Aircraft taxi system including drive chain

Patent metadata

Field	Value
Publication number	US-8979019-B2
Application number	US-201113192084-A
Country	US
Kind code	B2
Filing date	Jul 27, 2011
Priority date	Jul 27, 2011
Publication date	Mar 17, 2015
Grant date	Mar 17, 2015

Abstract

An aircraft taxi drive system includes a motor that is configured to transfer power to an aircraft wheel via a drive chain, such that the motor rotates the aircraft wheel via the drive chain. In some examples, the drive chain is movable between first and second positions. In the first position, the drive chain, such as an exterior surface of the drive chain, is engaged with a driven sprocket that is mechanically connected to an aircraft wheel. In the second position, the drive chain is disengaged from the driven sprocket.

First claim

The invention claimed is:

1. A landing gear drive system comprising:
a piston;
an axle;
a mounting assembly fixedly connected to at least one of the piston and the axle;
a driving assembly operably and fixedly connected to the mounting assembly to move between a first position and a second position, the driving assembly including;
a motor configured to generate a mechanical output;
a drive sprocket configured to be driven by the motor;
a drive chain configured to form a closed loop and mechanically connected to the drive sprocket, wherein the drive sprocket is configured to transfer the mechanical output from the motor to the drive chain, and wherein the drive chain defines an interior surface on an inner circumference of the closed loop and an exterior surface on the outer circumference of the closed loop, the interior surface facing the drive sprocket;

an aircraft wheel mounted on the axle; and
a driven sprocket mechanically connected to the aircraft wheel, wherein the exterior surface of the drive chain is configured to engage with and rotate the driven sprocket to transfer the mechanical output of the motor to the driven sprocket and the aircraft wheel when the driving assembly is in the first position; and
the drive chain is disengaged from the driven sprocket when the driving assembly is in the second position; and wherein rotation of the driven sprocket is configured to rotate the aircraft wheel.

2. The system of claim 1 , further comprising a controller configured to control the motor to rotate, before the drive chain is brought into engagement with the driven sprocket, at a speed that is based on a rotational speed of the driven sprocket.

3. The system of claim 1 , further comprising a controller, wherein the controller is configured to control a rotational speed of the motor and engagement of the drive chain with the driven sprocket based on user input.

4. The system of claim 1 , wherein the driven sprocket includes a plurality of teeth configured to be positioned within gaps defined by the drive chain when the drive chain is engaged with the driven sprocket.

5. The system of claim 1 , further comprising an actuator, wherein the actuator is configured to rotate the driving assembly about a pivot point between the first and second positions to engage and disengage, respectively, the drive chain from the driven sprocket.

6. The system of claim 1 , further comprising a linear bearing, wherein the linear bearing is configured to translate the driving assembly relative to the driven sprocket to engage and disengage, respectively, the drive chain from the driven sprocket.

7. The system of claim 1 , further comprising a linkage, wherein the linkage is configured to translate the driving assembly relative to the driven sprocket to engage and disengage the drive chain from the driven sprocket.

8. The system of claim 5 , wherein the actuator comprises a hydraulic piston.

9. The system of claim 5 , wherein the actuator comprises an electrically driven screw drive.

10. A method comprising:
moving a driving assembly including a motor and a closed loop drive chain, and operably mounted to at least one of a piston and an axle of a landing gear of an aircraft, to a first position wherein an exterior surface of the closed loop drive chain is engaged with a driven sprocket that is mechanically connected to an aircraft wheel, the drive chain defining an interior surface on inner circumference of the closed loop and the exterior surface on the outer circumference of the closed loop, the interior surface facing a drive sprocket;
rotating the aircraft wheel by transferring a mechanical output of the motor to the driven sprocket and aircraft wheel via the drive chain; and
disengaging the drive chain from the driven sprocket by moving the driving assembly to a second position.

11. The method of claim 10 , further comprising slowing an aircraft comprising the aircraft wheel to a speed of about 0 knots to about 25 knots prior to moving the driving assembly to the first position.

12. The method of claim 10 , further comprising, prior to moving the driving assembly to a first position, rotating the drive chain at a speed that is based on a rotational speed of the driven sprocket.

13. The method of claim 10 , wherein moving the driving assembly to the first position comprises moving the driving assembly radially towards the driven sprocket.

14. The method of claim 10 , wherein moving the driving assembly to the first position comprises rotating the driving assembly towards the driven sprocket about a pivot point.

15. The method of claim 10 , wherein moving the driving assembly to the first position and the second position comprises moving the driving assembly radially towards and away from, respectively, the driven sprocket.

Assignees

• Christensen Donald J
• Gaines Louie T
• Charles David L
• Honeywell Int Inc

Inventors

• Christensen Donald J
• Gaines Louie T
• Charles David L

Classifications

• B64C25/405 Primary

  Powered wheels, e.g. for taxing · CPC title

• Y02T50/823

  Cross-Sectional Technologies · mapped topic

• Y02T50/80

  Energy efficient operational measures, e.g. ground operations or mission management · CPC title