Hybrid Bearing System for Reducing Radial Thrust Loads

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Solution Overview

Problem

Current turbomachines face challenges such as high expense and complexity of magnetic bearings, scaling issues with foil bearings, high power consumption of hydrostatic bearings, and decreased reliability under high loads, making them unsuitable for large machines.

Innovation Solution

A turbomachine design incorporating a hybrid bearing system with a magnetic thrust bearing and axially floating radial bearings mounted on a flexible flexure, which reduces thrust loads on radial bearings and allows the magnetic thrust bearing to carry axial loads, enabling a more cost-effective and reliable operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If magnetic bearings are used in turbomachines, then reliability is improved, but device complexity and expense increase

Engineering Contradiction:
Improvebearing reliabilityVSAvoidbearing system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bearing system is segmented into two distinct functional components: a magnetic thrust bearing that handles only axial loads, and conventional radial bearings that handle radial loads. This segmentation allows each bearing type to be optimized for its specific function, reducing overall system complexity while maintaining reliability through specialized design.

Inventive Principle:
Principle #1Segmentation

2Ease of manufacture

If foil bearings are used in turbomachines, then expense is reduced, but scaling problems occur making large machines unfeasible

Engineering Contradiction:
Improvemanufacturing costVSAvoidscaling capability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent employs a hybrid bearing system where conventional radial bearings provide universal support for both small and large turbomachine applications. This multi-functional approach allows the same radial bearing design to scale across different machine sizes, overcoming the scaling limitations of foil bearings while maintaining cost-effectiveness.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Reliability

If hydrostatic bearings are used in turbomachines, then reliability is improved, but power consumption increases

Engineering Contradiction:
Improvebearing reliabilityVSAvoidpower consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent extracts the active control system from the radial bearing support function, using passive magnetic and mechanical elements instead. The magnetic thrust bearing provides active axial support only where needed, while radial support is achieved through passive floating mounting, eliminating the high power consumption associated with fully active hydrostatic bearing systems.

Inventive Principle:
Principle #2Taking out (Extraction)

4Productivity

If ball bearings are operated under high loads, then productivity is maintained, but reliability decreases

Engineering Contradiction:
Improveoperational capacityVSAvoidbearing reliability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The patent applies local quality by assigning different load-handling capabilities to different bearing locations. The magnetic thrust bearing is specifically designed to handle high axial loads, while radial bearings operate within their optimal load ranges. This localized specialization allows the system to maintain high productivity under high loads without compromising reliability.

Inventive Principle:
Principle #3Local quality

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 achieves cost and performance savings by enabling the production of smaller turbomachines with higher thrust loads and tighter clearance, while maintaining reliability and reducing complexity compared to traditional systems.

Implementation Method 1

a magnetic thrust bearing (128) to reduce thrust loads on the radial bearings (54)

Methodology Applied
Scientific EffectMagnetic field: Magnetic Field

Implementation Method 2

mounting the radial bearings (54) for axial movement on a flexible flexure (98)

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentEP2800913B1Turbomachine and method of reducing thrust loads on a radial bearing of a turbomachine
Publication Date: 2019.11.20 UNITED TECH CORP
  • EP2800913B1 patent drawingFigure 1~2
  • EP2800913B1 patent drawingFigure 3
  • EP2800913B1 patent drawingFigure 4~5

AI summary

A turbomachine includes a housing and a rotatable shaft, where at least a portion of the rotatable shaft is located in the housing. The turbomachine also includes a magnetic thrust bearing that axially positions the rotatable shaft and a radial bearing that centers the rotatable shaft. The turbomachine includes a flexure including a first portion secured to the housing and a second portion axially moveable relative to the first portion. The second portion of the flexure is connected to the radial bearing, and the second portion moves axially to eliminate thrust loads on the radial bearing and allow the magnetic thrust bearing to carry axial loads.