Liquid crystal displays utilizing polymer dispersed liquid crystal devices for enhanced performance and reduced power

• US 6,144,359 A
• Filed: 03/30/1998
• Issued: 11/07/2000
• Est. Priority Date: 03/30/1998
• Status: Expired due to Term

• Current Assignee: Teledyne Scientific & Imaging, LLC (Teledyne Technologies Incorporated)
• Original Assignee: Rockwell Science Center LLC
• Inventors: Grave, Duane A.
• Primary Examiner(s): WU, XIAO MIN
• Application Number:
  US09/050,781
• Time in Patent Office: 953 Days
• Field of Search: 345/102, 345/88, 345/87, 345/98, 345/100, 345/211, 345/207, 359/51, 359/53, 315/158, 340/784, 349/61, 349/64, 349/114, 349/25, 349/35
• US Class Current: 345/102
• CPC Class Codes: B60K 2360/349 Adjustment of brightness
• CPC Class Codes: B60Q 3/14 lighting through the surface to be illuminated
• CPC Class Codes: B60Q 3/18 for varying the light intensity
• CPC Class Codes: G02F 1/1334 based on polymer dispersed liquid crystals, e.g. microencapsulated liquid crystals
• CPC Class Codes: G02F 1/133605 including specially adapted reflectors
• CPC Class Codes: G02F 1/133626 providing two modes of illumination, e.g. day-night
• CPC Class Codes: G02F 2201/58 Arrangements comprising a monitoring photodetector
• CPC Class Codes: G09G 2300/0456 with a reflective area and a transmissive area combined in one pixel, such as in transflectance pixels
• CPC Class Codes: G09G 2320/0626 for control of overall brightness
• CPC Class Codes: G09G 2360/144 the light being ambient light
• CPC Class Codes: G09G 3/3406 Control of illumination source illumination devices structurally associated with liquid crystal cells G02F1/1336

Abstract

Disclosed is an avionics display device for use in the cockpit of an aircraft. The display device includes a liquid crystal display adapted for using a source of light to display information to a viewer and a backlight adapted to controllably provide a portion of the source of light for use by the liquid crystal display in displaying the information. A polymer dispersed liquid crystal (PDLC) device is positioned between the liquid crystal display and the backlight. An ambient light sensor adapted to sense a level of ambient light in the cockpit of the aircraft provides a sensor output indicative of the sensed ambient light level. Luminance control circuitry coupled to the ambient light sensor, to the backlight and to the PDLC device, receives the sensor output and generates as a function of the sensed ambient light level control signals for controlling the intensity of the light provided by the backlight and the transmissivity of the PDLC device.

Claims

1. An avionics display device for use in the cockpit of an aircraft, the display device comprising:

a liquid crystal display in a transflective mode adapted for using a source of light to display information to a viewer;

a backlight adapted to controllably provide at least a portion of the source of light for use by the liquid crystal display in displaying the information;

a polymer dispersed liquid crystal (PDLC) device positioned between the liquid crystal display and the backlight;

an ambient light sensor adapted to sense a level of ambient light in the cockpit of the aircraft and to provide a sensor output indicative of the sensed ambient light level; and

luminance control circuitry coupled to the ambient light sensor, to the backlight and to the PDLC device, the luminance control circuitry receiving the sensor output and generating as a function of the sensed ambient light level control signals for controlling an intensity of the light provided by the backlight and for controlling the transmissivity of the PDLC device.

2. The avionics display device of claim 1, wherein when the sensed ambient light level is indicative of day mode operations, the luminance control circuit reduces the intensity of the light provided by the backlight and reduces the transmissivity of the PDLC device such that the source of light used by the liquid crystal display is provided primarily by ambient light reflected by the PDLC device back toward the liquid crystal display.

3. The avionics display device of claim 2, wherein during day mode operations the luminance control circuit turns off the backlight such that its power consumption and light output are minimized.

4. The avionics display device of claim 2, wherein when the sensed ambient light level is indicative of night mode operations, the luminance control circuit increases the intensity of the light provided by the backlight and increases the transmissivity of the PDLC device such that an increased percentage of the light provided by the backlight is transmitted through the PDLC device and such that the source of light used by the liquid crystal display is provided primarily from the backlight.

5. The avionics display device of claim 4, wherein for each of a plurality of different levels of sensed ambient light the control circuit is adapted to control the intensity of the light provided by the backlight to a different one of plurality of intensity levels and to control the transmissivity of the PDLC device to a different one of a plurality of transmissivity levels in order to provide the source of light used by the liquid crystal display using different ones of a plurality of combinations of light from the backlight and reflected ambient light.

6. The avionics display device of claim 1, wherein the liquid crystal display is an active matrix liquid crystal display.

7. The avionics display device of claim 6, wherein the backlight includes a fluorescent lamp.

8. The avionics display device of claim 7, wherein when the sensed ambient light level is indicative of day mode operations, the luminance control circuit automatically increases the intensity of the light provided by the backlight and increases the transmissivity of the PDLC device such that an increased percentage of the light provided by the backlight is transmitted through the PDLC device to thereby increase an intensity level of the source of light used by the active matrix liquid crystal display.

9. The avionics display device of claim 8, wherein when the sensed ambient light level is indicative of night mode operations, the luminance control circuit automatically decreases the intensity of the light provided by the backlight and decreases the transmissivity of the PDLC device such that a decreased percentage of the light provided by the backlight is transmitted through the PDLC device to thereby decrease an intensity level of the source of light used by the active matrix liquid crystal display.

10. The avionics display device of claim 9, wherein when the sensed ambient light level is indicative of night mode operations, the luminance control circuit automatically decreases the intensity of the light provided by the backlight and decreases the transmissivity of the PDLC device such that the decreased percentage of the light provided by the backlight is transmitted through the PDLC device to thereby decrease the intensity level of the source of light used by the active matrix liquid crystal display.

11. The avionics display device of claim 10, wherein for each of a plurality of different levels of sensed ambient light the control circuit is adapted to control the intensity of the light provided by the backlight to a different one of plurality of intensity levels or to control the transmissivity of the PDLC device to a different one of a plurality of transmissivity levels in order to provide the source of light used by the liquid crystal display at a corresponding different one of a plurality of intensity levels.

12. An avionics display device for use in the cockpit of an aircraft, the display device comprising:

transmissive mode liquid crystal display means for displaying information to a viewer;

backlight means for controllably providing a first source of light for use by the transmissive mode liquid crystal display means in displaying the information; and

polymer dispersed liquid crystal (PDLC) device means positioned between the transmissive mode liquid crystal display means and the backlight means for controllably transmitting toward the transmissive mode liquid crystal display means a minority of the first source of light from the backlight means during night mode operations; and

ambient light sensing means for sensing a level of ambient light in the cockpit of the aircraft and providing a sensor output indicative of the sensed ambient light level; and

luminance control means coupled to the ambient light sensing means, to the backlight means and to the PDLC device means, for receiving the sensor output and automatically generating as a function of the sensed ambient light level control signals for controlling an intensity of the first source of light provided by the backlight means and for controlling a transmissivity of the PDLC device means.

13. The avionics display device of claim 12, wherein when the sensed ambient light level is indicative of day mode operations, the luminance control means controls the backlight means and the PDLC device means to increase the intensity of the first source of light provided by the backlight means and to increase the transmissivity of the PDLC device means such that the light used by the transmissive mode liquid crystal display means is provided primarily by the backlight means.

14. The avionics display device of claim 13, wherein when the sensed ambient light level is indicative of night mode operations, the luminance control means reduces the intensity of the first source of light provided by the backlight means and reduces the transmissivity of the PDLC device means such that light provided by the backlight means is transmitted through the PDLC device means at low level for night operation overcoming limitations of backlight low level operation.

15. The avionics display device of claim 14, wherein for each of a plurality of different levels of sensed ambient light the luminance control means controls the intensity of the first source of light provided by the backlight means to a different one of plurality of intensity levels and controls the transmissivity of the PDLC device means to a different one of a plurality of transmissivity levels in order to provide the light used by the transmissive mode liquid crystal display means.

16. A method of controlling an avionics display device having a liquid crystal display adapted for using a source of light to display information to a viewer, a backlight adapted to controllably provide at least a portion of the source of light for use by the liquid crystal display in displaying the information, and a polymer dispersed liquid crystal (PDLC) device positioned between the liquid crystal display and the backlight, the method comprising:

sensing a level of ambient light in the cockpit of an aircraft in which the avionics display device is installed; and

automatically controlling the intensity of the light provided by the backlight and the transmissivity of the PDLC device as functions of the sensed ambient light level.

17. The method of claim 16, wherein the step of controlling further includes automatically controlling the intensity of the light provided by the backlight and the transmissivity of the PDLC device when the sensed ambient light level is indicative of day mode operations such that the intensity of the light provided by the backlight and the transmissivity of the PDLC device are reduced so that the source of light used by the liquid crystal display is provided primarily by ambient light reflected by the PDLC device back toward the liquid crystal display.

18. The method of claim 17, wherein the step of controlling further includes automatically controlling the intensity of the light provided by the backlight and the transmissivity of the PDLC device when the sensed ambient light level is indicative of night mode operations such that the intensity of the light provided by the backlight and the transmissivity of the PDLC device are increased so that the source of light used by the liquid crystal display is provided primarily by the backlight.