Axle saddle

Patent metadata

Field	Value
Publication number	US-10329011-B2
Application number	US-201514874098-A
Country	US
Kind code	B2
Filing date	Oct 2, 2015
Priority date	Oct 2, 2015
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

According to various embodiments, disclosed is an axle saddle system for an axle having an undercut between the outboard and inboard bearing lands of the axle. According to various embodiments, the axle saddle system comprises a saddle configured to fill the axle undercut in order to protect the axle from damage by the installation of a wheel onto the axle.

First claim

The invention claimed is:

1. An axle saddle system comprising:
an axle comprising an outboard bearing land, an inboard bearing land, and an undercut situated between the outboard bearing land and the inboard bearing land, wherein the undercut is radially tapered with respect to at least one of the outboard bearing land and the inboard bearing land;
a saddle substantially covering the undercut, wherein the saddle fills the undercut, such that a diameter of the filled undercut is approximately equal to a diameter of the outboard bearing land and a diameter of the inboard bearing land; and
a first saddle strap configured to tighten the saddle around the undercut.

2. The axle saddle system of claim 1 , wherein an axial length of the saddle is equal to an axial length of the undercut.

3. The axle saddle system of claim 2 , wherein the saddle defines a first strap channel, and wherein the first saddle strap is configured to nest within the first strap channel.

4. The axle saddle system of claim 3 , wherein the first saddle strap comprises a buckle, and the saddle defines a buckle cut out adjacent the strap channel, and wherein the buckle is configured to nest within the buckle cut out.

5. The axle saddle system of claim 4 , wherein the first saddle strap and the buckle are level with an outer surface of the saddle when nested.

6. The axle saddle system of claim 4 , further comprising:
a second saddle strap located in a second strap channel defined by the saddle; and
a third saddle strap located in a third strap channel defined by the saddle.

7. The axle saddle system of claim 2 , wherein the first saddle strap is a stainless steel cable tie.

8. The axle saddle system of claim 1 , wherein the saddle further comprises a moisture draining system.

9. The axle saddle system of claim 8 , wherein the moisture draining system comprises a plurality of drain holes in the saddle.

10. The axle saddle system of claim 1 , the saddle comprising at least one of a cylindrical or a conical geometry.

11. The axle saddle system of claim 1 , wherein the saddle comprises a saddle perimeter and an axial split along a saddle axial length, the axial split spanning between 10° to 45° of the saddle perimeter.

12. The axle saddle system of claim 11 , wherein the saddle may be deformed to an open position for insertion over the undercut.

13. The axle saddle system of claim 1 , wherein the outboard bearing land and the inboard bearing land are each configured to receive a bearing assembly of an aircraft wheel.

14. The axle saddle system of claim 1 , wherein the undercut is tapered with respect to both the outboard bearing land and the inboard bearing land.

15. An axle saddle system comprising:
an axle comprising an outboard bearing land, an inboard bearing land, and an undercut situated between the outboard bearing land and the inboard bearing land, wherein the undercut is radially tapered with respect to at least one of the outboard bearing land and the inboard bearing land; and
a saddle substantially covering the undercut, wherein the saddle fills the undercut, such that a diameter of the saddle is approximately equal to a diameter of the outboard bearing land and a diameter of the inboard bearing land.

16. The axle saddle system of claim 15 , further comprising a first saddle strap configured to tighten the saddle around the undercut.

17. The axle saddle system of claim 16 , wherein the saddle defines a first strap channel, and wherein the first saddle strap is located within the first strap channel.

18. The axle saddle system of claim 17 , wherein the first saddle strap is configured to nest within the first strap channel such that a diameter of the first saddle strap is equal to the diameter of the saddle.

19. The axle saddle system of claim 15 , wherein the saddle further comprises a moisture draining system including a plurality of drain holes defined by the saddle.

20. The axle saddle system of claim 15 , wherein the saddle having a saddle perimeter and an axial split along a saddle axial length, the axial split spanning between approximately 10° to 45° of the saddle perimeter.

Assignees

• Goodrich Corp

Inventors

• Swank John
• Hunnicutt Shane E
• Kossler Joshua Stephen
• Patterson Michael Neal

Classifications

• B60B35/025

  the wheels being removable · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B64C25/36 Primary

  Arrangements or adaptations of wheels, tyres or axles in general · CPC title

• B60B2340/00

  Wheel transporting, Mounting of wheels · CPC title

• B60B2900/212

  Damage · CPC title