Single-Screw Extruder With Segmented Barrier Flights for Complete Melting

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Solution Overview

Problem

Existing single-screw extruders face challenges in achieving optimal mass throughput and complete melting of materials due to issues such as solids crossing over the barrier flight, incomplete melting, and inefficient heat transfer, particularly in grooved-barrel extruders with high conveyance and pressure-building capacity.

Innovation Solution

A single-screw extruder design with non-overlapping barrier portions and overflow flights, combined with a grooved cylinder wall, allows solids and melt to cross over multiple stages, enhancing melting efficiency by increasing heat transfer and reducing pressure requirements, while maintaining stable conveyance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If a barrier screw with a single barrier flight is used to prevent solids from crossing over, then complete melting is achieved, but the conveyance capacity and throughput are reduced

Engineering Contradiction:
Improvemelting completenessVSAvoidconveyance capacity
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The single barrier flight is segmented into multiple successive non-overlapping barrier portions (first barrier portion, second barrier portion, etc.), each with its own overflow flight. This segmentation allows the system to maintain effective solids blocking while distributing the barrier function across multiple sections, preserving conveyance capacity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Grooves are introduced as intermediary structures in the cylinder wall between the barrier portions. These grooves facilitate controlled material flow and heat transfer, acting as mediators that enable complete melting without requiring a continuous solid barrier that would impede conveyance.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If the barrier gap is made smaller to prevent solids from reaching the screw tip, then melting completeness improves, but pressure requirements increase

Engineering Contradiction:
Improvemelting completenessVSAvoidpressure requirements
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The barrier function is distributed across multiple segmented barrier portions rather than relying on a single tight barrier. This allows each segment to have optimized gap dimensions that balance solids retention with pressure management.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The problem is shifted from a one-dimensional gap width adjustment to a multi-dimensional solution involving the axial distribution of multiple barrier portions, the helical geometry of overflow flights, and the three-dimensional groove structures in the cylinder wall.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Manufacturing precision

If multiple overlapping barrier portions are used to ensure complete melting, then solids blocking improves, but device complexity increases

Engineering Contradiction:
Improvesolids blocking effectivenessVSAvoidscrew geometry complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The barrier is divided into discrete non-overlapping portions arranged successively along the screw axis. This segmentation provides a modular structure that achieves complete solids blocking while maintaining manageable geometric complexity through clear spatial separation of functional zones.

Inventive Principle:
Principle #1Segmentation

4Manufacturing precision

If a long barrier is used to ensure complete melting, then solids retention improves, but the melting zone length increases reducing throughput

Engineering Contradiction:
Improvesolids retentionVSAvoidthroughput
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The long continuous barrier is segmented into multiple shorter non-overlapping barrier portions distributed along the screw. This achieves equivalent or superior solids retention through cumulative blocking effect while reducing the continuous barrier length that would impede material flow and reduce throughput.

Inventive Principle:
Principle #1Segmentation

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

The design achieves incremental melting with reduced pressure and shear stress, ensuring complete melting and improved throughput by breaking up the solids bed early and maintaining effective heat conduction, preventing unmelted solids from reaching the screw tip.

Implementation Method 1

the material being melted from the so-called solids bed is brought into heat-conducting contact with the temperature-controlled cylinder wall

Methodology Applied
Scientific EffectHeat conduction: Conduction (thermal)

Implementation Method 2

the resulting melt is displaced into the melt-filled region of the screw duct

Methodology Applied
Scientific EffectViscous heating: Viscous Heating

Data Source

PatentUS12403430B2Single-screw extruder
Publication Date: 2025.09.02 BATTENFELD CINCINNATI GERMANY GMBH
  • US12403430B2 patent drawing
  • US12403430B2 patent drawing
  • US12403430B2 patent drawing

AI summary

A single-screw extruder for conveying and plasticizing a meltable material, including a screw and a heated cylinder, wherein the screw is rotatably held in the heated cylinder, the screw has a core and a helical main flight, which is at a first distance from the internal wall of the cylinder, a region of a transition zone and a melting zone has at least two successive, non-overlapping barrier portions, and a cylinder-side outside flight surface of one or more overflow flights is chamfered in full or in part over a flight width such that a conical gap that gets narrower in an overflow direction is formed between the internal wall of the cylinder and the cylinder-side outside flight surface.