Static Mixer Radial Vanes Exhaust Gas Mixing

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Solution Overview

Problem

Existing static mixers for exhaust gases in internal combustion engines face challenges in achieving effective mixing while minimizing pressure increases and condensate formation, leading to reduced efficiency and increased manufacturing complexity and costs.

Innovation Solution

A static mixer design featuring radial vanes with multiple bending lines and non-parallel impact surfaces, along with a free central portion, promotes turbulent flow and high nebulization of the reducing agent, reducing pressure increases and condensate formation, and can be manufactured through simple cutting and bending operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If a static mixer with vanes is used to promote mixing of exhaust gases with reducing agent, then mixing efficiency is improved, but pressure increase in the exhaust system worsens

Engineering Contradiction:
Improvemixing efficiencyVSAvoidpressure increase
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The vanes are designed with curved surfaces instead of flat planes, creating a three-dimensional configuration that promotes turbulent flow and mixing while maintaining smoother gas passage. The curved geometry allows the exhaust gases to follow the vane contours, reducing abrupt flow disturbances and pressure losses while still achieving effective mixing through controlled turbulence.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The invention transitions from traditional two-dimensional flat vane arrangements to three-dimensional curved vane structures with multiple bending lines. This dimensional enhancement creates complex flow patterns and multiple impact surfaces that improve mixing efficiency without proportionally increasing pressure drop, as the three-dimensional configuration optimizes flow guidance and reduces dead zones.

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

2Manufacturing precision

If the mixer surface area is increased to improve mixing, then mixing capability is improved, but condensate formation on the mixer surfaces worsens

Engineering Contradiction:
Improvemixing capabilityVSAvoidcondensate formation
Core Design Contradiction:
Manufacturing precisionVSObject-generated harmful factors

Solution Approach 1:

The curved surfaces of the vanes prevent liquid condensate from adhering and forming continuous films, as the liquid droplets follow the curved paths and are redistributed along the flow direction. This curvature effect reduces the effective surface area available for condensate accumulation while maintaining or enhancing mixing performance through improved flow turbulence and gas-liquid contact.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The invention converts the potential harmful effect of increased surface area (which would promote condensate formation) into a beneficial effect by using curved surfaces that actively prevent condensate accumulation. The same curved geometry that increases mixing capability also creates flow patterns that shed liquid films and redistribute condensate, turning what would be a disadvantage into an advantage.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

3Manufacturing precision

If complex vane arrangements are used to optimize mixing and reduce pressure increase, then mixing efficiency is improved, but manufacturing complexity and costs worsen

Engineering Contradiction:
Improvemixing efficiencyVSAvoidmanufacturing complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The complex three-dimensional vane structure is achieved through segmented manufacturing processes, where each vane is formed by sequential bending operations along multiple defined lines. This segmentation of the manufacturing process into discrete, repeatable steps (first bending line, second bending line, third bending line) allows complex geometries to be produced using standard sheet metal forming equipment, avoiding the need for complex molds or multi-component assemblies.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention achieves complex mixing performance through controlled changes in geometric parameters during the forming process. By defining specific bending lines and angular relationships (such as the radial arrangement of vanes and their convergence toward the center), the design translates simple flat sheet material into three-dimensional curved structures with optimized flow characteristics, maintaining manufacturing simplicity while achieving sophisticated mixing behavior.

Inventive Principle:
Principle #35Parameter changes

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 enhances mixing efficiency, reduces pressure increases, and simplifies manufacturing, making it suitable for various exhaust systems while maintaining cost-effectiveness.

Implementation Method 1

The static mixer promotes mixing of the gases with the reducing agent, generally thanks to the increase of the turbulence phenomenon within the exhaust gas flow

Methodology Applied
Scientific EffectTurbulence: Turbulence

Implementation Method 2

the surface of a mixer can cause condensation of the reducing mixture, with the consequent formation of a liquid film that adheres to the vanes

Methodology Applied
Scientific EffectCondensation: Condensation

Data Source

PatentEP2721265B1Static mixer for the treatment of exhaust gases and manufacturing method thereof
Publication Date: 2015.09.09 OFFICINE METALLURGICHE G CORNAGLIA
  • EP2721265B1 patent drawingFigure 1
  • EP2721265B1 patent drawingFigure 2
  • EP2721265B1 patent drawingFigure 3

AI summary

Static mixer (11) for the treatment of exhaust gases, comprising an annular support portion (13) and a plurality of substantially coplanar radial vanes (15) that are arranged radially with their rear portions or bases (17) associated with said support portion (13) and the front portions or radial tips (19a) converging towards the centre ("G") of the mixer, wherein the body of the vanes (15) comprises at least three lines of bending, which define respective portions (15a,15b,15c) arranged on non parallel planes and defining corresponding impact surfaces (A,B,C) for the exhaust gases.