Fan Blade Platform Clevis Pin Support Integration

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Solution Overview

Problem

In gas turbine engines, the use of separate metal bushings to support pins for mounting fan blade platforms is cumbersome and increases weight, as these bushings require additional assembly and surface operations.

Innovation Solution

The method involves forming apertures in the clevises during machining and molding, eliminating the need for separate bushings by integrating support structures directly into the platform and hub, allowing direct pin attachment without additional assembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If separate metal bushings are used to support pins for mounting fan blade platforms, then the pin is supported and mounted, but the weight increases and additional assembly operations are required

Engineering Contradiction:
Improvepin supportVSAvoidfan blade weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent merges the bushing function directly into the clevis by forming an integrated bushing recess that receives a bushing as part of the single piece structure, eliminating the need for separate bushing assembly operations while maintaining the support function for the pin

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The bushing recess is formed during the molding process before final assembly, pre-positioning the bushing support structure within the clevis so that no additional assembly operations are needed later in the manufacturing process

Inventive Principle:
Principle #10Preliminary action

2Reliability

If separate metal bushings are assembled into apertures in the clevises, then the pin is supported, but the manufacturing complexity and assembly time increase

Engineering Contradiction:
Improvepin supportVSAvoidassembly complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The clevis and bushing support structure are merged into a single integrated component where the bushing recess is formed as part of the mold cavity, eliminating the need for separate bushing assembly steps and reducing manufacturing complexity

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The bushing support structure is pre-formed during the molding process, preparing the recess in advance so that the pin can be directly installed without requiring separate bushing assembly operations

Inventive Principle:
Principle #10Preliminary action

3Reliability

If separate metal bushings are used, then the pin is supported, but additional surface operations are required

Engineering Contradiction:
Improvepin supportVSAvoidmanufacturing process
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The bushing support function is merged into the clevis structure with the recess formed during molding, eliminating the need for separate surface preparation and bushing installation operations that would otherwise be required

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The bushing recess is pre-formed during the molding process, preparing the surface and structure in advance to receive the pin directly without requiring additional surface operations or separate assembly steps

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3080417B1Fan blade platform spacer mounting
Publication Date: 2023.03.15 RTX CORP
  • EP3080417B1 patent drawingFigure 1
  • EP3080417B1 patent drawingFigure 2A
  • EP3080417B1 patent drawingFigure 2B

AI summary

In a featured embodiment, a fan rotor comprises a platform. Clevises extend radially inwardly of the platform. Each clevis has an aperture. A hub has hub lugs positioned intermediate spaced ends of the clevises, and apertures. A pin extends through the apertures in the hub and the clevises to connect the platform to the hub. The apertures in the clevises are formed to have an inner surface for supporting the pin. A method of forming a fan blade platform is also disclosed.