Wing Foil Leading-Edge Spoiler Profile for Lift and Stability

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Solution Overview

Problem

Existing wing rigs and kites for wind-powered sports suffer from high weight, complex construction leading to time-consuming assembly/disassembly, risk of injury, and suboptimal aerodynamics, with handling adjustments being difficult due to standard hand loops.

Innovation Solution

Incorporation of a radially projecting spoiler profile along the leading edge of the wing rig and kite, designed to induce flow separation, improving aerodynamics and handling by enhancing lift and stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a complex tubular structure is used for the leading edge and boom, then the wing rig achieves structural strength, but the overall weight becomes very high

Engineering Contradiction:
Improvestructural strengthVSAvoidoverall weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent replaces the complex rigid tubular structure with an inflatable leading edge tube that has a spoiler profile. The inflatable tube uses a flexible membrane structure that can maintain aerodynamic shape and structural integrity while being significantly lighter than rigid tubing. The spoiler profile on the inflatable tube provides the necessary aerodynamic function without requiring heavy internal support structures.

Inventive Principle:
Principle #30Flexible shells and thin films

2Stability of the object's composition

If a complex tubular structure is used for the leading edge and boom, then the wing rig achieves structural integrity, but assembly and disassembly become time-consuming

Engineering Contradiction:
Improvestructural integrityVSAvoidassembly time
Core Design Contradiction:
Stability of the object's compositionVSLoss of time

Solution Approach 1:

The inflatable leading edge tube with integrated spoiler profile can be quickly inflated to assume its structural form, eliminating the need for complex assembly of rigid tubular sections. The flexible membrane structure with integrated spoiler eliminates multiple connection points and joints that would require time-consuming assembly and disassembly operations.

Inventive Principle:
Principle #30Flexible shells and thin films

3Strength

If rigid tubing is used for the leading edge and boom, then structural strength is achieved, but the risk of injury to the user increases

Engineering Contradiction:
Improvestructural strengthVSAvoidinjury risk
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The inflatable leading edge tube replaces rigid tubing with a flexible, air-filled structure that maintains aerodynamic shape while being inherently safer for users. The flexible membrane can deform upon impact rather than causing injury, eliminating the hazard of rigid tubes striking the user during catapult falls or other accidents.

Inventive Principle:
Principle #30Flexible shells and thin films

4Device complexity

If a standard hand loop configuration is used, then the wing rig achieves simple construction, but grip position adjustments become difficult

Engineering Contradiction:
Improveconstruction simplicityVSAvoidgrip adjustment ease
Core Design Contradiction:
Device complexityVSEase of operation

Solution Approach 1:

The patent makes the grip position adjustable by providing multiple hand loop positions along the inflatable leading edge tube. Users can dynamically reposition their hands along the tube to optimize grip location for different maneuvers and wind conditions, transforming the static hand loop configuration into a dynamic, adaptable system.

Inventive Principle:
Principle #15Dynamics

5Weight of moving object

If an inflatable center strut is used, then low weight and high lift are achieved, but aerodynamic performance does not meet higher requirements

Engineering Contradiction:
ImproveweightVSAvoidaerodynamic performance
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The patent applies a spoiler profile specifically to the leading edge tube where it is most needed for aerodynamic performance. The spoiler profile creates controlled flow separation at the leading edge, improving lift and aerodynamic efficiency in the critical front section of the wing rig while maintaining the lightweight inflatable construction throughout the rest of the structure.

Inventive Principle:
Principle #3Local quality

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 spoiler profile significantly improves performance by increasing lift, simplifying grip adjustments, and enhancing roll and pitch stability, allowing for higher speeds and stable maneuvering.

Implementation Method 1

a radially projecting profile lip, hereinafter referred to as a spoiler profile, is formed in the area of the leading edge and extends along a portion of the leading edge/leading edge approximately transversely to the center strut. This spoiler profile is preferably designed such that flow separation occurs in the area it covers.

Methodology Applied
Scientific EffectFlow separation: Flow Separation

Implementation Method 2

a (hand-supported) wing rig for wind-powered sports, for example foil surfing, with an inflatable leading edge leading tube (6) and a rigid or inflatable center strut (20)

Methodology Applied
Scientific EffectInflation pressure: Pressure Increase

Data Source

PatentEP4323272B1Wing foil and kite
Publication Date: 2026.02.04 BOARDS & MORE GMBH
  • EP4323272B1 patent drawingFigure 1
  • EP4323272B1 patent drawingFigure 2~3
  • EP4323272B1 patent drawingFigure 4~5

AI summary

The invention relates to a hand-held wing foil (1) with a spoiler profile (36) that is formed substantially in the lower, tangential flow-receiving region of the leading edge (7). In addition, the invention relates to a kite (101) having a spoiler profile (116) that is formed substantially in the lower, tangential flow-receiving region of the leading edge (103).