Modular Fan Blade Pitch Setting via Recessed Ring

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Solution Overview

Problem

Conventional impellers, typically made from a single piece of material, require lengthy lead times and high costs due to the need for multiple design iterations and full re-manufacturing when airflow requirements change, as the pitch angle of their blades cannot be independently altered.

Innovation Solution

A modular impeller design comprising detachable blades and a pitch-setting ring with recesses that can be angled to provide specific pitch angles, allowing the hub and blades to be reused while only the ring is re-manufactured with new recesses to meet changing airflow requirements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If conventional single-piece impellers are used, then structural integrity is maintained, but lead time and manufacturing cost increase significantly due to full re-manufacturing for design iterations

Engineering Contradiction:
Improvelead timeVSAvoidimpeller structure
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The impeller is divided into separate modular components: a hub, multiple blades, and a pitch-setting ring. This segmentation allows individual components to be manufactured independently and assembled, enabling design iterations without re-manufacturing the entire impeller. The pitch-setting ring specifically can be modified to change blade pitch angles while reusing the hub and blades.

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If multiple design iterations are performed on single-piece impellers, then airflow requirements are met, but manufacturing cost increases due to full re-manufacturing

Engineering Contradiction:
Improveairflow requirementVSAvoidmanufacturing cost
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

By segmenting the impeller into modular components, the invention enables cost-effective design iterations. Only the pitch-setting ring needs to be re-manufactured with modified recess geometries to achieve different pitch angles, while the hub and blades can be reused. This dramatically reduces manufacturing cost compared to re-making entire single-piece impellers.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention enables parameter changes (pitch angle) by modifying the geometry of the recesses in the pitch-setting ring. Different recess shapes and orientations can be created in the ring to impart different pitch angles to the blades, allowing airflow optimization without re-manufacturing other components.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If pitch angle is fixed in conventional impellers, then manufacturing is simpler, but adaptability to different airflow requirements is reduced

Engineering Contradiction:
Improvepitch angleVSAvoidimpeller structure
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The pitch-setting ring provides dynamic adjustability of the pitch angle through its configurable recess geometry. The ring can be designed with different recess orientations and shapes to impart various pitch angles to the blades, enabling the impeller to adapt to different airflow requirements. This dynamic capability is achieved while maintaining relatively simple component structures.

Inventive Principle:
Principle #15Dynamics

4Loss of time

If modular impeller design is used, then lead time and cost are reduced, but structural integrity may be compromised

Engineering Contradiction:
Improvemanufacturing lead timeVSAvoidstructural integrity
Core Design Contradiction:
Loss of timeVSStrength

Solution Approach 1:

The modular design segments the impeller into components that are assembled together with fasteners or other joining mechanisms. This segmentation reduces manufacturing lead time and cost by enabling independent manufacturing and iteration of components. The design maintains structural integrity through proper joining methods and component interfaces that ensure reliable assembly.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10767500B2Fan blade pitch setting
Publication Date: 2020.09.08 GE AVIATION SYSTEMS LLC
  • US10767500B2 patent drawing
  • US10767500B2 patent drawing
  • US10767500B2 patent drawing

AI summary

There are provided techniques and apparatuses for fan blade pitch setting. For example, there is provided an impeller including a ring disposed in a hub of the impeller. The ring can include a recess shaped and positioned to impart a specified pitch angle to a blade extending outwardly from the ring through the hub.