Adjustable Gradient Tinting for Aircraft Windscreen
An aircraft windscreen comprises a plurality of liquid crystal display (LCD) films positioned on or within various portions of the windscreen to define a corresponding plurality of zones. The opacity of the LCD films are individually and separately controllable by control circuitry in communication with user controls to allow a user to darken or lighten portions of the various LCD films to achieve a desired level of gradient tint in the defined zones to block external light, such as sunlight, from the aircraft.
1 . An adjustable gradient tinting for an aircraft windscreen, comprising:
a windscreen comprising a contiguous transparent surface;
an electrochromic film attached to the windscreen, wherein the electrochromic film defines a plurality of zones on the windscreen; and
control circuitry operable to cause the electrochromic film to produce a semi-opaque gradient pattern such that the gradient pattern impedes the transmission of light through at least a portion of the windscreen.
2 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein the electrochromic film comprises: LCD technology, SPD technology, PDLC technology, or combinations thereof.
3 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein an opacity of the electrochromic film is adjusted by the control circuitry in response to a user input.
4 . The adjustable gradient tinting for an aircraft windscreen of claim 3 , wherein the user input comprises a user-operable control in communication with the control circuitry.
5 . The adjustable gradient tinting for an aircraft windscreen of claim 4 , wherein the user-operable control comprises a linear control, a rotary control, a sound actuated control, or combinations thereof.
6 . The adjustable gradient tinting for an aircraft windscreen of claim 3 , wherein the user input comprises a sensor operable to detect a gesture made by a user.
7 . The adjustable gradient tinting for an aircraft windscreen of claim 5 , wherein the sensor comprises an infrared sensor, a capacitive sensor, an ultrasonic sensor, a video sensor, a microwave sensor, or combinations thereof.
8 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , further comprising one or more cockpit side windows, wherein the one or more cockpit side windows comprise an electrochromic film in communication with and controlled by the control circuitry.
9 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein the electrochromic film is embedded within the windscreen.
10 . The adjustable gradient tinting for an aircraft windscreen, wherein the electrochromic film encompasses at least sixty percent of the windscreen.
11 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein the control circuitry includes driver circuitry operable to cause the electrochromic film to produce a semi-opaque gradient pattern such that the gradient pattern impedes the transmission of light through at least a portion of the windscreen.
12 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein the control circuitry comprises logic circuitry operable to limit the opacity of the electrochromic film.
13 . The adjustable gradient tinting for an aircraft windscreen of claim 12 , wherein limits to the opacity of the electrochromic film are user defined, predetermined, or combinations thereof.
14 . An adjustable gradient tinting for an aircraft windscreen, comprising:
a windscreen comprising a transparent surface;
an electrochromic film attached to the windscreen and covering at least a portion of the transparent surface, wherein the electrochromic film defines at least one zone on the windscreen; and
control circuitry operable to cause the electrochromic film to produce a semi-opaque gradient pattern such that the gradient pattern impedes the transmission of light through at least a portion of the transparent surface.
15 . The adjustable gradient tinting for an aircraft windscreen of claim 14 , wherein the electrochromic film comprises: LCD technology, SPD technology, PDLC technology, or combinations thereof.
16 . The adjustable gradient tinting for an aircraft windscreen of claim 1 , wherein an opacity of the electrochromic film is adjusted by the control circuitry in response to a user-operable control in communication with the control circuitry.
17 . The adjustable gradient tinting for an aircraft windscreen of claim 16 , wherein the user-operable control comprises a linear control, a rotary control, a sound actuated control, a motion sensor, an infrared sensor, a capacitive sensor, an ultrasonic sensor, a video sensor, a microwave sensor, or combinations thereof.
18 . The adjustable gradient tinting for an aircraft windscreen of claim 14 , wherein the control circuitry includes driver circuitry operable to cause the electrochromic film to produce a semi-opaque gradient pattern such that the gradient pattern impedes the transmission of light through at least a portion of the windscreen.
19 . The adjustable gradient tinting for an aircraft windscreen of claim 14 , wherein the control circuitry comprises logic circuitry operable to limit the opacity of the electrochromic film.
20 . The adjustable gradient tinting for an aircraft windscreen of claim 19 , wherein limits to the opacity of the electrochromic film are user defined, predetermined, or combinations thereof.