Marine Propeller Fairing Structure for Flow Optimization

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Solution Overview

Problem

Existing marine propulsion systems face sub-optimal flow characteristics due to limitations in propeller assembly shape, leading to decreased efficiency and the need for more powerful drive systems.

Innovation Solution

A fairing structure is integrated into the propeller assembly, featuring retention members and a fairing platform with a radially outer surface designed to enhance fluid flow between blades, improving the flow coefficient by conforming to a determined platform profile.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If propeller assembly components are constructed using conventional methods with limited shape flexibility, then manufacturing complexity is reduced, but flow characteristics become sub-optimal and efficiency decreases

Engineering Contradiction:
Improvepropeller assembly efficiencyVSAvoidpropeller assembly structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The propeller assembly is divided into modular components including a central hub, multiple propeller blades, and a fairing structure with retention members. This segmentation allows each component to be optimized independently for flow characteristics while maintaining manufacturing feasibility through standardized assembly procedures.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A fairing structure is added as a dimensional enhancement to the propeller assembly, extending between retention members on the central hub. This additional structural element creates a three-dimensional flow management system that improves fluid dynamics without fundamentally redesigning the entire propeller assembly.

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

2Power

If propeller assembly shape is constrained by construction methods and material limitations, then manufacturing ease is maintained, but flow characteristics deteriorate requiring more powerful drive systems

Engineering Contradiction:
Improvedrive system powerVSAvoidpropeller assembly construction
Core Design Contradiction:
PowerVSEase of manufacture

Solution Approach 1:

The fairing structure implements local quality optimization by specifically addressing flow characteristics in the region between propeller blades. Rather than redesigning the entire propeller assembly, the fairing provides localized flow management where it is most needed, reducing overall power requirements while maintaining conventional manufacturing methods for the main components.

Inventive Principle:
Principle #3Local quality

3Productivity

If conventional propeller assembly design is used without fairing structure, then device complexity is minimized, but flow coefficient is sub-optimal

Engineering Contradiction:
Improveflow coefficientVSAvoidfairing structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The fairing structure acts as an intermediary element between the central hub and the propeller blades, managing fluid flow in the inter-blade region. This mediator component improves flow characteristics by controlling the fluid path without requiring direct modification of the hub or blade structures, thus maintaining relative simplicity while enhancing performance.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS10633067B2Method and system for improving flow characteristics in marine propellers
Publication Date: 2020.04.28 GENERAL ELECTRIC CO
  • US10633067B2 patent drawing
  • US10633067B2 patent drawing
  • US10633067B2 patent drawing

AI summary

A propeller assembly is provided. The propeller assembly includes a central hub including a forward end, an aft end, and a hub body extending therebetween along an axis of rotation of the central hub. The propeller assembly further includes a first retention member including a first radial interference member, the first retention member coupled to the forward end of the central hub and a second retention member including a second radial interference member, the second retention member coupled to the aft end of the central hub. The propeller assembly also includes a fairing platform extending between the first retention member and the second retention member, wherein the fairing platform is retained by the first radial interference member and by the second radial interference member.