Workpiece Composite Joining With Local Thickness Reduction

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Solution Overview

Problem

Existing methods for joining metal sheets with significant thickness differences or unfavorable material pairings, such as aluminum and steel, face challenges in thermal joining and require complex structural designs or joining methods, limiting the freedom of design in producing workpiece composites for mass production.

Innovation Solution

A method involving a thermal joining process where one workpiece is provided with an indentation at the joining portion to reduce thickness, allowing for reliable joining of workpieces with large thickness differences by creating a uniform thickness at the joining location, and optionally using a combination of welding and brazing to form an integral connection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If thermal joining methods are used to join metal sheets with great differences in thickness, then joining of workpieces with different thicknesses is achieved, but joining reliability deteriorates due to thermal distortion and material transfer issues

Engineering Contradiction:
Improvejoining of workpieces with different thicknessesVSAvoidjoining reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The invention applies preliminary action by creating an indentation in the thicker workpiece before performing the thermal joining process. This pre-prepared geometric feature compensates for the thickness difference, allowing the thinner workpiece to be properly positioned and joined without excessive thermal distortion or material transfer issues. The indentation is formed in advance to optimize the joining conditions.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention applies local quality by creating a localized thickness reduction (indentation) only in the specific joining region of the thicker workpiece, while the rest of the workpiece maintains its original thickness. This localized modification allows for reliable joining at the critical joining zone without compromising the overall structural integrity and thickness requirements of the workpiece.

Inventive Principle:
Principle #3Local quality

2Reliability

If complex structural design measures are used to achieve workpiece composites with specific local reinforcements, then joining feasibility is improved, but device complexity increases

Engineering Contradiction:
Improvejoining feasibilityVSAvoidstructural design complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The invention applies segmentation by dividing the workpiece into distinct regions: the main body with original thickness and the localized indentation region. This segmentation allows the thicker workpiece to maintain its overall strength while having a specific localized area prepared for joining, simplifying the design compared to complex structural measures.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention applies local quality by creating a localized thickness reduction only in the joining region, rather than modifying the entire workpiece structure. This localized approach simplifies the overall design while achieving the necessary joining feasibility, avoiding complex structural design measures.

Inventive Principle:
Principle #3Local quality

3Ease of manufacture

If conventional thermal joining is used without thickness reduction, then manufacturing simplicity is maintained, but susceptibility to edge cracking increases

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidsusceptibility to edge cracking
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The invention applies preliminary action by forming the indentation before the thermal joining process. This pre-prepared geometry reduces stress concentration at the joining zone during welding, thereby reducing susceptibility to edge cracking while maintaining manufacturing simplicity through an integrated process approach.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention applies preliminary anti-action by creating the indentation in advance to counteract the harmful effects of thermal distortion and stress concentration that would otherwise lead to edge cracking during the joining process. This preventive measure reduces cracking susceptibility before the actual joining occurs.

Inventive Principle:
Principle #9Preliminary anti-action

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

Enables reliable joining of workpieces with thickness differences greater than 0.6 mm, improves joining of difficult material pairings, reduces susceptibility to edge cracking, and allows for the use of previously unutilized weld forms, enhancing design freedom and reducing material transfer issues.

Implementation Method 1

In the case of welding, the material of the parts to be connected by a joining process is heated to above the liquidus temperature. The molten phases of the two workpieces mix and solidify after cooling to form an integral connection.

Methodology Applied
Scientific EffectWelding: Welding

Implementation Method 2

In the case of brazing, a molten phase is produced by melting a braze material. The workpieces themselves are not heated to above the liquidus temperature or are only melted superficially. As in the case of welding, an integral connection of the workpieces is produced after solidifying.

Methodology Applied
Scientific EffectBrazing: Brazing

Data Source

PatentUS11383329B2Method for producing a workpiece composite, and workpiece composite
Publication Date: 2022.07.12 BAYERISCHE MOTOREN WERKE AG
  • US11383329B2 patent drawing
  • US11383329B2 patent drawing
  • US11383329B2 patent drawing

AI summary

A workpiece composite and a method for producing the workpiece composite having at least two workpieces are provided. A first workpiece and a second workpiece are positioned relative to each other, and an integral connection between the end face of the first workpiece and the second workpiece is formed in a joint section by way of a thermal joining method. Prior to forming the integral connection, the first workpiece is provided with an indentation or embossing, which adjoins the end face, at least in the joint section, whereby the thickness of the first workpiece is reduced in the region of the end face.