Planetary Gear Carrier Welding After Ion-Nitrided Surface Machining

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Solution Overview

Problem

The manufacturing of planetary gear carriers through sintering often results in welding defects such as bubbles or cracks when different materials are joined, due to variations in sintering powder composition and material types, affecting the strength and quality of the components.

Innovation Solution

A method involving sintering of the front carrier cap with a controlled carbon content, forming an ion-nitrided layer on its surface, and performing dry machining on the welding portion to remove the ion-nitrided layer before laser welding, ensuring a defect-free joint with components made of different materials.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If sintering is used to manufacture the front carrier cap, then components with complicated shapes can be easily manufactured, but bubbles or cracks occur at welding portions when different materials are joined

Engineering Contradiction:
Improveease of manufactureVSAvoidwelding quality
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

An ion-nitrided layer is formed on the surface of the sintered front carrier cap before welding. This preliminary surface treatment modifies the surface properties to prevent bubbles or cracks during subsequent welding of different materials, while maintaining the ease of sintering manufacturing process

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The surface properties of the sintered front carrier cap are changed by forming an ion-nitrided layer. This changes the chemical composition and structure of the surface layer, making it more suitable for welding with different materials and preventing welding defects

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If sintering is used to manufacture the front carrier cap, then components with complicated shapes can be easily manufactured, but there is a large dispersion of welding quality depending on sintering powder composition

Engineering Contradiction:
Improveease of manufactureVSAvoidwelding quality consistency
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

By forming an ion-nitrided layer on the surface, the welding interface properties are standardized regardless of the underlying sintering powder composition. This surface treatment creates a consistent welding surface that reduces dispersion in welding quality

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The ion-nitrided layer acts as an intermediary between the sintered material (with varying compositions) and the welding process. This intermediate layer buffers the variations from different sintering powders, ensuring consistent welding quality

Inventive Principle:
Principle #24Intermediary (Mediator)

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 approach prevents welding defects like bubbles and cracks, enhancing the strength and quality consistency of the planetary gear carrier by ensuring a strong and reliable bond between the sintered carrier cap and other components during the laser welding process.

Implementation Method 1

Sintering is a method of manufacturing a product by heating and solidifying a powdered molded product

Methodology Applied
Scientific EffectSintering: Sintering

Implementation Method 2

an ion-nitrided layer forming step of forming an ion-nitrided layer on a surface of the sintered front carrier cap

Methodology Applied
Scientific EffectIon nitriding: Ion Implantation

Data Source

PatentUS20240359276A1Method of manufacturing planetary gear carrier
Publication Date: 2024.10.31 HYUNDAI TRANSYS INC
  • US20240359276A1 patent drawing
  • US20240359276A1 patent drawing
  • US20240359276A1 patent drawing

AI summary

A method of manufacturing a planetary gear carrier includes a sintering step of forming a front carrier cap by sintering, an ion-nitrided layer forming step of forming an ion-nitrided layer on a surface of the sintered front carrier cap, a welding portion machining step of machining a surface of a welding portion of the front carrier cap by a thickness of the formed ion-nitrided influence layer, and a welding step of welding a welding portion of the front carrier cap connected to a component with a different type of material different from a material of the front carrier cap so that the welding portion is joined to the component with the different type of material.