Flow Equalization Air Ring Optimization for Coal Mill Aerodynamics

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Solution Overview

Problem

Existing methods struggle to accurately obtain aerodynamic characteristics and enhance the operational efficiency of flow equalization air ring structures in medium-speed coal mills, while also improving the computational speed and accuracy of their optimization.

Innovation Solution

A method and system utilizing Fluent simulation to optimize the aerodynamic characteristics of flow equalization air ring structures in medium-speed coal mills, involving modeling, meshing, setting boundary conditions, and iterative computation to achieve convergence, with features like a real gas model and multiple reference frame (MRF) rotating regions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional computation methods are used for aerodynamic optimization, then the process is simpler, but the accuracy and computational speed are insufficient

Engineering Contradiction:
Improveaccuracy of aerodynamic characteristicsVSAvoidcomplexity of computation method
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces traditional empirical and simplified computational methods with advanced CFD (Computational Fluid Dynamics) simulation technology. This substitution enables high-precision aerodynamic characteristic analysis by using numerical computation to solve complex fluid flow equations, achieving both high accuracy and computational efficiency that traditional methods cannot provide.

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

Solution Approach 2:

The patent implements parametric optimization by systematically varying geometric parameters of the air ring structure (such as hole diameter, hole distribution, ring thickness) and analyzing their effects on aerodynamic characteristics. This approach enables precise control and optimization of flow distribution patterns while maintaining computational efficiency through structured parameter studies.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If advanced simulation methods are used, then accuracy improves, but computation time and resource usage increase

Engineering Contradiction:
Improveaccuracy of aerodynamic characteristicsVSAvoidcomputation time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent segments the computational domain into structured mesh regions and divides the optimization process into systematic parameter studies. This segmentation allows the complex aerodynamic optimization problem to be broken down into manageable computational tasks that can be solved efficiently while maintaining high accuracy in critical flow regions.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent performs preliminary mesh generation and boundary condition setup before the actual aerodynamic simulation. By preparing the computational model in advance with optimized mesh structures and appropriate boundary conditions, the subsequent simulation runs require less computational time while maintaining high accuracy in predicting aerodynamic characteristics.

Inventive Principle:
Principle #10Preliminary action

3Manufacturing precision

If detailed meshing and iterative computation are used, then computation accuracy improves, but computational resources are consumed

Engineering Contradiction:
Improveprecision of flow field parametersVSAvoidcomputational resource usage
Core Design Contradiction:
Manufacturing precisionVSLoss of energy

Solution Approach 1:

The patent applies local mesh refinement in critical flow regions such as near the air ring holes and in the coal powder injection zone, while using coarser mesh in regions with less significant flow features. This local quality approach concentrates computational resources where they are most needed, achieving high precision in flow field parameters while reducing overall computational resource consumption.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS20260017439A1Methods and systems for optimizing aerodynamic characteristics of flow equalization air ring structures in medium-speed coal mills based on fluent simulation
Publication Date: 2026.01.15 DATANG DONGBEI ELECTRIC POWER TESTING & RES INST
  • US20260017439A1 patent drawing
  • US20260017439A1 patent drawing
  • US20260017439A1 patent drawing

AI summary

The present disclosure relates to a method and system for optimizing aerodynamic characteristics of a flow equalization air ring structure in a medium-speed coal mill based on Fluent simulation. The method comprises establishing and optimizing a model of the flow equalization air ring structure, meshing the model using Ansys ICEM, importing meshes, arranging an MRF rotating region on a dynamic ring structure, selecting an energy equation model, setting a DPM and a boundary condition, and adopting a modified mixture gas model based on empirical formulas for boundary conditions at an inlet and outlet, initializing computation information of a mesh node, setting a solver and performing iterative solving, after a computation result converges, performing post-processing on the computation result, storing the computation result, modifying structural parameters, and repeating the above steps to obtain a plurality of simulation results to obtain parameters of an optimal flow equalization air ring structure.