US5428265A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Processor controlled fluorescent lamp dimmer for aircraft liquid crystal display instruments
Assignee: Honeywell Inc
•
Filing: 1994-02-28
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Granted: 1995-06-27
•
Expires: 2014-02-28
Abstract
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.
Inventors
- 👤 Lawrence A. Booth, Jr.
- 👤 David W. Luz
- 👤 Robert J. Vitello
- 👤 Roger E. Wiegel
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 20:37
CPC Classifications
H; H05; H05B; H05B41/00; H05B41/14; H05B41/36; H05B41/38; H05B41/39; H05B41/392; H05B41/3921; H05B41/3922; Y; Y10; Y10S; Y10S315/00; Y10S315/04
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
125 words
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.
Claim 2
Dependent Claim
125 words
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.
Claim 3
Dependent Claim
39 words
The control arrangement according to claim 1 wherein said energy delivery system responds to a trigger signal providing trigger pulses at said selected frequency whereby said given magnitude of energy is delivered to said lamp for each trigger pulse.
Claim 4
Dependent Claim
37 words
The control arrangement according to claim 2 wherein said given magnitude of energy is delivered by delivering a given current flow into a transformer driving said fluorescent lamp until said current flow reaches a given current magnitude.
Claim 5
Dependent Claim
24 words
The control arrangement according to claim 1 wherein said sensors monitor at least one of ambient light, lamp temperature, and lamp light energy output.
Claim 6
Dependent Claim
36 words
The control arrangement according to claim 1 wherein said plurality frequencies are selected so that varying energy delivery to said lamp appears as a linear change in luminance to a viewer of the liquid crystal display.
Claim 7
Dependent Claim
15 words
The control arrangement according to claim 5 wherein the memory means is a look-up table.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1998-06-26 | 1998-12-26 | 1999-06-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2002-06-26 | 2002-12-26 | 2003-06-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2006-06-26 | 2006-12-26 | 2007-06-27 | $7700.00 | Window Closed / Lapsed |