Segmented Propeller Hub Assembly for Portable Blowers

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Solution Overview

Problem

Existing propellers for portable blowers with pulsed airflow generators face challenges in manufacturing complex geometries, leading to high costs, fragility, and reduced performance due to the need for complex molds and increased space requirements, especially in smaller sizes where existing methods and equipment are inadequate.

Innovation Solution

A propeller design consisting of two coaxially attached parts, a front part with twisted blades and a rear conical part, assembled using a clamping device with a hub that ensures integral rotation, allowing for a simple manufacturing process that produces high-performance, small-sized propellers with optimized aerodynamics and reduced tooling costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If complex propeller geometries are manufactured using existing molding methods, then manufacturing precision can be achieved, but device complexity and tooling costs increase significantly

Engineering Contradiction:
Improvepropeller geometry precisionVSAvoidmold complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The propeller is divided into multiple segments or blades that can be manufactured separately using simpler molding processes, then assembled together. This avoids the need for complex single-piece molds while achieving the desired geometric precision through modular construction.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The propeller design incorporates nested structural elements where simpler geometric forms are combined to create the overall complex geometry. This allows manufacturing with less complex tooling by building complexity through assembly of nested components rather than requiring complex molds for the entire structure.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Volume of moving object

If propeller size is reduced for portable applications, then adaptability to portable devices is improved, but manufacturing precision and performance deteriorate

Engineering Contradiction:
Improvepropeller sizeVSAvoidsmall-size manufacturing precision
Core Design Contradiction:
Volume of moving objectVSManufacturing precision

Solution Approach 1:

By segmenting the propeller into modular blades that can be manufactured separately and assembled, the design achieves precise geometric control even at reduced sizes. This modular approach allows for better tolerance control and assembly precision compared to attempting to manufacture small complex propellers as single pieces with existing molding equipment.

Inventive Principle:
Principle #1Segmentation

3Ease of manufacture

If blade root radius is increased to simplify blade manufacture, then ease of manufacture is improved, but air inlet cone length and space requirements increase

Engineering Contradiction:
Improveblade manufacture simplicityVSAvoidair inlet cone length
Core Design Contradiction:
Ease of manufactureVSLength of stationary object

Solution Approach 1:

The propeller is segmented into blades with optimized root geometries that can be manufactured with standard tooling, eliminating the need for excessively large blade root radii. The segmentation allows each blade to be designed and manufactured independently with appropriate root dimensions, avoiding the need for long air inlet cones while maintaining manufacturing simplicity.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10001135B2Propeller of a pulsed airflow generator, in particular for a portable blower
Publication Date: 2018.06.19 PELLENC SA
  • US10001135B2 patent drawing
  • US10001135B2 patent drawing
  • US10001135B2 patent drawing

AI summary

A propeller of a pulsed airflow generator, in particular for a standalone portable blower, of the type made up of the assembly of two parts coaxially adjoining one another, i.e.: a first front part made as a single piece and comprising a plurality of twisted blades connected to a central ring, and a second rear part with a generally conical shape also made as a single piece, the central portion of said assembly having a conical shape and making up the rear portion of an air-inlet cone, said propeller being characterised in that said first and second rear parts are secured by a clamping device made up of a hub including two parts assembled coaxially and between which said two parts that make up the propeller are clamped, said hub being rotatably secured to the latter and maintaining said front and rear parts in the assembled position thereof.