Nested Hybrid Thrust Bearing to Preserve Magnetic Bearing Gap

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Solution Overview

Problem

In existing hybrid thrust bearings, the integration of an airfoil bearing with a magnetic bearing leads to an increase in the gap between the thrust disk and the magnetic bearing, deteriorating the performance of the magnetic bearing.

Innovation Solution

The airfoil bearing is integrated into the magnetic bearing structure by inserting part of the airfoil bearing into the magnetic bearing's attachment part, with the airfoil pad covering the coil and being fastened to protruding columns, preventing the gap from increasing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Force

If an airfoil bearing is simply combined with a magnetic bearing, then the load capacity is improved, but the gap between the magnetic bearing and thrust disk increases causing performance deterioration

Engineering Contradiction:
Improveload capacityVSAvoidmagnetic bearing performance
Core Design Contradiction:
ForceVSReliability

Solution Approach 1:

The airfoil bearing is nested within the magnetic bearing structure by inserting the airfoil pad into the attachment part of the magnetic bearing. This nesting arrangement allows the airfoil bearing to be housed inside the magnetic bearing's attachment part, preventing gap increase while maintaining load capacity benefits

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The airfoil bearing is positioned in the radial direction (inserted into the attachment part) rather than only in the axial direction. This dimensional change allows the airfoil bearing to occupy space within the magnetic bearing structure without increasing the axial gap, thereby maintaining magnetic bearing performance while adding load capacity

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Reliability

If the airfoil bearing is inserted into the magnetic bearing attachment part, then the gap increase is prevented, but the structural complexity increases

Engineering Contradiction:
Improvemagnetic bearing performanceVSAvoidintegration structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The attachment part of the magnetic bearing serves multiple functions: it provides mechanical support for the coil and simultaneously houses the airfoil pad. This multi-functionality reduces the need for additional separate structures, thereby limiting the increase in structural complexity while achieving the integration goal

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

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 integration maintains the performance of the magnetic bearing while supporting axial loads and reducing lateral vibrations in turbomachinery, enhancing the axial load capacity and damping without additional backup bearings.

Implementation Method 1

magnetic bearings support the axial load using electromagnetic force

Methodology Applied
Scientific EffectElectromagnetic force: Electromagnet

Implementation Method 2

thrust bearings include bump foil bearings, leaf foil bearings, porous foil bearings using air lubrication

Methodology Applied
Scientific EffectAir lubrication: Air Lubrication

Data Source

PatentUS12584517B2Integrated hybrid thrust bearing
Publication Date: 2026.03.24 KOREA INST OF SCI & TECH
  • US12584517B2 patent drawing
  • US12584517B2 patent drawing
  • US12584517B2 patent drawing

AI summary

The present disclosure relates to a hybrid thrust bearing that combines an airfoil bearing and a magnetic bearing to support a rotating shaft with a disk-shaped thrust disk, and the magnetic bearing includes a disk-shaped housing into which the rotation shaft is inserted through a hole formed in a center and facing the thrust disk, a ring-shaped inner pole part formed around the hole on one side of the housing facing the thrust disk, a ring-shaped outer pole part disposed outside the inner pole part, an attachment part provided between the inner pole part and the outer pole part, and a coil stored in the attachment part, wherein a part of the airfoil bearing is inserted into the attachment part.