IP Library Granted Patent US 8,624,757
Granted Patent B2
US 8,624,757 · App. 13/169,676 · Granted Jan 7, 2014

Method for visually indicating an advisory from the traffic collision avoidance system on a flight display

Inventor: Andrew Thomas Schrauben (Lowell, MI)
Assignee: General Electric Company
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Quick Facts
Patent No.
US 8,624,757
App. No.
13/169,676
Granted
Jan 7, 2014
Kind
B2
Abstract

A method of visually indicating an advisory from a traffic collision avoidance system (TCAS) on a flight display of an aircraft, the method comprising receiving a TCAS advisory, determining a severity of the received TCAS advisory, displaying a geometric body on the flight display in response to the TCAS advisory, and altering a shape of the displayed geometric body in response to the determined severity wherein the shape of the displayed geometric body may be altered by altering at least one of an angle and an arc of the geometric body.

Claims (33)

1. A method of visually indicating an advisory from a traffic collision avoidance system (TCAS) on a flight display of an aircraft, the method comprising:

receiving a TCAS advisory;

determining a severity of the received TCAS advisory;

displaying a geometric body having a shape on the flight display in response to the TCAS advisory; and

reshaping the shape of the displayed geometric body in response to the determined severity

by altering at least one of an angle and an arc of the geometric body.

2. The method of claim 1 wherein the geometric body comprises a polygon and at least one angle of the polygon is altered as the determined severity increases.

3. The method of claim 2 wherein the polygon is a trapezoid having a cap and base connected by opposing sides.

4. The method of claim 3 wherein when the severity increases interior angles connecting the opposing sides to the cap are both increased to increase a width of the trapezoid.

5. The method of claim 3 wherein the trapezoid is displayed base-down when the TCAS advisory indicates a threat below a current flight path and base-up when the TCAS advisory indicates a threat above a current flight path.

6. The method of claim 3 wherein when the severity decreases interior angles connecting the opposing sides to the cap are both decreased to decrease a width of the trapezoid.

7. The method of claim 1 wherein the geometric body is altered when the TCAS advisory indicates a threat that is at least one of lateral and vertical to a current flight path.

8. The method of claim 1 wherein the geometric body is displayed on a flight display that is a primary flight display.

9. The method of claim 8 wherein the geometric body lies between an air speed indicator and an altitude indicator displayed on the primary flight display.

10. The method of claim 9 wherein no portion of the geometric body overlaps with either the air speed indicator and altitude indicator when the severity is low.

11. The method of claim 9 wherein at least a portion of the geometric body overlaps with at least a portion of either the air speed indicator and altitude indicator when the severity is high.

12. The method of claim 8 , further comprising a pitch ladder and wherein a portion of the geometric body underlies a portion of the pitch ladder.

13. The method of claim 1 , further comprising altering a fill style of the geometric body in response to the determined severity.

14. A method of visually indicating an advisory from a traffic collision avoidance system (TCAS) on a flight display of an aircraft, the method comprising:

receiving a TCAS advisory that indicates a threat that is at least one of lateral and vertical to a current flight path;

determining a severity of the received TCAS advisory; and

displaying a geometric body with a fill style on the flight display in response to the TCAS advisory;

wherein the fill style is set in response to the determined severity.

15. The method of claim 14 , wherein the fill style may be set as a non-uniform fill style in response to the determined severity.

16. The method of claim 15 wherein the non-uniform fill style includes at least one gradient transparencies, gradient colors, a varying pattern, and non-uniform lines.

17. The method of claim 14 wherein the geometric body with the fill style is displayed on a flight display that is a primary flight display.

18. A method of visually indicating an advisory from a traffic collision avoidance system (TCAS) on a flight display of an aircraft, the method comprising:

receiving a TCAS advisory;

determining a severity of the received TCAS advisory; and

displaying a geometric body with a fill style on the flight display in response to the TCAS advisory;

wherein the fill style is set as a non-uniform fill style in response to the determined severity in response to the determined severity.

19. The method of claim 18 wherein the non-uniform fill style includes at least one gradient transparencies, gradient colors, a varying pattern, and non-uniform lines.

20. The method of claim 18 wherein the TCAS advisory indicates a threat that is at least one of lateral and vertical to a current flight path.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 28, 2011
From: SCHRAUBEN, ANDREW THOMAS
To: GENERAL ELECTRIC COMPANY
Reel/Frame 026512/0350 →
Continuity (1)
Related Publication 20120326895A1 · Dec 27, 2012