Display device with multiple retractable flat screens

• US 4,988,995 A
• Filed: 06/07/1988
• Issued: 01/29/1991
• Est. Priority Date: 06/12/1987
• Status: Expired due to Fees

• Current Assignee: Thomson-CSF
• Original Assignee: Thomson-CSF
• Inventors: Soubrier, Jean-Marie, Buisson, Jean-Michel
• Primary Examiner(s): Orsino, Jospeh A.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/203,159
• Time in Patent Office: 966 Days
• Field of Search: 340/971, 340/973, 340/974, 340/975, 340/980, 340/705, 340/717, 340/713, 340/764, 340/765, 340/700, 340/425.5, 362/62, 40/446, 40/448, 40/452, 40/456, 40/463, 40/564, 40/572, 40/574, 40/577, 40/473, 116/46, 116/51, 116/52, 116/54
• US Class Current: 340/971
• CPC Class Codes: B60Q 3/10 for dashboards
• CPC Class Codes: G09F 9/00 Indicating arrangements for variable information in which the information is built-up on a support by selection or combination of individual elements in which the variable information is permanently attached to a movable support G09F11/00; abacus G06C1/00; slide-rules G06G1/00

Abstract

The display device of the invention includes several flat screens. Two sides of a case each form a flat screen display face controlled by the same control system. Under normal operation, the case is held in slides and only the screen disposed on one side is visible and in the emergency mode the case is pulled out of the slides and is pivoted so as to cause the other screen disposed on the othr side to appear.

Claims

1. A device for displaying information to an operator of an aircraft, said information contained in digital display signals output from an external processor, comprising:

a parallelepipedic shaped case having four sides;

means for fixing and pivotally mounting said case to present one of two display sides of said case to said operator;

first electronic display means for displaying a first plurality of aircraft information on said first display side of said case;

second electronic display means for displaying said first plurality of information and a second plurality of information on said second display side of said case;

means for inputting said digital display signals from said external processor; and

means for switching said input digital display signals to one of said first electronic display means and second electronic display means, said switching means also outputting a switching signal to said external processor so that digital display signals corresponding to one of said first plurality of information and said combined first and second plurality of information are output by said processor, depending on the position of said switching means.

2. A device according to claim 1 wherein each of said first and second electronic display means include a decoder circuit.

3. A device according to claim 1 wherein said switching means is automatically actuated following the occurrence of a particular predetermined event.

4. A device according to claim 3 wherein said predetermined event is a failure of said first electronic display means.

5. A device according to claim 1 wherein said switching means is manually actuated by the operator.

6. A device according to claim 1 wherein said first and second plurality of information together contain information necessary for said operator to pilot said aircraft.