Wind Turbine Rotor Blade Installation Angle Optimization

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Solution Overview

Problem

Long rotor blades in wind turbines face challenges in maintaining optimal aerodynamic performance and weight efficiency, particularly in varying wind conditions, as increased length and stiffness lead to higher weight and potential flow separation issues.

Innovation Solution

The rotor blade design features a progressive installation angle that decreases from the root, increases in the central region, and then decreases again towards the tip, allowing for a constant angle of attack and reducing the risk of flow separation by displacing high relative profile thicknesses towards the tip, thereby optimizing weight and structural properties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If the length of rotor blades is increased to improve power generation at locations with small average wind speeds, then the power generation capability is improved, but the weight of the rotor blade increases significantly

Engineering Contradiction:
Improvepower generation capabilityVSAvoidrotor blade weight
Core Design Contradiction:
PowerVSWeight of moving object

Solution Approach 1:

The patent applies local quality by varying the profile thickness distribution along the rotor blade length. The relative profile thickness is increased in specific regions (particularly in the outer 20-30% of the blade length) while maintaining thinner sections in other areas. This localized thickening provides structural reinforcement exactly where needed for long blades, improving power generation capability without proportionally increasing overall blade weight.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs parameter changes by systematically varying the relative profile thickness as a function of the normalized radius along the blade. The relative profile thickness changes from 0.15-0.25 in inner regions to 0.30-0.45 in outer regions, creating an optimized weight-strength distribution that enables longer blades to generate more power without excessive weight increase.

Inventive Principle:
Principle #35Parameter changes

2Strength

If the stiffness of rotor blades is increased to maintain structural integrity, then the structural strength is improved, but the weight of the rotor blade increases

Engineering Contradiction:
Improvestructural strengthVSAvoidrotor blade weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent applies local quality by concentrating increased profile thickness in the outer regions of the blade where bending moments and structural demands are highest. This localized reinforcement provides the necessary structural strength while avoiding unnecessary material in regions with lower stress, thereby minimizing weight increase.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent utilizes composite material structures with the varied profile thickness design, combining different material properties and thickness distributions to achieve high structural strength with optimized weight. The composite construction allows for strategic placement of material where it provides maximum structural benefit.

Inventive Principle:
Principle #40Composite materials

3Strength

If the relative profile thickness is increased in certain regions, then the structural properties are improved, but the angle of attack must be reduced to prevent flow separation

Engineering Contradiction:
Improvestructural propertiesVSAvoidangle of attack range
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The patent applies local quality by implementing region-specific profile thickness variations that correspond to different aerodynamic requirements. In regions with increased relative profile thickness, the installation angle is adjusted locally to prevent flow separation, while maintaining optimal angles in other regions. This localized adaptation allows the blade to maintain both structural integrity and aerodynamic efficiency.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs dynamic adaptation through pitch control mechanisms that can adjust the installation angle in real-time based on operating conditions. This dynamic adjustment compensates for the constraints imposed by varied profile thickness distribution, allowing the blade to optimize its angle of attack across different wind speeds and operational states.

Inventive Principle:
Principle #15Dynamics

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 design enables the creation of longer, lighter rotor blades with improved aerodynamic performance and reduced structural loads, preventing flow separation and allowing for reduced pitch angles during operation, thus enhancing the efficiency and durability of wind turbines.

Implementation Method 1

The aerodynamic properties of a rotor blade substantially depend on the shape, that is to say the geometry, of the profile of the rotor blade. In operation, air flows around the profile. Here, the resulting direction from which the air strikes the profile front edge is referred to as incident direction. The angle between the profile chord and the incident direction is referred to here as angle of attack of the profile. The local angle of attack determines the local lift and resistance of the rotor blade.

Methodology Applied
Scientific EffectAerodynamic lift and resistance: Aerofoil

Implementation Method 2

it is also expedient to change the shape of the profile section with increasing radius, that is to say adapt it to the changing rotational speed. A profile is designed in terms of a certain operating range in which the profile is intended to work. Here, the operating range is characterized, inter alia, by the incident speed to be expected. The profile is also designed in terms of a maximum angle of attack.

Methodology Applied
Scientific EffectFlow separation: Flow Separation

Data Source

PatentUS11454206B2Rotor blade for a wind turbine
Publication Date: 2022.09.27 WOBBEN PROPERTIES GMBH
  • US11454206B2 patent drawing
  • US11454206B2 patent drawing
  • US11454206B2 patent drawing

AI summary

A rotor blade of an aerodynamic rotor of a wind turbine having a rotor axis of rotation and an outer radius, comprising a blade root for fastening to a rotor hub, a blade tip which faces away from the blade root, a blade longitudinal axis which extends from the blade root to the blade tip, a blade front edge which faces toward the front in the direction of movement of the rotor blade, a blade rear edge which faces toward the rear in the direction of movement of the rotor blade, and profile sections which change along the blade longitudinal axis, wherein each profile section has a profile chord which extends from the blade front edge to the blade rear edge, and each profile chord has an installation angle as an angle in relation to a rotor plane, wherein the installation angle from the blade root to the blade tip first decreases in a blade inner region oriented toward the blade root, increases again in a blade central region and decreases again in a blade tip region oriented toward the blade tip. A rotor of a wind turbine and to a corresponding wind turbine.