Self-Aligning Foil Bearing for Gas Turbine Misalignment

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Solution Overview

Problem

Existing foil bearing systems for gas turbine engines face challenges in effectively handling misalignment, which affects their performance and reliability.

Innovation Solution

A self-aligning foil bearing system that includes a foil bearing, a housing, a fulcrum, and axial springs, which aligns with the axis of rotation and provides radial frictional damping to maintain a hydrodynamic air film, preventing contact between the rotor and the foil bearing during operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If existing foil bearing systems are used, then the structure is simple, but misalignment handling capability is poor

Engineering Contradiction:
Improvemisalignment handling capabilityVSAvoidbearing system structure
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The bearing system incorporates a compliant housing that can dynamically adjust its orientation to accommodate misalignment between the rotor and stator. The housing acts as a flexible element that bends and rotates to maintain optimal bearing alignment, transforming a static rigid structure into a dynamic adaptive system that self-adjusts to misalignment conditions

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

A fulcrum is introduced as an intermediary pivot point between the bearing housing and the engine structure. This fulcrum enables the housing to rotate and adjust its angle relative to the stator, serving as a mechanical mediator that decouples the rigid mounting structure from the flexible bearing alignment requirements

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If rigid bearing housings are used, then manufacturing is easy, but alignment adjustment capability is limited

Engineering Contradiction:
Improvealignment adjustment capabilityVSAvoidhousing manufacturing
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The bearing housing is designed as a thin-walled compliant structure that can elastically deform and bend to accommodate misalignment. This flexible shell approach allows the housing to act as a spring element, absorbing angular deviations through elastic deformation while maintaining structural integrity and supporting bearing loads

Inventive Principle:
Principle #30Flexible shells and thin films

3Reliability

If misalignment is not properly handled, then the system remains simple, but reliability deteriorates

Engineering Contradiction:
Improvebearing system reliabilityVSAvoidalignment compensation mechanism
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bearing system is designed to self-align and self-adjust to misalignment conditions without requiring external control systems or complex adjustment mechanisms. The compliant housing automatically bends and rotates to maintain optimal bearing alignment, and the fulcrum provides automatic pivot point functionality, enabling the system to service its own alignment requirements through passive mechanical compliance

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 system effectively transmits rotor loads and maintains alignment, reducing wear and stress, and providing Coulomb damping to manage vibratory loads, thereby enhancing the operational stability and efficiency of gas turbine engines.

Implementation Method 1

provides radial frictional damping to maintain a hydrodynamic air film, preventing contact between the rotor and the foil bearing during operation

Methodology Applied
Scientific EffectHydrodynamic air film: Air Lubrication

Implementation Method 2

provides radial frictional damping to maintain a hydrodynamic air film

Methodology Applied
Scientific EffectFrictional damping: Friction

Implementation Method 3

providing Coulomb damping to manage vibratory loads

Methodology Applied
Scientific EffectCoulomb damping: Coulomb Damping

Data Source

PatentUS9657594B2Gas turbine engine, machine and self-aligning foil bearing system
Publication Date: 2017.05.23 ROLLS ROYCE CORP
  • US9657594B2 patent drawing
  • US9657594B2 patent drawing
  • US9657594B2 patent drawing

AI summary

One embodiment of the present invention is a unique gas turbine engine. Another embodiment is a unique machine. A further embodiment is a unique self-aligning foil bearing system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for machines and self-aligning foil bearing systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.