Rotatable Vertical Tail Wing for Ship Resistance Reduction

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Solution Overview

Problem

Conventional transport ships with large structures over the water line, such as pure car carriers and container ships, face challenges in reducing both air and underwater resistance while maintaining cargo-holding functionality, as existing solutions either neglect air resistance or increase underwater resistance when correcting for swinging moments caused by wind.

Innovation Solution

The design incorporates a nearly hollow semispherical bow shape to decrease air resistance, a vertically rising tail with a chimney to reduce underwater resistance, and a rotatable vertical tail wing to convert lift into thrust, addressing both air and underwater resistance effectively.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If a large structure is provided over the water line to hold cargos, then the cargo-holding function is improved, but the air resistance increases

Engineering Contradiction:
Improvecargo-holding volumeVSAvoidair resistance
Core Design Contradiction:
Volume of moving objectVSObject-affected harmful factors

Solution Approach 1:

The bow is formed in a hollow semispherical shape to streamline the airflow and reduce air resistance. The curved surface allows air to flow smoothly over the structure rather than creating turbulent eddies, thereby reducing the harmful aerodynamic forces while maintaining the necessary cargo volume.

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Stability of the object's composition

If the rudder is adjusted to correct the swinging moment caused by aslant head wind, then the ship's course stability is improved, but the underwater resistance increases

Engineering Contradiction:
Improvecourse stabilityVSAvoidunderwater resistance
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The vertical tail wing is positioned and shaped to preliminarily counteract the swinging moment before it fully develops. By having the vertical tail wing work as a flap or aileron on the front hinge, the ship can correct its course earlier and with less rudder adjustment, thereby reducing the underwater resistance associated with continuous rudder corrections.

Inventive Principle:
Principle #10Preliminary action

3Use of energy by moving object

If a vertical tail with rotatable wing is provided to convert lift into thrust, then the fuel consumption is reduced, but the device complexity increases

Engineering Contradiction:
Improvefuel consumptionVSAvoidvertical tail mechanism complexity
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The vertical tail structure serves multiple functions: it acts as a stabilizer, a rudder, and a wind-powered thrust generator. The rotatable vertical tail wing can function as a flap or aileron depending on the sailing conditions, allowing the same structure to address both stability and propulsion needs, thereby reducing overall device complexity despite the added rotational capability.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 significantly reduces air resistance and underwater resistance, facilitating easier navigation and cargo operations while maintaining energy efficiency and reducing fuel consumption.

Implementation Method 1

forming the structure over the water line in the upper bow portion in at least a nearly hollow semispherical shape, a nearly quarter-spherical shape, holding the bridge and the like in this portion to decrease the air resistance

Methodology Applied
Scientific EffectAerodynamic shaping: Drag

Implementation Method 2

decreasing the underwater resistance which was so far produced by the rudder adjustment (check helm), and decreasing the underwater resistance of the hull by, further, utilizing the wind force as a thrust relying upon the lift produced by the vertical tail wing

Methodology Applied
Scientific EffectLift: Aerofoil

Implementation Method 3

providing a vertical tail of a symmetrical shape in cross section on the stern incorporating the chimney of the engine therein, the vertical wing being rotatable and adjustable and, as required, the rear end thereof working as a flap or an aileron of the front hinge, and, further, adding the leading flap to the vertical tail to cancel the swinging moment imparted to the hull by the aslant head wind or the side wind

Methodology Applied
Scientific EffectHydrodynamic force: Drag

Data Source

PatentEP2123550B1Low-fuel-consumption transport ship
Publication Date: 2013.12.25 KYOKUYO SHIPYARD
  • EP2123550B1 patent drawingFigure 1~2A
  • EP2123550B1 patent drawingFigure 2B~4
  • EP2123550B1 patent drawingFigure 5~6

AI summary

Transport ships having a relatively large structure over the water line, such as a pure car carrier, container ship and a passenger ship tend to receive the air resistance during the sailing. When sailing aslant against the wind, check helm had to be effected so far to cancel the swinging moment causing an extra increase in the underwater resistance. A low-fuel-consumption transport ship of the invention has a structure over the water line, comprising the bow of a shape integral with the bridge of a hollow nearly semispherical to quarter-spherical shape or a partly cylindrical shape which is smoothly continuing to the stern to decrease the air resistance. The low-fuel-consumption transport ship further has a vertical tail incorporating a chimney and is rotatable on the uppermost stern deck to cancel the swinging moment in the air, without almost requiring check helm and, therefore, decreasing the underwater resistance.