Plane tractor

• US 8,935,049 B2
• Filed: 02/15/2011
• Issued: 01/13/2015
• Est. Priority Date: 02/16/2010
• Status: Active Grant

• Current Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Original Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Inventors: Decoux, Laurent, Enault, Eric, Vermalle, Nicholas
• Primary Examiner(s): Cheung, Mary
• Assistant Examiner(s): MAZZARA, ANNE MARIE
• Application Number:
  US13/578,907
• Publication Number:
  US 20120310482A1
• Time in Patent Office: 1,428 Days
• Field of Search: 701/41
• US Class Current: 701/41
• CPC Class Codes: B64F 1/22 for handling aircraft
• CPC Class Codes: B64F 1/227 for direct connection to aircraft, e.g. tow tractors without towing bars
• CPC Class Codes: Y02T 50/80 Energy efficient operational measures, e.g. ground operations or mission management

Abstract

A plane tractor that grips a nose gear of a plane is disclosed, which includes: a chassis; wheel modules connected to the chassis, with each wheel module including at least one actuator for inducing a vertical movement of the wheel module in relation to the chassis; a gripping platform for gripping the nose gear of a plane, with the platform together with the chassis having freedom of movement substantially in circular translation; and a damping and actuating means connecting the platform and the chassis.

Claims

1. An airplane tractor having a gripping system for gripping a nose gear of an airplane, the airplane tractor comprising:

a chassis;

wheel modules connected to the chassis, each of the wheel modules including at least one actuator for inducing a vertical movement of the wheel module in relation to the chassis;

a gripping platform for gripping the nose gear of the airplane, the gripping platform having freedom of movement such that the gripping platform is movable in a substantially pendular movement in relation to the chassis; and

an actuating means connecting the platform and the chassis, the actuating means including a damping means for damping the freedom of movement of the gripping platform in relation to the chassis.

2. The airplane tractor according to claim 1, further comprising at least one gate intended to oppose a force exerted on at least one wheel of the nose gear of the airplane by the gripping platform.

3. The airplane tractor according to claim 1, wherein the gripping platform comprises a locking device for locking at least one wheel of the nose gear of the airplane.

4. The airplane tractor according to claim 3, wherein the locking device of the at least one wheel of the nose gear is installed on a turret positioned on the gripping platform, the turret rotating freely around a substantially vertical axis in relation to the gripping platform.

5. The airplane tractor according to claim 1, wherein the damping and actuating means comprise a sensor of the relative movement between the gripping platform and the chassis.

6. The airplane tractor according to claim 1, wherein the gripping platform includes a base connected to the chassis by vertical tie rods.

7. A method for gripping a nose gear of an airplane using an airplane tractor, the airplane tractor including a chassis;

wheel modules connected to the chassis, each of the wheel modules including at least one actuator for inducing a vertical movement of the wheel module in relation to the chassis;

a gripping system for gripping the nose gear of the airplane, the gripping system including a gripping platform being moveable in a substantially pendular movement in relation to the chassis, the gripping platform going from a retracted position to a gripping position by way of an equilibrium position; and

a damping and actuating means connecting the gripping platform and the chassis, the method comprising;

actuating the damping and actuating means to place the gripping platform in the retracted position;

lowering the chassis;

moving the airplane tractor so as to place the retracted gripping platform in contact with at least one wheel of the nose gear of the airplane;

actuating the damping and actuating means to move the gripping platform from the retracted position toward the gripping position while adjusting the height of the chassis by controlling the actuators of at least two wheel modules so as to slide the gripping platform under the wheel;

raising the chassis; and

bringing the platform back to the equilibrium position.

8. The method according to claim 7, further comprising closing a gate of the airplane tractor when the gripping platform is in contact with the at least one wheel of the nose gear of the airplane.

9. The method according to claim 8, further comprising opening the gate of the airplane tractor when the chassis raises.

10. The method according to claim 7, further comprising, when the gripping platform has been slid under the wheel, moving the airplane tractor to bring the at least one wheel onto a locking device.

11. The method according to claim 10, further comprising:

setting the location of an abutment as a function of a type of airplane and/or a type of wheel;

bringing the at least one wheel onto the locking device against the abutment; and

bringing a tightening plate against the wheel to maintain the wheel against the abutment.