Axial Fan Blade Tip Member for Low-Noise Airflow

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Large industrial axial fans face challenges in reducing noise levels due to manufacturing limitations of extrusion and pultrusion techniques, which restrict shaping and result in increased blade dimensions and reduced rotation speed, failing to effectively minimize noise generation.

Innovation Solution

The design of a blade with a terminal member having a rounded front and rear portion, a tapered shape, and a lobe at the trailing edge, which reduces turbulence by modifying the air trajectory and overlapping with adjacent blades to deflect recirculating air, combined with a manufacturing process involving extrusion or pultrusion followed by cutting to achieve aerodynamic shaping.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If extrusion and pultrusion techniques are used to manufacture large fan blades, then cost-effectiveness and mechanical strength are improved, but the ability to shape blades for noise reduction is worsened

Engineering Contradiction:
Improvecost-effectivenessVSAvoidblade shaping capability
Core Design Contradiction:
Ease of manufactureVSShape

Solution Approach 1:

The blade is divided into two functional parts: an extruded/pultruded hollow structure providing mechanical strength and cost-effectiveness, and an aerodynamic skin layer providing noise-reducing shaping. This segmentation allows each part to fulfill its specific function optimally.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The blade combines a hollow structural core (from extrusion/pultrusion) with an aerodynamic skin layer, creating a composite structure that integrates both mechanical strength requirements and aerodynamic noise reduction requirements in a single component.

Inventive Principle:
Principle #40Composite materials

2Object-generated harmful factors

If blade rotation speed is reduced to decrease noise, then noise levels are improved, but airflow performance is worsened

Engineering Contradiction:
Improvenoise levelVSAvoidairflow performance
Core Design Contradiction:
Object-generated harmful factorsVSProductivity

Solution Approach 1:

The terminal member features rounded contours including a rounded leading edge, rounded trailing edge, and rounded tip end. These curved surfaces guide air flow smoothly around the blade tip, reducing turbulence and vortex formation that cause noise, while maintaining aerodynamic efficiency for airflow performance.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Productivity

If blade dimensions are increased to maintain airflow at reduced speed, then airflow performance is improved, but noise reduction effectiveness is worsened

Engineering Contradiction:
Improveairflow performanceVSAvoidnoise reduction effectiveness
Core Design Contradiction:
ProductivityVSObject-generated harmful factors

Solution Approach 1:

The aerodynamic skin layer with specific rounded contours is applied locally at critical areas (terminal member, leading edge, trailing edge) where turbulence generation is most significant. This localized aerodynamic treatment effectively reduces noise without requiring overall blade dimension changes.

Inventive Principle:
Principle #3Local quality

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

This solution significantly reduces noise levels by minimizing turbulence and vortices, achieving noise reduction comparable to moulding techniques while maintaining cost-effectiveness and mechanical strength, and is adaptable for large industrial fans.

Implementation Method 1

The rounding facilitates the circulation of air around the terminal member, thus reducing the turbulence. In particular, the angle of the trajectory of the leading point in relation to the air, is gradually modified around the tip side of the blade, avoiding sudden changes and the creation of vortices.

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS20240344525A1Blade for a low-noise industrial axial fan with terminal member, industrial axial fan and process for manufacturing a blade of an industrial axial fan
Publication Date: 2024.10.17 COFIMCO
  • US20240344525A1 patent drawing
  • US20240344525A1 patent drawing
  • US20240344525A1 patent drawing

AI summary

A blade for an industrial axial fan includes an extruded or pultruded airfoil, extending along a blade axis and having a leading edge, a trailing edge, a root side and a tip side, an intrados and an extrados. A terminal member is arranged to close the tip side and has a rounded front portion in a plan view at the leading edge and a rounded rear portion in a plan view between the front portion and the trailing edge.