CA2010434A1 - Direct incorporation of night vision in a helmet mounted display - Google Patents
Direct incorporation of night vision in a helmet mounted displayInfo
- Publication number
- CA2010434A1 CA2010434A1 CA002010434A CA2010434A CA2010434A1 CA 2010434 A1 CA2010434 A1 CA 2010434A1 CA 002010434 A CA002010434 A CA 002010434A CA 2010434 A CA2010434 A CA 2010434A CA 2010434 A1 CA2010434 A1 CA 2010434A1
- Authority
- CA
- Canada
- Prior art keywords
- image
- optical
- lens
- helmet mounted
- helmet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/017—Head mounted
- G02B27/0176—Head mounted characterised by mechanical features
-
- A—HUMAN NECESSITIES
- A42—HEADWEAR
- A42B—HATS; HEAD COVERINGS
- A42B3/00—Helmets; Helmet covers ; Other protective head coverings
- A42B3/04—Parts, details or accessories of helmets
- A42B3/0406—Accessories for helmets
- A42B3/042—Optical devices
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B13/00—Optical objectives specially designed for the purposes specified below
- G02B13/16—Optical objectives specially designed for the purposes specified below for use in conjunction with image converters or intensifiers, or for use with projectors, e.g. objectives for projection TV
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B23/00—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
- G02B23/12—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices with means for image conversion or intensification
- G02B23/125—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices with means for image conversion or intensification head-mounted
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0149—Head-up displays characterised by mechanical features
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/017—Head mounted
- G02B27/0172—Head mounted characterised by optical features
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0101—Head-up displays characterised by optical features
- G02B2027/0138—Head-up displays characterised by optical features comprising image capture systems, e.g. camera
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0149—Head-up displays characterised by mechanical features
- G02B2027/0154—Head-up displays characterised by mechanical features with movable elements
- G02B2027/0156—Head-up displays characterised by mechanical features with movable elements with optionally usable elements
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0149—Head-up displays characterised by mechanical features
- G02B2027/0154—Head-up displays characterised by mechanical features with movable elements
- G02B2027/0159—Head-up displays characterised by mechanical features with movable elements with mechanical means other than scaning means for positioning the whole image
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0179—Display position adjusting means not related to the information to be displayed
- G02B2027/0187—Display position adjusting means not related to the information to be displayed slaved to motion of at least a part of the body of the user, e.g. head, eye
Abstract
Abstract of the Disclosure Direct Incorporation of Night Vision In A Helmet Mounted Display Helmet mounted display apparatus for use in aircraft and rotorcraft includes an first image source for generating images comprising pilotage symbol information, a second image source for sensing and generating images of the exterior scene, and relay optical components that optically superimpose the two images together and subsequently project the superimposed image into the observer's forward field of view.
Description
201~34 Description Direct Incorpora~ion of Night Vision In A Helmet Mounted Display Technical Field This invention relates to helmet mounted display , and more particularly to a helmet mounted display directly incorporating night vision.
Background Art The use of helmet mounted displays (HMDs) in modern high-performance aircraft and rotorcraft is well known. The increasing complexity of these crafts has led to an increased burden on the pilot to visually interpret flight data from a large number of sources. The HMD helps to alleviate this burden by providing in the pilot's forward field of view a display of information essential for the ~ ~-pilot'a performance of such tasks as target acquisition and weapon delivery. The ~MD allows him -~
to spend more time piloting the craft in a head-up ~-mode, i.e., looking out at the exterior scene and not looking down as often at the instrument panel.
The information displayed by the HMD typically consists of symbols relating to pilotage and weapon targeting. This symbol information is fed by the onboard flight computer to a cathode ray tube (CRT~
image source. The CRT image is then projected through a series of optical components, typically - including partially reflective/ partially transmissive optical components located in front of ~ 30 the pilot's eyes. Viewing through the partially transparent components, sometimes referred to as a "combiner", the pilot is presented with a virtual image of the CRT image projected in his view of the exterior "real world" scene.
Depending on the ambient light conditions in ~ ;
which the pilot is flying, different requirements are placed on the optical design of the HMD. For the relatively high brightness daytime light (as compared to nighttime light), the combiner must have high transparency (see-through) since the pilot views the external scene as well as the pro~ected symbol information. Consequently, the display source must have high brightness (e.g., a CRT
written in the stroke mode) so as to produce enough contrast in the projected symbols.
Vision aids are required at night since flying by the "naked eye" is dangerous or impossible. In the prior art, pilots utilize image intensifier devices employed in Night Vision Goggles (NVGs). An advantage of the HMD is that the nighttims viewing function can be accomplished with the HMD optical ~-system. for such use, the external scene may be `~ sensed by, for example, image intensified television or forward looking infrared devices. The output of ~ ;
25 these devices is electronically processed and fed to ~ ~
an image projection source such as a raster mode ~ -CRT. The processing may also include the addition of symbol data to the sensed image of the exterior scene. The rèsulting CRT image is projécted in the pilot's forward field of view through the HMD
pro~ection optical components.
A prob}em with these prior art HMDs arises from " `
the night vision devices being typically mounted on - 2 ~
... ..
gimbal platforms on the aircraft. The sensed image is transmitted to signal processing means in the cockpit that electronically combines the image with the desired symbol data. This electronic processing leads to added complexity and cost in providing for image storage, processing and transmission to the HMD.
A second problem arises with the prior art HMDs that is unique to night vision HMDs. When viewing a sensed image, it is desirable for the apparent image position in space to be properly maintained as the pilot moves his head. ~his feature is most desirable for angular head movements (as opposed to translational head movements). That is, the sensed image should track the head movement. Prior art head tracking systems employ a device attached to the helmet that senses angular head position with respect to an axis aligned with the pilot's forward field of view, and positions the gimbal-mounted night vision devices accordingly. However, a problem inherent in these head tracking devices i the amount of time it take the night vision devices to respond to the movement of the head. This -inherent time lag may be critical in combat ~-situations where the response time of the pilot in activating weapon systems depends on the image presented to him.
Disclosure of Invention An object of the invention is to provide a HMD
having a helmet mounted night vision sensor that senses the external scene and provides a visual image of the scene at an object surface thereof, the visual image being optically superimposed with symbol data from a CRT, the superimposed image being projected in the observer's forward field of view, whereby the resulting HMD avoids the inherent cost, complexity and time lag involved with prior art night vision HMDs.
According to the invention, helmet mounted apparatus for displaying an image in an observer's forward field of view includes a first image source, having an object surface, for generating optical signals indicative of a first visual image thereon, relay optics for projecting the first image along an optical path and into the observer's forward field of view, the relay optics having a predetermined back focus distance along the optical path from the first image source object suxface to a first lens disposed along the optical path, a second image :~
source, having an object surface, for generating ::
optical signals indicative of a second visual image ::
thereon, and a beamsplitter being disposed in the optical path between the first image source object : ~ surface and the first lens to transmit the optical signals indicative of the first image from the first image source to the first lens and being disposed to :
:: 25 reflect the optical signals indicative of the second image into the optical path in a direction toward .
~: the first lens, the direction being equal to the : :~
direction of the optical signals from the first :: ~
image source, the distance from the sedond image ! ~ ~ ' source object surface to the first lens equals the predetermined back focus distance, whereby the :~
spatial disposition of the beamsplitter results in : the superposition of the first and second optical _ 4 _ 20~0434 signals, the superimposed image being projected by the relay optics into the observer's forward field of view.
These and other objects, features and advantages of the present invention will become more apparent in light of the detailed description of a best mode embodiment thereof, as illustrated in the accompanying drawing.
Brief Description of Drawing Fig. 1 illustrates a perspective view of a pilot of a modern high-performance aircraft wearing helmet mounted display apparatus typical of that of the prior art;
Fig. 2 illustrates a perspective view of HMD ;
apparatus;
Fig. 3 is a cross sectional view of a portion of the HMD apparatus;
Fig. 4 illustrates an optical ray trace of HMD
optical components;
Fig. 5 illustrate~ a second optical ray trace of HMD optical components; ;-Fig. 6 illustrates an optical ray trace of an alternative embodiment of HMD optical components;
Fig. 7 illustrates a second optical ray trace of an alternative embodiment of HMD optical components;
Fig. 8 illustrates an optical ray trace of a preferred embodiment of optical components in accordance with the present invention;
Fig. 9 illustrates an optical ray trace of an - alternative embodiment of optical components in accordance with the present invention; and ~ 5 ~
20~0434 :;
Fig. 10 illustrates a perspective view of XMD
apparatus in accordance with the present invention.
Best Mode for Carrying Out the Invention Fig. 1 illustrates a perspective view of an aviator piloting a modern high-performance aircraft while wearing a h~lmet mounted display (HMD) 10 typical of that found in the prior art. In the HMD
10, flight information is viewed through partially transparent optical eyepieces 11,12 located along the pilot's forward line of sight The flight information is provided at the image surface of one ~-or more CRTs (not shown) to a series of optical components (not shown) that relay the image to the eyepieces 11,12. The CRTs and projection optics can all ke~helmet mounted, or some portion of the display co~ponents can be located in the cockpit. -The HMD illustrated in Fig~ 1 is solely for ;~
- daytime light conditions. For low luminance nighttime conditions, the pilot desires an intensified image of the exterior scene so as to ; enable him to pilot the craft to the best of his ability. In this case, the pilot i8 required to remove the entire daytime HMD and replace it with an ;
` ~ ~ entire HMD designed for nighttime light conditions.
~`~ 25 This changeover can be awkward and dangerous when performed during flight. ~ -Fig. 2 illustrates`a perspective view of a preferred embodiment of a HMD 20, in accordance with the invention as disclosed and claimed in a 30 copending U.S. patent application of the same `~
assignee entitled: A HELMET MOUNTED DISPLAY HAVING
6 ;;~
DUAL INTERCHANGEABLE OPTICAL EYEPIECES, U.S. Serial No. (Attorney docket No. H1935GC) fil~d on even date herewith by Fournier, et al. The HMD 20 mounts to the outer surface of a known type aviator's helmet 21, such as the model HGU55 provided by Gentex Corp.
of California. The helmet provides an opening in the outer surface in proximity to the facial area.
The HMD comprises two CRT image sources 22,23 together with a corresponding pair of identical relay optical component arrangements 24,25, one for each eye. Each CRT generates images of pilotage symbol information. The optical component arrangement is described in detail hereinafter with respect to the cross-sectional illustration of Fig.
Background Art The use of helmet mounted displays (HMDs) in modern high-performance aircraft and rotorcraft is well known. The increasing complexity of these crafts has led to an increased burden on the pilot to visually interpret flight data from a large number of sources. The HMD helps to alleviate this burden by providing in the pilot's forward field of view a display of information essential for the ~ ~-pilot'a performance of such tasks as target acquisition and weapon delivery. The ~MD allows him -~
to spend more time piloting the craft in a head-up ~-mode, i.e., looking out at the exterior scene and not looking down as often at the instrument panel.
The information displayed by the HMD typically consists of symbols relating to pilotage and weapon targeting. This symbol information is fed by the onboard flight computer to a cathode ray tube (CRT~
image source. The CRT image is then projected through a series of optical components, typically - including partially reflective/ partially transmissive optical components located in front of ~ 30 the pilot's eyes. Viewing through the partially transparent components, sometimes referred to as a "combiner", the pilot is presented with a virtual image of the CRT image projected in his view of the exterior "real world" scene.
Depending on the ambient light conditions in ~ ;
which the pilot is flying, different requirements are placed on the optical design of the HMD. For the relatively high brightness daytime light (as compared to nighttime light), the combiner must have high transparency (see-through) since the pilot views the external scene as well as the pro~ected symbol information. Consequently, the display source must have high brightness (e.g., a CRT
written in the stroke mode) so as to produce enough contrast in the projected symbols.
Vision aids are required at night since flying by the "naked eye" is dangerous or impossible. In the prior art, pilots utilize image intensifier devices employed in Night Vision Goggles (NVGs). An advantage of the HMD is that the nighttims viewing function can be accomplished with the HMD optical ~-system. for such use, the external scene may be `~ sensed by, for example, image intensified television or forward looking infrared devices. The output of ~ ;
25 these devices is electronically processed and fed to ~ ~
an image projection source such as a raster mode ~ -CRT. The processing may also include the addition of symbol data to the sensed image of the exterior scene. The rèsulting CRT image is projécted in the pilot's forward field of view through the HMD
pro~ection optical components.
A prob}em with these prior art HMDs arises from " `
the night vision devices being typically mounted on - 2 ~
... ..
gimbal platforms on the aircraft. The sensed image is transmitted to signal processing means in the cockpit that electronically combines the image with the desired symbol data. This electronic processing leads to added complexity and cost in providing for image storage, processing and transmission to the HMD.
A second problem arises with the prior art HMDs that is unique to night vision HMDs. When viewing a sensed image, it is desirable for the apparent image position in space to be properly maintained as the pilot moves his head. ~his feature is most desirable for angular head movements (as opposed to translational head movements). That is, the sensed image should track the head movement. Prior art head tracking systems employ a device attached to the helmet that senses angular head position with respect to an axis aligned with the pilot's forward field of view, and positions the gimbal-mounted night vision devices accordingly. However, a problem inherent in these head tracking devices i the amount of time it take the night vision devices to respond to the movement of the head. This -inherent time lag may be critical in combat ~-situations where the response time of the pilot in activating weapon systems depends on the image presented to him.
Disclosure of Invention An object of the invention is to provide a HMD
having a helmet mounted night vision sensor that senses the external scene and provides a visual image of the scene at an object surface thereof, the visual image being optically superimposed with symbol data from a CRT, the superimposed image being projected in the observer's forward field of view, whereby the resulting HMD avoids the inherent cost, complexity and time lag involved with prior art night vision HMDs.
According to the invention, helmet mounted apparatus for displaying an image in an observer's forward field of view includes a first image source, having an object surface, for generating optical signals indicative of a first visual image thereon, relay optics for projecting the first image along an optical path and into the observer's forward field of view, the relay optics having a predetermined back focus distance along the optical path from the first image source object suxface to a first lens disposed along the optical path, a second image :~
source, having an object surface, for generating ::
optical signals indicative of a second visual image ::
thereon, and a beamsplitter being disposed in the optical path between the first image source object : ~ surface and the first lens to transmit the optical signals indicative of the first image from the first image source to the first lens and being disposed to :
:: 25 reflect the optical signals indicative of the second image into the optical path in a direction toward .
~: the first lens, the direction being equal to the : :~
direction of the optical signals from the first :: ~
image source, the distance from the sedond image ! ~ ~ ' source object surface to the first lens equals the predetermined back focus distance, whereby the :~
spatial disposition of the beamsplitter results in : the superposition of the first and second optical _ 4 _ 20~0434 signals, the superimposed image being projected by the relay optics into the observer's forward field of view.
These and other objects, features and advantages of the present invention will become more apparent in light of the detailed description of a best mode embodiment thereof, as illustrated in the accompanying drawing.
Brief Description of Drawing Fig. 1 illustrates a perspective view of a pilot of a modern high-performance aircraft wearing helmet mounted display apparatus typical of that of the prior art;
Fig. 2 illustrates a perspective view of HMD ;
apparatus;
Fig. 3 is a cross sectional view of a portion of the HMD apparatus;
Fig. 4 illustrates an optical ray trace of HMD
optical components;
Fig. 5 illustrate~ a second optical ray trace of HMD optical components; ;-Fig. 6 illustrates an optical ray trace of an alternative embodiment of HMD optical components;
Fig. 7 illustrates a second optical ray trace of an alternative embodiment of HMD optical components;
Fig. 8 illustrates an optical ray trace of a preferred embodiment of optical components in accordance with the present invention;
Fig. 9 illustrates an optical ray trace of an - alternative embodiment of optical components in accordance with the present invention; and ~ 5 ~
20~0434 :;
Fig. 10 illustrates a perspective view of XMD
apparatus in accordance with the present invention.
Best Mode for Carrying Out the Invention Fig. 1 illustrates a perspective view of an aviator piloting a modern high-performance aircraft while wearing a h~lmet mounted display (HMD) 10 typical of that found in the prior art. In the HMD
10, flight information is viewed through partially transparent optical eyepieces 11,12 located along the pilot's forward line of sight The flight information is provided at the image surface of one ~-or more CRTs (not shown) to a series of optical components (not shown) that relay the image to the eyepieces 11,12. The CRTs and projection optics can all ke~helmet mounted, or some portion of the display co~ponents can be located in the cockpit. -The HMD illustrated in Fig~ 1 is solely for ;~
- daytime light conditions. For low luminance nighttime conditions, the pilot desires an intensified image of the exterior scene so as to ; enable him to pilot the craft to the best of his ability. In this case, the pilot i8 required to remove the entire daytime HMD and replace it with an ;
` ~ ~ entire HMD designed for nighttime light conditions.
~`~ 25 This changeover can be awkward and dangerous when performed during flight. ~ -Fig. 2 illustrates`a perspective view of a preferred embodiment of a HMD 20, in accordance with the invention as disclosed and claimed in a 30 copending U.S. patent application of the same `~
assignee entitled: A HELMET MOUNTED DISPLAY HAVING
6 ;;~
DUAL INTERCHANGEABLE OPTICAL EYEPIECES, U.S. Serial No. (Attorney docket No. H1935GC) fil~d on even date herewith by Fournier, et al. The HMD 20 mounts to the outer surface of a known type aviator's helmet 21, such as the model HGU55 provided by Gentex Corp.
of California. The helmet provides an opening in the outer surface in proximity to the facial area.
The HMD comprises two CRT image sources 22,23 together with a corresponding pair of identical relay optical component arrangements 24,25, one for each eye. Each CRT generates images of pilotage symbol information. The optical component arrangement is described in detail hereinafter with respect to the cross-sectional illustration of Fig.
3, and the optical ray diagrams of Figs. 4,5.
Each arrangement 24,25 comprises, in part, a "relay optic" portion 24a,25a having optical - components (not visible) enclosed in aluminum and used in both day and night HMD configurations. Each arrangement also comprises a daytime "eyepiece"
portion 24b,25b having optical components optimized for daytime light conditions, and a nighttime eyepiece (not shown) 24c,25c having optical components optimized for nighttime light conditions. ~
25 The daytime eyepieces 24b,25b mount in a first ;
interchangeable binocular goggle assembly 28a, and the nighttime eyepieces 24c,25c mount in a second interchangeable binocular goggle assembly 28b (not shown). It is to be understood that the goggle assemblies 28a,28b are similar in structure; the difference lies in the optical components comprising the eyepiece portions as described in detall hereinafter with respect to Figs. 4,5 and Tables I,II. Fig 2 illustrates the HMD with the goggle assembly 28a separated from the helmet 2'.
The goggle assembly mates with each relay optic portion 24a,25a by engagement slides 29,30. A known type, first ball detent 31 holds the goggle asse~bly to a mounting block 32 on the front of the HMD. The ball detent 31 and engagement slides 29,30 allow the pilot to quickly remove the goggle assembly from the helmet. The front mounting block 32 attaches to the front of the helmet using either a fixed screw mount or a second ball detent 33. A first rod 34 connects the two relay optic portions together. The rod 34 engages a hook 35 on the crown of the helmet. The second ball detent 33 and rod/hook 34/35 permit the pilot to quickly disengage the entire HMD 20 from the helmet 21.
A second rod 36 passes through the front mounting block 32 and connects to the two relay optic portions. The first and second rods 34,36 permit the relay optic portions to slide horizontally, thereby allowing the pilot to align ~'' ; 'the two relay optic portions for his particular eye spacing. This eye spacing is commonly referred to ;~
as the interpupillary distance (IPD). The second rod 36 has a knob (not shown) at one end to '~ faciIitate the IPD adjustment through a range of 58.9 - 73.3 mm, which is suitable for a wide ranga /' ~;
of pilot head sizes.
'In'order'to aliow IPD adjustment,'the optical 30 components of the eyepieces 24b,25b are mounted in ; ~ '~
segmented portions 39a,39b of the goggle assembly 28. The segmented portions 39a,39b slide relative to one another when a retaining screw 40 is . ~, . ~,.
loosened. Thus, to adjust the IPD, the pilot loosen~ the retaining screw 40 and adjusts the knob on the second rod 36 until the IPD is correct for his particular eye spacing. Then the pilot retightens the retaining screw.
Fig. 3 is a cross-sectional view of either one of the optical component arrangements 24,25. The CRT 22 presents a visual image of flight information on a plano concave fiber optic faceplate 41 that is a part of the CRT. The CRT is typically a Model H-1380, one inch diameter, miniature CRT provided by ~ughes Aircraft Company, Industrial Products Division, Carlsbad, California. The CRT drive electronics (not shown) are well known and are located in the aircraft cockpit. The drive electronics can operate the CRT in either the stroke (high brightness) mode or raster mode. The CRT
image information is presented to the drive electronics by the on-board flight computer. The drive electronics connect to the CRT by a shielded electrical cable 42. The CRT 22 attaches to the relay optic portion 24a by means of a flange 43 secured with adhesive to the CRT and a nut assémbly ~ -~
44 which mates with threads 45 on the relay optic 25 portion. This attachment point is located at an -entrance aperture 46a of the relay optic portion, as illustrated by the split line 46.
Proceeding along an optical axis 50, a pair of glass optical lenses 53,54 are positioned after the CRT faceplate 41. The first lens 53 is positioned with a machined seat 55. The second lèns 54 rests against the first lens. A first tubular spacer 56 follows the second lens, followed by a third lens : .
-,, ,,-: ~
_ g _ ~ .:
zo~oat34 58, a second tubular spacer 59, and a second pair of lenses 61,62. The two lenses comprising each of the first and second lens pairs are normally positioned next to each other and are made of different types of glass or plastic material so as to reduce chromatic abberrations.
A split line 63 designates a physical break in the relay optic portion; the segment to the left of the split line 63 is either press-fitted or secured with adhesive into the segment to the right of the split line. A lens retaining nut 64 is positioned to hold the lenses 53,54,58,61,62 and spacers 56,59 in place.
Attached to a back surface 65 is a fold mirror 66 which is used to direct (fold) the optical axis 50 downward in the relay optic portion. The mirror 66 is attached using conventional optical component mounting techniques known in the art so as to provide a low stress mount. A sixth lens 69 i8 positioned by a second lens retaining nut 70. The relay optic portion then physically terminates at a split line 72. The split line can also considered illustrative of the location of an intermediate image focal plane 72a of the relay optic portion, ~ and of an input aperture 72b of the eyepiece.
Located underneath the split line 72 is a first eyepiece lens 74 positioned against a machined seat 75a with a retaining nut 75b. Also contained in the eyepiece is a combiner 76 and a beamsplitter 77.
The beamsplitter 77 is held in place with clips 78a, 78b. The optical axis is illustrated as terminating ~ -at a focal point 79 at the observer's eye (i.e., with an observer wearing the HMD). It is to be , ' ." .': ,~
.'..
- 10 - ~ ' ;' ''' 20~0434 understood that the optical components comprising the nighttime eyepiece 25c are positioned inside the eyepiece with similar types of machined seats and retainer nuts.
Fig. 4 illustrates an optical ray trace of a preferred embodiment of the projection optical components. The relay optic portion components are above the split line 72, while the components of the daytime eyepiece 24b are below the split line.
Also, surfaces and inter-component spacings sf each component are enumerated in Fig. 4.
~, TABLE I
- ., .-.
Surface RadiusCurve Thick/ Mat'l No. (mm~ TypeDist (mm) __ 8440.000000 CV61.863200 AIR
8535.488000 CX3.000000 ~ F4 8621.770000 CV1.792300 AIR
8733.991000 CX6.000000 SI02 ~ -~- 8885.875000 CX21.905600 AIR - ~-89201.985000 CV5.500000 SI02 -~
9024.6}7000 CX5.209200 AIR
91175.000000 CX4.500000 SI02 9254.941000 CX1.433000 AIR
9330.044000 CV3.000000 F4 ~ : -94384.855000 CX34.294000 AIR
~ 95 -- --19.000000 AIR . '~
--~; 96221.803000 CV5.000000 SI02 -~
9774.673000 CX81.356900 AIR - ~
982000.000000 CX5.000000 ACRYL ~`
99221.803000 CV33.643100 AIR
00 ! . ~ 1 ` ' - - 34.801353~ AIR
101128.165000 CV35.941353 AIR
100 -- --3.000000 ACRYL 6 102 -- --51.420000 AIR
35 103 -- __ _~
- -~ : .
-- 1 1 -- : :~
Z01043(~
Table I lists the prescription data for the optical components. Listed in order from left to right are (1) the surface number, (2) the radius of -curvature in mm, (3) the type of curvature (CV =
concave; CX = convex), (4) the distance to the next surface or thickness in mm, and (5) the type of material between the surface and the next surface.
The type and radius of curvatures of the optical components are chosen in part to control astigmatism and spherical aberrations.
Thus, referring to Fig. 4 and Table I, the ~ -~
image produced by the CRT is presented on an outer surface 84 of the plano concave (CV) fiber optic ~-faceplate 41 having a radius of curvature of 40 mm.
The faceplate is located approximately at an entrance pupil 46a of the relay optic portion. The -~-optical rays then travel through air a distance of ~ I
61.8632 mm to a first surface 85 of the first glass lens 53. All distances listed in Table I are mea~ured from the centers of each component. The - first surface 85 of the first lens has a convex shape and a radius of curvature of 35.488 mm. Also, the lens is 3.0 mm thick and is made of F4 glass.
The physical characteristics and spatial disposition of the remaining optical components are determined from Fig. 4 and Table I in a similar manner.
It is to be noted that surface 95 is that of the fold mirror, whose surface comprises an alumihized reflective coating. Also, surface 100 is listed twice in Table I in accord with the path taken by the light which is first reflected from partially reflective surface 100 to surface 101, then reflected from partially reflective surface 101 ,~
.
back toward the eye, passing through the beamsplitter defined by surfaces 100 and 102. The first listing indicates a 34.801353 mm ray travel distance to surface 101, whereas the second listing indicatec a beamsplitter thickness of 3 mm. Al~o, surface 103 indicates the exit pupil of the optical rays. The exit pupil is approximately 8 mm in diameter.
The relay optics are designed to produce a focused CRT image at the point in the optical path in proximity to the intermediate image focal plane 72a. The focused image has a magnification range of 0.5 - 4 of the image at the CRT faceplate 41. The focused image at the focal plane is at a distance of -~
15 100 - 400 mm (i.e., the focal length of the relay optics) along the optical path 50 from the faceplate.
`~ The daytime eyepiece essentially creates a virtual image, in the observer's forward field of view, of the focused image at the focal plane. This virtual image is focused at a distance from the observer's eye of from one meter to infinity, which results in the image appearing in focus to the eye of the observer. Thus, the observer does not have -;
to refocus his eyes to view the image generated by ~- the CRT that is superimposed on the observer's view of the external terrain. The virtual image occupies a portion of the observer's visual field having a mihimum subtense at'the~eye of ten (10)~ degrees.
The focal length of the eyepiece is approximately 100 mm, resulting in an overall optical path length from the faceplate to the eye of 200 - 400 mm.
The CRT faceplate is shown with 19 mm diameter which is the active image area of the miniature CRT.
The lens diameters are chosen to contain the rays with margin to permit retention in the relay optic portions. The lenses comprising the relay optic portion are all glass: either F4 or fused silica (SI02). The eyepiece components are all acrylic plastic. Plastic elements were chosen for weight and safety rsasons. However, it is to be understood that the eyepiece lenses can be glass if so desired.
All components other than the folding mirror 66 have a known antireflective coating. In addition, ~ -the coatings on the surface 101 of the combiner 76 and the surface 100 of the beamsplitter 77 are -~
adjusted for a reflectivity of 20%-60% (40% -preferred) for visible light in the wavelength range of 400 - 700 nanometers. The resulting partial transmissivity of the beamsplitter and combiner allow the observer to view external scenes disposed ~,, .
20 beyond the daytime eyepiece. The day eyepiece can ~-be termed catadioptric due to the use of partially transmissive/ partially reflective optical components. Each optical element in Fig. 4 can be built from the prescription data of Table I using known techniques.
; Fig. 5 illustrates an optical ray trace of the optical components comprising the nighttime eyepiece 24c. Table II lists the corresponding prescription data. Since~the hous`ing portion components are the same as those illustrated in Fig. 4, the entries in Table II for surfaces 84-96 are similar to those in Table I. Note that surface 114 of component 114a is an aluminized reflective surface which totally ' reflects the optical rays and blocks transmission of ~ -optical rays of the external scene disposed beyond the night eyepiece. Thus, component 114a is ~ -essentially opaque. Also, the image projected into 5 the observer's forward field of view occupies an angle in the observer's forward field of view having a minimum subtense of twenty (20) degrees.
TA~LE II
~. ~
SurfaceRadius CurveThick/ Mat'l 10 No. (mm~ TypeDist ~mm) 8440.000000 CV61.863200 AIR
8535.488000 CX3.000000 F4 8621.770000 CV1.792300 AIR
8733.991000 CX6.000000 SI02 15 8885.875000 CX21.905600 AIR
89201.985000 CV5.500000 SIO2 9024.617000 CX5.209200 AIR ~, -91175.000000 CX4.500000 SI02 ~ , 9254.941000 CX1.433000 AlR
20 9330.044000 CV3.000000 F4 -94384.855000 CX34.294000 AIR
-- --19.000000 AIR
96221.803000 CV5.000000 SI02 ~-9774.673000 CX93.000000 AIR
25 }121863.457201 CX7.000000 ACRYL
11339.515000 CX21.000000 AIR
114 -- --20.500000 AIR
115 -- --4.000000 ACRYL
-~ 11683.478000 CX0.500000 AIR
30 11739.515000 CX4.500000 ACRYL
118 -- --25.000000 AIR
103 -- -- __ __ , I : , Fig. 6 illustrates an optical ray trace of an alternative embodiment of a hou~ing portion 120a and a daytime eyepiece portion 120b of optical components. The housing and eyepiece portions are 20~0434 separated at a split line 123. Table III list the corresponding prescription data. Fig. 7 illustrates the alternative embodiment nighttime eyepiece 120c.
Table IV list the corresponding prescription data.
The alternative embodiments are comprised entirely of conventional plastic optical elements. It should be noted that the alternative embodiment~
illustrated have a longer optical path length than the preferred embodiment~ of Figs. 4,S. This requires the CRTs 22,23 and a portion of the relay optic components to be mounted on the back side of the helmet 21 for best fit to the outer surface of the helmet.
~ , , TABLE III
15~urfaceRadius Curve Thick/ Nat~l No. (mm) Ty~e Dist (mm) ~- 84 40.000000 CV42.360000 AIR
130 149.880000 CX 3.000000 POLYC
131 53.660000 CV18.418400 AIR
20132 110.449000 CX 7.000000 ACRYL
133 57.279000 CX21.000000 AIR
- 134 -- -- 43.000000 AIR
- 135 316.793000 CX 4.000000 ACRYL
}36 316.793000 CX69.000000 AIR
25137 163.725000 CX 7.000000 ACRYL
138 42.692000 CX 0.000000 AIR
139 42.692000 CV -2.000000 POLYC
- 140 135.158000 CX130.000000 AIR
141 -- -- 76.000000 AIR
30142 65.596000 CV 4.20000q ACRYL
143 55.139000 CX64.000000 AIR
144 -- -- 25.300000 AIR ~`
145 135.158000 CV26.500000 AIR
144 -- -- 3.000000 ACRYL
35146 -- -- 47.000000 AIR
:
, 20~0434 TABLE IV :~ :
Surface Radius Curve Thick/ Mat'l No. ~mm~ Type Dist lmm) 8440.000000 CV 42.360000 AIR
130149.880000 CX 3.000000 POLYC
13153.660000 CV18.418400 AIR : -132110.449000 CX 7.000000 ACRYL ~ .
13357.279000 CX21.000000 AIR
134 -- -- 43.000000 AIR
135316.793000 CX 4.000000 ACRYL
136316.793000 CX69.000000 AIR ~ -137163.725000 CX 7.000000 ACRYL
13842.692000 CX o.ooooo0 AIR ~ ~ :
13942.692000 CV 2.000000 POLYC ~ -140135.158000 CX130.000000 AIR ::
141 -- -- 114.000000 AIR
17384.312000 CX 8.000000 POLYC ~ : : -17484.312000 CX23.000000 AIR
175 -- -- 21.000000 AIR
17634.836000 CX 5.000000 ACRYL
~ 177 -- -- 24.000000 AIR
: : 103 -- ---_ __ The preferred embodiment of the daytime optical components provide for data display in a 30-35 - 25 degree monocular field of view with 36% see-through luminance transmission, and approximately 6%
: luminance transfer from the CRT (60% beamsplitter.
transmission, 60% combiner transmission). The nighttime optical components provide for 30 ~ approximately 40 degree monocular field of view with no combiner see-through. The HMD is designed for ~-binocular viewing using two eyepieces with 100%
overlap of the left and right visual fields. Also, the optics are designed to accomodate a CRT image :~
source having an active image diameter in the range of 16 - 25 mm, with the~projection optical lenses 17 ~ ~
`.: ~ - :
20~0434 ~ ~
having an effective focal length in the range of 15 ~' - 55 mm.
The discussion thus far is directed to an HMD
having interchangeable eyepieces, as disclosed in the aforementioned copending U.S. patent application to Fournier et al. It is to be understood that the -present invention can be adapted to utilize concepts disclosed therein to achieve the objectives of the present invention without departing from the scope thereof.
F1g. 8 illustrates an optical ray trace of a preferred embodiment of the present invention.
Illustrated are the optical components comprising the relay optic portion 24a of Fig. 4 together with lS the nighttime eyepiece 24c of Fig. 5, and including the opt~cal components in accordance with the -~ presant invention. A visual image comprised of optical signals is provided on an object surface 200 - of an image source 201, such as a known type image ~20 inten~ifier device. The optical signals emanating from the ob~ect surface proceed to encounter a reflecting optical component (mirror) 204 which is disposed~to present the optical signals to a beamsplitter 206. Ths beamsplitter 206 is disposed in the optical path 50 both to reflect the optical ignals emanating from the image intensifier ob~ect surface 200, and to transmit the optical signals from the faceplate 41. The image intensifier optical signals are reflected by surface 208 of the beamsplitter, the surface being coated with a suitable known type optical coating so as to achieve a reflectivity of from 80 - 95%. This high reflectivity is desired because the luminance of the ~
: - ::.
image on the image intensifier object surface is typically much lower than the luminance of the image on the CRT faceplate (1~ or less). Consequently, -the transmissivity of the beamsplitter surface 208 is approximately 5 - 20% (i.e., 20~ of the optical signals from the faceplate 41 are transmitted through the beamsplitter).
The disposition of the beamsplitter in the optical path is such that the image intensifier optical signals are directed along the optical path 50 towards the surface 85 of the first lens 53 in the same direction as the optical signals from the faceplate. The result is that the image from the CRT faceplate is superimposed on the image from the image intensifer. (Note the Fig. 8 illustrates the path of the optical rays from the image intensifer ob~ect surface through the eyepiece only; not shown are the optical rays from the CRT faceplate). The superimposed image is then transferred by the relay optic portion and the eyepiece into the observer's ..
forward field of view.
However, in order to achieve proper superposition of the two images, the optical path length from the image intensifier object surface 200 to the surface 85 of the first lens 53 must equal the optical path length from the faceplate 41 to the surface 85 of the first lens 53. This distance is referred to as the back focus distance, which, from Table I, equals 61.863200 mm for the preferred embodiment of Fig. 8. Also, because the beamsplitter 206 is disposed in the optical path 50 at a point where the optical signals are not collimated, the beamsplitter is required to be thin , ~...-~-~, -19- ~ ~ ~
2010a~34 (less than 1 mm thick) so as to reduce astigmatism.
If a thicker beamsplitter were employed, additional lenses would be required to correct the aberrations.
Such additional lenses add an undersirable weight to the overall HMD. The thin beamsplitter can either be made of quartz or be that of a pellicle type consisting of a coated membrane supported on a frame. The pellicle beamsplitter effectively has zero optical thickness, and, thus, does not distort transmitted images.
Fig. 9 illustrates an alternative embodiment of the present invention comprising the all plastic optical component design of the relay optic portion of Fig. 6 together with the nighttime eyepiece of Fig. 7, and including the optical components in accordance with the present invention. Note that the all plastic alternative embodiment necessitates additional lenses in the optical path from the image - -intensifier object surface 200 to the beamsplitter 206. Table V lists the corresponding prescription data for the optical component surfaces from the image intensifier object surface 200 through surface 137. The remaining surfaces in the optical path are listed in Table IV. As with the preferred embodiment of Fig. 8, the optical path distance from the image intensifier object surface 200 to the lens surface 137 equals the optical path distance from the CRT faceplate 41 to the lens surface 137.
Z0~0434 - - ~
TABLE V
Surface RadiusCurve Thick/ Mat'l No. (mm) TypeDist ~mml 20040.000000 CV43.208237 AIR
220149.880000 CX3.000000 POLYC
22153.660000 CV18.472773 AIR
222110.449000 CX7.000000 ACRYL
22357.279000 CX24.000000 AIR
224 -- --33.000000 AIR
225316.793000 CX4.000000 ACRYL
226316.793000 CX33.000000 AIR
208 -- --36.000000 AIR
Fig. 10 illustrates a perspective view of a HMD
with a pair of identical image intensifier devices 201 mounted on the helmet 21 in accordance with the present invention. Fig. 10 is essentially a replicate of Fig. 2 with the addition of the image intensifier devices mounted on the helmet. Each image intensifier has a sensing surface 240,241 on ~` 20 ~ the~front of the device that senses the external scene. Each image intensifier processes the sensed scene and presents an image of it on the respective ;~
object surface 200 (not visible) of each device.
The image from the each image intensifier device is " ~; 25 ~ superimposed together with the image from the respective CRT 22,23 by the the corresponding mirror 204 and beamsplitter 206 (not visible)~ That is, each image intensifier has an identical mirror 204 and identical beamsplitter 206 disposed after its ob~ect surface for presenting the image into the respective relay optic portion 24a,24b. Each mirrorjbeamsplitter pair is enclosed in a separate - 21 ~
20~0434 aluminum housing portion 243,244 in a similar fashion as that of the optical components illustrated in Fig. 3 (i.e., with suitable machined seats).
In operation, the pilot dons the HMD having the image intensifier devices incorporated directly on the helmet in accordance with the present invention.
The pilot also attaches the night eyepiece to the HMD. Then, during flight, the exterior scene i8 sensed by the image intensifier devices and the image provided by these devices is superimposed with an image of symbol pilotage data provided by each CRT. The resulting superimposed image is pro~ected into the pilot's forward field of view by the relay optic portion and the nighttime eyepiece. There is no inherent time lag in this type of night vision HMD from the time the pilot moves his head angularly to the time the proper image of the external scene i8 presented to the pilot's forward field of view.
The present invention also lacks the complexity and cost of prior art night vision HMDs.
. ~
A binocular HMD has been illustrated herein incorporating two identical image intensifying ~; devices together with relay optic portions and eyepieces. However, it is to be understood that a monocular HMD can be implemented employing a single image intensifying device together with a single relay optic portion and eyepiece without departing from!the scope of the present invention. ! ' :
Although the invention has been shown and described with respect to a best mode embodiment thereof, it should be understood by those skilled in the art that the foregoing and various other changes, omissions, and additions in the form and detail thereof may be made therein without departing from the spirit and scope of the invention.
~.
~ - 23 -. ~ . . ,
Each arrangement 24,25 comprises, in part, a "relay optic" portion 24a,25a having optical - components (not visible) enclosed in aluminum and used in both day and night HMD configurations. Each arrangement also comprises a daytime "eyepiece"
portion 24b,25b having optical components optimized for daytime light conditions, and a nighttime eyepiece (not shown) 24c,25c having optical components optimized for nighttime light conditions. ~
25 The daytime eyepieces 24b,25b mount in a first ;
interchangeable binocular goggle assembly 28a, and the nighttime eyepieces 24c,25c mount in a second interchangeable binocular goggle assembly 28b (not shown). It is to be understood that the goggle assemblies 28a,28b are similar in structure; the difference lies in the optical components comprising the eyepiece portions as described in detall hereinafter with respect to Figs. 4,5 and Tables I,II. Fig 2 illustrates the HMD with the goggle assembly 28a separated from the helmet 2'.
The goggle assembly mates with each relay optic portion 24a,25a by engagement slides 29,30. A known type, first ball detent 31 holds the goggle asse~bly to a mounting block 32 on the front of the HMD. The ball detent 31 and engagement slides 29,30 allow the pilot to quickly remove the goggle assembly from the helmet. The front mounting block 32 attaches to the front of the helmet using either a fixed screw mount or a second ball detent 33. A first rod 34 connects the two relay optic portions together. The rod 34 engages a hook 35 on the crown of the helmet. The second ball detent 33 and rod/hook 34/35 permit the pilot to quickly disengage the entire HMD 20 from the helmet 21.
A second rod 36 passes through the front mounting block 32 and connects to the two relay optic portions. The first and second rods 34,36 permit the relay optic portions to slide horizontally, thereby allowing the pilot to align ~'' ; 'the two relay optic portions for his particular eye spacing. This eye spacing is commonly referred to ;~
as the interpupillary distance (IPD). The second rod 36 has a knob (not shown) at one end to '~ faciIitate the IPD adjustment through a range of 58.9 - 73.3 mm, which is suitable for a wide ranga /' ~;
of pilot head sizes.
'In'order'to aliow IPD adjustment,'the optical 30 components of the eyepieces 24b,25b are mounted in ; ~ '~
segmented portions 39a,39b of the goggle assembly 28. The segmented portions 39a,39b slide relative to one another when a retaining screw 40 is . ~, . ~,.
loosened. Thus, to adjust the IPD, the pilot loosen~ the retaining screw 40 and adjusts the knob on the second rod 36 until the IPD is correct for his particular eye spacing. Then the pilot retightens the retaining screw.
Fig. 3 is a cross-sectional view of either one of the optical component arrangements 24,25. The CRT 22 presents a visual image of flight information on a plano concave fiber optic faceplate 41 that is a part of the CRT. The CRT is typically a Model H-1380, one inch diameter, miniature CRT provided by ~ughes Aircraft Company, Industrial Products Division, Carlsbad, California. The CRT drive electronics (not shown) are well known and are located in the aircraft cockpit. The drive electronics can operate the CRT in either the stroke (high brightness) mode or raster mode. The CRT
image information is presented to the drive electronics by the on-board flight computer. The drive electronics connect to the CRT by a shielded electrical cable 42. The CRT 22 attaches to the relay optic portion 24a by means of a flange 43 secured with adhesive to the CRT and a nut assémbly ~ -~
44 which mates with threads 45 on the relay optic 25 portion. This attachment point is located at an -entrance aperture 46a of the relay optic portion, as illustrated by the split line 46.
Proceeding along an optical axis 50, a pair of glass optical lenses 53,54 are positioned after the CRT faceplate 41. The first lens 53 is positioned with a machined seat 55. The second lèns 54 rests against the first lens. A first tubular spacer 56 follows the second lens, followed by a third lens : .
-,, ,,-: ~
_ g _ ~ .:
zo~oat34 58, a second tubular spacer 59, and a second pair of lenses 61,62. The two lenses comprising each of the first and second lens pairs are normally positioned next to each other and are made of different types of glass or plastic material so as to reduce chromatic abberrations.
A split line 63 designates a physical break in the relay optic portion; the segment to the left of the split line 63 is either press-fitted or secured with adhesive into the segment to the right of the split line. A lens retaining nut 64 is positioned to hold the lenses 53,54,58,61,62 and spacers 56,59 in place.
Attached to a back surface 65 is a fold mirror 66 which is used to direct (fold) the optical axis 50 downward in the relay optic portion. The mirror 66 is attached using conventional optical component mounting techniques known in the art so as to provide a low stress mount. A sixth lens 69 i8 positioned by a second lens retaining nut 70. The relay optic portion then physically terminates at a split line 72. The split line can also considered illustrative of the location of an intermediate image focal plane 72a of the relay optic portion, ~ and of an input aperture 72b of the eyepiece.
Located underneath the split line 72 is a first eyepiece lens 74 positioned against a machined seat 75a with a retaining nut 75b. Also contained in the eyepiece is a combiner 76 and a beamsplitter 77.
The beamsplitter 77 is held in place with clips 78a, 78b. The optical axis is illustrated as terminating ~ -at a focal point 79 at the observer's eye (i.e., with an observer wearing the HMD). It is to be , ' ." .': ,~
.'..
- 10 - ~ ' ;' ''' 20~0434 understood that the optical components comprising the nighttime eyepiece 25c are positioned inside the eyepiece with similar types of machined seats and retainer nuts.
Fig. 4 illustrates an optical ray trace of a preferred embodiment of the projection optical components. The relay optic portion components are above the split line 72, while the components of the daytime eyepiece 24b are below the split line.
Also, surfaces and inter-component spacings sf each component are enumerated in Fig. 4.
~, TABLE I
- ., .-.
Surface RadiusCurve Thick/ Mat'l No. (mm~ TypeDist (mm) __ 8440.000000 CV61.863200 AIR
8535.488000 CX3.000000 ~ F4 8621.770000 CV1.792300 AIR
8733.991000 CX6.000000 SI02 ~ -~- 8885.875000 CX21.905600 AIR - ~-89201.985000 CV5.500000 SI02 -~
9024.6}7000 CX5.209200 AIR
91175.000000 CX4.500000 SI02 9254.941000 CX1.433000 AIR
9330.044000 CV3.000000 F4 ~ : -94384.855000 CX34.294000 AIR
~ 95 -- --19.000000 AIR . '~
--~; 96221.803000 CV5.000000 SI02 -~
9774.673000 CX81.356900 AIR - ~
982000.000000 CX5.000000 ACRYL ~`
99221.803000 CV33.643100 AIR
00 ! . ~ 1 ` ' - - 34.801353~ AIR
101128.165000 CV35.941353 AIR
100 -- --3.000000 ACRYL 6 102 -- --51.420000 AIR
35 103 -- __ _~
- -~ : .
-- 1 1 -- : :~
Z01043(~
Table I lists the prescription data for the optical components. Listed in order from left to right are (1) the surface number, (2) the radius of -curvature in mm, (3) the type of curvature (CV =
concave; CX = convex), (4) the distance to the next surface or thickness in mm, and (5) the type of material between the surface and the next surface.
The type and radius of curvatures of the optical components are chosen in part to control astigmatism and spherical aberrations.
Thus, referring to Fig. 4 and Table I, the ~ -~
image produced by the CRT is presented on an outer surface 84 of the plano concave (CV) fiber optic ~-faceplate 41 having a radius of curvature of 40 mm.
The faceplate is located approximately at an entrance pupil 46a of the relay optic portion. The -~-optical rays then travel through air a distance of ~ I
61.8632 mm to a first surface 85 of the first glass lens 53. All distances listed in Table I are mea~ured from the centers of each component. The - first surface 85 of the first lens has a convex shape and a radius of curvature of 35.488 mm. Also, the lens is 3.0 mm thick and is made of F4 glass.
The physical characteristics and spatial disposition of the remaining optical components are determined from Fig. 4 and Table I in a similar manner.
It is to be noted that surface 95 is that of the fold mirror, whose surface comprises an alumihized reflective coating. Also, surface 100 is listed twice in Table I in accord with the path taken by the light which is first reflected from partially reflective surface 100 to surface 101, then reflected from partially reflective surface 101 ,~
.
back toward the eye, passing through the beamsplitter defined by surfaces 100 and 102. The first listing indicates a 34.801353 mm ray travel distance to surface 101, whereas the second listing indicatec a beamsplitter thickness of 3 mm. Al~o, surface 103 indicates the exit pupil of the optical rays. The exit pupil is approximately 8 mm in diameter.
The relay optics are designed to produce a focused CRT image at the point in the optical path in proximity to the intermediate image focal plane 72a. The focused image has a magnification range of 0.5 - 4 of the image at the CRT faceplate 41. The focused image at the focal plane is at a distance of -~
15 100 - 400 mm (i.e., the focal length of the relay optics) along the optical path 50 from the faceplate.
`~ The daytime eyepiece essentially creates a virtual image, in the observer's forward field of view, of the focused image at the focal plane. This virtual image is focused at a distance from the observer's eye of from one meter to infinity, which results in the image appearing in focus to the eye of the observer. Thus, the observer does not have -;
to refocus his eyes to view the image generated by ~- the CRT that is superimposed on the observer's view of the external terrain. The virtual image occupies a portion of the observer's visual field having a mihimum subtense at'the~eye of ten (10)~ degrees.
The focal length of the eyepiece is approximately 100 mm, resulting in an overall optical path length from the faceplate to the eye of 200 - 400 mm.
The CRT faceplate is shown with 19 mm diameter which is the active image area of the miniature CRT.
The lens diameters are chosen to contain the rays with margin to permit retention in the relay optic portions. The lenses comprising the relay optic portion are all glass: either F4 or fused silica (SI02). The eyepiece components are all acrylic plastic. Plastic elements were chosen for weight and safety rsasons. However, it is to be understood that the eyepiece lenses can be glass if so desired.
All components other than the folding mirror 66 have a known antireflective coating. In addition, ~ -the coatings on the surface 101 of the combiner 76 and the surface 100 of the beamsplitter 77 are -~
adjusted for a reflectivity of 20%-60% (40% -preferred) for visible light in the wavelength range of 400 - 700 nanometers. The resulting partial transmissivity of the beamsplitter and combiner allow the observer to view external scenes disposed ~,, .
20 beyond the daytime eyepiece. The day eyepiece can ~-be termed catadioptric due to the use of partially transmissive/ partially reflective optical components. Each optical element in Fig. 4 can be built from the prescription data of Table I using known techniques.
; Fig. 5 illustrates an optical ray trace of the optical components comprising the nighttime eyepiece 24c. Table II lists the corresponding prescription data. Since~the hous`ing portion components are the same as those illustrated in Fig. 4, the entries in Table II for surfaces 84-96 are similar to those in Table I. Note that surface 114 of component 114a is an aluminized reflective surface which totally ' reflects the optical rays and blocks transmission of ~ -optical rays of the external scene disposed beyond the night eyepiece. Thus, component 114a is ~ -essentially opaque. Also, the image projected into 5 the observer's forward field of view occupies an angle in the observer's forward field of view having a minimum subtense of twenty (20) degrees.
TA~LE II
~. ~
SurfaceRadius CurveThick/ Mat'l 10 No. (mm~ TypeDist ~mm) 8440.000000 CV61.863200 AIR
8535.488000 CX3.000000 F4 8621.770000 CV1.792300 AIR
8733.991000 CX6.000000 SI02 15 8885.875000 CX21.905600 AIR
89201.985000 CV5.500000 SIO2 9024.617000 CX5.209200 AIR ~, -91175.000000 CX4.500000 SI02 ~ , 9254.941000 CX1.433000 AlR
20 9330.044000 CV3.000000 F4 -94384.855000 CX34.294000 AIR
-- --19.000000 AIR
96221.803000 CV5.000000 SI02 ~-9774.673000 CX93.000000 AIR
25 }121863.457201 CX7.000000 ACRYL
11339.515000 CX21.000000 AIR
114 -- --20.500000 AIR
115 -- --4.000000 ACRYL
-~ 11683.478000 CX0.500000 AIR
30 11739.515000 CX4.500000 ACRYL
118 -- --25.000000 AIR
103 -- -- __ __ , I : , Fig. 6 illustrates an optical ray trace of an alternative embodiment of a hou~ing portion 120a and a daytime eyepiece portion 120b of optical components. The housing and eyepiece portions are 20~0434 separated at a split line 123. Table III list the corresponding prescription data. Fig. 7 illustrates the alternative embodiment nighttime eyepiece 120c.
Table IV list the corresponding prescription data.
The alternative embodiments are comprised entirely of conventional plastic optical elements. It should be noted that the alternative embodiment~
illustrated have a longer optical path length than the preferred embodiment~ of Figs. 4,S. This requires the CRTs 22,23 and a portion of the relay optic components to be mounted on the back side of the helmet 21 for best fit to the outer surface of the helmet.
~ , , TABLE III
15~urfaceRadius Curve Thick/ Nat~l No. (mm) Ty~e Dist (mm) ~- 84 40.000000 CV42.360000 AIR
130 149.880000 CX 3.000000 POLYC
131 53.660000 CV18.418400 AIR
20132 110.449000 CX 7.000000 ACRYL
133 57.279000 CX21.000000 AIR
- 134 -- -- 43.000000 AIR
- 135 316.793000 CX 4.000000 ACRYL
}36 316.793000 CX69.000000 AIR
25137 163.725000 CX 7.000000 ACRYL
138 42.692000 CX 0.000000 AIR
139 42.692000 CV -2.000000 POLYC
- 140 135.158000 CX130.000000 AIR
141 -- -- 76.000000 AIR
30142 65.596000 CV 4.20000q ACRYL
143 55.139000 CX64.000000 AIR
144 -- -- 25.300000 AIR ~`
145 135.158000 CV26.500000 AIR
144 -- -- 3.000000 ACRYL
35146 -- -- 47.000000 AIR
:
, 20~0434 TABLE IV :~ :
Surface Radius Curve Thick/ Mat'l No. ~mm~ Type Dist lmm) 8440.000000 CV 42.360000 AIR
130149.880000 CX 3.000000 POLYC
13153.660000 CV18.418400 AIR : -132110.449000 CX 7.000000 ACRYL ~ .
13357.279000 CX21.000000 AIR
134 -- -- 43.000000 AIR
135316.793000 CX 4.000000 ACRYL
136316.793000 CX69.000000 AIR ~ -137163.725000 CX 7.000000 ACRYL
13842.692000 CX o.ooooo0 AIR ~ ~ :
13942.692000 CV 2.000000 POLYC ~ -140135.158000 CX130.000000 AIR ::
141 -- -- 114.000000 AIR
17384.312000 CX 8.000000 POLYC ~ : : -17484.312000 CX23.000000 AIR
175 -- -- 21.000000 AIR
17634.836000 CX 5.000000 ACRYL
~ 177 -- -- 24.000000 AIR
: : 103 -- ---_ __ The preferred embodiment of the daytime optical components provide for data display in a 30-35 - 25 degree monocular field of view with 36% see-through luminance transmission, and approximately 6%
: luminance transfer from the CRT (60% beamsplitter.
transmission, 60% combiner transmission). The nighttime optical components provide for 30 ~ approximately 40 degree monocular field of view with no combiner see-through. The HMD is designed for ~-binocular viewing using two eyepieces with 100%
overlap of the left and right visual fields. Also, the optics are designed to accomodate a CRT image :~
source having an active image diameter in the range of 16 - 25 mm, with the~projection optical lenses 17 ~ ~
`.: ~ - :
20~0434 ~ ~
having an effective focal length in the range of 15 ~' - 55 mm.
The discussion thus far is directed to an HMD
having interchangeable eyepieces, as disclosed in the aforementioned copending U.S. patent application to Fournier et al. It is to be understood that the -present invention can be adapted to utilize concepts disclosed therein to achieve the objectives of the present invention without departing from the scope thereof.
F1g. 8 illustrates an optical ray trace of a preferred embodiment of the present invention.
Illustrated are the optical components comprising the relay optic portion 24a of Fig. 4 together with lS the nighttime eyepiece 24c of Fig. 5, and including the opt~cal components in accordance with the -~ presant invention. A visual image comprised of optical signals is provided on an object surface 200 - of an image source 201, such as a known type image ~20 inten~ifier device. The optical signals emanating from the ob~ect surface proceed to encounter a reflecting optical component (mirror) 204 which is disposed~to present the optical signals to a beamsplitter 206. Ths beamsplitter 206 is disposed in the optical path 50 both to reflect the optical ignals emanating from the image intensifier ob~ect surface 200, and to transmit the optical signals from the faceplate 41. The image intensifier optical signals are reflected by surface 208 of the beamsplitter, the surface being coated with a suitable known type optical coating so as to achieve a reflectivity of from 80 - 95%. This high reflectivity is desired because the luminance of the ~
: - ::.
image on the image intensifier object surface is typically much lower than the luminance of the image on the CRT faceplate (1~ or less). Consequently, -the transmissivity of the beamsplitter surface 208 is approximately 5 - 20% (i.e., 20~ of the optical signals from the faceplate 41 are transmitted through the beamsplitter).
The disposition of the beamsplitter in the optical path is such that the image intensifier optical signals are directed along the optical path 50 towards the surface 85 of the first lens 53 in the same direction as the optical signals from the faceplate. The result is that the image from the CRT faceplate is superimposed on the image from the image intensifer. (Note the Fig. 8 illustrates the path of the optical rays from the image intensifer ob~ect surface through the eyepiece only; not shown are the optical rays from the CRT faceplate). The superimposed image is then transferred by the relay optic portion and the eyepiece into the observer's ..
forward field of view.
However, in order to achieve proper superposition of the two images, the optical path length from the image intensifier object surface 200 to the surface 85 of the first lens 53 must equal the optical path length from the faceplate 41 to the surface 85 of the first lens 53. This distance is referred to as the back focus distance, which, from Table I, equals 61.863200 mm for the preferred embodiment of Fig. 8. Also, because the beamsplitter 206 is disposed in the optical path 50 at a point where the optical signals are not collimated, the beamsplitter is required to be thin , ~...-~-~, -19- ~ ~ ~
2010a~34 (less than 1 mm thick) so as to reduce astigmatism.
If a thicker beamsplitter were employed, additional lenses would be required to correct the aberrations.
Such additional lenses add an undersirable weight to the overall HMD. The thin beamsplitter can either be made of quartz or be that of a pellicle type consisting of a coated membrane supported on a frame. The pellicle beamsplitter effectively has zero optical thickness, and, thus, does not distort transmitted images.
Fig. 9 illustrates an alternative embodiment of the present invention comprising the all plastic optical component design of the relay optic portion of Fig. 6 together with the nighttime eyepiece of Fig. 7, and including the optical components in accordance with the present invention. Note that the all plastic alternative embodiment necessitates additional lenses in the optical path from the image - -intensifier object surface 200 to the beamsplitter 206. Table V lists the corresponding prescription data for the optical component surfaces from the image intensifier object surface 200 through surface 137. The remaining surfaces in the optical path are listed in Table IV. As with the preferred embodiment of Fig. 8, the optical path distance from the image intensifier object surface 200 to the lens surface 137 equals the optical path distance from the CRT faceplate 41 to the lens surface 137.
Z0~0434 - - ~
TABLE V
Surface RadiusCurve Thick/ Mat'l No. (mm) TypeDist ~mml 20040.000000 CV43.208237 AIR
220149.880000 CX3.000000 POLYC
22153.660000 CV18.472773 AIR
222110.449000 CX7.000000 ACRYL
22357.279000 CX24.000000 AIR
224 -- --33.000000 AIR
225316.793000 CX4.000000 ACRYL
226316.793000 CX33.000000 AIR
208 -- --36.000000 AIR
Fig. 10 illustrates a perspective view of a HMD
with a pair of identical image intensifier devices 201 mounted on the helmet 21 in accordance with the present invention. Fig. 10 is essentially a replicate of Fig. 2 with the addition of the image intensifier devices mounted on the helmet. Each image intensifier has a sensing surface 240,241 on ~` 20 ~ the~front of the device that senses the external scene. Each image intensifier processes the sensed scene and presents an image of it on the respective ;~
object surface 200 (not visible) of each device.
The image from the each image intensifier device is " ~; 25 ~ superimposed together with the image from the respective CRT 22,23 by the the corresponding mirror 204 and beamsplitter 206 (not visible)~ That is, each image intensifier has an identical mirror 204 and identical beamsplitter 206 disposed after its ob~ect surface for presenting the image into the respective relay optic portion 24a,24b. Each mirrorjbeamsplitter pair is enclosed in a separate - 21 ~
20~0434 aluminum housing portion 243,244 in a similar fashion as that of the optical components illustrated in Fig. 3 (i.e., with suitable machined seats).
In operation, the pilot dons the HMD having the image intensifier devices incorporated directly on the helmet in accordance with the present invention.
The pilot also attaches the night eyepiece to the HMD. Then, during flight, the exterior scene i8 sensed by the image intensifier devices and the image provided by these devices is superimposed with an image of symbol pilotage data provided by each CRT. The resulting superimposed image is pro~ected into the pilot's forward field of view by the relay optic portion and the nighttime eyepiece. There is no inherent time lag in this type of night vision HMD from the time the pilot moves his head angularly to the time the proper image of the external scene i8 presented to the pilot's forward field of view.
The present invention also lacks the complexity and cost of prior art night vision HMDs.
. ~
A binocular HMD has been illustrated herein incorporating two identical image intensifying ~; devices together with relay optic portions and eyepieces. However, it is to be understood that a monocular HMD can be implemented employing a single image intensifying device together with a single relay optic portion and eyepiece without departing from!the scope of the present invention. ! ' :
Although the invention has been shown and described with respect to a best mode embodiment thereof, it should be understood by those skilled in the art that the foregoing and various other changes, omissions, and additions in the form and detail thereof may be made therein without departing from the spirit and scope of the invention.
~.
~ - 23 -. ~ . . ,
Claims (12)
1. Helmet mounted apparatus for use in a display system, comprising:
a helmet, adapted to be worn by an observer, having an outer surface with an opening provided in proximity to the eyes of the observer;
a first image source disposed on said helmet to provide an image:
relay optic means, comprising a plurality of optical components and being disposed on said helmet outer surface, for receiving the image from said first image source at an entrance pupil thereof and for guiding the image along an optical path to an intermediate image focal plane located in proximity to said outer surface opening, said plurality of optical components including a first lens disposed along the optical path at a predetermined distance from said first image source, said relay optic means being adapted to engage an eyepieces;
a second image source disposed on said helmet to provide an image;
an optical beamsplitter component disposed in the optical path between said first image source and said first lens both to reflect the image provided by said second image source in a direction along the optical path toward said first lens and to transmit the image from said first image source along the optical path toward said first lens, an optical path distance from said second image source to said first lens being equal to the predetermined optical path distance from said first image source to said first lens, said beamsplitter component being so spatially positioned as to effectively superimpose the image from said second image source upon the image from said first image source, the image in proximity to said intermediate image focal plane being a focused form of the superimposed image at said first lens;
and eyepiece means for receiving the superimposed image from said intermediate image focal plane at an input aperture thereof and for presenting, in the observer's forward field of view, the superimposed image as focused in the optical path in proximity to said intermediate image focal plane, said eyepiece means being adapted to releasably engage said relay optic means, said eyepiece means, when engaged, receiving the superimposed image from said intermediate image focal plane and presenting the image in the observer's forward field of view.
a helmet, adapted to be worn by an observer, having an outer surface with an opening provided in proximity to the eyes of the observer;
a first image source disposed on said helmet to provide an image:
relay optic means, comprising a plurality of optical components and being disposed on said helmet outer surface, for receiving the image from said first image source at an entrance pupil thereof and for guiding the image along an optical path to an intermediate image focal plane located in proximity to said outer surface opening, said plurality of optical components including a first lens disposed along the optical path at a predetermined distance from said first image source, said relay optic means being adapted to engage an eyepieces;
a second image source disposed on said helmet to provide an image;
an optical beamsplitter component disposed in the optical path between said first image source and said first lens both to reflect the image provided by said second image source in a direction along the optical path toward said first lens and to transmit the image from said first image source along the optical path toward said first lens, an optical path distance from said second image source to said first lens being equal to the predetermined optical path distance from said first image source to said first lens, said beamsplitter component being so spatially positioned as to effectively superimpose the image from said second image source upon the image from said first image source, the image in proximity to said intermediate image focal plane being a focused form of the superimposed image at said first lens;
and eyepiece means for receiving the superimposed image from said intermediate image focal plane at an input aperture thereof and for presenting, in the observer's forward field of view, the superimposed image as focused in the optical path in proximity to said intermediate image focal plane, said eyepiece means being adapted to releasably engage said relay optic means, said eyepiece means, when engaged, receiving the superimposed image from said intermediate image focal plane and presenting the image in the observer's forward field of view.
2. The helmet mounted apparatus of claim 1, wherein said first image source is a cathode ray tube.
3. The helmet mounted apparatus of claim 1, wherein said second image source is an image intensifying device.
4. The helmet mounted apparatus of claim 1, further comprising one or more optical components disposed to guide the image from said second image source to said beamsplitter component.
5. The helmet mounted apparatus of claim 4, wherein said one or more components includes a mirror.
6. The helmet mounted apparatus of claim 1, wherein a surface of said beamsplitter component nearest to said first lens is coated with an optical coating having a reflectivity in the range of from eighty to ninety five percent.
7. The helmet mounted apparatus of claim 1, wherein said beamsplitter component comprises optical quartz material having a thickness of approximately one millimeter.
8. The helmet mounted apparatus of claim 1, wherein said beamsplitter component comprises a pellicle type beamsplitter component.
9. The helmet mounted apparatus of claim 1, wherein said eyepiece means includes an optical reflecting component disposed in the observer's forward field of view to reflect, into the observer's forward field of view, the superimposed image as focused at said input aperture, said reflecting component being opaque to the exterior scene image disposed in the observer's forward field of view beyond said reflecting component.
10. The helmet mounted apparatus of claim 1, wherein said optical components comprising said relay optic means includes a plurality of lenses of different material composition disposed in proximity to one another, whereby each said lens pair reduces chromatic abberrations of the optical signals that are guided through said lenses.
11. The helmet mounted apparatus of claim 1, wherein said optical components comprising said relay optic means includes a mirror disposed to reflect the superimposed image along the optical path in the direction of said intermediate image focal plane.
12. The helmet mounted apparatus of claim 1, wherein the length of the optical path from said entrance pupil to said intermediste image focal plane is in the range of 100 - 400 millimeters.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US313,686 | 1989-02-21 | ||
| US07/313,686 US4961626A (en) | 1989-02-21 | 1989-02-21 | Direct incorporation of night vision in a helmet mounted display |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2010434A1 true CA2010434A1 (en) | 1990-08-21 |
Family
ID=23216701
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002010434A Abandoned CA2010434A1 (en) | 1989-02-21 | 1990-02-20 | Direct incorporation of night vision in a helmet mounted display |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4961626A (en) |
| EP (1) | EP0384880A3 (en) |
| JP (1) | JPH0339925A (en) |
| CA (1) | CA2010434A1 (en) |
| DE (1) | DE384880T1 (en) |
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| US10976551B2 (en) | 2017-08-30 | 2021-04-13 | Corning Incorporated | Wide field personal display device |
| EP3847503A4 (en) | 2018-09-04 | 2022-09-14 | HVRT Corp. | Reticles, methods of use and manufacture |
| WO2020121814A1 (en) * | 2018-12-11 | 2020-06-18 | 株式会社Ｑｄレーザ | Image display device and relay optical system |
| CN115755397A (en) | 2019-04-26 | 2023-03-07 | 苹果公司 | Head mounted display with low light operation |
| US11867908B2 (en) | 2021-12-17 | 2024-01-09 | Bae Systems Information And Electronic Systems Integration Inc. | Folded optic augmented reality display |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2521874A1 (en) * | 1975-05-16 | 1976-12-02 | Siemens Ag | Background information superimposition device - has frosted disc between partially transmitting mirror and background information original |
| IL55547A (en) * | 1977-10-17 | 1981-03-31 | Hughes Aircraft Co | Holographic one-tube goggle |
| US4361384A (en) * | 1980-06-27 | 1982-11-30 | The United States Of America As Represented By The Secretary Of The Army | High luminance miniature display |
| US4439755A (en) * | 1981-06-04 | 1984-03-27 | Farrand Optical Co., Inc. | Head-up infinity display and pilot's sight |
| GB2108702B (en) * | 1981-10-14 | 1985-06-19 | Marconi Avionics | Optical arrangements |
| US4763990A (en) * | 1984-02-03 | 1988-08-16 | Flight Dynamics, Inc. | Head up display system |
| US4660943A (en) * | 1984-12-17 | 1987-04-28 | Gec Avionics Limited | Night vision systems |
| EP0252200A1 (en) * | 1986-07-08 | 1988-01-13 | OIP OPTICS Naamloze Vennootschap | Night vision goggles |
| US4915487A (en) * | 1989-02-01 | 1990-04-10 | Systems Research Laboratories | Heads up display for night vision goggle |
-
1989
- 1989-02-21 US US07/313,686 patent/US4961626A/en not_active Expired - Fee Related
-
1990
- 1990-02-20 CA CA002010434A patent/CA2010434A1/en not_active Abandoned
- 1990-02-20 EP EP19900630046 patent/EP0384880A3/en not_active Withdrawn
- 1990-02-20 DE DE199090630046T patent/DE384880T1/en active Pending
- 1990-02-21 JP JP2040849A patent/JPH0339925A/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| EP0384880A2 (en) | 1990-08-29 |
| DE384880T1 (en) | 1990-11-29 |
| US4961626A (en) | 1990-10-09 |
| EP0384880A3 (en) | 1991-07-17 |
| JPH0339925A (en) | 1991-02-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |