Hydrofoil Negative Lift Control for Stable Seaglider Transition

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Solution Overview

Problem

Wing-in-ground effect (WIG) crafts face challenges in transitioning from hydrofoil-borne to wing-borne mode due to insufficient aero lift and hydrofoil lift, leading to premature takeoff failures and stall conditions, especially when trying to avoid water collisions and operate in rough seas or crowded harbors.

Innovation Solution

The implementation of a control system that adjusts hydrofoil lift to maintain the craft partially submerged until sufficient aero lift is generated, allowing for controlled transition to wing-borne mode by introducing negative lift via the hydrofoil and gradually releasing it to facilitate takeoff, while also using distributed propulsion and advanced control surfaces for stabilization and maneuverability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the craft transitions from hydrofoil-borne to wing-borne mode, then the craft can achieve sustained flight, but insufficient aero lift and hydrofoil lift cause premature takeoff failures and stall conditions

Engineering Contradiction:
Improvetakeoff reliabilityVSAvoidaero lift
Core Design Contradiction:
ReliabilityVSForce

Solution Approach 1:

The control system performs preliminary action by adjusting hydrofoil lift before the actual takeoff transition. The system maintains the craft partially submerged in water while building sufficient aero lift, then gradually releases hydrofoil support to facilitate a controlled transition to wing-borne mode, preventing premature takeoff failures and stall conditions

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The control system continuously monitors lift forces and adjusts hydrofoil configuration in real-time based on feedback from sensors. This closed-loop control ensures that the craft maintains adequate lift throughout the transition process, adapting to changing aerodynamic and hydrodynamic conditions to prevent stall conditions

Inventive Principle:
Principle #23Feedback

2Stability of the object's composition

If the hydrofoil maintains the craft fully submerged, then the craft has stable hydrofoil-borne operation, but the craft cannot transition to wing-borne mode due to insufficient aero lift

Engineering Contradiction:
Improvehydrofoil-borne stabilityVSAvoidmode transition capability
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The system transitions from a static hydrofoil configuration to a dynamic, adjustable configuration. The control system modifies hydrofoil lift characteristics in real-time, enabling the craft to adapt from stable hydrofoil-borne operation to wing-borne mode transition, combining stability with versatility

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The control system changes key operational parameters of the hydrofoil, including lift magnitude and distribution, to enable mode transition. By adjusting hydrofoil parameters from maintaining full submersion to gradual release, the system enables transition while maintaining stability throughout the process

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If the craft operates in rough seas or crowded harbors, then the craft can avoid water collisions and operate in challenging environments, but the transition from hydrofoil-borne to wing-borne mode becomes more difficult due to wave interference

Engineering Contradiction:
Improveenvironmental adaptabilityVSAvoidcontrol system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The control system uses feedback from sensors to monitor wave conditions and craft attitude, continuously adjusting hydrofoil lift to compensate for wave interference. This real-time adaptation enables operation in rough seas and crowded harbors while managing the increased complexity through intelligent control algorithms

Inventive Principle:
Principle #23Feedback

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 approach enables WIG crafts to achieve sustained flight by ensuring adequate aero lift before leaving the water, preventing premature takeoff and stall conditions, and allowing operation in challenging environments like rough seas and crowded harbors with reduced passenger discomfort.

Implementation Method 1

adjusts hydrofoil lift to maintain the craft partially submerged until sufficient aero lift is generated

Methodology Applied
Scientific EffectHydrodynamic lift: Aerofoil

Implementation Method 2

allowing for controlled transition to wing-borne mode by introducing negative lift via the hydrofoil and gradually releasing it to facilitate takeoff

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Data Source

PatentUS12116139B2Hydrofoil equipped seaglider takeoff
Publication Date: 2024.10.15 REGENT CRAFT INC
  • US12116139B2 patent drawing
  • US12116139B2 patent drawing
  • US12116139B2 patent drawing

AI summary

A craft includes a hull, a wing, a hydrofoil, and a control system. The wing is configured to generate upwards aero lift as air flows past the wing to facilitate wing-borne flight of the craft. The hydrofoil is configured to generate upwards hydrofoil lift during a first mode of operation as water flows past the hydrofoil to facilitate hydrofoil-borne movement of the craft through the water. While the craft is hydrofoil-borne, the control system is configured to determine the upwards aero lift generated by the wing. The control system is further configured to control the hydrofoil to generate downwards hydrofoil lift to counteract the upwards aero lift generated by the wing that maintains the hydrofoil at least partially submerged in the water while the determined upwards aero lift is below a threshold lift.