Aircraft display devices

• US 4,626,851 A
• Filed: 11/07/1984
• Issued: 12/02/1986
• Est. Priority Date: 11/09/1983
• Status: Expired due to Fees

• Current Assignee: GEC Avionics Ltd (Cornhill Corp. Holdings LLP)
• Original Assignee: GEC Avionics Ltd (Cornhill Corp. Holdings LLP)
• Inventors: Tooze, Michael J.
• Primary Examiner(s): Rowland, James L.
• Assistant Examiner(s): Swarthout, Brent A.
• Application Number:
  US06/669,318
• Time in Patent Office: 755 Days
• Field of Search: 73/178 R, 33/328, 340/967, 340/974, 340/975, 340/705, 340/784, 340/971, 340/973, 358/104, 364/434, 434/51, 244/1 R
• US Class Current: 340/975
• CPC Class Codes: G01C 19/32 Indicating or recording means specially adapted for rotary gyroscopes
• CPC Class Codes: G09G 3/001 using specific devices not provided for in groups G09G3/02 - G09G3/36, e.g. using an intermediate record carrier such as a film slide; Projection systems; Display of non-alphanumerical information, solely or in combination with alphanumerical information, e.g. digital display on projected diapositive as background slide projectors per se G03B23/00 = 42 HP

Abstract

An aircraft attitude display device comprising: a circular array of radially extending selectively activatable display elements (5), the radially inner ends of which constitute a boundary defining a central space; within the said central space, a fixed aircraft symbol (7); and means for selectively activating the said display elements in accordance with aircraft attitude so that the selected display elements form a visible pattern, e.g. a sector of the array, bearing a geometrical relationship with respect to the aircraft symbol indicative of the aircraft attitude.

The device is suitable for implementation using liquid crystal display technology to give a stand-by display of aircraft pitch and roll which is readily understandable by pilots since it is similar to the display given by conventional rolling ball action aircraft attitude instruments.

Claims

1. A display device for an aircraft comprising:

a circular array of radially extending selectively activatable display elements, the radially inner ends of which elements define a central space;

within the said central space, a symbol fixed with respect to the aircraft in use; and

means for selectively activating said display elements in accordance with aircraft attitude whereby the selected display elements form a visible pattern whose geometrical relationship with respect to said symbol is indicative of the aircraft attitude; and

wherein said means for selectively activating said display elements activates a group of said elements which together form a sector of said circular array whose angular position in the array relative to said symbol is indicative of the roll angle of the aircraft; and

said sector becomes progressively a larger angle sector as the aircraft pitch angle increases from zero in one direction and a smaller angle sector as the aircraft pitch angle increases from zero in the opposite direction.

2. A device according to claim 1 wherein said sector rotates about said symbol with change in the roll angle of the aircraft by an angle substantially equal to the change in the roll angle.

3. A device according to claim 2 wherein said sector is a 180°

angle sector when the aircraft pitch angle is zero and becomes a larger angle sector as the aircraft pitch angle increases from zero in the negative direction and becomes a smaller angle sector as the aircraft pitch angle increases from zero in the positive direction.

4. A device according to claim 2 wherein at least one element in the middle part of said sector is not activated for normal attitudes of the aircraft.

5. A device according to claim 1 wherein said angular position of said sector and the angle of said sector change with roll and pitch angle respectively of the aircraft by larger amounts when the aircraft attitude is approximately straight and level than for other aircraft attitudes.

6. A device according to claim 1 wherein said display elements are liquid crystal display elements.

7. A device according to claim 1 further including angle reference display elements at fixed positions around said circular array of display elements.

8. A device according to claim 1 wherein said means for selectively activating said display elements comprises a microprocessor.