Gas Turbine Bumper Cradle Mediator Design

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Solution Overview

Problem

Existing synchronizing assemblies in gas turbine engines face challenges in providing a low friction, wear-resistant, and cost-effective structure for variable stator vane actuation, particularly in maintaining accurate positioning and accommodating movement without preloading sensitive materials.

Innovation Solution

A synchronizing assembly featuring a cradle and bumper assembly where the cradle is secured to the synchronizing ring with fasteners, while the bumper is a composite material that projects outwardly and is not directly fastened, allowing for low friction and wear resistance without preloading the composite material, and is manufactured from sheet metal for cost-effectiveness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the bumper is made of composite material to reduce friction and wear, then wear resistance is improved, but the bumper becomes more sensitive to preloading and more expensive to manufacture

Engineering Contradiction:
Improvewear resistanceVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The cradle serves as an intermediary component between the synchronizing ring and the composite bumper. The cradle is secured to the synchronizing ring with fasteners that do not extend through the bumper, thereby protecting the composite bumper from preloading while still providing the necessary structural support and low-friction interface.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If fasteners extend through the bumper to secure it to the synchronizing ring, then the connection strength is improved, but the composite bumper is subjected to preloading that compromises its performance

Engineering Contradiction:
Improveconnection strengthVSAvoidbumper performance
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The cradle acts as a mediator that transfers the connection force from the synchronizing ring to the bumper without directly fastening the bumper itself. The fasteners attach to the cradle, not the bumper, eliminating preloading on the composite material while maintaining connection strength through the cradle structure.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If traditional bumper designs are used to provide a wear surface, then wear resistance is improved, but the structure becomes more complex and expensive to manufacture

Engineering Contradiction:
Improvewear resistanceVSAvoidstructure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bumper is constructed from composite material that inherently provides low friction and wear resistance properties. This eliminates the need for additional wear surfaces or complex structural features, simplifying the overall design while maintaining reliability.

Inventive Principle:
Principle #40Composite materials

Data Source

PatentUS9617869B2Bumper for synchronizing ring of gas turbine engine
Publication Date: 2017.04.11 RTX CORP
  • US9617869B2 patent drawing
  • US9617869B2 patent drawing
  • US9617869B2 patent drawing

AI summary

A synchronizing assembly for a gas turbine engine has a synchronizing ring. A bumper assembly has a cradle and a bumper held within the cradle. The cradle is secured to the synchronizing ring by at least one fastener without the fastener extending through the bumper. An engine is also disclosed.