Frustoconical Input Shaft for Torque and Misalignment Balance

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Solution Overview

Problem

Propulsion systems with speed reduction mechanisms face challenges in mechanical strength and flexibility due to misalignment issues, leading to reduced service life from concentrated static and dynamic loads, particularly at the junction of the shaft and gussets.

Innovation Solution

A shaft with a frustoconical barrel and symmetrical gussets is designed to decouple the concentration of static and dynamic loads, where the barrel's frustoconical shape and gusset dimensions optimize mechanical strength and flexibility, with the barrel being stiffer near the gusset connected to the bearing and more flexible near the sun gear.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a rigid barrel and straight gussets are used in the shaft, then torque transmission is improved, but misalignment compensation capability deteriorates

Engineering Contradiction:
Improvetorque transmission capabilityVSAvoidmisalignment compensation capability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The shaft employs different geometric properties in different regions: the barrel is frustoconical with varying diameter along its length, providing different stiffness characteristics at different locations. The gussets have optimized dimensions and positions to provide flexibility where needed while maintaining strength where required. This local differentiation allows simultaneous achievement of torque transmission and misalignment compensation.

Inventive Principle:
Principle #3Local quality

2Adaptability or versatility

If the shaft is made more flexible to compensate misalignments, then misalignment tolerance is improved, but mechanical strength under static loads deteriorates

Engineering Contradiction:
Improvemisalignment toleranceVSAvoidmechanical strength under static loads
Core Design Contradiction:
Adaptability or versatilityVSStrength

Solution Approach 1:

The shaft design utilizes parameter optimization including the frustoconical barrel geometry with specific diameter ratios, gusset thickness and positioning parameters, and material properties to achieve the desired balance between flexibility and strength. The geometric parameters are carefully selected to provide adequate misalignment tolerance while maintaining structural integrity under static loading conditions.

Inventive Principle:
Principle #35Parameter changes

3Strength

If the shaft geometry is optimized for strength, then mechanical robustness is improved, but flexibility to accommodate misalignments deteriorates

Engineering Contradiction:
Improvemechanical robustnessVSAvoidflexibility to accommodate misalignments
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The shaft is segmented into distinct functional zones: the frustoconical barrel section provides progressive stiffness transition, while the gusset regions provide localized flexibility. This segmentation allows each zone to perform its specific function optimally - the barrel for strength and the gussets for flexibility - thereby resolving the contradiction between mechanical robustness and adaptability.

Inventive Principle:
Principle #1Segmentation

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

This design significantly enhances the service life margin of the shaft by distributing loads effectively, improving mechanical robustness and flexibility while maintaining the shaft's geometric and inertial properties.

Implementation Method 1

the barrel being stiffer near the gusset connected to the bearing and more flexible near the sun gear

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

the barrel's frustoconical shape and gusset dimensions optimize mechanical strength and flexibility

Methodology Applied
Scientific EffectMechanical Advantage: Mechanical Advantage

Data Source

PatentUS11879398B2Flexible frustoconical input shaft
Publication Date: 2024.01.23 SAFRAN AIRCRAFT ENGINES SAS
  • US11879398B2 patent drawing
  • US11879398B2 patent drawing
  • US11879398B2 patent drawing

AI summary

The present invention relates to a shaft for a propulsion system configured to rotate a reducing mechanism about a rotational axis, the shaft comprising: —a first end configured to engage with an input gear of the reducing mechanism, —a first bellows and a second bellows, the first bellows and the second bellows being rotationally symmetrical about the rotational axis, the first bellows extending between the first end and the second bellows, and —a frustoconical body mechanically connecting the first bellows and the second bellows.