US20050200934A1 - Dimming control system for an array of electrochromic devices - Google Patents

Dimming control system for an array of electrochromic devices Download PDF

Info

Publication number
US20050200934A1
US20050200934A1 US10/974,240 US97424004A US2005200934A1 US 20050200934 A1 US20050200934 A1 US 20050200934A1 US 97424004 A US97424004 A US 97424004A US 2005200934 A1 US2005200934 A1 US 2005200934A1
Authority
US
United States
Prior art keywords
electrochromic
window
control
electrochromic device
plurality
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
Application number
US10/974,240
Inventor
Kevin Callahan
Roland Schafer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to US55245304P priority Critical
Priority to US55258904P priority
Priority to US55260604P priority
Application filed by Boeing Co filed Critical Boeing Co
Priority to US10/974,240 priority patent/US20050200934A1/en
Assigned to BOEING COMPANY, THE reassignment BOEING COMPANY, THE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CALLAHAN, KEVIN S., SCAFER, ROLAND L., JR.
Publication of US20050200934A1 publication Critical patent/US20050200934A1/en
Priority claimed from US11/877,133 external-priority patent/US8064120B2/en
Application status is Abandoned legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02FDEVICES OR ARRANGEMENTS, THE OPTICAL OPERATION OF WHICH IS MODIFIED BY CHANGING THE OPTICAL PROPERTIES OF THE MEDIUM OF THE DEVICES OR ARRANGEMENTS FOR THE CONTROL OF THE INTENSITY, COLOUR, PHASE, POLARISATION OR DIRECTION OF LIGHT, e.g. SWITCHING, GATING, MODULATING OR DEMODULATING; TECHNIQUES OR PROCEDURES FOR THE OPERATION THEREOF; FREQUENCY-CHANGING; NON-LINEAR OPTICS; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
    • G02F1/00Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics
    • G02F1/01Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour 
    • G02F1/15Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect
    • G02F1/1514Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect characterised by the electrochromic material, e.g. by the electrodeposited material
    • G02F1/1523Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect characterised by the electrochromic material, e.g. by the electrodeposited material comprising inorganic material
    • G02F1/1525Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect characterised by the electrochromic material, e.g. by the electrodeposited material comprising inorganic material characterised by a particular ion transporting layer, e.g. electrolyte
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476Canopies; Windscreens or similar transparent elements
    • B64C1/1484Windows
    • GPHYSICS
    • G02OPTICS
    • G02FDEVICES OR ARRANGEMENTS, THE OPTICAL OPERATION OF WHICH IS MODIFIED BY CHANGING THE OPTICAL PROPERTIES OF THE MEDIUM OF THE DEVICES OR ARRANGEMENTS FOR THE CONTROL OF THE INTENSITY, COLOUR, PHASE, POLARISATION OR DIRECTION OF LIGHT, e.g. SWITCHING, GATING, MODULATING OR DEMODULATING; TECHNIQUES OR PROCEDURES FOR THE OPERATION THEREOF; FREQUENCY-CHANGING; NON-LINEAR OPTICS; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
    • G02F1/00Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics
    • G02F1/01Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour 
    • G02F1/15Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect
    • G02F1/1506Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect caused by electrodeposition, e.g. electrolytic deposition of an inorganic material on or close to an electrode
    • GPHYSICS
    • G02OPTICS
    • G02FDEVICES OR ARRANGEMENTS, THE OPTICAL OPERATION OF WHICH IS MODIFIED BY CHANGING THE OPTICAL PROPERTIES OF THE MEDIUM OF THE DEVICES OR ARRANGEMENTS FOR THE CONTROL OF THE INTENSITY, COLOUR, PHASE, POLARISATION OR DIRECTION OF LIGHT, e.g. SWITCHING, GATING, MODULATING OR DEMODULATING; TECHNIQUES OR PROCEDURES FOR THE OPERATION THEREOF; FREQUENCY-CHANGING; NON-LINEAR OPTICS; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
    • G02F1/00Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics
    • G02F1/01Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour 
    • G02F1/15Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect
    • G02F1/1514Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect characterised by the electrochromic material, e.g. by the electrodeposited material
    • G02F1/1523Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect characterised by the electrochromic material, e.g. by the electrodeposited material comprising inorganic material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D2011/0061Windows displaying outside view, artificially generated
    • GPHYSICS
    • G02OPTICS
    • G02FDEVICES OR ARRANGEMENTS, THE OPTICAL OPERATION OF WHICH IS MODIFIED BY CHANGING THE OPTICAL PROPERTIES OF THE MEDIUM OF THE DEVICES OR ARRANGEMENTS FOR THE CONTROL OF THE INTENSITY, COLOUR, PHASE, POLARISATION OR DIRECTION OF LIGHT, e.g. SWITCHING, GATING, MODULATING OR DEMODULATING; TECHNIQUES OR PROCEDURES FOR THE OPERATION THEREOF; FREQUENCY-CHANGING; NON-LINEAR OPTICS; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
    • G02F1/00Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics
    • G02F1/01Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour 
    • G02F1/15Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect
    • G02F1/153Constructional details
    • GPHYSICS
    • G02OPTICS
    • G02FDEVICES OR ARRANGEMENTS, THE OPTICAL OPERATION OF WHICH IS MODIFIED BY CHANGING THE OPTICAL PROPERTIES OF THE MEDIUM OF THE DEVICES OR ARRANGEMENTS FOR THE CONTROL OF THE INTENSITY, COLOUR, PHASE, POLARISATION OR DIRECTION OF LIGHT, e.g. SWITCHING, GATING, MODULATING OR DEMODULATING; TECHNIQUES OR PROCEDURES FOR THE OPERATION THEREOF; FREQUENCY-CHANGING; NON-LINEAR OPTICS; OPTICAL LOGIC ELEMENTS; OPTICAL ANALOGUE/DIGITAL CONVERTERS
    • G02F1/00Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics
    • G02F1/01Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour 
    • G02F1/15Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect
    • G02F2001/164Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating, or modulating; Non-linear optics for the control of the intensity, phase, polarisation or colour  based on an electrochromic effect the electrolyte is made of polymers

Abstract

Electrochromic device control systems and methods are disclosed. In one embodiment, a window system includes a plurality of transparent windows, a plurality of electrochromic devices, a plurality of control modules, and a main controller. Each transparent window has an electrochromic device operatively associated therewith. A control module is operatively coupled to each electrochromic device and is adapted to controllably adjust an electric field to activate and de-activate the electrochromic device. Finally, the main controller is operatively coupled to the plurality of control modules and adapted to simultaneously adjust the electric fields of the plurality of electrochromic devices to activate and de-activate the plurality of electrochromic devices in unison. In one particular embodiment, a window dimming control system in accordance with the present invention may advantageously be incorporated into an existing cabin services system of a passenger aircraft.

Description

    CROSS REFERENCE TO RELATED APPLICATIONS
  • This patent application is related to U.S. Patent Application No. (undetermined) entitled “Low Vapor Pressure Solvent for Electrochromic Devices,” filed under Attorney Docket No. BING-1-1086 concurrently herewith on Oct. 27, 2004; to U.S. Patent Application No. (undetermined) entitled “Multi-Color Electrochromic Device,” filed under Attorney Docket No. BING-1-1085 concurrently herewith on Oct. 27, 2004; and to U.S. Pat. No. 6,747,780 entitled “Electrochromic Organic Polymer Syntheses and Devices Utilizing Electrochromic Organic Polymers”, Xu et al., issued Jun. 8, 2004; which applications are hereby incorporated by reference.
  • PRIORITY CLAIM
  • This non-provisional patent application claims priority from U.S. Provisional Application No. 60/552,453, filed on Mar. 12, 2004; from U.S. Provisional Application No. 60/552,589, filed on Mar. 12, 2004; and from U.S. Provisional Application No. 60/552,606, filed on Mar. 12, 2004, which provisional applications are incorporated herein by reference.
  • FIELD OF THE INVENTION
  • The present disclosure relates to apparatus and methods for electrochromic devices, and more specifically, to apparatus and methods for dimming or otherwise controlling arrays of electrochromic devices.
  • BACKGROUND OF THE INVENTION
  • Electrochromic devices are often used as windows, shades, dividers, mirrors, or electronic displays, that change color or degree of opacity in respect to an applied electric field or current. Such an electrochromic device typically is a multi-layer assembly. Outer layers of the electrochromic device typically are electrodes that are optically clear [i.e. substantially transparent to light in wavelengths of the visual spectrum or at other desired wavelengths, albeit in some instances bearing a limited tint or color]. At least one electrochromic layer is sandwiched between the electrodes. This layer is able to change color or opacity in response to changes in the applied electric field or current to create visual effects. The electrochromic layer is often an organic polymer film or an inorganic thin film of an electrochromic material. When the voltage is applied across the outer conductors, ions in an electrolyte typically move to the electrochromic layer causing the electrochromic material to change color states. Reversing the voltage moves ions away from the electrochromic layer, restoring the device to its previous state.
  • An electrolyte is often utilized in an electrochromic device to act as a reservoir for the ions that activate the electrochromic layer and/or provide a medium for transporting ions between a separate ion reservoir material or counter-electrode and the electrochromic layer. A salt such as lithium perchlorate (LiClO4) or trifluorosulfonimide (LiN(CF3SO2)2) may be utilized to provide the ions to activate and deactivate the electrochromic layer. The salt is typically dissociated in a solvent in the electrolyte, freeing the ions for use in activating the electrochromic layer.
  • Gel electrolytes in electrochromic devices are often preferred because they are less likely to leak than liquids and more stable dimensionally. One gel electrolyte usable in a preferred electrochromic device includes a solid polymer matrix, especially of polymethylmethacrylate (PMMA).
  • While pull down shades of aircraft windows in passenger cabins appear simple, the mechanisms for integrating them into the aircraft are complex, and the labor to install or repair them are high relative to alternatives that are emerging. Electrochromic (EC) devices that darken upon switching a controlling electrical power signal provide promise for lower initials and lifecycle costs.
  • SUMMARY OF THE INVENTION
  • The present invention provides systems and methods for EC array control systems, including control systems for dimming or otherwise controlling windows for commercial passenger aircraft. In one embodiment, a window system includes a plurality of transparent windows, a plurality of electrochromic devices, a plurality of control modules, and a main controller. Each transparent window has an electrochromic device operatively associated therewith. A control module is operatively coupled to each electrochromic device and is adapted to controllably adjust an electric field to activate and de-activate the electrochromic device. Finally, the main controller is operatively coupled to the plurality of control modules and adapted to simultaneously adjust the electric fields of the plurality of electrochromic devices to activate and de-activate the plurality of electrochromic devices in unison. In one particular embodiment, a window dimming control system in accordance with the present invention may advantageously be incorporated into an existing cabin services system of a passenger aircraft.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Preferred and alternate embodiments of the present invention are described in detail below with reference to the following drawings.
  • FIG. 1 is an exploded isometric view of an aircraft window incorporating an electrochromic device.
  • FIG. 2A is a perspective view of an aircraft interior incorporating a multi-color electrochromic device (shown in an inactivated transparent state) as a compartment divider.
  • FIG. 2B is a perspective view of an aircraft interior incorporating a multi-color electrochromic device exhibiting a logo (shown in an activated colored state).
  • FIG. 3A is an exemplary electrochromic device incorporating an exemplary γ-butyrolactone (gamma-butyrolactone or GBL) electrolyte in a deactivated state.
  • FIG. 3B is an exemplary electrochromic device including an exemplary GBL electrolyte in an activated state.
  • FIG. 4A is an enlargement of an exemplary interface between an electrochromic layer and an exemplary GBL electrolyte, with the electrochromic layer in a deactivated state.
  • FIG. 4B is an enlargement of an exemplary interface between an electrochromic layer and an exemplary GBL electrolyte, with the electrochromic layer in an activated state.
  • FIG. 5 is a chart of ionic conductivity of exemplary gel electrolytes over time.
  • FIG. 6 is a cross-section of an exemplary electrochromic aircraft window incorporating an exemplary GBL electrolyte.
  • FIG. 7 is a plan view of an exemplary multi-color electrochromic panel exhibiting a pattern.
  • FIG. 7A is an enlarged view of a section of the electrochromic panel of FIG. 7 showing exemplary interspersed pixels of a multi-color electrochromic layer.
  • FIG. 8 is a cross-section of an exemplary multi-color electrochromic device.
  • FIG. 9 is a cross-section of deposition of a multi-color electrochromic layer on a substrate.
  • FIG. 10 is a perspective view of an aircraft interior incorporating a multi-color electrochromic device exhibiting a pattern (shown in an activated colored state).
  • FIG. 11 is a schematic view of a window dimming system.
  • FIG. 12 is a schematic view of an alternate window dimming system.
  • FIG. 13 is a side elevational view of an aircraft in accordance with an alternate embodiment of the present invention.
  • FIG. 14 shows a top elevational view of a representative passenger aircraft floor plan incorporating an embodiment of the present invention.
  • FIG. 15A shows an end cross-sectional view of a passenger aircraft section incorporating an embodiment of the present invention.
  • FIG. 15B shows an end cross-sectional view of an alternate passenger aircraft section similar to FIG. 15B.
  • FIG. 16 is a front elevational view of a window assembly incorporating an electrochromic device.
  • FIG. 17 is an exploded isometric view of the window assembly of FIG. 16.
  • FIG. 18 is a partial cross-sectional view of the window assembly FIG. 16.
  • FIG. 19 is an exploded isometric view of another window assembly that includes an electrochromic device.
  • DETAILED DESCRIPTION
  • The present invention relates to electrochromic devices. Many specific details of certain embodiments of the invention are set forth in the following description and in FIGS. 1-19 to provide a thorough understanding of such embodiments. One skilled in the art, however, will understand that the present invention may have additional embodiments, and that the present invention may be practiced without several of the details described in the following description.
  • Embodiments of the present invention may include a γ-butyrolactone (gamma-butyrolactone or GBL) bearing electrolyte for electrochromic panels. In one embodiment, a GBL electrolyte exhibits high ionic conductivity, high transmittance of light, and stability over time and temperature. These features are useful, for example, in aircraft applications such as electrochromic shades for aircraft windows, replacing hand pulled window shades.
  • This application incorporates by this reference Xu et al., Electrochromic Organic Polymer Synthesis and Devices using Electrochromic Organic Polymers, U.S. Pat. No. 6,747,780 B2, issued Jun. 8, 2004; Xu, C., Liu, L., Legniski, S., Le Guilly, M., Taya, M., Weidner, A., Enhanced Smart Window Based on Electrochromic Polymers, Smart Structures and Materials 2003: Electroactive Polymer Actuators and Devices (EAPAD), edited by Bar-Cohen, Y., Proceedings of the SPIE, Volume 5051, pp. 404-411 (July, 2003) (hereinafter “Reference A”); Xu, C., Liu, L., Legniski, S., Le Guilly, M., Taya, M, Gel Electrolyte Candidates for Electrochromic Devices (ECD), Smart Structures and Materials 2004, Electroactive Polymer Actuators and Devices (EAPAD), edited by Bar-Cohen, Y., Proceedings of the SPIE, Volume 5385, pp. 319-325 (July, 2004) (hereinafter “Reference B”); and Liu, L., Xu, C., Legniski, S., Ning, D., M., Taya, M, Design of Smart Window based on Electrochromic Polymers: New Derivatives of 3,4-alkylenedioxythiophene, Electroactive Polymer Actuators and Devices (EAPAD), edited by Bar-Cohen, Y., Proceedings of the SPIE, Volume 5385, pp. 454-460 (July, 2004) (hereinafter “Reference C”).
  • FIG. 1 is an exploded view of an exemplary electrochromic device used as an aircraft window shade 5 in accordance with an embodiment of the present invention. A structural window 40 is installed in an aircraft fuselage wall 60 with a seal 30. Inboard of the structural window 40 is a safety backup pane 20. An electrochromic shade 10 is held in place between the safety pane 20 and an aircraft interior window molding 50 surrounding the window on the interior of the aircraft. When the electrochromic shade 10 is activated, it changes color and/or opacity states, typically either dimming or brightening the aircraft interior by controlling entry of light from outside the aircraft.
  • Turning to FIG. 2A, a multi-color electrochromic panel 210 in accordance with an embodiment of the invention is shown positioned as a part of a cabin compartment divider 220 in the interior 200 of a passenger aircraft. In FIG. 2A, the panel 210 is shown in the non-activated state, where it is substantially transparent, permitting viewing through the panel 210. The multi-color electrochromic panel 210 is held by, and forms a part of, the passenger compartment divider 220 that divides different segments of the passenger compartment from each other. When the electrochromic display 210 is substantially transparent as shown in FIG. 2A, viewing is permitted through the divider 220. In vehicular applications, for example, viewing through the divider 220 may be desirable for loading and unloading purposes, regulatory, or safety reasons.
  • In some embodiments, a control panel may be programmed to change the opacity of the electrochromic display 210 to change the environment based upon time of day, the status of the flight (take-off, landing, etc.), or other criteria. Alternately, the electrochromic display 210 may be programmed to change state when a sufficient amount brightness level is sensed within the cabin. An exemplary display 210 in a vehicle or any other environment may thus change with time, at certain times, or during certain events. The display 210 may thus adjust the natural lighting in the interior 200 of the aircraft, or any other vehicle or architectural environment. The display 210 may also be used in a combination with a window, in addition to forming a divider 220.
  • FIG. 2B shows a passenger aircraft cabin interior 300 similar to that in FIG. 8A. An embodiment of a multi-color electrochromic panel 310 is installed in the cabin interior 300 as a part of a cabin compartment divider 320. In FIG. 2B, the panel 310 is shown in the activated state exhibiting a multi-color logo 330. In an activated state, the panel 310 displays the logo 330, and passengers cannot see through the panel 310, visually dividing the passenger compartments. In a non-activated state, the multi-color logo 330 disappears and the panel 310 is transparent, in the manner shown in FIG. 2A.
  • FIG. 3A shows an exemplary electrochromic device 405 in cross-section in accordance with an embodiment of the invention in a deactivated state 461. The device 405 includes a first transparent electrode 410 and a second transparent electrode 440. Disposed between the first electrode 410 and the second electrode 440, and adjacent to the first electrode 410 is an electrochromic layer 420. The electrochromic layer 420 in this example changes color or darkens when it is in a reduced state. By way of example, but not limitation, the electrochromic layers may include a polymer film such as poly[3,3-dimethyl-3,4-dihydro-2H-thieno[3,4-b][1,4]dioxepine] (PProDOT-(CH3)2).
  • As further shown in FIG. 3A, positioned between the electrochromic layer 420 and the second electrode 440 is an electrolyte layer 430 including an embodiment of a γ-butyrolactone (gamma-butyrolactone or GBL) gel electrolyte (GBL electrolyte) 431. The GBL electrolyte 431 may include GBL and a salt that when dissociated activates the electrochromic layer 420 with the application of an electric field. GBL (C4H6O2) is an essentially colorless cyclic ester with a comparatively low vapor pressure capable of performing as a solvent for the salt. Depending upon the desired application, other known electrolytes suitably may be included in the electrolyte layer 430.
  • An electric field (not shown) is applied to the electrochromic layer 420 and the GBL electrolyte 431 to activate and deactivate the electrochromic layer 420. In this embodiment, the electric field is provided by an electrical power source 460 connected to the first electrode 410 and the second electrode 440. The first electrode 410 and the second electrode 440 may suitably include glass, acrylic or polycarbonate coated with Indium Tin Oxide (ITO) to form transparent sheet electrodes. Other transparent materials, other electrode materials, and other configurations including small scale printed circuitry grids may suitably be substituted for ITO coated transparent electrodes. In FIG. 3A, the first electrode 410 is connected to the positive pole of the voltage source 460 and the second electrode 440 is connected to the negative pole of the electrical source 460. As further described with reference to FIGS. 4A and 4B, in this configuration, with a positive charge applied to the first electrode 410, the electrochromic layer 420 becomes deactivated and substantially transparent. The first electrode 410, the second electrode 440, and the GBL electrolyte 431 are also substantially transparent, and thus the electrochromic device 405 in this state as a whole is substantially transparent.
  • The term transparent or colorless should not be limited to mean perfectly transparent (i.e. 100% transmissive) or perfectly colorless, but rather, should be read to include conditions of partial or imperfect transmissivity or substantial translucence. The terms transparent or colorless include being substantially optically clear and transmissive in the visual color frequencies of light, like ordinary glass, or having the property of transmitting visual light (or other desired frequencies, as desired) so that objects lying beyond are visible.
  • In FIG. 3B, the electrochromic device 405 of FIG. 3A is connected to a reversed electrical source 462. The negative pole of the reversed electrical source 462 is connected to the first electrode 410, and the positive pole of the reverse electrical source 462 is connected to the second electrode 40. In this configuration, the electrochromic layer 420 changes to an activated state 463, substantially darkens, and thus is no longer substantially transparent. As described with reference to FIGS. 4A and 4B, the reversed electric field (not shown) provided by the reversed electrical source 462 draws positive ions (not shown) from the GBL electrolyte 431 into interaction with the electrochromic layer 420, thereby activating the electrochromic layer 420. In many electrochromic devices, it is not necessary to maintain the electric field or the reversed electric field to maintain the color or transparency of the device, only to change the color state or transparency.
  • FIGS. 4A and 4B are enlarged symbolic diagrams of an exemplary interface 400 such as in FIGS. 3A and 3B, between an electrochromic layer 420 and a GBL-bearing gel electrolyte 431 (GBL electrolyte), with the electrochromic layer 420 in a one of its operative states 461 in FIG. 4A, and in a second operative state 463 in FIG. 4B. In this embodiment, the GBL electrolyte 431 includes a lithium perchlorate salt that dissociates in the GBL bearing electrolyte 430 into perchlorate ions 433 and lithium ions 435. The GBL acts as a solvent dissociating the lithium perchlorate salt into its component ions. As shown in FIG. 4A, while not intending to be bound by theory, in the presence of an electric field, with a positive pole 465 adjacent to and outside of the electrochromic layer 420 side of the interface 400, and a negative pole 467 adjacent to and outside of the GBL electrolyte 431 side of the interface 400, the perchlorate ions 433 in the GBL electrolyte 431 are drawn toward the electrochromic layer 420. This permits the electrochromic layer 420 to gain or maintain an oxidized state, and thus gain or maintain a substantially transparent or non-activated state. Alternately, the lithium ions 435 in the GBL electrolyte 431 are drawn away from the electrochromic layer 420 (towards the negative pole 467), and thus do not activate the electrochromic layer 420.
  • In FIG. 4B, the electric field is reversed from that in FIG. 2A. The negative pole 467 is adjacent to and outside of the electrochromic layer 420, and the positive pole 465 is adjacent to and outside of the GBL electrolyte 431. In this configuration, and again while not intending to be bound by theory, the interface 400 has lithium ions 435 drawn toward the electrochromic layer 420, or towards the negative pole 467 of the electric field, activating the electrochromic layer 420, changing its color state, in this instance substantially darkening it. An electrochromic layer 420 that is activated (in this example in a reduced state) when it forms or is adjacent a cathode or the negative pole of an electric field is a cathodic electrochromic layer. Electrochromic layers may also be anodic, and thus are activated when they form or are adjacent the anode or positive pole of an applied electric field. A GBL electrolyte 431 of the present invention may be used with both cathodic and anodic electrochromic layers.
  • A GBL electrolyte 431 advantageously dissociates and carries the lithium ions 435 and the perchlorate ions 433 while having a comparatively low vapor pressure, and comparatively low toxicity and low flammability as compared to other electrolytes. The GBL in a GBL electrolyte 431 acts as a solvent, disassociating the lithium perchlorate, triflourosulfonimide, another suitable salt, or mixtures thereof to allow ions to activate the electrochromic layer. A gelled GBL electrolyte 431 includes an effective amount of polymethylmethacrylate or other suitable colorless gelling agent. The GBL may also be mixed with one or more additional solvents such as ethylene carbonate, propylene carbonate, other higher molecular weight cyclic esters, or other suitable compounds that are essentially colorless, comparatively non-toxic, and have comparatively low volatility.
  • By way of example, but not limitation, propylene carbonate as a second solvent may suitably be mixed with GBL in a GBL-bearing electrolyte 130. In another embodiment, a suitable GBL-bearing electrolyte 130 includes approximately 70% by weight GBL, 20% by weight propylene carbonate, 3% by weight lithium perchlorate, and 7% by weight polymethylmethacrylate. The weight percentages of the components of this embodiment can vary and still maintain functionality. In some embodiments, the propylene carbonate percentage may be reduced to near 0%, resulting in decreased volatility, but typically higher cost as GBL typically is more expensive than propylene carbonate. Alternately, the weight percentage of propylene carbonate also may be increased to over 20% maintaining functionality, but increasing volatility. Additional quantities of lithium perchlorate may provide additional ions beyond those used in the electrochromic reactions, but typically do not otherwise affect functionality. Considerably smaller weight percentages of lithium perchlorate may decrease color changes in the electrochromic layer. In an alternate embodiment, for example, lithium perchlorate may be substituted or supplemented with the salt trifluorosulfonimide at approximately 3% by weight.
  • The weight percentage of polymethylmethacrylate may also vary, affecting the viscosity of the GBL-bearing electrolyte 130, but not otherwise affecting the functionality of the electrolyte. Some electrochromic devises use essentially liquid electrolytes with little gelling material or polymethylmethacrylate. Considerably larger quantities of polymethylmethacrylate may cause cloudiness in the electrochromic device.
  • GBL has a vapor pressure of approximately 1.5 mm of Hg at 20° C. Compared to higher vapor pressure solvents such as acetonitrile (ACN) with a vapor pressure of 72.8 mm of Hg at 20 C, GBL suitably has lower rates of diffusion and evaporation from electrochromic devices. GBL suitably exhibits high ionic conductivity, high transmittance of light, and stability over time and temperature. The low viscosity of the GBL provides an ionic environment that facilitates high ionic mobility of the salts activating and deactivating the electrochromic layer. In an example embodiment of a GBL bearing electrolyte 130, an electronic grade GBL is used and the GBL is dried over molecular sieves to remove any residual water.
  • GBL may suitably have a high ionic conductivity, resulting in a low activation energy facilitating ionic movement. The activation energy for an exemplary gel electrolyte including GBL, propylene carbonate, lithium perchlorate, and polymethylmethacrylate are approximately 9.7 kJ/mol. ACN as an electrolyte, by way of comparison, has an activation energy of 83 kJ/mol.
  • As shown in FIG. 5, an exemplary GBL-bearing electrolyte over time exhibits a stable comparatively high ionic conductivity. As shown in FIG. 3, ACN bearing electrolytes exhibit a high initial conductivity (mS/cm), but their ionic conductivity declines over a course of 90 days. Exemplary GBL gel electrolytes including lithium perchlorate exhibit a slightly lower ionic conductivity, but exhibit stable ionic conductivity over 100 days. Thus, a GBL-bearing electrolyte 130 of the present invention suitably provides stable ionic conductivity over time, and thus may increase the lifetime of an electrochromic device.
  • FIG. 6 shows a cross section of an electrochromic device used as a window or shade 500 installed in an aircraft fuselage 580. The window 500 includes a GBL electrolyte 530 that suitably provides comparatively low flammability and toxicity for aircraft or automotive applications. The window 500 is a multi-layer assembly 505, including a first electrode 510, an electrochromic layer 520, a GBL electrolyte 530, and a second electrode 540. The assembly 505 is suitably held in a frame 570, in this example, adapted to hold the electrochromic window 500 in the wall of an aircraft fuselage 580. A GBL electrolyte 530 bearing electrochromic window 500 suitably provides ionic conductivity and stability, while complying with appropriate safety limitations for an aircraft application. The GBL electrolyte 530 suitably permits the salt ions 535 within the GBL electrolyte 530 to activate and deactivate electrochromic layer 520 in an aircraft environment through multiple cycles. Structural window layers may be added to the window 500, leaving the window 500 to serve as a shade.
  • Electrochromic devices of the present invention may also include multi-color electrochromic panels, i.e., polychromatic, having at least two pigments of electrochromic materials. For example, FIG. 7 shows an exemplary multi-color electrochromic panel 605 in accordance with an embodiment of the present invention. The panel 605 includes three color zones, a first color zone 610, a second color zone 620, and a third color zone 630 arranged in the panel 605 in a design or pattern 607. Alternate color panels 605 suitably may have only one color zone, or a greater number of color zones. The pattern 607 in this embodiment is a colored wave pattern adapted to match or complement other designs, architectural features, patterns or colors in an area (not shown) where the panel 605 is installed, such as described further with reference to FIG. 10. The electrochromic device 605 is shown with the electrochromic layer activated to be in an opaque or colored state, as opposed to a substantially transparent state. In a non-activated state, this exemplary panel 605 would be substantially transparent, i.e., the zones 610, 620, and 630 would all be substantially transparent, and the pattern 607 would not be visible. In some embodiments, the pattern 607 may still permit an observer to see partially, or dimly, through the panel 605, even when the panel 605 is in a fully activated state.
  • FIG. 7A shows an enlargement of a typical section of an electrochromic layer 650 at an interface 625 between the second color zone 620, and third color zone 630 of the panel 605 of FIG. 7 at a pixel level. The electrochromic layer 650 is divided into a plurality of pixels 640. In this example, the pixels 640 are a uniform size and shape, are square and are of a size such that when viewed from ordinary human viewing distances of approximately two feet or greater, the pixels 640 blend to form colors. The colors formed are based upon the respective areal color densities or percentages of different colors of electrochromic materials in the pixels 640. In this example, the pixels 640 include varying densities of three colors of electrochromic material, a first color electrochromic material 641, a second color electrochromic material 643, and a third color electrochromic material 645. In this embodiment, the second color zone 620 of the panel 605 of FIG. 7 is composed of pixels of the third color electrochromic material 645, while the third color zone 630 is composed of a mixture of pixels of the first color electrochromic material 641 and the second color electrochromic material 643. By varying the areal percentage or density of pixels 640 of color electrochromic materials 641, 643, and 645, a wide variety and gradations of colors may be generated from the visual mixing of the pixels 640. When viewed by the human eye from normal viewing distances, pixels 640 of the first color electrochromic material 641, the second color electrochromic material 643, and the third color electrochromic material 645 blend into a desired configuration of varied and graduated colors. Suitable pixel sizes for partial wall size multi-color electrochromic panels 605 include pixels approximately one millimeter square. In single color areas intended to display an unmixed color of an electrochromic material, such areas may have much larger pixels or be aggregated into a single area wide “pixel.”
  • By way of example, but not limitation, electrochromic materials when activated can form various colors that can be mixed visually in a multi-color electrochromic panel 605 as described with reference to FIG. 7 and FIG. 7A. For example, 3,3-Dimethyl-3,4-dihydro-2H-thieno [3,4-b][1,4] dioxepine (1) forms a blue color when activated in a reduced state, and otherwise is substantially transparent. Similarly, 6,6-dimethyl-6,7-dihydro-2H, 5H-4,8-dioxa-2-aza-azulene (2) in an activated or reduced state forms a red color and is otherwise substantially transparent. Other colors of electrochromic materials are available and/or under development. Red and blue color electrochromic materials may be combined in various ratios to produce reds, blues, and purples. Red, blue, and green pixels will be able to be combined to form a very wide pallet of colors, as may cyan, magenta, and yellow electrochromic materials.
  • Overlapping of colors, either on a substrate or in a multiple-activated-layer sandwich, may also produce further colors or variable colors as each or multiple color layers are activated (see, e.g., Reference C). By way of example, red, purple, blue, substantially transparent, and black colors suitably may be displayed by activating one or both of the red and blue electrochromic materials to varying intensities either together, separately, or not at all, with a combination of red or blue electrochromic materials. Alternately, applying a segmented activating charge to a display 605, thus providing different charge regimes to differing subsets and combination of pixels 640 or sections of the display 605, similarly will also produce a variety of combinations of colors, transparency, and opacity, from the display 405 at different times.
  • FIG. 8 shows a cross-section of an exemplary single electrochromic layer multi-color electrochromic panel 705. The panel 705 has a first transparent substrate 710, upon which is deposited a transparent electrical conductor 720. Deposited on the transparent electrical conductor 720 is an electrochromic layer 730 including areas of a first color electrochromic material 731, areas of a second color electrochromic material 733, and areas of a third color electrochromic material 735. The transparent electrical conductor 720 permits an electrical charge or field to be applied to the color electrochromic materials 731, 733, and 735. As described above, the areas of the first material 731, the second material 733, and the third material 735 are suitably small enough that when activated and viewed from normal viewing distance the colors blend visually to form different areas on the panel 705 where different colors may be displayed. Adjacent to the electrochromic layer 730 is a gel electrolyte layer 740 that conducts, and to some degree stores, ions that activate and deactivate the electrochromic layer 730. In some embodiments of the present invention, the gel electrolyte includes GBL.
  • The example panel 705 may also incorporate an ion storage layer 750 with a conductor grid 760 that, in some embodiments, comprises a grid including gold (Au). The ion storage layer 750 suitably attracts and stores the oppositely charged counterparts to the ions activating and deactivating the electrochromic layer 730.
  • In operation, an electrical charge may be provided to the ion storage layer 750 and the grid 760 by a second transparent electrical conductor 780 mounted on a second transparent substrate 770.
  • In FIG. 9 a colored electrochromic material 811 is deposited onto a transparent electrical conductor 820 on a transparent substrate 830, during preparation of an exemplary multi-color electrochromic layer. Masks 810 and 815 cover separate, selected portions 812 and 816, respectively of the conductor 820. A third portion of the conductor 813 is unmasked, permitting a jet 809 of electrochromic material 808 (e.g. unpolymerized electrochromic material) to be jetted from a nozzle 807 of a spray device 805. The first mask 810 and the second mask 815 may subsequently be removed, and the spray device 805 used to direct a jet of alternate color electrochromic materials (not shown) onto the transparent electrical conductor 820 in the previously masked portions 812 and 816 of the conductor 820. Suitable masking materials include, for example, ablative masking materials such as polyimide.
  • In this embodiment, when the jet 809 of electrochromic material 808 is sprayed toward the unmasked portion 813 of the transparent electrical conductor 820, the electrochromic materials 808 is electropolymerized by an electrical charge applied to the conductor 820. At the time of spraying, the materials 808 polymerize on contact with the charged conductor 820. Alternately, for example, a separate screen mask may be used in lieu of ablative or removable masking materials 810 and 815. Furthermore, in alternate embodiments, with a defined delivery quantity and a shaped jet 808, different areas of the transparent electrical conductor 820 may be coated with a colored electrochromic material without utilizing a separate mask.
  • FIG. 10 shows an exemplary aircraft interior 900 similar to that shown in FIGS. 2A and 2B, with a multi-color electrochromic panel 910 installed in a passenger compartment divider 920. In this embodiment, the panel 910, when activated (as shown here) displays a color coordinated interior design or pattern 930 that may be coordinated with and visually match other portions of the compartment divider 920, which may have a similar, but non-electrochromic interior design or pattern 931. When the electrochromic panel 910 is in a non-activated state the panel 910 is substantially transparent. Multi-color panels 910, such as that shown in FIG. 10, suitably may have color patterns to match a wide variety of architectural details, designs, patterns, and colors and be used in vehicles, buildings, signs, or the like.
  • Additional embodiments of the present invention include systems and methods for controlling arrays of electrochromic devices. These may include window dimming control systems, such as for the windows of passenger cabins of large commercial transport aircraft. In one embodiment, a control system uses existing wiring to distribute electronic control signals to the windows throughout the passenger cabin. By doing so, much of the weight and cost of wiring for the electrochromic devices are avoided.
  • FIG. 11 is a schematic view of a window dimming system 1000 in accordance with another embodiment of the present invention. In this embodiment, the window dimming system 1000 includes at least one cabin attendant control panel 1002 operatively coupled to a first zone 1010 and a second zone 1020. Each zone 1010 and 1020 includes a zone control box 1012 and 1022, respectively, operatively coupled to the cabin attendant control panel 1002 and to a power source 1030. Also, each of the first and second zones 1010 and 1020 includes a plurality of lighting control modules 1014 and 1024 respectively, which are in turn operatively coupled to a plurality of passenger control panels 1049. The passenger control panels 1049 are separately connected to an associated electrochromic device 1050.
  • Although FIG. 11 depicts the cabin attendant control panel 1002 and the passenger control panels 1049 as being coupled to the electrochromic devices 1050 via conductive members (e.g. wires), in alternate embodiments, the control panels 1049, 1002 may be operatively coupled to the electrochromic devices 1050 in a wireless manner using, for example, radio signals or other electromagnetic signals. For example, the cabin attendant control panel 1002 suitably may be incorporated into a portable remote control unit carried by the attendant. Alternately, multi-way switching circuits may also be used, allowing a selection of electrochromic devices 1050 to control.
  • In operation, each of the passenger control modules 1049 may be adjustably controlled (e.g. by a passenger) to vary the color or opacity of its associated electrochromic device 1050, as described more fully below. Each zone control box 1012 and 1022 is adapted to receive control data 1003 from the cabin attendant control panel 1002, and responsible for relaying those control commands to the appropriate electrochromic device 1050. The passenger control modules 1049 may be controlled or overridden by the control data 1003 output from the cabin attendant control panel 1002, leaving the attendants in control of lighting, for example, for safety reasons.
  • In the embodiment shown in FIG. 11, one passenger control module 1049 is coupled to each electrochromic device 1050. This arrangement may be suitable, for example, for providing each window seat on the aircraft with a passenger control module 1049. In alternate embodiments, however, a plurality of passenger control modules 1049 may be coupled to each electrochromic device 1050, such as, for example, the other seats in the same row. In such alternate embodiments, a hierarchy of control authority may be established between the plurality of passenger control modules 1049, such as, for example, descending control authority with increasing distance from the respective window.
  • The window dimming control system 1000 advantageously provides improved control authority over the opacity of the plurality of electrochromic devices 1050. For example, in one mode of operation, each passenger within a cabin of the commercial aircraft may be permitted to control the opacity of his or her electrochromic device 1050, and thus, the tint, color, or transparency of his or her window, using the associated passenger control module 1049. In an alternate mode of operation, however, a cabin attendant or other authorized person may be permitted to override the settings of the individual passengers using the cabin attendant control panel 1002 as necessary (e.g. during an in-flight movie, during takeoff and landing, etc.) to control the uniformity of the lighting within the passenger cabin.
  • The cabin attendant control panel 1002 may be adapted to provide control authority over the electrochromic devices 1050 in a wide variety of ways. For example, the cabin attendant control panel 1002 may address one, several, all, or any other desired combination of the electrochromic devices 1050. The control panel 1002 may be programmable or include control options to be selected for the situation. The cabin attendant control panel may include or be linked to a computer processor 1007 providing for computerized or automated control of the electrochromic devices 1050. For example, in one particular embodiment, the cabin attendant control panel 1002 through the processor 1007 may be programmed to change the opacity of all electrochromic devices 1050 to change the environment based upon time of day, the status of the flight (take-off, landing, etc.), or other criteria. Alternately, the control panel 1002 might be programmed to change state automatically when a sufficient amount of light is sensed within the cabin. On the other hand, the attendant may utilize the cabin attendant control panel 1002 to override the passenger control modules 1049 of a particular passenger (e.g. a particular window seat) or a selected group of passengers (e.g. a selected group of window seats) as necessary for a desired lighting condition.
  • In one representative embodiment, the window dimming system 1000 is operated by means of the lighting control modules 1014 and 1024 and the cabin attendant control panel 1002 (via the first and second zone boxes 1012 and 1022) which are adapted to controllably vary the polarity and strength of electric fields powered by the power source 1030. By positioning the electrochromic devices 1050 adjacent the windows of the aircraft, the opacity of the electrochromic devices 1050 may be controllably varied to lighten or darken the windows of the aircraft.
  • The electrochromic device 1050 may assume a wide variety of embodiments and including those other than described above and shown in FIGS. 1 and 2A. The invention described above with reference to FIG. 11 should not be construed to being limited to any particular electrochromic device 1050, and indeed may be utilized with any electrically controlled shade. Furthermore, in alternate embodiments, electrochromic devices in accordance with the present invention need not be coupled to a surrounding structure (e.g. the aircraft fuselage 280 in FIG. 1). More specifically, in alternate embodiments, the electrochromic devices may be freestanding units.
  • In FIG. 12, a window dimming system 1100 includes a cabin attendant control panel 1102 operatively coupled to a first zone 1110 and a second zone 1120. Each zone includes a zone switch module 1112, 1122 operatively coupled to the cabin attendant control panel 1102 and to a power source 1130. In this embodiment, the zone switch module 1112 controls first and second sub-portions 1111 and 1113 of the first zone 1110, while the zone switch module 1124 controls the entire second zone 1120. Also, each of the first and second zones 1110 and 1120 includes a plurality of overhead electronic units 1114 and 1124, respectively, which are, in turn, each operatively coupled to associated passenger reading lights 1115 and 1125, respectively. The first zone 1110 further includes a plurality of dimmer controls 1118 operatively coupled to the overhead electronic units 1114 and to an associated electrochromic dimmable window 1119. The passenger dimmer controls 1118 are located conveniently for the passengers on each seat or row of seats on the armrests, tray tables, seat backs, or interior panels.
  • In operation, each of the dimmable windows 1119 of the first zone 1110 may be adjustably controlled independently of the other dimmable windows 1119 using the associated dimmer control 1118. Alternately, all of the dimmable windows 1119 may be controlled using the cabin attendant control panel 1102. The cabin attendant control panel 1102 may have override authority over each of the individual dimmer controls 1118, and is adapted to simultaneously adjust the electric fields within the plurality of dimmable windows 1119 of the first and second zones 1110, 1120 to selectively activate and de-activate the plurality of dimmable windows 1119 of the first and second zones 1110, 1120 either independently or in unison (or both).
  • The window dimming control system 1100 advantageously utilizes existing wiring to distribute the desired electronic control signals to the dimmable windows 1120 throughout the passenger cabin of the aircraft. In this way, much of the weight and cost of wiring that would otherwise be dedicated to this task is reduced or eliminated. In one particular embodiment, for example, the dimmer controls 1118 and the associated dimmable windows 1119 are simply incorporated into an existing Cabin Services System (CSS) that controls other functions within the main passenger cabin, including, for example, the reading lights associated with each passenger seat.
  • A wide variety of apparatus may be conceived that include electrochromic device array control systems in accordance with alternate embodiments of the present invention. For example, FIG. 13 is a side elevational view of an aircraft 1200 having a plurality of window assemblies 1201 and one or more window dimming control systems 1202 formed in accordance with alternate embodiments of the present invention.
  • In general, except for the window dimming control systems 1202 formed in accordance with the present invention, the various components and subsystems of the aircraft 1200 may be of known construction and, for the sake of brevity, will not be described in detail. Embodiments of window dimming control systems 1202 in accordance with the present invention, including but not limited to those embodiments described above and shown in FIGS. 11-12, may be employed in any desired location throughout the aircraft 1200.
  • More specifically, as shown in FIG. 13, the aircraft 1200 includes one or more propulsion units 1204 coupled to an airframe (not visible) disposed within a fuselage 1205, wing assemblies 1206 (or other lifting surfaces), a tail assembly 1208, a landing assembly 1210, a control system (not visible) 1212, and a host of other systems and subsystems that enable proper operation of the aircraft 1200. A plurality of window assemblies 1201 are distributed throughout the fuselage 1205, and a plurality of window dimming control systems 1202 in accordance with the present invention are distributed throughout the various portions of the aircraft 1200, including, for example, within the cockpit (1202 a), the first-class section (1202 c), and the coach or business class section (1202 c).
  • Although the aircraft 1200 shown in FIG. 11 is generally representative of a commercial passenger aircraft, including, for example, the 737, 747, 757, 767, 777, and 7E7 models commercially available from The Boeing Company of Chicago, Ill., the inventive apparatus and methods disclosed may also be employed in virtually any other types of aircraft. More specifically, the teachings of the present invention may be applied to other types and models of passenger aircraft, fighter aircraft, cargo aircraft, rotary aircraft, and any other types of aircraft, including those described, for example, in The Illustrated Encyclopedia of Military Aircraft by Enzo Angelucci, published by Book Sales Publishers, September 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. Alternate embodiments of apparatus and methods in accordance with the present invention may be used in the other applications, including, for example, ships, buses, trains, recreational vehicles, subways, monorails, houses, apartments, office buildings, or any other desired applications.
  • FIG. 14 shows a top elevational view of a representative passenger aircraft floor plan 1300. The passenger aircraft floor plan 1300 includes first port and starboard control systems 1310, 1311 covering port and starboard portions of the business section, a forward economy section control system 1320, and second port and starboard control systems 1330, 1331 covering the rear economy section. Each of the window control systems shown in FIG. 14 may include one or more zones such as described above with reference to FIGS. 11-12. Clearly, a wide variety of alternate embodiments of passenger aircraft floor plans 1300 having various configurations of window control systems in accordance with the present invention may be conceived.
  • In FIG. 15A passenger aircraft section 1400 includes a window control system 1410 having a first or left zone 1411 and a second or right zone 1413. A master control module 1412 is wirelessly coupled to electrochromic devices 1420 of the window control system 1410. Passenger control modules 1430 are positioned over the passenger seats 1440. As further shown in FIG. 15B, in another embodiment, a passenger aircraft section 1450 includes a control system 1460 adapted to control a freestanding electrochromic display or partition 1475. A master control module 1462 is located overhead in the aircraft section 1450. One or more passenger control modules 1480 may be located proximate the seats 1490, including, for example, within the armrests between the adjacent seats 1490, or on upper and lateral portions of the aircraft section 1450. Similarly, the master control module 1462 may be disposed in any desired location.
  • As shown in FIG. 16 and FIG. 17, an exemplary window assembly 1500 includes a window member 1510, and an electrochromic assembly 1550 disposed adjacent the window member 1510. A passenger control module 1560 is operatively coupled to the electrochromic assembly 1550. An edge trim 1514 is disposed about an outer perimeter of the window member 1510. A power source 1562 provides power to the window assembly 1500. Bus bars 1581 and 1583 around the perimeter of the electrochromic assembly 1550 provide electrical connections to the assembly 1550.
  • FIG. 18 is a detailed cross sectional view of an outer perimeter of the electrochromic device 1550 of FIG. 16. The device 1550 includes two outer transparent layers, a first outer layer 1551 and a second outer layer 1553 proximate to each other. The outer layers 1551 and 1553 by way of example may include glass, acrylic, or polycarbonate. The outer layers 1551 and 1553 are coated on their interior surfaces by a first transparent electrode coating 1577 and a second transparent electrode coating 1579, respectively. In a central portion 1552 of the first outer layer 1551, an electrochromic layer 1561 is deposited on the first electrode coating 1577. In a central portion 1552 of the second outer layer 1553, a counter-electrode grid 1565 is deposited on the second electrode coating 1579. Between the counter-electrode grid 1565 and the electrochromic layer 1561 is a layer of gel electrolyte 1563.
  • Attached to an edge portion 1554 of the first electrode coating 1571 is a first busbar 1581. As shown in FIG. 17, the first busbar 1581 suitably spans the circumference of the first outer layer 1551, providing an electrical connection to the first transparent electrode coating 1577. Attached to an edge portion 1554 of the second electrode coating 1579 is a second busbar 1583, that as shown in FIG. 17 suitably spans the circumference of the second outer layer 1553, providing an electrical connection to the second transparent electrode coating 1579. The first busbar 1581 and the second busbar 1583 suitably may be any conductor, including by way of example copper strips. A space 1585 is maintained between the first busbar 1581 and the second busbar 1583, so that charges may be provided to their respective electrode layers 1577 and 1579, without the first busbar 1581 and second busbar 1583 making contact with each other. The space 1585 may also hold or be filled with a dielectric, providing insulation between the busbars 1581 and 1582. A first adhesive seal 1571 between the first outer layer 1551 and second outer layer 1553, between their central portions 1552 and their edge portions 1554, suitably seals and contains the edge of the electrochromic layer 1561, the electrolyte 1563, and the counter electrode grid 1565, permitting the device to activate and deactivate when an electric charge is applied to the device 1550 through a power source (not shown) electrically coupled with the busbars 1581 and 1583. A second adhesive seal 1573 seals the outermost edge 1556 of the first outer layer 1551 and second outer layer 1553, suitably isolating and insulating the busbars 1581 and 1583 from the outside environment. Further, the edge portion 1554 and the outermost edge 1556 of the first outer layer 1551 and the second outer layer 1553 are surrounded by an edge trim 1587. The edge trim 1587 in this embodiment is in the form of a clip assisting in holding together the components of the device 1550, including the first outer layer 1551 and the second outer layer 1553, with the electrode layers 1577 and 1579, the electrochromic layer 1561, the electrolyte 1563, the counter electrode grid 1565, the two busbars 1581 and 1583 in a fixed configuration between them.
  • FIG. 19 is an exploded isometric view of a window assembly 1600 including a first window member 1610 having a transparent portion 1612 and an edge trim portion 1614. Similarly, an outer second window member 1620 includes a transparent portion 1622 and a mounting portion 1624. An electrochromic assembly 1650 is disposed between the first and second window members 1610, 1620. Passenger controls 1660 are disposed within the edge trim portion 1614 of the first window member 1610, in this example the inner window member for an aircraft, and are operatively coupled to the electrochromic assembly 1650. The passenger controls 1660, for example, allow the passenger in the window seat to control the electrochromic assembly 1650 as desired, subject to override signals from a master controller (not shown) as described with reference to FIGS. 11 and 12.
  • While preferred and alternate embodiments of the invention have been illustrated and described, as noted above, many changes may be made without departing from the spirit and scope of the invention. Accordingly, the scope of the invention is not limited by the disclosure of the preferred and alternate embodiments. Instead, the invention should be determined entirely by reference to the claims that follow:

Claims (38)

1. An electrochromic system, comprising:
a plurality of electrochromic devices;
a plurality of control modules, each control module being operatively coupled to at least one electrochromic device and adapted to controllably adjust an electric field to activate and de-activate the device; and
at least one main controller operatively coupled to the devices and adapted to simultaneously adjust the electric fields of a selected set of the devices to activate and de-activate the set.
2. The electrochromic system of claim 1, wherein at least one electrochromic device is disposed adjacent to a transparent window.
3. The electrochromic system of claim 1, wherein at least one electrochromic device is integrally formed with the transparent window.
4. The electrochromic system of claim 1, wherein at least one electrochromic device includes:
a first transparent electrode;
a second transparent electrode operatively positioned with and spaced apart from the first transparent electrode;
an electrochromic layer disposed between the first and second transparent electrodes; and
an electrolyte layer disposed between the first and second transparent electrodes and adjacent the electrochromic layer.
5. The electrochromic system of claim 1, further comprising a power source operatively coupled to at least one of the main controller, the plurality of control modules, and the plurality of electrochromic devices.
6. The electrochromic system of claim 1, wherein the plurality of electrochromic devices includes at least one polychromatic electrochromic device.
7. A window system, comprising:
a main controller operatively coupled to first and second zones, respectively, wherein the first zone includes:
a first plurality of window assemblies, each window assembly having an operative electrochromic device;
at least one control module operatively coupled to at least one electrochromic device and adapted to controllably adjust an electric field to control the device;
and wherein the second zone includes:
a second plurality of window assemblies, each window assembly having an operative electrochromic device;
at least one control module operatively coupled to at least one electrochromic device and adapted to controllably adjust an electric field to control the device;
and wherein the main controller is adapted to adjust the electric fields of the plurality of electrochromic devices of the first and second zones to provide zonal control of the electrochromic devices.
8. The window system of claim 7, wherein at least one electrochromic device is integrally formed with the window assembly.
9. The window system of claim 7, wherein at least one electrochromic device includes:
a first transparent electrode;
a second transparent electrode operatively positioned with and spaced apart from the first transparent electrode;
an electrochromic layer disposed between the first and second transparent electrodes; and
an electrolyte layer disposed between the first and second transparent electrodes and adjacent the electrochromic layer.
10. The window system of claim 7, further comprising a power source operatively coupled to at least one of the main controller, the first zone, and the second zone.
11. The window system of claim 7, wherein at least one zone further comprises a plurality of overhead electronic units coupled between the zone switch and at least one control module.
12. The window system of claim 11, further comprising at least one light operatively coupled to each overhead electronic unit.
13. The window system of claim 11, wherein the first plurality of window assemblies are arranged in a first area of an aircraft passenger cabin, and wherein the second plurality of window assemblies are arranged in a second area of an aircraft passenger cabin.
14. A structure, comprising:
a plurality of windows,
a window control assembly operatively associated with the windows, the window control assembly including:
a plurality of electrochromic devices, each electrochromic device being operatively associated with a respective window;
a plurality of control modules, each control module being operatively coupled to at least one electrochromic device and adapted to controllably adjust an electric field to activate and de-activate the device; and
a main controller operatively coupled to the devices and adapted to adjust the electric fields of the devices to activate and de-activate the devices in a selected manner.
15. The structure of claim 14, wherein each electrochromic device operatively forms a shade for a window.
16. The structure of claim 15, wherein each control module is positioned to be accessible to a seated user.
17. The structure of claim 14, wherein the main controller is spaced apart from the control modules
18. An aircraft, comprising:
a fuselage operatively coupled to an airframe;
a plurality of window assemblies formed within at least one of the fuselage and the airframe; and
a services system disposed within the fuselage, the services system including:
a plurality of lighting assemblies;
a plurality of control modules, each control module being operatively coupled to at least one of the lighting assemblies;
a window control system including a plurality of electrically operated shades, each shade being operatively associated with a respective one of the window assemblies and operatively coupled to at least one control module, wherein the control module is adapted to controllably activate and de-activate the shade; and
a main controller operatively coupled to the shades and adapted to adjust the shades to activate and de-activate the plurality of shades in a selected manner.
19. The aircraft of claim 18, wherein each shade is operatively disposed adjacent to a window assembly.
20. The aircraft of claim 18, wherein each shade is a component of a window assembly.
21. The aircraft of claim 18, wherein at least one of the electrically operated shades includes:
a first transparent electrode;
a second transparent electrode operatively positioned with and spaced apart from the first transparent electrode;
an electrochromic layer disposed between the first and second transparent electrodes; and
an electrolyte layer disposed between the first and second transparent electrodes and adjacent the electrochromic layer.
22. A method of controlling light through a plurality of windows, comprising:
providing at least one electrochromic device operatively associated with each window;
providing a plurality of control modules, each control module being operatively coupled to at least one electrochromic device and adapted to controllably activate and de-activate at least one device;
providing a main controller operatively coupled to the devices and adapted to control the devices in a selected manner.
adjusting a characteristic color of at least some of the devices.
23. The method of claim 22, wherein adjusting the characteristic color of at least some of the devices includes adjusting the devices using the main controller.
24. The method of claim 23, wherein adjusting the devices using the main controller includes overriding a control signal from at least one control module.
25. The method of claim 22, wherein the devices function as a shade for a window.
26. The method of claim 22, wherein the control modules are arranged in rows and are associated with aircraft seats to be accessible to seated passengers.
27. The method of claim 22, wherein the main controller is accessible to an aircraft passenger attendant.
28. An electrochromic system, comprising:
an electrochromic device;
a control module operatively coupled to the electrochromic device and adapted to controllably activate and de-activate the electrochromic device; and
a main controller operatively coupled to the device and adapted to override the control module to controllably activate and de-activate the device.
29. The system of claim 27, further comprising a window member operatively associated with the electrochromic device.
30. A method of adjusting a lighting level in a passenger cabin of a vehicle, comprising:
providing an electrochromic device operatively associated with a window of the vehicle;
providing a control module operatively coupled to the electrochromic device and adapted to controllably activate and de-activate the electrochromic device;
providing a main controller operatively coupled to at least one of the control module and the electrochromic device;
adjusting a characteristic of the electrochromic device by controllably adjusting the control module; and
adjusting the characteristic of the electrochromic device by overriding the control module using the main controller.
31. The method of claim 29, wherein the electrochromic device operates as a shade for the window.
32. The method of claim 29, wherein adjusting a characteristic of the electrochromic device includes adjusting opacity.
33. The method of claim 29, wherein adjusting a characteristic of the electrochromic device includes adjusting an electric field coupled to the device.
34. A system for controlling the environment in a passenger cabin of a vehicle, comprising:
at least one individual environment control located near a seat in the cabin;
a crew-control override arranged to override the control; and;
a processor arranged to automatically override the control in response to a selected flight/trip condition.
35. The system of claim 34, wherein the control operates a shade for a window.
36. The system of claim 34, wherein the control operates an electrochromic device.
37. An aircraft passenger cabin, comprising:
at least one window;
at least one shade arranged to operatively shade the window;
at least one seat control arranged to operate the shade;
at least one override, arranged to allow a crew member to override the seat control; and
at least one processor arranged to automatically set the shade based upon a flight/trip condition.
38. The system of claim 37, wherein the shade includes an electrochromic device.
US10/974,240 2004-03-12 2004-10-27 Dimming control system for an array of electrochromic devices Abandoned US20050200934A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US55245304P true 2004-03-12 2004-03-12
US55258904P true 2004-03-12 2004-03-12
US55260604P true 2004-03-12 2004-03-12
US10/974,240 US20050200934A1 (en) 2004-03-12 2004-10-27 Dimming control system for an array of electrochromic devices

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/974,240 US20050200934A1 (en) 2004-03-12 2004-10-27 Dimming control system for an array of electrochromic devices
US11/877,133 US8064120B2 (en) 2004-03-12 2007-10-23 Aircraft cabin services system including zone controllers for lighting control modules and dimmable windows

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US11/877,133 Continuation US8064120B2 (en) 2004-03-12 2007-10-23 Aircraft cabin services system including zone controllers for lighting control modules and dimmable windows

Publications (1)

Publication Number Publication Date
US20050200934A1 true US20050200934A1 (en) 2005-09-15

Family

ID=34923455

Family Applications (2)

Application Number Title Priority Date Filing Date
US10/974,240 Abandoned US20050200934A1 (en) 2004-03-12 2004-10-27 Dimming control system for an array of electrochromic devices
US10/974,088 Active 2027-01-23 US8988757B2 (en) 2004-03-12 2004-10-27 Low vapor pressure solvent for electrochromic devices

Family Applications After (1)

Application Number Title Priority Date Filing Date
US10/974,088 Active 2027-01-23 US8988757B2 (en) 2004-03-12 2004-10-27 Low vapor pressure solvent for electrochromic devices

Country Status (1)

Country Link
US (2) US20050200934A1 (en)

Cited By (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050200933A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Low vapor pressure solvent for electrochromic devices
US20070097484A1 (en) * 2004-11-03 2007-05-03 Libretto John Electrochromic glass control device
US20070097238A1 (en) * 2005-10-06 2007-05-03 Asia Optical Co., Inc. Method for rapidly changing the color of a light source and image apparatus using the same
US20070137117A1 (en) * 2005-12-02 2007-06-21 Carlson Ryan L Conductive gasket apparatus and method
US20080055731A1 (en) * 2006-08-31 2008-03-06 The Boeing Company Airplane window control
US7355161B2 (en) 2005-12-15 2008-04-08 The Boeing Company Systems and methods for controlling windows with variable light transmission
US20080144158A1 (en) * 2006-01-30 2008-06-19 Airbus Deutschland Gmbh Power supply for an electric window dimming device
US20080218434A1 (en) * 2007-03-05 2008-09-11 The Boeing Company Electrically Dimmable Combiner Optics for Head-Up Display
US20080230653A1 (en) * 2007-03-23 2008-09-25 The Boeing Company Self-Powered Dimmable Windows with Integrated Controls
US20080234893A1 (en) * 2007-03-23 2008-09-25 The Boeing Company Window control system
GB2448041A (en) * 2007-03-30 2008-10-01 Boeing Co Control system for dimmable windows
US20080259433A1 (en) * 2004-03-12 2008-10-23 The Boeing Company Multi-color electrochromic apparatus and methods
US20080308677A1 (en) * 2007-06-18 2008-12-18 Kirchoff Kenneth P Radio frequency shielding apparatus system and method
US7505136B2 (en) 2006-05-16 2009-03-17 The Boeing Company Testing and tuning electrically dimmable windows
FR2937006A1 (en) * 2008-10-09 2010-04-16 Airbus Aircraft i.e. airplane, has inner wall made of electrochromic material that is introduced to choose transparent state to see person in one of zones from other zone through wall and to choose opaque state inhibiting view of person
US20110029194A1 (en) * 2009-07-30 2011-02-03 Control Solutions, LLC Securable cover for vehicle lights
US20110026092A1 (en) * 2009-07-30 2011-02-03 Control Solutions, LLC Light blocking apparatus for vehicle mirror assembly
US20110026091A1 (en) * 2009-07-31 2011-02-03 Control Solutions, LLC Electrically activatable light blocking cover for vehicle mirrors
US20110043922A1 (en) * 2008-02-07 2011-02-24 Daimler Ag Vehicle Pane and Motor Vehicle Having a Vehicle Pane
US20110063864A1 (en) * 2009-09-16 2011-03-17 Control Solutions, LLC Securable cover with electrically activatable light inhibiting lens for vehicle lights
US7956869B1 (en) * 2007-07-13 2011-06-07 Adobe Systems Incorporated Proximity based transparency of windows aiding in obscured window selection
US20110199976A1 (en) * 2008-03-31 2011-08-18 The Boeing Company Wireless Aircraft Sensor Network
US8064120B2 (en) 2004-03-12 2011-11-22 The Boeing Company Aircraft cabin services system including zone controllers for lighting control modules and dimmable windows
US20120013238A1 (en) * 2010-07-19 2012-01-19 Greenwave Reality, Inc. Electrically Controlled Glass in a Lamp
US20120144496A1 (en) * 2010-12-04 2012-06-07 Hon Hai Precision Industry Co., Ltd. Electronic device with data protection function and method thereof
US8213074B1 (en) 2011-03-16 2012-07-03 Soladigm, Inc. Onboard controller for multistate windows
US8254013B2 (en) 2011-03-16 2012-08-28 Soladigm, Inc. Controlling transitions in optically switchable devices
CN103009970A (en) * 2011-09-23 2013-04-03 通用汽车环球科技运作有限责任公司 Window module with integrated electropolymeric sunshade
US8705162B2 (en) 2012-04-17 2014-04-22 View, Inc. Controlling transitions in optically switchable devices
US20140140080A1 (en) * 2012-06-11 2014-05-22 Msa Aircraft Products Ltd. Light ring for an aircraft cabin window
US8764210B2 (en) 2010-07-19 2014-07-01 Greenwave Reality Pte Ltd. Emitting light using multiple phosphors
US9030725B2 (en) 2012-04-17 2015-05-12 View, Inc. Driving thin film switchable optical devices
WO2016081858A1 (en) * 2014-11-21 2016-05-26 Gentex Corporation Electro-optic assembly
US9412290B2 (en) 2013-06-28 2016-08-09 View, Inc. Controlling transitions in optically switchable devices
US9454055B2 (en) 2011-03-16 2016-09-27 View, Inc. Multipurpose controller for multistate windows
US9470828B1 (en) 2015-06-19 2016-10-18 The Boeing Company Local light attenuation for improving reliability of electronic dimmable windows
US9523902B2 (en) 2011-10-21 2016-12-20 View, Inc. Mitigating thermal shock in tintable windows
US9638978B2 (en) 2013-02-21 2017-05-02 View, Inc. Control method for tintable windows
US20170121007A1 (en) * 2013-05-17 2017-05-04 Honda Patents & Technologies North America, Llc Window of an aircraft
US9645465B2 (en) 2011-03-16 2017-05-09 View, Inc. Controlling transitions in optically switchable devices
US9694896B1 (en) * 2013-01-03 2017-07-04 The Boeing Company Airplane window having infrared heat reflection capability
US9778532B2 (en) 2011-03-16 2017-10-03 View, Inc. Controlling transitions in optically switchable devices
US20170283065A1 (en) * 2016-04-04 2017-10-05 B/E Aerospace, Inc. Aircraft Interior Surface and Method of Illuminating an Aircraft Interior Surface
US9885935B2 (en) 2013-06-28 2018-02-06 View, Inc. Controlling transitions in optically switchable devices
US9927609B2 (en) 2015-08-14 2018-03-27 Gentex Corporation Heads up display system
US10048561B2 (en) 2013-02-21 2018-08-14 View, Inc. Control method for tintable windows
US10101583B2 (en) 2015-06-16 2018-10-16 Gentex Corporation Heads up display system
US10221612B2 (en) 2014-02-04 2019-03-05 View, Inc. Infill electrochromic windows
US10303035B2 (en) 2009-12-22 2019-05-28 View, Inc. Self-contained EC IGU
US10365531B2 (en) 2012-04-13 2019-07-30 View, Inc. Applications for controlling optically switchable devices
US10495939B2 (en) 2015-10-06 2019-12-03 View, Inc. Controllers for optically-switchable devices
US10503039B2 (en) 2013-06-28 2019-12-10 View, Inc. Controlling transitions in optically switchable devices
US10539854B2 (en) 2017-03-21 2020-01-21 View, Inc. Control method for tintable windows

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104597682B (en) * 2006-06-09 2018-04-13 金泰克斯公司 Variable transmission window system
DE102011018672B4 (en) * 2011-04-27 2016-01-07 Diehl Aerospace Gmbh Device for controlling the brightness in an aircraft
WO2013096779A1 (en) 2011-12-21 2013-06-27 Gentex Corporation Switchable variable transmittance window assembly
US9302452B2 (en) 2012-03-02 2016-04-05 Ppg Industries Ohio, Inc. Transparent laminates comprising inkjet printed conductive lines and methods of forming the same
US9365281B2 (en) 2013-11-19 2016-06-14 Gentex Corporation Reducing condensation in dimmable window systems
US9606412B2 (en) 2015-03-09 2017-03-28 Gentex Corporation Window system with indicia
US10167073B2 (en) 2015-06-09 2019-01-01 Gentex Corporation Multi-piece bezel for electro-optic window assembly
US9986669B2 (en) * 2015-11-25 2018-05-29 Ppg Industries Ohio, Inc. Transparency including conductive mesh including a closed shape having at least one curved side

Citations (74)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3330506A (en) * 1965-07-12 1967-07-11 Lockheed Aircraft Corp Adjustable passenger utility carrier
US3370813A (en) * 1965-10-22 1968-02-27 Mc Donnell Douglas Corp Adjustable passenger reading lights and utilities
US4135790A (en) * 1976-05-14 1979-01-23 Nippon Kogaku K.K. Electrochromic element
US4214820A (en) * 1978-09-15 1980-07-29 Timex Corporation Electrochromic display having enhanced night viewability
US4229080A (en) * 1977-06-29 1980-10-21 Sharp Kabushiki Kaisha Additional electrode of electrochromic display and refreshing method for the same
US4286308A (en) * 1979-09-04 1981-08-25 Polaroid Corporation Apparatus and method for reducing headlight glare
US4893908A (en) * 1988-06-27 1990-01-16 Allied-Signal Inc. Adjustable tint window with electrochromic conductive polymer
US4993810A (en) * 1989-04-14 1991-02-19 Ford Motor Company Electrochromic devices comprising metal salts in an ion conductive material
US5042923A (en) * 1988-06-27 1991-08-27 Allied-Signal, Inc. Adjustable tint window with electrochromic conductive polymer
US5069535A (en) * 1987-10-24 1991-12-03 Schott Glaswerke Electrochromic layer-set
US5097358A (en) * 1989-04-27 1992-03-17 Toyoda Gosei Co., Ltd. Electrochromic element
US5108048A (en) * 1989-09-15 1992-04-28 The Boeing Company Stowage bin and support panel system for convertible aircraft and method of installation
US5347434A (en) * 1992-07-06 1994-09-13 Mcdonnell Douglas Corporation Aircraft bag-rack with an illuminated handrail
US5384653A (en) * 1992-11-06 1995-01-24 Midwest Research Institute Stand-alone photovoltaic (PV) powered electrochromic window
US5457564A (en) * 1990-02-26 1995-10-10 Molecular Displays, Inc. Complementary surface confined polymer electrochromic materials, systems, and methods of fabrication therefor
US5598293A (en) * 1993-01-22 1997-01-28 Societa Italiana Vetro - Siv - S.P.A Electrochromic glass for use in cars and buildings
US5642022A (en) * 1995-12-01 1997-06-24 Msa Aircraft Interior Products, Inc. Aircraft window shade speed regulation control system
US5654786A (en) * 1996-01-11 1997-08-05 Robert C. Burlingame Optical lens structure and control system for maintaining a selected constant level of transmitted light at a wearer's eyes
US5699192A (en) * 1992-04-10 1997-12-16 Sun Active Glass Electrochromics, Inc. Electrochromic structures and methods
US5724176A (en) * 1993-03-30 1998-03-03 Nippon Oil Co., Ltd. Counterelectrode for smart window and smart window
US5729379A (en) * 1994-10-26 1998-03-17 Donnelly Corporation Electrochromic devices
US5750282A (en) * 1995-06-07 1998-05-12 Duracell Inc. Process for improving lithium ion cell
US5764402A (en) * 1994-04-29 1998-06-09 Glaverbel Optical cell control system
US5805330A (en) * 1996-03-15 1998-09-08 Gentex Corporation Electro-optic window incorporating a discrete photovoltaic device
US5838483A (en) * 1995-02-10 1998-11-17 Donnelly Corporation Photochromic devices
US5878809A (en) * 1995-07-20 1999-03-09 Mercedes-Benz Ag Process and system for controlling an air-conditioning system for a vehicle interior
US5883220A (en) * 1992-01-12 1999-03-16 Centre National De La Recherche Scientifique Redox copolymers and their use in preparing mixed conduction materials
US5888431A (en) * 1994-07-22 1999-03-30 Gentex Corporation Electrochromic layer and devices comprising same
US5923456A (en) * 1997-12-19 1999-07-13 Rockwell International Corporation Reversible electrochemical mirror
US6005705A (en) * 1994-04-18 1999-12-21 Institut Fuer Neue Materialien Gemeinnuetzige Gmbh Electrochromic thin-film systems and components thereof
US6011642A (en) * 1997-04-18 2000-01-04 U.S. Philips Corporation Electrochromic element, a display device provided with same and a method of manufacturing an electrochromic layer
US6056410A (en) * 1997-04-02 2000-05-02 Donnelly Corporation Digital electrochromic mirror system
US6130772A (en) * 1997-06-06 2000-10-10 Cava; Frank James Electrochromic device and method
US6136161A (en) * 1993-11-12 2000-10-24 Ppg Industries Ohio, Inc. Fabrication of electrochromic device with plastic substrates
US6178034B1 (en) * 1996-04-10 2001-01-23 Donnelly Corporation Electrochromic devices
US6197923B1 (en) * 1995-10-27 2001-03-06 Nissan Chemical Industries, Ltd. Polymers, method of producing the same and use of the same
US6222177B1 (en) * 1999-01-19 2001-04-24 Gentex Corporation Electrochromic element driver with negative output resistance
US6280882B1 (en) * 1997-01-17 2001-08-28 Hydro-Quebec Electrolytic composition with polymer base for electrochemical generator
US6296973B1 (en) * 1997-09-11 2001-10-02 Hydro - Quebec Solvents and novel electrolytic compositions having a large range of stability and high conductivity
US6297900B1 (en) * 1997-07-22 2001-10-02 Sustainable Technologies Australia Limited Electrophotochromic smart windows and methods
US6317248B1 (en) * 1998-07-02 2001-11-13 Donnelly Corporation Busbars for electrically powered cells
US6327070B1 (en) * 1998-05-29 2001-12-04 Bayer Aktiengesellschaft Electrochromic assembly based on poly(3,4-ethylenedioxythiophene) derivatives in combination with a lithium niobate counterelectrode
US20020080290A1 (en) * 2000-12-25 2002-06-27 Fuji Photo Film Co., Ltd. Method and apparatus for displaying image by producing polarization inversion in ferroelectric member and producing contrast in contrast production member
US6433913B1 (en) * 1996-03-15 2002-08-13 Gentex Corporation Electro-optic device incorporating a discrete photovoltaic device and method and apparatus for making same
US20020118437A1 (en) * 2000-06-13 2002-08-29 Rukavina Thomas G. Colored electrochromic transparent window assemblies
US20020135881A1 (en) * 2000-08-03 2002-09-26 Rukavina Thomas G. Switchable electrochromic devices with uniform switching and preferential area shading
US6493128B1 (en) * 1996-08-20 2002-12-10 Donnelly Corporation Chromogenic window assembly construction and other chromogenic devices
US20020196518A1 (en) * 2001-06-25 2002-12-26 University Of Washington Electrochromic organic polymer synthesis and devices utilizing electrochromic organic polymers
US20020196519A1 (en) * 2001-04-24 2002-12-26 Yasser Elkadi Electrochromic safety glazing
US6501587B1 (en) * 2000-09-27 2002-12-31 Board Of Regents, The University Of Texas System Method of creating color-changing displays
US6515787B1 (en) * 2000-03-07 2003-02-04 Eclipse Energy Systems, Inc. Electrochromic layer
US6535126B2 (en) * 2000-12-15 2003-03-18 Ppg Industries Ohio, Inc. Electrochromic transparency incorporating security system
US6541156B1 (en) * 1999-11-16 2003-04-01 Mitsubishi Chemical Corporation Negative electrode material for non-aqueous lithium secondary battery, method for manufacturing the same, and non-aqueous lithium secondary battery using the same
US6561460B2 (en) * 2000-08-03 2003-05-13 Ppg Industries Ohio, Inc. Switchable electrochromic devices for use in aircraft transparency windows
US6567708B1 (en) * 2000-07-25 2003-05-20 Gentex Corporation System to interconnect, link, and control variable transmission windows and variable transmission window constructions
US6587250B2 (en) * 2001-03-07 2003-07-01 Acreo Ab Electrochromic device
US6594065B2 (en) * 1998-11-30 2003-07-15 Gentex Corporation Electrochromic structures
US20030174377A1 (en) * 2001-11-21 2003-09-18 University Of Florida Electrochromic polymers and polymer electrochromic devices
US20030184692A1 (en) * 2002-03-26 2003-10-02 Nobukazu Nagae Light modulating device
US20030209893A1 (en) * 1992-05-05 2003-11-13 Breed David S. Occupant sensing system
US20030233172A1 (en) * 2000-09-04 2003-12-18 Claes-Goran Granqvist Climate control system and a method for controlling such
US20040021928A1 (en) * 2002-06-21 2004-02-05 Warner Benjamin P. Electrolytes for electrooptic devices comprising ionic liquids
US6795226B2 (en) * 2000-05-04 2004-09-21 Schott Corporation Chromogenic glazing
US6819367B1 (en) * 2001-10-19 2004-11-16 Frank James Cava Shade-free light control system and method
US6843068B1 (en) * 2003-07-25 2005-01-18 Honeywell International Inc. Method and apparatus for adjusting the temperature set point based on humidity level for increased comfort
US6848653B2 (en) * 2002-05-10 2005-02-01 Goodrich Hella Aerospace Lighting Systems Gmbh Operating and/or display unit for vehicles
US20050068629A1 (en) * 2003-09-26 2005-03-31 Primal Fernando Adjustably opaque window
US20050200933A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Low vapor pressure solvent for electrochromic devices
US20050200937A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Multi-color electrochromic apparatus and methods
US6954300B2 (en) * 1993-02-26 2005-10-11 Donnelly Corporation Electrochromic polymeric solid films, manufacturing electrochromic devices using such sold films, and processes for making such solid films and devices
US20050270619A1 (en) * 2002-07-26 2005-12-08 Koninklijke Philips Electronics N.V. Electrochromic color display having different electrochromic materials
US7001868B2 (en) * 2000-12-27 2006-02-21 Fuji Photo Film Co., Ltd. Image recording apparatus and method and recording sheet for use therewith
US7300166B2 (en) * 2003-03-05 2007-11-27 Electrochromix, Inc. Electrochromic mirrors and other electrooptic devices
US7526923B2 (en) * 2002-12-23 2009-05-05 Knutsen Oas Shipping As Device for condensing volatile organic compounds from a storage or transport tank into oil

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US601642A (en) * 1898-04-05 Stove-truck
JPH1138454A (en) * 1997-07-15 1999-02-12 Nippon Oil Co Ltd Electrochromic mirror
US6597489B1 (en) * 1999-06-30 2003-07-22 Gentex Corporation Electrode design for electrochromic devices
JP2001209078A (en) * 2000-01-26 2001-08-03 Nippon Mitsubishi Oil Corp Electrochromic device
US7256923B2 (en) * 2001-06-25 2007-08-14 University Of Washington Switchable window based on electrochromic polymers
US7390336B2 (en) * 2003-07-29 2008-06-24 Solicore, Inc. Polyimide-based lithium metal battery

Patent Citations (83)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3330506A (en) * 1965-07-12 1967-07-11 Lockheed Aircraft Corp Adjustable passenger utility carrier
US3370813A (en) * 1965-10-22 1968-02-27 Mc Donnell Douglas Corp Adjustable passenger reading lights and utilities
US4135790A (en) * 1976-05-14 1979-01-23 Nippon Kogaku K.K. Electrochromic element
US4229080A (en) * 1977-06-29 1980-10-21 Sharp Kabushiki Kaisha Additional electrode of electrochromic display and refreshing method for the same
US4214820A (en) * 1978-09-15 1980-07-29 Timex Corporation Electrochromic display having enhanced night viewability
US4286308A (en) * 1979-09-04 1981-08-25 Polaroid Corporation Apparatus and method for reducing headlight glare
US5069535A (en) * 1987-10-24 1991-12-03 Schott Glaswerke Electrochromic layer-set
US4893908A (en) * 1988-06-27 1990-01-16 Allied-Signal Inc. Adjustable tint window with electrochromic conductive polymer
US5042923A (en) * 1988-06-27 1991-08-27 Allied-Signal, Inc. Adjustable tint window with electrochromic conductive polymer
US4993810A (en) * 1989-04-14 1991-02-19 Ford Motor Company Electrochromic devices comprising metal salts in an ion conductive material
US5097358A (en) * 1989-04-27 1992-03-17 Toyoda Gosei Co., Ltd. Electrochromic element
US5108048A (en) * 1989-09-15 1992-04-28 The Boeing Company Stowage bin and support panel system for convertible aircraft and method of installation
US5457564A (en) * 1990-02-26 1995-10-10 Molecular Displays, Inc. Complementary surface confined polymer electrochromic materials, systems, and methods of fabrication therefor
US5883220A (en) * 1992-01-12 1999-03-16 Centre National De La Recherche Scientifique Redox copolymers and their use in preparing mixed conduction materials
US5699192A (en) * 1992-04-10 1997-12-16 Sun Active Glass Electrochromics, Inc. Electrochromic structures and methods
US20030209893A1 (en) * 1992-05-05 2003-11-13 Breed David S. Occupant sensing system
US5347434A (en) * 1992-07-06 1994-09-13 Mcdonnell Douglas Corporation Aircraft bag-rack with an illuminated handrail
US5384653A (en) * 1992-11-06 1995-01-24 Midwest Research Institute Stand-alone photovoltaic (PV) powered electrochromic window
US5598293A (en) * 1993-01-22 1997-01-28 Societa Italiana Vetro - Siv - S.P.A Electrochromic glass for use in cars and buildings
US6954300B2 (en) * 1993-02-26 2005-10-11 Donnelly Corporation Electrochromic polymeric solid films, manufacturing electrochromic devices using such sold films, and processes for making such solid films and devices
US5724176A (en) * 1993-03-30 1998-03-03 Nippon Oil Co., Ltd. Counterelectrode for smart window and smart window
US6136161A (en) * 1993-11-12 2000-10-24 Ppg Industries Ohio, Inc. Fabrication of electrochromic device with plastic substrates
US6005705A (en) * 1994-04-18 1999-12-21 Institut Fuer Neue Materialien Gemeinnuetzige Gmbh Electrochromic thin-film systems and components thereof
US5764402A (en) * 1994-04-29 1998-06-09 Glaverbel Optical cell control system
US5888431A (en) * 1994-07-22 1999-03-30 Gentex Corporation Electrochromic layer and devices comprising same
US5729379A (en) * 1994-10-26 1998-03-17 Donnelly Corporation Electrochromic devices
US5838483A (en) * 1995-02-10 1998-11-17 Donnelly Corporation Photochromic devices
US6246505B1 (en) * 1995-02-10 2001-06-12 Donnelly Corporation Photochromic devices
US5750282A (en) * 1995-06-07 1998-05-12 Duracell Inc. Process for improving lithium ion cell
US5878809A (en) * 1995-07-20 1999-03-09 Mercedes-Benz Ag Process and system for controlling an air-conditioning system for a vehicle interior
US6197923B1 (en) * 1995-10-27 2001-03-06 Nissan Chemical Industries, Ltd. Polymers, method of producing the same and use of the same
US5642022A (en) * 1995-12-01 1997-06-24 Msa Aircraft Interior Products, Inc. Aircraft window shade speed regulation control system
US5654786A (en) * 1996-01-11 1997-08-05 Robert C. Burlingame Optical lens structure and control system for maintaining a selected constant level of transmitted light at a wearer's eyes
US5805330A (en) * 1996-03-15 1998-09-08 Gentex Corporation Electro-optic window incorporating a discrete photovoltaic device
US6433913B1 (en) * 1996-03-15 2002-08-13 Gentex Corporation Electro-optic device incorporating a discrete photovoltaic device and method and apparatus for making same
US6178034B1 (en) * 1996-04-10 2001-01-23 Donnelly Corporation Electrochromic devices
US6493128B1 (en) * 1996-08-20 2002-12-10 Donnelly Corporation Chromogenic window assembly construction and other chromogenic devices
US6280882B1 (en) * 1997-01-17 2001-08-28 Hydro-Quebec Electrolytic composition with polymer base for electrochemical generator
US6056410A (en) * 1997-04-02 2000-05-02 Donnelly Corporation Digital electrochromic mirror system
US6011642A (en) * 1997-04-18 2000-01-04 U.S. Philips Corporation Electrochromic element, a display device provided with same and a method of manufacturing an electrochromic layer
US6130772A (en) * 1997-06-06 2000-10-10 Cava; Frank James Electrochromic device and method
US6297900B1 (en) * 1997-07-22 2001-10-02 Sustainable Technologies Australia Limited Electrophotochromic smart windows and methods
US6296973B1 (en) * 1997-09-11 2001-10-02 Hydro - Quebec Solvents and novel electrolytic compositions having a large range of stability and high conductivity
US5923456A (en) * 1997-12-19 1999-07-13 Rockwell International Corporation Reversible electrochemical mirror
US6327070B1 (en) * 1998-05-29 2001-12-04 Bayer Aktiengesellschaft Electrochromic assembly based on poly(3,4-ethylenedioxythiophene) derivatives in combination with a lithium niobate counterelectrode
US20020044331A1 (en) * 1998-07-02 2002-04-18 Anoop Agrawal Busbars for electrically powered cells
US6317248B1 (en) * 1998-07-02 2001-11-13 Donnelly Corporation Busbars for electrically powered cells
US6594065B2 (en) * 1998-11-30 2003-07-15 Gentex Corporation Electrochromic structures
US6222177B1 (en) * 1999-01-19 2001-04-24 Gentex Corporation Electrochromic element driver with negative output resistance
US6541156B1 (en) * 1999-11-16 2003-04-01 Mitsubishi Chemical Corporation Negative electrode material for non-aqueous lithium secondary battery, method for manufacturing the same, and non-aqueous lithium secondary battery using the same
US6822778B2 (en) * 2000-03-07 2004-11-23 Eclipse Energy Systems, Inc. Electrochromic layer
US6515787B1 (en) * 2000-03-07 2003-02-04 Eclipse Energy Systems, Inc. Electrochromic layer
US6795226B2 (en) * 2000-05-04 2004-09-21 Schott Corporation Chromogenic glazing
US20020118437A1 (en) * 2000-06-13 2002-08-29 Rukavina Thomas G. Colored electrochromic transparent window assemblies
US6567708B1 (en) * 2000-07-25 2003-05-20 Gentex Corporation System to interconnect, link, and control variable transmission windows and variable transmission window constructions
US20030192991A1 (en) * 2000-08-03 2003-10-16 Rukavina Thomas G. Switchable electrochromic devices for use in aircraft transparency windows
US20020135881A1 (en) * 2000-08-03 2002-09-26 Rukavina Thomas G. Switchable electrochromic devices with uniform switching and preferential area shading
US6561460B2 (en) * 2000-08-03 2003-05-13 Ppg Industries Ohio, Inc. Switchable electrochromic devices for use in aircraft transparency windows
US20030047457A1 (en) * 2000-08-03 2003-03-13 Rukavina Thomas G. Switchable electrochromic devices with uniform switching and preferential area shading
US6783099B2 (en) * 2000-08-03 2004-08-31 Ppg Industries Ohio, Inc. Switchable electrochromic devices for use in aircraft transparency windows
US6471360B2 (en) * 2000-08-03 2002-10-29 Ppg Industries Ohio, Inc. Switchable electrochromic devices with uniform switching and preferential area shading
US20030233172A1 (en) * 2000-09-04 2003-12-18 Claes-Goran Granqvist Climate control system and a method for controlling such
US6501587B1 (en) * 2000-09-27 2002-12-31 Board Of Regents, The University Of Texas System Method of creating color-changing displays
US6535126B2 (en) * 2000-12-15 2003-03-18 Ppg Industries Ohio, Inc. Electrochromic transparency incorporating security system
US20020080290A1 (en) * 2000-12-25 2002-06-27 Fuji Photo Film Co., Ltd. Method and apparatus for displaying image by producing polarization inversion in ferroelectric member and producing contrast in contrast production member
US7001868B2 (en) * 2000-12-27 2006-02-21 Fuji Photo Film Co., Ltd. Image recording apparatus and method and recording sheet for use therewith
US6587250B2 (en) * 2001-03-07 2003-07-01 Acreo Ab Electrochromic device
US6639708B2 (en) * 2001-04-24 2003-10-28 Schott North America, Inc Electrochromic safety glazing
US20020196519A1 (en) * 2001-04-24 2002-12-26 Yasser Elkadi Electrochromic safety glazing
US20020196518A1 (en) * 2001-06-25 2002-12-26 University Of Washington Electrochromic organic polymer synthesis and devices utilizing electrochromic organic polymers
US6747780B2 (en) * 2001-06-25 2004-06-08 University Of Washington Electrochromic organic polymer synthesis and devices utilizing electrochromic organic polymers
US6819367B1 (en) * 2001-10-19 2004-11-16 Frank James Cava Shade-free light control system and method
US20030174377A1 (en) * 2001-11-21 2003-09-18 University Of Florida Electrochromic polymers and polymer electrochromic devices
US20030184692A1 (en) * 2002-03-26 2003-10-02 Nobukazu Nagae Light modulating device
US6848653B2 (en) * 2002-05-10 2005-02-01 Goodrich Hella Aerospace Lighting Systems Gmbh Operating and/or display unit for vehicles
US20040021928A1 (en) * 2002-06-21 2004-02-05 Warner Benjamin P. Electrolytes for electrooptic devices comprising ionic liquids
US20050270619A1 (en) * 2002-07-26 2005-12-08 Koninklijke Philips Electronics N.V. Electrochromic color display having different electrochromic materials
US7526923B2 (en) * 2002-12-23 2009-05-05 Knutsen Oas Shipping As Device for condensing volatile organic compounds from a storage or transport tank into oil
US7300166B2 (en) * 2003-03-05 2007-11-27 Electrochromix, Inc. Electrochromic mirrors and other electrooptic devices
US6843068B1 (en) * 2003-07-25 2005-01-18 Honeywell International Inc. Method and apparatus for adjusting the temperature set point based on humidity level for increased comfort
US20050068629A1 (en) * 2003-09-26 2005-03-31 Primal Fernando Adjustably opaque window
US20050200937A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Multi-color electrochromic apparatus and methods
US20050200933A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Low vapor pressure solvent for electrochromic devices

Cited By (106)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080259433A1 (en) * 2004-03-12 2008-10-23 The Boeing Company Multi-color electrochromic apparatus and methods
US8988757B2 (en) 2004-03-12 2015-03-24 The Boeing Company Low vapor pressure solvent for electrochromic devices
US8064120B2 (en) 2004-03-12 2011-11-22 The Boeing Company Aircraft cabin services system including zone controllers for lighting control modules and dimmable windows
US20050200933A1 (en) * 2004-03-12 2005-09-15 The Boeing Company Low vapor pressure solvent for electrochromic devices
US7782519B2 (en) 2004-03-12 2010-08-24 The Boeing Company Multi-color electrochromic apparatus and methods
US20070097484A1 (en) * 2004-11-03 2007-05-03 Libretto John Electrochromic glass control device
US7375871B2 (en) * 2004-11-03 2008-05-20 Leviton Manufacturing Co., Inc. Electrochromic glass control device
US20070097238A1 (en) * 2005-10-06 2007-05-03 Asia Optical Co., Inc. Method for rapidly changing the color of a light source and image apparatus using the same
US7913385B2 (en) 2005-12-02 2011-03-29 The Boeing Company Method of attenuating electromagnetic energy
US20070137117A1 (en) * 2005-12-02 2007-06-21 Carlson Ryan L Conductive gasket apparatus and method
US7355161B2 (en) 2005-12-15 2008-04-08 The Boeing Company Systems and methods for controlling windows with variable light transmission
US20080144158A1 (en) * 2006-01-30 2008-06-19 Airbus Deutschland Gmbh Power supply for an electric window dimming device
US7746037B2 (en) * 2006-01-30 2010-06-29 Airbus Deutschland Gmbh Power supply for an electric window dimming device
US7505136B2 (en) 2006-05-16 2009-03-17 The Boeing Company Testing and tuning electrically dimmable windows
US20080055731A1 (en) * 2006-08-31 2008-03-06 The Boeing Company Airplane window control
US7893890B2 (en) 2007-03-05 2011-02-22 The Boeing Company Electrically dimmable combiner optics for head-up display
US20080218434A1 (en) * 2007-03-05 2008-09-11 The Boeing Company Electrically Dimmable Combiner Optics for Head-Up Display
US20080230653A1 (en) * 2007-03-23 2008-09-25 The Boeing Company Self-Powered Dimmable Windows with Integrated Controls
US20080234893A1 (en) * 2007-03-23 2008-09-25 The Boeing Company Window control system
US9146438B2 (en) 2007-03-23 2015-09-29 The Boeing Company Self-powered dimmable windows with integrated controls
US8632034B2 (en) 2007-03-23 2014-01-21 The Boeing Company Self-powered dimmable windows with integrated controls
US9016630B2 (en) 2007-03-30 2015-04-28 The Boeing Company Control system for dimmable windows
US8292228B2 (en) * 2007-03-30 2012-10-23 The Boeing Company Control system for dimmable windows
GB2448041A (en) * 2007-03-30 2008-10-01 Boeing Co Control system for dimmable windows
GB2448041B (en) * 2007-03-30 2009-08-05 Boeing Co Control system for dimmable windows
US20080239451A1 (en) * 2007-03-30 2008-10-02 The Boeing Company Control System for Dimmable Windows
WO2008156966A1 (en) * 2007-06-18 2008-12-24 The Boeing Company Radio frequency shielding apparatus system and method
US8800926B2 (en) 2007-06-18 2014-08-12 The Boeing Company Radio frequency shielding apparatus system and method
US20140284425A1 (en) * 2007-06-18 2014-09-25 The Boeing Company Radio frequency shielding system
US20080308677A1 (en) * 2007-06-18 2008-12-18 Kirchoff Kenneth P Radio frequency shielding apparatus system and method
US9038949B2 (en) * 2007-06-18 2015-05-26 The Boeing Company Radio frequency shielding system
US7956869B1 (en) * 2007-07-13 2011-06-07 Adobe Systems Incorporated Proximity based transparency of windows aiding in obscured window selection
GB2468599A (en) * 2007-09-27 2010-09-15 Boeing Co Window control system
WO2009042359A1 (en) * 2007-09-27 2009-04-02 The Boeing Company Window control system
GB2468599B (en) * 2007-09-27 2012-08-29 Boeing Co Window control system
US20110043922A1 (en) * 2008-02-07 2011-02-24 Daimler Ag Vehicle Pane and Motor Vehicle Having a Vehicle Pane
US20110199976A1 (en) * 2008-03-31 2011-08-18 The Boeing Company Wireless Aircraft Sensor Network
US8344912B2 (en) 2008-03-31 2013-01-01 The Boeing Company Wireless aircraft sensor network
FR2937006A1 (en) * 2008-10-09 2010-04-16 Airbus Aircraft i.e. airplane, has inner wall made of electrochromic material that is introduced to choose transparent state to see person in one of zones from other zone through wall and to choose opaque state inhibiting view of person
US8200390B2 (en) 2009-07-30 2012-06-12 Control Solutions LLC Securable cover for vehicle lights
US20110029194A1 (en) * 2009-07-30 2011-02-03 Control Solutions, LLC Securable cover for vehicle lights
US20110026092A1 (en) * 2009-07-30 2011-02-03 Control Solutions, LLC Light blocking apparatus for vehicle mirror assembly
US8432600B2 (en) 2009-07-30 2013-04-30 Control Solutions LLC Light blocking apparatus for vehicle mirror assembly
US8248680B2 (en) 2009-07-31 2012-08-21 Control Solutions LLC Electrically activatable light blocking cover for vehicle mirrors
US20110026091A1 (en) * 2009-07-31 2011-02-03 Control Solutions, LLC Electrically activatable light blocking cover for vehicle mirrors
US20110063864A1 (en) * 2009-09-16 2011-03-17 Control Solutions, LLC Securable cover with electrically activatable light inhibiting lens for vehicle lights
US8256940B2 (en) 2009-09-16 2012-09-04 Control Solutions LLC Securable cover with electrically activatable light inhibiting lens for vehicle lights
US9128346B2 (en) 2009-12-22 2015-09-08 View, Inc. Onboard controller for multistate windows
US9946138B2 (en) 2009-12-22 2018-04-17 View, Inc. Onboard controller for multistate windows
US10001691B2 (en) 2009-12-22 2018-06-19 View, Inc. Onboard controller for multistate windows
US10268098B2 (en) 2009-12-22 2019-04-23 View, Inc. Onboard controller for multistate windows
US9442341B2 (en) 2009-12-22 2016-09-13 View, Inc. Onboard controller for multistate windows
US10303035B2 (en) 2009-12-22 2019-05-28 View, Inc. Self-contained EC IGU
US9436055B2 (en) 2009-12-22 2016-09-06 View, Inc. Onboard controller for multistate windows
US9234637B2 (en) 2010-07-19 2016-01-12 Greenwave PTE. LTD. Emitting light using multiple phosphors
US8820981B2 (en) * 2010-07-19 2014-09-02 Greenwave Reality Pte Ltd Electrically controlled glass in a lamp
US20120013238A1 (en) * 2010-07-19 2012-01-19 Greenwave Reality, Inc. Electrically Controlled Glass in a Lamp
US8764210B2 (en) 2010-07-19 2014-07-01 Greenwave Reality Pte Ltd. Emitting light using multiple phosphors
US9442340B2 (en) 2010-07-19 2016-09-13 Greenwave Systems, PTE LTD Electrically controlled glass in a lamp
US20120144496A1 (en) * 2010-12-04 2012-06-07 Hon Hai Precision Industry Co., Ltd. Electronic device with data protection function and method thereof
US9482922B2 (en) 2011-03-16 2016-11-01 View, Inc. Multipurpose controller for multistate windows
US8864321B2 (en) 2011-03-16 2014-10-21 View, Inc. Controlling transitions in optically switchable devices
US8213074B1 (en) 2011-03-16 2012-07-03 Soladigm, Inc. Onboard controller for multistate windows
US8254013B2 (en) 2011-03-16 2012-08-28 Soladigm, Inc. Controlling transitions in optically switchable devices
US9927674B2 (en) 2011-03-16 2018-03-27 View, Inc. Multipurpose controller for multistate windows
US9778532B2 (en) 2011-03-16 2017-10-03 View, Inc. Controlling transitions in optically switchable devices
US9645465B2 (en) 2011-03-16 2017-05-09 View, Inc. Controlling transitions in optically switchable devices
US9454055B2 (en) 2011-03-16 2016-09-27 View, Inc. Multipurpose controller for multistate windows
US8925286B2 (en) 2011-09-23 2015-01-06 GM Global Technology Operations LLC Window module with integrated electropolymeric sunshade
CN103009970A (en) * 2011-09-23 2013-04-03 通用汽车环球科技运作有限责任公司 Window module with integrated electropolymeric sunshade
US10254618B2 (en) 2011-10-21 2019-04-09 View, Inc. Mitigating thermal shock in tintable windows
US9523902B2 (en) 2011-10-21 2016-12-20 View, Inc. Mitigating thermal shock in tintable windows
US10365531B2 (en) 2012-04-13 2019-07-30 View, Inc. Applications for controlling optically switchable devices
US9348192B2 (en) 2012-04-17 2016-05-24 View, Inc. Controlling transitions in optically switchable devices
US9454056B2 (en) 2012-04-17 2016-09-27 View, Inc. Driving thin film switchable optical devices
US9921450B2 (en) 2012-04-17 2018-03-20 View, Inc. Driving thin film switchable optical devices
US10520784B2 (en) 2012-04-17 2019-12-31 View, Inc. Controlling transitions in optically switchable devices
US8705162B2 (en) 2012-04-17 2014-04-22 View, Inc. Controlling transitions in optically switchable devices
US9081247B1 (en) 2012-04-17 2015-07-14 View, Inc. Driving thin film switchable optical devices
US10520785B2 (en) 2012-04-17 2019-12-31 View, Inc. Driving thin film switchable optical devices
US9423664B2 (en) 2012-04-17 2016-08-23 View, Inc. Controlling transitions in optically switchable devices
US9030725B2 (en) 2012-04-17 2015-05-12 View, Inc. Driving thin film switchable optical devices
US9477131B2 (en) 2012-04-17 2016-10-25 View, Inc. Driving thin film switchable optical devices
US20140140080A1 (en) * 2012-06-11 2014-05-22 Msa Aircraft Products Ltd. Light ring for an aircraft cabin window
US9694896B1 (en) * 2013-01-03 2017-07-04 The Boeing Company Airplane window having infrared heat reflection capability
US9638978B2 (en) 2013-02-21 2017-05-02 View, Inc. Control method for tintable windows
US10048561B2 (en) 2013-02-21 2018-08-14 View, Inc. Control method for tintable windows
US20170121007A1 (en) * 2013-05-17 2017-05-04 Honda Patents & Technologies North America, Llc Window of an aircraft
US9919789B2 (en) * 2013-05-17 2018-03-20 Honda Patents & Technologies North America, Llc Window of an aircraft
US10451950B2 (en) 2013-06-28 2019-10-22 View, Inc. Controlling transitions in optically switchable devices
US9412290B2 (en) 2013-06-28 2016-08-09 View, Inc. Controlling transitions in optically switchable devices
US10514582B2 (en) 2013-06-28 2019-12-24 View, Inc. Controlling transitions in optically switchable devices
US10120258B2 (en) 2013-06-28 2018-11-06 View, Inc. Controlling transitions in optically switchable devices
US9885935B2 (en) 2013-06-28 2018-02-06 View, Inc. Controlling transitions in optically switchable devices
US10503039B2 (en) 2013-06-28 2019-12-10 View, Inc. Controlling transitions in optically switchable devices
US10401702B2 (en) 2013-06-28 2019-09-03 View, Inc. Controlling transitions in optically switchable devices
US10221612B2 (en) 2014-02-04 2019-03-05 View, Inc. Infill electrochromic windows
CN107107715A (en) * 2014-11-21 2017-08-29 金泰克斯公司 Electro-optical package
US10054836B2 (en) 2014-11-21 2018-08-21 Gentex Corporation Electro-optic assembly
WO2016081858A1 (en) * 2014-11-21 2016-05-26 Gentex Corporation Electro-optic assembly
US10101583B2 (en) 2015-06-16 2018-10-16 Gentex Corporation Heads up display system
US9470828B1 (en) 2015-06-19 2016-10-18 The Boeing Company Local light attenuation for improving reliability of electronic dimmable windows
US9927609B2 (en) 2015-08-14 2018-03-27 Gentex Corporation Heads up display system
US10495939B2 (en) 2015-10-06 2019-12-03 View, Inc. Controllers for optically-switchable devices
US20170283065A1 (en) * 2016-04-04 2017-10-05 B/E Aerospace, Inc. Aircraft Interior Surface and Method of Illuminating an Aircraft Interior Surface
US10539854B2 (en) 2017-03-21 2020-01-21 View, Inc. Control method for tintable windows

Also Published As

Publication number Publication date
US8988757B2 (en) 2015-03-24
US20050200933A1 (en) 2005-09-15

Similar Documents

Publication Publication Date Title
KR101775332B1 (en) Variable transmittance optical filter and uses thereof
JP4874524B2 (en) Electrophoretic display device
DE69920228T2 (en) Method for improving color reproduction in electrophoretic devices using microcapsules
US7144289B2 (en) Method of forming an illuminated design on a substrate
US5638084A (en) Lighting-independent color video display
US20030047457A1 (en) Switchable electrochromic devices with uniform switching and preferential area shading
JP6440791B2 (en) Light modulator
TWI484275B (en) Electro-optic display, method for driving the same and microcavity electrophoretic display
EP2548077B1 (en) Multi-color electrophoretic displays
CN101501757B (en) Variable transmission window system
JP2005003964A (en) Image display medium, image display device, and image display method
JP3566524B2 (en) Electrophoretic display
JP4265149B2 (en) Electro-optical device and method for manufacturing electro-optical device
EP2512920B1 (en) Supply module for passenger transport vehicles
US7663797B2 (en) Multicolor display element
CN101738812B (en) Vehicular rearview mirror elements and assemblies incorporating these elements
CA2513063C (en) Vehicle information displays
RU2369889C1 (en) Video panel with multi-layer priming
JP4085565B2 (en) Image display medium driving method and image display apparatus
KR101856834B1 (en) Colored electrophoretic displays
US7237933B2 (en) Door trim bolster with electroluminescent lamp and injection molding method of making same
US20080079012A1 (en) Illuminated devices utilizing transparent light active sheet material with integrated light emitting diode (LED), and methods and kit therefor
JP2006106669A (en) Multicolor display element
WO1993024922A1 (en) Electromagnetic-wave modulating, movable electrode, capacitor elements
US6864927B1 (en) Head up display with adjustable transparency screen

Legal Events

Date Code Title Description
AS Assignment

Owner name: BOEING COMPANY, THE, ILLINOIS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:CALLAHAN, KEVIN S.;SCAFER, ROLAND L., JR.;REEL/FRAME:015934/0001

Effective date: 20041026

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION