Conical Stator Blade Guide Grooves for Refiner Flow

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Solution Overview

Problem

The feed of material into the conical portion of refiners is limited due to large open volumes and changes in flow direction, leading to inefficiencies in material flow and potential blockages, especially in refiners with only a conical portion where no specific pressure is applied to promote flow.

Innovation Solution

Implementing guide grooves on the conical stator's refining surface at the feed zone, which minimizes blade element thickness, allowing for increased height of blade bars on the rotor and reducing wear, thereby enhancing material flow and guiding efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If shoulder-like guide elements are provided on the conical stator to guide material flow, then material flow guidance is improved, but the blade element thickness increases and wear resistance decreases

Engineering Contradiction:
Improvematerial flow guidanceVSAvoidwear resistance
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

Instead of adding protruding guide elements on the stator (which increases thickness and reduces wear resistance), the patent inverts the approach by creating guide grooves - recesses in the stator surface. These grooves provide guidance functionality while removing material rather than adding it, thus maintaining thinner blade elements with better wear resistance and longevity.

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The guide grooves create a textured surface structure on the stator that guides material flow through the groove geometry. This porous-like surface structure provides guidance functionality without requiring thick solid protrusions, allowing for thinner, more wear-resistant blade elements while maintaining effective material flow control.

Inventive Principle:
Principle #31Porous materials

2Productivity

If the blade element thickness is reduced to improve material flow, then production capacity increases, but the structural strength decreases

Engineering Contradiction:
Improveproduction capacityVSAvoidstructural strength
Core Design Contradiction:
ProductivityVSStrength

Solution Approach 1:

The patent transitions from using thick blade elements (one-dimensional thickness increase) to using groove geometry (two-dimensional surface feature). By moving the guidance function to the surface dimension rather than requiring volumetric thickness, the blade elements can be thinner and more wear-resistant while maintaining structural integrity through optimized groove design rather than mass addition.

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

3Reliability

If guide grooves are implemented instead of shoulder elements, then wear is reduced and guiding effectiveness is maintained longer, but manufacturing complexity increases

Engineering Contradiction:
Improveguiding effectiveness durationVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent replaces complex mechanical guide protrusions with simpler groove geometries that can be manufactured using standard machining processes. The groove structure achieves guidance through its geometric form rather than complex mechanical interlocking, reducing manufacturing steps and tooling requirements while extending component life by eliminating wear-prone protruding elements.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentEP2664709B1Blade element for a conical portion of a stator
Publication Date: 2018.11.28 VALMET TECH INC
  • EP2664709B1 patent drawingFigure 1~6
  • EP2664709B1 patent drawingFigure 3~5
  • EP2664709B1 patent drawingFigure 7

AI summary

A blade element (20) for a conical portion (4) of a stator (2) of a refiner (1). The blade element (20) comprises a feed end (24), a discharge end (25), and a refining surface (21) which comprises a feed zone (26) at the feed end (24) of the blade element (20). The feed zone (26) of the blade element (20) comprises at least one guide groove (29) extending from the feed end (24) towards the discharge end (25) for guiding a flow of material to be refined from the feed end (24) towards the discharge end (25). The depth of the guide groove (29) is arranged to change in a direction transverse in relation to the extending direction of the guide groove (29).