# US 10,311,738 B2 · Display system and method for indicating a time-based requirement

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- Number: US 10,311,738 B2
- Document ID: US10311738B2
- Status: Granted
- Kind: B2
- Application number: 15/588,944
- Filed: 2017-05-08
- Published: 2018-11-08
- Granted: 2019-06-04
- Earliest claimed: 2017-05-08
- Assignees: Honeywell International Inc.
- Applicants: Honeywell International Inc.
- Inventors: Sachin Pratap; Jagadeesh Shankar; Visvanathan Thanigai Nathan; Mohammed Ibrahim Mohideen; Shobana Arumugam
- Web page: https://patentgrep.com/patent/US10311738B2

## CPC

- G08G 5/21: located onboard the aircraft
- B64D 43/00: Arrangements or adaptations of instruments
- G01C 23/00: Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
- G06F 3/04845: for image manipulation, e.g. dragging, rotation, expansion or change of colour
- G06F 3/04847: Interaction techniques to control parameter settings, e.g. interaction with sliders or dials
- G08G 5/26: Transmission of traffic-related information between aircraft and ground stations
- G08G 5/50: Navigation or guidance aids
- G08G 5/53: for cruising
- G08G 5/55: for a single aircraft
- G08G 5/723: {from the aircraft}
- G08G 5/76: for monitoring atmospheric conditions
- G08G: TRAFFIC CONTROL SYSTEMS (guiding railway traffic, ensuring the safety of railway traffic B61L; arrangement of road signs or traffic signals E01F9/00; radar or analogous systems, sonar systems, lidar systems specially adapted for traffic control G01S13/91, G01S15/88, G01S17/88; {radar or analogous systems, sonar systems, lidar systems specially adapted for anti-collision purposes G01S13/93, G01S15/93, G01S17/93})
- B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- G01C: MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY (measuring liquid level G01F; radio navigation, determining distance or velocity by use of propagation effects, e.g. Doppler effects, propagation time, of radio waves, analogous arrangements using other waves G01S)
- G06F: ELECTRIC DIGITAL DATA PROCESSING (computer systems based on specific computational models G06N)

## Abstract

A display system is configured to provide a display to an aircraft flight crew. The system includes an image display device, a data storage device, a flight management system, a processing unit in operable electronic communication with the image display device, the data storage device, and the flight management system. The processing unit includes a computer processor that is configured to receive a time-based requirement to a point of interest associated with operation of the aircraft. Via the image display device, a flight display includes a graphically depicted time tape. The time tape includes a time scale. Also graphically depicted within the time tape is the point of interest using a first symbology and the time-based requirement using a second symbology. Operational parameter data of the aircraft allows determination of the ability of the aircraft to achieve the time-based requirement and graphical depiction within the time tape of the ability of the aircraft to achieve the time-based requirement using a third symbology.

## Claims

### Claim 1

A display system configured to provide a display to a flight crew of an aircraft comprising:
an image display device;
a data storage device;
a flight management system; and
a processing unit in operable electronic communication with the image display device, the data storage device, and the flight management system, wherein the processing unit comprises a computer processor that is configured to:
receive a time-based requirement to a point of interest associated with operation of the aircraft;
provide via the image display device a flight display including a graphically depicted time tape, wherein the time tape comprises a time scale;
graphically depict within the time tape the point of interest using a first symbology;
graphically depict within the time tape the time-based requirement using a second symbology, different than the first symbology;
query the flight management system to obtain therefrom operational parameter data of the aircraft,
determine an ability of the aircraft to achieve the time-based requirement based upon the operational parameter data; and
in a first mode of operation to graphically depict within the time tape the ability of the aircraft to achieve the time-based requirement using a third symbology, different than the first symbology and second symbology; and
in a second mode of operation to graphically depict within the time tape an indicator of progress of the aircraft to the time-based requirement using the third symbology, wherein the mode of operation is selected by the processing unit based upon the time-based requirement.

### Claim 2 (depends on 1)

The display system of claim 1, wherein the first symbology is a first color and the second symbology is a second color that differs from the first color.

### Claim 3 (depends on 2)

The display system of claim 2, wherein the first symbology is a first color and the third symbology is a third color that differs from the second color.

### Claim 4 (depends on 1)

The display system of claim 1, wherein the first symbology is a first shape and the second symbology is a second shape that differs from the first shape.

### Claim 5 (depends on 4)

The display system of claim 4, wherein the first symbology is a first shape and the third symbology is a third shape that differs from the second shape.

### Claim 6 (depends on 1)

The display of claim 1, wherein one of the first symbology and the second symbology is an alpha-numeric symbol.

### Claim 7 (depends on 1)

The display of claim 1, wherein one of the first symbology and the second symbology is an alpha-numeric symbol, and the third symbology is a shape.

### Claim 8 (depends on 1)

The display system of claim 1, wherein one of the first symbology and the second symbology is an alpha-numeric symbol, and the third symbology is a color.

### Claim 9 (depends on 1)

The display of claim 1, wherein the point of interest comprises a required time of arrival requirement (RTA), a waypoint requirement (WPT), a mission point requirement (MPT), an arrival point requirement (APT), a reporting point requirement (RPT), a fueling point in air (FPT) or a reporting altitude requirement (ALT).

### Claim 10

A method for providing a display to a flight crew of an aircraft comprising:
receiving a time-based requirement to a point of interest associated with operation of the aircraft;
providing a flight display including a graphically depicted time tape, wherein the time tape comprises a time scale;
graphically depicting within the time tape the point of interest using a first symbology;
graphically depicting within the time tape the time-based requirement using a second symbology, different than the first symbology;
receiving operational parameter data of the aircraft;
determining an ability of the aircraft to achieve the time-based requirement based upon the operational parameter data; and
in a first mode of operation graphically depicting within the time tape the ability of the aircraft to achieve the time-based requirement using a third symbology, different than the first symbology and second symbology; and in a second mode of operation to graphically depict within the time an indicator of progress of the aircraft to the time-based requirement using the third symbology, wherein the mode of operation is selected by the processing unit based upon the time-based requirement.

### Claim 11 (depends on 10)

The method of claim 10, wherein the first symbology is a first color and the second symbology is a second color that differs from the first color.

### Claim 12 (depends on 11)

The method of claim 11, wherein the first symbology is a first color and the third symbology is a third color that differs from the second color.

### Claim 13 (depends on 10)

The method of claim 10, wherein the first symbology is a first shape and the second symbology is a second shape that differs from the first shape.

### Claim 14 (depends on 13)

The method of claim 13, wherein the first symbology is a first shape and the third symbology is a third shape that differs from the second shape.

### Claim 15 (depends on 10)

The method of claim 10, wherein one of the first symbology and the second symbology is an alpha-numeric symbol.

### Claim 16 (depends on 10)

The method of claim 10, wherein one of the first symbology and the second symbology is an alpha-numeric symbol, and the third symbology is a shape.

### Claim 17 (depends on 10)

The method of claim 10, wherein one of the first symbology and the second symbology is an alpha-numeric symbol, and the third symbology is a color.

### Claim 18 (depends on 10)

The method of claim 10, wherein the point of interest comprises a required time of arrival requirement (RTA), a waypoint requirement (WPT), a mission point requirement (MPT), an arrival point requirement (APT), a reporting point requirement (RPT), a fueling point in air (FPT) or a reporting altitude requirement (ALT).
