Diffuser-Type Endplate Propeller Cavitation Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current propeller designs, such as the contracted loaded tip (CLT) propeller, experience sheet cavitation phenomena at the endplate under inclined-shaft conditions, leading to increased resistance, vibration, and noise, which are detrimental to low-vibration and low-noise ship designs.

Innovation Solution

A diffuser-type endplate propeller design is introduced, where the endplate is shaped to prevent sheet cavitation by maintaining a negative angle of attack, reducing the likelihood of water flow from the high-pressure side to the low-pressure side, and optimizing the leading and trailing edge distances to minimize cavitation occurrence.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If a CLT propeller is used to prevent tip vortex and reduce blade load, then the load of blade-tips is suppressed, but sheet cavitation occurs at the endplate under inclined-shaft conditions, increasing resistance and vibration

Engineering Contradiction:
Improvetip vortex intensityVSAvoidsheet cavitation at endplate
Core Design Contradiction:
Object-affected harmful factorsVSObject-generated harmful factors

Solution Approach 1:

The endplate is designed with a diffuser shape where the trailing edge radius is greater than the leading edge radius, inverting the conventional CLT approach. This reverse geometry creates a negative angle of attack that prevents cavitation by directing flow away from the endplate outer surface, while still maintaining tip vortex suppression through the endplate's presence

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The invention changes the geometric parameters of the endplate by defining specific radius relationships (trailing edge radius > leading edge radius) and angle of attack conditions (negative angle). These parameter changes transform the endplate from a cavitation-prone structure to a cavitation-resistant diffuser that maintains aerodynamic efficiency

Inventive Principle:
Principle #35Parameter changes

2Loss of energy

If the endplate is contracted (CLT design) to follow the blade-tip cylindrical surface, then viscous resistance is reduced, but sheet cavitation is generated at the outer-sides of the endplate, reducing propeller efficiency

Engineering Contradiction:
Improveviscous resistanceVSAvoidpropeller efficiency
Core Design Contradiction:
Loss of energyVSProductivity

Solution Approach 1:

Instead of contracting the endplate to follow the blade-tip cylindrical surface, the invention inverts the approach by designing the endplate to diffuse outward (trailing edge radius > leading edge radius). This creates a negative angle of attack that eliminates the adverse pressure gradient causing cavitation, thereby maintaining propeller efficiency while still reducing viscous resistance through streamlined geometry

Inventive Principle:
Principle #13The other way round (Inversion)

3Adaptability or versatility

If a CLT propeller is applied to an inclined-shaft hull, then the propeller can be installed on speedboats, but severe sheet cavitation occurs at the endplate when the blade turns to the upper-vertical position, increasing noise and vibration

Engineering Contradiction:
Improveinclined-shaft installation capabilityVSAvoidsheet cavitation noise and vibration
Core Design Contradiction:
Adaptability or versatilityVSObject-generated harmful factors

Solution Approach 1:

The invention changes the operational parameters by maintaining a negative angle of attack throughout the rotation cycle through the diffuser geometry. This parameter change ensures that even when the blade turns to the upper-vertical position in inclined-shaft installations, the flow remains attached to the endplate surface, eliminating severe sheet cavitation and its associated noise and vibration

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The diffuser-type endplate inverts the conventional design by having the trailing edge extend further than the leading edge, creating a geometry that works advantageously under inclined-shaft conditions. This inverted shape maintains favorable pressure gradients throughout the rotation cycle, preventing cavitation-related noise and vibration while preserving inclined-shaft installation capability

Inventive Principle:
Principle #13The other way round (Inversion)

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

The diffuser-type endplate propeller effectively eliminates or significantly reduces sheet cavitation, enhancing propeller efficiency, reducing hull vibration and noise, and maintaining performance across various propeller blade positions.

Implementation Method 1

when a propeller blade rotates, there is a pressure difference existing between a high-pressure side-surface and a low-pressure side-surface of the propeller blade, and the pressure difference forms a thrust to make the ship proceed on the water surface

Methodology Applied
Scientific EffectPressure difference: Pressure Gradient

Implementation Method 2

the diffuser-type endplate propeller effectively eliminates or significantly reduces sheet cavitation

Methodology Applied
Scientific EffectCavitation: Cavitation

Data Source

PatentEP3508415B1Diffuser-type endplate propeller
Publication Date: 2021.12.01 HUNG SHEN PROPELLER CO LTD
  • EP3508415B1 patent drawingFigure 1
  • EP3508415B1 patent drawingFigure 2
  • EP3508415B1 patent drawingFigure 3A~3B

AI summary

A diffuser-type endplate propeller (100) driving a hull (20) and including a propeller hub (110) a plurality of blades (120) is provided. The propeller hub (110) has an axis (L) of rotation and is connected to a transmission shaft (22) of the hull (20). The blade (120) has a blade-body (122) and an endplate (124). The blade-body (122) is connected to the propeller hub (110) and extends outward from the propeller hub (110) to the corresponding endplate (124), the endplate (124) bends from the corresponding blade-body (122) to extend towards a stern (24) of the hull (20), and the endplate (124) has a leading edge (124a) and a trailing edge (124b). A cylindrical surface (S1) is imaginarily formed by the leading edges (124a) while the diffuser-type endplate propeller (100) is rotated about the axis (L). Each of the endplates (124) has a first tangent plane (C1) at the leading edge (124a) thereof, the cylindrical surface (S1) has a second tangent plane (C2) at the leading edge (124a). An included angle (α) is measured from the second tangent plane (C2) to the first tangent plane (C1).