Cockpit display systems and methods for generating cockpit displays including enhanced flight visibility indicators

Patent metadata

Field	Value
Publication number	US-9936191-B2
Application number	US-201615007673-A
Country	US
Kind code	B2
Filing date	Jan 27, 2016
Priority date	Jan 27, 2016
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

Cockpit display systems and methods are provided for generating cockpit displays including symbology useful in assessing whether enhanced flight visibility requirements are satisfied during approach and landing. In one embodiment, the cockpit display system includes an Enhanced Flight Vision System (EFVS) sensor configured to monitor a region forward of the aircraft for runway reference features, a cockpit display device on which an EFVS image is generated utilizing EFVS sensor data, and a controller coupled to the EFVS sensor and to the display device. The controller determines an enhanced flight visibility requirement for a runway approached by the aircraft, and then visually indicates on the EFVS image whether the enhanced flight visibility requirement is currently satisfied by, for example. generating an enhanced flight visibility indicator (EFVI) graphic on the EFVS image visually identifying a ground location beyond which the appearance of a runway reference feature satisfies the enhanced flight visibility requirement.

First claim

What is claimed is:

1. A cockpit display system for deployment onboard an aircraft, the cockpit display system comprising:
an Enhanced Flight Vision System (EFVS) sensor configured to monitor a region forward of the aircraft for runway reference features;
a cockpit display device on which an EFVS image is generated utilizing data received from the EFVS sensor; and
a controller operably coupled to the EFVS sensor and to the cockpit display device, the controller configured to:
determine an enhanced flight visibility requirement for a runway approached by the aircraft for landing; and
visually indicate on the EFVS image whether the enhanced flight visibility requirement is currently satisfied for the runway approach by the aircraft.

2. The cockpit display system of claim 1 wherein, in visually indicating on the EFVS image whether the enhanced flight visibility requirement is currently satisfied for the runway approach by the aircraft, the controller is configured to generate an enhanced flight visibility indicator (EFVI) graphic on the EFVS image indicative of the enhanced flight visibility requirement.

3. The cockpit display system of claim 2 wherein the controller is configured to generate the EFVI graphic as a flight visibility marker, which visually identifies a ground location beyond which the appearance of a runway reference feature on the EFVS image satisfies the enhanced flight visibility requirement.

4. The cockpit display system of claim 3 further comprising one or more data sources coupled to the controller and configured to supply thereto data indicative of a current aircraft height above a threshold region of the runway, the controller configured to determine the ground location based at least in part on the enhanced flight visibility requirement and the current aircraft height above the threshold region of the runway.

5. The cockpit display system of claim 3 wherein the controller is configured to generate the flight visibility marker to have a central window through which graphics representative of runway approach lights can be seen when the aircraft is aligned parallel to and approaches the runway for landing.

6. The cockpit displays system of claim 3 wherein the controller is configured to generate the flight visibility marker as one or more arcs included in a larger, non-displayed ring centered on a current position of the aircraft.

7. The cockpit display system of claim 2 further comprising an altimeter indicating the current altitude of the aircraft, the controller coupled to the altimeter and further configured to:
establish a decision altitude for the runway approached by the aircraft for landing; and
alter the appearance of the EFVI graphic based, at least in part, on a current altitude of the aircraft relative to the established decision altitude.

8. The cockpit display system of claim 2 further comprising an altimeter indicating the current altitude of the aircraft, the controller coupled to the altimeter and further configured to:
determine whether any approach lights are detected by the EFVS sensor beyond the EFVI graphic, as considered from the vantage point of the aircraft;
establish a decision altitude for the runway approached by the aircraft for landing; and
generate a visual warning on the cockpit display device if determining that: (i) the aircraft has descended below or is within a threshold distance of the decision altitude, and (ii) no approach lights are detected by the forward-looking sensor beyond the flight visibility marker.

9. The cockpit display system of claim 1 further comprising a memory coupled to the controller and storing a database, the controller configured to determine the enhanced flight visibility requirement by recalling data from the database specifying the enhanced flight visibility requirement for the runway.

10. The cockpit display system of claim 9 wherein the data comprises a runway visibility requirement value or a status miles value included in an approach chart corresponding to the runway and stored in the database.

11. The cockpit display system of claim 1 further comprising a pilot interface coupled to the controller, the controller configured to determine the enhanced flight visibility requirement from pilot input data received via the pilot interface.

12. The cockpit display system of claim 1 further comprising a datalink coupled to the controller, the controller configured to determine the enhanced flight visibility requirement based, at least in part, on data received from a remote source over the datalink.

13. The cockpit display system of claim 1 wherein the controller is configured to combine the EFVS image with a Synthetic Vision System image to yield a Combined Vision Primary Flight Display generated on the cockpit display device.

14. The cockpit display system of claim 1 wherein the controller is further configured to:
determine whether the enhanced flight visibility requirement is currently satisfied for the runway approach by the aircraft based, at least in part, on the enhanced flight visibility requirement and a current position of the aircraft relative to the runway; and
generate the one or more graphics on the EFVS image indicative of whether the enhanced flight visibility requirement is currently satisfied for the runway approach by the aircraft.

15. The cockpit display system of claim 1 wherein, in generating the one or more graphics on the EFVS image, the controller generates the one or more graphics to comprise a text annunciation indicating whether the enhanced flight visibility requirement is currently satisfied for the runway approach by the aircraft.

16. A cockpit display system for deployment onboard an aircraft, the cockpit display system comprising:
a forward-looking sensor configured to monitor a region forward of the aircraft for runway approach lights;
a cockpit display device on which a three dimensional cockpit display is generated utilizing data received from the forward-looking sensor; and
a controller operably coupled to the forward-looking sensor and to the cockpit display device, the controller configured to:
determine an enhanced flight visibility requirement for a runway approached by the aircraft for landing; and
generate on the three dimensional cockpit display (i) approach light graphics representative of runway approach lights detected by the forward-looking sensor and (ii) a marker visually identifying a ground location beyond which the appearance of an approach light graphic satisfies the enhanced flight visibility requirement.

17. The cockpit display system of claim 16 further comprising one or more data sources coupled to the controller and configured to supply thereto data indicative of a current aircraft height above a threshold region of the runway, the controller configured to determine the ground location based at least in part on the enhanced flight visibility requirement and the current aircraft height above the threshold region of the runway.

18. The cockpit display system of claim 16 wherein the controller is configured to determine the enhanced flight visibility requirement based on one or more of the group consisting of a published enhanced flight visibility requirement stored in memory, pilot input, and data wirelessly received from Air Traffic Control.

19. A method carried-out by a cockpit display system onboard an aircraft, the cockpit display system including a cockpit display device, an Enhanced Flight Vision System (EFVS) sensor configured to monitor a region forward of the aircraft

Assignees

• Honeywell Int Inc

Inventors

• Wyatt Ivan Sandy
• Tunheim David Allen
• He Gang

Classifications

• H04N13/302 Primary

  for viewing without the aid of special glasses, i.e. using autostereoscopic displays · CPC title

• G06F1/163

  Wearable computers, e.g. on a belt · CPC title

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title

• G06T15/005

  General purpose rendering architectures · CPC title

• H04N13/0402 Primary

  Electricity · mapped topic