Compact track arrangement for aerodynamic surfaces

Patent metadata

Field	Value
Publication number	US-11702186-B2
Application number	US-202117385540-A
Country	US
Kind code	B2
Filing date	Jul 26, 2021
Priority date	Jul 26, 2021
Publication date	Jul 18, 2023
Grant date	Jul 18, 2023

Abstract

Certain aspects of the present disclosure provide techniques for an aerodynamic surface actuation system, including: a plurality of outer tracks, wherein each outer track of the plurality of outer tracks includes: an inner outer roller channel; and an outer inner roller channel positioned above the inner outer roller channel; an aerodynamic surface connected to a carrier, wherein the carrier includes rollers configured to move within inboard inner roller channels of the plurality of outer tracks; and a plurality of fixed rollers mounted to one or more longitudinal structural elements in an aerodynamic structure, wherein the plurality of fixed rollers are disposed within the outer roller channels of the plurality of outer tracks.

First claim

What is claimed is:

1. An aerodynamic surface actuation system, comprising:
a plurality of outer tracks, wherein each outer track of the plurality of outer tracks comprises:
an outer roller channel; and
an inner roller channel positioned above the outer roller channel;

an aerodynamic surface connected to a carrier, wherein the carrier comprises rollers configured to move within inner roller channels of the plurality of outer tracks; and
a plurality of fixed rollers mounted to one or more longitudinal structural elements in an aerodynamic structure, wherein the plurality of fixed rollers are disposed within the outer roller channels of the plurality of outer tracks.

2. The aerodynamic surface actuation system of claim 1 , further comprising:
a rack gear connected with the plurality of outer tracks; and
a pinion gear configured to interface with the rack gear and cause the rack gear to move forward and backward.

3. The aerodynamic surface actuation system of claim 2 , further comprising a belt assembly disposed within a channel of the rack gear and connected to the carrier.

4. The aerodynamic surface actuation system of claim 3 , wherein the belt assembly comprises:
a forward roller;
an aft roller; and
a belt running continuously around the forward roller and the aft roller,
wherein the belt is connected to the carrier.

5. The aerodynamic surface actuation system of claim 4 , further comprising a reaction link disposed within the channel of the rack gear and connected to a transverse structural element in the aerodynamic structure.

6. The aerodynamic surface actuation system of claim 5 , wherein:
the aerodynamic structure is an aircraft wing, and
the aerodynamic surface is a slat.

7. The aerodynamic surface actuation system of claim 6 , wherein:
the one or more longitudinal structural elements comprise ribs of the aircraft wing, and
the transverse structure element comprises a spar of the aircraft wing.

8. The aerodynamic surface actuation system of claim 7 , further comprising an actuator configured to rotate the pinion gear in a first direction to cause the aerodynamic surface to move away from the aerodynamic structure, and configured to rotate the pinion gear in a second direction to cause the aerodynamic surface to move toward the aerodynamic structure.

9. The aerodynamic surface actuation system of claim 7 , wherein when in a fully retracted position, no part of the aerodynamic surface actuation system extends beyond the spar of the aircraft wing.

10. The aerodynamic surface actuation system of claim 1 , wherein the inner roller channel and outer roller channel of each outer track generally define curvilinear paths.

11. A method of actuating an aerodynamic surface, comprising:
moving a plurality of outer tracks along a plurality of fixed rollers, wherein:
each outer track of the plurality of outer tracks comprises:
an outer roller channel; and
an inner roller channel positioned above the outer roller channel, and

the plurality of fixed rollers are connected to one or more longitudinal structural elements in an aerodynamic structure and disposed within outer roller channels of the plurality of outer tracks; and

moving a carrier connected to an aerodynamic surface via rollers connected to the carrier and disposed within inner roller channels of the plurality of outer tracks.

12. The method of claim 11 , wherein moving the carrier connected to the aerodynamic surface further comprises rotating a pinion gear to cause a rack gear connected with the plurality of outer tracks to move.

13. The method of claim 12 , wherein moving the carrier connected to the aerodynamic surface further comprises rotating a belt assembly disposed within a channel of the rack gear and connected to the carrier.

14. The method of claim 13 , wherein the belt assembly comprises:
a forward roller;
an aft roller; and
a belt running continuously around the forward roller and aft roller.

15. The method of claim 14 , wherein the belt assembly further comprises a reaction link disposed within the channel of the rack gear and connected to a transverse structural element in the aerodynamic structure.

16. The method of claim 15 , wherein:
the aerodynamic structure is an aircraft wing, and
the aerodynamic surface is a slat.

17. The method of claim 16 , wherein:
the one or more longitudinal structural elements comprise ribs of the aircraft wing, and
the transverse structure element comprises a spar of the aircraft wing.

18. The method of claim 17 , wherein moving the carrier connected to the aerodynamic surface further comprises operating an actuator configured to rotate the pinion gear in a first direction to cause the aerodynamic surface to move away from the aerodynamic structure, and configured to rotate the pinion gear in a second direction to cause the aerodynamic surface to move toward the aerodynamic structure.

19. The method of claim 17 , further comprising fully retracting a position of the aerodynamic surface without any of the outer tracks or the rack gear extending beyond the spar of the aircraft wing.

20. The method of claim 11 , wherein the inner roller channel and outer roller channel of each outer track generally define curvilinear paths.

Assignees

• Boeing Co

Inventors

• Walker Steven P
• Santini Gregory M
• Prow Clayton
• Wright Gary

Classifications

• B64C9/24 Primary

  by single flap · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C9/22

  at the front of the wing · CPC title

• B64C13/34

  using toothed gearing · CPC title

• B64C9/08

  bodily displaceable · CPC title