Turbine Shaft Support with Elastomer Inserts

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Solution Overview

Problem

Existing support systems for connecting a degassing pipe to a turbine shaft with a changing inner diameter cause scratches and potential cracks on the turbine shaft during installation and operation, leading to structural deterioration and risk of rupture.

Innovation Solution

A split support system with elastomer inserts along outer contact spans and dimples to prevent metal/metal contact, combined with a conical socket and nut for radial expansion, ensuring secure and protective assembly and disassembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a split support system is used to connect the degassing pipe to the turbine shaft, then the connection is secured, but scratches and cracks occur on the turbine shaft during installation and operation

Engineering Contradiction:
Improveconnection strengthVSAvoidshaft deterioration
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

An elastomer insert is introduced as an intermediary element between the split support and the turbine shaft. This elastomer insert acts as a protective mediator that prevents direct metal-to-metal contact, thereby eliminating scratches and cracks on the turbine shaft while maintaining the secure connection function of the support system.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The support system transitions from a purely metallic construction to a composite structure combining metal (split support) with elastomer material (insert). This composite approach leverages the strength of metal for structural integrity and the protective properties of elastomer to prevent shaft deterioration, resolving the contradiction between connection strength and shaft protection.

Inventive Principle:
Principle #40Composite materials

2Reliability

If the support system is tightly secured to the turbine shaft, then connection reliability is improved, but assembly and disassembly become difficult

Engineering Contradiction:
Improveconnection reliabilityVSAvoidassembly and disassembly ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The elastomer insert introduces dynamic characteristics to the connection system. During assembly, the elastomer can deform to accommodate insertion; during operation, it maintains reliable connection through elastic recovery; and during disassembly, its flexibility facilitates removal. This dynamic behavior resolves the contradiction between secure connection and ease of assembly/disassembly.

Inventive Principle:
Principle #15Dynamics

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

The solution reduces the risk of turbine shaft deterioration, facilitates faster and safer assembly and disassembly, and extends the lifespan of the turbine shaft by minimizing contact and wear during operation.

Implementation Method 1

the different spans are each bordered by at least one elastomer insert which contributes to the protection of the turbine shaft during insertion of the support therein

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

a nut intended to exert an axial thrust force on said support by screwing onto the threaded portion of a conical socket, said socket having a conical portion intended to transform the axial thrust into radial expansion of said support

Methodology Applied
Scientific EffectPoisson's effect: Poisson's Effect

Implementation Method 3

The oils are captured by centrifugal effect to then be re-injected into the compartments of the rolling elements

Methodology Applied
Scientific EffectCentrifugal separation: Centrifugal Separation

Data Source

PatentUS10302016B2Support providing a complete connection between a turbine shaft and a degassing pipe of a turbojet
Publication Date: 2019.05.28 SAFRAN AIRCRAFT ENGINES SAS
  • US10302016B2 patent drawing
  • US10302016B2 patent drawing
  • US10302016B2 patent drawing

AI summary

The invention relates to a support providing a complete connection between a degassing pipe (3) and a turbine shaft (2), said support including a plurality of outer contact spans (41a) intended to bear on the inner walls of the turbine shaft to secure the degassing pipe with respect thereto, characterized in that the different spans are each bordered by at least one elastomer insert (41g) which contributes to the protection of the turbine shaft during insertion of the support therein.