Aircraft Wheel Hub Protector With T-Bar Guide for Bearing Protection

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Solution Overview

Problem

Existing aircraft wheel protectors do not adequately protect the internal components of aircraft wheels and bearings from damage during transport, particularly from the T-bar used to secure the protector covers, which can cause nicks, scratches, and misalignment.

Innovation Solution

The introduction of internal protective protrusions within the aircraft wheel and wheel bearing cover that guide the T-bar for easy installation while preventing it from contacting the wheel bearings, thus protecting the internal surfaces and preventing misalignment or dislodgment of unretained bearings.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the T-bar is used to secure the protector covers, then the covers are tightly fastened to the wheel assembly, but the T-bar contacts the internal metal surfaces causing nicks, scratches, and grease transfer

Engineering Contradiction:
Improvefastening strengthVSAvoidsurface damage
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

A plastic guide member is introduced as an intermediary between the T-bar and the internal metal surfaces. The guide member has a passage that directs the T-bar through the wheel assembly while its outer surface protects the internal surfaces from contact with the T-bar, preventing nicks, scratches, and grease transfer while still allowing the T-bar to perform its fastening function

Inventive Principle:
Principle #24Intermediary (Mediator)

2Object-affected harmful factors

If the protective cover extends over internal components, then external forces and intrusions are blocked, but the internal components remain vulnerable to T-bar contact and misalignment

Engineering Contradiction:
Improveexternal protectionVSAvoidinternal component protection
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The protective cover is divided into two functional segments: the main cover body that provides external protection by extending over internal components, and the separate plastic guide member that specifically protects against T-bar contact. This segmentation allows each component to specialize in protecting against different types of damage

Inventive Principle:
Principle #1Segmentation

3Ease of operation

If unretained bearings rely on proper wheel installation, then bearing retention is achieved, but improper T-bar installation can dislodge bearings and cause safety issues

Engineering Contradiction:
Improveinstallation simplicityVSAvoidbearing retention
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The plastic guide member acts as a mediator that guides the T-bar through the wheel assembly along a predetermined path. The guide member's structure ensures proper T-bar alignment and positioning, preventing misinstallation that could dislodge unretained bearings while maintaining the simplicity of the installation process

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS20250050681A1Aircraft Wheel & Bearing Protectors with Integrated Internal Protection Protrusion and Fastening Member Guide
Publication Date: 2025.02.13 BILL THOMAS ASSOCIATES INC
  • US20250050681A1 patent drawing
  • US20250050681A1 patent drawing
  • US20250050681A1 patent drawing

AI summary

An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with one or more protective protrusions. The one or more protrusions retain one or more bearing races in a support section of the hub and protect an internal surface within an axle void within the hub of the rim of the aircraft wheel. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism is provided on or engaging the at least one protective protrusion and coupling the first cover section and second cover section together, thereby securing the aircraft wheel hub protector to the aircraft wheel and retaining the at least one bearing race.