Aerodynamic Bearing Depth Profiling for High-Speed Air Cushion Stability

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Solution Overview

Problem

Existing methods for manufacturing aerodynamic bearings with varying depth profiles are complex and difficult to achieve, limiting the ability to maintain optimal pressure distribution and high rotational speeds.

Innovation Solution

The use of a discrete depth profile with a predetermined number of depth levels for the depressions in aerodynamic bearings, allowing for simplified manufacturing and improved pressure distribution, even at high rotational speeds.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If conventional methods such as lasers are used to manufacture continuous or step-free depth profiles, then the bearing can maintain optimal pressure distribution, but the manufacturing process becomes complex

Engineering Contradiction:
Improvedepth profile precisionVSAvoidmanufacturing process complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The continuous depth profile is segmented into discrete depth levels, transforming the manufacturing approach from creating a continuous variation to creating distinct stepped levels. This segmentation simplifies the manufacturing process while maintaining functional effectiveness in generating the required air cushion pressure distribution.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The depth profile parameter is changed from continuous to discrete, allowing the bearing surface to be manufactured with a finite number of depth levels rather than requiring continuous variation. This parameter change enables simpler manufacturing methods while preserving the essential function of pressure distribution.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If varying depth profiles are introduced into bearing surfaces, then the air cushion remains consistent and loadable at high rotational speeds, but the manufacturing complexity increases

Engineering Contradiction:
Improveair cushion consistencyVSAvoidbearing manufacturing ease
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The varying depth profile is segmented into discrete levels that can be manufactured using standard processes. These segmented depth levels maintain the air cushion consistency at high rotational speeds while being achievable through conventional manufacturing techniques rather than requiring complex continuous profiling.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Instead of implementing a full continuous depth profile, a partial approximation using discrete depth levels is employed. This partial action achieves sufficient air cushion consistency for high-speed operation without the excessive manufacturing complexity of a perfectly continuous profile.

Inventive Principle:
Principle #16Partial or excessive action

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 the production of aerodynamic bearings that maintain optimal pressure distribution and support higher rotational speeds through a simplified manufacturing process.

Implementation Method 1

an air cushion or gas cushion, respectively, for aerodynamic mounting is generatable between the bearing parts

Methodology Applied
Scientific EffectAir cushion: Air Lubrication

Implementation Method 2

a pressure distribution required for mounting is maintained on the bearing surfaces

Methodology Applied
Scientific EffectPressure distribution: Pressure Gradient

Data Source

PatentUS20250243901A1Aerodynamic bearing for axial and/or radial mounting of a shaft as well as methods of manufacture of such a bearing
Publication Date: 2025.07.31 EBM PAPST MULFINGEN GMBH & CO KG
  • US20250243901A1 patent drawing

AI summary

An aerodynamic bearing for axial and/or radial mounting of a shaft for a turbocompressor extending along an axis of rotation, wherein the aerodynamic bearing has a first bearing part denotable as a rotor, and a second bearing part denotable as a stator with respect to which the first bearing part is rotatable about the axis of rotation. The first bearing part and/or the second bearing part have a bearing surface facing the respective other bearing part and on which an air cushion for aerodynamic mounting is generatable between the bearing parts. The bearing surface has a plurality of depressions, each following a predetermined longitudinal profile on the bearing surface and arranged to form a predetermined pattern. The depressions each have, over their respective longitudinal profiles on the bearing surface, a varying depth which is determined by a depth profile restricted to a predetermined number of depth levels.