METHODS AND SYSTEMS FOR MANAGEMENT OF AIRPLANE SPEED PROFILE

• US 20110118908A1
• Filed: 11/18/2009
• Published: 05/19/2011
• Est. Priority Date: 11/18/2009
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: GUNN, Peter D., BOORMAN, Daniel J., MUMAW, Randall J.
• Application Number:
  US12/621,298
• Publication Number:
  US 20110118908A1
• Time in Patent Office: Days
• US Class Current: 701/14
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00
• CPC Class Codes: Y02T 50/80 Energy efficient operational measures, e.g. ground operations or mission management

Abstract

Methods and systems for airplane speed profile management are disclosed. A method and system in accordance to one embodiment of the disclosure includes a graphical display of speed segments and constraints as well as controls for managing the speeds and associated constraints. Speed Profile Management System (SPMS) provides an integrated and interactive speed profile management tool where pilots can view, update, or change the speed profile of their airplane'"'"'s current or subsequent phases of flight.

Claims

1. An airplane system for managing a speed profile of an airplane, comprising:

a computer having instructions having contents that perform a method that includes;

displaying at a first display location, a first information identifying a phase of flight of the airplane, the first information comprising at least one of a takeoff phase of flight, a climb phase of flight, a cruise phase of flight, a descent phase of flight, an approach phase of flight, and a landing phase of flight;

displaying at a second display location, a second information graphically depicting the speed profile of the airplane, the second information comprising at least one of a phase of flight indicator, a speed segment indicator, a speed command change indicator, an altitude indicator, a configuration indicator, a waypoint, a speed constraint, and a speed restriction;

displaying at a third display location, a third information identifying a flight procedure influencing the speed profile of the airplane for a phase of flight; and

displaying at a fourth display location, a fourth information including an interactive input tool controlling the speed constraints and the speed restrictions displayed at the second display location; and

a display operatively coupled to the computer to display the first, second, third and fourth information at the first, second, third, and fourth display location, respectively.

2. An airplane comprising:

a speed profile management system, the speed profile management system providing a speed profile of an airplane for a phase of flight;

a flight management system operatively connected to the speed profile management system;

a cockpit graphics display system operatively connected to the speed profile management system;

an aircraft control system operatively connected to the speed profile management system;

a navigation system operatively connected to the speed profile management system;

a control input device operatively connected to the speed profile management system; and

a graphical display of the speed profile of the airplane displayed on the cockpit graphical display system, wherein the speed profile is interactively managed on the graphical display to affect the speed of the airplane.

3. The airplane of claim 2 further comprising a communication system operatively connected to the speed profile management system.

4. The airplane of claim 2 further comprising a surveillance system operatively connected to the speed profile management system.

5. The airplane of claim 2 wherein the speed profile further comprises a phase of flight indicator, a speed segment indicator, a speed command change indicator, an altitude indicator, a configuration indicator, a waypoint, a speed constraint, and a speed restriction.

6. The airplane of claim 2 wherein the speed profile is controlled by a section of a flight procedure.

7. The airplane of claim 2 wherein the speed profile is interactively managed by speed profile control input tool, further wherein the speed profile control input tool configures at least one of economic speed, pilot-selected speed, altitude-based speed restriction, and waypoint speed constraint.

8. The airplane of claim 2 wherein the cockpit graphical display system comprises at least one of a Primary Flight Display (PFD), a Head-up Display (HUD), a Navigation Display (ND), an Electronic Flight Bag (EFB) display, a Multi-Function Display (MFD), and Speed Profile Management System (SPMS) display.

9. The airplane of claim 2 wherein the control input device is at least one of a control panel, a keyboard, a cursor with a cursor control device, line select keys (LSK) on a control display unit, and a touchscreen, further wherein the control input device may be integrated into at least one of a Mode Control Panel (MCP), a control display unit (CDU), an Electronic Flight Bag, and Speed Profile Management System (SPMS) control panel.

10. The airplane of claim 2 wherein the speed profile of a phase of flight comprises at least one of at least one of a takeoff phase of flight, a climb phase of flight, a cruise phase of flight, a descent phase of flight, an approach phase of flight, and a landing phase of flight.

11. The airplane of claim 2 further comprising an Electronic Flight Bag (EFB) system.

12. A computer-implemented method of managing a speed of an airplane, comprising:

initiating the Speed Profile Management System;

receiving a first information, the first information comprises of a flight plan information defining a lateral and a vertical flight profile of the airplane wherein the flight profile of the airplane are further defined by an originating airport, a destination airport, and intermediate waypoints;

receiving a second information, the second information comprising of information from an off-board source, wherein the information containing instructions affecting the speed of the airplane for at least a portion of the flight;

receiving a third information, the third information comprising of an airplane state and an airplane intent information from an on-board source, wherein the airplane state and airplane intent information affecting the speed of the airplane for at least a portion of the flight;

responsive to pilot input, calculating the speed profile of the airplane based on the first, second, and third information;

displaying the speed profile on an integrated and interactive graphical display;

updating continuously the calculated speed profile and the speed profile graphical display; and

transmitting the calculated speed profile to the Aircraft Control System to affect the speed of the airplane.

13. The computer-implemented method of claim 12 wherein the flight plan information further comprises of a phase of flight information, wherein the phase of flight information comprises of at least one of a takeoff phase of flight, a climb phase of flight, a cruise phase of flight, a descent phase of flight, an approach phase of flight, and a landing phase of flight.

14. The computer-implemented method of claim 12 wherein the off-board source comprises at least one of an air traffic control authority, an airline authority, and a second airplane with which the airplane is coordinating a flight procedure.

15. The computer-implemented method of claim 12 wherein the on-board source comprises at least of a Cockpit Graphical Display System (CGDS), a Navigation System, and an Aircraft Control System, the Aircraft Control System further comprising at least one of an autopilot system, an autothrottle system, and a Mode Control Panel (MCP).

16. The computer-implemented method of claim 12 wherein the aircraft state information comprises of information controlling the speed of the aircraft at a first time and intent information comprises of target information controlling the speed of the aircraft at a second time, the second time being different from the first time.

17. The computer-implemented method of claim 12 wherein calculating the speed profile of the airplane comprises of processing received information to calculate speeds for different phases of flight and segments, adjusting the speed profile based on flight procedures, speed constraints, and speed restrictions, transforming the speed profile calculations for applicable display management, and arranging speed profile information by phase of flight, significant altitudes, waypoints, speed segments, and speed restrictions for interactive management by a pilot.

18. The computer-implemented method of claim 12 wherein displaying the speed profile further comprises displaying the speed profile for at least one phase of flight on a cockpit display, further wherein the cockpit display is at least one of a Primary Flight Display (PFD), a Head-up Display (HUD), a Navigation Display (ND), an Electronic Flight Bag (EFB) display, a Multi-Function Display (MFD), and Speed Profile Management System (SPMS) display.

19. The computer-implemented method of claim 12 wherein initiating the SPMS comprises at least on of initiating the SPMS via a control input device and initiating the SPMS via a Flight Management System.

20. The computer-implemented method of claim 12 wherein transmitting the speed profile to the Aircraft Control System to affect the speed of the airplane, further comprises of commanding the Aircraft Control System to change the speed of the airplane to match the calculated speed profile of the SPMS.

21. A method of operating an airplane, the airplane having a real time graphical display, the display instantaneously displaying images reflecting commanded changes to the operating flight profile, the method comprising:

collecting airplane flight operating parameters in real time to create a real time airplane flight operating parameters information;

supplying the real time airplane flight operating parameter information to a cockpit graphical display and a speed profile management system;

displaying airplane flight operating parameters in real time on the cockpit graphical display;

processing an airplane speed profile command in the speed profile management system;

generating a speed profile of the command prior to the airplane operation reflecting such speed;

supplying commanded speed profile information to the cockpit graphical display from the speed profile management system; and

displaying instantaneously graphical images reflecting the airplane speed profile prior to the airplane operation reflecting such change.

22. The method of claim 21 further comprising validating the airplane speed profile command in the speed profile management system.

23. The method of claim 21 further comprising enabling a pilot viewing of the graphical display of the commanded speed profile change to validate the commanded speed profile change.

24. The method of claim 21 further comprising enabling a pilot viewing the graphical display of the commanded speed profile change to change the commanded speed profile.

25. The method of claim 21 further comprising:

collecting airplane operating speed profile information in the speed profile management system;

supplying the airplane operating speed profile information to the graphical display from the speed profile management system;

displaying the actual speed profile of the airplane in the graphical display.

26. The method of claim 21 further comprising validating the speed profile by comparing the displayed actual performance with the projected performance after the change.

27. The method of claim 21 further comprising changing the speed profile by comparing the displayed actual performance with the projected performance after the change.