Bridle Sheave Roll Control for Airborne Wing Wind Adaptation

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Solution Overview

Problem

Existing airborne wind energy systems face challenges in accurately controlling the roll angle of airborne wings due to continuous variation with changing wind conditions, affecting power generation efficiency.

Innovation Solution

A bridle system with a roll control sheave and motor, connected to an electronic controller, adjusts the relative lengths of medial bridle segments to precisely control the roll of the airborne wing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the roll angle is allowed to vary continuously with wind conditions, then the system can adapt to changing wind conditions, but the control precision and stability of the roll angle deteriorates

Engineering Contradiction:
Improveadaptability to wind conditionsVSAvoidroll angle control precision
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent implements a dynamic roll control system where the bridle configuration can be actively adjusted in real-time. The roll control mechanism allows the bridle to transition between different configurations (symmetric and asymmetric) based on wind conditions, enabling the system to adapt dynamically while maintaining precise control through active management of the roll angle

Inventive Principle:
Principle #15Dynamics

2Measurement precision

If a roll control mechanism is implemented, then the roll control precision is improved, but the device complexity increases

Engineering Contradiction:
Improveroll control precisionVSAvoidbridle system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The roll control sheave serves multiple functions: it guides the bridle segments, provides the rolling motion necessary for roll control, and works in conjunction with the bridle configuration changes. This multi-functionality reduces the need for separate dedicated components, thereby limiting the increase in device complexity while achieving precise roll control

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

3Speed

If the bridle configuration is changed to control roll, then the roll control speed is improved, but the structural complexity of the bridle system increases

Engineering Contradiction:
Improveroll control speedVSAvoidbridle system complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The bridle is pre-configured with specific attachment points and segments (lateral and medial segments) that are positioned to enable rapid roll control. The roll control sheave is pre-positioned within the fuselage with grooves that guide the bridle segments, allowing the system to execute roll commands quickly without requiring complex real-time reconfiguration of the entire bridle structure

Inventive Principle:
Principle #10Preliminary action

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

Enables quick and accurate roll control of the wing, enhancing power generation efficiency by aligning lift forces with changing wind conditions.

Implementation Method 1

A roll control motor is preferably connected to the sheave and is controlled by an electronic controller to rotate and change the relative lengths of the medial bridle segments

Methodology Applied
Scientific EffectMechanical Advantage: Mechanical Advantage

Implementation Method 2

This rolling orients the lift force of the wing to balance other forces on the vehicle and generate required centripetal accelerations for turning

Methodology Applied
Scientific EffectAerodynamic Lift: Aerofoil

Data Source

PatentUS12473891B2Roll control for airborne wind energy system
Publication Date: 2025.11.18 WINDLIFT INC
  • US12473891B2 patent drawing
  • US12473891B2 patent drawing
  • US12473891B2 patent drawing

AI summary

A bridle system and roll control sheave for quickly and accurately directing the roll of an airborne wing in an airborne wind energy system is disclosed. A pair of medial bridle segments are connected to a sheave which is placed within the fuselage. A roll control motor is preferably connected to the sheave and is controlled by an electronic controller to rotate and change the relative lengths of the medial bridle segments.