Cam-Driven Blade Incidence Adjustment for Vertical-Axis Wind Turbines

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Solution Overview

Problem

Vertical-axis wind turbines, particularly of the Darrieus type, face inefficiencies and complex maintenance due to low efficiency, non-constant torque, and difficulty in starting, which limits their widespread adoption compared to horizontal-axis turbines.

Innovation Solution

A rotor turbine generator with a simple mechanism for adjusting blade incidence using a cam and follower system, allowing each blade to adapt its angle optimally relative to the apparent wind throughout its rotation, enhancing efficiency and reducing maintenance complexity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If variable-incidence blade mechanisms are added to vertical-axis wind turbines, then efficiency increases, but device complexity and maintenance requirements increase significantly

Engineering Contradiction:
ImproveefficiencyVSAvoidmechanism complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The cam mechanism is passively driven by the rotor's own rotation, automatically adjusting blade incidence without requiring external power sources, control systems, or active components. The system self-regulates based on rotational position, eliminating the need for complex motorized pitch control while maintaining variable-incidence benefits

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Complex motorized pitch control systems are replaced with a simple cam-follower mechanical linkage. The cam profile geometrically translates rotor position into blade angle adjustments, substituting electronic control and actuators with pure mechanical geometry that requires no power, sensors, or complex control logic

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Adaptability or versatility

If complex variable-incidence mechanisms are implemented, then blade orientation optimizes, but ease of manufacture and maintenance deteriorate

Engineering Contradiction:
Improveblade orientation optimizationVSAvoidmanufacturing simplicity
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The incidence adjustment function is extracted from complex motorized systems and isolated into a single cam component. This separates the orientation optimization function from power transmission and control systems, allowing the cam to be manufactured independently as a simple molded or machined part with a predetermined profile, significantly easing manufacturing

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The cam profile is designed with specific geometric parameters that directly correspond to desired blade incidence angles at different rotor positions. By changing the cam profile geometry (radius, curvature, pitch), the entire orientation optimization characteristic changes without altering other system components, simplifying design iterations and manufacturing

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If traditional Darrieus rotor design is used, then vertical-axis operation is achieved, but efficiency remains low due to non-constant torque and difficulty starting

Engineering Contradiction:
Improvevertical-axis operationVSAvoidefficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

The cam mechanism dynamically adjusts blade incidence throughout the rotation cycle, transforming the static blade geometry into a dynamic system that adapts to changing flow conditions. This creates favorable torque characteristics during critical phases of rotation, smoothing out torque fluctuations and improving overall efficiency while maintaining vertical-axis operation

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The cam profile is designed to set optimal blade incidence angles in advance for each rotor position, including pre-positioning blades for maximum torque generation during the power stroke and minimizing drag during reverse flow portions. This preliminary geometric preparation ensures efficient operation throughout the cycle without requiring real-time control adjustments

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

The solution increases the efficiency of vertical-axis wind turbines by optimizing blade incidence relative to the apparent wind, reducing maintenance needs, and lowering costs, making them more viable for electricity generation and water pumping.

Implementation Method 1

the Darrieus type wind turbine is based on the lift effect undergone by a profile subjected to the action of an apparent wind

Methodology Applied
Scientific EffectLift effect: Aerofoil

Data Source

PatentEP2572100B1Turbogenerator with rotor having blades adapting to the apparent wind
Publication Date: 2016.03.09 NOTTEGHEM BERNARD
  • EP2572100B1 patent drawingFigure 1~3
  • EP2572100B1 patent drawingFigure 2~4
  • EP2572100B1 patent drawingFigure 5

AI summary

The invention relates to a turbogenerator (1) comprising a mounting (6) and a rotor (2) that can be pivoted around a main axis (5) in relation to said mounting (6) and that is provided with at least two blades (3) that are each pivotably mounted around a secondary axis (33) on at least one base (4) coupled with said rotor (2). Said turbogenerator is characterized in that it comprises a means (10) for adjusting the angle of attack of said blades (3), said setting means including at least one cam (101) and at least one follower member (102) that is rigidly connected to each of said blades (3) and is capable of engaging with said cam (101) so as to separately set each of said blades (3). Said cam (101) is shaped so as to enable the selected optimal angle of attack of each of said blades (3) to be adapted in relation to the relative wind (Va), at each point (P1-P18) of the circle (34) covered by said secondary axis (33) of each blade (3) during the rotation of said rotor (2) around the main axis (5) thereof, for a defined ratio between the values of the true wind (Vr) and the linear wind (Vd) that is generated by the movement of said blades (3).