the remote processing module 132 and/or remote data repository 134, possibly for passage to the display subsystem 104 after such processing or retrieval. The remote processing module 132 may comprise one or more relatively powerful processors or controllers configured to analyze and process data and/or image information. The remote data repository 134 may comprise a relatively large-scale digital data storage facility, which may be available through the internet or other networking configuration in a “cloud” resource configuration. In some embodiments, all data is stored and all computation is performed in the local processing and data module 130, allowing fully autonomous use from any remote modules.
The couplings 136, 138, 140 between the various components described above may include one or more wired interfaces or ports for providing wires or optical communications, or one or more wireless interfaces or ports, such as via RF, microwave, and IR for providing wireless communications. In some implementations, all communications may be wired, while in other implementations all communications may be wireless. In still further implementations, the choice of wired and wireless communications may be different from that illustrated in
In the illustrated embodiment, the user orientation module 112 is contained in the local processing and data module 130, while CPU 114 and GPU 116 are contained in the remote processing module 132, although in alternative embodiments, the CPU 114, GPU 124, or portions thereof may be contained in the local processing and data module 130. The 3D database 120 can be associated with the remote data repository 134.
Before describing the details of embodiments of the light guiding optical elements, this disclosure will now provide a brief description of illustrative MR systems.
One possible approach to implementing an MR system uses a plurality of volume phase holograms, surface-relief holograms, or light guiding optical elements that are embedded with depth plane information to generate images that appear to originate from respective depth planes. In other words, a diffraction pattern, or diffractive optical element (“DOE”) may be embedded within or imprinted/embossed upon a light guiding optical element (“LOE”; e.g., a planar waveguide) such that as collimated light (light beams with substantially planar wavefronts) is substantially totally internally reflected along the LOE, it intersects the diffraction pattern at multiple locations and exits toward the user's eye. The DOEs are configured so that light exiting therethrough from an LOE are verged so that they appear to originate from a particular depth plane. The collimated light may be generated using an optical condensing lens (a “condenser”).
For example, a first LOE may be configured to deliver collimated light to the eye that appears to originate from the optical infinity depth plane (0 diopters). Another LOE may be configured to deliver collimated light that appears to originate from a distance of 2 meters (½ diopter). Yet another LOE may be configured to deliver collimated light that appears to originate from a distance of 1 meter (1 diopter). By using a stacked LOE assembly, it can be appreciated that multiple depth planes may be created, with each LOE configured to display images that appear to originate from a particular depth plane. It should be appreciated that the stack may include any number of LOEs. However, at least N stacked LOEs are required to generate N depth planes. Further, N, 2N or 3N stacked LOEs may be used to generate RGB colored images at N depth planes.
In order to present 3-D virtual content to the user, the mixed reality (MR) system projects images of the virtual content into the user's eye so that they appear to originate from various depth planes in the Z direction (i.e., orthogonally away from the user's eye). In other words, the virtual content may not only change in the X and Y directions (i.e., in a 2D plane orthogonal to a central visual axis of the user's eye), but it may also appear to change in the Z direction such that the user may perceive an object to be very close or at an infinite distance or any distance in between. In other embodiments, the user may perceive multiple objects simultaneously at different depth planes. For example, the user may see a virtual dragon appear from infinity and run towards the user. Alternatively, the user may simultaneously see a virtual bird at a distance of 3 meters away from the user and a virtual coffee cup at arm's length (about 1 meter) from the user.
Multiple-plane focus systems create a perception of variable depth by projecting images on some or all of a plurality of depth planes located at respective fixed distances in the Z direction from the user's eye. Referring now to
Depth plane positions 502 may be measured in diopters, which is a unit of optical power equal to the inverse of the focal length measured in meters. For example, in some embodiments, depth plane 1 may be ⅓ diopters away, depth plane 2 may be 0.3 diopters away, depth plane 3 may be 0.2 diopters away, depth plane 4 may be 0.15 diopters away, depth plane 5 may be 0.1 diopters away, and depth plane 6 may represent infinity (i.e., 0 diopters away). It should be appreciated that other embodiments may generate depth planes 502 at other distances/diopters. Thus, in generating virtual content at strategically placed depth planes 502, the user is able to perceive virtual objects in three dimensions. For example, the user may perceive a first virtual object as being close to him when displayed in depth plane 1, while another virtual object appears at infinity at depth plane 6. Alternatively, the virtual object may first be displayed at depth plane 6, then depth plane 5, and so on until the virtual object appears very close to the user. It should be appreciated that the above examples are significantly simplified for illustrative purposes. In another embodiment, all six depth planes may be concentrated on a particular focal distance away from the user. For example, if the virtual content to be displayed is a coffee cup half a meter away from the user, all six depth planes could be generated at various cross-sections of the coffee cup, giving the user a highly granulated 3-D view of the coffee cup.
In some embodiments, the AR system may work as a multiple-plane focus system. In other words, all six LOEs may be illuminated simultaneously, such that images appearing to originate from six fixed depth planes are generated in rapid succession with the light sources rapidly conveying image information to LOE 1, then LOE 2, then LOE 3 and so on. For example, a portion of the desired image, comprising an image of the sky at optical infinity may be injected at time 1 and the LOE 1090 retaining collimation of light (e.g., depth plane 6 from
AR systems are required to project images (i.e., by diverging or converging light beams) that appear to originate from various locations along the Z axis (i.e., depth planes) to generate images for a 3-D experience/scenario. As used in this application, light beams include, but are not limited to, directional projections of light energy (including visible and invisible light energy) radiating from a light source. Generating images that appear to originate from various depth planes conforms the vergence and accommodation of the user's eye for that image, and minimizes or eliminates vergence-accommodation conflict.
Referring now to
The image projection assembly 108 further comprises a scanning device 152 that scans the light in a predetermined scan pattern in response to control signals. The scanning device 152 comprises one or more optical fibers 154 (e.g., single mode optical fiber), each of which has a proximal end 154a into which light is received from the light source(s) 150 and a distal end 154b from which light is provided to the display screen 110. The scanning device 152 further comprises a mechanical drive assembly 156 to which the optical fiber(s) 154 is mounted. The drive assembly 156 is configured for displacing the distal end 154b of each optical fiber 154 about a fulcrum 158 in accordance with a scan pattern.
To this end, the drive assembly 156 comprises a piezoelectric element 160 to which the optical fiber(s) 154 is mounted, and drive electronics 162 configured for conveying electrical signals to the piezoelectric element 160, thereby causing the distal end 154b of the optical fiber 154 to vibrate in accordance with the scan pattern. Thus, operation of the light source(s) 150 and drive electronics 162 are coordinated in a manner that generates image data that is encoded in the form of light that is spatially and/or temporally varying. Descriptions of optical fiber scanning techniques are provided in U.S. Patent No. 2015/0309264, which is expressly incorporated herein by reference.
The image projection assembly 108 further comprises an optical coupling assembly 164 that couples the light from the scanning device 152 into the display screen 110. The optical coupling assembly 164 comprises a collimation element 166 that collimates the light emitted by the scanning device 152 into a collimated light beam 250. Although the collimation element 166 is illustrated in
As will be described in further detail below, the optical coupling subsystem 164 optically couples the collimated light beam 250 into the display screen 110, which will expand the pupil size of the collimated light beam 250 to be commensurate with the entrance pupil size of the end user 50. In the embodiments described below, the display screen 110 employs a technique known as “beam multiplication,” which refers to methods of exit pupil expansion that are specifically designed to expand a small diameter entrance pupil of each collimated light beam 250 from the image projection assembly 108 (e.g., on the order of 50 microns to 1 mm) by multiplying the respective light beam 250 into multiple light beamlets, resulting in a light beamlet array exit pupil that effectively matches the entrance pupil of the user's eye or eyes (e.g., on the order of 5 mm-7 mm) for a fixed eye relief. Notably, although the “beam multiplication” techniques are described herein as being performed in the display screen 110, it should be appreciated that such “beam multiplication” techniques can be applied anywhere in the image generation system 100, including any similar substrate system/subsystem upstream from the display screen 110.
The extent to which the beam of collimated light 250 needs to be multiplied to achieve a given fill factor will depend upon the original pupil size of the collimated light beam 250. For example, if the original pupil size of the collimated light beam output by the image projection assembly 108 is 500 microns, such pupil size may need to be multiplied ten times to achieve desired fill factor, whereas if the original pupil size of the collimated light beam 250 output by the image projection assembly 108 is 50 microns, such pupil may need to be multiplied one hundred times to achieve a desired fill factor.
Preferably, the light beamlet array exit pupil of the display screen is completely in-filled or saturated with light beamlets to maximize the wavefront density and minimize the depth of field. If the in-fill of the light beamlets in the exit pupil is too sparse, the wavefront density and depth of field of the display screen will be compromised, and if the diameter of the light beamlets is too small, the angular resolution of the display screen will be compromised.
Theoretically, the thickness of display screen 110 can be reduced to increase the number of light beamlets created from a single collimated light beam 250 input into the display screen 110, thereby increasing the in-fill of the exit pupil with the light beamlets. However, due to durability and manufacturing limitations, a display screen 110 can only be made so thin, thereby limiting the in-fill of the exit pupil. Also, although the entrance pupil of the collimated light beam 250 transmitted from the image projection assembly 108 into the display screen 110 can theoretically be increased in order to increase the in-fill of the exit pupil with the light beamlets, this would require a commensurate increase in the size of the image projection assembly 108, thereby affecting the wearability of the VR/AR system in a negative manner. Significantly, the embodiments described below increase the in-fill of the exit pupil without requiring an increase in the size of the image projection assembly 108.
To this end, the display screen 110 serves as a pupil expander (PE) that expands the effective entrance pupil of the collimated light beam 250 (carrying the image information) for display to the eye 52 (monocular) or eyes 52 (binocular) of the end user 50. The display screen 110 takes the form of a waveguide apparatus 170 that includes a planar optical waveguide 172 and one or more diffractive optical elements (DOEs) 174 associated with the planar optical waveguide 172 for two-dimensionally expanding the effective entrance pupil of the collimated light beam 250 optically coupled into the planar optical waveguide 172. In alternative embodiments, the waveguide apparatus 170 may comprise multiple planar optical waveguides 172 and DOEs 174 respectively associated with the planar optical waveguides 172.
As best illustrated in
The DOE(s) 174 (illustrated in
In the illustrated embodiment, the DOE(s) 174 comprise one or more diffraction gratings, each of which can be characterized as an optical component with a periodic structure on the order of the light wavelength that splits and diffracts light into several beams travelling in different directions. The diffraction gratings can be composed of, e.g., surface nano-ridges, nano-patterns, slits, etc. that may be photolithographically printed on a substrate. The DOE(s) 174 may allow positioning of apparent objects and focus plane for apparent objects. Such may be achieved on a frame-by-frame, subframe-by-subframe, or even pixel-by-pixel basis.
As illustrated in
A collimated light beam 250 entering the waveguide 172 at one of two different angles will follow one of the two TIR optical paths 182a, 182b, resulting in light beamlets 256 exiting the planar optical waveguide 172 along one of the two sets of external optical paths 185a, 185b. That is, a collimated light beam 250a that enters the waveguide 172 at an angle represented by the TIR optical path 182a will result in the light beamlets 256a exiting the planar optical waveguide 172 along the set of external optical paths 185a, and a collimated light beam 250b that enters the waveguide 172 at an angle represented by the TIR optical path 182b will result in the light beamlets 256b exiting the planar optical waveguide 172 along the set of external optical paths 185b.
In can be appreciated from the foregoing, the display subsystem 104 generates a series of synthetic image frames of pixel information that present an image of one or more virtual objects to the user. Further details describing display subsystems are provided in U.S. patent application Ser. No. 14/212,961, entitled “Display Subsystem and Method,” and U.S. patent application Ser. No. 14/696,347, entitled “Planar optical waveguide Apparatus With Diffraction Element(s) and Subsystem Employing Same,” which are expressly incorporated herein by reference.
As described above,
As shown in
The LOEs 490 discussed above can additionally function as exit pupil expanders 496 (“EPE”) to increase the numerical aperture of a light source 420, thereby increasing the resolution of the system 400. Since the light source 420 produces light of a small diameter/spot size, the EPE 496 expands the apparent size of the pupil of light exiting from the LOE 490 to increase the system resolution. In other embodiments of the MR system 400, the system may further comprise an orthogonal pupil expander 494 (“OPE”) in addition to an EPE 496 to expand the light in both the X and Y directions. More details about the EPEs 496 and OPEs 494 are described in the above-referenced U.S. Utility patent application Ser. No. 14/555,585 and U.S. Utility patent application Ser. No. 14/726,424, the contents of which have been previously incorporated by reference.
The ICG 492 is a DOE (e.g., a linear grating) that is configured to admit light from a light source 420 for propagation by TIR. In the embodiment depicted in
The OPE 494 is a DOE (e.g., a linear grating) that is slanted in the lateral plane (i.e., perpendicular to the light path) such that a light beam that is propagating through the system 400 will be deflected by 90 degrees laterally. The OPE 494 is also partially transparent and partially reflective along the light path, so that the light beam partially passes through the OPE 494 to form multiple (e.g., 11) beamlets. In some embodiments, the light path is along an X axis, and the OPE 494 configured to bend the beamlets to the Y axis.
The EPE 496 is a DOE (e.g., a linear grating) that is slanted in the axial plane (i.e., parallel to the light path or the Y direction) such that the beamlets that are propagating through the system 400 will be deflected by 90 degrees axially. The EPE 496 is also partially transparent and partially reflective along the light path (the Y axis), so that the beamlets partially pass through the EPE 496 to form multiple (e.g., 7) beamlets. The EPE 496 is also slated in a Z direction to direction portions of the propagating beamlets toward a user's eye.
The OPE 494 and the EPE 496 are both also at least partially transparent along the Z axis to allow real-world light (e.g., reflecting off real-world objects) to pass through the OPE 494 and the EPE 496 in the Z direction to reach the user's eyes. In some embodiments, the ICG 492 is at least partially transparent along the Z axis also at least partially transparent along the Z axis to admit real-world light.
The size of a beam spot on the retina affects the resolution of an image as follows. The function of an eye is to collect light information related to a “3-D” scene, which is comprised of a plurality of point sources of light (e.g., emitted or reflected). For instance, a tree may include millions of point sources of light that reflect light from the sun. The eye (e.g., the lens therein) bends light beams to a spot on the retina. Ideally, the beam spot on the retina is the size of a photoreceptor. An eye that is well focused on an object will focus light beams from that object on as small a spot on the retina as possible. When an eye is out of focus relative to an object, the light beams will be brought into focus in front of or behind retina, and the spot resembles a circle instead of a point. A wider circular spot may impinge on several photoreceptors on the retina resulting in a blurred image as interpreted by the optical cortex of the viewer. Further, smaller beam spots (e.g., from 2-3 mm diameter beams) will change spot size (i.e., blur or focus) with lens accommodation more quickly. On the other hand, larger beam spots (e.g., from a 0.5 mm diameter beam) will not change spot size (i.e., blur or focus) with lens accommodation.
Compounding this image focus limitation are various other optical, anatomical, and technological limitations. Image resolution is a function of beam diameter and beam angle (“optical invariant”), which is tied to the number of resolvable spots (e.g., as in the laser scanner industry). The optical invariant is related to a numerical aperture collected by pixels multiplied by the number of pixels. Larger light beam diameters result in higher image resolutions. Smaller light beam diameters result in the ability to conserve increasing light beam angles to maximize the FOV. These optical limitations render beam diameter optimization difficult, because beam diameter affects both image resolution and light beam angle, resulting in a tradeoff between image quality and FOV size.
Further, if a light beam diameter is around 0.5 mm, open loop accommodation with some eyes, as a result of which everything will appear to be at the same poor level of focus. As in pin-hole cameras, the entire FOV will be equally and poorly focused, because the retina space is too small to resolve larger spots displayed thereon, as shown in
As described above, various other optical, anatomical, and technological limitations result in performance limitations of head-worn displays. For instance, light beams with smaller diameters (e.g., around 0.5 mm) compared to light beams with larger diameters (e.g., around 2-3 mm) will result in lower image resolution and optical aberrations. On the other hand, light beams with larger diameters (e.g., around 2-3 mm) compared to light beams with smaller diameters (e.g., around 0.5 mm) will result in narrower FOVs. Balancing image resolution with FOV results in sub-optimal image resolution and FOVs.
The following disclosure describes various embodiments of systems and methods for simulating a larger diameter light beam using a plurality (e.g., an array) of smaller diameter light beams. These beam multiplier systems and methods generate bundles of interrelated, interacting, cloned beamlets 1116 that pass through the pupil to impinge on the retina 1104, as shown in
The plurality/array of beamlets (each with a smaller diameter) simulates the light energy from a much larger diameter light beam, increasing image resolution while maintaining the wider FOV based on the smaller beam diameter.
The spacing of beamlet spots can also affect image quality. As shown in
While the beam multiplier 1430 is depicted inside view in
As shown in
The beam multipliers depicted in
The second LOS 17306 is disposed over the first LOS 1730A such that an incoming light beam 1710 at least partially passes through the first LOS 1730A and enters the second LOS 1730B. As an incoming light beam 1710 passes through the first LOS 1730A, a portion thereof is partially reflected by the second reflective surface 1734. The portion of the incoming light beams 1710 that passes through the second LOS 1730B is reflected by the third reflective surface 1736 in substantially the same direction as the portion of the incoming light beam 1710 that is reflected by the second reflective surface 1734. The result of the addition of the second LOS 17306 and its third reflective surface 1736 is a multiplication of the number of beamlets 1716 propagating along the first and second LOSs 1730A, 17306 by substantially TIR.
The thickness of the second LOS 17306 depicted in
The beam multiplier 1730 depicted in
The beam multiplier 1830 depicted in
The second LOS 1830B is disposed over the first LOS 1830A such that an incoming light beam 1810 at least partially passes through the first LOS 1830A and enters the second LOS 1830B. As an incoming light beam 1810 passes through the first LOS 1830A, a portion thereof is partially reflected by the second reflective surface 1834. The portion of the incoming light beams 1810 that passes through the second LOS 1830B is reflected by the third reflective surface 1836 in substantially the same direction as the portion of the incoming light beam 1810 that is reflected by the second reflective surface 1834. Before the reflected beamlet 1816 exits the second LOS 1830B, a portion of the reflected beamlet 1816 is reflected by the fourth reflective surface 1838 back toward the third reflective surface 1836. The result of the addition of the fourth reflective surfaces 1838 in the second LOS 1830B is a further multiplication of the number of beamlets 1816 propagating along the first and second LOSs 1830A, 1830B by substantially TIR even compared to the beam multiplier 1730 depicted in
The beam multiplier 1930 depicted in
The third LOS 1930C is disposed over the second LOS 19306 (and therefore the first LOS 1930A) such that an incoming light beam 1910 at least partially passes through the first and second LOSs 1930A, 19306 and enters the third LOS 1930C. As an incoming light beam 1910 passes through the first LOS 1930A, a portion thereof is partially reflected by the second reflective surface 1934. Similarly, as an incoming light beam 1910 passes through the second LOS 1930B, a portion thereof is partially reflected by the third reflective surface 1936. The portion of the incoming light beams 1910 that passes through the second LOS 19306 is reflected by the third reflective surface 1936 in substantially the same direction as the portion of the incoming light beam 1910 that is reflected by the second reflective surface 1934. Similarly, The portion of the incoming light beams 1910 that passes through the third LOS 1930C is reflected by the fifth reflective surface 1940 in substantially the same direction as the portions of the incoming light beam 1910 that are respectively reflected by the second and third reflective surfaces 1934, 1936.
Before the reflected beamlet 1916 exits the second LOS 1930B, a portion of the reflected beamlet 1916 is reflected by the fourth reflective surface 1938 back toward the third reflective surface 1936. Similarly, before the reflected beamlet 1916 exits the third LOS 1930C, a portion of the reflected beamlet 1916 is reflected by the sixth reflective surface 1942 back toward the fifth reflective surface 1940. The result of the addition of the third LOS 1930C and its fifth and sixth reflective surfaces 1940, 1942 is a further multiplication of the number of beamlets 1916 propagating along the first, second, and third LOSs 1930A, 1930B, 1930C by substantially TIR. As shown in
Multi-surface beam multipliers can be fabricated using a lamination process. In some embodiments, a second substrate (e.g., a second LOS) having a second thickness is laminated onto a first substrate (e.g., a first LOS) having a first thickness. The interface between the two substrates may be partially reflective (e.g., a metallic coating/half-silvered mirror, a thin film coating, a dichroic mirror, a dielectric interface, a diffraction grating, a diffractive element, etc.) In another embodiment, separate waveguides/LOEs can be laminated together with a partially-reflective interface.
Further, the ratio of thicknesses of first and second LOSs (and various sub combinations of any plurality of LOSs in a system) can affect beamlet multiplication by beamlet overlap. If the respective thicknesses are whole number multiples or quotients (i.e., factors), then cloned beamlets may overlap when they exit the first and second LOSs, reducing the degree of beamlet multiplication. Therefore, in some embodiments (see
Beam multipliers can also be tuned by varying the degree of reflectiveness/transmittance of various surfaces (e.g., other than 50/50). Using this and other techniques, the multipliers can be tuned to have an even distribution of energy across the beamlets. For moderate amounts of beam multiplication (e.g., sufficient to fill the pupils of the eyes), the beam multiplier(s) can be two to ensure that beamlets (and groups thereof) have the same amounts of energy, as the eye sweeps across different sets of beamlets. Equalizing the amount of energy across beamlets minimizes dropouts in intensity (artifacts; winking) as the user's eyes sweep the FOV. With an exponentially increasing number of beamlets, beamlets will eventually randomly overlap, thereby reducing intensity artifacts.
A FOV may be expanded with kaleidoscopically tuned beam multipliers. The relative reflectivity of surfaces can be tuned such that the beam multiplier has dense beam multiplication in optically important regions (e.g., center of an FOV) and sparse beam multiplication in optically less important regions (e.g., periphery of an FOV). The FOV can be determined to various types of eye tracking, including but not limited to interpupillary distance measurement and pupil motion tracking.
The OPE 494 and EPE 496 depicted in
There are two exit edges 2612, 2614 for OPE1 2604 (see
Using such a system, the OPE (as a separate element) can be removed from the LOE 490 (e.g., see
Using this design can also create a large region including a smaller region in which all or most of the information/light energy is contained. Such a system can use depth switching mechanisms to route light to different layers (e.g., multiple depth plane layers). The layers can be polymer dispersed liquid crystal (“PDLC”) switchable layers. Alternatively, the layers can be waveguides with respective LC shutters. Such a system can use TIR based structures from a main LOE to generate multiple exit ports for redundant optical information that can be selected by LC shutter or PDLC swatches. In some embodiments, a single OPE can feed light/optical information to multiple EPE layers (e.g., EPEs corresponding to red, green, and blue light).
In a similar embodiment 3000 depicted in
For both of the embodiments depicted in
The beam multiplier 3100 depicted in
The beam multiplier 3200 depicted in
The beam multipliers 3300 depicted in
Referring now to
To this end, the DOE(s) 174 comprises an orthogonal pupil expansion (OPE) element 186 closely associated with (e.g., embedded in) the face 180b of the waveguide 172 for splitting the in-coupled light beam 252 into orthogonal light beamlets 254, and an exit pupil expansion (EPE) element 188 closely associated with (e.g., embedded in) the face 180b of the waveguide 172 for splitting the orthogonal light beamlets 254 into a set of out-coupled light beamlets 256 that exit the face 180b of the waveguide 172 towards the eye(s) 52 of the end user 50. In the alternative embodiment where the waveguide 172 is composed of distinct panes, the OPE element(s) 174 and EPE element 188 may be incorporated into different panes of the waveguide 172.
The OPE element 186 relays light along a first axis (horizontal or x-axis in
In a similar fashion, at each point of intersection with the OPE element 186, a portion (e.g., greater than 90%) of each orthogonal light beamlet 254 continues to propagate in the waveguide 172 via TIR along the respective internally reflective optical path parallel to the axis 264 (x-axis), and the remaining portion (e.g., less than 10%) of the respective orthogonal light beamlet 254 is diffracted as secondary light beamlets 256 that propagate within the waveguide 172 via TIR along respective internally reflective optical paths (shown by dashed lines) parallel to the axis 262 (y-axis). In turn, at each point of intersection with the OPE element 186, a portion of (e.g., greater than 90%) of each secondary light beamlet 256 continues to propagate in the waveguide 172 via TIR along a respective internally reflective optical path parallel to the axis 262 (y-axis), and the remaining portion (e.g., less than 10%) of the respective secondary light beamlet 256 is diffracted as tertiary light beamlets 258 that combine in phase with the orthogonal light beamlets 254 and propagate within the waveguide 172 via TIR along respective internally reflective optical paths parallel to the axis 264 (x-axis).
Thus, by dividing the in-coupled light beam 252 into multiple orthogonal light beamlets 254 that propagate within the waveguide 172 via TIR along respective internally reflective optical paths parallel to the axis 264 (x-axis), the entrance pupil of the collimated light beam 250 in-coupled into the display screen 110 is expanded vertically along the y-axis by the OPE element 186.
The EPE element 188, in turn, further expands the light's effective exit pupil along the first axis (horizontal x-axis in
Thus, by dividing each orthogonal light beamlet 254 into multiple out-coupled light beamlets 256, the entrance pupil of the collimated light beam 250 is further expanded horizontally along the x-axis by the EPE element 188, resulting in a two-dimensional array of out-coupled light beamlets 256 that resemble a larger version of the original in-coupled light beam 252.
Although the OPE element 186 and EPE element 188 are illustrated in
In addition to the function of out-coupling the light beamlets 256 from the face 180b of the waveguide 172, the EPE element 188 serves to focus the output set of light beamlets 256 at along a given focal plane, such that a portion of an image or virtual object is seen by end user 50 at a viewing distance matching that focal plane. For example, if the EPE element 188 has only a linear diffraction pattern, the out-coupled light beamlets 256 exiting the face 180b of the waveguide 172 toward the eye(s) 52 of the end user 50 will be substantially parallel, as shown in
Although the waveguide apparatus 170 has been described herein as having only one focal plane, it should be appreciated that multiple planar optical waveguides 172 with associated OPEs 176 and EPEs 178 can be used to simultaneously or sequentially generate images at multiple focal planes, as discussed in U.S. Patent Publication Nos. 2015/0309264 and 2015/0346490, which are expressly incorporated herein by reference.
As previously described, it is desirable to increase the saturation or in-fill of the exit pupil of the display screen 110. Without modification, the exit pupil of the display screen 110 may not be optimally saturated. For example, as illustrated in
For example, in some embodiments, two OPEs 186 are employed to double the number of orthogonal light beamlets 254 obtained from the in-coupled light beam 252, and thus, double the saturation of the two-dimensional array of out-coupled light beamlets 256 that exit the face 180b of the waveguide 172.
In particular, as shown in
That is, because the in-coupled light beam 252 propagating within the waveguide 172 via TIR along the internally reflective optical path parallel to the axis 262 (y-axis) alternately intersects the first and second OPE elements 186a, 186b on the opposite faces 180a, 180b of the waveguide 172, portions of the in-coupled light beam 252 are respectively diffracted as the first and second primary sets of light beamlets 254a, 254b for propagation within the waveguide 172 via TIR along alternating internally reflective optical paths parallel to the axis 264 (x-axis). Secondary light beamlets 256a, 256b (shown in
In another embodiment, partially reflective interfaces are incorporated into the waveguide 172 to increase the number of light beamlets propagating within the waveguide 172, and thus, increase the saturation of the two-dimensional array of out-coupled light beamlets 256 exiting the face 180b of the waveguide 172. In the embodiments illustrated below, the waveguide 172 comprises a plurality of layered substrates having at least one pair of adjacent substrates and a semi-reflective interface between each of the pair(s) of adjacent substrates, such that a light beam that intersects each semi-reflective interface is split into multiple beamlets that propagate within the waveguide 172 via TIR, thereby increasing the density of the out-coupled light beamlets exiting the face 180b of the waveguide 172. It should be noted that the adjacent substrates described below are not drawn to scale and are illustrated as being multiples of each other for purposes of simplicity. However, adjacent substrates may be, and preferably are, non-multiples of each other, such that the density of the in-fill of out-coupled light beamlets exiting the face of the waveguide is maximized.
In particular, and with reference to
In some embodiments, the semi-reflective interface 190 takes the form of a semi-reflective coating, such as one composed of, e.g., a metal, such as gold, aluminum, silver, nickel-chromium, chromium, etc., a dielectric, such as oxides, fluorides, sulfides, etc., a semiconductor, such as silicon, germanium, etc., and/or a glue or adhesive with reflective properties can be disposed between the primary waveguide 172a and secondary waveguide 172b via any suitable process, such as physical vapor deposition (PVD), ion-assisted deposition (IAD), ion beam sputtering (IBS), etc. The ratio of reflection to transmission of the semi-reflective coating 190 may be selected or determined based at least in part upon the thickness of the coating 190, or the semi-reflective coating 190 may have a plurality of small perforations to control the ratio of reflection to transmission. In an alternative embodiment, the primary waveguide 172a and secondary waveguide 172b are composed of materials having different indices of refraction, such that the interface between the waveguides 172a, 172b are semi-reflective for light that is incident on the semi-reflective interface of less than a critical angle (i.e., the incidence angle at which a portion of the light is transmitted through the semi-reflective interface, and the remaining portion of the light is reflected by the semi-reflective interface). The semi-reflective interface 190 is preferably designed, such that the angle of a light beam incident on the semi-reflective interface 190 is preserved.
In any event, as best shown in
In particular, the semi-reflective interface 190 is configured for splitting the in-coupled light beam 252 into two primary in-coupled light beamlets (in this case, a first primary in-coupled light beamlet 252a (shown by a solid line) and a second primary in-coupled light beamlet 252b (shown by a dashed line) that propagate within the primary waveguide 172a along an internally reflective optical path parallel to the axis 262 (y-axis). As shown in
It should be appreciated that, because the thickness of the primary waveguide 172 is a multiple of the thickness of the secondary waveguide 172b (in this case, exactly twice as thick), only two primary in-coupled light beamlets 252a, 252b are generated due to recombination of light beamlets. However, in the preferred case where the thickness of the primary waveguide 172a is a non-multiple of the thickness of the secondary waveguide 172b, an additional primary in-coupled light beamlet 252 is generated at each point of intersection between a secondary in-coupled light beamlet 252′ and the semi-reflective interface 190, and likewise, an additional secondary in-coupled light beamlet 252′ is generated at each point of intersection between a primary in-coupled light beamlet 252 and the semi-reflective interface 190. In this manner, the number of primary in-coupled light beamlets 252 geometrically increases from the ICO 168 along the axis 262.
The OPE element 186 is configured for respectively splitting the primary in-coupled light beamlets 252a, 252b into two sets of primary orthogonal light beamlets. In particular, the primary in-coupled light beamlets 252a, 252b intersect the OPE element 186 adjacent the face 180b of the waveguide 172, such that portions of the primary in-coupled light beamlets 252a, 252b are diffracted as two sets of primary orthogonal light beamlets 254a, 254b that propagate within the waveguide 172 via TIR along respective internally reflective optical paths parallel to the axis 264 (x-axis).
As best shown in
It should be appreciated that, because the thickness of the primary waveguide 172a is a multiple of the thickness of the secondary waveguide 172b (in this case, exactly twice as thick), only two primary orthogonal light beamlets 254 are generated from each orthogonal light beamlet 254. However, in the preferred case where the thickness of the primary waveguide 172a is a non-multiple of the thickness of the secondary waveguide 172b, an additional primary orthogonal light beamlet 254 is generated at each point of intersection between a secondary orthogonal light beamlet 254′ and the semi-reflective interface 190, and likewise, an additional secondary orthogonal light beamlet 254′ is generated at each point of intersection between a primary in-coupled light beamlet 254 and the semi-reflective interface 190. In this manner, the number of primary orthogonal light beamlets 254 geometrically increases from the ICO 168 along the axis 264 (x-axis).
The EPE element 188 is configured for splitting each of the orthogonal light beamlets into the set of out-coupled light beamlets 256. For example, the sets of primary orthogonal light beamlets 254 (only the sets of primary orthogonal light beamlets 254a(1) and 254a(2) shown) intersect the EPE element 188 adjacent the face 180b of the waveguide 172, such that portions of the primary orthogonal light beamlets 254 are diffracted as the set of out-coupled light beamlets 256 that exit the face 180b of the waveguide 172. Thus, the increase in the number of the in-coupled light beamlets 252 and the number of orthogonal light beamlets 254 correspondingly increases the saturation of the exit pupil 300a expanded by the display screen 110 (shown in
Referring to
At the first point of intersection P1 with the semi-reflective interface 190, a portion of the light beam 252 is transmitted through the semi-reflective interface 190 into the secondary waveguide 172b as the secondary light beamlet 252′, which is reflected by the face 180a of the waveguide 172 back to a second point of intersection P2 of the semi-reflective interface 190, while a portion of the light beam 252 is reflected by the semi-reflective interface 190 back into the primary waveguide 172a as the primary light beamlet 252a, which is reflected by the face 180b of the waveguide 172 back to a third point of intersection P3 of the semi-reflective interface 190 (
At the second point of intersection P2 with the semi-reflective interface 190, a portion of the secondary light beamlet 252′ is transmitted through the semi-reflective interface 190 into the primary waveguide 172b as the primary light beamlet 252b, which is reflected by the face 180a of the waveguide 172 back to a fourth point of intersection P4 of the semi-reflective interface 190, while a portion of the secondary light beamlet 252′ is reflected by the semi-reflective interface 190 back into the secondary waveguide 172b as the secondary light beamlet 252′, which is reflected by the face 180a of the waveguide 172 back to the third point of intersection P3 of the semi-reflective interface 190 (
At the third point of intersection P3 with the semi-reflective interface 190, a portion of the primary light beamlet 252a is transmitted through the semi-reflective interface 190 into the secondary waveguide 172b, and a portion of the secondary light beamlet 252′ is reflected by the semi-reflective interface 190 back into the secondary waveguide 172b, which portions happen to combine together as the secondary light beamlet 252′ and reflected by the face 180b of the waveguide 172 back to the fourth point of intersection P4 (
At the fourth point of intersection P4 with the semi-reflective interface 190, a portion of the primary light beamlet 252b is transmitted through the semi-reflective interface 190 into the secondary waveguide 172b, and a portion of the secondary light beamlet 252′ is reflected by the semi-reflective interface 190 back into the secondary waveguide 172b, which portions may combine together as the secondary light beamlet 252′ and reflected by the face 180b of the waveguide 172 back to the fifth point of intersection P5 (
Thus, it can be appreciated from the foregoing that light energy is transferred between the primary waveguide 172a and secondary waveguide 172b to generate and propagate two light beamlets 252a, 252b within the waveguide apparatus 170.
Significantly, the thicknesses of the layered substrates, in coordination with the expected incident angles of the light beams on each semi-reflective interface, are selected, such that there is no gap between the edges of adjacent out-coupled beamlets 256.
For example, in the embodiment illustrated in
It should be noted that the width w of the collimated light beam 250 relative to the size of the IC element 168 has been exaggerated for purposes of illustration. In reality, the width w of the collimated light beam 250 will be much smaller than the size of the IC element 168, which needs to be large enough to accommodate all scan angles of the collimated light beam 250. In the preferred embodiment, the average spacing between adjacent out-coupled light beamlets 256 is minimized for the worst-case scan angle. For example, for the worst-case scan angle, although there may be gaps between some of the adjacent out-coupled light beamlets 256, there will be no gaps between most of the adjacent out-coupled light beamlets 256.
Thus, the thickness Δt of the secondary waveguide 172b may be selected based on the worst-case scan angle to minimize the spacings between adjacent out-coupled beamlets 256. It should be noted that the worst-case scan angle is one that results in the smallest angle of incidence of the in-coupled light beam 252 on the semi-reflective interface 190. Of course, if the primary waveguide 172a is not a multiple of the secondary waveguide 172b, more out-coupled beamlets 256 will be generated, thereby naturally decreasing the average spacing between adjacent out-coupled beamlets 256. In this case, it may be beneficial to select the thickness values t and Δt to have a least common multiple that is relatively high. For example, in selecting the thickness values t and Δt, one may seek to maximize the least common multiple of the thickness values t and Δt to maximize the quantity of out-coupled beamlets 256 for the worst-case scan angle. Furthermore, selecting the thickness values t and Δt may also yield an uneven/complex distribution of out-coupled beamlets 256 that may minimize adverse effects created by coherent light interactions between adjacent out-coupled beamlets 256.
For example, if it is assumed that the worst-case angle of incidence between the in-coupled light beam 252 and the semi-reflective interface 190 is sixty degrees, and the thickness t of the primary waveguide 172a is exactly twice the thickness Δt of the secondary waveguide 172b, the thickness Δt of the secondary waveguide 172b should be √{square root over (3)}/2 the width w of the in-coupled light beam 252, so that, as illustrated in
It should be appreciated that, for purposes of simplicity in explanation, no refraction of light transmitted through the semi-reflective interface 190 is assumed. However, in the case where substantial refraction of the transmitted light through the semi-reflective interface 190 occurs, the angle of transmission of the light due to such refraction must be taken into account when selecting the thickness Δt of the secondary waveguide 172b. For example, the greater the refraction of the light, such that the angle of the transmitted light relative to the semi-reflective interface 190 decreases, the more the thickness Δt of the secondary waveguide 172b must be decreased to compensate for such refraction.
It should also be appreciated from the foregoing that the generation of the primary in-coupled light beamlets 252 propagating within the primary waveguide 172a via TIR along the internally reflective optical paths parallel to the axis 262 (y-axis), and then the generation of the primary out-coupled light beamlets 256 propagating within the primary waveguide 172a along the internally reflective optical paths parallel to the axis 264 (x-axis), assuming an appropriate thickness Δt of the secondary waveguide 172b, will completely in-fill the exit pupil of the display screen 110.
In the case where it is desirable to decrease the thickness Δt of the secondary waveguide 172b to further decrease the average spacing between the adjacent primary in-coupled light beamlets 252, primary orthogonal light beamlets 254, and out-coupled light beamlets 256, the thickness t of the primary waveguide 172a may be much greater than the thickness Δt of the secondary waveguide 172b, e.g., greater than three, four, five, or even more times the thickness Δt of the secondary waveguide 172b.
For example, as illustrated with respect to the waveguide apparatus 170c in
It should be appreciated that, because the thickness of the primary waveguide 172a is a multiple of the thickness of the secondary waveguide 172b (in this case, exactly three times as thick), only three primary in-coupled light beamlets 252a, 252b, 252c are generated due to recombination of light beamlets. However, in the preferred case where the thickness of the primary waveguide 172a is a non-multiple of the thickness of the secondary waveguide 172b, an additional primary in-coupled light beamlet 252 is generated at each point of intersection between a secondary in-coupled light beamlet 252′ and the semi-reflective interface 190, and likewise, an additional secondary in-coupled light beamlet 252′ is generated at each point of intersection between a primary in-coupled light beamlet 252 and the semi-reflective interface 190. In this manner, the number of primary in-coupled light beamlets 252 geometrically increases from the ICO 168 along the axis 262 (y-axis).
The OPE element 186 is configured for respectively splitting the primary in-coupled light beamlets 252a-252c into three sets of primary orthogonal light beamlets. In particular, the primary in-coupled light beamlets 252a-252c intersect the OPE element 186 adjacent the face 180b of the waveguide 172, such that portions of the primary in-coupled light beamlets 252a-252c are diffracted as three sets of primary orthogonal light beamlets 254a-254c that propagate within the waveguide 172 via TIR along respective internally reflective optical paths parallel to the axis 264 (x-axis).
As best shown in
It should be appreciated that, because the thickness of the primary waveguide 172a is a multiple of the thickness of the secondary waveguide 172b (in this case, exactly three times as thick), only three primary sets of orthogonal light beamlets 254a, 254b, 254c are generated due to recombination of light beamlets. However, in the preferred case where the thickness of the primary waveguide 172a is a non-multiple of the thickness of the secondary waveguide 172b, an additional set of primary orthogonal light beamlets 254 is generated at each point of intersection between a set of secondary orthogonal light beamlets 254′ and the semi-reflective interface 190, and likewise, an additional set of secondary orthogonal light beamlets 254′ is generated at each point of intersection between a primary set of orthogonal light beamlet 254 and the semi-reflective interface 190. In this manner, the number of primary orthogonal light beamlets 254 geometrically increases from the ICO 168 along the axis 264 (x-axis).
The EPE element 188 is configured for splitting the nine sets of orthogonal light beamlets into the set of out-coupled light beamlets 256. In particular, as shown in
Notably, such saturation of the exit pupil 300a by the waveguide apparatus 170c of
the width w or the in-coupled light beam 252, so that, as illustrated in
It can be appreciated from the foregoing that, while the thickness t of the primary waveguide 172a may be much larger than the width w of the collimated light beam 250 in-coupled into the waveguide apparatuses 170b, 170c, illustrated in
Thus, in this case, the thickness of the secondary waveguide 172b may be selected to be slightly less than the thickness t of the primary waveguide 172a, i.e., t-Δt. As best shown in
The OPE element 186 is configured for respectively splitting the primary in-coupled light beamlets 252a-252c into three sets of primary orthogonal light beamlets. In particular, the primary in-coupled light beamlets 252a-252c intersect the OPE element 186 adjacent the face 180b of the waveguide 172, such that portions of the primary in-coupled light beamlets 252a-252c are diffracted as three sets of primary orthogonal light beamlets 254a-254c that propagate within the waveguide 172 via TIR along respective internally reflective optical paths parallel to the axis 264 (x-axis).
As best shown in
The EPE element 188 is configured for splitting the nine sets of orthogonal light beamlets into the set of out-coupled light beamlets 256. In particular, as shown in
In the same manner that the thickness Δt of the secondary waveguide 172b is selected above with respect to the waveguide apparatuses 170b and 170c of
the width w of the in-coupled light beam 252, so that the adjacent primary in-coupled light beamlets 252 and the edges of the adjacent primary orthogonal light beamlets 254 will have no gaps therebetween, and thus, the edges of the adjacent out-coupled light beamlets 256 will have no gaps therebetween. Thus, in this case, the thickness of the secondary waveguide 172b will be greater than the width w of the in-coupled light beam 252.
Although the previous waveguide apparatuses 170a-170d illustrated in
As best shown in
The OPE element 186 is configured for respectively splitting the primary in-coupled light beamlets 252a-252c into three sets of primary orthogonal light beamlets. In particular, the primary in-coupled light beamlets 252a-252c intersect the OPE element 186 adjacent the face 180b of the waveguide 172, such that portions of the primary in-coupled light beamlets 252a-252c are diffracted as three sets of primary orthogonal light beamlets 254a-254c that propagate within the waveguide 172 via TIR along internally reflective optical paths parallel to the axis 264 (x-axis).
As best shown in
The EPE element 188 is configured for splitting the nine sets of orthogonal light beamlets into the set of out-coupled light beamlets 256. In particular, as shown in
In the prior embodiments, the entrance pupil of the collimated light beam output by the collimation element 154 is expanded only by the combination of the OPE element 186 and EPE element 188 of the display screen 110, and includes features in close association with the OPE element 186 and EPE element 188 for increasing the saturation of the exit pupil of the display screen 110. In the embodiments of a display subsystem 104′ subsequently described herein, the image projection assembly 108 further includes a pre-pupil expansion (PPE) 192, which in the embodiment illustrated in
The PPE 192 represents the first pupil expansion stage, and is designed to use one or more beam-multiplication techniques to pre-expand the entrance pupil of the collimated light beam 250 to an intermediate exit pupil 300a of a set (in this case, a two-dimensional 3×3 array) of initial out-coupled light beamlets 256′ prior to in-coupling into the waveguide apparatus 170 of the display screen 110 (which emulates inputting a conventional collimated light beam having a larger pupil size as illustrated in
In alternative embodiments, the display screen 110 may further expand the pupil size of the collimated light beam 250 to an exit pupil of an even more saturated set of final out-coupled light beamlets 256 using the aforementioned enhanced beam multiplication techniques. However, it should be appreciated that the use of the PPE 192 lends itself well to miniature-scale image devices that output relatively small pupil sized light beams that can be expanded to normal pupil sized light beams for input into a conventional PE for expansion to an exit pupil commensurate with the entrance pupil size of the eye(s) 52 of the end user 50. For example, the PPE 192 may expand the entrance pupil of a collimated beam to a pre-expanded pupil that is at least ten times larger (e.g., at least 0.5 mm pupil) than the entrance pupil (e.g., 50 mil pupil size), and the waveguide apparatus 170 of the display screen 110 may further expand the pre-expanded pupil of the collimated light beam 250 to an exit pupil that is at least ten times larger (e.g., at least 5 mm pupil) than the pre-expanded pupil of the collimated light beam 250. By utilizing a multi-stage pupil expansion system, manufacturing constraints associated with expanding the relatively small pupil of a collimated beam to a relatively large and saturated exit pupil need not be imposed on just one pupil expansion device, but rather can be distributed amongst multiple expansion devices, thereby facilitating manufacture of the entire system.
Referring now to
To this end, the PPE 192a takes the form of a waveguide apparatus 170′ having a size commensurate with the size of the IC element 168 of the primary waveguide apparatus 170. As with the primary waveguide apparatus 170 of the display screen 110, the mini-waveguide apparatus 170′ comprises a planar optical waveguide 172′ that takes the form of a single unitary substrate or plane of optically transparent material (as described above with respect to the waveguide 172) and one or more DOEs 174′ associated with the waveguide 172′ for two-dimensionally pre-expanding the effective exit pupil of a collimated light beam 250 optically coupled into the waveguide 172′. The PPE 192a further comprises an IC element 168′ disposed on the face 180b′ of the waveguide 172′ for receiving the collimated light beam 250 from the collimation element 166 into the waveguide 172′ via the face 180b′, although in alternative embodiments, the IC element 168′ may be disposed on the other face 180a′ or even the edge of the waveguide 172′ for coupling the collimated light beam 250 into the waveguide 172 as an in-coupled light beam. The DOE(s) 174′ are associated with the waveguide 172′ (e.g., incorporated within the waveguide 172′ or abutting or adjacent one or more of the faces 180a′, 180b′ of the waveguide 172′) for, as briefly discussed above, two-dimensionally pre-expanding the effective entrance pupil of the collimated light beam 250 optically coupled into the waveguide 172′.
To this end, the DOE(s) 174 comprise an orthogonal pupil expansion (OPE) element 186 for splitting the in-coupled light beam 252 into a set of initial orthogonal light beamlets 254′, and an exit pupil expansion (EPE) element 188′ for splitting each initial orthogonal light beamlet 254′ into a set of initial out-coupled light beamlets 256′ that exit the face 180b′ of the waveguide 172′. In the particular embodiment illustrated in
The OPE element 186′ relays light along a first axis (horizontal or x-axis in
Thus, by dividing the in-coupled light beam 252′ into multiple initial orthogonal light beamlets 254′ that propagate along parallel internally reflective optical paths 264, the entrance pupil of the collimated light beam 250 in-coupled into the mini-waveguide apparatus 170′ is pre-expanded vertically along the y-axis by the OPE element 186′.
The EPE element 188′, in turn, further pre-expands the light's effective pupil along the first axis (horizontal x-axis in
Thus, by dividing each initial orthogonal light beamlet 254′ into multiple initial out-coupled light beamlets 256′, the exit pupil of the in-coupled light beam 252 is further pre-expanded horizontally along the x-axis by the EPE element 188′, resulting in a two-dimensional array of initial out-coupled light beamlets 256′ that resemble a larger version of the original in-coupled light beam 252.
In the same manner as described above with respect to
Thus, as illustrated in
Referring now to
In particular, the PPE 192b comprises a diffractive beam splitter 194 that utilizes a single DOE that splits the collimated light beam 250 into a set of initial out-coupled light beamlets 256′. As best shown in
The diffraction grating 198 can be designed to generate an odd number of diverging light beamlets 254′ from the single collimated light beam 250 or an even number of diverging light beamlets 254′ from the single collimated light beam 250. Significantly, when the collimated light beam 250 intersects the diffraction grating 198, beamlets are created at different diffraction orders. For example, as illustrated in
The diffraction grating 198 may either split the collimated light beam 250′ into a one-dimensional array of diverging light beamlets 254′ or a two-dimensional (M×N) array of diverging light beamlets 254′. In the embodiment illustrated in
Significantly, the PPE 192b applies an angle preserving expansion to the collimated light beam 250. That is, the PPE 192b bends the set of diverging light beamlets 254′ exiting the face 196b of the substrate 196 back to the original angle of the collimated light beam 250′. To this end, the PPE 192b comprises a lens 200, and in this embodiment a diffractive lens, that refocuses the diverging light beamlets 254′ as the set of initial out-coupled light beamlets 256′ back to the original angle of the collimated light beam 250′. Although the diffractive lens 200 is illustrated as being separate from the IC element 168, the function of the diffractive lens 200 can be incorporated into the IC element 168.
It can be appreciated from the foregoing that the PPE 192b two-dimensionally pre-expands the effective entrance pupil of the collimated light beam 250. In the same manner as described above with respect to
Referring now to
As best shown in
The prism body 202 comprises prism sections 206a-202f that are bonded together to create the whole of the prism body 202. The prism plane 204a(1) is formed at the interface between the prism sections 206a and 206b; the prism plane 204a(2) is formed at the interface between the prism sections 206b and 206c; the prism plane 204b(1) is formed at the interface between the prism sections 206d and 206e; and the prism plane 204b(2) is formed at the interface between the prism sections 206e and 206f.
The prism planes 204 are configured for splitting a collimated light beam 250 entering the first face 202a of the prism body 202 into a set of initial out-coupled light beamlets 256′ (and in this case, a 2×2 array of light beamlets 256′) that exit the second face 202b of the prism body 202.
To this end, each of the prism planes 204a(1) and 204b(1) is formed of a semi-reflective coating, such as one composed of, e.g., a metal, such as gold, aluminum, silver, nickel-chromium, chromium, etc., a dielectric, such as oxides, fluorides, sulfides, etc., a semiconductor, such as silicon, germanium, etc., and/or a glue or adhesive with reflective properties, which can be disposed between adjacent prism sections 206 via any suitable process, such as physical vapor deposition (PVD), ion-assisted deposition (IAD), ion beam sputtering (IBS), etc. The ratio of reflection to transmission of the semi-reflective coating may be selected or determined based at least in part upon the thickness of the coating, or the semi-reflective coating may have a plurality of small perforations to control the ratio of reflection to transmission. Thus, each of the prism planes 204a(1) and 204b(1) will split a light beam by reflecting a portion of the light beam and transmitted the remaining portion of the light beam. In contrast, each of the prism planes 204a(2) and 204b(2) is preferably formed of a completely reflective coating, which may be composed of the same material as the semi-reflective coating. However, the thickness of the coating may be selected, such that the prism planes 204a(2) and 204b(2) are completely reflective.
In an alternative embodiment, adjacent prism sections 206 may be composed of materials having different indices of refraction, such that the prism plane 204 between the respective prism sections 206 is semi-reflective (in the case of prism planes 204a(1) or 204b(1)) or completely reflective (in the case of prism planes 204a(2) and 204b(2)) for light that is incident on the semi-reflective interface at less than a critical angle. In any event, each prism plane 204 is preferably designed, such that the angle of a light beam incident on the prism plane 204 is preserved.
As best shown in
As best shown in
It can be appreciated from the foregoing that the PPE 192c two-dimensionally pre-expands the effective entrance pupil of the collimated light beam 250. In the same manner as described above with respect to
The distance d between the prism planes 204 are preferably selected, such that the distance s between adjacent initial out-coupled light beamlets 256′ will be equal to the desired spacings of the final out-coupled light beamlets 256 exiting the primary waveguide apparatus 170. In the illustrated embodiment, the prism planes 204 are oriented at forty-five degree angle to the faces 202a, 202b of the prism body 202, and thus, the distance d can be expressed as a function of the distance s, as follows: d=s*sin 45°. The thickness of the waveguide 172 in the primary waveguide apparatus 170 can be multiples of the distance d between the prism planes 204 in each set of parallel prism planes 204 of the PPE 192c (in this case, two times the distance d between the parallel prism planes 204), such that the in-fill of final out-coupled light beamlets 256 is facilitated.
It should be appreciated that larger arrays of initial out-coupled light beamlets 256′ may be created by decreasing the distance between the prism planes 204 in each set of parallel prism planes 204 of the PPE 192c relative to the size of the prism body 202, as illustrated in
For example, as illustrated in
As illustrated in
Again, the distance d between the prism planes 204 are preferably selected, such that the distance s between adjacent initial out-coupled light beamlets 256′ will be equal to the desired spacings of the final out-coupled light beamlets 256 exiting the primary waveguide apparatus 170. In the illustrated embodiment, the prism planes 204 are oriented at forty-five degree angle to the faces 202a, 202b of the prism body 202, and thus, the distance d can be expressed as a function of the distance s, as follows: d=s*sin 45°.
Thus, for each orthogonal light beamlet 254, three initial out-coupled light beamlets 256′ will be generating, thereby creating a 3×3 array of initial out-coupled light beamlets 256′ exit the second face 202b of the prism body 202. Of course, the PPE 192c can be designed to create even larger arrays of initial out-coupled light beamlets 256′, e.g., a 4×4 array, a 5×5 array, etc., by further decreasing the distance between the prism planes 204 in each set of parallel prism planes 204 of the PPE 192c relative to the size of the prism body 202.
Although the PPE 192c has been described as generated square arrays of initial out-coupled light beamlets 256′, the PPE 192c can alternatively be designed to generate non-square arrays of initial out-coupled light beamlets 256′, e.g., a 2×3 array, 3×2 array, 2×3 array, 3×2 array, etc., by making the distance between the prism planes 204a(1) and 204a(2) different from the distance between the prism planes 204b(1) and 204b(2). Furthermore, although the PPE 192c has been described as creating two-dimensional arrays of initial out-coupled light beamlets 256′, the PPE 192c can be designed to create one-dimensional arrays of initial out-coupled light beamlets 256′, e.g., 1×2 array, 1×3 array, etc., by designing the PPE 192c with only one set of parallel prism planes 204.
Furthermore, although the PPE 192c has been described as generating initial out-coupled light beamlets 256′ that exit the prism body 202 at an orthogonal angle to the face 202b of the prism body 202, the PPE 192c can be designed, such that the initial out-coupled light beamlets 256′ exit the prism body 202 at an oblique angle to the face 202b of the prism body 202 by changing the orientations of one or both of the sets of prism planes 204 relative to the face 202b of the prism body 202.
Referring now to
As best shown in
The prism planes 212 are configured for splitting a collimated light beam 250 entering the first face 202a of the prism section 210 into a set of initial light beamlets 256′ (in this case, a 1×4 array of initial out-coupled light beamlets 256′) that exit the second face 214b of the first prism section 210a. To this end, the first prism plane 212a is designed to be partially reflective, whereas the second prism plane 212b is designed to be completely reflective in the same manner that the prism planes 204 of the PPE 192c described above are designed to be partially reflective or completely reflective. Each prism plane 212 is preferably designed, such that the angle of a light beam incident on the prism plane 212 is preserved.
As best shown in
It can be appreciated from the foregoing that the PPE 192e one-dimensionally pre-expands the effective entrance pupil of the collimated light beam 250. In the same manner as described above with respect to
The distance d between the prism planes 212 are preferably selected, such that the distance s between adjacent initial out-coupled light beamlets 256′ will be equal to the desired spacings of the final out-coupled light beamlets 256 exiting the primary waveguide apparatus 170. In the illustrated embodiment, the prism planes 212 are oriented at forty-five degree angle to the faces 214a, 214b of the prism body 202, and thus, the distance d can be expressed as a function of the distance s, as follows: d=s*sin 45°. Significantly, the thickness of the waveguide 172 in the primary waveguide apparatus 170 will be multiples of the distance d between the prism planes 212 of the PPE 192e (in this case, two times the distance d between the prism planes 212), such that the in-fill of the final out-coupled light beamlets 256 is facilitated.
It should be appreciated that the because the distance d between the prism planes 212 is set merely by locating the prism planes 212 relative to each other, the spacings between the final out-coupled light beamlets 256 may be arbitrarily set without concern for manufacturing limitations. That is, since the PPE 192e does not utilize an optical substrate between the prism planes 212, but rather utilizes a cavity between the prism planes 212, one need not be concerned with the limitations related to the minimum thickness of such optical substrate.
Referring now to
The mini-waveguide apparatus 220 has a size commensurate with the size of the IC element 168 of the primary waveguide apparatus 170. The mini-waveguide apparatus 220 comprises a plurality of waveguide assemblies 222, and in this case, a top waveguide assembly 222a and a bottom waveguide assembly 222b. Each waveguide assembly 222 is configured for splitting each of one or more collimated beams or beamlets (collimated light beam 250 in the bottom waveguide assembly 222b and out-coupled light beamlets 256′ in the top waveguide assembly 222b) a two-dimensional array (in this case, a 4×4 array) of out-coupled light beamlets 256′, as will be described in further detail below.
In the particular mini-waveguide apparatus 220 described herein, the bottom waveguide assembly 222b functions to split a single collimated light beam 250 into a two-dimensional array of out-coupled light beamlets 256′, whereas the top waveguide assembly 222a functions to split the two-dimensional array of out-coupled light beamlets 256′ from the bottom waveguide assembly 222b into multiple two-dimensional arrays of out-coupled light beamlets 256″, as illustrated in
Referring further to
Each IC element 232 is configured for in-coupling one or more light beams or beamlets into the respective planar optical waveguide 230 for propagation via TIR along an internally reflective optical path (236a in the case of the top orthogonal waveguide unit 226a, and 236b in the case of the bottom orthogonal waveguide unit 226b), and in doing so, repeatedly intersects the EPE element 234. In the same manner as described above with respect to the EPE element 188 of the primary waveguide apparatus 170, the EPE element 234 has a relatively low diffraction efficiency (e.g., less than 50%), such that, at each point of intersection with the EPE element 234, a portion (e.g., greater than 90%) of each light beam or beamlet continues to propagate along the respective internally reflective optical path 236, and the remaining portion of each light beam or beamlet is diffracted as an initial out-coupled light beamlet 256′ that exits the top face 230a of the respective planar optical waveguide 230. In the illustrated embodiment, the sizes of the IC element 232 and EPE element 234 are equal to each other and are commensurate to the size of the respective planar optical waveguide 230 with which the IC element 232 and EPE element 234 are associated, such that pupil expansion of the collimated light beam 250 is maximized, while also facilitating in-coupling of two-dimensional arrays of out-coupled light beamlets 256′ from the bottom orthogonal waveguide unit 226b to the top orthogonal waveguide unit 226a, as will be described in further detail below.
The IC elements 232 of the orthogonal waveguide units 226 are oriented orthogonally to each other, such that each light beam or beamlet (250 or 256′) that is in-coupled into the bottom face 224b of a respective waveguide assembly 222 is split into a two-dimensional array of initial out-coupled light beamlets 256′ (or 256″) that exit the top face 224a of the waveguide assembly 222, as illustrated in
In particular, the IC elements 232 of each waveguide assembly 222 are oriented orthogonally relative to each other, such that the IC element 232 associated with the bottom orthogonal waveguide unit 226b in-couples light for propagation via TIR along an internally reflective optical path parallel to a first axis 262 (in this case, along the y-axis), such that the light is expanded by the corresponding EPE element 234 along the first axis 262 (see
As briefly discussed above with respect to
In particular, with further reference to
That is, the IC element 224 associated with the bottom orthogonal waveguide unit 226b of the bottom waveguide assembly 222b optically couples the collimated light beam 250 as an initial in-coupled light beam 252′ for propagation within the respective planar optical waveguide 230 via TIR along the first internally reflective optical path parallel to the axis 262 (y-axis), and the EPE element 226 associated with the bottom orthogonal waveguide unit 226b of the bottom waveguide assembly 222b splits the collimated light beam 250 into a one-dimensional array of initial out-coupled light beamlets 256′ that exit the top face 228a of the respective bottom orthogonal waveguide unit 226b.
In turn, the IC element 224 associated with the top orthogonal waveguide unit 226a of the bottom waveguide assembly 222b optically couples the one-dimensional array of initial out-coupled light beamlets 256′ as initial orthogonal light beamlets 254′ for propagation within the respective planar optical waveguide 230 via TIR along respective second internally reflective optical paths parallel to the axis 264 (x-axis) that are orthogonal to first internally reflective optical path parallel to the axis 262 (y-axis), and the EPE element 226 associated with the top orthogonal waveguide unit 226a of the bottom waveguide assembly 222b splits the initial orthogonal light beamlets 254′ into a two-dimensional array of initial out-coupled light beamlets 256′ that exit the top face 228a of the respective top orthogonal waveguide unit 226a.
The top waveguide assembly 222a receives the two-dimensional array of initial out-coupled light beamlets 256′ from the bottom waveguide assembly 222b and splits this two-dimensional array of initial out-coupled light beamlets 256′ into a plurality of two-dimensional arrays of intermediate out-coupled light beamlets 256″ that exit the top face 224a of the top waveguide assembly 222a.
That is, the IC element 224 associated with the bottom orthogonal waveguide unit 226b of the top waveguide assembly 222a optically couples the two-dimensional array of initial out-coupled light beamlets 256′ as intermediate sets of in-coupled light beams 252″ for propagation within the respective planar optical waveguide 230 via TIR along the first internally reflective optical path parallel to the axis 262 (y-axis), and the EPE element 226 associated with the bottom orthogonal waveguide unit 226b of the top waveguide assembly 222a splits the intermediate sets of in-coupled light beamlets 252″ into two-dimensional arrays of intermediate out-coupled light beamlets 256″ of initial out-coupled light beamlets 256′ that exit the top face 228a of the respective bottom orthogonal waveguide unit 226b.
In turn, the IC element 224 associated with the top orthogonal waveguide unit 226a of the top waveguide assembly 222a optically couples the two-dimensional arrays of intermediate out-coupled light beamlets 256″ as intermediate orthogonal light beamlets 254″ for propagation within the respective planar optical waveguide 230 via TIR along respective second internally reflective optical paths 264 (x-axis) that are orthogonal to first internally reflective optical path parallel to the axis 262 (y-axis), and the EPE element 226 associated with the top orthogonal waveguide unit 226a of the top waveguide assembly 222a splits the intermediate orthogonal light beamlets 254″ into two-dimensional arrays of intermediate out-coupled light beamlets 256″ that exit the top face 228a of the respective top orthogonal waveguide unit 226a.
Thus, the bottom waveguide assembly 222b splits the collimated light beam 250 into a two-dimensional array of initial out-coupled light beamlets 256′, and the top waveguide assembly 222a splits the two-dimensional array of out-coupled light beamlets 256′ into several two-dimensional arrays of intermediate out-coupled light beamlets 256″. The two-dimensional array of initial out-coupled light beamlets 256′, as well as each of the two-dimensional arrays of intermediate out-coupled light beamlets 256″, have an inter-beamlet spacing s1, and the two-dimensional array of intermediate out-coupled light beamlets 256″ have an inter-array spacing s2 different from the inter-beamlet spacing s1 of the two-dimensional arrays of initial out-coupled light beamlets 256′ and intermediate out-coupled light beamlets 256″ (see, e.g.,
Notably, the inter-beamlet spacing s1 is dictated by the respective thicknesses of the waveguides 230 of the bottom waveguide assembly 222b. Similarly, the inter-array spacing s2 is dictated by the respective thicknesses of the waveguides 240 of the top waveguide assembly 222a. The thicknesses of the waveguides 230 of the top and bottom waveguide assemblies 222 may be strategically selected based on the diameter of the collimated light beam 250. In some examples, the inter-beamlet spacing s1 and inter-array spacing s2, although different from each other, may each be a multiple of the diameter of the collimated light beam 250 to maximize the in-fill of the exit pupil of the PPE 192f.
Thus, the inter-beamlet spacing s1 may be a multiple (“m”) of the diameter of the collimated light beam 250 (“d”), such that s1=m×d. Using this value of s1, the inter-array spacing s2 may be described by: s2 =s1+d. That is, s1 and s2 may be consecutive multiples of the diameter of the collimated light beam 250, such that s2=(m+1)×d. For example, the inter-beamlet spacing s1 may be three times the diameter of the diameter of the collimated light beam 250. Using this value of s1, the inter-array spacing s2 may be four times the diameter of the collimated light beam 250. As exemplified in the illustrated embodiment below, this results in the inter-array spacing s2 being 1.33 times the inter-beamlet spacing s1.
The first and second planar optical waveguide assemblies 222a, 222b respectively have unequal thicknesses t1, t2, as illustrated in
As briefly discussed above, the bottom waveguide assembly 222b splits the collimated light beam 250 into a two-dimensional array of initial out-coupled light beamlets 256′, and the top waveguide assembly 222a splits the two-dimensional array of out-coupled light beamlets 256′ into several two-dimensional arrays of intermediate out-coupled light beamlets 256″. In other words, the bottom waveguide assembly 222b and top waveguide assembly 222a respectively generate two transfer functions that are convolved to produce the desired pattern of intermediate out-coupled light beamlets 252″.
For example, as illustrated in
Referring now to
In particular, the two-dimensional array of intermediate out-coupled light beamlets 256(1)″ is generated directly from the two-dimensional array of initial out-coupled light beamlets 256′ (see
At the second generation, the two-dimensional array of intermediate out-coupled light beamlets 256(2)″ spawns a two-dimensional array of intermediate out-coupled light beamlets 256(4)″ along the x-axis; both the two-dimensional arrays of intermediate out-coupled light beamlets 256(2)″ and 256(3)″ combine to spawn the two-dimensional array of intermediate out-coupled light beamlets 256(5)″ respectively along the x-axis and the y-axis; and the two-dimensional array of intermediate out-coupled light beamlets 256(3)″ spawns a two-dimensional array of intermediate out-coupled light beamlets 256(6)″ along the y-axis (see
At the third generation, the two-dimensional array of intermediate out-coupled light beamlets 256(4)″ spawns a two-dimensional array of intermediate out-coupled light beamlets 256(7)″ along the x-axis; both the two-dimensional arrays of intermediate out-coupled light beamlets 256(4)″ and 256(5)″ combine to spawn the two-dimensional array of intermediate out-coupled light beamlets 256(8)″ respectively along the x-axis and the y-axis; both the two-dimensional arrays of intermediate out-coupled light beamlets 256(5)″ and 256(6)″ combine to spawn the two-dimensional array of intermediate out-coupled light beamlets 256(9)″ respectively along the x-axis and the y-axis; and the two-dimensional array of intermediate out-coupled light beamlets 256(6)″ spawns a two-dimensional array of intermediate out-coupled light beamlets 256(10)″ along the y-axis (see
At the fourth generation, both the two-dimensional arrays of intermediate out-coupled light beamlets 256(7)″ and 256(8)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(11)″ respectively along the x-axis and the y-axis; both the two-dimensional arrays of intermediate out-coupled light beamlets 256(8)″ and 256(8)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(12)″ respectively along the x-axis and the y-axis; and both the two-dimensional arrays of intermediate out-coupled light beamlets 256(9)″ and 256(10)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(13)″ respectively along the x-axis and the y-axis (see
At the fifth generation, both the two-dimensional arrays of intermediate out-coupled light beamlets 256(11)″ and 256(12)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(14)″ respectively along the x-axis and the y-axis; and both the two-dimensional arrays of intermediate out-coupled light beamlets 256(12)″ and 256(13)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(15)″ respectively along the x-axis and the y-axis (see
At the sixth generation, the both the two-dimensional arrays of intermediate out-coupled light beamlets 256(14)″ and 256(15)″ combine to spawn a two-dimensional array of intermediate out-coupled light beamlets 256(16)″ respectively along the x-axis and the y-axis (see
It can be appreciated that all of the intermediate out-coupled light beamlets 256″ designated with a specific letter in the light beamlet pattern illustrated in
It can be appreciated from the foregoing that the PPE 192f two-dimensionally pre-expands the effective entrance pupil of the collimated light beam 250. In the same manner as described above with respect to
It should be noted that, although the multi-layered mini-waveguide apparatus 220 lends itself for use as a PPE 192f, a larger version of the multi-layered waveguide apparatus 220 can be used as the primary waveguide apparatus 170 in order to expand the entrance pupil of a collimated light beam 250 (unexpanded or pre-expanded) in-coupled into the primary waveguide apparatus 170.
While beam multipliers have been described above as OPEs and EPEs, beam multipliers according to the embodiments described herein can be disposed anywhere in an LOE. For instance, beam multipliers described herein can be disposed as a separate multiplication stage/region between various parts of an LOE (e.g., between ICG and OPE). Further, beam multipliers described herein can function as ICGs.
While certain numbers of beams and beamlets are depicted in some of the figures, it should be appreciated that this is for clarity. Each single beam or beamlet depicted in the figures may represent a plurality of beams or beamlets carrying related information and having similar trajectories.
While certain numbers of LOSs and reflective surfaces are depicted in some of the figures, other embodiments may include other combinations of LOSs and reflective surfaces.
The above-described MR systems are provided as examples of various optical systems that can benefit from more selectively reflective optical elements. Accordingly, use of the optical systems described herein is not limited to the disclosed MR systems, but rather applicable to any optical system.
Various exemplary embodiments of the disclosure are described herein. Reference is made to these examples in a non-limiting sense. They are provided to illustrate more broadly applicable aspects of the disclosure. Various changes may be made to the disclosure described and equivalents may be substituted without departing from the true spirit and scope of the disclosure. In addition, many modifications may be made to adapt a particular situation, material, composition of matter, process, process act(s) or step(s) to the objective(s), spirit or scope of the present disclosure. Further, as will be appreciated by those with skill in the art that each of the individual variations described and illustrated herein has discrete components and features which may be readily separated from or combined with the features of any of the other several embodiments without departing from the scope or spirit of the present disclosure. All such modifications are intended to be within the scope of claims associated with this disclosure.
The disclosure includes methods that may be performed using the subject devices. The methods may comprise the act of providing such a suitable device. Such provision may be performed by the end user. In other words, the “providing” act merely requires the end user obtain, access, approach, position, set-up, activate, power-up or otherwise act to provide the requisite device in the subject method. Methods recited herein may be carried out in any order of the recited events which is logically possible, as well as in the recited order of events.
Exemplary aspects of the disclosure, together with details regarding material selection and manufacture have been set forth above. As for other details of the present disclosure, these may be appreciated in connection with the above-referenced patents and publications as well as generally known or appreciated by those with skill in the art. The same may hold true with respect to method-based aspects of the disclosure in terms of additional acts as commonly or logically employed.
In addition, though the disclosure has been described in reference to several examples optionally incorporating various features, the disclosure is not to be limited to that which is described or indicated as contemplated with respect to each variation of the disclosure. Various changes may be made to the disclosure described and equivalents (whether recited herein or not included for the sake of some brevity) may be substituted without departing from the true spirit and scope of the disclosure. In addition, where a range of values is provided, it is understood that every intervening value, between the upper and lower limit of that range and any other stated or intervening value in that stated range, is encompassed within the disclosure.
Also, it is contemplated that any optional feature of the inventive variations described may be set forth and claimed independently, or in combination with any one or more of the features described herein. Reference to a singular item, includes the possibility that there are plural of the same items present. More specifically, as used herein and in claims associated hereto, the singular forms “a,” “an,” “said,” and “the” include plural referents unless the specifically stated otherwise. In other words, use of the articles allow for “at least one” of the subject item in the description above as well as claims associated with this disclosure. It is further noted that such claims may be drafted to exclude any optional element. As such, this statement is intended to serve as antecedent basis for use of such exclusive terminology as “solely,” “only” and the like in connection with the recitation of claim elements, or use of a “negative” limitation.
Without the use of such exclusive terminology, the term “comprising” in claims associated with this disclosure shall allow for the inclusion of any additional element—irrespective of whether a given number of elements are enumerated in such claims, or the addition of a feature could be regarded as transforming the nature of an element set forth in such claims. Except as specifically defined herein, all technical and scientific terms used herein are to be given as broad a commonly understood meaning as possible while maintaining claim validity.
The breadth of the present disclosure is not to be limited to the examples provided and/or the subject specification, but rather only by the scope of claim language associated with this disclosure.
In the foregoing specification, the disclosure has been described with reference to specific embodiments thereof. It will, however, be evident that various modifications and changes may be made thereto without departing from the broader spirit and scope of the disclosure. For example, the above-described process flows are described with reference to a particular ordering of process actions. However, the ordering of many of the described process actions may be changed without affecting the scope or operation of the disclosure. The specification and drawings are, accordingly, to be regarded in an illustrative rather than restrictive sense.
In the foregoing specification, the disclosure has been described with reference to specific embodiments thereof. It will, however, be evident that various modifications and changes may be made thereto without departing from the broader spirit and scope of the disclosure. For example, the above-described process flows are described with reference to a particular ordering of process actions. However, the ordering of many of the described process actions may be changed without affecting the scope or operation of the disclosure. The specification and drawings are, accordingly, to be regarded in an illustrative rather than restrictive sense.
The present application claims priority to U.S. Provisional Application Ser. No. 62/506,841, filed on May 16, 2017 under attorney docket number ML.30110.00 and entitled “SYSTEMS AND METHODS FOR MIXED REALITY,” and U.S. Provisional Application Ser. No. 62/509,499 under attorney docket number ML.30052.00 and filed on May 22, 2017, titled “TECHNIQUE FOR MULTIPLYING BEAMS TO OBTAIN EFFECTIVELY WIDER BEAM IN VIRTUAL/AUGMENTED REALITY SYSTEM.” This application is related to U.S. Utility patent application Ser. No. 15/479,700, filed on Apr. 5, 2017 under attorney docket number ML.20065.00 and entitled “SYSTEMs AND METHODS FOR AUGMENTED REALITY,” U.S. Utility patent application Ser. No. 14/331,218 filed on Jul. 14, 2014 under attorney docket number ML.20020.00 and entitled “PLANAR WAVEGUIDE APPARATUS WITH DIFFRACTION ELEMENT(S) AND SYSTEM EMPLOYING SAME,” U.S. Utility patent application Ser. No. 14/555,585 filed on Nov. 27, 2014 under attorney docket number ML.20011.00 and entitled “VIRTUAL AND AUGMENTED REALITY SYSTEMS AND METHODS,” U.S. Utility patent application Ser. No. 14/726,424 filed on May 29, 2015 under attorney docket number ML.20016.00 and entitled “METHODS AND SYSTEMS FOR VIRTUAL AND AUGMENTED REALITY,” U.S. Utility patent application Ser. No. 14/726,429 filed on May 29, 2015 under attorney docket number ML.20017.00 and entitled “METHODS AND SYSTEMS FOR CREATING FOCAL PLANES IN VIRTUAL AND AUGMENTED REALITY,” and U.S. Utility patent application Ser. No. 14/726,396 filed under on May 29, 2015 under attorney docket number ML.20018.00 and entitled “METHODS AND SYSTEMS FOR DISPLAYING STEREOSCOPY WITH A FREEFORM OPTICAL SYSTEM WITH ADDRESSABLE FOCUS FOR VIRTUAL AND AUGMENTED REALITY.” The contents of the aforementioned patent applications are hereby expressly and fully incorporated by reference in their entirety, as though set forth in full.
| Number | Date | Country | |
|---|---|---|---|
| 62506841 | May 2017 | US | |
| 62509499 | May 2017 | US |
