UV Curable Resin Prepregs for Flexible Circuit Barrel Crack Reduction

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Solution Overview

Problem

Current flexible multilayer manufacturing processes for printed circuit boards using polyimide foil layers face issues such as reliability problems with plated through holes, inadequate metallization, and barrel cracks due to thermal expansion differences, and require complex and costly manual processing steps.

Innovation Solution

Replacing polyimide foil layers with prepregs comprising a UV curable resin layer and a thermally curable resin layer, where the UV curable resin is partially cured using a mask with transparent and opaque portions to control curing, and then laminated with a core layer under heat and pressure, resulting in a semi-flexible core that is not substantially bonded to the cured UV resin portion.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If polyimide foil layers are used in flexible multilayer manufacturing, then the laminate structure is formed, but reliability problems occur with plated through holes and barrel cracks due to thermal expansion differences

Engineering Contradiction:
Improvereliability of plated through holesVSAvoidmanufacturing process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent changes the material parameters by replacing polyimide foil with a composite prepreg system containing UV curable resin and thermally curable resin. The UV curable resin portion is cured before lamination to create a non-substantially bonded interface, reducing thermal expansion stress and eliminating barrel cracks while maintaining structural integrity

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention uses a composite prepreg material combining UV curable resin and thermally curable resin with semi-flexible core layers. This composite structure allows differential bonding behavior where the UV cured portion remains partially unbonded, creating a stress-relief interface that prevents reliability failures

Inventive Principle:
Principle #40Composite materials

2Reliability

If polyimide foil layers are used, then laminate structure is achieved, but plasma cleaning is required for plated through holes

Engineering Contradiction:
Improvemetallization qualityVSAvoidmanufacturing process simplicity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent changes the surface chemistry parameters by using UV curable resin that can be selectively cured to create bonding interfaces. This eliminates the need for plasma cleaning because the UV cured resin provides adequate surface preparation and adhesion without requiring additional plasma treatment steps

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If FR4 material layer is used instead of polyimide foil, then cost is reduced, but the layup can only be bent a few times before damage

Engineering Contradiction:
Improvematerial costVSAvoidflexibility
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The invention creates a composite structure using UV curable resin and thermally curable resin with semi-flexible core layers. The UV cured portion that is not substantially bonded to the core layer acts as a stress-relief interface, allowing the laminate to maintain flexibility and withstand repeated bending while using cost-effective materials

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies local quality by creating different bonding characteristics in different regions. The UV curable resin portion is cured to create a non-substantially bonded interface locally, while other portions maintain full bonding. This localized unbonded region provides flexibility and stress relief without compromising overall structural integrity

Inventive Principle:
Principle #3Local quality

4Manufacturing precision

If manual processing steps are used for flex-rigid laminates, then precise assembly is achieved, but manufacturing complexity and cost increase

Engineering Contradiction:
Improveassembly precisionVSAvoidnumber of processing steps
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent applies preliminary action by pre-curing the UV curable resin portion before the lamination process. This pre-curing creates a stable, non-substantially bonded interface that maintains precise alignment and positioning during subsequent lamination steps, eliminating the need for complex manual adjustment and PTFE inlay placement

Inventive Principle:
Principle #10Preliminary 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

This approach reduces reliability issues like barrel cracks and eliminates the need for plasma cleaning, simplifies the lamination process, and allows for the production of flexible multilayer laminates with improved peel strength and reduced manufacturing complexity.

Implementation Method 1

directing UV light at the mask for a period of time sufficient to cure the UV curable resin layer underlying the UV light transparent portion of the mask

Methodology Applied
Scientific EffectUV curing: Photopolymerisation

Implementation Method 2

applying heat and/or pressure to the lay-up to form a laminated layup

Methodology Applied
Scientific EffectThermal lamination: Heating

Data Source

PatentEP3164265B1A method for preparing a laminate sheet and its resulting products
Publication Date: 2023.09.20 ISOLA USA CORP
  • EP3164265B1 patent drawingFigure 1
  • EP3164265B1 patent drawingFigure 2~3
  • EP3164265B1 patent drawingFigure 4~6

AI summary

Prepregs (100) having a UV curable resin layer (102) located adjacent to a thermally curable resin layer (104) wherein the UV curable resin layer includes at least one UV cured resin portion (125) and at least one UV uncured resin (127) as well as methods for preparing flexible printed circuit boards using the prepregs.