CA2674878A1 - Electrically dimmable combiner optics for head-up display - Google Patents
Electrically dimmable combiner optics for head-up display Download PDFInfo
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- CA2674878A1 CA2674878A1 CA002674878A CA2674878A CA2674878A1 CA 2674878 A1 CA2674878 A1 CA 2674878A1 CA 002674878 A CA002674878 A CA 002674878A CA 2674878 A CA2674878 A CA 2674878A CA 2674878 A1 CA2674878 A1 CA 2674878A1
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- combiner
- head
- dimmable
- operator
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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
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- B60K2360/334—
-
- 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
- G02B2027/0118—Head-up displays characterised by optical features comprising devices for improving the contrast of the display / brillance control visibility
Abstract
Methods and systems for providing an electrically dimmable combiner optic s for head-up displays are disclosed. In one embodiment, a dimmable head-up display (400) includes a display portion (408) configured to provide head-up display information to an operator (402). Additionally, a dimmable portion (406) is coupled to the display portion configured to change a transmissivit y of the display portion from a first transmissivity level to a second trans missivity level. The dimmable portion (406) includes a plurality of dimmable segments of independent variable transmissivity. The head-up display (HUD) may include a light sensor (412, 414) to detect the light intensity of the e nvironment surrounding the dimmable combiner (116).
Description
ELECTRICALLY DIMMABLE COMBIlVTER OPTICS FOR HEAD-UP DISPLAY
FIELD OF THE DISCLOSURI:
The disclosure relates generally to head-up displays, and more specifically to methods and systems for providing head-up displays with variable light transmission.
BACKGROUND OF THE DISCLOSURF
A head-up display (HUD) is a display surface that is substantially transparent and allows a user to look through the HUD and view information presented on the surface of the HUD, including the outside environment, without refocusing the user's eyes.
Aircraft and niotor vehicles typically utilize one type of HUD, called a fixed HUD, which allows the HUD to depict iziformation relative to the oiientation of the aircraft or vehicle. Another type of HUD is a moveable HUD, which is oflen mounted in a helmet or head-mounted visor. A
moveable HUD
can display similar elements, but corrects the positions of the image by sensing the movement of a person's head or body so that the images are still stable with respect to the outside world.
Military and commercial cockpits or flight decks have employed head-up displays for decades. HUD's have also migrated into many other applications including motorized vehicles. In aviation, with the exception of specific pilot tasks (e.g., targcting), HUD's are generally used to provide the pilot with flight instrument information such as airplane attitude, airspeed, altitude, flight path, and other information while the pilot's attention is foci,Lsed outside of the aircraft. In a typical installation, a HUD projector projects an image onto an optical transparent "combiner' . 'The pilot or operator views the outside world through the traiasparent combiner, and the optical qualities of the combiner and the projector work together to focus the displayed image in a far field (e.g., focal point well outside the aircraft) as viewed by the pilot through the combiner, so that the pilot can view inforniation and the outside ivorld at the same time without re-focusing his or her eyes. The image appears to the operator to be projected onto the outside world. Aircraft also generally include primary flight displays installed on the fnain instrument panel. in front of the pilot for use during head-down instrument flying.
Because of limitations inherent in existing HUD's, regulators do not usually approve HUD's as the sole source of aircraft display information for maintaining awareness of critical paranieters and controlling the airplane. One drawback of existing I-iUD's is the difficulty to read data on a HUD under bright conditions, such as when the sun is near the horizon and appears in or near the HUD from the pilot's viewpoint.
Additionally, when pilots are flying through or near brightly sunlit clouds, it may be difficult or iinpossible to read data presented on a HUD. For this reason, a HUD cannot be certified as the sole display on an aircraft for critical flight parameters such as attitude, altitude, airspeed, or heading.
Therefore, there exists a need for iniproved apparatuses and systems for ] 0 providing head-up displays.
SUMMARY
Embodiments of methods and systems for providing head-up displays are disclosed. Embodimen:ts of methods and systems in accordance with the present disclosure may advantageously improve operation and reliability of head-up displays, and thus provide a user with a greater opportunity to utilize the HUD to receive infotmation.
In one embodiment, a dimmabl.e head-up display includes a display portion configured to provide head-up display infonnation to an operator.
Additionally, a dimmable portion is coupled to the display portion configured to change a transmissivity of the display portion from a first tran.cinissivity level to a second transmissivity level.
In another embodiment, a system for providing a dimmable head-up display includes a dinimable combiner configured to provide head-up display inforrnation to an operator, the dimr.zable combiner adjustable fron- a substantially transparent level to a less transparent level., a light sensor configured to detect the light intensity of an environment surrounding the dimrnable combiner, and a combiner control module configured to receive a light sensor signal from the lio t serisor and transmit a control signal to the dimiliable combiner for adjusting the transmissivity of the dirnmabl.e conabiner.
FIELD OF THE DISCLOSURI:
The disclosure relates generally to head-up displays, and more specifically to methods and systems for providing head-up displays with variable light transmission.
BACKGROUND OF THE DISCLOSURF
A head-up display (HUD) is a display surface that is substantially transparent and allows a user to look through the HUD and view information presented on the surface of the HUD, including the outside environment, without refocusing the user's eyes.
Aircraft and niotor vehicles typically utilize one type of HUD, called a fixed HUD, which allows the HUD to depict iziformation relative to the oiientation of the aircraft or vehicle. Another type of HUD is a moveable HUD, which is oflen mounted in a helmet or head-mounted visor. A
moveable HUD
can display similar elements, but corrects the positions of the image by sensing the movement of a person's head or body so that the images are still stable with respect to the outside world.
Military and commercial cockpits or flight decks have employed head-up displays for decades. HUD's have also migrated into many other applications including motorized vehicles. In aviation, with the exception of specific pilot tasks (e.g., targcting), HUD's are generally used to provide the pilot with flight instrument information such as airplane attitude, airspeed, altitude, flight path, and other information while the pilot's attention is foci,Lsed outside of the aircraft. In a typical installation, a HUD projector projects an image onto an optical transparent "combiner' . 'The pilot or operator views the outside world through the traiasparent combiner, and the optical qualities of the combiner and the projector work together to focus the displayed image in a far field (e.g., focal point well outside the aircraft) as viewed by the pilot through the combiner, so that the pilot can view inforniation and the outside ivorld at the same time without re-focusing his or her eyes. The image appears to the operator to be projected onto the outside world. Aircraft also generally include primary flight displays installed on the fnain instrument panel. in front of the pilot for use during head-down instrument flying.
Because of limitations inherent in existing HUD's, regulators do not usually approve HUD's as the sole source of aircraft display information for maintaining awareness of critical paranieters and controlling the airplane. One drawback of existing I-iUD's is the difficulty to read data on a HUD under bright conditions, such as when the sun is near the horizon and appears in or near the HUD from the pilot's viewpoint.
Additionally, when pilots are flying through or near brightly sunlit clouds, it may be difficult or iinpossible to read data presented on a HUD. For this reason, a HUD cannot be certified as the sole display on an aircraft for critical flight parameters such as attitude, altitude, airspeed, or heading.
Therefore, there exists a need for iniproved apparatuses and systems for ] 0 providing head-up displays.
SUMMARY
Embodiments of methods and systems for providing head-up displays are disclosed. Embodimen:ts of methods and systems in accordance with the present disclosure may advantageously improve operation and reliability of head-up displays, and thus provide a user with a greater opportunity to utilize the HUD to receive infotmation.
In one embodiment, a dimmabl.e head-up display includes a display portion configured to provide head-up display infonnation to an operator.
Additionally, a dimmable portion is coupled to the display portion configured to change a transmissivity of the display portion from a first tran.cinissivity level to a second transmissivity level.
In another embodiment, a system for providing a dimmable head-up display includes a dinimable combiner configured to provide head-up display inforrnation to an operator, the dimr.zable combiner adjustable fron- a substantially transparent level to a less transparent level., a light sensor configured to detect the light intensity of an environment surrounding the dimrnable combiner, and a combiner control module configured to receive a light sensor signal from the lio t serisor and transmit a control signal to the dimiliable combiner for adjusting the transmissivity of the dirnmabl.e conabiner.
-2-T'he features, functions, and advantages can be achieved independently in various enibodiments of the present disclosure or may be combined in yet other embodinients.
BRIEF DESCRIPTION OF THE DItAWINGS
Embodiments of the disclosure are described in detail below with reference to the following drawings.
Figure 1 is a side, partial elevational schematic view of an aircraft having a cockpit portion that includes a dimmable head-up display in accordance with an embodiment of the disclosure;
Figure 2 is a top, partial sectional view of a cockpit portion of the aircraft of Figure 1, including a dinunable head-up display;
Figure 3 is a schematic of a dinimabie head-up display in accordance with another einbodiment of the disclosure;
Figure 4 is a schematic of a dimmable head-up display in. accordance with another embodiment of the disclosure:
Figure 5 is a schematic of a segmented dimmable head-up display in accordance rvith an embodiment of the disclosure;
Figure 6 is an isometric view of a head-mountable diinmable head-up display in accor.daitce with another embodiment of the disclosure;
Figure 7 is a flow diagram of a system for providing a dimmable head-up display in accordance with embodinzents of the disclosure; and Figure 8 is a side elevational view of an aircraft having a dimmable head-up display in accordance with yet anotller embodiinent of the disclosure.
DETAILED DESCRIPTION
Methods arid systems for providing an electrically diniinable combiner optics for head-up displays are described herein.. Many specific details of cf.'rtain embodiments of the
BRIEF DESCRIPTION OF THE DItAWINGS
Embodiments of the disclosure are described in detail below with reference to the following drawings.
Figure 1 is a side, partial elevational schematic view of an aircraft having a cockpit portion that includes a dimmable head-up display in accordance with an embodiment of the disclosure;
Figure 2 is a top, partial sectional view of a cockpit portion of the aircraft of Figure 1, including a dinunable head-up display;
Figure 3 is a schematic of a dinimabie head-up display in accordance with another einbodiment of the disclosure;
Figure 4 is a schematic of a dimmable head-up display in. accordance with another embodiment of the disclosure:
Figure 5 is a schematic of a segmented dimmable head-up display in accordance rvith an embodiment of the disclosure;
Figure 6 is an isometric view of a head-mountable diinmable head-up display in accor.daitce with another embodiment of the disclosure;
Figure 7 is a flow diagram of a system for providing a dimmable head-up display in accordance with embodinzents of the disclosure; and Figure 8 is a side elevational view of an aircraft having a dimmable head-up display in accordance with yet anotller embodiinent of the disclosure.
DETAILED DESCRIPTION
Methods arid systems for providing an electrically diniinable combiner optics for head-up displays are described herein.. Many specific details of cf.'rtain embodiments of the
-3-disclosure are set forth in the following description and in Figures 1 through 8 to provide a thorough understanding of such embodiments. One skilled in the art, however, will understar.d that the present disclosure may have additional embodiments, or that the present disclosure may be practiced without several of the details described in the following description.
Embod'unents of methods and systems in accordance with the disclosure may provide considerable advantages over the prior art. For example, in a situation where too much outside light reaches an operator's eyes, embodiments of the disclosure may reduce or replace the need for visors, sun shades, and sunglasses, prevent or reduce squinting, and reduce the risk of loss of visual acuity. Where the light intensity increases too quickly, embodiments of the disclosure may prevent or mitigate undesirable effects on the operator by reducing the maxilnuni light intensity and consequently the undesirable effects of a rapid change in outside light intensity experienced by the operator, such as a pilot. Throughout this disclosure, the term `dimmable' may be interchangeable with variable light transmission, such as variable light transmission through a variably transparent object.
Figure 1 is a side, partial elevational schematic view of an aircraft 102 having a cockpit portion 104 that includes a dimunable head-up display (HUD) 106 in accordatice with an einbodiment of the disclosure. As shown'in ati environment 100 in Figure 1, light from the sun 108 rnay enter the cockpit portion 104 in several ways. A direct portion 110 may shine directly into the cockpit portion 104 from the sun 1.08, while an indirect portion 112 may reflect from a cloud 114 or other reflective object into the cockpit portion 104.
In an embodiinent, the HUD 106 includes a combiner 116 and a projector 118.
'The projector 118 projects an image on. the coinbiner 116, such as vehicle information. In other embod.iments, the HUD 106 may display images on a combiner 116 without a projector 118. For exarnple, the combiner 116 may have an intemally integrated display module.
When. the system is on or excited, the operator 120 rnay view images, graphics, and other inforrnation presented by the internally integrated display module or the projector 118. The operator 120 may view images through the combiner 116, such as the outside environment of the vehicle, when the combiner is at least partially transparent.
Embod'unents of methods and systems in accordance with the disclosure may provide considerable advantages over the prior art. For example, in a situation where too much outside light reaches an operator's eyes, embodiments of the disclosure may reduce or replace the need for visors, sun shades, and sunglasses, prevent or reduce squinting, and reduce the risk of loss of visual acuity. Where the light intensity increases too quickly, embodiments of the disclosure may prevent or mitigate undesirable effects on the operator by reducing the maxilnuni light intensity and consequently the undesirable effects of a rapid change in outside light intensity experienced by the operator, such as a pilot. Throughout this disclosure, the term `dimmable' may be interchangeable with variable light transmission, such as variable light transmission through a variably transparent object.
Figure 1 is a side, partial elevational schematic view of an aircraft 102 having a cockpit portion 104 that includes a dimunable head-up display (HUD) 106 in accordatice with an einbodiment of the disclosure. As shown'in ati environment 100 in Figure 1, light from the sun 108 rnay enter the cockpit portion 104 in several ways. A direct portion 110 may shine directly into the cockpit portion 104 from the sun 1.08, while an indirect portion 112 may reflect from a cloud 114 or other reflective object into the cockpit portion 104.
In an embodiinent, the HUD 106 includes a combiner 116 and a projector 118.
'The projector 118 projects an image on. the coinbiner 116, such as vehicle information. In other embod.iments, the HUD 106 may display images on a combiner 116 without a projector 118. For exarnple, the combiner 116 may have an intemally integrated display module.
When. the system is on or excited, the operator 120 rnay view images, graphics, and other inforrnation presented by the internally integrated display module or the projector 118. The operator 120 may view images through the combiner 116, such as the outside environment of the vehicle, when the combiner is at least partially transparent.
-4-~ . CA 02674878 2009-07-07 The combiner 116 is typically an optical glass or plastic device that allows the operator 120 to see through the combiner 116 to monitor outside activities.
The operator 120 sees HUD images, such as vehicle information, focused outside the vehicle by looking through the combiner 116. For example, the combiner 116 may display infonnation to allow an operator 120 (e.g., pilot) to view flight control information, such as altitude, airspeed, and horizon orientation, while also allowing the operator 120 to see outside the aircraft 102 through the coinbiner 116. Therefore, the operator 120 can shift his attention between flight control infonnation presented by the HUD 106 and external activity outside of the aircraft 102 without refocusing his eyes.
The cornbiner 116 generally includes at least one variable transmissivity portion. The dimmability (or variable transmissivity) of the combiner 116 may be provided in any suitable manner. For example, in alternate embodiments, the combiner 116 may include an electrochromic, a gel-type (e.g. GentexrM), a thin-film (e.g. St. GobianTm or Su1lyT"I), a photochromic, or any other suitabl.e technology that provides variably controllable light transrnission levels. More specifically, in alternate embodiments, the combiner 116 may include any of those clectrochromic devices, materials, and systcros generally disclosed in U.S. Patent Application Publication No. 2002/0196518 entitled "Electrochromic Organic Polymer Syntheses and Devices Utilizing Electrochromic Organic Polymers", filed on June 25, 2002, and in the following co-pending, conlmonly-owned U.S. Patent Applications filed on October 2?, 2004: US
Patent Application Publication No. 2005/0200934 entitled "Dimming Control System for an Airay of Electrochromic Devices", U.S. Patent Application Publication No.
entitled "Low Vapor Pressure Solvent for Electrochronlic Devices", and U.S.
Patent Application Publication No. 2005/0200937 entitled "Multi-Color Electrochromic Apparatus and Methods", which applications are hereby incorporated by reference. In this manner, the combiner 116 includes dis-amable or variably controllable transmissivity.
The variably controllable transmissivity of the coinbiner 116 enables the operator 120 to view the HUD 106 display regardless of ainbient brightness or sun position,
The operator 120 sees HUD images, such as vehicle information, focused outside the vehicle by looking through the combiner 116. For example, the combiner 116 may display infonnation to allow an operator 120 (e.g., pilot) to view flight control information, such as altitude, airspeed, and horizon orientation, while also allowing the operator 120 to see outside the aircraft 102 through the coinbiner 116. Therefore, the operator 120 can shift his attention between flight control infonnation presented by the HUD 106 and external activity outside of the aircraft 102 without refocusing his eyes.
The cornbiner 116 generally includes at least one variable transmissivity portion. The dimmability (or variable transmissivity) of the combiner 116 may be provided in any suitable manner. For example, in alternate embodiments, the combiner 116 may include an electrochromic, a gel-type (e.g. GentexrM), a thin-film (e.g. St. GobianTm or Su1lyT"I), a photochromic, or any other suitabl.e technology that provides variably controllable light transrnission levels. More specifically, in alternate embodiments, the combiner 116 may include any of those clectrochromic devices, materials, and systcros generally disclosed in U.S. Patent Application Publication No. 2002/0196518 entitled "Electrochromic Organic Polymer Syntheses and Devices Utilizing Electrochromic Organic Polymers", filed on June 25, 2002, and in the following co-pending, conlmonly-owned U.S. Patent Applications filed on October 2?, 2004: US
Patent Application Publication No. 2005/0200934 entitled "Dimming Control System for an Airay of Electrochromic Devices", U.S. Patent Application Publication No.
entitled "Low Vapor Pressure Solvent for Electrochronlic Devices", and U.S.
Patent Application Publication No. 2005/0200937 entitled "Multi-Color Electrochromic Apparatus and Methods", which applications are hereby incorporated by reference. In this manner, the combiner 116 includes dis-amable or variably controllable transmissivity.
The variably controllable transmissivity of the coinbiner 116 enables the operator 120 to view the HUD 106 display regardless of ainbient brightness or sun position,
-5-while still maintaining the transparent capabilities of the HUD 106.
Additionally, the dimmable combiner 116 may iimction as a sunshade in lieu of tinted and movable plastic shades.
With continued reference to Figure 1, the HUD may also include operator controls 124 to adjust the transmissiv-ity of the combiner 116 or the display characteristics of the combiner 116 via the projector 11. 8 or other display source. In other einbodiments, the HUD 106 may include a light sensor 122. The light sensor 122 may detect the light intensity outside the cockpit portion 104 and transfer this information to an operatively coupled combiner control device 126 in connection to the combiner 116. The control device 126 may adjust the transmissivity of the combiner 116 after receiving information relating to the light sensor 122 detection of the light intensity. Additionally, the operator controls 124 may allow the operator 120 to manually control the transmissivity of the combiner 116 based on preferences of the operator 120. Similarly, a projector control device 128 may receive input fi=oni the light sensor 122 and the operator controls 124 to adjust the display cliaracteristics (e.g., brightness) of the image projected onto the combiner 116 via the projector 118. In further embodiments, the control devices 126, 128, may utilize both manual and automatic controls in combination.
Figure 2 is a top, partial sectional view of an environment 200, including the cockpit portion 104 of the aircraft 102 of Figure 1 having the dinunable HUD
106. In this embodiment, the cockpit portion 104 includes a front (or main) window 202 and a pair of side windows 204. A first pilot (or captain) 206 is positioned on a first side of the cockpit portion 104, and a second pilot (or co-pilot) 208 is positioned ori a sccond side of the cockpit portion 104. The first pilot 206 may bave a first combiner 210 positioned behveen the first pilot 206 and the front window 202. The second pilot 208 may have a second combiner 212 positioned between the second pilot 208 and the front window 202. T'he cockpit portion 104 includes light sensor 122a, 1.22b to detect the intensity of light from outside the cock-pit portion 106, such as by the sun 108 by direct or reflected sunlight 110. In orie embodiment, two light sensors 122a, 122b nlay be utilized, each detecting light for a corresponding combiner 210, 212, respectively. In other embodiments, one centrally located light sensor, such as light sensor 122, may detect the liglit for all combiners, such as combiners 210, 212.
Additionally, the dimmable combiner 116 may iimction as a sunshade in lieu of tinted and movable plastic shades.
With continued reference to Figure 1, the HUD may also include operator controls 124 to adjust the transmissiv-ity of the combiner 116 or the display characteristics of the combiner 116 via the projector 11. 8 or other display source. In other einbodiments, the HUD 106 may include a light sensor 122. The light sensor 122 may detect the light intensity outside the cockpit portion 104 and transfer this information to an operatively coupled combiner control device 126 in connection to the combiner 116. The control device 126 may adjust the transmissivity of the combiner 116 after receiving information relating to the light sensor 122 detection of the light intensity. Additionally, the operator controls 124 may allow the operator 120 to manually control the transmissivity of the combiner 116 based on preferences of the operator 120. Similarly, a projector control device 128 may receive input fi=oni the light sensor 122 and the operator controls 124 to adjust the display cliaracteristics (e.g., brightness) of the image projected onto the combiner 116 via the projector 118. In further embodiments, the control devices 126, 128, may utilize both manual and automatic controls in combination.
Figure 2 is a top, partial sectional view of an environment 200, including the cockpit portion 104 of the aircraft 102 of Figure 1 having the dinunable HUD
106. In this embodiment, the cockpit portion 104 includes a front (or main) window 202 and a pair of side windows 204. A first pilot (or captain) 206 is positioned on a first side of the cockpit portion 104, and a second pilot (or co-pilot) 208 is positioned ori a sccond side of the cockpit portion 104. The first pilot 206 may bave a first combiner 210 positioned behveen the first pilot 206 and the front window 202. The second pilot 208 may have a second combiner 212 positioned between the second pilot 208 and the front window 202. T'he cockpit portion 104 includes light sensor 122a, 1.22b to detect the intensity of light from outside the cock-pit portion 106, such as by the sun 108 by direct or reflected sunlight 110. In orie embodiment, two light sensors 122a, 122b nlay be utilized, each detecting light for a corresponding combiner 210, 212, respectively. In other embodiments, one centrally located light sensor, such as light sensor 122, may detect the liglit for all combiners, such as combiners 210, 212.
-6-In some einbodiments, the combiners 210,212 include an electrically dimmable portion. For example, when light passes through the combiners 210, 212, the electrically dimmable portion reduces the light transmissivity, and thus reduces the intensity of the liglit.
'rherefore, the pilots 206, 208 may utilize the combiners 210, 212 in bright sunlight conditions instead of relying on head-down displays, such as those typically relied upon for instrument-based navigation or control.
A first solar flux graph 214 and a second solar flux graph 216 are presented to further illustrate the light intensity before and after light passes through the combiners 210, 212.
The first solar graph 214, with line 218, represents the amount of light received from the sun before the light reaches the coinbiners 210, 212. The second solar graph 216, with line 220, represents the amount of light received from the sun. after the light passes through the combiners 210, 212. For example, in the solar graphs 214, 216, the abscissa represents time (t) while the ordinate represents the solar flux (f). As illustrated, the transmissivity filtering of the combiners 210, 212 reduces the solar flux in the second graph 216. Therefore, the combiners 210, 212 may be utilized by the pilots 206, 208 in conditions with direct sunlight or bright outside ambieiit conditions because the pilots 206, 208 may decrease the transmissiNity of the combiners to reduce the solar flux passing through. the combiner.
Figure 3 is a scheinatic of a dimmable head-up display 300 in accordance with another embodiment of the disclosure. The combiner 116 is configured between the front window 202 and an operator's head 302. The combiner 116 includes an electrically d'uiunable layer. The combiner 116 may receive an image from the projector 118 to provide information to the operator 302. A.lternatively, the conibiner 116 may include an internally integrated display module. The head-up display 300 may also include a light sensor 122 and operator input devices 304, 306.
With continued reference to Figure 3, the light sensor 122 may be configured to measure the intensity of light, such as from the direct light 110. In turn, the combiner control system 308 receives the information froni the light sen.sor 122. The combiner control system 308 may also receive a transmission level preference from an operator via an operator dimming input
'rherefore, the pilots 206, 208 may utilize the combiners 210, 212 in bright sunlight conditions instead of relying on head-down displays, such as those typically relied upon for instrument-based navigation or control.
A first solar flux graph 214 and a second solar flux graph 216 are presented to further illustrate the light intensity before and after light passes through the combiners 210, 212.
The first solar graph 214, with line 218, represents the amount of light received from the sun before the light reaches the coinbiners 210, 212. The second solar graph 216, with line 220, represents the amount of light received from the sun. after the light passes through the combiners 210, 212. For example, in the solar graphs 214, 216, the abscissa represents time (t) while the ordinate represents the solar flux (f). As illustrated, the transmissivity filtering of the combiners 210, 212 reduces the solar flux in the second graph 216. Therefore, the combiners 210, 212 may be utilized by the pilots 206, 208 in conditions with direct sunlight or bright outside ambieiit conditions because the pilots 206, 208 may decrease the transmissiNity of the combiners to reduce the solar flux passing through. the combiner.
Figure 3 is a scheinatic of a dimmable head-up display 300 in accordance with another embodiment of the disclosure. The combiner 116 is configured between the front window 202 and an operator's head 302. The combiner 116 includes an electrically d'uiunable layer. The combiner 116 may receive an image from the projector 118 to provide information to the operator 302. A.lternatively, the conibiner 116 may include an internally integrated display module. The head-up display 300 may also include a light sensor 122 and operator input devices 304, 306.
With continued reference to Figure 3, the light sensor 122 may be configured to measure the intensity of light, such as from the direct light 110. In turn, the combiner control system 308 receives the information froni the light sen.sor 122. The combiner control system 308 may also receive a transmission level preference from an operator via an operator dimming input
-7-device 304. The combiner control system. 308 may automatically maintain or adjust the transmission level of one or more combiner portions of the combiner 116 in accordance with the desired transtnission level from the light intensity measurements from the light sensor 122 and the operator dimming input device 304. In one particular embodiment, the combiner control system 308 adjustably controls the transmissivity of the combiner 116 by varying a voltage value provided by a power source (not shown) to one or more variably controllable transmissivity portions of the combiner 116. In another alternate embodiment, the combiner control system 308 may eliminate the user inputs from the dimming user input device 304.
In other embodiments, the head-up display 300 may include the operator projector input device 306, as presented above, and a HUD projector image control system 310.
The image control systein 310 may adjust the projection's brightness, contrast, or other projection attributes to improve the resulting display on the conibiner 116.
For example, when the combiner 116 reduces transmissivity because of briglit conditions, it may be desirable to adjust the contrast of the image presented on the combiner 116 by the projector 118 by adjusting the projector input device 306. In other embodiments, the image control system 310 may be in operable connection with the light sensor 122. The light sensor may detect changes in the light intensity and comniunicate the light intensity changes to the image control systeni 310, which may then adjust the display on the combiner 116. ln still further embodiunents, the image control system 310 may be in operable connection with the operator dinuning input device 304, therefore enabling the image control systein 310 to adjust the projection atts-ibutes in response to dinuning of the combiner via operator 302 input from the operator diinming input device 304.
In still further configurations of the head up display 300, the image control systezn 310 may be in cominunication with. the combiner control systeni 308.
The combiner control system 308 may send the image control system 310 a signal Nvhen the combiner control.
system 308 changes the transmissivity of the combiner 116, therefore allowing the image control system 310 to make adjustinents to the projcction of images on the combiner 116. The image control system 310 may also send a signal to the combiner control system 308, such as tc, communicate a change to the image display setting of the combiner 116. As discussed above,
In other embodiments, the head-up display 300 may include the operator projector input device 306, as presented above, and a HUD projector image control system 310.
The image control systein 310 may adjust the projection's brightness, contrast, or other projection attributes to improve the resulting display on the conibiner 116.
For example, when the combiner 116 reduces transmissivity because of briglit conditions, it may be desirable to adjust the contrast of the image presented on the combiner 116 by the projector 118 by adjusting the projector input device 306. In other embodiments, the image control system 310 may be in operable connection with the light sensor 122. The light sensor may detect changes in the light intensity and comniunicate the light intensity changes to the image control systeni 310, which may then adjust the display on the combiner 116. ln still further embodiunents, the image control system 310 may be in operable connection with the operator dinuning input device 304, therefore enabling the image control systein 310 to adjust the projection atts-ibutes in response to dinuning of the combiner via operator 302 input from the operator diinming input device 304.
In still further configurations of the head up display 300, the image control systezn 310 may be in cominunication with. the combiner control systeni 308.
The combiner control system 308 may send the image control system 310 a signal Nvhen the combiner control.
system 308 changes the transmissivity of the combiner 116, therefore allowing the image control system 310 to make adjustinents to the projcction of images on the combiner 116. The image control system 310 may also send a signal to the combiner control system 308, such as tc, communicate a change to the image display setting of the combiner 116. As discussed above,
-8-= CA 02674878 2009-07-07 the images may be presented on the coinbiner by other means than a projector, such as by iiiternally integrated display modules, which may also be in conununication with the image control system 310 and operate in accordance with the head-up display 300, including the projector 118 immediately above. In some embodiments, the conibiner control system 308 and image control system 310 may be combined into a single control system.
Figure 4 is a schematic of a diinmable head-up display 400 in accordance with another embodiment of the disclosure. The combiner 116 is configured between a viewing point 402 (such as a view from an operator's perspective) and the light source, such as the sun 108.
Light 404 from the sun 108 intersects the combiner 116. The combiner 116 includes a dinunable portion 406 and a display portion 408. The resulting light 410 reaches the viewing point 402 after passing through the combiner 116. The light 404 may include the solar flux 214 wliile the resulting light 410 may include the solar flux 216, depending on the transinissivity setting of the combiner 116 resulting from activation of the dimmable portion 406.
As noted above, the dimmable portion 406 may be an electrochromic, a gel-type (e.g. GentexT"'), a thin-film (e.g. St. GobianTM or Sully"11), or any other suitable technology that provides variably controllable light transmission levels. In other embodiments, the dimmable portion 406 may be pllotochromic, and thus undergo a chemical reaction when the dimmable portion is exposed to ultraviolet (LJV) radiation. In other embodiments, it may be desirable to combine two or more of the above dimmable portions to reduce the transmissivity of ligbt through the conibiner 11.6.
The display portion 406 may be configured for displaying imagery from a projector or from an internally integrated display module. For example, in an embodiment, the display portion 408 may be an internally integrated display module display integrated into the combiner 116. The internally integrated display inodule inay require additional layers or portions Nvitliin the display portion to produce head-up display images for tiiewing by an operator 402.
The HUD 400 may include a first light sensor 412 and a second light sensor 414. The first li,glit sensor 412 may be disposed between the combiner :l 16 and the sun 108, or
Figure 4 is a schematic of a diinmable head-up display 400 in accordance with another embodiment of the disclosure. The combiner 116 is configured between a viewing point 402 (such as a view from an operator's perspective) and the light source, such as the sun 108.
Light 404 from the sun 108 intersects the combiner 116. The combiner 116 includes a dinunable portion 406 and a display portion 408. The resulting light 410 reaches the viewing point 402 after passing through the combiner 116. The light 404 may include the solar flux 214 wliile the resulting light 410 may include the solar flux 216, depending on the transinissivity setting of the combiner 116 resulting from activation of the dimmable portion 406.
As noted above, the dimmable portion 406 may be an electrochromic, a gel-type (e.g. GentexT"'), a thin-film (e.g. St. GobianTM or Sully"11), or any other suitable technology that provides variably controllable light transmission levels. In other embodiments, the dimmable portion 406 may be pllotochromic, and thus undergo a chemical reaction when the dimmable portion is exposed to ultraviolet (LJV) radiation. In other embodiments, it may be desirable to combine two or more of the above dimmable portions to reduce the transmissivity of ligbt through the conibiner 11.6.
The display portion 406 may be configured for displaying imagery from a projector or from an internally integrated display module. For example, in an embodiment, the display portion 408 may be an internally integrated display module display integrated into the combiner 116. The internally integrated display inodule inay require additional layers or portions Nvitliin the display portion to produce head-up display images for tiiewing by an operator 402.
The HUD 400 may include a first light sensor 412 and a second light sensor 414. The first li,glit sensor 412 may be disposed between the combiner :l 16 and the sun 108, or
-9-adjacent to the combiner 116, such as above or below the combiner 116.
Therefore, the first light sensor 412 detects the light intensity before the light 404 passes through the combiner 116.
The second light sensor 414 is disposed between the combiner 116 and the operator 402.
Therefore, the second light sensor 414 detects the light intensity after the light (i.e., resulting light 410) passes through the combiner 116. In some embodiments, the HUD may only include one of the light sensors 412, 414.
The first light sensor 412 may provide a fixed relationship between the outside brightness and the degree of dimniing of the combiner 116. For example, the first light sensor 412 may be calibrated to adjust the transmissivity of the combiner 116 to a substantially transparent state when the first light sensor 412 detects a low intensity of light. NVhen the first light sensor 412 detects a high intensity of light, the first light sensor 412 may restrict the transmissivity of the combiner 116 to reduce the light intensity viewed by the operator 402.
'The second light sensor 414 may provide a closed loop control system, whlcll adjusts the dimming of the combiner 116 based on the light intensity the second light sensor 414 detects froni the resulting light 410 after it passes through the combiner 116. For example, the second light sensor 414 may calibrate the transmissivity of the combiner 116 by periodically sensing the light intensity, and then adjusting the transmissivity according the measured light intensity. Therefore, the second ligh.t sensor 414 may receive a relatively constant light intensity level through the combiner 116 by continually adjusting the transmissivity of the conibir,er 116.
In a further embodiment of the dimmable HUD 400, the second light sensor 414 measures inte.rior light intensity ineasurernents, arid the combiner control system 308, as shown in Figure 3, autoinatically maintains the transmission levels of the one or more combiner portions of the combiner 116 at suitable transmission levels unless the desired transmission level renders the interior light intensity measurements below a predetennined (or minimum desired) threshold. Wlien the desired transmission level results in the light intensity measurements being below the certain threshold, the combiner control system 308 adjusts (e.g., increases) the t.ransmission level of one or niore combiner portions of the combiner 1.16 to any level that results in the light intensity measurements being at or above the certain threshold.
The combiner control system 308 may periodically or continuously evaluate the light intensity measureinents provided by the second light sensor 414, and may pe,`riodically or continuously adjust the' transmission level of the combiner 116 when the light intensity measurernents fall below the certain threshold.
In another einbodiment, the combiner control system 308 may be further adapted to adjust the transmissivity of the conibiner 116 based on a second predetermined threshold, such as, for example, a maximum allowable (or maxinlum desired) light intensity measurement. More specifically, the second light sensor 414 may measure a light intensity (e.g within the structure) that exceeds a maximum desired threshold. When the combiner control systc. 308 determines that the measured light intensity has exceeded the maximum desired threshold, the combiner control system 308 may automatically adjust (e.g., decrease) the transmissivity of one or more combiner portions of the combiner 116 to lower the measured light intensity. In a particLilar embodiment, a vehicle, such as a cockpit of an aircraft, may employ the head-up display 400 and use it to provide protection t.o the pilot (or other vehicle operator) from a high intensity light or laser.
I.n yet aiiother embodiment, the head-up display 400 may be configured with a fail-safe mechanisin. In this embodimerit, if any component of the head-up display 400 experiences a problem, the fail-safe mechanism (e.g., a component of the combiner control system 308) may automatically default the transmission level of the combiner 116 to a predetennined acceptable level. In some emboditnents, such as in a cockpit of an aircraft, the predetermined acceptable level may be a relatively high transmission level that prosrides normal, non-attenuated visibility levels to the operator 302. In alternate embodiments, however, the fail-safe mechanism rnay result in reduced transmissivity, in comparison with a norinal, non-at.tenuated visibility level. In further einbodiments, the diinmable combiner 116 may be movably configured in front of an operator 302. For example, the conibiner 116 may nlove outside of the operator's line of sigbt through the front window 202 if the dimmable combiner fails to operate properly, therefore giving the operator an unobstructed view through the front rindow 202.
Figure 5 is a schematic of a segmented dimmable head-up display 500 in accordance with an enibodiment of the disclosure. hi some embodiments, the coinbiner 116 may include one or more segments to provide varying levels of transmissivity of light through different segments of the combiner 116. For example, the combiner 116 may be divided vertically 502, horizontally 504, or both to create segments of the combiner 116.
In some embodiments, the combiner may be segmented by an outer segmenting parameter 506 and an iriner segnienting parameter 508. It may be advantageous to position the segmenting parameters 506, 508 to reduce the light intensity from specific areas of the combiner 116, such as the outer segnient 510, including sub-segmetits 510a-510d, while maintaining more transmissivity in an intermediary segment 512 or inner segment 514. Further, each seginent 510, 512, 514 may be subdivided borizontally, vertically, or botli to form corresponding sub-segqn.ents 510a-510d, 512a-512d, 514a-514d, respectively. Segmenting the combiner 116 may include utilizing fewer or more segmenting parameters. For example, a segment, such as segment 510, 512, 514, may include any number of sub-segments. Additionally, the configuration of segmenting parameters may be configured in any number of patterns, including elliptical segments, rectangular segtnents, circular segments, or other segment fonns or sliapes.
Each seginent may be configured to provide adjustable transmissivity of light through the combiner 116. For example, the outer segment 510 may be configured to provide a different transniissivity of liglrt through the combiner 116 that the transmissivity of light through the intei-mediate segment 512 or inner segi.nent 510. Further, each segnnent may be controlled autoniatically, such as by the combiner control systerr- 308 (Figure 3) or by one or more operator input devices 306.
Figure 6 is an isometric view of a head-mountable dunmable head-up display 600 in accordance with another embodiment of the disclosure. In some embodiments, the combiner 602 niay be wearable, such as in the fonn of a visor 604 configured with a helmet 606.
For example, the hehnet 606 xnay be an aviator helmet including a cliinstrap 608 and protective cushioning 610. In other t~nbodimeitts, the IiUD 600 rnay be configured without a helmet 606, such as in a pair of glasses or a mountable head visor. The HUD 600 may include intenaally integrated display modules to display information to an operator. The coinbiner 602 may include at least one variable transm3ssivity portion of the combiner 116. Smaller sub-segments may alsc segment the transmissivity portion. The combiner 602 may be controlled automatically, such as by the combiner control system 308 (Figure 3) or by one or more operator input derices 306.
Figure 7 is a flow chart for a system (or method) 700 for provicl.ing a dimmable head-up display in accordance with embodiments of the disclosure. In this embodiment, the system 700 begins at a state of initial conditions at a block 702. At a decision block 704, the system 700 determines whether to adjust the transmissivity of the combiner to increase or reduce the light intensity viewable through the combiner. If the system 700 selects adjusting the transmissivity of the combiner at the decision block 704, at a block 706, the systeni receives one or more user inputs from the operator input device 304. At a block 708, the combiner control system 308 receives one or more sensor inputs from the light sensor 122. At a block 710, the system 700 adjusts the transmissivity of the conibiner utilizing information from the blocks 706, 708, or both. If the system 700 does not select adjusting the transmissivity of the combiner at the block 704, the system proceeds to a decision block 712.
At the decision block 712, the system 700 makes a determination whether to adjust the transinissivity of the combiner incrementally. For example, at the decision block 712, the system 700 may implement a calibration algoritlun to fine tune the transmissivity of the combiner. If the system 700 selects an incremental adjustment, at a decision block 714, the systern detennines wheth.er the light intensity is too liigh. If so, then at a block 716, the system 700 incrementally reduces the transmissivity of the combiner 116 if the combiner is not already at a minimum allowabl.e level, and then the system returns to block 71.4.
Alternately, if the light level is not too high (block 714), the lit;ht level is deemed to be too low, and the transinissivity of combiner 116 is incrementally increased provided that the combiner is not already at a maximuz.n level, and then the system returns to the decision block 712.
If the system 700 does not select an incremental adjustment at the decision block 712, at a decision block 720, the system determin:,s whether to adjust the combiner display. For example, the combinei- display produced by the projector 1.18 may be difficult to see wher: the system adjusts the transmi.ssivity of the combiner 1.16 at the block 710. Therefore, it may be desirable to adjust the contrast, brightness, or other display characteristics of the combiner display to allow an operator to view the displayed information easier. If the system 700 selects adjusting the display characteristics of the combiner 116 at the decision block 720, at a block 722, the system receives one or more user inputs from the operator input device 306. At a block 724, the image control system 310 receives one or more sensor inputs from the light sensor 122. At a block 726, the system 700 adjusts the display characteristics of the combiner 116 utilizing the information from the blocks 722, 724, or both. lf the system 700 does not select adjusting the display characteristics of the combiner at the decision block 720, the system may reiterate to the decision block 704.
Although the systein 700 makes general reference to a combiner 116, one should appreciate that embodiments of the system 700 may apply to segments or sub-segments of the combiner. For example, with reference to Figure 5, the systein 700 may separately adjust the segments 510, 512, 514, or it may adjust them in combination to create the desirable level of transmissivity at the block 710.
Generally, any of the functions described herein can be impleniented using software, firmware (e.g., fixed logic circuitry), hardware, manual processing, or any combination of these implementations. In the case of a soti:ware iinplementation, the module, functionality, or logic described herein represents program code that perforins specified tasks when executed on processor(s) (e.g., any of microprocessors, controllers, and the like). The prograzn code can be stored in one or more computer readable nzemory devices. Further, the features and aspects described herein are platform-indepeiident such that the tecluliques may be implemented on a variety of coinmercial coinputing platforms having a variety of processors.
It will also be appreciated that methods and systeins in accordance with the teachings of the present disclosure may be described in the general context of computer executable instructions. Generally, coinputer executable instructions can include routines, programs, objects, components, data structures, procedures, modules, functions, and the like that perform particular functions or impleznent particular abstract data types.
'rhe methods may also be practiced in a distributed computing environment where fiulctions are performed by remote processing devices that are linked through a communications network. In a distributed.
computing environment, computer executable instructions may be located in both local and remote computer storage media, including memory storage devices.
Figure 8 is a side elevational view of an aircraft 800 having a dimmable head-up display in accordance with yet another embodiment of the disclosure. One may appreciate that embodiments of dimmable head-up display may be employed in a wide variety of circumstances and settings, including cockpits, cabins, and other operator control settings for movable platforms such as motor veliicles, aircraft, maritime vessels, or spacecraft, or other suitable systems including applications with wearable dimmable head-up displays such as visor combiners. For example, an aircraft 800 may have one or more dimmable head-up displays in accordance with an embodiment of the disclosure.
In this etnbodiment, the aircraft 800 includes a fuselage 802 including wing asset-nblies 804, a tail assembly 806, and a landing assembly 808. The aircraft 800 fiirther includes one or more propulsion units 81.0, a control system 812 (not visible), and a host of other systems and sulisystems that enable proper opcration of the aircraft 800. One should appreciate that embodiments of dimmable HUD's in accordance with the disclosure may be employed in the aircraft 800, such as in a cockpit configured dirrtmable HUD 814, and any other suitable areas of the aircraft 800. In general, except for the cockpit configured dirnmable HLTD 814 in accordance with embodiments of the disclosure, the various components and subsysterns of the aircraft. 800 may be of known construction and, for the sake of brevity, will not be described in detail herein.
Although the aircraft 800 shown in Figure 8 is generally representative of a commercial passenger aircraft, including, for example, the 737, 747, 757, 767, 777, and 787 niodels comnlercially available fi-o.in The Boeing Company of Chicago, Illinois, the inventive apparatus and methods disclosed herein may also be employed in the assembly of virtually any other types of aircraft. More specifically, the teachings of the present disclosure may be applied to the manufacture and assembly of other passenger aircraft, figliter aircraft, cargo aircraft, rotary aircraft, and any other types of manned or unmanned aircraft, including those described, for example, in The Illustrated E.ncyclopedia of Military Aircraft by Enzo Angelucci, published by = CA 02674878 2009-07-07 Book Sales Publishers, Septeznber 2001, and in Jane's All the World's Aircraft published by Jane's Information Group of Coulsdon, Surrey, United Kingdom, -which texts are incorporated herein by reference.
While preferred and alternate embodiments of the disclosure have been illustrated and described, as noted above, many changes can be made without departing from the spirit and scope of the disclosure. Accordingly, the scope of the disclosure is not limited by the disclosure of these preferred and alternate e.mbodiments. Instead, the disclosure should be determined entirely by reference to the claims that follow.
Therefore, the first light sensor 412 detects the light intensity before the light 404 passes through the combiner 116.
The second light sensor 414 is disposed between the combiner 116 and the operator 402.
Therefore, the second light sensor 414 detects the light intensity after the light (i.e., resulting light 410) passes through the combiner 116. In some embodiments, the HUD may only include one of the light sensors 412, 414.
The first light sensor 412 may provide a fixed relationship between the outside brightness and the degree of dimniing of the combiner 116. For example, the first light sensor 412 may be calibrated to adjust the transmissivity of the combiner 116 to a substantially transparent state when the first light sensor 412 detects a low intensity of light. NVhen the first light sensor 412 detects a high intensity of light, the first light sensor 412 may restrict the transmissivity of the combiner 116 to reduce the light intensity viewed by the operator 402.
'The second light sensor 414 may provide a closed loop control system, whlcll adjusts the dimming of the combiner 116 based on the light intensity the second light sensor 414 detects froni the resulting light 410 after it passes through the combiner 116. For example, the second light sensor 414 may calibrate the transmissivity of the combiner 116 by periodically sensing the light intensity, and then adjusting the transmissivity according the measured light intensity. Therefore, the second ligh.t sensor 414 may receive a relatively constant light intensity level through the combiner 116 by continually adjusting the transmissivity of the conibir,er 116.
In a further embodiment of the dimmable HUD 400, the second light sensor 414 measures inte.rior light intensity ineasurernents, arid the combiner control system 308, as shown in Figure 3, autoinatically maintains the transmission levels of the one or more combiner portions of the combiner 116 at suitable transmission levels unless the desired transmission level renders the interior light intensity measurements below a predetennined (or minimum desired) threshold. Wlien the desired transmission level results in the light intensity measurements being below the certain threshold, the combiner control system 308 adjusts (e.g., increases) the t.ransmission level of one or niore combiner portions of the combiner 1.16 to any level that results in the light intensity measurements being at or above the certain threshold.
The combiner control system 308 may periodically or continuously evaluate the light intensity measureinents provided by the second light sensor 414, and may pe,`riodically or continuously adjust the' transmission level of the combiner 116 when the light intensity measurernents fall below the certain threshold.
In another einbodiment, the combiner control system 308 may be further adapted to adjust the transmissivity of the conibiner 116 based on a second predetermined threshold, such as, for example, a maximum allowable (or maxinlum desired) light intensity measurement. More specifically, the second light sensor 414 may measure a light intensity (e.g within the structure) that exceeds a maximum desired threshold. When the combiner control systc. 308 determines that the measured light intensity has exceeded the maximum desired threshold, the combiner control system 308 may automatically adjust (e.g., decrease) the transmissivity of one or more combiner portions of the combiner 116 to lower the measured light intensity. In a particLilar embodiment, a vehicle, such as a cockpit of an aircraft, may employ the head-up display 400 and use it to provide protection t.o the pilot (or other vehicle operator) from a high intensity light or laser.
I.n yet aiiother embodiment, the head-up display 400 may be configured with a fail-safe mechanisin. In this embodimerit, if any component of the head-up display 400 experiences a problem, the fail-safe mechanism (e.g., a component of the combiner control system 308) may automatically default the transmission level of the combiner 116 to a predetennined acceptable level. In some emboditnents, such as in a cockpit of an aircraft, the predetermined acceptable level may be a relatively high transmission level that prosrides normal, non-attenuated visibility levels to the operator 302. In alternate embodiments, however, the fail-safe mechanism rnay result in reduced transmissivity, in comparison with a norinal, non-at.tenuated visibility level. In further einbodiments, the diinmable combiner 116 may be movably configured in front of an operator 302. For example, the conibiner 116 may nlove outside of the operator's line of sigbt through the front window 202 if the dimmable combiner fails to operate properly, therefore giving the operator an unobstructed view through the front rindow 202.
Figure 5 is a schematic of a segmented dimmable head-up display 500 in accordance with an enibodiment of the disclosure. hi some embodiments, the coinbiner 116 may include one or more segments to provide varying levels of transmissivity of light through different segments of the combiner 116. For example, the combiner 116 may be divided vertically 502, horizontally 504, or both to create segments of the combiner 116.
In some embodiments, the combiner may be segmented by an outer segmenting parameter 506 and an iriner segnienting parameter 508. It may be advantageous to position the segmenting parameters 506, 508 to reduce the light intensity from specific areas of the combiner 116, such as the outer segnient 510, including sub-segmetits 510a-510d, while maintaining more transmissivity in an intermediary segment 512 or inner segment 514. Further, each seginent 510, 512, 514 may be subdivided borizontally, vertically, or botli to form corresponding sub-segqn.ents 510a-510d, 512a-512d, 514a-514d, respectively. Segmenting the combiner 116 may include utilizing fewer or more segmenting parameters. For example, a segment, such as segment 510, 512, 514, may include any number of sub-segments. Additionally, the configuration of segmenting parameters may be configured in any number of patterns, including elliptical segments, rectangular segtnents, circular segments, or other segment fonns or sliapes.
Each seginent may be configured to provide adjustable transmissivity of light through the combiner 116. For example, the outer segment 510 may be configured to provide a different transniissivity of liglrt through the combiner 116 that the transmissivity of light through the intei-mediate segment 512 or inner segi.nent 510. Further, each segnnent may be controlled autoniatically, such as by the combiner control systerr- 308 (Figure 3) or by one or more operator input devices 306.
Figure 6 is an isometric view of a head-mountable dunmable head-up display 600 in accordance with another embodiment of the disclosure. In some embodiments, the combiner 602 niay be wearable, such as in the fonn of a visor 604 configured with a helmet 606.
For example, the hehnet 606 xnay be an aviator helmet including a cliinstrap 608 and protective cushioning 610. In other t~nbodimeitts, the IiUD 600 rnay be configured without a helmet 606, such as in a pair of glasses or a mountable head visor. The HUD 600 may include intenaally integrated display modules to display information to an operator. The coinbiner 602 may include at least one variable transm3ssivity portion of the combiner 116. Smaller sub-segments may alsc segment the transmissivity portion. The combiner 602 may be controlled automatically, such as by the combiner control system 308 (Figure 3) or by one or more operator input derices 306.
Figure 7 is a flow chart for a system (or method) 700 for provicl.ing a dimmable head-up display in accordance with embodiments of the disclosure. In this embodiment, the system 700 begins at a state of initial conditions at a block 702. At a decision block 704, the system 700 determines whether to adjust the transmissivity of the combiner to increase or reduce the light intensity viewable through the combiner. If the system 700 selects adjusting the transmissivity of the combiner at the decision block 704, at a block 706, the systeni receives one or more user inputs from the operator input device 304. At a block 708, the combiner control system 308 receives one or more sensor inputs from the light sensor 122. At a block 710, the system 700 adjusts the transmissivity of the conibiner utilizing information from the blocks 706, 708, or both. If the system 700 does not select adjusting the transmissivity of the combiner at the block 704, the system proceeds to a decision block 712.
At the decision block 712, the system 700 makes a determination whether to adjust the transinissivity of the combiner incrementally. For example, at the decision block 712, the system 700 may implement a calibration algoritlun to fine tune the transmissivity of the combiner. If the system 700 selects an incremental adjustment, at a decision block 714, the systern detennines wheth.er the light intensity is too liigh. If so, then at a block 716, the system 700 incrementally reduces the transmissivity of the combiner 116 if the combiner is not already at a minimum allowabl.e level, and then the system returns to block 71.4.
Alternately, if the light level is not too high (block 714), the lit;ht level is deemed to be too low, and the transinissivity of combiner 116 is incrementally increased provided that the combiner is not already at a maximuz.n level, and then the system returns to the decision block 712.
If the system 700 does not select an incremental adjustment at the decision block 712, at a decision block 720, the system determin:,s whether to adjust the combiner display. For example, the combinei- display produced by the projector 1.18 may be difficult to see wher: the system adjusts the transmi.ssivity of the combiner 1.16 at the block 710. Therefore, it may be desirable to adjust the contrast, brightness, or other display characteristics of the combiner display to allow an operator to view the displayed information easier. If the system 700 selects adjusting the display characteristics of the combiner 116 at the decision block 720, at a block 722, the system receives one or more user inputs from the operator input device 306. At a block 724, the image control system 310 receives one or more sensor inputs from the light sensor 122. At a block 726, the system 700 adjusts the display characteristics of the combiner 116 utilizing the information from the blocks 722, 724, or both. lf the system 700 does not select adjusting the display characteristics of the combiner at the decision block 720, the system may reiterate to the decision block 704.
Although the systein 700 makes general reference to a combiner 116, one should appreciate that embodiments of the system 700 may apply to segments or sub-segments of the combiner. For example, with reference to Figure 5, the systein 700 may separately adjust the segments 510, 512, 514, or it may adjust them in combination to create the desirable level of transmissivity at the block 710.
Generally, any of the functions described herein can be impleniented using software, firmware (e.g., fixed logic circuitry), hardware, manual processing, or any combination of these implementations. In the case of a soti:ware iinplementation, the module, functionality, or logic described herein represents program code that perforins specified tasks when executed on processor(s) (e.g., any of microprocessors, controllers, and the like). The prograzn code can be stored in one or more computer readable nzemory devices. Further, the features and aspects described herein are platform-indepeiident such that the tecluliques may be implemented on a variety of coinmercial coinputing platforms having a variety of processors.
It will also be appreciated that methods and systeins in accordance with the teachings of the present disclosure may be described in the general context of computer executable instructions. Generally, coinputer executable instructions can include routines, programs, objects, components, data structures, procedures, modules, functions, and the like that perform particular functions or impleznent particular abstract data types.
'rhe methods may also be practiced in a distributed computing environment where fiulctions are performed by remote processing devices that are linked through a communications network. In a distributed.
computing environment, computer executable instructions may be located in both local and remote computer storage media, including memory storage devices.
Figure 8 is a side elevational view of an aircraft 800 having a dimmable head-up display in accordance with yet another embodiment of the disclosure. One may appreciate that embodiments of dimmable head-up display may be employed in a wide variety of circumstances and settings, including cockpits, cabins, and other operator control settings for movable platforms such as motor veliicles, aircraft, maritime vessels, or spacecraft, or other suitable systems including applications with wearable dimmable head-up displays such as visor combiners. For example, an aircraft 800 may have one or more dimmable head-up displays in accordance with an embodiment of the disclosure.
In this etnbodiment, the aircraft 800 includes a fuselage 802 including wing asset-nblies 804, a tail assembly 806, and a landing assembly 808. The aircraft 800 fiirther includes one or more propulsion units 81.0, a control system 812 (not visible), and a host of other systems and sulisystems that enable proper opcration of the aircraft 800. One should appreciate that embodiments of dimmable HUD's in accordance with the disclosure may be employed in the aircraft 800, such as in a cockpit configured dirrtmable HUD 814, and any other suitable areas of the aircraft 800. In general, except for the cockpit configured dirnmable HLTD 814 in accordance with embodiments of the disclosure, the various components and subsysterns of the aircraft. 800 may be of known construction and, for the sake of brevity, will not be described in detail herein.
Although the aircraft 800 shown in Figure 8 is generally representative of a commercial passenger aircraft, including, for example, the 737, 747, 757, 767, 777, and 787 niodels comnlercially available fi-o.in The Boeing Company of Chicago, Illinois, the inventive apparatus and methods disclosed herein may also be employed in the assembly of virtually any other types of aircraft. More specifically, the teachings of the present disclosure may be applied to the manufacture and assembly of other passenger aircraft, figliter aircraft, cargo aircraft, rotary aircraft, and any other types of manned or unmanned aircraft, including those described, for example, in The Illustrated E.ncyclopedia of Military Aircraft by Enzo Angelucci, published by = CA 02674878 2009-07-07 Book Sales Publishers, Septeznber 2001, and in Jane's All the World's Aircraft published by Jane's Information Group of Coulsdon, Surrey, United Kingdom, -which texts are incorporated herein by reference.
While preferred and alternate embodiments of the disclosure have been illustrated and described, as noted above, many changes can be made without departing from the spirit and scope of the disclosure. Accordingly, the scope of the disclosure is not limited by the disclosure of these preferred and alternate e.mbodiments. Instead, the disclosure should be determined entirely by reference to the claims that follow.
Claims (17)
1. A dimmable head-up display (106/400), comprising:
a display portion (408) configured to provide head-up display (106/400) information to an operator (120); and a dimmable portion (406) coupled to the display portion (408) configured to change a transmissivity of the display portion (408) from a first transmissivity level to a second transmissivity level.
a display portion (408) configured to provide head-up display (106/400) information to an operator (120); and a dimmable portion (406) coupled to the display portion (408) configured to change a transmissivity of the display portion (408) from a first transmissivity level to a second transmissivity level.
2. The head-up display (106/400) of claim 1, wherein the dimmable portion (406) includes a plurality of dimmable segments.
3. The head-up display (106/400) of claim 2, wherein the plurality of dimmable segments includes independent variable transmissivity.
4. The head-up display (106/400) of claim 2, wherein the display portion (408) includes a plurality of display segments providing head-up display (106/400) information, the plurality of display segments corresponding to the plurality of dimmable segments.
5. The head-up display (106/400) of claim 1, further comprising a combiner control system (126/308) in communication with the dimmable portion (406) and configured to receive one or more inputs including:
a manual control input from an operator (120); and a light sensor (122) input from a light sensor (122).
a manual control input from an operator (120); and a light sensor (122) input from a light sensor (122).
6. The head-up display (106/400) of claim 1, wherein the head-up display (106/400) is configured in one of:
a helmet mounted head-up display (600);
a movable visor (604) head-up display (106/400); and a fixably mounted head up display (106/400) in a moveable platform.
a helmet mounted head-up display (600);
a movable visor (604) head-up display (106/400); and a fixably mounted head up display (106/400) in a moveable platform.
7. The head-up display (106/400) of claim 1, wherein the display portion (408) is configured to receive a projected display from a projector (11.8).
8. The head-up display (106/400) of claim 1, wherein the display portion (408) includes a liquid crystal display to provide information to the operator (120).
9. A system for providing a dimmable head-up display (106/400), comprising:
a dimmable combiner (116) configured to provide head-up display (106/400) information to an operator (120), the dimmable combiner (116) adjustable from a substantially transparent level to a less transparent level;
a light sensor (122) configured to detect the light intensity of an environment surrounding the dimmable combiner (116); and a combiner control system (126/308) configured to receive a light sensor (122) signal from the light sensor (122) and transmit a control signal to the dimmable combiner (116) for adjusting the transmissivity of the dimmable combiner (116).
a dimmable combiner (116) configured to provide head-up display (106/400) information to an operator (120), the dimmable combiner (116) adjustable from a substantially transparent level to a less transparent level;
a light sensor (122) configured to detect the light intensity of an environment surrounding the dimmable combiner (116); and a combiner control system (126/308) configured to receive a light sensor (122) signal from the light sensor (122) and transmit a control signal to the dimmable combiner (116) for adjusting the transmissivity of the dimmable combiner (116).
10. The system of claim 9, further comprising a manual combiner (116) control input configured to receive an operator (120) input, the combiner control system (126/308) configured to receive the operator (120) input from the manual combiner (116) control input, the control signal for adjusting the transparency of the dimmable combiner (116) depending on at least one of the operator (120) input and the light sensor (122) signal.
11. The system of claim 9, further comprising:
an imaging device configured to produce an image of a head-up display (106/400) with the combiner (116) for viewing by an operator (120); and an imaging control system (310) configured to receive an input from the light sensor (122) and transmit a signal to the imaging device for adjusting the head-up display (106/400) on the dimmable combiner (116).
an imaging device configured to produce an image of a head-up display (106/400) with the combiner (116) for viewing by an operator (120); and an imaging control system (310) configured to receive an input from the light sensor (122) and transmit a signal to the imaging device for adjusting the head-up display (106/400) on the dimmable combiner (116).
12. The system of claim 11, wherein the imaging control system (310) is configured to receive a manual imaging control input configured to receive an image input, the imaging control system (310) configured to receive the image input from the manual imaging control input and transmit the image input to the imaging device for adjusting the imaging device.
13. The system of claim 11, wherein the combiner control system (308) is in communication with the imaging control system (310), the combiner control system (308) sending a signal to the imaging control system (310) when the combiner control system (308) adjusts the transparency of the combiner (116), the imaging control system (310) processing the signal and adjusting transparency of the combine.r (116) to improve the head-up display (106/400) information visibility for the operator (120).
14. The system of claim 9, wherein the combiner (116) is segmented into a plurality of dimmable combiner (116) portions.
1.5. The system of claim 9, wherein the dimmable head-up display (106/400) is configured for at least one of an aircraft (102/800) and a passenger vehicle.
16. The system of claim 9, wherein head-up (106/400) display includes a fail-safe setting configured to increase the transmissivity of the dimmable combiner (116) to a substantially transparent state.
17. The system of claim 9, wherein the dimmable combiner (116) utilizes one of electrochromic and photochromic to adjust the transmissivity of the dimmable combiner (116).
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| US11/682,255 US7893890B2 (en) | 2007-03-05 | 2007-03-05 | Electrically dimmable combiner optics for head-up display |
| US11/682,255 | 2007-03-05 | ||
| PCT/US2008/053752 WO2008109231A2 (en) | 2007-03-05 | 2008-02-12 | Electrically dimmable combiner optics for head-up display |
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| CA2674878C CA2674878C (en) | 2013-07-16 |
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| CA2674878A Active CA2674878C (en) | 2007-03-05 | 2008-02-12 | Electrically dimmable combiner optics for head-up display |
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2007
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- 2008-02-12 CA CA2674878A patent/CA2674878C/en active Active
- 2008-02-12 JP JP2009552786A patent/JP5279733B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| JP2010521347A (en) | 2010-06-24 |
| US20080218434A1 (en) | 2008-09-11 |
| US7893890B2 (en) | 2011-02-22 |
| WO2008109231A3 (en) | 2008-10-30 |
| CA2674878C (en) | 2013-07-16 |
| JP5279733B2 (en) | 2013-09-04 |
| WO2008109231A2 (en) | 2008-09-12 |
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