Relief-Zone Bushing Geometry for Edge Load Wear Reduction

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Solution Overview

Problem

Traditional bushings with uniform inner diameters concentrate stress on the edges, leading to excessive wear and potential failure of the parent part, particularly in aircraft components like rotor mounts, due to end loading and elastic deformation during operation.

Innovation Solution

Incorporating edge relief zones into the bushing design, where the inner diameter is greater than the central diameter, helps distribute the load more evenly and reduces stress concentrations on the parent part, thereby extending its service life without adding weight or requiring redesign.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a bushing with uniform inner diameter is used, then the structure is simple and easy to manufacture, but stress concentrates on the edges leading to excessive wear and potential failure

Engineering Contradiction:
Improveservice life of parent partVSAvoidbushing structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bushing is designed with different inner diameters in different zones: a larger inner diameter in the relief zones at the ends and a smaller inner diameter in the central portion. This local variation in geometry redistributes the load from the edges to the central area, reducing stress concentration on the parent part while maintaining structural integrity.

Inventive Principle:
Principle #3Local quality

2Reliability

If edge relief zones are incorporated into the bushing design, then stress distribution is improved and wear is reduced, but the manufacturing process becomes more complex

Engineering Contradiction:
Improvedurability of aircraft componentsVSAvoidbushing manufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The bushing design varies the inner diameter parameter along its length, creating distinct zones with different dimensions. The relief zones have a larger inner diameter than the central portion, which changes the stress distribution pattern and reduces edge loading on the parent part while maintaining ease of manufacturing through standard machining or molding processes.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS20220135215A1Zoned contact bushing
Publication Date: 2022.05.05 TEXTRON INNOVATIONS INC
  • US20220135215A1 patent drawing
  • US20220135215A1 patent drawing
  • US20220135215A1 patent drawing

AI summary

There is disclosed in one example a mechanical assembly, including: a parent part including a parent part lug; a bushing to pass through the lug, the bushing comprising a central inner diameter, and respective left and right relief zones having a second inner diameter different from the central inner diameter; and a through-pin to pass through the bushing.