Centrifugal Fan Wing Tab Airflow Guide Structure

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing centrifugal heat dissipation fans face challenges with insufficient air intake and wind pressure due to large air gaps between blades, leading to inefficient heat dissipation and potential air leakage, especially in thinner and lighter notebook computers.

Innovation Solution

The centrifugal heat dissipation fan incorporates a wing tab on each blade with an inclined surface adjacent to the flow inlet, guiding external airflow into the housing and preventing leakage by forming a guide structure that maintains airflow pressure until it exits.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If the flow inlet is increased to increase air intake, then the quantity of input air is improved, but air leakage occurs and wind pressure becomes insufficient

Engineering Contradiction:
Improveair intakeVSAvoidair leakage prevention
Core Design Contradiction:
Quantity of substanceVSReliability

Solution Approach 1:

The wing tab is added locally at the leading edge of the blade, creating a localized structural modification that addresses airflow control at the critical inlet region without requiring changes to the entire blade or housing structure

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The wing tab acts as an intermediary structure between the flow inlet and the blade, forming a guide structure that mediates airflow entry and prevents leakage by creating a controlled transition zone

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of manufacture

If the air gap between blades is increased for easier manufacturing, then the device complexity is reduced, but wind pressure becomes insufficient and heat dissipation efficiency decreases

Engineering Contradiction:
Improveblade assemblyVSAvoidwind pressure
Core Design Contradiction:
Ease of manufactureVSPower

Solution Approach 1:

The wing tab is positioned specifically at the leading edge region of the blade where it interacts with the flow inlet, creating a localized airflow control feature that enhances wind pressure generation without requiring modifications to the entire blade structure

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The wing tab extends in the radial direction from the blade surface, adding a dimensional feature that creates a three-dimensional guide structure for airflow, enhancing airflow control and pressure generation

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

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 design enhances air intake and wind pressure, improving heat dissipation efficiency while preventing air leakage, thus increasing the operational efficiency of the fan.

Implementation Method 1

the inclined surface of the wing tab can also cooperate with the flow inlet to form a guide structure that guides the airflow outside the housing into the housing

Methodology Applied
Scientific EffectFlow guidance:

Implementation Method 2

these wing tabs will provide a shielding effect for the inside of the housing, that is, the airflow that has been sucked into the housing can be continuously kept in the housing to be pressurized

Methodology Applied
Scientific EffectPressure maintenance:

Implementation Method 3

The impeller is rotatably assembled in the housing along an axial direction. The impeller has a hub and multiple blades arranged around the hub

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS11629725B2Centrifugal heat dissipation fan
Publication Date: 2023.04.18 ACER INC
  • US11629725B2 patent drawing
  • US11629725B2 patent drawing
  • US11629725B2 patent drawing

AI summary

A centrifugal heat dissipation fan including a housing and an impeller is provided. The housing has at least one flow inlet. The impeller assembled in the housing and rotating about an axial direction includes a hub and a plurality blades disposed around the hub. The flow inlet is located in the axial direction and faces the hub. Each of the blades has a wing tab next to the flow inlet, and the wing tab extends from a main surface of the blade to another blade. The wing tab has an inclined surface facing toward a periphery of the flow inlet along a radial direction of the impeller.