Two-Part Bearing Outer Ring for Balanced Turbine Load Transfer

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing structural subassemblies for gas turbine engines face challenges in uniformly transferring loads from bearings to support structures, often resulting in bending moments that can lead to inefficiencies and potential damage.

Innovation Solution

A structural subassembly with a two-part outer ring design, where each part is connected to the housing flange, ensuring symmetrical load transfer and minimizing bending moments by arranging the housing flange centrally between the connecting elements, thereby maintaining the center of mass in a plane perpendicular to the bearing's axis.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a unilateral connection of the outer ring to the housing flange is used, then the device complexity is reduced, but bending moments occur during load transfer

Engineering Contradiction:
Improvebearing connection structureVSAvoidload transfer uniformity
Core Design Contradiction:
Device complexityVSStrength

Solution Approach 1:

The outer ring is divided into two separate parts (first outer ring part and second outer ring part), each connected to the housing flange via its own connecting element. This segmentation allows the bearing to connect to the housing flange at multiple locations, distributing the load transfer path and eliminating bending moments by ensuring forces act through the center of mass.

Inventive Principle:
Principle #1Segmentation

2Strength

If the housing flange is arranged centrally between two connecting elements, then bending moments are avoided, but the device complexity increases

Engineering Contradiction:
Improvestructural integrityVSAvoidbearing assembly structure
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The two outer ring parts are merged with the housing flange through connecting elements that are integrated into the bearing assembly. This merging approach allows the load transfer paths to converge at the center of mass of the housing flange, achieving balanced force distribution while maintaining a compact, unified structure.

Inventive Principle:
Principle #5Merging (Combining)

3Strength

If a two-part outer ring design is implemented, then the contact area for frictional load transfer is increased, but manufacturing complexity increases

Engineering Contradiction:
Improvefrictional contact areaVSAvoidouter ring fabrication
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The outer ring is segmented into two parts that can be manufactured separately and then assembled. This segmentation enables the creation of larger total contact area with the housing flange while maintaining manufacturing feasibility through modular production and assembly of the divided components.

Inventive Principle:
Principle #1Segmentation

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

This design enhances load transfer efficiency by increasing the contact area for frictional load distribution, avoiding bending moments and ensuring uniform stress distribution, thus improving the structural integrity and performance of the gas turbine engine's support system.

Implementation Method 1

the contact area available for load transfer to the housing flange by friction is increased

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS11698006B2Structural assembly for a gas turbine engine
Publication Date: 2023.07.11 ROLLS ROYCE DEUT LTD & CO KG
  • US11698006B2 patent drawing
  • US11698006B2 patent drawing
  • US11698006B2 patent drawing

AI summary

A structural subassembly which has a bearing which comprises a statically arranged outer ring and a rotatably arranged inner ring, wherein the inner ring is connected for conjoint rotation to a component that is rotatable about a longitudinal axis or said inner ring forms part of such a component, and wherein the longitudinal axis defines an axial direction of the bearing. The structural subassembly furthermore comprises a housing flange of a support structure, to which flange the statically arranged outer ring is connected. Provision is made for the outer ring to be of two-part design, wherein each part of the outer ring has a connecting element which is connected to the housing flange, wherein the housing flange is arranged between the two connecting elements in the axial direction.