Pivotable Vertical Axis Turbine Blades

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Solution Overview

Problem

Existing wind turbines and water wheels with vertical axes face inefficiencies due to complex adjustment mechanisms for optimal angle of attack, leading to wear and increased costs, and suboptimal efficiency when wings are firmly coupled.

Innovation Solution

The blades pivot automatically under flow influence to adjust between larger and smaller contact surfaces, with individual wing control and a cambered profile to enhance efficiency, and are designed with a stop to optimize positioning, allowing for independent alignment and power generation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If adjustment mechanisms are used to optimize the angle of attack of blades, then efficiency is improved, but device complexity increases and wear problems occur

Engineering Contradiction:
ImproveefficiencyVSAvoidcomplexity of adjustment mechanism
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The blade adjusts its own angle of attack automatically through the flow-induced tilting mechanism without external control systems. The flow itself serves as the actuator, eliminating complex adjustment mechanisms while maintaining efficiency optimization

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces mechanical adjustment systems with a flow-driven automatic tilting mechanism. The aerodynamic forces directly control the blade angle, substituting complex mechanical actuators with a simpler fluid-structure interaction system

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

2Productivity

If wings are firmly coupled to arms, then structural simplicity is maintained, but efficiency decreases due to inability to optimize angle of attack

Engineering Contradiction:
ImproveefficiencyVSAvoidcoupling structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The blade is divided into independent rotational segments that can tilt relative to the arm. This segmentation allows each blade to independently optimize its angle of attack while maintaining overall structural integrity, resolving the conflict between simplicity and efficiency

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The coupling between blade and arm is made dynamic rather than fixed. The blade can dynamically adjust its angle through automatic tilting in response to flow conditions, transforming a static simple structure into a dynamic efficient system

Inventive Principle:
Principle #15Dynamics

3Productivity

If blades have symmetric geometry, then manufacturing is simplified, but aerodynamic efficiency is reduced

Engineering Contradiction:
Improveaerodynamic efficiencyVSAvoidblade geometry
Core Design Contradiction:
ProductivityVSEase of manufacture

Solution Approach 1:

The blade cross-section uses asymmetric cambered geometry to optimize aerodynamic performance. The asymmetric shape generates lift forces that improve efficiency, while the manufacturing complexity is managed through the self-adjusting mechanism that reduces the need for precision mechanical control

Inventive Principle:
Principle #4Asymmetry

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 significantly improves efficiency by optimizing wing positioning and reducing resistance, ensuring even operation and enhanced power generation through independent wing alignment and aerodynamic lift.

Implementation Method 1

the wings have a cambered wing profile. As a result, the efficiency can be significantly increased, since in addition to the wind resistance, the aerodynamic lift force on the wing acts in the direction of the rotational movement of the vertical wind wheel axis

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

The center of mass of the wings is preferably outside the pivot axis and is arranged in such a way that the wings automatically tilt from the second position (without the influence of flow) into a rest position with a larger contact surface

Methodology Applied
Scientific EffectGravitational moment: Gravitation

Implementation Method 3

Under the influence of the flow, a tilting moment thus arises, which adjusts the wing in question either in the direction of the first or the second position

Methodology Applied
Scientific EffectFlow-induced tilting moment: Drag

Data Source

PatentEP2078849B1Wind and water turbine with pivotable blades
Publication Date: 2018.08.15 OSTERHAMMER JOHANN JUN
  • EP2078849B1 patent drawingFigure 1
  • EP2078849B1 patent drawingFigure 2

AI summary

The device comprises a rotating axis (2) with one or more arms (3), where wings (4) are arranged at the arms and are supported in a swiveling manner. The wings are inclined in one position with a larger contact surface and inclined in another position with smaller contact surface. A flank area is inclined when it automatically moves into the former position with a stream (10) or in the latter position against the stream.