Aircraft Wheel Rotational Drive Flexible Ring Clevis Attachment

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Solution Overview

Problem

Existing aircraft wheel rotational drive systems face challenges in accommodating deformations and movements due to ovalization and axle bending during taxiing, requiring complex and costly ball joint-type elements for attachment.

Innovation Solution

An aircraft wheel with a rotational drive system featuring a flexible and deformable chain ring attached to clevises on the rim, allowing for absorption of deformations and movement without complex attachments, using a drive pinion and rollers to transmit rotational force.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a toothed ring is mounted rigidly on the wheel rim, then the drive transmission is simple and direct, but the system cannot accommodate wheel deformations and movements during taxiing

Engineering Contradiction:
Improvedrive transmission reliabilityVSAvoidadaptability to wheel deformations
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The toothed ring is divided into multiple segments that can move relative to each other, allowing the ring to deform with the wheel while maintaining drive transmission. Each segment is connected through attachment members with clearances, enabling the ring to accommodate ovalization and axle bending movements.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The attachment members are designed with specific clearance parameters that allow controlled relative movement between the toothed ring segments and the wheel rim. This clearance enables the system to adapt to deformation parameters while maintaining functional integrity.

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If attachment members with clearances are used to allow relative movement, then the system can accommodate deformations, but complex ball joint-type elements are required

Engineering Contradiction:
Improveadaptability to wheel deformationsVSAvoidattachment mechanism complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The complex ball joint elements are extracted and replaced with simpler attachment members that have built-in clearances. The attachment members directly connect the toothed ring segments to the wheel rim through clearance holes, eliminating the need for separate ball joint components while maintaining the required adaptability.

Inventive Principle:
Principle #2Taking out (Extraction)

3Adaptability or versatility

If complex ball joint-type attachment elements are used, then relative movement is enabled, but the cost of the attachment system increases

Engineering Contradiction:
Improveadaptability to wheel deformationsVSAvoidmanufacturing cost
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The attachment members are designed as simple, inexpensive components with clearance holes that can be manufactured using standard processes. These simple attachment members replace costly ball joint elements, significantly reducing the overall manufacturing cost while maintaining the required functional adaptability.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables efficient rotation of the aircraft wheel while absorbing deformations and movements, utilizing standard rims and reducing the need for costly attachment components.

Implementation Method 1

the ring forms a flexible and deformable segment between two attachment members... The flexibility of the segments of the ring makes it possible to absorb deformations and movement of the wheel

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS9708055B2Aircraft wheel with rotational drive attached to clevises projecting from wheel rim
Publication Date: 2017.07.18 SAFRAN LANDING SYSTEMS
  • US9708055B2 patent drawing
  • US9708055B2 patent drawing
  • US9708055B2 patent drawing

AI summary

An aircraft wheel equipped with rotation-drivers (10) attached to clevises (19) projecting from a side of wheel rim (5). The rotation driver includes a ring (11) that is adapted to cooperate with a drive actuator and is provided with members (12) for attaching to the clevises in such a way that, between two attachment members, the ring forms a flexible and deformable segment.