Machining Dissimilar Materials in Shell and Sun Gear Assemblies

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Solution Overview

Problem

Conventional single-cut machining operations for dissimilar materials, such as in shell and sun gear assemblies, result in poor tool life and high scrap rates due to the damage caused by cutting through hard surfaces, leading to defects in the thrust face surface and increased costs.

Innovation Solution

A multiple-cut machining method involving a first chamfer cut to remove a portion of the hardest material and expose a chamfer surface, followed by a second cut along a path that avoids the hardest material, using different cutting tools tailored to the materials' hardness, thereby extending tool life and reducing waste and costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a single-cut machining operation is used to machine through dissimilar materials including hard surfaces, then the machining operation can be completed in one pass, but the tool life is poor and scrap rates are high due to tool damage from cutting hard material

Engineering Contradiction:
Improvemachining operation efficiencyVSAvoidtool life
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The single machining operation is divided into multiple sequential cuts. The first cut removes material down to just before the hard surface is reached, and the second cut completes the machining through the softer materials only. This segmentation allows each cutting tool to be optimized for its specific material, preventing tool damage from cutting hard material while maintaining overall productivity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The first cut is performed as a preliminary operation to remove the majority of material and expose the interface between hard and soft materials. This preliminary action prepares the workpiece for the second cut by eliminating the need for the second tool to contact the hard surface, thereby protecting the second tool and preventing scrap.

Inventive Principle:
Principle #10Preliminary action

2Device complexity

If a single cutting tool is used for the entire machining operation, then the process is simpler, but the tool suffers damage from cutting hard material resulting in high scrap rates

Engineering Contradiction:
Improvenumber of cutting toolsVSAvoidsurface quality and scrap rate
Core Design Contradiction:
Device complexityVSManufacturing precision

Solution Approach 1:

Different cutting tools with different properties are used for different sections of the machining operation. The first cutting tool is designed for cutting through harder materials, while the second cutting tool is optimized for softer materials and never contacts the hard surface. This local optimization of tool properties for each section prevents tool damage and ensures high surface quality.

Inventive Principle:
Principle #3Local quality

3Manufacturing precision

If the cutting path extends through the hardest material, then the complete thrust face surface is machined, but tool damage occurs leading to increased costs and downtime

Engineering Contradiction:
Improvethrust face surface qualityVSAvoidequipment downtime
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The cutting path is segmented into two separate operations. The first cut follows a path that stops before reaching the hard material interface, and the second cut follows a different path that goes through the soft materials only. This segmentation ensures that the second tool, which creates the final thrust face surface, never contacts the hard material, eliminating tool damage and associated downtime.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10315254B2Method of machining dissimilar materials
Publication Date: 2019.06.11 FORD MOTOR CO
  • US10315254B2 patent drawing
  • US10315254B2 patent drawing
  • US10315254B2 patent drawing

AI summary

Methods of machining a component including multiple dissimilar materials are disclosed. One method may include making a first cut in the component to remove at least a portion of a hardest material in the component and making a second cut in the component along a second cutting-path that does not include the hardest material. The first cut may expose a cut surface in the component and the second cut may extend through the cut surface. The cuts may be made using a turning operation and different cutting tools may be used for the first and second cuts. The hardest material may have a hardness of at least 50 HRC and the remaining materials may have a hardness of at most 45 HRC. The disclosed methods may be used to form a thrust face surface in a shell and sun gear assembly to extend tool life and reduce scrap.