Self-Pressurizing Hydrodynamic Bearing for Rotary Machines

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Solution Overview

Problem

Rotary machines face significant challenges with axial thrust, axial oscillations, and radial oscillations, which affect their reliability and efficiency due to factors like wear in rotor seals and fluid dynamics, leading to premature bearing failure and instability.

Innovation Solution

A self-pressurizing hydrodynamic or aerodynamic bearing system is created using a stationary subdividing disc and a rotor, with peripheral vanes and restrictive means to alter flow dynamics, reducing axial thrust and radial oscillations by redirecting leakage flows and increasing pressure, thereby improving rotor stability and positioning precision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional rotor seal designs are used, then the machine can operate, but axial thrust increases and bearing reliability decreases due to leakage flow and pressure changes

Engineering Contradiction:
Improvebearing reliabilityVSAvoidaxial thrust
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The rotor seal is segmented into multiple restrictive means areas (first, second, third restrictive means) distributed around the periphery, each contributing to pressure control. This segmentation allows better management of leakage flow and pressure distribution, reducing axial thrust while maintaining reliability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A pre-dam area is introduced as an intermediary zone between the restrictive means and the dam area. This pre-dam area gradually builds up pressure before the main dam, creating a more controlled pressure transition that reduces axial thrust on the bearing

Inventive Principle:
Principle #24Intermediary (Mediator)

2Duration of action of moving object

If rotor seals wear out, then the machine continues to operate, but annular gap leakage flow increases causing higher axial thrust and premature bearing failure

Engineering Contradiction:
Improveoperational lifeVSAvoidaxial thrust
Core Design Contradiction:
Duration of action of moving objectVSObject-affected harmful factors

Solution Approach 1:

The design incorporates a pre-dam area that acts as a cushioning zone before the main dam. This pre-dam area gradually increases pressure in advance, compensating for wear in the rotor seals and maintaining pressure control throughout the operational life, preventing sudden increases in axial thrust

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The pressure distribution parameters are changed by introducing multiple restrictive means and a pre-dam area. This creates a progressive pressure build-up mechanism that adapts to seal wear over time, maintaining acceptable axial thrust levels throughout the operational life

Inventive Principle:
Principle #35Parameter changes

3Force

If axial thrust bearings are designed to handle high loads, then they can support the rotor, but the complexity and cost of maintenance increases

Engineering Contradiction:
Improveaxial load capacityVSAvoidbearing system complexity
Core Design Contradiction:
ForceVSDevice complexity

Solution Approach 1:

The invention converts the harmful leakage flow that causes axial thrust into a beneficial pressure-building mechanism. The leakage flow through the restrictive means and pre-dam area creates controlled pressure zones that actually reduce the net axial thrust on the bearing, allowing simpler bearing designs

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The rotor seal system with multiple restrictive means and pre-dam area creates a self-regulating pressure distribution that automatically compensates for operating conditions. This self-service mechanism reduces axial thrust without requiring complex external control systems or high-capacity bearings

Inventive Principle:
Principle #25Self-service

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 effectively reduces axial thrust and radial oscillations, enhancing the reliability and efficiency of rotary machines by minimizing the impact of wear and fluid-induced instability, allowing for closer tolerance seals and increased operational stability across a wide range of parameters.

Implementation Method 1

A self-pressurizing hydrodynamic or aerodynamic bearing system is created using a stationary subdividing disc and a rotor, with peripheral vanes and restrictive means to alter flow dynamics

Methodology Applied
Scientific EffectHydrodynamic:

Implementation Method 2

reducing axial thrust and radial oscillations by redirecting leakage flows and increasing pressure

Methodology Applied
Scientific EffectPressure increase: Pressure Increase

Implementation Method 3

for the purpose of changing the nature of the flow dynamics and the pressure distribution along the outside of the rotor

Methodology Applied
Scientific EffectFluid dynamics:

Data Source

PatentUS7731476B2Method and device for reducing axial thrust and radial oscillations and rotary machines using same
Publication Date: 2010.06.08 TECHNOLOGY COMMERCIALIZATION CORP
  • US7731476B2 patent drawing
  • US7731476B2 patent drawing
  • US7731476B2 patent drawing

AI summary

A method and apparatus to reduce the axial thrust in rotary machines such as compressors, centrifugal pumps, turbines, etc. includes providing additional peripheral restrictive means (7) attached at the peripheral portion of the disk forming the subdividing means (4) on the side facing the rotating rotor (2). An additional ring element at the periphery of the subdividing means forms additional radial (11) and axial restrictive means (15). Such peripheral restrictive means (7, 11 and 15) function as sealing dams, which combined with the outward flow induced by the rotating impeller, form self-pressurizing hydrodynamic bearings in the axial and radial planes, improving rotordynamic stability. Additionally, a stationary ring element in the center of the cavity forms a seal with the rotor, reducing leakage to suction.