High lift control method and system for aircraft

Patent metadata

Field	Value
Publication number	US-9821902-B2
Application number	US-201414771974-A
Country	US
Kind code	B2
Filing date	Feb 26, 2014
Priority date	Mar 6, 2013
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

A high lift control system for an aircraft having at least one high lift surface includes a selector having a predetermined number of discrete positions, at least one of the predetermined positions corresponding to different positions of the at least one high lift surface.

First claim

What is claimed is:

1. A high lift control system for an aircraft having one or more high lift surfaces including one or more of the following: one or more slats disposed on a leading edge of a wing of the aircraft and one or more flaps disposed on a trailing edge of the wing of the aircraft, the high lift control system comprising:
a high lift selector movable between a number of predetermined discrete positions, one of the predetermined discrete positions of the selector being associated with a first high lift configuration for a first flight phase of the aircraft and also with a different second high lift configuration for a second flight phase of the aircraft; and
a computer configured to, based on one or more signals from one or more aircraft systems, command the one or more high lift surfaces according to either the first high lift configuration or the second high lift configuration when the selector is moved to the one of the predetermined discrete positions.

2. The high lift control system of claim 1 , wherein the first high lift configuration and the second high lift configuration correspond to different positions of at least one slat.

3. The high lift control system of claim 1 , wherein the first high lift configuration and the second high lift configuration correspond to different positions of at least one flap.

4. The high lift control system of claim 1 , wherein the first high lift configuration and the second high lift configuration correspond to different positions of at least one slat and of at least one flap.

5. The high lift control system of claim 1 , wherein the one or more signals are indicative of a direction of movement of the selector for arriving to the one of the predetermined discrete positions.

6. The high lift control system of claim 1 , wherein the one or more signals are indicative of whether the aircraft is on the ground or in flight.

7. A high lift control system for an aircraft having at least one high lift surface, the high lift control system comprising:
a high lift selector that is movable in:
a first direction of movement from an in-flight cruise position to land the aircraft; and
a second direction of movement from an on-the-ground position toward the in-flight cruise position to have the aircraft take-off,
the selector having a plurality of discrete positions, at least one of the plurality of discrete positions of the selector being one in which the at least one high lift surface has a corresponding different position for each of the first direction of movement and the second direction of movement of the selector for arriving to the at least one discrete position.

8. The high lift control system of claim 7 , comprising a computer configured to determine which corresponding different position of the at least one high lift surface is to be selected based on an operating condition of the aircraft.

9. The high lift control system of claim 8 , wherein the operating condition comprises an aircraft on ground condition or an aircraft in flight condition.

10. The high lift control system of claim 7 , comprising a computer configured to determine which corresponding different position of the at least one high lift surface is to be selected based on the first direction of movement of the selector or on the second direction of movement of the selector.

11. The high lift control system of claim 7 , comprising a computer configured to determine which corresponding different position of the at least one high lift surface is to be selected based on an aircraft speed.

12. The high lift control system of claim 7 , wherein the selector comprises one of a lever, a knob, a graphical representation of a lever on a touchscreen and a graphical representation of a knob on a touchscreen.

13. A method for controlling a position of at least one high lift surface on an aircraft, the method comprising the steps of:
determining a discrete position of a selector having a number of predetermined discrete positions, at least one of the predetermined discrete positions of the selector corresponding to at least two different positions of the at least one high lift surface;
determining if the determined discrete position of the selector corresponds to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface;
if the determined discrete position of the selector corresponds to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface, then controlling the position of the at least one high lift surface based on a parameter of the aircraft; and
if the determined discrete position of the selector does not correspond to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface, then controlling the position of the at least one high lift surface based on the determined position of the selector.

14. The method of claim 13 , wherein the parameter of the aircraft comprises an operating condition of the aircraft.

15. The method of claim 14 , wherein the operating condition of the aircraft comprises one of the aircraft being on the ground or in-flight.

16. The method of claim 13 , wherein the parameter of the aircraft comprises a direction of movement of the selector for arriving to the determined discrete position.

17. The method of claim 13 , wherein the parameter of the aircraft comprises a speed of the aircraft.

18. A computer program product for controlling a position of at least one high lift surface on an aircraft, the computer program product comprising a computer readable storage medium having program code embodied therewith, the program code readable/executable by a computer, processor or logic circuit to perform a method comprising the steps of:
determining a discrete position of a selector having a number of predetermined discrete positions, at least one of the predetermined discrete positions of the selector corresponding to at least two different positions of the at least one high lift surface;
determining if the determined discrete position of the selector corresponds to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface;
if the determined discrete position of the selector corresponds to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface, then controlling the position of the at least one high lift surface based on a parameter of the aircraft; and
if the determined discrete position of the selector does not correspond to the at least one of the predetermined discrete positions of the selector that corresponds to at least two different positions of the at least one high lift surface, then controlling the position of the at least one high lift surface based on the determined position of the selector.

19. The computer program product of claim 18 , wherein the parameter of the aircraft comprises an operating condition of the aircraft.

20. The computer program product of claim 19 , wherein the operating condition of the aircraft comprises one of the aircraft being on the ground or in-flight.

21. The computer program product of claim 18 , wherein the parameter o

Assignees

• Bombardier Inc

Inventors

• Young Robert
• Grenier Yves
• Sadek Hany

Classifications

• B64C13/0421

  control sticks for primary flight controls · CPC title

• B64C9/28

  by flaps at both the front and rear of the wing operating in unison · CPC title

• B64D2045/001

  for indicating symmetry of flaps deflection · CPC title

• B64C13/0425 Primary

  for actuating trailing or leading edge flaps, air brakes or spoilers · CPC title

• B64C13/16

  actuated automatically, e.g. responsive to gust detectors · CPC title