Underwater Glider High-Wing Design for Stability

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Solution Overview

Problem

Existing underwater gliders face challenges in achieving balance and stability due to the conflicting hydrodynamic balance requirements, which can lead to instability and damage to equipment during transit and launch/recovery processes.

Innovation Solution

A high-wing design where the centerline of the wings extends above the body's centerline, providing continuous rise from attachment to the tip, enhancing stability and versatility, and allowing for safer mounting of sensors and equipment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional hydrodynamic balance requirements are applied to underwater gliders, then the vehicle can achieve forward motion, but the vehicle experiences instability and equipment damage during transit and launch/recovery

Engineering Contradiction:
Improvevehicle stabilityVSAvoidequipment damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent applies asymmetry by positioning the wings in a high-wing configuration where the wing centerline is above the body centerline, creating an asymmetric mass distribution that raises the center of gravity. This asymmetric design provides a stabilizing effect during transit and launch/recovery operations, preventing equipment damage while maintaining forward motion capability.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent moves the wings from a traditional side-mounted position to a high-wing position, effectively changing the vertical dimension of the vehicle's mass distribution. This dimensional change raises the center of gravity above the center of buoyancy, creating a stable configuration that resolves the contradiction between forward motion and vehicle stability.

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

2Reliability

If high-wing design is implemented, then vehicle stability and versatility are enhanced, but the hydrodynamic balance requirements become more complex

Engineering Contradiction:
Improvevehicle stabilityVSAvoidhydrodynamic balance requirements
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The high-wing asymmetric configuration inherently provides stability through its mass distribution, reducing the need for complex active balance control systems. The geometric asymmetry creates a natural stabilizing moment that simplifies the overall balance requirements while enhancing vehicle stability.

Inventive Principle:
Principle #4Asymmetry

3Device complexity

If wings are positioned at traditional height, then hydrodynamic balance is simpler, but vehicle stability and equipment protection are compromised

Engineering Contradiction:
Improvehydrodynamic balance requirementsVSAvoidvehicle stability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

By transitioning from a side-mounted wing configuration to a high-wing configuration, the patent changes the vertical positioning of the wings. This dimensional change raises the center of gravity, creating a stable mass-buoyancy relationship that enhances vehicle stability and equipment protection while maintaining manageable hydrodynamic balance requirements.

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

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 high-wing design improves stability and flexibility, protecting equipment during transit and launch/recovery, and enables more efficient use of space for additional instruments and power sources like solar panels, while maintaining effective lift and drag characteristics.

Implementation Method 1

A high-wing design provides stability and versatility for an underwater glider. In a high-wing design, a centerline of the wings extending from the sides of the body of the glider are located above a relative centerline of the body of the glider.

Methodology Applied
Scientific EffectCenter of gravity and center of buoyancy relationship: Gravitation

Data Source

PatentUS12110085B2Underwater glider
Publication Date: 2024.10.08 RON ALLUM DEEPSEA SERVICES PTY LTD
  • US12110085B2 patent drawing
  • US12110085B2 patent drawing
  • US12110085B2 patent drawing

AI summary

In an underwater glider, stability and versatility can be enhanced by the use of a high wing design. In a high wing design, a centerline of the wings extending from the sides of the body of the glider are located above a relative centerline of the body of the glider. The relative centerline of the wings may rise continuously from a region where the wings attach to the body to respective ends of the wings. In particular for a blended wing glider, a top surface of the glider is level in a line extending between ends of each wing.