Cyclone Vortex Finder Vanes for Low-Turbulence Outlet Flow

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Solution Overview

Problem

Cyclonic separators face challenges in minimizing pressure drop and turbulence at the outlet, which affects air flow and separation efficiency, while also allowing debris to escape through the outlet.

Innovation Solution

A vortex finder with radially spaced stationary vanes is designed, where air flows over the outer surface of each vane and is redirected through gaps between vanes, creating an overpressure region that reduces turbulence and minimizes pressure drop by shaping the vanes to direct air inwardly and impact on adjacent vanes, forming an arcuate surface to maintain smooth flow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a vortex finder is used to stabilize rotational flow and improve separation performance, then separation efficiency is improved, but pressure drop increases and air flow is restricted

Engineering Contradiction:
Improveseparation efficiencyVSAvoidpressure drop
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The vortex finder is segmented into multiple stationary vanes (at least three) spaced radially around the axis. This segmentation allows the air flow to be divided into multiple paths, with portions of air redirected through gaps between adjacent vanes, reducing the overall resistance and pressure drop compared to a solid vortex finder structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The outer surface of each vane features a specific geometric configuration where a portion lies on a circle centered coaxial with the axis, and another portion extends inwardly toward the leading edge. This local geometric variation creates regions of overpressure that reduce turbulence at leading edges, optimizing flow characteristics locally while maintaining overall low pressure drop.

Inventive Principle:
Principle #3Local quality

2Productivity

If the vortex finder design reduces pressure drop to increase air flow, then air flow is improved, but turbulence increases and separation performance deteriorates

Engineering Contradiction:
Improveair flowVSAvoidturbulence
Core Design Contradiction:
ProductivityVSObject-generated harmful factors

Solution Approach 1:

The vanes are designed with specific local geometric features where the outer surface extends inwardly toward the leading edge, creating localized overpressure regions. These local pressure zones act to suppress turbulence at critical locations (leading edges) while allowing the overall air flow to remain high due to the open vane structure.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The outer surface of each vane incorporates curved geometries, with portions lying on circles and extending inwardly in arcuate paths. These curved surfaces guide air flow smoothly over the vanes, reducing flow separation and turbulence generation while maintaining the low pressure drop characteristics of the segmented vane structure.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Reliability

If the vortex finder stabilizes rotational flow to prevent debris exit, then separation performance is improved, but the structure becomes more complex

Engineering Contradiction:
Improveseparation performanceVSAvoidvortex finder structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The vortex finder is divided into multiple discrete stationary vanes rather than using a solid or continuously complex structure. This segmentation achieves flow stabilization through the radial spacing and interaction of multiple simple vane elements, reducing manufacturing complexity compared to monolithic complex designs.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Instead of using a solid central structure that extends downward (conventional approach), this invention uses multiple radial vanes extending upward from the outlet end. This inverted configuration achieves similar flow stabilization功能的 with simpler, more manufacturable components that are easier to clean and maintain.

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

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 solution effectively reduces turbulence and pressure drop, enhancing air flow and separation performance while preventing debris from exiting through the outlet, thereby improving the overall efficiency of the cyclonic separator.

Implementation Method 1

Cyclonic separators rely on rotational effects to separate solids entrained in a fluid flow without using a filter. When debris laden air enters the cyclone chamber via the inlet, a rapidly rotating flowing air flow or vortex is established within the cyclone chamber. Centrifugal force generated by the circular air flow throws the dust particles towards the wall of the cyclone chamber

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

a portion of the outer surface of each vane extends inwardly away from the circle towards the leading edge of the vane so that the leading edge of each vane about which air is redirected through the gap between vanes is located within a region bound by said circle. At least some air flowing across a vane follows its outer surface and so is directed inwardly and towards the surface of the next vane where it impacts to create a region of overpressure that reduces the degree of turbulence

Methodology Applied
Scientific EffectFlow redirection and pressure gradient: Pressure Gradient

Data Source

PatentUS10016768B2Vortex finder for a cyclonic separator
Publication Date: 2018.07.10 VERSUNI HLDG BV
  • US10016768B2 patent drawing
  • US10016768B2 patent drawing
  • US10016768B2 patent drawing

AI summary

A vortex finder (18,27,40) for a cyclonic separator (1) through which air flowing in a helical path ‘D’ about an axis A-A of a cyclone chamber (4) passes to an outlet (6) is disclosed. The vortex finder comprises a plurality of stationary overlapping vanes (13,19) extending in an axial direction and spaced radially around said axis ‘A’, the vanes (13,19) being positioned relative to each other so a helical flow of air about the axis of the cyclone chamber (4) passes over an outer surface (16) of the vanes (13,19) with a portion of the air flow being redirected around a leading edge (14) of each vane (13,19) and through a gap between adjacent vanes (13,19) to the outlet (6). At any point along the axis, a portion of an outer surface (16,20,30,46) of each vane (13,19,28,41) lies on a circle having its center coaxial with said axis, the outer surface (16,20,30,46) of each vane (13,19,28,41) having a portion leading towards the leading edge (14,33,47) that extends inwardly away from the circle so that the leading edge (14,33,47) of each vane (13,19,28,41) about which air is redirected through the gap between vanes (13,19,28,41) is located within a region bound by said circle to create a region of overpressure on the outer surface (16) of the adjacent vane (13,19) in the vicinity of the gap.