IP Library › Granted Patent US 10,330,493
Granted Patent B2
US 10,330,493 · App. 14/559,755 · Granted Jun 25, 2019

Systems and methods for displaying position sensitive datalink messages on avionics displays

Inventors: Raghu Shamasundar (Karnataka, IN); Prasad Rao Piradi (Karnataka, IN); Thomas D. Judd (Woodinville, WA); David Pepitone (Suny City West, AZ); Abhishek Gupta (Karnataka, IN); Adib Bouanani (Laveen, AZ); Prashanth Ramanna (Karnataka, IN)
Assignee: Honeywell International Inc.
G01C23/005G06F3/0481
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Quick Facts
Patent No.
US 10,330,493
App. No.
14/559,755
Granted
Jun 25, 2019
Kind
B2
Abstract

Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.

Claims (33)

1. An instrument display system for an aircraft, the system comprising:

a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path;

wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path, wherein the flight plan display screen locates the at least one symbol at a position that indicates a point of applicability along the aircraft's planned flight path for a received uplink datalink message;

wherein the received uplink datalink message includes a conditional clearance request; and

wherein the at least one symbol on the flight plan display screen indicates a margin until a condition specified by the conditional clearance request is met based on current aircraft conditions.

2. The system of claim 1 , wherein the at least one symbol is positioned along the aircraft's planned flight path at a waypoint specified in the received uplink datalink message.

3. The system of claim 1 , wherein the system further includes a human-machine interface;

wherein when a user selects the at least one symbol on the flight plan display screen using the human-machine interface, the flight plan display screen displays contents of the uplink datalink message with one or more applicable action buttons.

4. The system of claim 1 , wherein the point of applicability for the received uplink datalink message is derived from contents of the received uplink datalink message.

5. The system of claim 1 , wherein the point of applicability for the received uplink datalink message is selectable by a pilot.

6. The system of claim 1 , wherein the system further includes a human-machine interface;

wherein when a user selects the at least one symbol on the flight plan display screen using the human-machine interface, the flight plan display screen displays an action specified by the conditional clearance request.

7. The system of claim 1 , wherein the at least one symbol on the flight plan display screen indicates a position where the condition specified by the conditional clearance request is predicted to become satisfied.

8. The system of claim 7 , wherein the at least one symbol further includes an action alert when the aircraft comes within a predefined threshold of satisfying the condition, wherein the action alert displays the action specified by the conditional clearance request.

9. The system of claim 1 , wherein the margin is expressed as a time margin, a distance margin, or an altitude margin.

10. The system of claim 1 , wherein the at least one symbol further includes one or both of a vertical error symbol and a lateral error symbol;

wherein the vertical error symbol and the lateral error symbol indicate a tolerance for satisfying the condition when the aircraft has deviated from the aircraft's planned flight path.

11. The system of claim 1 , wherein the flight plan display screen is implemented in one of either:

on-board aircraft avionics; or

an air traffic control center.

12. A method for contextual displaying uplink messages on a flight plan display screen, the method comprising:

receiving an uplink datalink message;

associating the uplink datalink message with a point of applicability along a planned flight path;

displaying a representation of the planned flight path on the flight plan display screen; and

positioning a symbol on the flight plan display screen along the representation of the planned flight path at a position indicating the point of applicability;

wherein the received uplink datalink message includes a conditional clearance request; and

wherein the at least one symbol on the flight plan display screen indicates a margin until a condition specified by the conditional clearance request is met based on current aircraft conditions.

13. The method of claim 12 , further comprising:

displaying additional contents of the uplink datalink message on the flight plan display screen when the symbol is selected using a human-machine interface.

14. The method of claim 12 , wherein the symbol indicates a position where a condition specified by the conditional clearance request is predicted to become satisfied.

15. The method of claim 12 , wherein the symbol on the flight plan display screen further includes an action alert when the aircraft comes within a predefined threshold of satisfying the condition, wherein the action alert displays an action specified by the conditional clearance request.

16. The method of claim 12 , wherein the symbol on the flight plan display screen further includes one or both of a vertical error symbol and a lateral error symbol;

wherein the vertical error symbol and the lateral error symbol indicate a tolerance for satisfying the condition when the aircraft has deviated from the aircraft's planned flight path.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 24, 2019
From: PIRADI, PRASAD RAO
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 049278/0049 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 3, 2014
From: SHAMASUNDAR, RAGHU; PIRADI, PRASADRAO RAO; JUDD, THOMAS D.; PEPITONE, DAVID; GUPTA, ABHISHEK; BOUANANI, ADIB; RAMANNA, PRASHANTH
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 034364/0691 →
Continuity (1)
Related Publication 20160161283A1 · Jun 9, 2016