Processor controlled fluorescent lamp dimmer for aircraft liquid crystal display instruments
First Claim
1. A dimmer control arrangement for an aircraft display including a liquid crystal display and associated fluorescent lamp backlight, the control arrangement comprising:
- sensors monitoring conditions of said fluorescent lamp effecting perceived luminance of said display, said sensors providing corresponding sensor outputs;
an energy delivery mechanism delivering a selected magnitude of energy to said lamp at a selected frequency;
a memory means containing a plurality of frequencies, each frequency of said plurality of frequencies is retrievable as a function of said sensor outputs; and
a processor element receiving said sensor outputs and programmed to access said memory means and provide to said energy delivery system a representation of said selected frequency whereby said energy delivery system delivers said selected magnitude of energy at said selected frequency.
1 Assignment
0 Petitions
Accused Products
Abstract
A processor controlled fluorescent lamp dimmer circuit is shown for use in an aircraft display system utilizing a fluorescent lamp in the backlight system of individual LCD display devices. By use of a processor control dimming circuit in control over each LCD display, greater flexibility, e.g., as by adjustment in software parameters, is made possible in the operation of a dimmer control circuit. The dimmer control circuit reacts to such conditions as ambient light within the aircraft cockpit, fluorescent lamp light energy output, and fluorescent lamp temperature to provide substantially consistent actual and perceived luminance on the LCD display as a function of such detected conditions. Furthermore, the processor control achieves the desired luminance without over-driving, and therefore deteriorating, the lamps. As a result, the pilot of the aircraft enjoys a more reliable and consistent LCD display and need not be distracted by variation in luminance of the LCD display in operation of the aircraft.
87 Citations
6 Claims
-
1. A dimmer control arrangement for an aircraft display including a liquid crystal display and associated fluorescent lamp backlight, the control arrangement comprising:
-
sensors monitoring conditions of said fluorescent lamp effecting perceived luminance of said display, said sensors providing corresponding sensor outputs; an energy delivery mechanism delivering a selected magnitude of energy to said lamp at a selected frequency; a memory means containing a plurality of frequencies, each frequency of said plurality of frequencies is retrievable as a function of said sensor outputs; and a processor element receiving said sensor outputs and programmed to access said memory means and provide to said energy delivery system a representation of said selected frequency whereby said energy delivery system delivers said selected magnitude of energy at said selected frequency. - View Dependent Claims (2, 3, 4, 5, 6)
-
Specification