Self-powered dimmable windows with integrated controls
First Claim
1. A dimmable window system for a vehicle, comprising:
- a sidewall panel assembly having at least one window opening;
an electrically dimmable window mounted in the window opening on the sidewall panel;
an inner window mounted within the window opening, inside of the dimmable window;
a pair of photovoltaic energy harvesting devices for converting ambient light into electrical power;
a seal comprising a boot surrounding the window opening and configured to seal an air gap between the dimmable window and an outer window of the vehicle, wherein the pair of photovoltaic energy harvesting devices are placed within folds of the boot within the air gap and substantially hidden from a line of sight of a person in an interior of the vehicle; and
,a controller mounted in proximity to the dimmable window for controlling the opacity of the dimmable window using only the energy harvested by the energy harvesting device;
all wiring associated with powering and controlling said dimmable window is internal to said sidewall panel assembly.
1 Assignment
0 Petitions
Accused Products
Abstract
An electrically controlled dimmable window for aircraft includes a controller and power that eliminates the need for wiring connections to on-board systems. The controller is integrated into the sidewall in which the window is mounted. Power for controlling the window is derived from an energy harvesting device that generates power by converting thermal gradients, motion/vibration or light energy present near the window. The integrated controller includes passenger controls for adjusting the opacity of the window, power conditioning circuitry, an electrical power storage device such as a battery, a processor and a radio receiver. The window can be remotely controlled by a cabin attendant from a central controller that transmits window control signals to the radio receiver.
28 Citations
24 Claims
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1. A dimmable window system for a vehicle, comprising:
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a sidewall panel assembly having at least one window opening; an electrically dimmable window mounted in the window opening on the sidewall panel; an inner window mounted within the window opening, inside of the dimmable window; a pair of photovoltaic energy harvesting devices for converting ambient light into electrical power; a seal comprising a boot surrounding the window opening and configured to seal an air gap between the dimmable window and an outer window of the vehicle, wherein the pair of photovoltaic energy harvesting devices are placed within folds of the boot within the air gap and substantially hidden from a line of sight of a person in an interior of the vehicle; and
,a controller mounted in proximity to the dimmable window for controlling the opacity of the dimmable window using only the energy harvested by the energy harvesting device; all wiring associated with powering and controlling said dimmable window is internal to said sidewall panel assembly. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A sidewall assembly for aircraft, comprising:
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a sidewall panel having a window opening; an electrically dimmable window mounted in the window opening on the sidewall panel; an inner window mounted within the window opening, inside of the dimmable window; a seal comprising a boot surrounding the window opening and configured to seal an air gap between the dimmable window and an outer window of the aircraft; a pair of photovoltaic energy harvesting devices, placed within folds of the boot within the air gap and substantially hidden from a line of sight of a person in an interior of the aircraft, configured for converting ambient light into electrical power; and a control module connected with the sidewall panel for powering and controlling the operation of the dimmable window, the control module including a device for storing electrical energy used to control the dimmable window, said dimmable window controlled by using only energy harvested by the photovoltaic energy harvesting device; all wiring associated with powering and controlling said dimmable window is internal to said sidewall panel assembly. - View Dependent Claims (9, 10, 11, 12, 13)
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14. A self-powered, electrically dimmable window assembly for aircraft, comprising:
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a dimmable window having electrically controlled opacity; outer and inner windows mounted on opposite sides of the dimmable window; a seal comprising a boot that seals an air gap between the dimmable window and the outer window; a photovoltaic energy harvesting device placed within folds of the boot in the air gap and substantially hidden from a line of sight of a person in an interior of the aircraft, configured for harvesting energy on-board the aircraft and converting the harvested energy to electrical power; a device for storing the electrical power harvested by the energy harvesting device; and
,a controller for controlling the opacity of the dimmable window using only said harvested electrical power stored in the storage device; said dimmable window comprises a sidewall panel assembly and all wiring associated with powering and controlling said dimmable window is associated only with said dimmable window and internal to said sidewall panel assembly. - View Dependent Claims (15, 16, 17, 18)
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19. A sidewall panel assembly for aircraft, comprising:
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a sidewall panel assembly having at least one window opening therein; an electrically dimmable window mounted on the sidewall panel within the window opening; a seal comprising a boot surrounding the window opening and configured to seal an air gap between the dimmable window and an outer window of the aircraft; a pair of photovoltaic devices for converting ambient light into electrical power, placed in folds of the boot in the air gap; and
,a controller for controlling the operation of the dimmable window using only electrical power produced by the photovoltaic device; all wiring associated with powering and controlling said dimmable window is associated only with said dimmable window and internal to said sidewall panel assembly. - View Dependent Claims (20, 21, 22, 23, 24)
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Specification