Multi-Bearing Shaft Assembly with Eccentric Alignment and Damping

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Solution Overview

Problem

Maintaining alignment and operational efficiency of multiple bearings on a shaft in gas turbine engines is challenging due to tolerance variations, which complicates assembly and can lead to misalignment and increased vibrations.

Innovation Solution

A bearing assembly comprising a combination of hard-mounted and resiliently mounted bearings, including a fourth bearing with an eccentric outer race that can be adjusted to ensure proper alignment, along with a method of assembly that involves sequential mounting and adjustment to address radial offset, allowing for effective shaft alignment and reduced vibrations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple bearings are mounted on a shaft to maintain alignment and operational speed range, then the shaft alignment and operational efficiency are improved, but the assembly difficulty increases due to tolerance variations

Engineering Contradiction:
Improveshaft alignmentVSAvoidassembly difficulty
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent employs bearings with different mounting characteristics (hard-mounted vs. resiliently mounted) to change the operational parameters of the bearing assembly. This allows the system to accommodate tolerance variations while maintaining proper shaft alignment, resolving the contradiction between improved alignment and increased assembly difficulty.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

By incorporating resiliently mounted bearings with dampers, the patent introduces dynamic elements that can adapt to misalignment conditions. These resilient mountings allow for movement and adjustment, making the assembly process more forgiving of tolerance variations while maintaining operational alignment.

Inventive Principle:
Principle #15Dynamics

2Reliability

If multiple bearings are mounted on a shaft to maintain alignment, then the shaft alignment is improved, but the vibrations increase due to misalignment

Engineering Contradiction:
Improveshaft alignmentVSAvoidvibrations
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent introduces dampers as intermediary elements between the resiliently mounted bearings and the engine structure. These dampers act as mediators that absorb and reduce vibrations caused by misalignment, while still allowing the bearings to maintain proper shaft alignment through their resilient mounting.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent converts the potentially harmful effect of misalignment-induced vibrations into a benefit by using resiliently mounted bearings with dampers. These components are designed to absorb and dissipate vibration energy, transforming the harmful vibrational forces into controlled damping actions that protect the engine structure.

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

3Object-generated harmful factors

If a combination of hard-mounted and resiliently mounted bearings is used, then the vibrations are reduced, but the device complexity increases

Engineering Contradiction:
ImprovevibrationsVSAvoidbearing assembly complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The patent applies different mounting qualities to different bearings in the assembly - some are hard-mounted while others are resiliently mounted with dampers. This local differentiation allows vibration reduction at critical locations without requiring all bearings to be complex resilient mountings, thus balancing vibration control with overall system complexity.

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

The solution ensures proper alignment of the shaft, reduces vibrations, and maintains the shaft within desired operational speed ranges, enhancing the overall efficiency and reliability of the gas turbine engine.

Implementation Method 1

at least one second bearing mounted between the shaft and the static engine structure, wherein the at least one second bearing includes a damper

Methodology Applied
Scientific EffectViscous damping: Viscous Damping

Implementation Method 2

at least one third bearing mounted between the shaft and the static engine structure, wherein the at least one third bearing includes a resilient member in parallel combination with a viscous damper

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 3

at least one fourth bearing that is hard mounted directly between the shaft and the static engine structure, wherein the at least one fourth bearing includes an inner race that has a first centerline and an eccentric outer race that has a second centerline that is radially offset from the first centerline

Methodology Applied
Scientific EffectEccentric geometry: Eccentric

Data Source

PatentEP3748179B1Method and apparatus for mounting multiple bearings on a shaft
Publication Date: 2023.06.28 RTX CORP
  • EP3748179B1 patent drawingFigure 1
  • EP3748179B1 patent drawingFigure 2~3
  • EP3748179B1 patent drawingFigure 4~5

AI summary

A method and an apparatus includes a static engine structure, at least one shaft (40) that rotates relative to the static engine structure, and a bearing assembly (60) that supports the shaft (40). The bearing assembly (60) includes at least one first bearing (62) hard mounted directly between the shaft (40) and the static engine structure and at least one second bearing (64) mounted between the shaft (40) and the static engine structure. The at least one second bearing (64) includes a damper (116). Also included is at least one third bearing (66) that is mounted between the shaft (40) and the static engine structure, wherein the at least one third bearing (66) includes a resilient member (118).