Threaded Bearing Retainer Rings to Prevent Shaft Bearing Walking

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Solution Overview

Problem

Shaft bearings in turbomachines, such as gas turbine engines, often experience undesirable movement or 'walking' due to vibration and loading, necessitating a structure that prevents bearing movement while being easily manufactured and cost-effective.

Innovation Solution

A shaft bearing retainer assembly with a bearing and a bearing retainer subassembly, featuring first and second retainer rings with threaded engagements and a locking mechanism to secure the bearing in place, utilizing different thread pitches and locking mechanisms to inhibit relative rotation and maintain the bearing's position.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a bearing is mounted on a shaft without a retainer mechanism, then the structure is simple and manufacturing is easy, but the bearing experiences undesirable movement or walking due to vibration and loading

Engineering Contradiction:
Improvebearing stabilityVSAvoidretainer assembly structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The retainer assembly is segmented into multiple functional components: a retainer body with threaded engagement with the shaft, and a separate locking mechanism with locking elements. This segmentation allows each component to perform its specific function efficiently while maintaining overall simplicity of the assembly process.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The retainer body is preliminarily positioned and secured to the shaft via threaded engagement before the locking mechanism is applied. This preliminary action establishes the basic bearing retention, and the locking mechanism then reinforces this position to prevent walking during operation.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If a locking mechanism with multiple retainer rings is used to secure the bearing, then bearing stability is improved, but manufacturing complexity and cost increase

Engineering Contradiction:
Improvebearing position stabilityVSAvoidassembly manufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The locking mechanism is designed to be self-securing through threaded engagement and locking elements that automatically maintain bearing position without requiring external adjustment or monitoring systems. The structure itself provides the retention function.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Different thread pitches are used in the threaded engagement portions to optimize the mechanical characteristics of the retainer assembly. By varying thread parameters, the design achieves both secure retention and ease of assembly/disassembly.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If threaded engagements with different thread pitches are used in the retainer rings, then relative rotation is better inhibited, but manufacturing precision requirements increase

Engineering Contradiction:
Improverotation inhibitionVSAvoidthread pitch consistency
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

Different portions of the retainer assembly have different thread pitch characteristics optimized for their specific functions. The first threaded engagement portion has one pitch optimized for engagement with the shaft, while the second portion has a different pitch optimized for engagement with the retainer body, allowing each local region to have the quality needed for its purpose.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS12480546B2Shaft bearing retainer assembly
Publication Date: 2025.11.25 RTX CORP
  • US12480546B2 patent drawing
  • US12480546B2 patent drawing
  • US12480546B2 patent drawing

AI summary

A shaft bearing retainer assembly is provided that includes an axially extending shaft, a bearing, and a bearing retainer subassembly. The shaft has first and second radial surfaces, a distal end, a bearing seat, and a retainer cavity. The bearing seat is engaged with the first radial surface and extends axially inward from the distal end. The retainer cavity is disposed in the second radial surface of the shaft and extends axially inward from the distal end. The shaft includes a first threaded surface portion disposed in the retainer cavity and a second threaded surface portion in the second radial surface. The bearing has a race mounted in the bearing seat. The bearing retainer subassembly includes first and second retainer rings. The first retainer ring is in threaded engagement with the first threaded surface portion. The second retainer ring is in threaded engagement with the second threaded surface portion.