Aircraft moving device

• US 8,235,152 B2
• Filed: 06/23/2009
• Issued: 08/07/2012
• Est. Priority Date: 06/23/2008
• Status: Expired due to Fees

• Current Assignee: Redline Aviation, LLC
• Original Assignee: Redline Aviation, LLC
• Inventors: Kastan, Linn
• Primary Examiner(s): Morris, Lesley D.
• Assistant Examiner(s): STABLEY, MICHAEL R
• Application Number:
  US12/489,791
• Publication Number:
  US 20100006354A1
• Time in Patent Office: 1,141 Days
• Field of Search: 180/19.2, 180/19.1, 180/904
• US Class Current: 180/19.2
• CPC Class Codes: B60S 13/00 Vehicle-manoeuvring devices separate from the vehicle vehicle lifting , e.g. liftable turntables or pushing devices B66F; workshop equipment B25H
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64F 1/22 for handling aircraft
• CPC Class Codes: B64F 1/226 hand manipulated, e.g. hand carts or motorised walk-type tractors
• CPC Class Codes: Y10S 180/904 Traction dollies for aircraft

Abstract

A tow apparatus for moving an aircraft comprising a frame, a drive member, a contact wheel configured to engage with a nosewheel tire of an aircraft, a transmission portion, a shaft engageable with a nosewheel tire of an aircraft, and a torque arm rotatably supported by the frame. The transmission portion can be configured such that the drive wheels transfer and increase a rotational force produced by the drive member to the contact wheel. The shaft can be movable between a first position and a second position relative to the contact wheel so as to bring the contact wheel into contact with the nosewheel of the aircraft. The torque arm can substantially prevent the rotation of the tow apparatus relative to the nosewheel assembly of the aircraft when the torque arm is engaged with the nosewheel assembly of the aircraft. The drive member can have a portable power source.

Claims

1. A portable tow apparatus for moving an aircraft, comprising:

a frame;

a drive member supported by the frame, the drive member having a portable power source;

a contact wheel supported by the frame and configured to be engageable with a nosewheel tire of an aircraft;

a transmission portion comprising one or more drive wheels supported by the frame, the drive wheels being rotatable relative to the frame, the transmission portion being configured such that the drive wheels transfer and increase a rotational force produced by the drive member to the contact wheel;

a shaft supported by the frame and configured to be insertable into an opening in a nosewheel assembly of an aircraft, the shaft being movable between a first position and a second position relative to the contact wheel, the shaft being closer to the contact wheel in the second position than in the first position; and

a torque arm supported by the frame and configured to be engageable with the nosewheel assembly of the aircraft, the torque arm being configured to substantially prevent the rotation of the tow apparatus relative to the nosewheel assembly of the aircraft when the torque arm is engaged with the nosewheel assembly of the aircraft;

wherein a centerline axis of the shaft is closer to a centerline axis of the contact wheel when the shaft is in the second position than in the first position.

2. The tow apparatus of claim 1, wherein the drive wheels are gears.

3. The tow apparatus of claim 1, wherein the drive wheels are pulleys.

4. The tow apparatus of claim 1, wherein the transmission portion comprises two or more gears supported by the frame.

5. The tow apparatus of claim 4, wherein the transmission portion further comprises a chain that is supported by two or more of the gears.

6. The tow apparatus of claim 1, wherein the transmission portion comprises four gears supported by the frame.

7. The tow apparatus of claim 6, wherein the transmission portion further comprises a first chain supported by a first gear and a second gear, and a second chain supported by a third gear and a fourth gear.

8. The tow apparatus of claim 7, wherein the second gear is rotationally linked to the third gear.

9. The tow apparatus of claim 1, wherein the tow apparatus is configured so that the drive member can securably rotate between a compact position and an extended position relative to the frame, wherein the overall length of tow apparatus is significantly reduced in the compact position as compared to the extended position.

10. The tow apparatus of claim 1, wherein the transmission portion can increase the torque generated by the drive member by a ratio of 4:

1.

11. The tow apparatus of claim 1, wherein the transmission portion can increase the torque generated by the drive member by between approximately 2:

1 and approximately 8;

1.

12. The tow apparatus of claim 1, wherein the tow apparatus is configured so that the shaft is securable in the second position after the tow apparatus has been engaged with the nosewheel assembly of an aircraft.

13. The tow apparatus of claim 1, wherein the shaft is moved between the first position and the second position relative to the contact wheel by rotating a lever arm linked to the shaft.

14. The tow apparatus of claim 1, wherein the shaft is configured to be insertable into an opening in a nosewheel assembly so that the centerline of the shaft is approximately collinear with the axis of rotation of the nosewheel of the aircraft.

15. The tow apparatus of claim 1, wherein the drive member is battery powered.

16. The tow apparatus of claim 1, wherein the drive member is a right angled, battery powered drill.

17. The tow apparatus of claim 1, wherein the torque arm is rotatably supported by the frame.

18. The tow apparatus of claim 1, wherein the shaft is configured to attach to the nosewheel assembly at a first location and the torque arm is configured to attach to the nosewheel assembly at a second location that is different than the first location.