Composite PDU tire in an aircraft cargo handling system

Patent metadata

Field	Value
Publication number	US-12522022-B2
Application number	US-202217846267-A
Country	US
Kind code	B2
Filing date	Jun 22, 2022
Priority date	Nov 17, 2021
Publication date	Jan 13, 2026
Grant date	Jan 13, 2026

Abstract

A composite PDU tire in an aircraft cargo handling system may include a plurality of bonded regions configured to propel cargo within an aircraft cargo bay. The composite tire may include edge regions that are stiffer than a cylindrical region. The edge regions may be configured to have a greater wear resistance and abrasion resistance relative to the cylindrical region. The cylindrical region may be configured to have greater traction relative to the edge regions. The edge regions may include a fillet profile and may be configured to reduce chipping as cargo climbs across the tire.

First claim

What is claimed is:

1 . A composite tire, the composite tire comprising:
a cylindrical region having a first circumferential groove and a second circumferential groove, an inner radial portion of the cylindrical region configured to couple to a first outer radial portion of a wheel; a first edge region having a fillet, wherein the first edge region is configured to axially couple to the first circumferential groove at a first bonding region and wherein an inner radial portion of the first edge region is configured to couple to a second outer radial portion of the wheel; and a second edge region having a fillet, wherein the second edge region is configured to axially couple to the second circumferential groove at a second bonding region and wherein an inner radial portion of the second edge region is configured to couple to a third outer radial portion of the wheel, wherein the first edge region and the second edge region comprise a first material and the cylindrical region comprises a second material, wherein the first material is stiffer than the second material, wherein the first material and the second material are different materials.

2 . The composite tire of claim 1 , wherein the first edge region comprises a first extended cylindrical step coupled to the first circumferential groove at the first bonding region.

3 . The composite tire of claim 2 , wherein the second edge region comprises a second extended cylindrical step coupled to the second circumferential groove at the second bonding region.

4 . The composite tire of claim 1 , wherein the first edge region comprises a first box joint profile coupled to a first complementary interlocking profile extending from the first circumferential groove at the first bonding region.

5 . The composite tire of claim 4 , wherein the second edge region comprises a second box joint profile coupled to a second complimentary interlocking profile extending from the second circumferential groove at the second bonding region.

6 . The composite tire of claim 1 , wherein the first edge region comprises a first dovetail profile coupled to a first dovetail pin extending from the first circumferential groove at the first bonding region.

7 . The composite tire of claim 6 , wherein the second edge region comprises a second dovetail profile coupled to a second dovetail pin extending from the second circumferential groove at the second bonding region.

8 . The composite tire of claim 1 , wherein the first edge region and the second edge region have a greater wear resistance relative to the cylindrical region.

9 . The composite tire of claim 1 , wherein the first edge region and the second edge region have a greater abrasion resistance relative to the cylindrical region.

10 . The composite tire of claim 1 , wherein the cylindrical region comprises a plurality of treads.

11 . The composite tire of claim 10 , wherein the cylindrical region has greater traction relative to the first edge region and the second edge region.

12 . The composite tire of claim 1 , wherein the cylindrical region has a higher coefficient of thermal expansion relative to the first edge region and the second edge region.

13 . A tire assembly comprising:
a composite tire bonded to a wheel, the composite tire comprising:
a cylindrical region having a first circumferential groove and a second circumferential groove, an inner radial portion of the cylindrical region configured to couple to a first outer radial portion of the wheel;
a first edge region having a fillet, wherein the first edge region is configured to axially couple to the first circumferential groove at a first bonding region and wherein an inner radial portion of the first edge region is configured to couple to a second outer radial portion of the wheel; and
a second edge region having a fillet, wherein the second edge region is configured to axially couple to the second circumferential groove at a second bonding region and wherein an inner radial portion of the second edge region is configured to couple to a third outer radial portion of the wheel,
wherein the first edge region and the second edge region comprise a first material and the cylindrical region comprises a second material, wherein the first material is stiffer than the second material, wherein the first material and the second material are different.

14 . The tire assembly of claim 13 , the wheel further comprising:
an inner hub, wherein the inner hub defines a cavity; and an outer rim having a flange.

15 . The tire assembly of claim 14 , wherein the first edge region comprises a first extended cylindrical step coupled to the first circumferential groove at the first bonding region.

16 . The tire assembly of claim 15 , wherein the second edge region comprises a second extended cylindrical step coupled to the second circumferential groove at the second bonding region.

17 . The tire assembly of claim 15 , wherein the first edge region comprises a first box joint profile coupled to a first complementary interlocking profile extending from the first circumferential groove at the first bonding region.

Assignees

• Goodrich Corp

Inventors

• Yadav Sanjay
• Saini Mohinder

Classifications

• B60B9/10

  of rubber or the like · CPC title

• B60B21/02

  characterised by transverse section · CPC title

• B29D30/02

  Solid tyres {; Moulds therefor} · CPC title

• B60C2007/005

  made by casting, e.g. of polyurethane · CPC title

• B60Y2200/50

  Aeroplanes, Helicopters · CPC title