Aircraft display combining error tape and reference bugs

• US 5,797,562 A
• Filed: 07/26/1995
• Issued: 08/25/1998
• Est. Priority Date: 07/26/1995
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Wyatt, Ivan Sandy
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US08/506,743
• Time in Patent Office: 1,126 Days
• Field of Search: 244/1 R, 340/971-980, 342/29, 342/33
• US Class Current: 244/1.00R
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32

Abstract

An aircraft display combines speed error tapes and multiple speed reference bugs to produce a display which reduces pilot workload. The length of the speed error tape is indicative of the difference between a current aircraft speed and a reference speed. Multiple reference bugs are adjacent to the error tape and are indicative of the difference between the current aircraft speed and other selected reference speeds. The reference bugs move along the error tape thereby communicating the status of the current aircraft speed relative to the multiple reference speeds. The display reduces the need for the pilot to scan and analyze numerous instruments for the same information.

Claims

1. A display apparatus for an aircraft comprising:

a) an electronic display unit having,

1) a display screen,

2) a flight path vector symbol displayed on said screen,

3) a speed error tape displayed on said screen, said tape having a first end and a second end, said first end adjacent said flight path vector symbol, said tape extending from said symbol to said second end,

4) at least one speed bug positioned adjacent to said tape, each of said bugs representative of an associated reference speed, and,

5) whereas the position of said speed bug relative to said first end of said tape is indicative of the difference between a current speed of said aircraft and said associated reference speed and once the associated reference speed is achieved said bug vanishes.

2. The display apparatus according to claim 1 wherein said electronic display unit is a HUD.

3. The display apparatus according to claim 1 wherein said electronic display unit is a CRT.

4. The display apparatus according to claim 1 wherein said electronic display unit is an LCD.

5. The display apparatus according to claim 1 wherein said flight path vector symbol includes a wing from which said tape extends.

6. The display apparatus according to claim 1 wherein said at least one speed bug includes at least one speed bug representative of a takeoff reference speed.

7. The display apparatus according to claim 6 wherein said at least one speed bug includes a V1 speed bug representative of a v1 speed of said aircraft.

8. The display apparatus according to claim 6 wherein said at least one speed bug includes a V2 speed bug representative of a v2 speed of said aircraft.

9. The display apparatus according to claim 6 wherein said at least one speed bug includes a VR speed bug representative of a VR speed of said aircraft.

10. The display apparatus according to claim 1 wherein the length of said error tape is representative of the difference between said current speed and a predetermined selected reference speed.

11. An information display device for vehicles comprising:

a) electronic display means for displaying information to an operator, said display means having;

1) a display screen;

b) an error tape displayed by said display means on said display screen, the length of said tape being variable and representative of a difference between a current vehicle parameter and a primary reference value; and

,

c) at least one reference bug displayed on said display screen, said bugs positioned adjacent said tape, said bugs being moveable along the length of said tape, the position of each of said bugs along said tape indicative of a difference between said current aircraft parameter and a secondary reference parameter associated with each of said bugs and once the reference parameter is achieved said at least one reference bug vanishes.

12. An information display device for vehicles according to claim 11 further comprising a flight path vector symbol displayed on said display screen, said error tape emanating from said flight path vector symbol.

13. An information display device for vehicles according to claim 12 wherein said current vehicle parameter is velocity.

14. An information display device for vehicles according to claim 13 wherein said vehicle is an aircraft and reference bugs are representative of V-speeds of said aircraft.

15. An information display device for vehicles according to claim 14 wherein said vehicle is an aircraft and reference bugs include a V1 reference bug representative of a v1 speed of said aircraft.

16. An information display device for vehicles according to claim 14 wherein said vehicle is an aircraft and reference bugs include a VR reference bug representative of a VR speed of said aircraft.

17. An information display device for vehicles according to claim 14 wherein said vehicle is an aircraft and reference bugs include a v2 reference bug representative of a v2 speed of said aircraft.

18. An information display device for vehicles according to claim 14 wherein said electronic display means is a HUD.

19. An information display device for vehicles according to claim 14 wherein said electronic display means is a LCD.

20. An information display device for vehicles according to claim 14 wherein said electronic display means is a CRT.

21. A vehicle comprising:

a) a frame;

b) an engine support by said frame; and

,

c) an electronic display supported by said frame, said display having,

1) a display screen,

2) a flight path vector symbol displayed on said screen,

3) a speed error tape displayed on said screen, said tape having a first end and a second end, said first end adjacent said flight path vector symbol, said tape extending from said symbol to said second end,

4) at least one speed bug positioned adjacent to said tape, each of said bugs representative of an associated reference speed, and,

5) whereas the position of said speed bug relative to said first end of said tape is indicative of the difference between a current speed of said aircraft and said associated reference speed and once the associated reference speed is achieved said bug vanishes.